ad-pa compliance status report i-dpcc...s tcca cf-92-22 faa 94-04-02 tcca cf-2003-02 bombardier...
TRANSCRIPT
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCC s/n 2066
Delivery Date: Dec 07
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 1
pag. 1 of 4 S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCC Compliance Status
A N FAA
77-17-13 - - - - NLG DOORS
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N FAA
77-13-05 - - - -
MISSING RIVETS IN BULKHEAD
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N TCCA
CF-90-11R2 FAA 93-16-06R2
Bombardier SB215-A435
SoREM Scheda analisi AD
JUNE. 10, 1994 N/A
RUDDER-AILERON INTERCONNECT TAB (TO PREVENT POSSIBILE
FLUTTER)
CLOSED: NOT EFFECTIVE AS PER POWERED AILERON
SYSTEM INSTALLED
S TCCA
CF-92-22
FAA 94-04-02 TCCA CF-2003-
02
Bombardier SB215-A3040
SoREM Scheda analisi AD
- N/A ENGINE REAR
MOUNT STRUTS
CLOSED: SUPERSEDED BY AD CF-2003-02
I Y ENAC 95-064
TCCA CF-92-10R1
P&WC: SB20914 SB21113 SB21211 SB21314
Bombardier SB215-A3060
SoREM Scheda Analisi PA
N/A ENGINE FIRE-WIRE DETECTION LOOP
CLOSED: AD COMPLIED WITH
ENGINE FIRE DETECTION SYSTEM CONNECTED TO AIRCRAFT FIRE WARNING
SYSTEM
I Y FAA
97-11-08 - - - -
AFM - LIMITATION SECTION - POWER
LEVERS
CLOSED: AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION SECTION
PAGE 8
A N TCCA
CF-96-02R1 ENAC 1999-268 - - - -
CLOSED: AD ISSUED JUST TO CANCEL PREVIOUS REVISION
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCC s/n 2066
Delivery Date: Dec 07
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 1
pag. 2 of 4 S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCC Compliance Status
R N ENAC 00-265
FAA 2004-03-13 - - - MLG AXLES NOT APPLICABLE AS PER AD
EFFECTIVITY
A N TCCA
CF-2002-14 FAA 2004-26-08
ENAC 02-167
Bombardier SB215-4234
SoREM DT CL-61-4234
MARCH 04, 2003 N/A PCU BACKUP
PRESSURE VALVE
NOT APPLICABLE AS PER VALVE INCORPORATED AT
MANUFACTURE
R N ENAC 00-496
FAA 2002-12-12 - - - WING TO FUSELAGE
FRAME ANGLES NOT APPLICABLE AS PER AD
EFFECTIVITY
S - FAA
2003-04-06 ENAC 03-067
FAA 2006-22-05
SoREM
DT-CL-34-05 DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II
RNZ-850/ -851
REF TO COMPONENTS
SUPERSEDED BY FAA 2006-22-05
R Y TCCA
CF-2003-02 FAA 2004-10-04
ENAC 03-251
Bombardier SB215-A4287R2
SoREM BM-CL-71-A4287
BM-CL-71-A4287R2 SMJC 31 and 32
WITHIN 50 F/H SINCE FEBRUARY
28, 2003
EVERY 250 F/H REPETITIVE ACTION
FOLLOWED BY SoREM SMJC #31 and #32
ENGINE REAR MOUNT STRUTS
OPEN: CARRIED OUT WITH SMJC 31 & SMJC 32 ON 29/08/2011 (W/O
11/308); 194.25 FH TO GO
28/09/2003
R Y FAA
2004-21-05 -
SCHEDA ANALISI Disposizione Tecnica
DT-CL-21-01
A 500 heater Hrs Total or 100 heater hrs TIS from 19/11/04
(whichever occurs later)
100 Hrs funzion. 24 Months
PRESSURE DECAY TEST and CABIN
HEATER (JANITROL)
OPERATIONAL TEST
REF TO COMPONENTS
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCC s/n 2066
Delivery Date: Dec 07
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 1
pag. 3 of 4 S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCC Compliance Status
A N FAA
2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
REGOLATORE CARBURANTE CON VALVOLE SHUTOFF
A/B/C 14D11 o A/B/C/P 23D04
REF TO COMPONENTS
R N FAA
2005-18-05 - - - -
LOWER CAPS OF THE WING FRONT SPAR AND
REAR SPAR
CLOSED NOT APPLICABLE AS PER AD EFFECTIVITY
A N EASA
2006-0375 - Scheda Analisi AD Dec. 29, 2006 -
CARLING TECHNOLOGIES
SWITCHES
CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY
N N FAA
2006-22-05 EASA 2006-479 Scheda Analisi AD - N/A
INTEGRATED NAVIGATION UNITS
REF TO COMPONENTS
Supersedes FAA 2003-04-06
R Y TCCA
CF-2008-29 FAA 2009-05-04 ENAC 2008-316
SMJC-60 Mar 8, 2009
BEFORE AND AFTER EVERY FIRE SEASON
OR AT SIX MONTH INTERVAL,
WHICHEVER IS SHORTER TIME
PERIOD
RUDDER LOWER TORQUE TUBE UPPER BEARING
OPEN: AD COVERED BY SMJC 60 CARRIED OUT ON 04/04/2011(W/O
11/019 ADD 2) EXPIRED OCT 03, 11
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCC s/n 2066
Delivery Date: Dec 07
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 1
pag. 4 of 4 S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCC Compliance Status
R Y TCCA
CF-2010-38R2 ENAC 2011-88
Bombardier SB 215 -A4424 Jun 01, 2011
FIRST INSPECTION WITHIN 50 FC FROM
20 DEC 2010; THEREAFTER REPEAT
PERRFORM AN INSPECTION BEFORE
100 FC WITH TERMINATING ACTION NOT LATER THAN Jun
01, 2011.
INSPECTION OF THE EMERGENCY WATER DUMP
PULLEY BRACKET AND STRUCTURE
CLOSED SB 215-A4424 PART B EMBODIED ON 01/06/2011 (W/0 11/019 ADD 2)
R Y TCCA
CF-2011-35
Bombardier SB 215-A4450;
Bombardier SB 215-A4451
ESB-4-32-A4450 Rev 01;
ESB-4-32-A4451 Rev 01;
Ref. To AD-PA Compliance Components
Ref. To AD-PA Compliance Components
Liquid Penetrant & Eddy Current Inspection on MLG Upper Member
Forward Lug
REF. TO AD-PA COMPLIANCE COMPONENTS
EASA/TCA/FAA/ENAC
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0086 Manuf. date:
AUG 2001
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 2
pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance AF0086.doc
I Y TCA
CF-90-21 -
P&WC SB20355R1
SB20897 30/04/91 N/A
O-RING DETERIORATION DURING FUEL FILTER COVER INSTALLATION
- CLOSED - AD COMPLIED WITH AT
DELIVERY
I Y TCCA
CF-90-22R1 RAI 91-296
P&WC SB21018R1
30/06/94 N/A OIL SYSTEM INSPECTION
DUE TO BEARING DETERIORATION
- CLOSED - AD COMPLIED WITH AT
DELIVERY
A N TCA
CF-91-02 -
P&WC SB20946R1
31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS
- CLOSED – N/A DUE TO ENGINE S/N AD COMPLIED WITH AT
DELIVERY
I Y TCCA
CF-91-26R1 RAI 91-347
P&WC SB20914R3
SB21053 31/03/92 N/A
TO IMPROVE THE RETENTION OF THE
P2.5/P3 TUBE ASSEMBLY.
- CLOSED - AD COMPLIED WITH AT
DELIVERY
S Y TCCA
CF-92-03R1 RAI 93-284 - - N/A
INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
- CLOSED – SUPERSEDED BY TCCA CF-92-03R2
I Y TCA
CF-92-03R2 -
P&WC SB20957R3 SB20962R2
SB21065
30/06/94 N/A INTERNAL OIL FIRES IN
THE ICC.
- CLOSED - AD COMPLIED WITH AT
DELIVERY
EASA/TCA/FAA/ENAC
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0086 Manuf. date:
AUG 2001
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 2
pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance AF0086.doc
A N TCCA
CF-94-01
FAA 94-03-02 Amdt 39-8808
RAI 94-001 P&WC SIL 307
Since 14/01/94
1000⇔2000 cycles N/A
REPLACEMENT HP TURBINE DISK
- CLOSED - NOT EFFECTIVE FOR
ENGINES S/N 109022 AND SUBSEQUENT
I Y TCCA
CF-96-22 ENAC 96-353
P&WC SB21077R7 SB21364R1 SB21373R3
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
- CLOSED - ALL SBs RELATED TO AD
EMBODIED AD COMPLIED WITH
A N TCCA
CF-2000-34 FAA 2003-16-04
ENAC 01-065 P&WC
SB 21100R2
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES
FUEL HEATERS
- CLOSED – NOT APPLICABLE FOR
ENGINES S/N 109036 AND SUB’S
A N TCCA
CF-2002-10 ENAC 02-090
- CLOSED – N/A AS PER ENGINE MODEL
I Y TCCA
CF-2002-34 FAA 2004-20-01
ENAC 02-448
P&WC SB21562R0/R1/R2
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within 2400 f/h
or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
- CLOSED - POST SB21562
28/09/2003
EASA/TCA/FAA/ENAC
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0094 Manuf. date:
DEC 2006
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 2
pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCC Left Engine
I Y TCCA
CF-90-21 -
P&WC SB20355R1
SB20897 30/04/91 N/A
O-RING DETERIORATION DURING FUEL FILTER COVER INSTALLATION
- CLOSED - AD COMPLIED WITH AT
DELIVERY
I Y TCCA
CF-90-22R1 RAI 91-296
P&WC SB21018R1
30/06/94 N/A OIL SYSTEM INSPECTION
DUE TO BEARING DETERIORATION
- CLOSED - AD COMPLIED WITH AT
DELIVERY
A N TCCA
CF-91-02 -
P&WC SB20946R1
31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS - CLOSED –
N/A DUE TO ENGINE S/N
I Y TCCA
CF-91-26R1 RAI 91-347
P&WC SB20914R3
SB21053 31/03/92 N/A
TO IMPROVE THE RETENTION OF THE
P2.5/P3 TUBE ASSEMBLY.
- CLOSED - AD COMPLIED WITH AT
DELIVERY
S TCCA
CF-92-03R1 RAI 93-284 - - N/A
INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
- CLOSED – SUPERSEDED BY TCCA CF-92-03R2
I Y TCCA
CF-92-03R2 -
P&WC SB20957R3 SB20962R2
SB21065
30/06/94 N/A INTERNAL OIL FIRES IN
THE ICC.
- CLOSED - AD COMPLIED WITH AT
DELIVERY
EASA/TCA/FAA/ENAC
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0094 Manuf. date:
DEC 2006
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 2
pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCC Left Engine
A N TCCA
CF-94-01
FAA 94-03-02 Amdt 39-8808
RAI 94-001 P&WC SIL 307
Since 14/01/94
1000⇔2000 cycles N/A
REPLACEMENT HP TURBINE DISK
- CLOSED – NOT EFFECTIVE FOR
ENGINES S/N 109022 AND SUBSEQUENT
I Y TCCA
CF-96-22 ENAC 96-353
P&WC SB21077R7 SB21364R1 SB21373R3
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
- CLOSED - ALL SBs RELATED TO AD
EMBODIED AD COMPLIED WITH
A N TCCA
CF-2000-34 FAA 2003-16-04
ENAC 01-065 P&WC
SB 21100R2
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES
FUEL HEATERS
- CLOSED – NOT EFFECTIVE FOR
ENGINES S/N 109036 AND SUB’S
A N TCCA
CF-2002-10 ENAC 02-090
P&WC SB 21914R4
Next shop visit or before 31/12/03
Whichever occurs first
N/A PW118, PW120 and PW121
INTERCOMPRESSOR CASE FIRE
- CLOSED – N/A AS PER ENGINE MODEL
I Y TCCA
CF-2002-34 FAA 2004-20-01
ENAC 02-448
P&WC SB21562R0/R1/R2
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within 2400 f/h
or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
- CLOSED - POST SB21562
28/09/2003
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
20070112 Manuff. date:
JAN 2007
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 2
pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance 200707112
I Y FAA
93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided
transfer tube
- CLOSED – AD COMPLIED WITH
P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs.
PCU INSPECTION/ MODIFICATION
OPEN: PCU COMPLIANT WITH HS-SB14SF-61-82.
CHECK COVERED BY O/H PROCEDURE (TTG 1177.30 FH – REF. TO ENG AF0086)
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
- CLOSED – NOT APPLICABLE FOR
BLADE #1 S/N 2007010567
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
- CLOSED – NOT APPLICABLE FOR
BLADE #2 S/N 2007010568
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
- CLOSED – NOT APPLICABLE FOR
BLADE #3 S/N 2007010569
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
- CLOSED – NOT APPLICABLE FOR
BLADE #4 S/N 2007010822
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
20070112 Manuff. date:
JAN 2007
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 2
pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance 200707112
R Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE INSPECTED DURING LAST
O/H (TTG 633.10 FH)
R Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: ACTUATOR INSPECTED DURING LAST
O/H (TTG 633.10 FH)
R Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: PCU INSPECTED DURING LAST SHOP VISIT
(TTG 1177.30 FH)
28/09/2003
A N FAA
2006-24-07 Scheda Analisi PA Jan 3, 2007
- CLOSED – NOT APPLICABLE AS PER
PROPELLER MODEL
A N FAA
US-2011-04-02 ENAC 2011-68 ADE issued Apr 15, 2011
NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
20070111 Manuf. date:
JAN 2007
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 2
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance 20070111.doc
I Y FAA
93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrated
transfer tube
- CLOSED – AD COMPLIED WITH
P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs
PCU INSPECTION/ MODIFICATION
OPEN: PCU COMPLIANT WITH HS-SB14SF-61-82.
CHECK COVERED BY O/H PROCEDURE (TTG 197.10 FH – REF.TO ENG AF0094)
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97
500 cycles up-to incorporating of HS SB 14SF-61-A92
BLADE INSPECTION / MODIFICATION
- CLOSED – NOT APPLICABLE FOR
BLADE #1 S/N 2007010564
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97
500 cycles up-to incorporating of HS SB 14SF-61-A92
BLADE INSPECTION / MODIFICATION
- CLOSED – NOT APPLICABLE FOR
BLADE #2 S/N 2007010565
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
- CLOSED – NOT APPLICABLE FOR
BLADE #3 S/N 2007010566
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
- CLOSED – NOT APPLICABLE FOR
BLADE #4 S/N 2006070373
I Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE INSPECTED DURING LAST
O/H (TTG 633.25 FH)
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
20070111 Manuf. date:
JAN 2007
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 2
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance 20070111.doc
I Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: ACTUATOR INSPECTED DURING LAST
O/H (TTG 633.25 FH)
I Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: PCU INSPECTED DURING LAST O/H
(TTG 197.10 FH)
28/09/2003
A N FAA
2006-24-07 Scheda Analisi PA Jan 3, 2007
- CLOSED – NOT APPLICABLE AS PER
PROPELLER MODEL
A N FAA
US-2011-04-02 ENAC 2011-68 ADE issued Apr 15, 2011
NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCC s/n 2066
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 1
pag. 1 of 9 S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCC Components Compliance Status
A N FAA
81-21-05 - - Nov 19, 1981 N/A
ARTEX ELT Battery not usable in salt environment
CLOSED: NOT APPLICABLE – SUBJECT ELT BATTERY NOT
INSTALLED
A N TCCA
CF-96-21
FAA 72-19-04 Amdt. 39-1782
RAI 74-225 - N/A N/A
Ni-Cd batterie con celle in polistirolo
CLOSED: NOT APPLICABLE - TEMPERATURE SENSING
INSTALLED ON BATTERIES EMBODIED
S - RAI
82-113 - - - - -
CLOSED: SUPERS. BY ENAC 96-348
N N TCCA
CF-96-21
FAA 72-19-04 Amdt. 39-1782 - N/A N/A Ni-Cd batteries
CLOSED: CF96-21 ISSUED TO CANCEL THE APPLICABILITY OF
FAA 72-19-04
S - RAI
88-052 - - - - - SUPERS. BY ENAC 88-096
R Y RAI
88-096 FAR 43
Appendix E Norma di lavoro
NL-CL-34-06 19/11/2005 24 Months
ALTIMETER AND STATIC PRESSURE SYSTEM
OPEN: TEST CARRIED OUT ON 13/05/2011 (W/O 11/019 ADD 2) (NEXT DUE WITHIN 12/05/2013)
I Y ENAC 96-052
FAA FAR 91.21 - N/A N/A USE OF PORTABLE
ELETTRONIC DEVICES CLOSED: AFM UPDATED – CREW
INFORMED
N N ENAC 96-348
FAA 96-20-07 Amdt 39-9773 -
Within 500 Hrs (TIS) or 12 mths from 14/11/96
100 Hrs funzion. 24 Months
COMBUSTION CHAMBER DECAY TEST (JANITROL)
CLOSED: NOT APPLICABLE - HEATER MODEL B4500
(CERAMIC COMBUSTION TUBE) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCC s/n 2066
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 1
pag. 2 of 9 S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCC Components Compliance Status
N N ENAC 97-167
FAA 97-11-10 - - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N TCCA
CF-95-16 ENAC 97-221
Marathon Power SB 111692-014
27/07/96 N/A PCB SERIES PC-250 MODIFICATION OR
REMOVAL
CLOSED: NOT APPLICABLE AS PER INVERTER INSTALLED
(Serie MSI-800)
N N ENAC 97-274
FAA 97-18-03 - - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - AVOX OXYGEN MASKS
INSTALLED
N N ENAC 99-231
FAA 99-08-21 - - N/A
PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - AVOX OXYGEN MASKS
INSTALLED
S - ENAC 00-018
FAA 99-23-22 Norma di Lavoro
NL-CL-34-07 Apr 17, 2000 Every 90 days TRANSPONDER MODO
“C” INSPECTION/TEST
CLOSED: SUPERSEDED BY ENAC 00-209
N N ENAC 00-209
FAA 99-23-22 Amdt. 39-11686
Engineering Instruction
EI 004/00 18/05/00 N/A
TRANSPONDER MODO “C”
CLOSED: NOT APPLICABLE AD RESCINDED APR. 12, ‘00
SUPERSEDES ENAC 00-018
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCC s/n 2066
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 1
pag. 3 of 9 S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCC Components Compliance Status
S - ENAC 01-173
FAA 2001-08-01 Scheda Analisi PA May 2, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04
CLOSED: SUPERSEDED BY ENAC 01-368
A N ENAC 01-368
FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
P/N installed on A/C: J20C30
CLOSED: NOT APPLICABLE AS PER FUEL SHUT-OFF P/N
INSTALLED Supersedes ENAC 01-173
N N ENAC 01-442
FAA 2001-18-05 - Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.
CLOSED: NOT APPLICABLE PER P/N
I Y ENAC 01-470
FAA 2001-22-14 SoREM
DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER
DISCHARGER
CLOSED: P/N AFFECTED CHECKED. WALTER KIDDE
CARTRIDGES INSTALLED ON
I Y TCCA
CF-2002-14 ENAC 02-167
BOMBARDIER SB215-3108 SB215-4234
SoREM BM-CL-61-4234
04/03/2003 N/A
PROPELLER CONTROL UNIT
BACKUP PRESSURE RELIEF VALVE
CLOSED: SB 215-4234 INCORPORATED
I Y ENAC 03-067
FAA 2003-04-06 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II
RNZ -850/ -851
CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND
7510100-731 (#2) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCC s/n 2066
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 1
pag. 4 of 9 S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCC Components Compliance Status
28/09/2003
N N FAA
2003-23-05 ENAC 2004-003 ENAC-2004-073
- December 24, 2005 N/A Titeflex Corporation,
Tubi Flessibili
CLOSED: NOT APPLICABLE
HOSES INSTALLATI P/N 114040-4
R Y FAA
2004-21-05 Amdt.39-13826
- Scheda Analisi PA DT-CL-21-01
A 500 heater Hrs or 100 heater Hrs TIS
since 19/11/04 (whichever occurs
later)
100 Hrs (TIS) or
24 Months
PRESSURE DECAY TEST ed Operational Test del
CABIN HEATER (JANITROL)
OPEN: HEATER TIME IN SERVICE CHECKED:
60,35 HOURS TEST NOT YET PERFORMED
A N FAA
2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
CLOSED: NOT APPLICABLE AS PER HEATER INSTALLED
R Y EASA
2006-0265 -
Scheda Analisi PA ESP-4-34-001
Within Mar 13, 2007
24 Months MODE “S” and “C”
TRANSPONDERS CHECK
OPEN: CARRIED OUT DURING ANNUAL
CHECK ON 6/6/2011 (W/O 11/019)
NEXT DUE WITHIN 5/06/2013
A N EASA
2006-0269 - Scheda Analisi PA - -
MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
A N FAA
2006-18-08 - Scheda Analisi AD Oct. 11, 2006 -
GOODYEAR NOSE WHEEL TIRES
CLOSED: NOT APPLICABLE AS PER
GOODYEAR TIRES NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCC s/n 2066
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 1
pag. 5 of 9 S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCC Components Compliance Status
A N FAA
2006-19-04 - Scheda Analisi AD - -
MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER PART NUMBER NOT
INSTALLED
N N FAA
2006-22-05 ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU
CLOSED: NOT APPLICABLE AS PER
COMPONENT MODIFIED (REF TO
FAA-2003-04-06)
A N EASA
2006-0366 - Scheda Analisi PA Dec 14, 2006 - LIFE RAFT
CLOSED: NOT APPLICABLE AS PER
AIRCRAFT MODEL
A N EASA
2006-0286R1 - Scheda Analisi PA Sep 9, 2006 - Oxygen Cylinders
CLOSED: NOT APPLICABLE: P/N NOT
INSTALLED
A N EASA
2007-0256 - Scheda Analisi PA Sep 19, 2007 - Seat Restraint System
CLOSED: NOT APPLICABLE: P/N NOT
INSTALLED
A N EASA
2007-0294 ENAC 2009-060 Scheda Analisi PA - -
APU Turbine wheel life limit reduction
CLOSED: NOT EFFECTIVE AS PER
APU NOT INSTALLED ON SOREM CL415
FLEET
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCC s/n 2066
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 1
pag. 6 of 9 S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCC Components Compliance Status
N N EASA
2009-0200 - Scheda Analisi AD Sep 22, 2010 N/A
Navigation – Mode A/C Transponder – Check /
Modification
CLOSED: NOT EFFECTIVE: P/N NOT
INSTALLED
N N FAA
2009-20-10 - Scheda Analisi AD Jan 17, 2010 N/A
Autopilot – servo motors modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
S - CF 2009-42 - SOREM ESB-4-32-4414
(SMJC 063)
Part I within 50Fh Part II: within 750 Fc Part III: every 750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
CLOSED: SUPERSEDED BY CF
2009-42R1 (PART I CARRIED OUT ON NOV
26, 2009)
R Y CF 2009-42R1 - SOREM ESB-4-32-
4414R1 - Every 750 Flight
cycles Special Inspection of
Accumulator Screw Caps
OPEN: AD COVERED BY SMJC-63
PERFORMED ON 20/04/2011 (W/O 11/019 ADD 2) 668 FC TO GO
A N EASA
2009-0251 - Scheda Analisi AD Nov 26, 2009 N/A
Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE: S/N NOT
INSTALLED
A N EASA
2009-0262R1 Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A
Portable Halon 1211 Fire Extinguisher
NOT EFFECTIVE: S/N NOT INSTALLED
A N EASA
2009-0278 - Scheda Analisi AD Jan 22, 2010 N/A
Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCC s/n 2066
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 1
pag. 7 of 9 S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCC Components Compliance Status
N N TCA
CF-2009-44 - Scheda Analisi AD Jul 01, 2011 N/A
ELT-Potential Failure to Transmit the Required 406MHz Coded Signal
CLOSED: NOT EFFECTIVE: P/N NOT
INSTALLED
N N EASA
2010-003R1 - Scheda Analisi AD 18 Apr, 2010 N/A
TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE : P/N NOT
INSTALLED
Y N EASA
2010-0062R1 - Scheda Analisi AD 14 Apr 2010 N/A
Portable Halon 1211 Fire Extinguisher
NOT EFFECTIVE: P/N NOT INSTALLED
A Y FAA
2010-07-02 - Scheda Analisi AD 31 Ott 2012 N/A
Honeywell Primus II RNZ 850()/-851
CLOSED INU #1 AND INU #2
ALREADY MODIFIED”
N N EASA
2010-0067 - Scheda Analisi AD 26 Apr, 2010 N/A
TDR-94 and TDR-94D transponders
CLOSED - NOT EFFECTIVE: P/N NOT
INSTALLED
N N EASA
2010-30 Scheda Analisi SIB N/A N/A
Risks in Transporting Lithium Batteries in Cargo by
Aircraft
CLOSED - NOT APPLICABLE SINCE
INAER FLEET IS NOT OPERATING IN CARGO
TRANSPORT CONFIGURATION
N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer –
Erroneous Airspeed and Altitude Indications
CLOSED - NOT APPLICABLE AS PER A/C TYPE, REFER TO ADE ISSUED DATED
NOV 09, 2010
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCC s/n 2066
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 1
pag. 8 of 9 S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCC Components Compliance Status
N N FAA
2011-01-09 Scheda Analisi AD 9/06/2011 N/R
B/E Aerospace protective breathing equipment P/N 119003-11 inspection for
B/A Aerospace S.B. 119003-35-6 compliance.
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
N N EASA
2011-0043 Scheda Analisi AD 30/04/2013 N/R
Gables Engineering Mode S Transponder Control Panel
Modification
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N EASA
2011-0103 Scheda Analisi AD 03/12/2011 N/R
ELT TRI-BAND Antennas P/N 21-41 ( ) series Mod/Replacement
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N FAA
2011-11-04
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire
Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N EASA
2010-0204 ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A
TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N FAA 2011-14-
08 Scheda Analisi AD
Aug 19,2014 or 6500 FH from Aug
19,2011 N/A
B/E Aerospace pax oxy mask inspection
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCC s/n 2066
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 1
pag. 9 of 9 S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCC Components Compliance Status
R Y TCCA
CF-2011-35 - ESB-4-32-A4451 Rev 01
First incorporation: Within 50 Flight Hrs
upon receipt of Bombardier SB 215-
A4451
To be repeated every 165 land landings
Inspection of the MLG Upper Member forward lug using
eddy current method
FIRST INCORPORATION: CLOSED WITH WO
11/183 ON JUL 22, 11; REPETITIVE ACTION:
OPEN; TO GO: 91 LANDINGS
A Y TCCA
CF-2011-35 - ESB-4-32-A4450 Rev 01 November 11, 2011 N/A
Inspection of the MLG Upper Member forward lug using
liquid penetrant method
OPEN
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCD s/n 2003
Delivery Date: Oct 18, 94
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 4
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCD Compliance Status
A N FAA
77-17-13 - - - - NLG DOORS
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N FAA
77-13-05 - - - -
MISSING RIVETS IN BULKHEAD
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N TCCA
CF-90-11R2 FAA 93-16-06R2
Bombardier SB215-A435
SoREM Scheda analisi AD
JUNE. 10, 1994 N/A
RUDDER-AILERON INTERCONNECT TAB (TO PREVENT POSSIBILE
FLUTTER)
CLOSED: NOT EFFECTIVE AS PER POWERED AILERON
SYSTEM INSTALLED
S TCCA
CF-92-22
FAA 94-04-02 TCCA CF-2003-
02
Bombardier SB215-A3040
SoREM Scheda analisi AD
- N/A ENGINE REAR
MOUNT STRUTS
CLOSED: SUPERSEDED BY AD CF-2003-02
I Y ENAC 95-064
TCCA CF-92-10R1
P&WC: SB20914 SB21113 SB21211 SB21314
Bombardier SB215-A3060
SoREM Scheda Analisi PA
N/A ENGINE FIRE-WIRE DETECTION LOOP
CLOSED: AD COMPLIED WITH ENGINE FIRE DETECTION SYSTEM CONNECTED TO AIRCRAFT FIRE WARNING
SYSTEM
I Y FAA
97-11-08 - - - -
AFM - LIMITATION SECTION - POWER
LEVERS
CLOSED: AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION
SECTION PAGE 8
A N TCCA
CF-96-02R1 ENAC 1999-268 - - - -
CLOSED: AD ISSUED JUST TO CANCEL PREVIOUS REVISION
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCD s/n 2003
Delivery Date: Oct 18, 94
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 4
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCD Compliance Status
R N ENAC 00-265
FAA 2004-03-13 - - - MLG AXLES CLOSED: NOT APPLICABLE AS
PER AIRCRAFT S/N
A N TCCA
CF-2002-14 FAA 2004-26-08
ENAC 02-167
Bombardier SB215-4234
SoREM DT CL-61-4234
MARCH 04, 2003 N/A PCU BACKUP
PRESSURE VALVE
CLOSED: NOT APPLICABLE AS PER AIRCRAFT AND ENGINE
SERIAL NUMBERS
R N ENAC 00-496
FAA 2002-12-12 - - - WING TO FUSELAGE
FRAME ANGLES CLOSED: NOT APPLICABLE AS
PER AIRCRAFT S/N
S - FAA
2003-04-06 ENAC 03-067
FAA 2006-22-05
SoREM
DT-CL-34-05 DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II
RNZ-850/ -851 CLOSED: SUPERSEDED BY
FAA 2006-22-05
R Y TCCA
CF-2003-02 FAA 2004-10-04
ENAC 03-251
Bombardier SB215-A4287R2
SoREM BM-CL-71-A4287
BM-CL-71-A4287R2 SMJC 31 and 32
WITHIN 50 F/H SINCE FEBRUARY
28, 2003
EVERY 250 F/H REPETITIVE ACTION
FOLLOWED BY SoREM SMJC #31 and #32
ENGINE REAR MOUNT STRUTS
OPEN: CARRIED OUT WITH SMJC 31 & SMJC 32 WO 10/080 – 74 FH
TO GO
28/09/2003
R Y FAA
2004-21-05 -
SCHEDA ANALISI Disposizione Tecnica
DT-CL-21-01
A 500 heater Hrs Total or 100 heater hrs TIS from 19/11/04
(whichever occurs later)
100 Hrs funzion. 24 Months
PRESSURE DECAY TEST and CABIN
HEATER (JANITROL)
OPERATIONAL TEST
REF TO COMPONENTS
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCD s/n 2003
Delivery Date: Oct 18, 94
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 3 of 4
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCD Compliance Status
A N FAA
2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
REGOLATORE CARBURANTE CON VALVOLE SHUTOFF
A/B/C 14D11 o A/B/C/P 23D04
REF TO COMPONENTS
R N FAA
2005-18-05 - - - -
LOWER CAPS OF THE WING FRONT SPAR AND
REAR SPAR
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N EASA
2006-0375 - Scheda Analisi AD Dec. 29, 2006 -
CARLING TECHNOLOGIES
SWITCHES
CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY
N N FAA
2006-22-05 EASA 2006-479 Scheda Analisi AD - N/A
INTEGRATED NAVIGATION UNITS
REF TO COMPONENTS
Supersedes FAA 2003-04-06
R Y TCCA
CF-2008-29 FAA 2009-05-04 ENAC 2008-316
SMJC-60 Mar 8, 2009
BEFORE AND AFTER EVERY FIRE SEASON
OR AT SIX MONTH INTERVAL,
WHICHEVER IS SHORTER TIME
PERIOD
RUDDER LOWER TORQUE TUBE UPPER BEARING
OPEN: TO BE CARRIED OUT ON MAR 28,
11 (AD COVERED BY SMJC 60) INAER W.O. 11/017
NEXT DUE WITHIN SEP 27, 11
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCD s/n 2003
Delivery Date: Oct 18, 94
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 4 of 4
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCD Compliance Status
R Y TCCA
CF-2010-38R2 ENAC 2011-88
Bombardier SB 215 -A4424 Jun 01, 2011
FIRST INSPECTION WITHIN 50 FC FROM
20 DEC 2010; THEREAFTER REPEAT
PERRFORM AN INSPECTION BEFORE
100 FC WITH TERMINATING ACTION NOT LATER THAN Jun
01, 2011.
INSPECTION OF THE EMERGENCY WATER
DUMP PULLEY BRACKET AND STRUCTURE
OPEN PART A TO BE ACCOMPLISHED
WITH SMJC-062 PLANNED TERMINATING ACTION PART B INCLUDED IN W.O. 11/017
PERFORMED APR 18, 11
R Y TCCA
CF-2011-35
Bombardier SB 215-A4450;
Bombardier SB 215-A4451
ESB-4-32-A4450 Rev 01;
ESB-4-32-A4451 Rev 01;
Ref. To AD-PA Compliance Components
Ref. To AD-PA Compliance Components
Liquid Penetrant & Eddy Current Inspection on MLG Upper Member
Forward Lug
REF. TO AD-PA COMPLIANCE COMPONENTS
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCD s/n 2003
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCD Components Compliance Status
A N FAA
81-21-05 - - Nov 19, 1981 N/A
ARTEX ELT Battery not usable in salt environment
CLOSED: NOT APPLICABLE – SUBJECT ELT BATTERY NOT
INSTALLED
A N TCCA
CF-96-21
FAA 72-19-04 Amdt. 39-1782
RAI 74-225 - N/A N/A
Ni-Cd batterie con celle in polistirolo
CLOSED: NOT APPLICABLE - TEMPERATURE SENSING
INSTALLED ON BATTERIES EMBODIED
S - RAI
82-113 - - - - -
CLOSED: SUPERS. BY ENAC 96-348
N N TCCA
CF-96-21
FAA 72-19-04 Amdt. 39-1782 - N/A N/A Ni-Cd batteries
CLOSED: CF96-21 ISSUED TO CANCEL THE APPLICABILITY OF
FAA 72-19-04
S - RAI
88-052 - - - - - SUPERS. BY ENAC 88-096
R Y RAI
88-096 FAR 43
Appendix E Norma di lavoro
NL-CL-34-06 19/11/2005 24 Months
ALTIMETER AND STATIC PRESSURE SYSTEM
OPEN: TEST CARRIED OUT ON JAN 22, 2010 (NEXT DUE WITHIN
JAN 21, 2012)
I Y ENAC 96-052
FAA FAR 91.21 - N/A N/A USE OF PORTABLE
ELETTRONIC DEVICES CLOSED: AFM UPDATED – CREW
INFORMED
N N ENAC 96-348
FAA 96-20-07 Amdt 39-9773 -
Within 500 Hrs (TIS) or 12 mths from 14/11/96
100 Hrs funzion. 24 Months
COMBUSTION CHAMBER DECAY TEST (JANITROL)
CLOSED: NOT APPLICABLE - HEATER MODEL B4500
(CERAMIC COMBUSTION TUBE) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCD s/n 2003
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCD Components Compliance Status
N N ENAC 97-167
FAA 97-11-10 - - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N TCCA
CF-95-16 ENAC 97-221
Marathon Power SB 111692-014
27/07/96 N/A PCB SERIES PC-250 MODIFICATION OR
REMOVAL
CLOSED: NOT APPLICABLE AS PER INVERTER INSTALLED
(Serie MSI-800)
N N ENAC 97-274
FAA 97-18-03 - - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N ENAC 99-231
FAA 99-08-21 - - N/A
PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
S - ENAC 00-018
FAA 99-23-22 Norma di Lavoro
NL-CL-34-07 Apr 17, 2000 Every 90 days TRANSPONDER MODO
“C” INSPECTION/TEST
CLOSED: SUPERSEDED BY ENAC 00-209
N N ENAC 00-209
FAA 99-23-22 Amdt. 39-11686
Engineering Instruction
EI 004/00 18/05/00 N/A
TRANSPONDER MODO “C”
CLOSED: NOT APPLICABLE AD RESCINDED APR. 12, ‘00
SUPERSEDES ENAC 00-018
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCD s/n 2003
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 3 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCD Components Compliance Status
S - ENAC 01-173
FAA 2001-08-01 Scheda Analisi PA May 2, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04
CLOSED: SUPERSEDED BY ENAC 01-368
A N ENAC 01-368
FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
P/N installed on A/C: J20C30
CLOSED: NOT APPLICABLE AS PER FUEL SHUT-OFF P/N
INSTALLED Supersedes ENAC 01-173
N N ENAC 01-442
FAA 2001-18-05 - Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.
CLOSED: NOT APPLICABLE PER P/N
I Y ENAC 01-470
FAA 2001-22-14 SoREM
DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER
DISCHARGER
CLOSED: P/N AFFECTED CHECKED. WALTER KIDDE
CARTRIDGES INSTALLED ON
I Y TCCA
CF-2002-14 ENAC 02-167
BOMBARDIER SB215-3108 SB215-4234
SoREM BM-CL-61-4234
04/03/2003 N/A
PROPELLER CONTROL UNIT
BACKUP PRESSURE RELIEF VALVE
CLOSED: SB 215-4234 INCORPORATED
I Y ENAC 03-067
FAA 2003-04-06 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II
RNZ -850/ -851
CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND
7510100-731 (#2) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCD s/n 2003
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 4 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCD Components Compliance Status
28/09/2003
N N FAA
2003-23-05 ENAC 2004-003 - December 24, 2005 N/A
Titeflex Corporation, Tubi Flessibili
CLOSED: NOT APPLICABLE
HOSES INSTALLATI P/N 114040-4
R Y FAA
2004-21-05 Amdt.39-13826
- Scheda Analisi PA DT-CL-21-01
A 500 heater Hrs or 100 heater Hrs TIS
since 19/11/04 (whichever occurs
later)
100 Hrs (TIS) or
24 Months
PRESSURE DECAY TEST ed Operational Test del
CABIN HEATER (JANITROL)
OPEN: HEATER TIME IN SERVICE CHECKED:
285.54 HOURS TEST NOT YET PERFORMED
A N FAA
2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
CLOSED: NOT APPLICABLE BY
COMPONENT P/N 91E18-1 INSTALLED
R Y EASA
2006-0265 - Scheda Analisi PA
Within Mar 13, 2007
24 Months MODE “S” and “C”
TRANSPONDERS CHECK
OPEN: CARRIED OUT DURING LAST ANNUAL
CHECK W.O. 10/080 NEXT DUE WITHIN
13/06/2012
A N EASA
2006-0269 - Scheda Analisi PA - -
MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
A N FAA
2006-18-08 - Scheda Analisi AD Oct. 11, 2006 -
GOODYEAR NOSE WHEEL TIRES
CLOSED: NOT APPLICABLE AS PER
GOODYEAR TIRES P/N INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCD s/n 2003
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 5 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCD Components Compliance Status
A N FAA
2006-19-04 - Scheda Analisi AD - -
MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
N N FAA
2006-22-05 ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU
CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND
7510100-731 (#2) INSTALLED
A N EASA
2006-0366 - Scheda Analisi PA Dec 14, 2006 - LIFE RAFT
CLOSED: NOT APPLICABLE AS PER
AIRCRAFT MODEL
A N EASA
2006-0286R1 - Scheda Analisi PA Sep 9, 2006 - Oxygen Cylinders
CLOSED: NOT APPLICABLE AS PER
P/N INSTALLED
A N EASA
2007-0256 - Scheda Analisi PA Sep 19, 2007 - Seat Restraint System
CLOSED: NOT APPLICABLE AS PER
P/N INSTALLED
A N EASA
2007-0294 ENAC 2009-060 Scheda Analisi PA - -
APU Turbine wheel life limit reduction
CLOSED: NOT EFFECTIVE AS PER
APU NOT INSTALLED ON SOREM CL415
FLEET
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCD s/n 2003
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 6 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCD Components Compliance Status
N N EASA
2009-0200 - Scheda Analisi AD Sep 22, 2010 N/A
Navigation – Mode A/C Transponder – Check /
Modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N FAA
2009-20-10 - Scheda Analisi AD Jan 17, 2010 N/A
Autopilot – servo motors modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
S - CF 2009-42 - SOREM ESB-4-32-4414
(SMJC 063)
Part I within 50Fh Part II: within 750 Fc Part III: every 750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
CLOSED: SUPERSEDED BY CF 2009-42R1 (PART I &
PART II CARRIED OUT O DURING THE LAST ANNUAL CHECK W.O.
10/080)
R Y CF 2009-42R1 - ESB-4-32-4414R1 - Every 750 Flight
cycles Special Inspection of
Accumulator Screw Caps
OPEN: AD COVERED BY SMJC-63 – 664
FLIGHT CYCLES TO GO
A N EASA
2009-0251 - Scheda Analisi AD Nov 26, 2009 N/A
Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER S/N
INSTALLED
A N EASA
2009-0262R1 Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A
Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER S/N
NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCD s/n 2003
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 7 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCD Components Compliance Status
A N EASA
2009-0278 - Scheda Analisi AD Jan 22, 2010 N/A
Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N TCA
CF-2009-44 - Scheda Analisi AD Jul 01, 2011 N/A
ELT-Potential Failure to Transmit the Required 406MHz Coded Signal
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N EASA
2010-003R1 - Scheda Analisi AD 18 Apr, 2010 N/A
TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
Y N EASA
2010-0062 - Scheda Analisi AD 14 Apr 2010 N/A
Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
A Y FAA
2010-07-02 - Scheda Analisi AD 31 Ott 2012 N/A
Honeywell Primus II RNZ 850()/-851
OPEN: APPLICABLE AND EFFECTIVE DUE
TO NEW REQUIREMENTS
NOT YET PERFOMED
N N EASA
2010-0067 - Scheda Analisi AD 26 Apr, 2010 N/A
TDR-94 and TDR-94D transponders
NOT EFFECTIVE AS PER P/N NOT INSTALLED
N N EASA
2010-30 Scheda Analisi SIB N/A N/A
Risks in Transporting Lithium Batteries in Cargo by
Aircraft
NOT APPLICABLE SINCE SOREM FLEET IS NOT OPERATING IN CARGO TRANSPORT
CONFIGURATION
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCD s/n 2003
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 8 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCD Components Compliance Status
N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer –
Erroneous Airspeed and Altitude Indications
NOT APPLICABLE AS PER A/C TYPE, REFER TO ADE ISSUED DATED
NOV 09, 2010
N N FAA
2011-01-09 Scheda Analisi AD 9/06/2011 N/R
B/E Aerospace protective breathing equipment P/N 119003-11 inspection for
B/A Aerospace S.B. 119003-35-6 compliance.
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
N N EASA
2011-0043 Scheda Analisi AD 30/04/2013 N/R
Gables Engineering Mode S Transponder Control Panel
Modification
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N EASA
2011-0090R1 ENAC 2011-202 Scheda Analisi AD 27/07/2011 N/R Oxygen mask regulator
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N EASA
2011-0103 Scheda Analisi AD 03/12/2011 N/R
ELT TRI-BAND Antennas P/N 21-41 ( ) series Mod/Replacement
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N FAA
2011-11-04
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire
Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCD s/n 2003
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 9 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCD Components Compliance Status
N N EASA
2010-0204 ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A
TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N FAA 2011-14-
08 Scheda Analisi AD
Aug 19,2014 or 6500 FH from Aug
19,2011 N/A
B/E Aerospace pax oxy mask inspection
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
R Y TCCA
CF-2011-35 - ESB-4-32-A4451 Rev 01
First incorporation: Within 50 Flight Hrs
upon receipt of Bombardier SB 215-
A4451
To be repeated every 165 land landings
Inspection of the MLG Upper Member forward lug using
eddy current method
OPEN: FIRST
INCORPORATION NOT YET PERFORMED
A Y TCCA
CF-2011-35 - ESB-4-32-A4450 Rev 01 November 11, 2011 N/A
Inspection of the MLG Upper Member forward lug using
liquid penetrant method
OPEN
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCE s/n 2004
Delivery Date: Jan 94
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 4
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCE Compliance Status
A N FAA
77-17-13 - - - - NLG DOORS
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N FAA
77-13-05 - - - -
MISSING RIVETS IN BULKHEAD
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N TCCA
CF-90-11R2 FAA 93-16-06R2
Bombardier SB215-A435
SoREM Scheda analisi AD
JUNE. 10, 1994 N/A
RUDDER-AILERON INTERCONNECT TAB (TO PREVENT POSSIBILE
FLUTTER)
CLOSED: NOT EFFECTIVE AS PER POWERED AILERON
SYSTEM INSTALLED
S TCCA
CF-92-22
FAA 94-04-02 TCCA CF-2003-
02
Bombardier SB215-A3040
SoREM Scheda analisi AD
- N/A ENGINE REAR
MOUNT STRUTS
CLOSED: SUPERSEDED BY AD CF-2003-02
I Y ENAC 95-064
TCCA CF-92-10R1
P&WC: SB20914 SB21113 SB21211 SB21314
Bombardier SB215-A3060
SoREM Scheda Analisi PA
N/A ENGINE FIRE-WIRE DETECTION LOOP
CLOSED: AD COMPLIED WITH ENGINE FIRE DETECTION SYSTEM CONNECTED TO AIRCRAFT FIRE WARNING
SYSTEM
I Y FAA
97-11-08 - - - -
AFM - LIMITATION SECTION - POWER
LEVERS
CLOSED: AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION
SECTION PAGE 8
A N TCCA
CF-96-02R1 ENAC 1999-268 - - - -
CLOSED: AD ISSUED JUST TO CANCEL PREVIOUS REVISION
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCE s/n 2004
Delivery Date: Jan 94
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 4
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCE Compliance Status
R N ENAC 00-265
FAA 2004-03-13 - - - MLG AXLES CLOSED: NOT APPLICABLE AS
PER AIRCRAFT S/N
A N TCCA
CF-2002-14 FAA 2004-26-08
ENAC 02-167
Bombardier SB215-4234
SoREM DT CL-61-4234
MARCH 04, 2003 N/A PCU BACKUP
PRESSURE VALVE
CLOSED: NOT APPLICABLE AS PER AIRCRAFT AND ENGINE
SERIAL NUMBERS
R N ENAC 00-496
FAA 2002-12-12 - - - WING TO FUSELAGE
FRAME ANGLES CLOSED: NOT APPLICABLE AS
PER AIRCRAFT S/N
S - FAA
2003-04-06 ENAC 03-067
FAA 2006-22-05
SoREM
DT-CL-34-05 DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II
RNZ-850/ -851 CLOSED: SUPERSEDED BY
FAA 2006-22-05
R Y TCCA
CF-2003-02 FAA 2004-10-04
ENAC 03-251
Bombardier SB215-A4287R2
SoREM BM-CL-71-A4287
BM-CL-71-A4287R2 SMJC 31 and 32
WITHIN 50 F/H SINCE FEBRUARY
28, 2003
EVERY 250 F/H REPETITIVE ACTION
FOLLOWED BY SoREM SMJC #31 and #32
ENGINE REAR MOUNT STRUTS
OPEN: CARRIED OUT WITH SMJC 31 & SMJC 32 WO 11/006 – 128 FH
TO GO
28/09/2003
R Y FAA
2004-21-05 -
SCHEDA ANALISI Disposizione Tecnica
DT-CL-21-01
A 500 heater Hrs Total or 100 heater hrs TIS from 19/11/04
(whichever occurs later)
100 Hrs funzion. 24 Months
PRESSURE DECAY TEST and CABIN
HEATER (JANITROL)
OPERATIONAL TEST
REF TO COMPONENTS
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCE s/n 2004
Delivery Date: Jan 94
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 3 of 4
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCE Compliance Status
A N FAA
2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
REGOLATORE CARBURANTE CON VALVOLE SHUTOFF
A/B/C 14D11 o A/B/C/P 23D04
REF TO COMPONENTS
R N FAA
2005-18-05 - - - -
LOWER CAPS OF THE WING FRONT SPAR AND
REAR SPAR
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N EASA
2006-0375 - Scheda Analisi AD Dec. 29, 2006 -
CARLING TECHNOLOGIES
SWITCHES
CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY
N N FAA
2006-22-05 EASA 2006-479 Scheda Analisi AD - N/A
INTEGRATED NAVIGATION UNITS
REF TO COMPONENTS
Supersedes FAA 2003-04-06
R Y TCCA
CF-2008-29 FAA 2009-05-04 ENAC 2008-316
SMJC-60 Mar 8, 2009
BEFORE AND AFTER EVERY FIRE SEASON
OR AT SIX MONTH INTERVAL,
WHICHEVER IS SHORTER TIME
PERIOD
RUDDER LOWER TORQUE TUBE UPPER BEARING
OPEN: TO BE CARRIED OUT WITH(AD
COVERED BY SMJC 60) INAER W.O. 11/036 ON JUN 13, 11
NEXT DUE WITHIN DEC 12, 11
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCE s/n 2004
Delivery Date: Jan 94
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 4 of 4
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCE Compliance Status
R Y TCCA
CF-2010-38R2 ENAC 2011-88
Bombardier SB 215 -A4424 Jun 01, 2011
FIRST INSPECTION WITHIN 50 FC FROM
20 DEC 2010; THEREAFTER REPEAT
PERRFORM AN INSPECTION BEFORE
100 FC WITH TERMINATING ACTION NOT LATER THAN Jun
01, 2011.
INSPECTION OF THE EMERGENCY WATER
DUMP PULLEY BRACKET AND STRUCTURE
CLOSED PART A ACCOMPLISHED WITH
SMJC-062 TERMINATING ACTION
PERFORMED WITH W.O. 11/006 ON 12/04/11
R Y TCCA
CF-2011-35
Bombardier SB 215-A4450;
Bombardier SB 215-A4451
ESB-4-32-A4450 Rev 01;
ESB-4-32-A4451 Rev 01;
Ref. To AD-PA Compliance Components
Ref. To AD-PA Compliance Components
Liquid Penetrant & Eddy Current Inspection on MLG Upper Member
Forward Lug
REF. TO AD-PA COMPLIANCE COMPONENTS
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0022 Manuf. date: May 1997
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
AD Compliance Status – Engine 1 AF0022
I Y TCA
CF-90-21 -
P&WC SB20355R1
SB20897 30/04/91 N/A
O-RING DETERIORATION DURING FUEL FILTER COVER INSTALLATION
CLOSED: AD COMPLIED WITH AT DELIVERY
I Y RAI
91-296 TCA CF-90-22R1
P&WC SB21018R1
30/06/94 N/A OIL SYSTEM INSPECTION
DUE TO BEARING DETERIORATION
CLOSED: AD COMPLIED WITH AT DELIVERY
I N TCA
CF-91-02 -
P&WC SB20946R1
31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS CLOSED: NA DUE TO ENGINE S/N
I Y RAI
91-347 TCA CF-91-26R1
P&WC SB20914R3
SB21053 31/03/92 N/A
TO IMPROVE THE RETENTION OF THE
P2.5/P3 TUBE ASSEMBLY.
CLOSED: AD COMPLIED WITH AT DELIVERY
S RAI
93-284 TCA CF-92-03R1 - - N/A
INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
CLOSED: AD COMPLIED WITH AT DELIVERY
SUPERSEDED BY CF-92-03R2
I Y TCA
CF-92-03R2 -
P&WC SB20957R3 SB20962R2
SB21065
30/06/94 N/A INTERNAL OIL FIRES IN
THE ICC.
CLOSED: AD COMPLIED WITH AT DELIVERY
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0022 Manuf. date: May 1997
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
AD Compliance Status – Engine 1 AF0022
A N RAI
94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94
1000⇔2000 cycles N/A
REPLACEMENT HP TURBINE DISK
CLOSED: NOT EFFECTIVE FOR ENGINES S/N 109022
AND SUBSEQUENT
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077R7 SB21364R1 SB21373R3
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
CLOSED: ALL SBs RELATED TO AD EMBODIED PRIOR
TO DELIVERY
A N ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB 21100R2
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES
FUEL HEATERS
CLOSED: NOT APPLICABLE FOR ENGINES S/N 109036
AND SUBSEQUENT
N N ENAC 02-090
TCA CF-2002-10 P&WC
SB 20914 R4
At the next scheduled engine
shop visit, or before 31 December 2003, whichever occurs
first
N/A PW118, PW120 and PW121
INTERCOMPRESSOR CASE FIRE
CLOSED: N/A AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21562R0/R1/R2
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within 2400 f/h
or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
CLOSED: AD COMPLIED WIYH AT DELIVERY
(NO REPEATITIVE ACTION) CKD ON ENG CHK LIST
28/09/2003
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0059 Manuf. date: DEC 1999
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
AD Compliance Status – Engine 2 AF0059
I Y TCA
CF-90-21 -
P&WC SB20355R1
SB20897 30/04/91 N/A
O-RING DETERIORATION DURING FUEL FILTER COVER INSTALLATION
CLOSED: AD COMPLIED WITH AT DELIVERY
I Y RAI
91-296 TCA CF-90-22R1
P&WC SB21018R1
30/06/94 N/A OIL SYSTEM INSPECTION
DUE TO BEARING DETERIORATION
CLOSED: AD COMPLIED WITH AT DELIVERY
I N TCA
CF-91-02 -
P&WC SB20946R1
31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS CLOSED: N/A TO ENGINE S/N
I Y RAI
91-347 TCA CF-91-26R1
P&WC SB20914R3
SB21053 31/03/92 N/A
TO IMPROVE THE RETENTION OF THE
P2.5/P3 TUBE ASSEMBLY.
CLOSED: AD COMPLIED WITH AT DELIVERY
S RAI
93-284 TCA CF-92-03R1 - - N/A
INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
CLOSED: AD COMPLIED WITH AT DELIVERY
SUPERSEDED BY CF-92-03R2
I Y TCA
CF-92-03R2 -
P&WC SB20957R3 SB20962R2
SB21065
30/06/94 N/A INTERNAL OIL FIRES IN
THE ICC. CLOSED: AD COMPLIED WITH
AT DELIVERY
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0059 Manuf. date: DEC 1999
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
AD Compliance Status – Engine 2 AF0059
A N RAI
94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94
1000⇔2000 cycles N/A
REPLACEMENT HP TURBINE DISK
CLOSED: nOT EFFECTIVE FOR ENGINES S/N 109022 AND
SUBSEQUENT
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077R7 SB21364R1 SB21373R3
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
CLOSED: ALL SBs RELATED TO AD EMBODIED PRIOR TO
DELIVERY
A N ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB 21100R2
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES
FUEL HEATERS CLOSED: NOT APPLICABLE FOR ENGINES S/N 109036 AND SUB’S
N N ENAC 02-090
TCA CF-2002-10 P&WC
SB 20914 R4
At the next scheduled engine
shop visit, or before 31 December 2003, whichever occurs
first
N/A PW118, PW120 and PW121
INTERCOMPRESSOR CASE FIRE
CLOSED: N/A AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21562R0/R1/R2
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within 2400 f/h
or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
CLOSED: AS COMPLIED WITH AT DELIVERY
(NO REPEATITIVE ACTION) CKD ON ENG LIST
28/09/2003
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
20010616 Manuf. date:
Aug 17, 2001
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report prop1 sn 20010616 CE
I Y FAA
93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided
transfer tube
CLOSED: AD COMPLIED WITH
P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs.
PCU INSPECTION/ MODIFICATION
OPEN: PCU COMPLIANT WITH HS-SB14SF-61-82.
INSPECTED DURING LAST O/H. (every 2000 FH) 1441.44 FH TO GO
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #1 S/N 890293-
19
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #2 S/N
200007012-19
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #3 S/N
200108014-19
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #4 S/N
2005070453
I Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE INSPECTED DURING LAST
O/H. (every 2000 FH) 319.15 FH TO GO
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
20010616 Manuf. date:
Aug 17, 2001
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report prop1 sn 20010616 CE
I Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: ACTUATOR INSPECTED DURING LAST
O/H. (every 2000 FH) 319.15 FH TO GO
I Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: PCU INSPECTED DURING LAST O/H..
(every 2000 FH) 1441.44 FH TO GO
A N FAA
2006-24-07 Scheda Analisi PA Jan 3, 2007
CLOSED: NOT APPLICABLE AS PER PROPELLER
MODEL
A N FAA
US-2011-04-02 ENAC 2011-68 ADE issued Apr 15, 2011
CLOSED: NOT APPLICABLE AS PER PROPELLER
MODEL
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
930703 Manuf. date:
May 07, 2001
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 2
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report prop2 sn 930703 CE
I Y FAA
93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided
transfer tube
CLÒSED: AD COMPLIED WITH
P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs.
PCU INSPECTION/ MODIFICATION
OPEN: PCU COMPLIANT WITH HS-SB14SF-61-82.
(every 2000 FH) 48.47 FH TO GO
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLÒSED: NOT APPLICABLE FOR BLADE #1 S/N
200106017-19
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLÒSED: NOT APPLICABLE FOR BLADE #2 S/N
2005070454-19
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLÒSED: BLADE #3 S/N 882976-19 MODIFIED AS PER ASB 14SF-61-A92R1
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLÒSED: NOT APPLICABLE FOR BLADE #4 S/N 9910026-
19
I Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE INSPECTED DURING LAST
O/H. (every 2000 FH) 1125.09 FH TO GO
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
930703 Manuf. date:
May 07, 2001
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 2
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report prop2 sn 930703 CE
I Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: ACTUATOR INSPECTED DURING LAST
O/H. (every 2000 FH)
1125.09 FH TO GO
I Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: PCU INSPECTED DURING LAST O/H.
(every 2000 FH) 48.47 FH TO GO
A N FAA
2006-24-07 Scheda Analisi PA Jan 3, 2007
CLÒSED: NOT APPLICABLE AS PER PROPELLER
MODEL
A N FAA
US-2011-04-02 ENAC 2011-68 ADE issued Apr 15, 2011
CLÒSED: NOT APPLICABLE AS PER PROPELLER
MODEL
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCE s/n 2004
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCE Components Compliance Status
A N FAA
81-21-05 - - Nov 19, 1981 N/A
ARTEX ELT Battery not usable in salt environment
CLOSED: NOT APPLICABLE – SUBJECT ELT BATTERY NOT
INSTALLED
A N TCCA
CF-96-21
FAA 72-19-04 Amdt. 39-1782
RAI 74-225 - N/A N/A
Ni-Cd batterie con celle in polistirolo
CLOSED: NOT APPLICABLE - TEMPERATURE SENSING
INSTALLED ON BATTERIES EMBODIED
S - RAI
82-113 - - - - -
CLOSED: SUPERS. BY ENAC 96-348
N N TCCA
CF-96-21
FAA 72-19-04 Amdt. 39-1782 - N/A N/A Ni-Cd batteries
CLOSED: CF96-21 ISSUED TO CANCEL THE APPLICABILITY OF
FAA 72-19-04
S - RAI
88-052 - - - - - SUPERS. BY ENAC 88-096
R Y RAI
88-096 FAR 43
Appendix E Norma di lavoro
NL-CL-34-06 19/11/2005 24 Months
ALTIMETER AND STATIC PRESSURE SYSTEM
OPEN TEST CARRIED OUT ON SEP 27, 2010 WITH W.O. 10/319
(NEXT DUE WITHIN SEP 24, 2012)
I Y ENAC 96-052
FAA FAR 91.21 - N/A N/A USE OF PORTABLE
ELETTRONIC DEVICES CLOSED: AFM UPDATED – CREW
INFORMED
N N ENAC 96-348
FAA 96-20-07 Amdt 39-9773 -
Within 500 Hrs (TIS) or 12 mths from 14/11/96
100 Hrs funzion. 24 Months
COMBUSTION CHAMBER DECAY TEST (JANITROL)
CLOSED: NOT APPLICABLE - HEATER MODEL B4500
(CERAMIC COMBUSTION TUBE) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCE s/n 2004
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCE Components Compliance Status
N N ENAC 97-167
FAA 97-11-10 - - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N TCCA
CF-95-16 ENAC 97-221
Marathon Power SB 111692-014
27/07/96 N/A PCB SERIES PC-250 MODIFICATION OR
REMOVAL
CLOSED: NOT APPLICABLE AS PER INVERTER INSTALLED
(Serie MSI-800)
N N ENAC 97-274
FAA 97-18-03 - - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N ENAC 99-231
FAA 99-08-21 - - N/A
PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
S - ENAC 00-018
FAA 99-23-22 Norma di Lavoro
NL-CL-34-07 Apr 17, 2000 Every 90 days TRANSPONDER MODO
“C” INSPECTION/TEST
CLOSED: SUPERSEDED BY ENAC 00-209
N N ENAC 00-209
FAA 99-23-22 Amdt. 39-11686
Engineering Instruction
EI 004/00 18/05/00 N/A
TRANSPONDER MODO “C”
CLOSED: NOT APPLICABLE AD RESCINDED APR. 12, ‘00
SUPERSEDES ENAC 00-018
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCE s/n 2004
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 3 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCE Components Compliance Status
S - ENAC 01-173
FAA 2001-08-01 Scheda Analisi PA May 2, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04
CLOSED: SUPERSEDED BY ENAC 01-368
A N ENAC 01-368
FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
P/N installed on A/C: J20C30
CLOSED: NOT APPLICABLE AS PER FUEL SHUT-OFF P/N
INSTALLED Supersedes ENAC 01-173
N N ENAC 01-442
FAA 2001-18-05 - Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.
CLOSED: NOT APPLICABLE PER P/N
I Y ENAC 01-470
FAA 2001-22-14 SoREM
DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER
DISCHARGER
CLOSED: P/N AFFECTED CHECKED. WALTER KIDDE
CARTRIDGES INSTALLED ON
I Y TCCA
CF-2002-14 ENAC 02-167
BOMBARDIER SB215-3108 SB215-4234
SoREM BM-CL-61-4234
04/03/2003 N/A
PROPELLER CONTROL UNIT
BACKUP PRESSURE RELIEF VALVE
CLOSED: SB 215-4234 INCORPORATED
I Y ENAC 03-067
FAA 2003-04-06 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II
RNZ -850/ -851
CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND
7510100-731 (#2) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCE s/n 2004
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 4 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCE Components Compliance Status
28/09/2003
N N FAA
2003-23-05 ENAC 2004-003 - December 24, 2005 N/A
Titeflex Corporation, Tubi Flessibili
CLOSED: NOT APPLICABLE
HOSES INSTALLATI P/N 114040-4
R Y FAA
2004-21-05 Amdt.39-13826
- Scheda Analisi PA DT-CL-21-01
A 500 heater Hrs or 100 heater Hrs TIS
since 19/11/04 (whichever occurs
later)
100 Hrs (TIS) or
24 Months
PRESSURE DECAY TEST ed Operational Test del
CABIN HEATER (JANITROL)
OPEN: HEATER TIME IN SERVICE CHECKED: 92 HEATER TIME TO GO OR WITHIN 04/03/12
A N FAA
2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
CLOSED: NOT APPLICABLE BY
COMPONENT P/N 91E18-1 INSTALLED
R Y EASA
2006-0265 - Scheda Analisi PA
Within Mar 13, 2007
24 Months MODE “S” and “C”
TRANSPONDERS CHECK
OPEN: CARRIED OUT DURING ANNUAL
CHECK W.O. 11/006
A N EASA
2006-0269 - Scheda Analisi PA - -
MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
A N FAA
2006-18-08 - Scheda Analisi AD Oct. 11, 2006 -
GOODYEAR NOSE WHEEL TIRES
CLOSED: NOT APPLICABLE AS PER
GOODYEAR TIRES P/N INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCE s/n 2004
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 5 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCE Components Compliance Status
A N FAA
2006-19-04 - Scheda Analisi AD - -
MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
N N FAA
2006-22-05 ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU
CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND
7510100-731 (#2) INSTALLED
A N EASA
2006-0366 - Scheda Analisi PA Dec 14, 2006 - LIFE RAFT
CLOSED: NOT APPLICABLE AS PER
AIRCRAFT MODEL
A N EASA
2006-0286R1 - Scheda Analisi PA Sep 9, 2006 - Oxygen Cylinders
CLOSED: NOT APPLICABLE AS PER
P/N INSTALLED
A N EASA
2007-0256 - Scheda Analisi PA Sep 19, 2007 - Seat Restraint System
CLOSED: NOT APPLICABLE AS PER
P/N INSTALLED
A N EASA
2007-0294 ENAC 2009-060 Scheda Analisi PA - -
APU Turbine wheel life limit reduction
CLOSED: NOT EFFECTIVE AS PER
APU NOT INSTALLED ON SOREM CL415
FLEET
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCE s/n 2004
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 6 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCE Components Compliance Status
N N EASA
2009-0200 - Scheda Analisi AD Sep 22, 2010 N/A
Navigation – Mode A/C Transponder – Check /
Modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N FAA
2009-20-10 - Scheda Analisi AD Jan 17, 2010 N/A
Autopilot – servo motors modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
S - CF 2009-42 - SOREM ESB-4-32-4414
(SMJC 063)
Part I within 50Fh Part II: within 750 Fc Part III: every 750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
CLOSED: SUPERSEDED BY CF 2009-42R1 (PART I &
PART II CARRIED OUT O DURING THE LAST ANNUAL CHECK W.O.
10/080)
R Y CF 2009-42R1 - ESB-4-32-4414R1 - Every 750 Flight
cycles Special Inspection of
Accumulator Screw Caps
OPEN: AD COVERED BY SMJC-63 – OPEN:
TO GO 51 FC
A N EASA
2009-0251 - Scheda Analisi AD Nov 26, 2009 N/A
Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER S/N
INSTALLED
A N EASA
2009-0262R1 Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A
Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER S/N
NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCE s/n 2004
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 7 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCE Components Compliance Status
A N EASA
2009-0278 - Scheda Analisi AD Jan 22, 2010 N/A
Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N TCA
CF-2009-44 - Scheda Analisi AD Jul 01, 2011 N/A
ELT-Potential Failure to Transmit the Required 406MHz Coded Signal
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N EASA
2010-003R1 - Scheda Analisi AD 18 Apr, 2010 N/A
TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
Y N EASA
2010-0062 - Scheda Analisi AD 14 Apr 2010 N/A
Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
A Y FAA
2010-07-02 - Scheda Analisi AD 31 Ott 2012 N/A
Honeywell Primus II RNZ 850()/-851
OPEN: APPLICABLE AND EFFECTIVE DUE
TO NEW REQUIREMENTS
NOT YET PERFOMED”
N N EASA
2010-0067 - Scheda Analisi AD 26 Apr, 2010 N/A
TDR-94 and TDR-94D transponders
NOT EFFECTIVE AS PER P/N NOT INSTALLED
N N EASA
2010-30 Scheda Analisi SIB N/A N/A
Risks in Transporting Lithium Batteries in Cargo by
Aircraft
NOT APPLICABLE SINCE SOREM FLEET IS NOT OPERATING IN CARGO TRANSPORT
CONFIGURATION
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCE s/n 2004
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 8 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCE Components Compliance Status
N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer –
Erroneous Airspeed and Altitude Indications
NOT APPLICABLE AS PER A/C TYPE, REFER TO ADE ISSUED DATED
NOV 09, 2010
N N FAA
2011-01-09 Scheda Analisi AD 9/06/2011 N/R
B/E Aerospace protective breathing equipment P/N 119003-11 inspection for
B/A Aerospace S.B. 119003-35-6 compliance.
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
N N EASA
2011-0043 Scheda Analisi AD 30/04/2013 N/R
Gables Engineering Mode S Transponder Control Panel
Modification
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N EASA
2011-0090R1 ENAC 2011-202 Scheda Analisi AD 27/07/2011 N/R Oxygen mask regulator
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N EASA
2011-0103 Scheda Analisi AD 03/12/2011 N/R
ELT TRI-BAND Antennas P/N 21-41 ( ) series Mod/Replacement
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N FAA
2011-11-04
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire
Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCE s/n 2004
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 9 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCE Components Compliance Status
N N EASA
2010-0204 ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A
TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N FAA 2011-14-
08 Scheda Analisi AD
Aug 19,2014 or 6500 FH from Aug
19,2011 N/A
B/E Aerospace pax oxy mask inspection
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
R Y TCCA
CF-2011-35 - ESB-4-32-A4451 Rev 01
First incorporation: Within 50 Flight Hrs
upon receipt of Bombardier SB 215-
A4451
To be repeated every 165 land landings
Inspection of the MLG Upper Member forward lug using
eddy current method
OPEN: FIRST
INCORPORATION CARRIED OUT WITH
W.O. 11/186 ON JUL 22, 11
REPETITIVE ACTION WITHIN 131 LL
A Y TCCA
CF-2011-35 - ESB-4-32-A4450 Rev 01 November 11, 2011 N/A
Inspection of the MLG Upper Member forward lug using
liquid penetrant method
OPEN
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCF s/n 2059
Delivery Date: Sep 01
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 1 of 4 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCF Compliance Status
A N FAA 77-17-13
- - - - NLG DOORS CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N FAA 77-13-05
- - - - MISSING RIVETS IN BULKHEAD
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N TCCA CF-90-11R2 FAA 93-16-06R2
Bombardier SB215-A435
SoREM Scheda analisi AD
JUNE. 10, 1994 N/A RUDDER-AILERON
INTERCONNECT TAB (TO PREVENT POSSIBILE
FLUTTER)
CLOSED: NOT EFFECTIVE AS PER POWERED AILERON SYSTEM
INSTALLED
S TCCA CF-92-22
FAA 94-04-02 TCCA CF-2003-
02
Bombardier SB215-A3040
SoREM Scheda analisi AD
- N/A ENGINE REAR MOUNT STRUTS
CLOSED: SUPERSEDED BY AD CF-2003-02
I Y ENAC 95-064
TCCA CF-92-10R1
P&WC: SB20914 SB21113 SB21211 SB21314
Bombardier SB215-A3060
SoREM Scheda Analisi PA
N/A ENGINE FIRE-WIRE DETECTION LOOP
CLOSED: AD COMPLIED WITH ENGINE FIRE DETECTION SYSTEM CONNECTED TO AIRCRAFT FIRE WARNING
SYSTEM
I Y FAA 97-11-08
- - - - AFM - LIMITATION SECTION - POWER
LEVERS
CLOSED: AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION
SECTION PAGE 8
A N TCCA CF-96-02R1
ENAC 1999-268 - - - - CLOSED: AD ISSUED JUST TO CANCEL PREVIOUS REVISION
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCF s/n 2059
Delivery Date: Sep 01
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 2 of 4 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCF Compliance Status
R N ENAC 00-265
FAA 2004-03-13 - - - MLG AXLES CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N TCCA CF-2002-14
FAA 2004-26-08 ENAC 02-167
Bombardier SB215-4234
SoREM DT CL-61-4234
MARCH 04, 2003 N/A PCU BACKUP PRESSURE VALVE
CLOSED: NOT APPLICABLE AS PER AIRCRAFT AND ENGINE
SERIAL NUMBERS
R N ENAC 00-496
FAA 2002-12-12 - - - WING TO FUSELAGE FRAME ANGLES
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
S - FAA 2003-04-06
ENAC 03-067 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ-850/ -851
CLOSED: SUPERSEDED BY FAA 2006-22-05
R Y TCCA CF-2003-02
FAA 2004-10-04 ENAC 03-251
Bombardier SB215-A4287R2
SoREM BM-CL-71-A4287
BM-CL-71-A4287R2 SMJC 31 and 32
WITHIN 50 F/H SINCE FEBRUARY
28, 2003
EVERY 250 F/H REPETITIVE ACTION
FOLLOWED BY SoREM SMJC #31 and #32
ENGINE REAR MOUNT STRUTS
OPEN: CARRIED OUT WITH SMJC 31 & SMJC 32 WO 11/246 – 129.04
FH TO GO
28/09/2003
R Y FAA 2004-21-05 -
SCHEDA ANALISI Disposizione Tecnica
DT-CL-21-01
A 500 heater Hrs Total or 100 heater hrs TIS from 19/11/04
(whichever occurs later)
100 Hrs funzion. 24 Months
PRESSURE DECAY TEST and CABIN
HEATER (JANITROL)
OPERATIONAL TEST
REF TO COMPONENTS
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCF s/n 2059
Delivery Date: Sep 01
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 3 of 4 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCF Compliance Status
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
REGOLATORE CARBURANTE CON VALVOLE SHUTOFF
A/B/C 14D11 o A/B/C/P 23D04
REF TO COMPONENTS
R N FAA 2005-18-05
- - - - LOWER CAPS OF THE
WING FRONT SPAR AND REAR SPAR
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N EASA 2006-0375
- Scheda Analisi AD Dec. 29, 2006 - CARLING
TECHNOLOGIES SWITCHES
CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY
N N FAA 2006-22-05
EASA 2006-479 Scheda Analisi AD - N/A INTEGRATED NAVIGATION UNITS
REF TO COMPONENTS Supersedes
FAA 2003-04-06
R Y TCCA CF-2008-29
FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009
BEFORE AND AFTER EVERY FIRE SEASON
OR AT SIX MONTH INTERVAL,
WHICHEVER IS SHORTER TIME
PERIOD
RUDDER LOWER TORQUE TUBE UPPER BEARING
OPEN: CARRIED OUT ON APR 05, 11 WITH W.O. 11/045 R1 (AD
COVERED BY SMJC 60) NEXT DUE WITHIN OCT 05, 11
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCF s/n 2059
Delivery Date: Sep 01
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 4 of 4 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCF Compliance Status
R Y TCCA CF-2010-38R2
ENAC 2010-443 Bombardier SB 215 -A4424 Jun 01, 2011
FIRST INSPECTION WITHIN 50 FC FROM
20 DEC 2010; THEREAFTER REPEAT
PERRFORM AN INSPECTION BEFORE
100 FC WITH TERMINATING ACTION NOT LATER THAN 01
Jun 2011.
INSPECTION OF THE EMERGENCY WATER
DUMP PULLEY BRACKET AND STRUCTURE
CLOSED: PART B TERMINATING ACTION PERFORMED WITH W.O. 11/045 R1
R Y TCCA CF-2011-35
Bombardier SB 215-A4450;
Bombardier SB 215-A4451
ESB-4-32-A4450 Rev 01;
ESB-4-32-A4451 Rev 01;
Ref. To AD-PA Compliance Components
Ref. To AD-PA Compliance Components
Liquid Penetrant & Eddy Current Inspection on MLG Upper Member
Forward Lug
REF. TO AD-PA COMPLIANCE COMPONENTS
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
109083 Manuf. date:
SEPT 1995
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 2
pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 2011 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance 109083.doc
I Y TCA CF-90-21 -
P&WC SB20355R1
SB20897 30/04/91 N/A
O-RING DETERIORATION DURING FUEL FILTER COVER INSTALLATION
- CLOSED - AD COMPLIED WITH AT
DELIVERY
I Y RAI 91-296
TCA CF-90-22R1 P&WC SB21018R1 30/06/94 N/A
OIL SYSTEM INSPECTION DUE TO BEARING DETERIORATION
- CLOSED - SB21018 EMBODIED AS PER BUILD SPEC 723. AD COMPLIED WITH
A N TCA CF-91-02
- P&WC SB20946R1 31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS
- CLOSED – N/A DUE TO ENGINE S/N AD COMPLIED WITH AT
DELIVERY
I Y RAI 91-347
TCA CF-91-26R1 P&WC
SB20914R3 SB21053
31/03/92 N/A TO IMPROVE THE
RETENTION OF THE P2.5/P3 TUBE ASSEMBLY.
- CLOSED - SB21053 EMBODIED AS PER BUILD SPEC 723. AD COMPLIED WITH
S Y RAI 93-284
TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
- CLOSED – SUPERSEDED BY TCCA CF-92-03R2
I Y TCA CF-92-03R2
- P&WC
SB20957R3 SB20962R2
SB21065
30/06/94 N/A INTERNAL OIL FIRES IN THE ICC.
- CLOSED - AD COMPLIED WITH AT
DELIVERY
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
109083 Manuf. date:
SEPT 1995
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 2
pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 2011 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance 109083.doc
I Y RAI 94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94 1000⇔2000 cycles N/A REPLACEMENT HP
TURBINE DISK
- CLOSED - AD COMPLIED WITH AT
DELIVERY
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077R7 SB21364R1 SB21373R3
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
- CLOSED - ALL SBs RELATED TO AD
EMBODIED AD COMPLIED WITH
A N ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB 21100R2
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES FUEL HEATERS
- CLOSED – NOT APPLICABLE FOR
ENGINES S/N 109036 AND SUB’S
A N ENAC 02-090
TCA CF-2002-10 - CLOSED –
N/A AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21562R0/R1/R2
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within 2400 f/h
or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
- CLOSED - AD COMPLIED WITH AT
DELIVERY (NO REPETETIVE ACTION)
28/09/2003
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0071 Manuf. date:
JUN 20, 2000
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 2
pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCF Left Engine
I Y TCCA CF-90-21 -
P&WC SB20355R1
SB20897 30/04/91 N/A
O-RING DETERIORATION DURING FUEL FILTER COVER INSTALLATION
- CLOSED - AD COMPLIED WITH AT
DELIVERY
I Y TCCA CF-90-22R1
RAI 91-296 P&WC SB21018 (last R6) 30/06/94 N/A
OIL SYSTEM INSPECTION DUE TO BEARING DETERIORATION
- CLOSED - SB21018 EMBODIED AS PER BUILD SPEC 723. AD COMPLIED WITH
A N TCCA CF-91-02
- P&WC SB20946R1 31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS - CLOSED –
N/A DUE TO ENGINE S/N
I Y TCCA CF-91-26R1
RAI 91-347 P&WC
SB20914 (last R4) SB21053 (last R2)
31/03/92 N/A TO IMPROVE THE
RETENTION OF THE P2.5/P3 TUBE ASSEMBLY.
- CLOSED - SB21053 EMBODIED AS PER BUILD SPEC 723. AD COMPLIED WITH
S TCCA CF-92-03R1
RAI 93-284 - - N/A INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
- CLOSED – SUPERSEDED BY TCCA CF-92-03R2
I Y TCCA CF-92-03R2
- P&WC
SB20957R3 SB20962R2
SB21065
30/06/94 N/A INTERNAL OIL FIRES IN THE ICC.
- CLOSED - AD COMPLIED WITH AT
DELIVERY
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0071 Manuf. date:
JUN 20, 2000
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 2
pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCF Left Engine
A N TCCA CF 94-01
FAA 94-03-02 Amdt 39-8808
RAI 94-001 P&WC SIL 307 Since 14/01/94
1000⇔2000 cycles N/A REPLACEMENT HP TURBINE DISK
- CLOSED – NOT EFFECTIVE FOR
ENGINES S/N 109022 AND SUBSEQUENT
I Y TCCA CF-96-22
ENAC 96-353
P&WC SB21077R7 SB21364R1 SB21373R3
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
- CLOSED - ALL SBs RELATED TO AD
EMBODIED AD COMPLIED WITH
A N TCCA CF-2000-34
FAA 2003-16-04 ENAC 01-065
P&WC SB 21100R2
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES FUEL HEATERS
- CLOSED – NOT EFFECTIVE FOR
ENGINES S/N 109036 AND SUB’S
A N TCCA CF-2002-10
ENAC 02-090
P&WC SB 21914R4
Next shop visit or before 31/12/03
Whichever occurs first
N/A PW118, PW120 and PW121
INTERCOMPRESSOR CASE FIRE
- CLOSED – N/A AS PER ENGINE
MODEL
I Y TCCA CF-2002-34
FAA 2004-20-01 ENAC 02-448
P&WC SB21562R0/R1/R2
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within 2400 f/h
or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
- CLOSED - AD COMPLIED WITH
(NO REPETETIVE ACTION)
28/09/2003
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
970228 Manuff. date:
FEBRUARY 19, 1997
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 2
pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance 970228
I Y FAA 93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided transfer tube
- CLOSED – AD COMPLIED WITH
P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs.
PCU INSPECTION/ MODIFICATION
OPEN: PCU COMPLIANT WITH HS-SB14SF-61-82.
CHECK COVERED BY O/H PROCEDURE (TTG 966.08
FH)
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
- CLOSED – BLADE #1 S/N 882969-19 APPLIED FINAL MODIFICATION HS SB 14SF-61-A92 BY SISAM
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
- CLOSED – BLADE #2 S/N 882973-19 APPLIED FINAL MODIFICATION HS SB 14SF-61-A92 BY SISAM
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
- CLOSED – NOT APPLICABLE FOR
BLADE #3 S/N 889087-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
- CLOSED – NOT APPLICABLE FOR
BLADE #4 S/N 889089-19
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
970228 Manuff. date:
FEBRUARY 19, 1997
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 2
pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance 970228
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRANSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE INSPECTED DURING LAST
O/H (TTG 1379.39 FH)
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: ACTUATOR INSPECTED DURING LAST
O/H (TTG 1379.39 FH)
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: PCU INSPECTED DURING LAST SHOP VISIT
(TTG 966.08 FH)
28/09/2003
A N FAA 2006-24-07
Scheda Analisi PA Jan 3, 2007 - CLOSED –
NOT APPLICABLE AS PER PROPELLER MODEL
A N FAA US-2011-04-02
ENAC 2011-68 ADE issued Apr 15, 2011 - CLOSED –
NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
921236 Manuf. date:
FEB 1994
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance 921236.doc
I Y FAA 93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrated transfer tube
- CLOSED – AD COMPLIED WITH
P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs
PCU INSPECTION/ MODIFICATION
OPEN: PCU COMPLIANT WITH HS-SB14SF-61-82.
CHECK COVERED BY O/H PROCEDURE (TTG 16.45
FH)
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97
500 cycles up-to incorporating of HS SB 14SF-61-A92
BLADE INSPECTION / MODIFICATION
- CLOSED – BLADE #1 S/N 877724-19 APPLIED FINAL MODIFICATION HS SB 14SF-61-A92 BY SISAM
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97
500 cycles up-to incorporating of HS SB 14SF-61-A92
BLADE INSPECTION / MODIFICATION
- CLOSED – BLADE #2 S/N 878391-19 APPLIED FINAL MODIFICATION HS SB 14SF-61-A92 BY SISAM
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
- CLOSED – NOT APPLICABLE FOR
BLADE #3 S/N 200006034-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
- CLOSED – NOT APPLICABLE FOR
BLADE #4 S/N 200107038-19
I Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE INSPECTED DURING LAST
O/H (TTG 800.19 FH)
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
921236 Manuf. date:
FEB 1994
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance 921236.doc
I Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: ACTUATOR INSPECTED DURING LAST
O/H (TTG 800.19 FH)
I Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: PCU INSPECTED DURING LAST O/H
(TTG 16.45 FH)
28/09/2003
A N FAA 2006-24-07
Scheda Analisi PA Jan 3, 2007 - CLOSED –
NOT APPLICABLE AS PER PROPELLER MODEL
A N FAA US-2011-04-02
ENAC 2011-68 ADE issued Apr 15, 2011 - CLOSED –
NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCF s/n 2059
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 1 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCF Components Compliance Status
A N FAA 81-21-05
- - Nov 19, 1981 N/A ARTEX ELT Battery not usable in salt environment
CLOSED: NOT APPLICABLE – SUBJECT ELT BATTERY NOT
INSTALLED
A N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782
RAI 74-225 - N/A N/A Ni-Cd batterie con celle in
polistirolo
CLOSED: NOT APPLICABLE - TEMPERATURE SENSING
INSTALLED ON BATTERIES EMBODIED
S - RAI 82-113
- - - - - CLOSED: SUPERS. BY ENAC 96-348
N N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782 - N/A N/A Ni-Cd batteries
CLOSED: CF96-21 ISSUED TO CANCEL THE APPLICABILITY OF
FAA 72-19-04
S - RAI 88-052
- - - - - SUPERS. BY ENAC 88-096
R Y RAI 88-096
FAR 43 Appendix E
Norma di lavoro NL-CL-34-06 19/11/2005 24 Months ALTIMETER AND STATIC
PRESSURE SYSTEM OPEN: TEST CARRIED OUT ON
FEB 27, 2010 (NEXT DUE WITHIN FEB 25, 2012)
I Y ENAC 96-052
FAA FAR 91.21 - N/A N/A USE OF PORTABLE ELETTRONIC DEVICES
CLOSED: AFM UPDATED – CREW INFORMED
N N ENAC 96-348
FAA 96-20-07 Amdt 39-9773 -
Within 500 Hrs (TIS) or 12 mths from 14/11/96
100 Hrs funzion. 24 Months
COMBUSTION CHAMBER DECAY TEST (JANITROL)
CLOSED: NOT APPLICABLE - HEATER MODEL B4500
(CERAMIC COMBUSTION TUBE) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCF s/n 2059
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 2 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCF Components Compliance Status
N N ENAC 97-167
FAA 97-11-10 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N TCCA CF-95-16
ENAC 97-221 Marathon Power SB 111692-014 27/07/96 N/A
PCB SERIES PC-250 MODIFICATION OR
REMOVAL
CLOSED: NOT APPLICABLE AS PER INVERTER INSTALLED
(Serie MSI-800)
N N ENAC 97-274
FAA 97-18-03 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N ENAC 99-231
FAA 99-08-21 - - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS CLOSED: NOT APPLICABLE -
SCOTT OXYGEN MASKS INSTALLED
S - ENAC 00-018
FAA 99-23-22 Norma di Lavoro NL-CL-34-07 Apr 17, 2000 Every 90 days
TRANSPONDER MODO “C”
INSPECTION/TEST
CLOSED: SUPERSEDED BY ENAC 00-209
N N ENAC 00-209
FAA 99-23-22 Amdt. 39-11686
Engineering InstructionEI 004/00 18/05/00 N/A TRANSPONDER MODO
“C”
CLOSED: NOT APPLICABLE AD RESCINDED APR. 12, ‘00
SUPERSEDES ENAC 00-018
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCF s/n 2059
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 3 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCF Components Compliance Status
S - ENAC 01-173
FAA 2001-08-01 Scheda Analisi PA May 2, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04
CLOSED: SUPERSEDED BY ENAC 01-368
A N ENAC 01-368
FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04 P/N installed on A/C: J20C30
CLOSED: NOT APPLICABLE AS PER FUEL SHUT-OFF P/N
INSTALLED Supersedes ENAC 01-173
N N ENAC 01-442
FAA 2001-18-05 - Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.
CLOSED: NOT APPLICABLE PER P/N
I Y ENAC 01-470
FAA 2001-22-14 SoREM DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER
DISCHARGER CLOSED: P/N AFFECTED
CHECKED. WALTER KIDDE CARTRIDGES INSTALLED ON
I Y TCCA CF-2002-14
ENAC 02-167
BOMBARDIER SB215-3108 SB215-4234
SoREM BM-CL-61-4234
04/03/2003 N/A
PROPELLER CONTROL UNIT
BACKUP PRESSURE RELIEF VALVE
CLOSED: SB 215-4234 INCORPORATED
I Y ENAC 03-067
FAA 2003-04-06 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ -850/ -851
CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND
7510100-731 (#2) INSTALLED
28/09/2003
EASA/TCA/FAA/ENAC
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCF s/n 2059
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 4 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCF Components Compliance Status
N N FAA 2003-23-05
ENAC 2004-003 ENAC 2004-073 - December 24, 2005 N/A Titeflex Corporation,
Tubi Flessibili
CLOSED: NOT APPLICABLE
HOSES INSTALLATI P/N 114040-4
R Y FAA
2004-21-05 Amdt.39-13826
- Scheda Analisi PA DT-CL-21-01
A 500 heater Hrs or 100 heater Hrs TIS
since 19/11/04 (whichever occurs
later)
100 Hrs (TIS) or
24 Months
PRESSURE DECAY TEST ed Operational Test del
CABIN HEATER (JANITROL)
OPEN: HEATER TIME IN SERVICE CHECKED:
310.54 HOURS TEST NOT YET PERFORMED
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
CLOSED: NOT APPLICABLE BY
COMPONENT P/N 91E18-1 INSTALLED
R Y EASA 2006-0265 - Scheda Analisi PA
ESP-4-34-001 Within
Mar 13, 2007 24 Months MODE “S” and “C” TRANSPONDERS CHECK
OPEN: CARRIED OUT WITH ON FEB 27, 2010. NEXT DUE WITHIN FEB
25, 2012
A N EASA 2006-0269
- Scheda Analisi PA - - MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
A N FAA 2006-18-08 - Scheda Analisi AD Oct. 11, 2006 - GOODYEAR
NOSE WHEEL TIRES
CLOSED: NOT APPLICABLE AS PER
GOODYEAR TIRES P/N INSTALLED
EASA/TCA/FAA/ENAC
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCF s/n 2059
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 5 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCF Components Compliance Status
A N FAA 2006-19-04
- Scheda Analisi AD - - MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
N N FAA 2006-22-05
ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU
CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND
7510100-731 (#2) INSTALLED
A N EASA 2006-0366
- Scheda Analisi PA Dec 14, 2006 - LIFE RAFT CLOSED: NOT
APPLICABLE AS PER AIRCRAFT MODEL
A N EASA 2006-0286R1
- Scheda Analisi PA Sep 9, 2006 - Oxygen Cylinders CLOSED: NOT
APPLICABLE AS PER P/N INSTALLED
A N EASA 2007-0256
- Scheda Analisi PA Sep 19, 2007 - Seat Restraint System CLOSED: NOT
APPLICABLE AS PER P/N INSTALLED
A N EASA 2007-0294
ENAC 2009-060 Scheda Analisi PA - - APU Turbine wheel life limit reduction
CLOSED: NOT EFFECTIVE AS PER
APU NOT INSTALLED ON SOREM CL415
FLEET
EASA/TCA/FAA/ENAC
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCF s/n 2059
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 6 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCF Components Compliance Status
N N EASA 2009-0200
- Scheda Analisi AD Sep 22, 2010 N/A Navigation – Mode A/C Transponder – Check /
Modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N FAA 2009-20-10
- Scheda Analisi AD Jan 17, 2010 N/A Autopilot – servo motors modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
S - CF 2009-42 - SOREM ESB-4-32-4414 (SMJC 063)
Part I within 50Fh Part II: within 750 Fc
Part III: every 750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
CLOSED: SUPERSEDED BY CF 2009-42R1 (PART
I CARRIED OUT ON NOV 26, 2009)
R Y CF 2009-42R1 Enac 2010-183 FAA 2011-03-08
SOREM ESB-4-32-4414R1 - Every 750 Flight
cycles Special Inspection of
Accumulator Screw Caps
OPEN: AD COVERED BY SMJC-63
PERFORMED ON FEB 19, 02– 541 FLIGHT
CYCLES TO GO
A N EASA 2009-0251
- Scheda Analisi AD Nov 26, 2009 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER S/N
INSTALLED
A N EASA 2009-0262R1
Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A Portable Halon 1211 Fire Extinguisher
NOT EFFECTIVE AS PER S/N NOT INSTALLED
A N EASA 2009-0278
- Scheda Analisi AD Jan 22, 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
EASA/TCA/FAA/ENAC
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCF s/n 2059
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 7 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCF Components Compliance Status
N N TCA CF-2009-44
- Scheda Analisi AD Jul 01, 2011 N/A ELT-Potential Failure to Transmit the Required 406MHz Coded Signal
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N EASA 2010-003R1
- Scheda Analisi AD 18 Apr, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
Y N EASA 2010-0062R1
- Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
NOT EFFECTIVE AS PER P/N NOT INSTALLED
A Y FAA 2010-07-02
- Scheda Analisi AD 31 Ott 2012 N/A Honeywell Primus II RNZ 850()/-851
OPEN: APPLICABLE AND EFFECTIVE DUE
TO NEW REQUIREMENTS
NOT YET PERFOMED”
N N EASA 2010-0067
- Scheda Analisi AD 26 Apr, 2010 N/A TDR-94 and TDR-94D transponders
NOT EFFECTIVE AS PER P/N NOT INSTALLED
N N EASA 2010-30
Scheda Analisi SIB N/A N/A Risks in Transporting
Lithium Batteries in Cargo by Aircraft
NOT APPLICABLE SINCE SOREM FLEET IS NOT OPERATING IN CARGO TRANSPORT
CONFIGURATION
N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer –
Erroneous Airspeed and Altitude Indications
NOT APPLICABLE AS PER A/C TYPE, REFER
TO ADE ISSUED DATED NOV 09, 2010
EASA/TCA/FAA/ENAC
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCF s/n 2059
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 8 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCF Components Compliance Status
N N FAA 2011-01-09
Scheda Analisi AD 9/06/2011 N/R
B/E Aerospace protective breathing equipment P/N 119003-11 inspection for
B/A Aerospace S.B. 119003-35-6 compliance.
NOT APPLICABLE AS PER P/N NOT INSTALLED
N N EASA 2011-0043
Scheda Analisi AD 30/04/2013 N/R Gables Engineering Mode S Transponder Control Panel
Modification
CLOSED: NOT APPLICABLE AS PER
P/N NOT INSTALLED ON THE A/C TYPE
N N EASA 2011-0090R1
ENAC 2011-202 Scheda Analisi AD 27/07/2011 N/R Oxygen mask regulator CLOSED: NOT
APPLICABLE AS PER P/N NOT INSTALLED ON
THE A/C TYPE
N N EASA 2011-0103
Scheda Analisi AD 03/12/2011 N/R ELT TRI-BAND Antennas
P/N 21-41 ( ) series Mod/Replacement
CLOSED: NOT APPLICABLE AS PER
P/N NOT INSTALLED ON THE A/C TYPE
N N FAA
2011-11-04
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N EASA 2010-0204
ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
EASA/TCA/FAA/ENAC
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCF s/n 2059
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 9 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCF Components Compliance Status
N N FAA 2011-14-08
Scheda Analisi AD Aug 19,2014 or
6500 FH from Aug 19,2011
N/A B/E Aerospace pax oxy mask inspection
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
R Y TCCA CF-2011-35
- ESB-4-32-A4451 Rev 01
First incorporation: Within 50 Flight Hrs
upon receipt of Bombardier SB 215-
A4451
To be repeated every 165 land landings
Inspection of the MLG Upper Member forward lug using eddy current method
FIRST INCORPORATION:
CLOSED (REF TO WO 11/187);
REPETITIVE ACTION: OPEN; TO GO: 70
LANDINGS
A Y TCCA CF-2011-35
- ESB-4-32-A4450 Rev 01 November 11, 2011 N/A
Inspection of the MLG Upper Member forward lug
using liquid penetrant method
OPEN
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCH s/n 2062
Delivery Date: Apr 04
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 3 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Compliance Status
A N FAA 77-17-13
- - - - NLG DOORS CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N FAA 77-13-05
- - - - MISSING RIVETS IN BULKHEAD
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N TCCA CF-90-11R2 FAA 93-16-06R2
Bombardier SB215-A435
SoREM Scheda analisi AD
JUNE. 10, 1994 N/A RUDDER-AILERON
INTERCONNECT TAB (TO PREVENT POSSIBILE
FLUTTER)
CLOSED: NOT EFFECTIVE AS PER POWERED AILERON SYSTEM
INSTALLED
S TCCA CF-92-22
FAA 94-04-02 TCCA CF-2003-
02
Bombardier SB215-A3040
SoREM Scheda analisi AD
- N/A ENGINE REAR MOUNT STRUTS
CLOSED: SUPERSEDED BY AD CF-2003-02
I Y ENAC 95-064
TCCA CF-92-10R1
P&WC: SB20914 SB21113 SB21211 SB21314
Bombardier SB215-A3060
SoREM Scheda Analisi PA
N/A ENGINE FIRE-WIRE DETECTION LOOP
CLOSED: AD COMPLIED WITH ENGINE FIRE DETECTION SYSTEM CONNECTED TO AIRCRAFT FIRE WARNING
SYSTEM
I Y FAA 97-11-08
- - - - AFM - LIMITATION SECTION - POWER
LEVERS
CLOSED: AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION
SECTION PAGE 8
A N TCCA CF-96-02R1
ENAC 1999-268 - - - - CLOSED: AD ISSUED JUST TO CANCEL PREVIOUS REVISION
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCH s/n 2062
Delivery Date: Apr 04
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 3 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Compliance Status
R N ENAC 00-265
FAA 2004-03-13 - - - MLG AXLES CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N TCCA CF-2002-14
FAA 2004-26-08 ENAC 02-167
Bombardier SB215-4234
SoREM DT CL-61-4234
MARCH 04, 2003 N/A PCU BACKUP PRESSURE VALVE
CLOSED: NOT APPLICABLE AS PER AIRCRAFT AND ENGINE
SERIAL NUMBERS
R N ENAC 00-496
FAA 2002-12-12 - - - WING TO FUSELAGE FRAME ANGLES
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
S - FAA 2003-04-06
ENAC 03-067 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ-850/ -851
CLOSED: SUPERSEDED BY FAA 2006-22-05
R Y TCCA CF-2003-02
FAA 2004-10-04 ENAC 03-251
Bombardier SB215-A4287R2
SoREM BM-CL-71-A4287
BM-CL-71-A4287R2 SMJC 31 and 32
WITHIN 50 F/H SINCE FEBRUARY
28, 2003
EVERY 250 F/H REPETITIVE ACTION
FOLLOWED BY INAER SMJC #31 and #32
ENGINE REAR MOUNT STRUTS
OPEN: INSPECTION COVERED BY INAER SMJC 31 AND 32 AND
CARRIED OUT WITH W.O. 11/283 (NEXT DUE WITHIN 147.40 FH)
28/09/2003
R Y FAA 2004-21-05 -
SCHEDA ANALISI Disposizione Tecnica
DT-CL-21-01
A 500 heater Hrs Total or 100 heater hrs TIS from 19/11/04
(whichever occurs later)
100 Hrs funzion. 24 Months
PRESSURE DECAY TEST and CABIN
HEATER (JANITROL)
OPERATIONAL TEST
OPEN: HEATER TIME IN SERVICE CHECKED ON AUG 05, 2010:
96.53 HOURS TEST NOT YET PERFORMED REF
TO COMPONENTS
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCH s/n 2062
Delivery Date: Apr 04
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 3 of 3 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Compliance Status
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
REGOLATORE CARBURANTE CON VALVOLE SHUTOFF
A/B/C 14D11 o A/B/C/P 23D04
REF TO COMPONENTS
R N FAA 2005-18-05
- - - - LOWER CAPS OF THE
WING FRONT SPAR AND REAR SPAR
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N EASA 2006-0375
- Scheda Analisi AD Dec. 29, 2006 - CARLING
TECHNOLOGIES SWITCHES
CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY
N N FAA 2006-22-05
EASA 2006-479 Scheda Analisi AD - N/A INTEGRATED NAVIGATION UNITS
REF TO COMPONENTS Supersedes
FAA 2003-04-06
R Y TCCA CF-2008-29
FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009
BEFORE AND AFTER EVERY FIRE SEASON
OR AT SIX MONTH INTERVAL,
WHICHEVER IS SHORTER TIME
PERIOD
RUDDER LOWER TORQUE TUBE UPPER BEARING
OPEN: COVERED BY SMJC 60 PERFORMED WITH WO 11/022
NEXT DUE ON NOV 11, 2011
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0024 Manuf. date:
SEPTEMBER 1993
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Left Engine
I Y TCA CF-90-21 -
P&WC SB20355R1
SB20897 30/04/91 N/A
O-RING DETERIORATION DURING FUEL FILTER COVER INSTALLATION
CLOSED: FUEL PUMP P/N: 5008269H INSTALLED (Post
SB21360) AD COMPLIED WITH
I Y RAI 91-296
TCA CF-90-22R1 P&WC SB21018R1 30/06/94 N/A
OIL SYSTEM INSPECTION DUE TO BEARING DETERIORATION
CLOSED: SB21018 EMBODIED AS PER BUILD SPEC 723. AD COMPLIED
WITH
A N TCA CF-91-02
- P&WC SB20946R1 31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS CLOSED: N/A DUE TO
ENGINE S/N
I Y RAI 91-347
TCA CF-91-26R1 P&WC
SB20914R3 SB21053
31/03/92 N/A TO IMPROVE THE
RETENTION OF THE P2.5/P3 TUBE ASSEMBLY.
CLOSED: SB21053 EMBODIED AS PER BUILD
SPEC 723. AD COMPLIED WITH
S RAI 93-284
TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
CLOSED: SUPERSEDED BY TCA CF-92-03R2
I Y TCA CF-92-03R2
- P&WC
SB20957R3 SB20962R2
SB21065
30/06/94 N/A INTERNAL OIL FIRES IN THE ICC.
CLOSED: SBs EMBODIED AS PER BUILD SPEC 723.
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0024 Manuf. date:
SEPTEMBER 1993
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Left Engine
A N RAI 94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94 1000⇔2000 cycles N/A REPLACEMENT HP
TURBINE DISK
CLOSED: HP DISK P/N: 3041511 INSTALLED. AD COMPLIED WITH
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077R7 SB21364R1 SB21373R3
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
CLOSED: FUEL NOZZLES OVERHAULED DURING
LAST SHOP VISIT. SB21373 INTRODUCED.
AD COMPLIED WITH
A N ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB 21100R2
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES FUEL HEATERS
CLOSED: NOT EFFECTIVE FOR ENGINES S/N 109036
AND SUB’S
A N ENAC 02-090
TCA CF-2002-10 P&WC SB 21914R4
Next shop visit or before 31/12/03
Whichever occurs first
N/A PW118, PW120 and PW121
INTERCOMPRESSOR CASE FIRE
CLOSED: N/A AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21562R0/R1/R2
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within 2400 f/h
or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
CLOSED: AD COMPLIED WITH
(NO REPETETIVE ACTION)
28/09/2003
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
109041 Manuf. date:
SEPTEMBER 1993
EFFE
CT
A.D. PA-ENAC ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Right Engine
I Y TCA CF-90-21 -
P&WC SB20355R1
SB20897 30/04/91 N/A
O-RING DETERIORATION DURING FUEL FILTER COVER INSTALLATION
CLOSED: FUEL PUMP P/N: 5008269H INSTALLED (Post
SB21360 AD COMPLIED WITH
I Y RAI 91-296
TCA CF-90-22R1 P&WC SB21018R1 30/06/94 N/A
OIL SYSTEM INSPECTION DUE TO BEARING DETERIORATION
CLOSED: SB21018 EMBODIED AS PER BUILD
SPEC 723. AD COMPLIED WITH
A N TCA CF-91-02
- P&WC SB20946R1 31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS CLOSED: N/A DUE TO
ENGINE S/N
I Y RAI 91-347
TCA CF-91-26R1 P&WC
SB20914R3 SB21053
31/03/92 N/A TO IMPROVE THE
RETENTION OF THE P2.5/P3 TUBE ASSEMBLY.
CLOSED: SB21053 EMBODIED AS PER BUILD
SPEC 723. AD COMPLIED WITH
S - RAI 93-284
TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
CLOSED: SUPERSEDED BY TCA CF-92-03R2
I Y TCA CF-92-03R2
- P&WC
SB20957R3 SB20962R2
SB21065
30/06/94 N/A INTERNAL OIL FIRES IN THE ICC.
CLOSED: SBs EMBODIED AS PER BUILD SPEC 723.
AD COMPLIED WITH
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
109041 Manuf. date:
SEPTEMBER 1993
EFFE
CT
A.D. PA-ENAC ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Right Engine
A N RAI 94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94 1000⇔2000 cycles N/A REPLACEMENT HP
TURBINE DISK
CLOSED: HP DISK P/N: 3041511
INSTALLED. AD COMPLIED WITH
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077R7 SB21364R1 SB21373R3
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
CLOSED: FUEL NOZZLES OVERHAULED DURING
LAST SHOP VISIT. SB21373 INTRODUCED.
AD COMPLIED WITH
A N ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB 21100R2
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES FUEL HEATERS
CLOSED: NOT EFFECTIVE FOR ENGINES S/N 109036
AND SUB’S
A N ENAC 02-090
TCA CF-2002-10 P&WC SB 21914R4
Next shop visit or before 31/12/03
Whichever occurs first
N/A PW118, PW120 and PW121
INTERCOMPRESSOR CASE FIRE
CLOSED: N/A AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21562R0/R1/R2
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within 2400 f/h
or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
CLOSED: AD COMPLIED WITH
(NO REPETETIVE ACTION)
28/09/2003
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
960340 Manuf. date:
MARCH 1996
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Right Propeller
I Y FAA 93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided transfer tube
CLOSED: AD COMPLIED WITH
P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs.
PCU INSPECTION/ MODIFICATION
OPEN: PCU HOURS: 1469.58 INSPECTION PERFORMED
EVERY O/H AD COMPLIED WITH
(NEXT DUE WITHIN 530.02)
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION CLOSED: NOT APPLICABLE
FOR BLADE #1 S/N 889085-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
CLOSED: BLADE #2 S/N 880302-19 MODIFIED (ref to
SISAM DECLARATION) AD COMPLIED WITH
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION CLOSED: NOT APPLICABLE
FOR BLADE #3 S/N 200010014-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION CLOSED: NOT APPLICABLE
FOR BLADE #4 S/N 2009040360-19
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
960340 Manuf. date:
MARCH 1996
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Right Propeller
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE HOURS: (TSO): 758.00
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 1242.00)
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: ACTUATOR HOURS (TSO): 758.00
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 1242.00)
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: PCU HOURS (TSN): 1469.58
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 530.02)
28/09/2003
A N FAA 2006-24-07
Scheda Analisi PA Jan 3, 2007 CLOSED: NOT APPLICABLE
AS PER PROPELLER MODEL
A N FAA US-2011-04-02
ENAC 2011-68 ADE issued Apr 15, 2011 CLOSED: NOT APPLICABLE
AS PER PROPELLER MODEL
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
20090618 Manuf. date:
JUNE 2009
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Left Propeller
I Y FAA 93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided transfer tube
CLOSED: AD COMPLIED WITH P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs.
PCU INSPECTION/ MODIFICATION
OPEN: PCU HOURS: 1469.58
INSPECTION PERFORMED EVERY O/H
(NEXT DUE WITHIN 530.02)
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION CLOSED: NOT APPLICABLE
FOR BLADE #1 S/N 2009050173-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION CLOSED: NOT APPLICABLE
FOR BLADE #2 S/N 2009050174-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION CLOSED: NOT APPLICABLE
FOR BLADE #3 S/N 2009040361-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION CLOSED: NOT APPLICABLE
FOR BLADE #4 S/N 2009050175-19
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
20090618 Manuf. date:
JUNE 2009
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Left Propeller
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE HOURS: TSO: N/A; TTSN:
758.00 INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 1242.00)
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: ACTUATOR HOURS TSO: N/A; TTSN: 758.00
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 1242.00)
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: PCU HOURS (TSN): 1469.58
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 530.02)
28/09/2003
A N FAA 2006-24-07
Scheda Analisi PA Jan 3, 2007 CLOSED: NOT APPLICABLE AS PER PROPELLER MODEL
A N FAA US-2011-04-02
ENAC 2011-68 ADE issued Apr 15, 2011 CLOSED: NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
20090618 Manuf. date:
JUNE 2009
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 3 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Left Propeller
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCH s/n 2062
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Components Compliance Status
A N FAA 81-21-05
- - Nov 19, 1981 N/A ARTEX ELT Battery not usable in salt environment
CLOSED: NOT APPLICABLE – SUBJECT ELT BATTERY NOT
INSTALLED
A N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782
RAI 74-225 - N/A N/A Ni-Cd batterie con celle in
polistirolo
CLOSED: NOT APPLICABLE - TEMPERATURE SENSING
INSTALLED ON BATTERIES EMBODIED
S - RAI 82-113
- - - - - CLOSED: SUPERS. BY ENAC 96-348
N N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782 - N/A N/A Ni-Cd batteries
CLOSED: CF96-21 ISSUED TO CANCEL THE APPLICABILITY OF
FAA 72-19-04
S - RAI 88-052
- - - - - CLOSED: SUPERS. BY ENAC 88-096
R Y RAI 88-096
FAR 43 Appendix E
Norma di lavoro NL-CL-34-06 19/11/2005 24 Months ALTIMETER AND STATIC
PRESSURE SYSTEM OPEN: CARRIED OUT DURING LAST ANNUAL CHECK (W.O.
11/022). NEXT DUE WHITIN 3/06/13
I Y ENAC 96-052
FAA FAR 91.21 - N/A N/A USE OF PORTABLE ELETTRONIC DEVICES
CLOSED: AFM UPDATED – CREW INFORMED
N N ENAC 96-348
FAA 96-20-07 Amdt 39-9773 -
Within 500 Hrs (TIS) or 12 mths from 14/11/96
100 Hrs funzion. 24 Months
COMBUSTION CHAMBER DECAY TEST (JANITROL)
CLOSED: NOT APPLICABLE - HEATER MODEL B4500
(CERAMIC COMBUSTION TUBE) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCH s/n 2062
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Components Compliance Status
N N ENAC 97-167
FAA 97-11-10 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N TCCA CF-95-16
ENAC 97-221 Marathon Power SB 111692-014 27/07/96 N/A
PCB SERIES PC-250 MODIFICATION OR
REMOVAL
CLOSED: NOT APPLICABLE AS PER INVERTER INSTALLED
(Serie MSI-800)
N N ENAC 97-274
FAA 97-18-03 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N ENAC 99-231
FAA 99-08-21 - - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS CLOSED: NOT APPLICABLE -
SCOTT OXYGEN MASKS INSTALLED
S - ENAC 00-018
FAA 99-23-22 Norma di Lavoro NL-CL-34-07 Apr 17, 2000 Every 90 days
TRANSPONDER MODO “C”
INSPECTION/TEST
CLOSED: SUPERSEDED BY ENAC 00-209
N N ENAC 00-209
FAA 99-23-22 Amdt. 39-11686
Engineering InstructionEI 004/00 18/05/00 N/A TRANSPONDER MODO
“C”
CLOSED: NOT APPLICABLE AD RESCINDED APR. 12, ‘00
SUPERSEDES ENAC 00-018
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCH s/n 2062
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 3 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Components Compliance Status
S - ENAC 01-173
FAA 2001-08-01 Scheda Analisi PA May 2, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04
CLOSED: SUPERSEDED BY ENAC 01-368
A N ENAC 01-368
FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04 P/N installed on A/C: J20C30
CLOSED: NOT APPLICABLE AS PER FUEL SHUT-OFF P/N
INSTALLED Supersedes ENAC 01-173
N N ENAC 01-442
FAA 2001-18-05 - Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.
CLOSED: NOT APPLICABLE PER P/N
I Y ENAC 01-470
FAA 2001-22-14 SoREM DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER
DISCHARGER CLOSED: P/N AFFECTED
CHECKED. WALTER KIDDE CARTRIDGES INSTALLED ON
I Y TCCA CF-2002-14
ENAC 02-167
BOMBARDIER SB215-3108 SB215-4234
SoREM BM-CL-61-4234
04/03/2003 N/A
PROPELLER CONTROL UNIT
BACKUP PRESSURE RELIEF VALVE
CLOSED: SB 215-4234 INCORPORATED
I Y ENAC 03-067
FAA 2003-04-06 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ -850/ -851
CLOSED: INU#1 #2 REPLACED ON 08/04/04
W/O SOREM 04/028 NOTIFIED TO THE CREW – INFO
INSERTED IN AFM
28/09/2003
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCH s/n 2062
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 4 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Components Compliance Status
N N FAA 2003-23-05
ENAC 2004-003 - December 24, 2005 N/A Titeflex Corporation, Tubi Flessibili
CLOSED: NOT APPLICABLE
HOSES INSTALLATI P/N 114040-4
N N FAA 2003-23-05
ENAC 2004-073 - December 24, 2005 N/A Titeflex Corporation, Tubi Flessibili
CLOSED: NOT APPLICABLE
HOSES INSTALLATI P/N 114040-4
R Y FAA
2004-21-05 Amdt.39-13826
- Scheda Analisi PA DT-CL-21-01
A 500 heater Hrs or 100 heater Hrs TIS
since 19/11/04 (whichever occurs
later)
100 Hrs (TIS) or
24 Months
PRESSURE DECAY TEST ed Operational Test del
CABIN HEATER (JANITROL)
OPEN: HEATER TIME IN SERVICE CHECKED ON
AUG 05, 2010: 96.53 HOURS
TEST NOT YET PERFORMED
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
CLOSED: NOT APPLICABLE BY
COMPONENT P/N 91E18-1 INSTALLED
R Y EASA 2006-0265 - Scheda Analisi PA
ESP-4-34-001 Within
Mar 13, 2007 24 Months MODE “S” and “C” TRANSPONDERS CHECK
OPEN: COVERED BY ANN-AT-10
(REF W.O. 11/022)
A N EASA 2006-0269
- Scheda Analisi PA - - MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
A N FAA 2006-18-08 - Scheda Analisi AD Oct. 11, 2006 - GOODYEAR
NOSE WHEEL TIRES
CLOSED: NOT APPLICABLE AS PER
GOODYEAR TIRES P/N INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCH s/n 2062
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 5 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Components Compliance Status
A N FAA 2006-19-04
- Scheda Analisi AD - - MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
N N FAA 2006-22-05
ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU
CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND
7510100-731 (#2) INSTALLED
A N EASA 2006-0366
- Scheda Analisi PA Dec 14, 2006 - LIFE RAFT CLOSED: NOT
APPLICABLE AS PER AIRCRAFT MODEL
A N EASA 2006-0286R1
- Scheda Analisi PA Sep 9, 2006 - Oxygen Cylinders CLOSED: NOT
APPLICABLE AS PER P/N INSTALLED
A N EASA 2007-0256
- Scheda Analisi PA Sep 19, 2007 - Seat Restraint System CLOSED: NOT
APPLICABLE AS PER P/N INSTALLED
A N EASA 2007-0294
ENAC 2009-060 Scheda Analisi PA - - APU Turbine wheel life limit reduction
CLOSED: NOT EFFECTIVE AS PER
APU NOT INSTALLED ON SOREM CL415
FLEET
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCH s/n 2062
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 6 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Components Compliance Status
N N EASA 2009-0200
- Scheda Analisi AD Sep 22, 2010 N/A Navigation – Mode A/C Transponder – Check /
Modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N FAA 2009-20-10
- Scheda Analisi AD Jan 17, 2010 N/A Autopilot – servo motors modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
S - CF 2009-42 - SOREM ESB-4-32-4414 (SMJC 063)
Part I within 50Fh Part II: within 750 Fc
Part III: every 750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
CLOSED: SUPERSEDED BY CF 2009-42R1 (PART
I CARRIED OUT ON NOV 26, 2009)
R Y CF 2009-42R1 - SOREM ESB-4-32-
4414R1 (SMJC 063)
Part I within 50Fh Part II: within 750 Fc
Part III: every 750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
OPEN: COVERED BY SOREM ESB-4-32-4414
(SMJC 063; PERF. WITH WO 11/022)
616 CYCLES TO GO
A N EASA 2009-0251
- Scheda Analisi AD Nov 26, 2009 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER S/N
INSTALLED
Y N EASA 2009-0262R1
Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED:NOT EFFECTIVE AS PER S/N
NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCH s/n 2062
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 7 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Components Compliance Status
N N EASA 2009-0278
- Scheda Analisi AD Jan 22, 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N TCA CF-2009-44
- Scheda Analisi AD Jul 01, 2011 N/A ELT-Potential Failure to Transmit the Required 406MHz Coded Signal
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N EASA 2010-003R1
- Scheda Analisi AD 18 Apr, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
Y N EASA
2010-0062R1
- Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
A Y FAA 2010-07-02
- Scheda Analisi AD 31 Oct 2012 N/A Honeywell Primus II RNZ 850()/-851
OPEN: INU #1 AND INU #2 TO
BE PERFORMED
N N EASA 2010-0067
- Scheda Analisi AD 26 Apr, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCH s/n 2062
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 8 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Components Compliance Status
N N EASA 2010-30
Scheda Analisi SIB N/A N/A Risks in Transporting Lithium Batteries in Cargo by Aircraft
CLOSED: NOT APPLICABLE SINCE
SOREM FLEET IS NOT OPERATING IN CARGO
TRANSPORT CONFIGURATION
N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer – Erroneous Airspeed and Altitude Indications
CLOSED: NOT APPLICABLE AS PER A/C TYPE, REFER TO ADE ISSUED DATED
NOV 09, 2010
N N FAA 2011-01-09
Scheda Analisi AD 9/06/2011 N/R
B/E Aerospace protective breathing equipment P/N 119003-11 inspection for B/A Aerospace S.B. 119003-35-6 compliance.
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
N N EASA 2011-0043
Scheda Analisi AD 30/04/2013 N/R Gables Engineering Mode S Transponder Control Panel
Modification
CLOSED: NOT APPLICABLE AS PER
P/N NOT INSTALLED ON THE A/C TYPE
N N EASA 2011-0090R1
ENAC 2011-202 Scheda Analisi AD 27/07/2011 N/R Oxygen mask regulator CLOSED: NOT
APPLICABLE AS PER P/N NOT INSTALLED ON
THE A/C TYPE
N N EASA 2011-0103
Scheda Analisi AD 03/12/2011 N/R ELT TRI-BAND Antennas P/N 21-41 ( ) series Mod/Replacement
CLOSED: NOT APPLICABLE AS PER
P/N NOT INSTALLED ON THE A/C TYPE
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCH s/n 2062
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 9 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCH Components Compliance Status
N N FAA
2011-11-04
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N EASA 2010-0204
ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N FAA 2011-14-08
Scheda Analisi AD Aug 19,2014 or 6500 FH from Aug 19,2011
N/A B/E Aerospace pax oxy mask inspection
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
R Y TCCA CF-2011-35
- ESB-4-32-A4451 Rev 01
First incorporation:
Within 50 Flight Hrs upon receipt of Bombardier SB 215-A4451
To be repeated every 165 land
landings
Inspection of the MLG Upper Member forward lug using eddy
current method
FIRST INCORPORATION:
CLOSED (REF TO WO 11/189);
REPETITIVE ACTION: OPEN; TO GO: 1744
LANDINGS
A Y TCCA CF-2011-35
- ESB-4-32-A4450 Rev 01
November 11, 2011 N/A
Inspection of the MLG Upper Member forward lug using liquid
penetrant method OPEN
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCI s/n 2058
Delivery Date: May 01
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 4 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Compliance Status
A N FAA 77-17-13
- - - - NLG DOORS CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N FAA 77-13-05
- - - - MISSING RIVETS IN BULKHEAD
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N TCCA CF-90-11R2 FAA 93-16-06R2
Bombardier SB215-A435
SoREM Scheda analisi AD
JUNE. 10, 1994 N/A RUDDER-AILERON
INTERCONNECT TAB (TO PREVENT POSSIBILE
FLUTTER)
CLOSED: NOT EFFECTIVE AS PER POWERED AILERON SYSTEM
INSTALLED
S TCCA CF-92-22
FAA 94-04-02 TCCA CF-2003-
02
Bombardier SB215-A3040
SoREM Scheda analisi AD
- N/A ENGINE REAR MOUNT STRUTS
CLOSED: SUPERSEDED BY AD CF-2003-02
I Y ENAC 95-064
TCCA CF-92-10R1
P&WC: SB20914 SB21113 SB21211 SB21314
Bombardier SB215-A3060
SoREM Scheda Analisi PA
N/A ENGINE FIRE-WIRE DETECTION LOOP
CLOSED: AD COMPLIED WITH ENGINE FIRE DETECTION SYSTEM CONNECTED TO AIRCRAFT FIRE WARNING
SYSTEM
I Y FAA 97-11-08
- - - - AFM - LIMITATION SECTION - POWER
LEVERS
CLOSED: AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION
SECTION PAGE 8
A N TCCA CF-96-02R1
ENAC 1999-268 - - - - CLOSED: AD ISSUED JUST TO CANCEL PREVIOUS REVISION
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCI s/n 2058
Delivery Date: May 01
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 4 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Compliance Status
R N ENAC 00-265
FAA 2004-03-13 - - - MLG AXLES CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N TCCA CF-2002-14
FAA 2004-26-08 ENAC 02-167
Bombardier SB215-4234
SoREM DT CL-61-4234
MARCH 04, 2003 N/A PCU BACKUP PRESSURE VALVE
CLOSED: NOT APPLICABLE AS PER AIRCRAFT AND ENGINE
SERIAL NUMBERS
R N ENAC 00-496
FAA 2002-12-12 - - - WING TO FUSELAGE FRAME ANGLES
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
S - FAA 2003-04-06
ENAC 03-067 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ-850/ -851
CLOSED: SUPERSEDED BY FAA 2006-22-05
R Y TCCA CF-2003-02
FAA 2004-10-04 ENAC 03-251
Bombardier SB215-A4287R2
SoREM BM-CL-71-A4287
BM-CL-71-A4287R2 SMJC 31 and 32
WITHIN 50 F/H SINCE FEBRUARY
28, 2003
EVERY 250 F/H REPETITIVE ACTION
FOLLOWED BY SoREM SMJC #31 and #32
ENGINE REAR MOUNT STRUTS
OPEN: CARRIED OUT WITH SMJC 31 & SMJC 32 WO 11/002 – 47.15
FH TO GO
28/09/2003
R Y FAA 2004-21-05 -
SCHEDA ANALISI Disposizione Tecnica
DT-CL-21-01
A 500 heater Hrs Total or 100 heater hrs TIS from 19/11/04
(whichever occurs later)
100 Hrs funzion. 24 Months
PRESSURE DECAY TEST and CABIN
HEATER (JANITROL)
OPERATIONAL TEST
REF TO COMPONENTS
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCI s/n 2058
Delivery Date: May 01
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 3 of 4 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Compliance Status
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
REGOLATORE CARBURANTE CON VALVOLE SHUTOFF
A/B/C 14D11 o A/B/C/P 23D04
REF TO COMPONENTS
R N FAA 2005-18-05
- - - - LOWER CAPS OF THE
WING FRONT SPAR AND REAR SPAR
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N EASA 2006-0375
- Scheda Analisi AD Dec. 29, 2006 - CARLING
TECHNOLOGIES SWITCHES
CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY
N N FAA 2006-22-05
EASA 2006-479 Scheda Analisi AD - N/A INTEGRATED NAVIGATION UNITS
REF TO COMPONENTS Supersedes
FAA 2003-04-06
R Y TCCA CF-2008-29
FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009
BEFORE AND AFTER EVERY FIRE SEASON
OR AT SIX MONTH INTERVAL,
WHICHEVER IS SHORTER TIME
PERIOD
RUDDER LOWER TORQUE TUBE UPPER BEARING
OPEN: CARRIED OUT WITH W.O. 11/002
(AD COVERED BY SMJC 60) NEXT DUE WITHIN SET 30, 11
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCI s/n 2058
Delivery Date: May 01
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 4 of 4 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Compliance Status
R Y TCCA CF-2010-38R2
ENAC 2011-88 Bombardier SB 215 -A4424 Jun 01, 2011
FIRST INSPECTION WITHIN 50 FC FROM
20 DEC 2010; THEREAFTER REPEAT
PERRFORM AN INSPECTION BEFORE
100 FC WITH TERMINATING ACTION NOT LATER THAN Jun
01, 2011.
INSPECTION OF THE EMERGENCY WATER
DUMP PULLEY BRACKET AND STRUCTURE
CLOSED: PART A TO BE ACCOMPLISHED WITH SMJC-062
(W.O. 10/269) TERMINATING ACTION PART B PERFORMED
WITH W.O. 11/011
R Y TCCA CF-2011-35
Bombardier SB 215-A4450;
Bombardier SB 215-A4451
ESB-4-32-A4450 Rev 01;
ESB-4-32-A4451 Rev 01;
Ref. To AD-PA Compliance Components
Ref. To AD-PA Compliance Components
Liquid Penetrant & Eddy Current Inspection on MLG Upper Member
Forward Lug
REF. TO AD-PA COMPLIANCE COMPONENTS
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0087 Manuf. date:
AUGUST 2001
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Right Engine
I Y TCA CF-90-21 -
P&WC SB20355 (last R1) SB20897 (last R3)
30/04/91 N/A O-RING DETERIORATION
DURING FUEL FILTER COVER INSTALLATION
CLOSED: AD COMPLIED WITH
AT DELIVERY
I Y RAI 91-296
TCA CF-90-22R1 P&WC SB21018 (last R6) 30/06/94 N/A
OIL SYSTEM INSPECTION DUE TO BEARING DETERIORATION
CLOSED: AD COMPLIED WITH
AT DELIVERY
A N TCA CF-91-02
- P&WC SB20946 (last R2) 31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS CLOSED: N/A DUE TO
ENGINE S/N
I Y RAI 91-347
TCA CF-91-26R1 P&WC
SB20914 (last R4) SB21053 (last R2)
31/03/92 N/A TO IMPROVE THE
RETENTION OF THE P2.5/P3 TUBE ASSEMBLY.
CLOSED: AD COMPLIED WITH
AT DELIVERY
S - RAI 93-284
TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
CLOSED: SUPERSEDED BY TCA CF-92-03R2
I Y TCA CF-92-03R2
- P&WC
SB20957 (last R5) SB20962 (last R4) SB21065 (last R7)
30/06/94 N/A INTERNAL OIL FIRES IN THE ICC.
CLOSED: AD COMPLIED WITH
AT DELIVERY
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0087 Manuf. date:
AUGUST 2001
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Right Engine
A N RAI 94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94 1000⇔2000 cycles N/A REPLACEMENT HP
TURBINE DISK
CLOSED: NOT EFFECTIVE FOR ENGINES S/N 109022
AND SUBSEQUENT
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077 (last R8) SB21364 (last R1) SB21373 (last R3)
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
CLOSED: ALL SBs RELATED TO AD EMBODIED
AD COMPLIED WITH
A N ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB21100 (last R3)
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES FUEL HEATERS
CLOSED: NOT APPLICABLE FOR ENGINES S/N 109036
AND SUBSEQUENT
A N ENAC 02-090
TCA CF-2002-10 P&WC SB 21914R4
Next shop visit or before 31/12/03
Whichever occurs first
N/A PW118, PW120 and PW121
INTERCOMPRESSOR CASE FIRE
CLOSED: N/A AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21562 (last R2)
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within 2400 f/h
or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
CLOSED: AD COMPLIED WITH
AT DELIVERY (NO REPETETIVE ACTION)
28/09/2003
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0081 Manuf. date:
JAN 27, 2001
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Left Engine
I Y TCA CF-90-21 -
P&WC SB20355R1
SB20897 30/04/91 N/A
O-RING DETERIORATION DURING FUEL FILTER COVER INSTALLATION
CLOSED: AD COMPLIED WITH AT DELIVERY
I Y RAI 91-296
TCA CF-90-22R1 P&WC SB21018R1 30/06/94 N/A
OIL SYSTEM INSPECTION DUE TO BEARING DETERIORATION
CLOSED: AD COMPLIED WITH AT DELIVERY
A N TCA CF-91-02
- P&WC SB20946R1 31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS CLOSED: N/A DUE TO
ENGINE S/N
I Y RAI 91-347
TCA CF-91-26R1 P&WC
SB20914R3 SB21053
31/03/92 N/A TO IMPROVE THE
RETENTION OF THE P2.5/P3 TUBE ASSEMBLY.
CLOSED: AD COMPLIED WITH AT DELIVERY
S - RAI 93-284
TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
CLOSED: SUPERSEDED BY TCA CF-92-03R2
I Y TCA CF-92-03R2
- P&WC
SB20957R3 SB20962R2
SB21065
30/06/94 N/A INTERNAL OIL FIRES IN THE ICC.
CLOSED: AD COMPLIED WITH AT DELIVERY
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0081 Manuf. date:
JAN 27, 2001
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Left Engine
A N RAI 94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94 1000⇔2000 cycles N/A REPLACEMENT HP
TURBINE DISK
CLOSED: NOT EFFECTIVE FOR ENGINES S/N 109022
AND SUBSEQUENT
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077R7 SB21364R1 SB21373R3
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
CLOSED: ALL SBs RELATED TO AD EMBODIED
AD COMPLIED WITH
A N ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB 21100R2
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES FUEL HEATERS
CLOSED: NOT EFFECTIVE FOR ENGINES S/N 109036
AND SUB’S
A N ENAC 02-090
TCA CF-2002-10 P&WC SB 21914R4
Next shop visit or before 31/12/03
Whichever occurs first
N/A PW118, PW120 and PW121
INTERCOMPRESSOR CASE FIRE
CLOSED: N/A AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21562R0/R1/R2
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within 2400 f/h
or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
CLOSED: AD COMPLIED WITH AT DELIVERY
(NO REPETETIVE ACTION)
28/09/2003
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
971016 Manuf. date:
OCT 1997
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCI right propeller
I Y FAA 93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided transfer tube
- CLOSED – AD COMPLIED WITH
P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs.
PCU INSPECTION/ MODIFICATION
OPEN: PCU COMPLIANT WITH HS-SB14SF-61-82
CHECK COVERED BY O/H PROCEDURE (TTG 626.07
FH)
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
- CLOSED – BLADE #1 S/N 890287-19
N/A AS PER SERIAL NUMBER
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
- CLOSED – BLADE #2 S/N 890289-19
N/A AS PER SERIAL NUMBER
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
- CLOSED – BLADE #3 890290-19 N/A AS PER SERIAL
NUMBER
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
- CLOSED – BLADE #4 2007010560-19
N/A AS PER SERIAL NUMBER
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
971016 Manuf. date:
OCT 1997
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCI right propeller
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE INSPECTED DURING LAST
O/H (every 2000 Fh) TTG 1488.30 FH
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: ACTUATOR INSPECTED DURING LAST
O/H. (every 2000 Fh) TTG 1488.30 FH
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: PCU INSPECTED DURING LAST SHOP VISIT.
(every 2000 Fh) TTG 626.07 FH
28/09/2003
A N FAA 2006-24-07
Scheda Analisi PA Jan 3, 2007 - CLOSED –
NOT APPLICABLE AS PER PROPELLER MODEL
A N FAA US-2011-04-02
ENAC 2011-68 ADE issued Apr 15, 2011 - CLOSED –
NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
20010811 Manuf. date:
AUG 2001
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCI left propeller
I Y FAA 93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided transfer tube
- CLOSED – AD COMPLIED WITH
P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs.
PCU INSPECTION/ MODIFICATION
OPEN: PCU COMPLIANT WITH HS-SB14SF-61-82
CHECK COVERED BY O/H PROCEDURE (TTG 162.52
FH)
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
- CLOSED – BLADE #1 S/N 880300
APPLIED FINAL MODIFICATION HS SB 14SF-61-A92 BY SISAM
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
- CLOSED – BLADE #2 S/N 200105011
N/A AS PER SERIAL NUMBER
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
- CLOSED – BLADE #3 S/N 200108013
N/A AS PER SERIAL NUMBER
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
- CLOSED – BLADE #4 S/N 20010811
N/A AS PER SERIAL NUMBER
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
20010811 Manuf. date:
AUG 2001
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCI left propeller
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE INSPECTED DURING LAST
O/H (every 2000 Fh) TTG 415.12 FH
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: ACTUATOR INSPECTED DURING LAST
O/H. (every 2000 Fh) TTG 415.12 FH
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: PCU INSPECTED DURING LAST SHOP VISIT.
(every 2000 Fh) TTG 162.52 FH
28/09/2003
A N FAA 2006-24-07
Scheda Analisi PA Jan 3, 2007 - CLOSED –
NOT APPLICABLE AS PER PROPELLER MODEL
A N FAA US-2011-04-02
ENAC 2011-68 ADE issued Apr 15, 2011 - CLOSED –
NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCI s/n 2058
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Components Compliance Status
A N FAA 81-21-05
- - Nov 19, 1981 N/A ARTEX ELT Battery not usable in salt environment
CLOSED: NOT APPLICABLE – SUBJECT ELT BATTERY NOT
INSTALLED
A N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782
RAI 74-225 - N/A N/A Ni-Cd batterie con celle in
polistirolo
CLOSED: NOT APPLICABLE - TEMPERATURE SENSING
INSTALLED ON BATTERIES EMBODIED
S - RAI 82-113
- - - - - CLOSED: SUPERS. BY ENAC 96-348
N N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782 - N/A N/A Ni-Cd batteries
CLOSED: CF96-21 ISSUED TO CANCEL THE APPLICABILITY OF
FAA 72-19-04
S - RAI 88-052
- - - - - SUPERS. BY ENAC 88-096
R Y RAI 88-096
FAR 43 Appendix E
Norma di lavoro NL-CL-34-06 19/11/2005 24 Months ALTIMETER AND STATIC
PRESSURE SYSTEM
OPEN TEST CARRIED OUT ON LH&RH ALTIMETER ON JUL
22,2011WITH W.O. 11/011 R1. (NEXT DUE WITHIN JUL 21, 2013)
I Y ENAC 96-052
FAA FAR 91.21 - N/A N/A USE OF PORTABLE ELETTRONIC DEVICES
CLOSED: AFM UPDATED – CREW INFORMED
N N ENAC 96-348
FAA 96-20-07 Amdt 39-9773 -
Within 500 Hrs (TIS) or 12 mths from 14/11/96
100 Hrs funzion. 24 Months
COMBUSTION CHAMBER DECAY TEST (JANITROL)
CLOSED: NOT APPLICABLE - HEATER MODEL B4500
(CERAMIC COMBUSTION TUBE) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCI s/n 2058
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Components Compliance Status
N N ENAC 97-167
FAA 97-11-10 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N TCCA CF-95-16
ENAC 97-221 Marathon Power SB 111692-014 27/07/96 N/A
PCB SERIES PC-250 MODIFICATION OR
REMOVAL
CLOSED: NOT APPLICABLE AS PER INVERTER INSTALLED
(Serie MSI-800)
N N ENAC 97-274
FAA 97-18-03 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N ENAC 99-231
FAA 99-08-21 - - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS CLOSED: NOT APPLICABLE -
SCOTT OXYGEN MASKS INSTALLED
S - ENAC 00-018
FAA 99-23-22 Norma di Lavoro NL-CL-34-07 Apr 17, 2000 Every 90 days
TRANSPONDER MODO “C”
INSPECTION/TEST
CLOSED: SUPERSEDED BY ENAC 00-209
N N ENAC 00-209
FAA 99-23-22 Amdt. 39-11686
Engineering InstructionEI 004/00 18/05/00 N/A TRANSPONDER MODO
“C”
CLOSED: NOT APPLICABLE AD RESCINDED APR. 12, ‘00
SUPERSEDES ENAC 00-018
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCI s/n 2058
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 3 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Components Compliance Status
S - ENAC 01-173
FAA 2001-08-01 Scheda Analisi PA May 2, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04
CLOSED: SUPERSEDED BY ENAC 01-368
A N ENAC 01-368
FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04 P/N installed on A/C: J20C30
CLOSED: NOT APPLICABLE AS PER FUEL SHUT-OFF P/N
INSTALLED Supersedes ENAC 01-173
N N ENAC 01-442
FAA 2001-18-05 - Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.
CLOSED: NOT APPLICABLE PER P/N
I Y ENAC 01-470
FAA 2001-22-14 SoREM DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER
DISCHARGER CLOSED: P/N AFFECTED
CHECKED. WALTER KIDDE CARTRIDGES INSTALLED ON
I Y TCCA CF-2002-14
ENAC 02-167
BOMBARDIER SB215-3108 SB215-4234
SoREM BM-CL-61-4234
04/03/2003 N/A
PROPELLER CONTROL UNIT
BACKUP PRESSURE RELIEF VALVE
CLOSED: SB 215-4234 INCORPORATED
I Y ENAC 03-067
FAA 2003-04-06 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ -850/ -851
CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND
7510100-731 (#2) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCI s/n 2058
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 4 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Components Compliance Status
28/09/2003
N N FAA 2003-23-05
ENAC 2004-003 ENAC 2004-073 - December 24, 2005 N/A Titeflex Corporation,
Tubi Flessibili
CLOSED: NOT APPLICABLE
HOSES INSTALLATI P/N 114040-4
R Y FAA
2004-21-05 Amdt.39-13826
- Scheda Analisi PA DT-CL-21-01
A 500 heater Hrs or 100 heater Hrs TIS
since 19/11/04 (whichever occurs
later)
100 Hrs (TIS) or
24 Months
PRESSURE DECAY TEST ed Operational Test del
CABIN HEATER (JANITROL)
OPEN: NEW HEATER INSTALLED DURING
ANNUAL CHECK W.O. 11/011 R1. TIME IN
SERVICE CHECKED: 0 HOURS. TEST NOT YET
PERFORMED
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
CLOSED: NOT APPLICABLE BY
COMPONENT P/N 91E18-1 INSTALLED
R Y EASA 2006-0265 - Scheda Analisi PA Within
Mar 13, 2007 24 Months MODE “S” and “C” TRANSPONDERS CHECK
OPEN: CARRIED OUT DURING ANNUAL
CHECK W.O. 11/011 R1. NEXT DUE JUL 21, 2013
A N EASA 2006-0269
- Scheda Analisi PA - - MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
A N FAA 2006-18-08 - Scheda Analisi AD Oct. 11, 2006 - GOODYEAR
NOSE WHEEL TIRES
CLOSED: NOT APPLICABLE AS PER
GOODYEAR TIRES P/N INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCI s/n 2058
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 5 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Components Compliance Status
A N FAA 2006-19-04
- Scheda Analisi AD - - MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
N N FAA 2006-22-05
ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU
CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND
7510100-731 (#2) INSTALLED
A N EASA 2006-0366
- Scheda Analisi PA Dec 14, 2006 - LIFE RAFT CLOSED: NOT
APPLICABLE AS PER AIRCRAFT MODEL
A N EASA 2006-0286R1
- Scheda Analisi PA Sep 9, 2006 - Oxygen Cylinders CLOSED: NOT
APPLICABLE AS PER P/N INSTALLED
A N EASA 2007-0256
- Scheda Analisi PA Sep 19, 2007 - Seat Restraint System CLOSED: NOT
APPLICABLE AS PER P/N INSTALLED
A N EASA 2007-0294
ENAC 2009-060 Scheda Analisi PA - - APU Turbine wheel life limit reduction
CLOSED: NOT EFFECTIVE AS PER
APU NOT INSTALLED ON SOREM CL415
FLEET
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCI s/n 2058
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 6 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Components Compliance Status
N N EASA 2009-0200
- Scheda Analisi AD Sep 22, 2010 N/A Navigation – Mode A/C Transponder – Check /
Modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N FAA 2009-20-10
- Scheda Analisi AD Jan 17, 2010 N/A Autopilot – servo motors modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
S - CF 2009-42 - SOREM ESB-4-32-4414 (SMJC 063)
Part I within 50Fh Part II: within 750 Fc
Part III: every 750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
CLOSED: SUPERSEDED BY CF 2009-42R1 (PART
I & PART II CARRIED OUT O DURING THE
LAST ANNUAL CHECK W.O. 10/080)
R Y CF 2009-42R1 - ESB-4-32-4414R1 - Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
OPEN: AD COVERED BY SMJC-63 – OPEN:
TO GO 486 FC
A N EASA 2009-0251
- Scheda Analisi AD Nov 26, 2009 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER S/N
INSTALLED
A N EASA 2009-0262R1
Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER S/N
NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCI s/n 2058
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 7 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Components Compliance Status
A N EASA 2009-0278
- Scheda Analisi AD Jan 22, 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N TCA CF-2009-44
- Scheda Analisi AD Jul 01, 2011 N/A ELT-Potential Failure to Transmit the Required 406MHz Coded Signal
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N EASA 2010-003R1
- Scheda Analisi AD 18 Apr, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
Y N EASA 2010-0062
- Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
A Y FAA 2010-07-02
- Scheda Analisi AD 31 Ott 2012 N/A Honeywell Primus II RNZ 850()/-851
OPEN: APPLICABLE AND EFFECTIVE DUE
TO NEW REQUIREMENTS
NOT YET PERFOMED”
N N EASA 2010-0067
- Scheda Analisi AD 26 Apr, 2010 N/A TDR-94 and TDR-94D transponders
NOT EFFECTIVE AS PER P/N NOT INSTALLED
N N EASA 2010-30
Scheda Analisi SIB N/A N/A Risks in Transporting
Lithium Batteries in Cargo by Aircraft
NOT APPLICABLE SINCE SOREM FLEET IS NOT OPERATING IN CARGO TRANSPORT
CONFIGURATION
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCI s/n 2058
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 8 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Components Compliance Status
N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer –
Erroneous Airspeed and Altitude Indications
NOT APPLICABLE AS PER A/C TYPE, REFER
TO ADE ISSUED DATED NOV 09, 2010
N N FAA 2011-01-09
Scheda Analisi AD 9/06/2011 N/R
B/E Aerospace protective breathing equipment P/N 119003-11 inspection for
B/A Aerospace S.B. 119003-35-6 compliance.
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
N N EASA 2011-0043
Scheda Analisi AD 30/04/2013 N/R Gables Engineering Mode S Transponder Control Panel
Modification
CLOSED: NOT APPLICABLE AS PER
P/N NOT INSTALLED ON THE A/C TYPE
N N EASA 2011-0090R1
ENAC 2011-202 Scheda Analisi AD 27/07/2011 N/R Oxygen mask regulator CLOSED: NOT
APPLICABLE AS PER P/N NOT INSTALLED ON
THE A/C TYPE
N N EASA 2011-0103
Scheda Analisi AD 03/12/2011 N/R ELT TRI-BAND Antennas
P/N 21-41 ( ) series Mod/Replacement
CLOSED: NOT APPLICABLE AS PER
P/N NOT INSTALLED ON THE A/C TYPE
N N FAA
2011-11-04
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
NOT EFFECTIVE AS PER P/N NOT INSTALLED
N N EASA 2010-0204
ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCI s/n 2058
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 9 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCI Components Compliance Status
N N FAA 2011-14-08
Scheda Analisi AD Aug 19,2014 or
6500 FH from Aug 19,2011
N/A B/E Aerospace pax oxy mask inspection
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
R Y TCCA CF-2011-35
- ESB-4-32-A4451 Rev 01
First incorporation: Within 50 Flight Hrs
upon receipt of Bombardier SB 215-
A4451
To be repeated every 165 land landings
Inspection of the MLG Upper Member forward lug using eddy current method
FIRST INCORPORATION:
CLOSED (REF TO WO 11/011 R1);
REPETITIVE ACTION: OPEN; TO GO: 110
LANDINGS
A Y TCCA CF-2011-35
- ESB-4-32-A4450 Rev 01 November 11, 2011 N/A
Inspection of the MLG Upper Member forward lug
using liquid penetrant method
OPEN
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCO s/n 2009
Delivery Date: Apr 98
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 1 of 4 S Superseded N Not effective
Date:
Sept 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCO Compliance Status
A N FAA 77-17-13
- - - - NLG DOORS - CLOSED -
NOT APPLICABLE AS PER AIRCRAFT S/N
A N FAA 77-13-05
- - - - MISSING RIVETS IN BULKHEAD
- CLOSED - NOT APPLICABLE AS PER
AIRCRAFT S/N
A N TCCA CF-90-11R2 FAA 93-16-06R2
Bombardier SB215-A435
SoREM Scheda analisi AD
JUNE. 10, 1994 N/A RUDDER-AILERON
INTERCONNECT TAB (TO PREVENT POSSIBILE
FLUTTER)
- CLOSED - NOT EFFECTIVE AS PER
POWERED AILERON SYSTEM INSTALLED
S TCCA CF-92-22
FAA 94-04-02 TCCA CF-2003-
02
Bombardier SB215-A3040
SoREM Scheda analisi AD
- N/A ENGINE REAR MOUNT STRUTS
- CLOSED – SUPERSEDED BY
AD CF-2003-02
I Y ENAC 95-064
TCCA CF-92-10R1
P&WC: SB20914 SB21113 SB21211 SB21314
Bombardier SB215-A3060
SoREM Scheda Analisi PA
N/A ENGINE FIRE-WIRE DETECTION LOOP
- CLOSED - AD COMPLIED WITH
ENGINE FIRE DETECTION SYSTEM CONNECTED TO AIRCRAFT FIRE WARNING
SYSTEM
I Y FAA 97-11-08
- - - - AFM - LIMITATION SECTION - POWER
LEVERS
- CLOSED - AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION SECTION
PAGE 8
A N TCCA CF-96-02R1
ENAC 1999-268 - - - - - CLOSED -
AD ISSUED JUST TO CANCEL PREVIOUS REVISION
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCO s/n 2009
Delivery Date: Apr 98
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 2 of 4 S Superseded N Not effective
Date:
Sept 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCO Compliance Status
R N ENAC 00-265
FAA 2004-03-13 - - - MLG AXLES - CLOSED -
NOT APPLICABLE AS PER AIRCRAFT S/N
A N TCCA CF-2002-14
FAA 2004-26-08 ENAC 02-167
Bombardier SB215-4234
SoREM DT CL-61-4234
MARCH 04, 2003 N/A PCU BACKUP PRESSURE VALVE
- CLOSED - NOT APPLICABLE AS PER
AIRCRAFT AND ENGINE SERIAL NUMBERS
R N ENAC 00-496
FAA 2002-12-12 - - - WING TO FUSELAGE FRAME ANGLES
- CLOSED - NOT APPLICABLE AS PER
AIRCRAFT S/N
S - FAA 2003-04-06
ENAC 03-067 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ-850/ -851
- CLOSED - SUPERSEDED BY
FAA 2006-22-05
R Y TCCA CF-2003-02
FAA 2004-10-04 ENAC 03-251
Bombardier SB215-A4287R2
SoREM BM-CL-71-A4287
BM-CL-71-A4287R2 SMJC 31 and 32
WITHIN 50 F/H SINCE FEBRUARY
28, 2003
EVERY 250 F/H REPETITIVE ACTION
FOLLOWED BY SoREM SMJC #31 and #32
ENGINE REAR MOUNT STRUTS
- OPEN - COVERED SMJC 31 & SMJC 32 –
NEXT DUE: WITHIN 217.23 FH
28/09/2003
R Y FAA 2004-21-05 -
SCHEDA ANALISI Disposizione Tecnica
DT-CL-21-01
A 500 heater Hrs Total or 100 heater hrs TIS from 19/11/04
(whichever occurs later)
100 Hrs funzion. 24 Months
PRESSURE DECAY TEST and CABIN
HEATER (JANITROL)
OPERATIONAL TEST
REF TO COMPONENTS
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCO s/n 2009
Delivery Date: Apr 98
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 3 of 4 S Superseded N Not effective
Date:
Sept 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCO Compliance Status
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
REGOLATORE CARBURANTE CON VALVOLE SHUTOFF
A/B/C 14D11 o A/B/C/P 23D04
REF TO COMPONENTS
R N FAA 2005-18-05
- - - - LOWER CAPS OF THE
WING FRONT SPAR AND REAR SPAR
- CLOSED - NOT APPLICABLE AS PER
AIRCRAFT S/N
A N EASA 2006-0375
- Scheda Analisi AD Dec. 29, 2006 - CARLING
TECHNOLOGIES SWITCHES
- CLOSED - NOT APPLICABLE AS PER AD
EFFECTIVITY
N N FAA 2006-22-05
EASA 2006-479 Scheda Analisi AD - N/A INTEGRATED NAVIGATION UNITS
REF TO COMPONENTS Supersedes
FAA 2003-04-06
R Y TCCA CF-2008-29
FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009
BEFORE AND AFTER EVERY FIRE SEASON
OR AT SIX MONTH INTERVAL,
WHICHEVER IS SHORTER TIME
PERIOD
RUDDER LOWER TORQUE TUBE UPPER BEARING
- OPEN - CARRIED OUT DURING LAST ANNUAL CHECK W.O. 11/018
NEXT DUE: WITHIN SEP 26, 2011
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCO s/n 2009
Delivery Date: Apr 98
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 4 of 4 S Superseded N Not effective
Date:
Sept 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCO Compliance Status
R Y TCCA
CF-2010-38R2
ENAC 2011-88 Bombardier SB 215 -A4424 Jun 01, 2011
FIRST INSPECTION WITHIN 50 FC FROM
20 DEC 2010; THEREAFTER REPEAT
PERRFORM AN INSPECTION BEFORE
100 FC WITH TERMINATING ACTION NOT LATER THAN Jun
01, 2011.
INSPECTION OF THE EMERGENCY WATER DUMP
PULLEY BRACKET AND STRUCTURE
CLOSED ESB-4-42-A4424 PART B TERMINATING ACTION
PERFORMED ON 15/02/2011 REF. WO 11/018
R Y TCCA CF-2011-35
Bombardier SB 215-A4450;
Bombardier SB 215-A4451
ESB-4-32-A4450 Rev 01;
ESB-4-32-A4451 Rev 01;
Ref. To AD-PA Compliance Components
Ref. To AD-PA Compliance Components
LIQUID PENETRANT & EDDY CURRENT INSPECTION ON
MLG UPPER MEMBER FORWARD LUG
OPEN
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
109073 Manuf. date:
DECEMBER 1994
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 1 of 2 S Superseded N Not effective
Date:
Sept 09, 11 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - Engine 109073 - I-DPCO RH.doc
I Y TCA CF-90-21
- P&WC
SB20355 (last R1) SB20897 (last R3)
30/04/91 N/A O-RING DETERIORATION
DURING FUEL FILTER COVER INSTALLATION
- CLOSED- AD COMPLIED BY
SB20355 AND SB20897 INCORPORATION
PRIOR TO DELIVERY (SEE ENGINE TECHNICAL LOG)
I Y TCA CF-91-02
- P&WC SB20946 (last R2) 31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS
- CLOSED- AD COMPLIED BY
SB20946 INCORPORATION PRIOR TO DELIVERY
(SEE ENGINE TECHNICAL LOG)
I Y RAI 91-296
TCA CF-90-22R1 P&WC SB21018 (last R6) 30/06/94 N/A
OIL SYSTEM INSPECTION DUE TO BEARING DETERIORATION
- CLOSED- AD COMPLIED BY
SB21018 INCORPORATION PRIOR TO DELIVERY
(SEE ENGINE TECHNICAL LOG)
I Y RAI 91-347
TCA CF-91-26R1 P&WC
SB20914 (last R4) SB21053 (last R2)
31/03/92 N/A TO IMPROVE THE
RETENTION OF THE P2.5/P3 TUBE ASSEMBLY.
- CLOSED- AD COMPLIED BY
SB20914 AND SB21053 INCORPORATION
PRIOR TO DELIVERY (SEE ENGINE TECHNICAL LOG)
I Y TCA
CF-92-03R2 Supersedes RAI 93-284
-
P&WC SB20957 (last R5) SB20962 (last R4) SB21065 (last R7)
30/06/94 N/A INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
- CLOSED- AD COMPLIED BY
SB20957, SB20962 AND SB21065 INCORPORATION
PRIOR TO DELIVERY (SEE ENGINE TECHNICAL LOG)
S RAI 93-284
TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
SUPERSEEDED BY
TCA CF-92-03R2
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
109073 Manuf. date:
DECEMBER 1994
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 2 of 2 S Superseded N Not effective
Date:
Sept 09, 11 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - Engine 109073 - I-DPCO RH.doc
A N RAI 94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94 1000⇔2000 cycles N/A
REPLACEMENT HIGH PRESSURE TURBINE DISK (APPLICABLE TO ENGINE
INCORPORATING HPT DISK P/N 3035711 OR 3038411)
- CLOSED- NOT APPLICABLE
DUE TO INSTALLED HPT DISK P/N DIFFERENT TO THE ONES
INTO EFFECTIVITY (SEE ENGINE TECHNICAL LOG)
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077 (last R8) SB21364 (last R1) SB21373 (last R3)
First nozzle replacement or within
30/11/98 whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
- CLOSED- AD COMPLIED-WITH
(SEE ENGINE TECHNICAL LOG)
A N ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB21100 (last R3)
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES FUEL HEATERS
- CLOSED- NOT APPLICABLE FOR ENGINES
S/N 109036 AND SUBS
N N ENAC 02-090
TCA CF-2002-10 - - - - NOT APPLICABLE AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21669
(INSPECTION)
P&WC SB21562 (last R2) (MODIFICATION)
SOREM DT-CL-73-04
400 F/H
1200 F/H (REPETITIVE INSPECTION)
4500 F/H
(FINAL MODIFICATION)
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
- CLOSED- FINAL MODIFICATION COMPLIED
BY SB21562 INCORPORATION (SEE ENGINE TECHNICAL LOG)
28/09/2003
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0009 Manuf. date:
OCTOBER 1996
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 1 of 2 S Superseded N Not effective
Date:
Sept 9, 11 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - Engine AF0009 - I-DPCO LH.doc
I Y TCA CF-90-21
- P&WC
SB20355 (last R1) SB20897 (last R3)
30/04/91 N/A O-RING DETERIORATION
DURING FUEL FILTER COVER INSTALLATION
- CLOSED- AD COMPLIED BY
SB20355 AND SB20897 INCORPORATION
PRIOR TO DELIVERY (SEE ENGINE TECHNICAL LOG)
I Y TCA CF-91-02
- P&WC SB20946 (last R2) 31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS
- CLOSED- AD COMPLIED BY
SB20946 INCORPORATION PRIOR TO DELIVERY
(SEE ENGINE TECHNICAL LOG)
I Y RAI 91-296
TCA CF-90-22R1 P&WC SB21018 (last R6) 30/06/94 N/A
OIL SYSTEM INSPECTION DUE TO BEARING DETERIORATION
- CLOSED- AD COMPLIED BY
SB21018 INCORPORATION PRIOR TO DELIVERY
(SEE ENGINE TECHNICAL LOG)
I Y RAI 91-347
TCA CF-91-26R1 P&WC
SB20914 (last R4) SB21053 (last R2)
31/03/92 N/A TO IMPROVE THE
RETENTION OF THE P2.5/P3 TUBE ASSEMBLY.
- CLOSED- AD COMPLIED BY
SB20914 AND SB21053 INCORPORATION
PRIOR TO DELIVERY (SEE ENGINE TECHNICAL LOG)
I Y TCA
CF-92-03R2 Supersedes RAI 93-284
-
P&WC SB20957 (last R5) SB20962 (last R4) SB21065 (last R7)
30/06/94 N/A INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
- CLOSED- AD COMPLIED BY
SB20957, SB20962 AND SB21065 INCORPORATION
PRIOR TO DELIVERY (SEE ENGINE TECHNICAL LOG)
S RAI 93-284
TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
SUPERSEDED BY
TCA CF-92-03R2
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0009 Manuf. date:
OCTOBER 1996
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 2 of 2 S Superseded N Not effective
Date:
Sept 9, 11 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - Engine AF0009 - I-DPCO LH.doc
A N RAI 94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94 1000⇔2000 cycles N/A
REPLACEMENT HIGH PRESSURE TURBINE DISK (APPLICABLE TO ENGINE
INCORPORATING HPT DISK P/N 3035711 OR 3038411)
- CLOSED- NOT APPLICABLE
DUE TO INSTALLED HPT DISK P/N DIFFERENT TO THE ONES
INTO EFFECTIVITY (SEE ENGINE TECHNICAL LOG)
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077 (last R8) SB21364 (last R1) SB21373 (last R3)
First nozzle replacement or within
30/11/98 whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
- CLOSED- AD COMPLIED-WITH
(SEE ENGINE TECHNICAL LOG)
A N ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB21100 (last R3)
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES FUEL HEATERS
- CLOSED- NOT APPLICABLE FOR ENGINES
S/N 109036 AND SUBS
N N ENAC 02-090
TCA CF-2002-10 - - - - NOT APPLICABLE AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21669
(INSPECTION)
P&WC SB21562 (last R2) (MODIFICATION)
SOREM DT-CL-73-04
400 F/H
1200 F/H (REPETITIVE INSPECTION)
4500 F/H
(FINAL MODIFICATION)
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
- CLOSED- FINAL MODIFICATION COMPLIED
BY SB21562 INCORPORATION (SEE ENGINE TECHNICAL LOG)
28/09/2003
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
991013 Manuf. date:
OCTOBER 1999
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 1 of 2 S Superseded N Not effective
Date:
Sept 9, 11 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - Propeller 991013 - I-DPCO.doc
I Y FAA 93-06-06
- H.S. ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1)
nitrided transfer tube
- CLOSED- COMPLIED-WITH
AS PER TRANSFER TUBE P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs TIS (Post
HS SB 14SF-61-82)
5000 Hrs TIS (Post
HS SB 14SF-61-82) PCU TORQUE CHECK
- OPEN- INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
242.41 F/H TO GO
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97
500 cycles up-to incorporating of HS SB 14SF-61-A92
BLADE INSPECTION / MODIFICATION
- CLOSED- NOT APPLICABLE FOR
BLADE #1 S/N 9910014-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97
500 cycles up-to incorporating of HS SB 14SF-61-A92
BLADE INSPECTION / MODIFICATION
- CLOSED- NOT APPLICABLE FOR
BLADE #2 S/N 9910015-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97
500 cycles up-to incorporating of HS SB 14SF-61-A92
BLADE INSPECTION / MODIFICATION
- CLOSED- NOT APPLICABLE FOR
BLADE #3 S/N 9910016-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97
500 cycles up-to incorporating of HS SB 14SF-61-A92
BLADE INSPECTION / MODIFICATION
- CLOSED- NOT APPLICABLE FOR
BLADE #4 S/N 9910017-19
I Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
- OPEN- TRANSFER TUBE INSPECTION SCHEDULED EVERY 2000 FH
(prop. O/H) 226.32 F/H TO GO
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
991013 Manuf. date:
OCTOBER 1999
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 2 of 2 S Superseded N Not effective
Date:
Sept 9, 11 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - Propeller 991013 - I-DPCO.doc
I Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
- OPEN- ACTUATOR INSPECTION
SCHEDULED EVERY 2000 FH (prop. O/H)
226.32 F/H TO GO
I Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
- OPEN- PCU INSPECTION
SCHEDULED EVERY 2000 FH (prop. O/H)
242.41 F/H TO GO 28/09/2003
A N FAA 2006-24-07
- - Jan 3, 2007 - - - CLOSED-
NOT APPLICABLE AS PER PROPELLER MODEL
A N FAA US-2011-04-02
ENAC 2011-68 ADE issued Apr 15, 2011 - CLOSED -
NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
941009 Manuf. date:
OCTOBER 1994
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 1 of 2 S Superseded N Not effective
Date:
Sept 9, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCD Left Propeller
I Y FAA 93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided transfer tube
CLOSED: AD COMPLIED WITH
P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs.
PCU INSPECTION/ MODIFICATION
OPEN: PCU INSPECTION PERFORMED EVERY O/H
AD COMPLIED WITH (NEXT DUE WITHIN 1152.20)
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION CLOSED: NOT APPLICABLE
FOR BLADE #1 S/N 2009060223-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION CLOSED: NOT APPLICABLE
FOR BLADE #1 S/N 2009081091-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION CLOSED: NOT APPLICABLE
FOR BLADE #3 S/N 2009060219-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION CLOSED: NOT APPLICABLE
FOR BLADE #4 S/N 2009031495-19
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
941009 Manuf. date:
OCTOBER 1994
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 2 of 2 S Superseded N Not effective
Date:
Sept 9, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCD Left Propeller
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE HOURS: (TSO): 428.24
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN: 1571.36)
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: ACTUATOR HOURS (TSO): 428.24
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 1571.36)
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: PCU HOURS (TSO): 847.40
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 1152.20)
28/09/2003
A N FAA 2006-24-07
Scheda Analisi PA Jan 3, 2007 CLOSED: NOT APPLICABLE
AS PER PROPELLER MODEL
A N FAA US-2011-04-02
ENAC 2011-68 ADE issued Apr 15, 2011 - CLOSED –
NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCO s/n 2009
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 1 of 9 S Superseded N Not effective
Date:
Sept 9, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCO Components Compliance Status
A N FAA 81-21-05
- - Nov 19, 1981 N/A ARTEX ELT Battery not usable in salt environment
-CLOSED- NOT APPLICABLE – SUBJECT ELT
BATTERY NOT INSTALLED
A N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782
RAI 74-225 - N/A N/A Ni-Cd batterie con celle in
polistirolo
-CLOSED- NOT APPLICABLE -
TEMPERATURE SENSING INSTALLED ON BATTERIES
EMBODIED
S - RAI 82-113
- - - - - -CLOSED- : SUPERS. BY ENAC 96-348
N N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782 - N/A N/A Ni-Cd batteries
-CLOSED- CF96-21 ISSUED TO CANCEL THE
APPLICABILITY OF FAA 72-19-04
S - RAI 88-052
- - - - - -CLOSED- SUPERS. BY ENAC 88-096
R Y RAI 88-096
FAR 43 Appendix E
Norma di lavoro NL-CL-34-06 19/11/2005 24 Months ALTIMETER AND STATIC
PRESSURE SYSTEM
-OPEN- CARRIED OUT DURING LAST ANNUAL CHECK W.O. 11/018;
NEXT DUE: WITHIN APR 25, 2013
I Y ENAC 96-052
FAA FAR 91.21 - N/A N/A USE OF PORTABLE ELETTRONIC DEVICES
-CLOSED- AFM UPDATED – CREW
INFORMED
N N ENAC 96-348
FAA 96-20-07 Amdt 39-9773 -
Within 500 Hrs (TIS) or 12 mths from 14/11/96
100 Hrs funzion. 24 Months
COMBUSTION CHAMBER DECAY TEST (JANITROL)
-CLOSED- NOT APPLICABLE -
HEATER MODEL B4500 (CERAMIC COMBUSTION TUBE)
INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCO s/n 2009
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 2 of 9 S Superseded N Not effective
Date:
Sept 9, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCO Components Compliance Status
N N ENAC 97-167
FAA 97-11-10 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
-CLOSED- NOT APPLICABLE -
SCOTT OXYGEN MASKS INSTALLED
N N TCCA CF-95-16
ENAC 97-221 Marathon Power SB 111692-014 27/07/96 N/A
PCB SERIES PC-250 MODIFICATION OR
REMOVAL
-CLOSED- NOT APPLICABLE AS PER
INVERTER INSTALLED (Serie MSI-800)
N N ENAC 97-274
FAA 97-18-03 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
-CLOSED- NOT APPLICABLE -
SCOTT OXYGEN MASKS INSTALLED
N N ENAC 99-231
FAA 99-08-21 - - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS
-CLOSED- NOT APPLICABLE -
SCOTT OXYGEN MASKS INSTALLED
S - ENAC 00-018
FAA 99-23-22 Norma di Lavoro NL-CL-34-07 Apr 17, 2000 Every 90 days
TRANSPONDER MODO “C”
INSPECTION/TEST
-CLOSED- SUPERSEDED BY ENAC 00-209
N N ENAC 00-209
FAA 99-23-22 Amdt. 39-11686
Engineering InstructionEI 004/00 18/05/00 N/A TRANSPONDER MODO
“C”
-CLOSED- NOT APPLICABLE
AD RESCINDED APR. 12, ‘00
SUPERSEDES ENAC 00-018
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCO s/n 2009
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 3 of 9 S Superseded N Not effective
Date:
Sept 9, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCO Components Compliance Status
S - ENAC 01-173
FAA 2001-08-01 Scheda Analisi PA May 2, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04
-CLOSED- SUPERSEDED BY ENAC 01-368
A N ENAC 01-368
FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04 P/N installed on A/C: J20C30
-CLOSED- NOT APPLICABLE AS PER FUEL
SHUT-OFF P/N INSTALLED Supersedes ENAC 01-173
N N ENAC 01-442
FAA 2001-18-05 - Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.
-CLOSED- NOT APPLICABLE PER P/N
I Y ENAC 01-470
FAA 2001-22-14 SoREM DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER
DISCHARGER
-CLOSED- P/N AFFECTED CHECKED.
WALTER KIDDE CARTRIDGES INSTALLED ON
I Y TCCA CF-2002-14
ENAC 02-167
BOMBARDIER SB215-3108 SB215-4234
SoREM BM-CL-61-4234
04/03/2003 N/A
PROPELLER CONTROL UNIT
BACKUP PRESSURE RELIEF VALVE
-CLOSED- SB 215-4234 INCORPORATED
I Y ENAC 03-067
FAA 2003-04-06 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ -850/ -851
-CLOSED- NOT APPLICABLE, INU P/N
7510100-732 (#1) AND 7510100-731 (#2) INSTALLED
EASA/TCA/FAA/ENAC
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCO s/n 2009
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 4 of 9 S Superseded N Not effective
Date:
Sept 9, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCO Components Compliance Status
28/09/2003
N N FAA 2003-23-05
ENAC 2004-003 Enac 2004-073 - December 24, 2005 N/A Titeflex Corporation,
Tubi Flessibili
-CLOSED- NOT APPLICABLE
HOSES INSTALLATI P/N 114040-4
R Y FAA
2004-21-05 Amdt.39-13826
- Scheda Analisi PA DT-CL-21-01
A 500 heater Hrs or 100 heater Hrs TIS
since 19/11/04 (whichever occurs
later)
100 Hrs (TIS) or
24 Months
PRESSURE DECAY TEST ed Operational Test del
CABIN HEATER (JANITROL)
-OPEN- HEATER TIME IN
SERVICE CHECKED: 238.36 HOURS TEST NOT YET PERFORMED
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
-CLOSED- NOT APPLICABLE BY
COMPONENT P/N 91E18-1 INSTALLED
R Y EASA 2006-0265 - Scheda Analisi PA
ESP-4-34-001 Within
Mar 13, 2007 24 Months MODE “S” and “C” TRANSPONDERS CHECK
-OPEN- CARRIED OUT DURING LAST ANNUAL CHECK
W.O. 11/018; NEXT DUE: WITHIN APR
27, 2013
A N EASA 2006-0269
- Scheda Analisi PA - - MODE “S” TRANSPONDERS
-CLOSED- NOT APPLICABLE AS
PER MODEL INSTALLED
A N FAA 2006-18-08 - Scheda Analisi AD Oct. 11, 2006 - GOODYEAR
NOSE WHEEL TIRES
-CLOSED- NOT APPLICABLE AS
PER GOODYEAR TIRES P/N
INSTALLED
EASA/TCA/FAA/ENAC
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCO s/n 2009
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 5 of 9 S Superseded N Not effective
Date:
Sept 9, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCO Components Compliance Status
A N FAA 2006-19-04
- Scheda Analisi AD - - MODE “S” TRANSPONDERS
-CLOSED- NOT APPLICABLE AS
PER MODEL INSTALLED
N N FAA 2006-22-05
ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU
-CLOSED- NOT APPLICABLE, INU P/N 7510100-732 (#1) AND 7510100-731 (#2)
INSTALLED
A N EASA 2006-0366
- Scheda Analisi PA Dec 14, 2006 - LIFE RAFT -CLOSED-
NOT APPLICABLE AS PER AIRCRAFT MODEL
A N EASA 2006-0286R1
- Scheda Analisi PA Sep 9, 2006 - Oxygen Cylinders -CLOSED-
NOT APPLICABLE AS PER P/N INSTALLED
A N EASA 2007-0256
- Scheda Analisi PA Sep 19, 2007 - Seat Restraint System -CLOSED-
NOT APPLICABLE AS PER P/N INSTALLED
A N EASA 2007-0294
ENAC 2009-060 Scheda Analisi PA - - APU Turbine wheel life limit reduction
-CLOSED- NOT EFFECTIVE AS
PER APU NOT INSTALLED ON SOREM
CL415 FLEET
EASA/TCA/FAA/ENAC
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCO s/n 2009
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 6 of 9 S Superseded N Not effective
Date:
Sept 9, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCO Components Compliance Status
N N EASA 2009-0200
- Scheda Analisi AD Sep 22, 2010 N/A Navigation – Mode A/C Transponder – Check /
Modification
-CLOSED- NOT EFFECTIVE AS PER P/N INSTALLED
N N FAA 2009-20-10
- Scheda Analisi AD Jan 17, 2010 N/A Autopilot – servo motors modification
-CLOSED- NOT EFFECTIVE AS PER P/N INSTALLED
S - CF 2009-42 - SOREM ESB-4-32-4414 (SMJC 063)
Part I within 50Fh Part II: within 750 Fc
Part III: every 750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
- CLOSED - SUPERSEDED BY CF
2009-42R1 (PART I CARRIED OUT ON NOV
26, 2009)
R Y CF 2009-42R1 - SOREM ESB-4-32-4414 - Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
CLOSED: PART I (CARRIED OUT ON NOV
26, 2009) OPEN: PART II and Part
III COVERED BY SMJC-63 PERFORMED:DURING LAST ANNUAL CHECK
W.O. 11/018; NEXT DUE WITHIN 559 FLIGHT
CYCLES TO GO
A N EASA 2009-0251
- Scheda Analisi AD Nov 26, 2009 N/A Portable Halon 1211 Fire Extinguisher
-CLOSED- NOT EFFECTIVE AS PER S/N INSTALLED
EASA/TCA/FAA/ENAC
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCO s/n 2009
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 7 of 9 S Superseded N Not effective
Date:
Sept 9, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCO Components Compliance Status
Y N EASA 2009-0262R1
Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A Portable Halon 1211 Fire Extinguisher
-CLOSED- NOT EFFECTIVE AS
PER S/N NOT INSTALLED
N N EASA 2009-0278
- Scheda Analisi AD Jan 22, 2010 N/A Portable Halon 1211 Fire Extinguisher
-CLOSED- NOT EFFECTIVE AS PER P/N INSTALLED
N N TCA CF-2009-44
- Scheda Analisi AD Jul 01, 2011 N/A ELT-Potential Failure to Transmit the Required 406MHz Coded Signal
-CLOSED- NOT EFFECTIVE AS PER P/N INSTALLED
N N EASA 2010-003R1
- Scheda Analisi AD 18 Apr, 2010 N/A TDR-94 and TDR-94D transponders
-CLOSED- NOT EFFECTIVE AS
PER P/N NOT INSTALLED
Y N EASA
2010-0062R1
- Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
-CLOSED- NOT EFFECTIVE AS
PER P/N NOT INSTALLED
A Y FAA 2010-07-02
- Scheda Analisi AD 31 Oct 2012 N/A Honeywell Primus II RNZ 850()/-851
-OPEN- APPLICABLE AND
EFFECTIVE DUE TO “NEW
REQUIREMENTS”; NOT YET PERFORMED
EASA/TCA/FAA/ENAC
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCO s/n 2009
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 8 of 9 S Superseded N Not effective
Date:
Sept 9, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCO Components Compliance Status
N N EASA 2010-0067
- Scheda Analisi AD 26 Apr, 2010 N/A TDR-94 and TDR-94D transponders
NOT EFFECTIVE AS PER P/N NOT INSTALLED
N N EASA 2010-30
Scheda Analisi SIB N/A N/A Risks in Transporting
Lithium Batteries in Cargo by Aircraft
- CLOSED - NOT APPLICABLE
SINCE SOREM FLEET IS NOT OPERATING IN CARGO TRANSPORT
CONFIGURATION
N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer –
Erroneous Airspeed and Altitude Indications
- CLOSED - NOT APPLICABLE AS
PER A/C TYPE, REFER TO ADE ISSUED DATED
NOV 09, 2010
N N FAA 2011-01-09
Scheda Analisi AD 9/06/2011 N/R
B/E Aerospace protective breathing equipment P/N 119003-11 inspection for
B/A Aerospace S.B. 119003-35-6 compliance.
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
N N EASA 2011-0043
Scheda Analisi AD 30/04/2013 N/R Gables Engineering Mode S Transponder Control Panel
Modification
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N EASA 2011-0090R1
ENAC 2011-202 Scheda Analisi AD 27/07/2011 N/R Oxygen mask regulator CLOSED: NOT
APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
EASA/TCA/FAA/ENAC
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCO s/n 2009
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 9 of 9 S Superseded N Not effective
Date:
Sept 9, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCO Components Compliance Status
N N EASA 2011-0103
Scheda Analisi AD 03/12/2011 N/R ELT TRI-BAND Antennas
P/N 21-41 ( ) series Mod/Replacement
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N FAA
2011-11-04
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N EASA 2010-0204
ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N FAA 2011-14-08
Scheda Analisi AD Aug 19,2014 or
6500 FH from Aug 19,2011
N/A B/E Aerospace pax oxy mask inspection
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
R Y TCCA CF-2011-35
- ESB-4-32-A4451 Rev 01
First incorporation: Within 50 Flight Hrs
upon receipt of Bombardier SB 215-
A4451
To be repeated every 165 land landings
Inspection of the MLG Upper Member forward lug using eddy current method
FIRST INCORPORATION:
CLOSED (REF TO WO 11/191);
REPETITIVE ACTION: OPEN; TO GO: 78
LANDINGS
A Y TCCA CF-2011-35
- ESB-4-32-A4450 Rev 01 November 11, 2011 N/A
Inspection of the MLG Upper Member forward lug
using liquid penetrant method
OPEN
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCR s/n 2074
Delivery Date: Jan 10
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 1 of 4 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCR Compliance Status
A N FAA 77-17-13
- - - - NLG DOORS - CLOSED -
NOT APPLICABLE AS PER AIRCRAFT S/N
A N FAA 77-13-05
- - - - MISSING RIVETS IN BULKHEAD
- CLOSED - NOT APPLICABLE AS PER
AIRCRAFT S/N
A N TCCA CF-90-11R2 FAA 93-16-06R2
Bombardier SB215-A435
SoREM Scheda analisi AD
JUNE. 10, 1994 N/A RUDDER-AILERON
INTERCONNECT TAB (TO PREVENT POSSIBILE
FLUTTER)
- CLOSED - NOT EFFECTIVE AS PER
POWERED AILERON SYSTEM INSTALLED
S TCCA CF-92-22
FAA 94-04-02 TCCA CF-2003-
02
Bombardier SB215-A3040
SoREM Scheda analisi AD
- N/A ENGINE REAR MOUNT STRUTS
- CLOSED - SUPERSEDED BY
AD CF-2003-02
I Y ENAC 95-064
TCCA CF-92-10R1
P&WC: SB20914 SB21113 SB21211 SB21314
Bombardier SB215-A3060
SoREM Scheda Analisi PA
N/A ENGINE FIRE-WIRE DETECTION LOOP
- CLOSED - AD COMPLIED WITH
ENGINE FIRE DETECTION SYSTEM CONNECTED TO AIRCRAFT FIRE WARNING
SYSTEM
I Y FAA 97-11-08
- - - - AFM - LIMITATION SECTION - POWER
LEVERS
- CLOSED - AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION SECTION
PAGE 8
A N TCCA CF-96-02R1
ENAC 1999-268 - - - - - CLOSED -
AD ISSUED JUST TO CANCEL PREVIOUS REVISION
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCR s/n 2074
Delivery Date: Jan 10
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 2 of 4 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCR Compliance Status
R N ENAC 00-265
FAA 2004-03-13 - - - MLG AXLES - CLOSED -
NOT APPLICABLE AS PER AIRCRAFT S/N
A N TCCA CF-2002-14
FAA 2004-26-08 ENAC 02-167
Bombardier SB215-4234
SoREM DT CL-61-4234
MARCH 04, 2003 N/A PCU BACKUP PRESSURE VALVE
- CLOSED - NOT APPLICABLE AS PER
AIRCRAFT AND ENGINE SERIAL NUMBERS
R N ENAC 00-496
FAA 2002-12-12 - - - WING TO FUSELAGE FRAME ANGLES
- CLOSED - NOT APPLICABLE AS PER
AIRCRAFT S/N
S - FAA 2003-04-06
ENAC 03-067 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ-850/ -851
- CLOSED - SUPERSEDED BY
FAA 2006-22-05
A N TCCA CF-2003-02
FAA 2004-10-04 ENAC 03-251
Bombardier SB215-A4287R2
SoREM BM-CL-71-A4287
BM-CL-71-A4287R2 SMJC 31 and 32
WITHIN 50 F/H SINCE FEBRUARY
28, 2003
EVERY 250 F/H REPETITIVE ACTION
FOLLOWED BY SoREM SMJC #31 and #32
ENGINE REAR MOUNT STRUTS
- CLOSED - NOT APPLICABLE SINCE REAR
MOUNTS P/N 87110047-001 INSTALLED IN PRODUCTION
28/09/2003
R Y FAA 2004-21-05 -
SCHEDA ANALISI Disposizione Tecnica
DT-CL-21-01
A 500 heater Hrs Total or 100 heater hrs TIS from 19/11/04
(whichever occurs later)
100 Hrs funzion. 24 Months
PRESSURE DECAY TEST and CABIN
HEATER (JANITROL)
OPERATIONAL TEST
REF TO COMPONENTS
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCR s/n 2074
Delivery Date: Jan 10
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 3 of 4 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCR Compliance Status
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
REGOLATORE CARBURANTE CON VALVOLE SHUTOFF
A/B/C 14D11 o A/B/C/P 23D04
REF TO COMPONENTS
R N FAA 2005-18-05
- - - - LOWER CAPS OF THE
WING FRONT SPAR AND REAR SPAR
- CLOSED - NOT APPLICABLE AS PER
AIRCRAFT S/N
A N EASA 2006-0375
- Scheda Analisi AD Dec. 29, 2006 - CARLING
TECHNOLOGIES SWITCHES
- CLOSED - NOT APPLICABLE AS PER AD
EFFECTIVITY
N N FAA 2006-22-05
EASA 2006-479 Scheda Analisi AD - N/A INTEGRATED NAVIGATION UNITS
REF TO COMPONENTS Supersedes
FAA 2003-04-06
R Y TCCA CF-2008-29
FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009
BEFORE AND AFTER EVERY FIRE SEASON
OR AT SIX MONTH INTERVAL,
WHICHEVER IS SHORTER TIME
PERIOD
RUDDER LOWER TORQUE TUBE UPPER
BEARING
- OPEN - AD COMPLIED WITH
ON APR 14, 2011. NEXT DUE OCT 13, 2011 (AD COVERED BY SMJC
60)
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCR s/n 2074
Delivery Date: Jan 10
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 4 of 4 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCR Compliance Status
R Y TCCA
CF-2010-38R2
ENAC 2011-88 Bombardier SB 215 -A4424 Jun 01, 2011
FIRST INSPECTION WITHIN 50 FC FROM
20 DEC 2010; THEREAFTER REPEAT
PERRFORM AN INSPECTION BEFORE
100 FC WITH TERMINATING ACTION NOT LATER THAN Jun
01, 2011.
INSPECTION OF THE EMERGENCY WATER
DUMP PULLEY BRACKET AND STRUCTURE
CLOSED ESB-4-42-A4424 PART B TERMINATING ACTION
PERFORMED ON 10/05/2011 REF. WO 11/069
R Y TCCA CF-2011-35
Bombardier SB 215-A4450;
Bombardier SB 215-A4451
ESB-4-32-A4450 Rev 01;
ESB-4-32-A4451 Rev 01;
Ref. To AD-PA Compliance Components
Ref. To AD-PA Compliance Components
LIQUID PENETRANT & EDDY CURRENT
INSPECTION ON MLG UPPER MEMBER FORWARD LUG
OPEN
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0124 Manuf. date:
JUNE 2009
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 1 of 2 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - AF0124 - Engine1 - I-DPCR (WIP).doc
I Y TCA CF-90-21 -
P&WC SB20355 (last R1) SB20897 (last R3)
30/04/91 N/A O-RING DETERIORATION
DURING FUEL FILTER COVER INSTALLATION
- CLOSED- FUEL PUMP P/N: 3117094-02 INSTALLED (Post SB21360)
I Y RAI 91-296
TCA CF-90-22R1 P&WC SB21018 (last R6) 30/06/94 N/A
OIL SYSTEM INSPECTION DUE TO BEARING DETERIORATION
- CLOSED- SB21018 EMBODIED AS PER
BUILD SPEC 723.
A N TCA CF-91-02
- P&WC SB20946 (last R2) 31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS - CLOSED-
N/A DUE TO ENGINE S/N
I Y RAI 91-347
TCA CF-91-26R1 P&WC
SB20914 (last R4) SB21053 (last R2)
31/03/92 N/A ENGINE FIRE DUE TO OIL
ACCUMULATING IN THE ICC CAVITY.
- CLOSED- SB21053 AND SB20914
EMBODIED AS PER BUILD SPEC 723.
S - RAI 93-284
TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES IN THE ICC.
- CLOSED- SUPERSEEDED BY TCA CF-
92-03R2
I Y TCA CF-92-03R2
- P&WC
SB20957 (last R5) SB20962 (last R4) SB21065 (last R7)
21211 (last R6)
30/06/94 N/A INTERNAL OIL FIRES IN THE ICC.
- CLOSED- SBs EMBODIED AS PER
BUILD SPEC 723.
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0124 Manuf. date:
JUNE 2009
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 2 of 2 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - AF0124 - Engine1 - I-DPCR (WIP).doc
I Y RAI 94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94
1000⇔2000 cycles
N/A REPLACEMENT HP TURBINE DISK
- CLOSED- HP DISK P/N 3041511
INSTALLED
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077 (last R8) SB21364 (last R1) SB21373 (last R3)
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
- CLOSED- SBs INTRODUCED AT
MANUFACTURE
I Y ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB21100 (last R3)
all spare heaters within 02/03/01
installed p/n 10718
before 31/08/02
N/A ENGINE PW100 SERIES FUEL HEATERS
- CLOSED- FUEL HEATER P/N: 10839F
(Post SB21519)
A N ENAC 02-090
TCA CF-2002-10 - - N/A INTERCOMPRESSOR CASE FIRE
- CLOSED- N/A AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21562 (last R2)
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within
2400 f/h or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
- CLOSED- MFCU P/N 3244857-15
INSTALLED (Post SB21562)
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0126 Manuf. date:
JUNE 2009
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 1 of 2 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - AF0126 - Engine2 - I-DPCR (WIP).doc
I Y TCA CF-90-21 -
P&WC SB20355 (last R1) SB20897 (last R3)
30/04/91 N/A
O-RING DETERIORATION
DURING FUEL FILTER COVER INSTALLATION
- CLOSED- FUEL PUMP P/N: 3117094-02 INSTALLED (Post SB21360)
I Y RAI 91-296
TCA CF-90-22R1 P&WC SB21018 (last R6) 30/06/94 N/A
OIL SYSTEM INSPECTION DUE TO
BEARING DETERIORATION
- CLOSED- SB21018 EMBODIED AS PER BUILD
SPEC 723
A N TCA CF-91-02
- P&WC SB20946 (last R2) 31/10/91 N/A
TO PREVENT IN FLIGHT TORQUE
FLUCTUATIONS
- CLOSED- N/A DUE TO ENGINE S/N
I Y RAI 91-347
TCA CF-91-26R1 P&WC
SB20914 (last R4) SB21053 (last R2)
31/03/92 N/A ENGINE FIRE DUE TO
OIL ACCUMULATING IN THE ICC CAVITY.
- CLOSED- SB21053 AND SB20914 EMBODIED
AS PER BUILD SPEC 723
S - RAI 93-284
TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES IN THE ICC.
- CLOSED- SUPERSEEDED BY TCA CF-92-
03R2
I Y TCA CF-92-03R2
- P&WC
SB20957 (last R5) SB20962 (last R4) SB21065 (last R7)
21211 (last R6)
30/06/94 N/A INTERNAL OIL FIRES IN THE ICC.
- CLOSED- SBs EMBODIED AS PER BUILD
SPEC 723
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0126 Manuf. date:
JUNE 2009
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 2 of 2 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - AF0126 - Engine2 - I-DPCR (WIP).doc
I Y RAI 94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94
1000⇔2000 cycles
N/A REPLACEMENT HP TURBINE DISK
- CLOSED- HP DISK P/N 3041511 INSTALLED
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077 (last R8) SB21364 (last R1) SB21373 (last R3)
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A
REPLACEMENT OF FUEL NOZZLES
LOCKING PLATES AND “O” RINGS
- CLOSED- SBs INTRODUCED AT
MANUFACTURE
I Y ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB21100 (last R3)
all spare heaters within 02/03/01
installed p/n 10718
before 31/08/02
N/A ENGINE PW100 SERIES FUEL HEATERS
- CLOSED- FUEL HEATER P/N 10839F (Post
SB21519)
A N ENAC 02-090
TCA CF-2002-10 - - N/A INTERCOMPRESSOR CASE FIRE
- CLOSED- N/A AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21562 (last R2)
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within
2400 f/h or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
- CLOSED- MFCU P/N 3244857-15 INSTALLED
(Post SB21562)
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
20090710 Manuf. date:
JULY 2009
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 1 of 2 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - 20090710 - Propeller 1 - I-DPCR (WIP).doc
I Y FAA 93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided transfer tube
- CLOSED- COMPLIED-WITH
AS PER TRANSFER TUBE P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS
SB 14SF-61-82)
Shaft Torque Check
5000 Hrs
PCU INSPECTION/ MODIFICATION
- OPEN- INSPECTION SCHEDULED EVERY
2000 FH (prop. O/H) 1425.13 F/H TO GO
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION - CLOSED-:
NOT APPLICABLE - BLADE #1 S/N 2009060220-19 INSTALLED
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION - CLOSED-:
NOT APPLICABLE - BLADE #2 S/N 2009060574-19 INSTALLED
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION - CLOSED-:
NOT APPLICABLE - BLADE #3 S/N 2009060224-19 INSTALLED
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION - CLOSED-:
NOT APPLICABLE - BLADE #4 S/N 2009060221-19 INSTALLED
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
6000 Hrs or 3 years since February 7,
1997
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
- OPEN- TRANSFER TUBE INSPECTION SCHEDULED EVERY 2000 FH
(prop. O/H) 1425.13 F/H TO GO
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
20090710 Manuf. date:
JULY 2009
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 2 of 2 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - 20090710 - Propeller 1 - I-DPCR (WIP).doc
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
6000 Hrs or 3 years since February 7,
1997
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
- OPEN- ACTUATOR INSPECTION
SCHEDULED EVERY 2000 FH (prop. O/H)
1425.13 F/H TO GO
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
6000 Hrs or 3 years since February 7,
1997
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
- OPEN- PCU INSPECTION SCHEDULED
EVERY 2000 FH (prop. O/H) 1425.13 F/H TO GO
28/09/2003
A N FAA 2006-24-07
Scheda Analisi PA Jan 3, 2007 - CLOSED-
NOT APPLICABLE AS PER PROPELLER MODEL
A N FAA US-2011-04-02
ENAC 2011-68 ADE issued Apr 15, 2011 - CLOSED -
NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
20090711 Manuf. date:
AUGUST 2009
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 1 of 2 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - 20090711 - Propeller 2 - I-DPCR (WIP).doc
I Y FAA 93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided transfer tube
- CLOSED- COMPLIED-WITH
AS PER TRANSFER TUBE P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS
SB 14SF-61-82)
Shaft Torque Check
5000 Hrs
PCU INSPECTION/ MODIFICATION
- OPEN- INSPECTION SCHEDULED EVERY
2000 FH (prop. O/H) 1425.13 F/H TO GO
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION - CLOSED-:
NOT APPLICABLE - BLADE #1 S/N 2009060222-19 INSTALLED
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
- CLOSED-: S/N 882977-19 INSTALLED ON 31/05/10 AS PER W.O. 10/103
ALREADY MODIFIED
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION - CLOSED-:
NOT APPLICABLE - BLADE #3 S/N 2009060573-19 INSTALLED
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION - CLOSED-:
NOT APPLICABLE - BLADE #4 S/N 2009060575-19 INSTALLED
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
6000 Hrs or 3 years since February 7,
1997
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
- OPEN- TRANSFER TUBE INSPECTION SCHEDULED EVERY 2000 FH
(prop. O/H) 1425.13 F/H TO GO
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
20090711 Manuf. date:
AUGUST 2009
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 2 of 2 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - 20090711 - Propeller 2 - I-DPCR (WIP).doc
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
6000 Hrs or 3 years since February 7,
1997
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
- OPEN- ACTUATOR INSPECTION
SCHEDULED EVERY 2000 FH (prop. O/H)
1425.13 F/H TO GO
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
6000 Hrs or 3 years since February 7,
1997
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
- OPEN- PCU INSPECTION SCHEDULED
EVERY 2000 FH (prop. O/H) 1425.13 F/H TO GO
28/09/2003
A N FAA 2006-24-07
Scheda Analisi PA Jan 3, 2007 - CLOSED-
NOT APPLICABLE AS PER PROPELLER MODEL
A N FAA US-2011-04-02
ENAC 2011-68 ADE issued Apr 15, 2011 - CLOSED -
NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCR s/n 2074
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 1 of 9 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
_______________________
Approved by:
________________________
I-DPCR Components Compliance Status
A N FAA 81-21-05
- - Nov 19, 1981 N/A ARTEX ELT Battery not usable in salt environment
CLOSED: NOT APPLICABLE – SUBJECT ELT BATTERY NOT
INSTALLED
A N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782
RAI 74-225 - N/A N/A Ni-Cd batterie con celle in
polistirolo
CLOSED: NOT APPLICABLE - TEMPERATURE SENSING
INSTALLED ON BATTERIES EMBODIED
S - RAI 82-113
- - - - - CLOSED: SUPERS. BY ENAC 96-348
N N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782 - N/A N/A Ni-Cd batteries
CLOSED: CF96-21 ISSUED TO CANCEL THE APPLICABILITY OF
FAA 72-19-04
S - RAI 88-052
- - - - - SUPERS. BY ENAC 88-096
R Y RAI 88-096
FAR 43 Appendix E
Norma di lavoro NL-CL-34-06 19/11/2005 24 Months ALTIMETER AND STATIC
PRESSURE SYSTEM OPEN
TEST CARRIED OUT ON SEP 30, 2009 (NEXT DUE SEP 28, 2011)
I Y ENAC 96-052
FAA FAR 91.21 - N/A N/A USE OF PORTABLE ELETTRONIC DEVICES
CLOSED: AFM UPDATED – CREW INFORMED
N N ENAC 96-348
FAA 96-20-07 Amdt 39-9773 -
Within 500 Hrs (TIS) or 12 mths from 14/11/96
100 Hrs funzion. 24 Months
COMBUSTION CHAMBER DECAY TEST (JANITROL)
CLOSED: NOT APPLICABLE - HEATER MODEL B4500
(CERAMIC COMBUSTION TUBE) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCR s/n 2074
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 2 of 9 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
_______________________
Approved by:
________________________
I-DPCR Components Compliance Status
N N ENAC 97-167
FAA 97-11-10 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N TCCA CF-95-16
ENAC 97-221 Marathon Power SB 111692-014 27/07/96 N/A
PCB SERIES PC-250 MODIFICATION OR
REMOVAL
CLOSED: NOT APPLICABLE AS PER INVERTER INSTALLED
(Serie MSI-800)
N N ENAC 97-274
FAA 97-18-03 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N ENAC 99-231
FAA 99-08-21 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
S - ENAC 00-018
FAA 99-23-22 Norma di Lavoro NL-CL-34-07 Apr 17, 2000 Every 90 days
TRANSPONDER MODO “C”
INSPECTION/TEST
CLOSED: SUPERSEDED BY ENAC 00-209
N N ENAC 00-209
FAA 99-23-22 Amdt. 39-11686
Engineering InstructionEI 004/00 18/05/00 N/A TRANSPONDER MODO
“C”
CLOSED: NOT APPLICABLE AD RESCINDED APR. 12, ‘00
SUPERSEDES ENAC 00-018
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCR s/n 2074
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 3 of 9 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
_______________________
Approved by:
________________________
I-DPCR Components Compliance Status
S - ENAC 01-173
FAA 2001-08-01 Scheda Analisi PA May 2, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04
CLOSED: SUPERSEDED BY ENAC 01-368
A N ENAC 01-368
FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04 P/N installed on A/C: J20C30
CLOSED: NOT APPLICABLE AS PER FUEL SHUT-OFF P/N
INSTALLED Supersedes ENAC 01-173
N N ENAC 01-442
FAA 2001-18-05 - Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.
CLOSED: NOT APPLICABLE PER P/N
I Y ENAC 01-470
FAA 2001-22-14 SoREM DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER
DISCHARGER CLOSED: P/N AFFECTED
CHECKED. WALTER KIDDE CARTRIDGES INSTALLED ON
I Y TCCA CF-2002-14
ENAC 02-167
BOMBARDIER SB215-3108 SB215-4234
SoREM BM-CL-61-4234
04/03/2003 N/A
PROPELLER CONTROL UNIT
BACKUP PRESSURE RELIEF VALVE
CLOSED: SB 215-4234 INCORPORATED IN PRODUCTION
I Y ENAC 03-067
FAA 2003-04-06 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ -850/ -851
CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND
7510100-731 (#2) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCR s/n 2074
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 4 of 9 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
_______________________
Approved by:
________________________
I-DPCR Components Compliance Status
28/09/2003
N N FAA 2003-23-05
ENAC 2004-003 - December 24, 2005 N/A Titeflex Corporation, Tubi Flessibili
CLOSED: NOT APPLICABLE
HOSES INSTALLATI P/N 114040-4
R Y FAA
2004-21-05 Amdt.39-13826
- Scheda Analisi PA DT-CL-21-01
A 500 heater Hrs or 100 heater Hrs TIS
since 19/11/04 (whichever occurs
later)
100 Hrs (TIS) or
24 Months
PRESSURE DECAY TEST ed Operational Test del
CABIN HEATER (JANITROL)
OPEN HEATER TIME IN
SERVICE CHECKED: 5.40 HOURS
TEST NOT YET PERFORMED
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
P/N installed on A/C: J20C30
CLOSED: NOT APPLICABLE BY
COMPONENT P/N 91E18-1 INSTALLED
R Y EASA 2006-0265 - Scheda Analisi PA
ESP-4-34-001 Within
Mar 13, 2007 24 Months MODE “S” and “C” TRANSPONDERS CHECK
OPEN LAST PERFORMANCE
DURING ANNUAL INSPECTION
07/06/2011. (COVERED BY ANN-AT-10)
NEXT DUE: ANNUAL INSPECTION
A N EASA 2006-0269
- Scheda Analisi PA - - MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCR s/n 2074
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 5 of 9 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
_______________________
Approved by:
________________________
I-DPCR Components Compliance Status
A N FAA 2006-18-08 - Scheda Analisi AD Oct. 11, 2006 - GOODYEAR
NOSE WHEEL TIRES
CLOSED: NOT APPLICABLE AS PER
GOODYEAR TIRES P/N INSTALLED
A N FAA 2006-19-04
- Scheda Analisi AD - - MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
N N FAA 2006-22-05
ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU
CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND
7510100-731 (#2) INSTALLED
A N EASA 2006-0366
- Scheda Analisi PA Dec 14, 2006 - LIFE RAFT CLOSED: NOT
APPLICABLE AS PER AIRCRAFT MODEL
A N EASA 2006-0286R1
- Scheda Analisi PA Sep 9, 2006 - Oxygen Cylinders CLOSED: NOT
APPLICABLE AS PER P/N INSTALLED
A N EASA 2007-0256
- Scheda Analisi PA Sep 19, 2007 - Seat Restraint System CLOSED: NOT
APPLICABLE AS PER P/N INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCR s/n 2074
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 6 of 9 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
_______________________
Approved by:
________________________
I-DPCR Components Compliance Status
A N EASA 2007-0294
ENAC 2009-060 Scheda Analisi PA - - APU Turbine wheel life limit reduction
CLOSED: NOT EFFECTIVE AS PER
APU NOT INSTALLED ON SOREM CL415
FLEET
N N EASA 2009-0200
- Scheda Analisi AD Sep 22, 2010 N/A Navigation – Mode A/C Transponder – Check /
Modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N FAA 2009-20-10
- Scheda Analisi AD Jan 17, 2010 N/A Autopilot – servo motors modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
S - CF 2009-42 - SOREM ESB-4-32-4414 (SMJC 063)
Part I within 50Fh Part II: within 750 Fc
Part III: every 750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
A/C DELIVERED WHEN AD REV. 1 WAS
ALREADY ISSUED.
R Y CF 2009-42R1 - SOREM ESB-4-32-4414 - Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
OPEN AD COVERED BY INAER SMJC 063 (723 FCY TO
GO)
Y N EASA 2009-0251
- Scheda Analisi AD Nov 26, 2009 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER S/N
INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCR s/n 2074
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 7 of 9 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
_______________________
Approved by:
________________________
I-DPCR Components Compliance Status
Y N EASA 2009-0262R1
Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A Portable Halon 1211 Fire Extinguisher
NOT EFFECTIVE AS PER S/N NOT INSTALLED
Y N EASA 2009-0278
- Scheda Analisi AD Jan 22, 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N TCA CF-2009-44
- Scheda Analisi AD Jul 1, 2011 N/A ELT-Potential Failure to Transmit the Required 406MHz Coded Signal
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N EASA 2010-003R1
- Scheda Analisi AD 18 Apr, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
Y N EASA
2010-0062R1
- Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
NOT EFFECTIVE AS PER P/N NOT INSTALLED
A Y FAA 2010-07-02
- Scheda Analisi AD 31 Oct 2012 N/A Honeywell Primus II RNZ 850()/-851
CARRIED OUT ON MAY 28, 10. BOTH INU # 1
AND # 2 ARE IN COMPLIANCE
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCR s/n 2074
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 8 of 9 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
_______________________
Approved by:
________________________
I-DPCR Components Compliance Status
N N EASA 2010-0067
- Scheda Analisi AD 26 Apr, 2010 N/A TDR-94 and TDR-94D transponders
NOT EFFECTIVE AS PER P/N NOT INSTALLED
N N EASA 2010-30
Scheda Analisi SIB N/A N/A Risks in Transporting
Lithium Batteries in Cargo by Aircraft
NOT APPLICABLE SINCE INAER FLEET IS
NOT OPERATING IN CARGO TRANSPORT
CONFIGURATION
N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer –
Erroneous Airspeed and Altitude Indications
NOT APPLICABLE AS PER A/C TYPE, REFER
TO ADE ISSUED DATED NOV 09, 2010
N N FAA 2011-01-09
Scheda Analisi AD 9/06/2011 N/R
B/E Aerospace protective breathing equipment P/N 119003-11 inspection for
B/A Aerospace S.B. 119003-35-6 compliance.
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
N N EASA 2011-0043
Scheda Analisi AD 30/04/2013 N/R Gables Engineering Mode S Transponder Control Panel
Modification
CLOSED: NOT APPLICABLE AS PER
P/N NOT INSTALLED ON THE A/C TYPE
N N EASA 2011-0090R1
ENAC 2011-202 Scheda Analisi AD 27/07/2011 N/R Oxygen mask regulator CLOSED: NOT
APPLICABLE AS PER P/N NOT INSTALLED ON
THE A/C TYPE
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCR s/n 2074
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 9 of 9 S Superseded N Not effective
Date:
Sept 9, 2011 Prepared by:
_______________________
Approved by:
________________________
I-DPCR Components Compliance Status
N N EASA 2011-0103
Scheda Analisi AD 03/12/2011 N/R ELT TRI-BAND Antennas
P/N 21-41 ( ) series Mod/Replacement
CLOSED: NOT APPLICABLE AS PER
P/N NOT INSTALLED ON THE A/C TYPE
N N FAA
2011-11-04
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N EASA 2010-0204
ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N FAA 2011-14-08
Scheda Analisi AD Aug 19,2014 or
6500 FH from Aug 19,2011
N/A B/E Aerospace pax oxy mask inspection
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
R Y TCCA CF-2011-35
- ESB-4-32-A4451 Rev 01
First incorporation: Within 50 Flight Hrs
upon receipt of Bombardier SB 215-
A4451
To be repeated every 165 land landings
Inspection of the MLG Upper Member forward lug using eddy current method
FIRST INCORPORATION:
CLOSED (REF TO WO 11/193);
REPETITIVE ACTION: OPEN; TO GO: 114
LANDINGS
A Y TCCA CF-2011-35
- ESB-4-32-A4450 Rev 01 November 11, 2011 N/A
Inspection of the MLG Upper Member forward lug
using liquid penetrant method
OPEN
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCT s/n 2029
Delivery Date: Feb 27, 98
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 4
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCT Compliance Status
A N FAA
77-17-13 - - - - NLG DOORS
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N FAA
77-13-05 - - - -
MISSING RIVETS IN BULKHEAD
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N TCCA
CF-90-11R2 FAA 93-16-06R2
Bombardier SB215-A435
SoREM Scheda analisi AD
JUNE. 10, 1994 N/A
RUDDER-AILERON INTERCONNECT TAB (TO PREVENT POSSIBILE
FLUTTER)
CLOSED: NOT EFFECTIVE AS PER POWERED AILERON
SYSTEM INSTALLED
S TCCA
CF-92-22
FAA 94-04-02 TCCA CF-2003-
02
Bombardier SB215-A3040
SoREM Scheda analisi AD
- N/A ENGINE REAR
MOUNT STRUTS
CLOSED: SUPERSEDED BY AD CF-2003-02
I Y ENAC 95-064
TCCA CF-92-10R1
P&WC: SB20914 SB21113 SB21211 SB21314
Bombardier SB215-A3060
SoREM Scheda Analisi PA
N/A ENGINE FIRE-WIRE DETECTION LOOP
CLOSED: AD COMPLIED WITH
ENGINE FIRE DETECTION SYSTEM CONNECTED TO AIRCRAFT FIRE WARNING
SYSTEM
I Y FAA
97-11-08 - - - -
AFM - LIMITATION SECTION - POWER
LEVERS
CLOSED: AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION SECTION
PAGE 8
A N TCCA
CF-96-02R1 ENAC 1999-268 - - - -
CLOSED: AD ISSUED JUST TO CANCEL PREVIOUS REVISION
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCT s/n 2029
Delivery Date: Feb 27, 98
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 4
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCT Compliance Status
R N ENAC 00-265
FAA 2004-03-13 - - - MLG AXLES NOT APPLICABLE AS PER AD
EFFECTIVITY
A N TCCA
CF-2002-14 FAA 2004-26-08
ENAC 02-167
Bombardier SB215-4234
SoREM DT CL-61-4234
MARCH 04, 2003 N/A PCU BACKUP
PRESSURE VALVE
NOT APPLICABLE AS PER VALVE INCORPORATED AT
MANUFACTURE
R N ENAC 00-496
FAA 2002-12-12 - - - WING TO FUSELAGE
FRAME ANGLES NOT APPLICABLE AS PER AD
EFFECTIVITY
S - FAA
2003-04-06 ENAC 03-067
FAA 2006-22-05
SoREM
DT-CL-34-05 DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II
RNZ-850/ -851
REF TO COMPONENTS
SUPERSEDED BY FAA 2006-22-05
R Y TCCA
CF-2003-02 FAA 2004-10-04
ENAC 03-251
Bombardier SB215-A4287R2
SoREM BM-CL-71-A4287
BM-CL-71-A4287R2 SMJC 31 and 32
WITHIN 50 F/H SINCE FEBRUARY
28, 2003
EVERY 250 F/H REPETITIVE ACTION
FOLLOWED BY SoREM SMJC #31 and #32
ENGINE REAR MOUNT STRUTS
OPEN: CARRIED OUT WITH SMJC 31 & SMJC 32 ON 08/07/2011 (W/O
11/129); 39.52 FH TO GO
28/09/2003
R Y FAA
2004-21-05 -
SCHEDA ANALISI Disposizione Tecnica
DT-CL-21-01
A 500 heater Hrs Total or 100 heater hrs TIS from 19/11/04
(whichever occurs later)
100 Hrs funzion. 24 Months
PRESSURE DECAY TEST and CABIN
HEATER (JANITROL)
OPERATIONAL TEST
REF TO COMPONENTS
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCT s/n 2029
Delivery Date: Feb 27, 98
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 3 of 4
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCT Compliance Status
A N FAA
2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
REGOLATORE CARBURANTE CON VALVOLE SHUTOFF
A/B/C 14D11 o A/B/C/P 23D04
REF TO COMPONENTS
R N FAA
2005-18-05 - - - -
LOWER CAPS OF THE WING FRONT SPAR AND
REAR SPAR
CLOSED NOT APPLICABLE AS PER AD EFFECTIVITY
A N EASA
2006-0375 - Scheda Analisi AD Dec. 29, 2006 -
CARLING TECHNOLOGIES
SWITCHES
CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY
N N FAA
2006-22-05 EASA 2006-479 Scheda Analisi AD - N/A
INTEGRATED NAVIGATION UNITS
REF TO COMPONENTS
Supersedes FAA 2003-04-06
R Y TCCA
CF-2008-29 FAA 2009-05-04 ENAC 2008-316
SMJC-60 Mar 8, 2009
BEFORE AND AFTER EVERY FIRE SEASON
OR AT SIX MONTH INTERVAL,
WHICHEVER IS SHORTER TIME
PERIOD
RUDDER LOWER TORQUE TUBE UPPER BEARING
OPEN: AD COVERED BY SMJC 60 CARRIED OUT ON 31/05/2011(W/O
11/099) NEXT DUE WITHIN NOV 30, 11
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCT s/n 2029
Delivery Date: Feb 27, 98
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 4 of 4
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCT Compliance Status
R Y TCCA
CF-2010-38R2 ENAC 2011-88
Bombardier SB 215 -A4424 Jun 01, 2011
FIRST INSPECTION WITHIN 50 FC FROM
20 DEC 2010; THEREAFTER REPEAT
PERRFORM AN INSPECTION BEFORE
100 FC WITH TERMINATING ACTION NOT LATER THAN Jun
01, 2011.
INSPECTION OF THE EMERGENCY WATER DUMP
PULLEY BRACKET AND STRUCTURE
CLOSED SB 215-A4424 PART B EMBODIED
ON 31/05/2011 (W/0 11/099)
R Y TCCA
CF-2011-35
Bombardier SB 215-A4450;
Bombardier SB 215-A4451
ESB-4-32-A4450 Rev 01;
ESB-4-32-A4451 Rev 01;
Ref. To AD-PA Compliance Components
Ref. To AD-PA Compliance Components
Liquid Penetrant & Eddy Current Inspection on MLG Upper Member
Forward Lug
REF. TO AD-PA COMPLIANCE COMPONENTS
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0014 Manuf. date:
DECEMBER 5, 1996
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCT righr engine
I Y TCA
CF-90-21 -
P&WC SB20355R1
SB20897 30/04/91 N/A
O-RING DETERIORATION DURING FUEL FILTER COVER INSTALLATION
- CLOSED – AD COMPLIED WITH
I Y RAI
91-296 TCA CF-90-22R1
P&WC SB21018R1
30/06/94 N/A OIL SYSTEM INSPECTION
DUE TO BEARING DETERIORATION
- CLOSED – AD COMPLIED WITH
I Y TCA
CF-91-02 -
P&WC SB20946R1
31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS - CLOSED –
AD COMPLIED WITH
I Y RAI
91-347 TCA CF-91-26R1
P&WC SB20914R3
SB21053 31/03/92 N/A
TO IMPROVE THE RETENTION OF THE
P2.5/P3 TUBE ASSEMBLY.
- CLOSED – AD COMPLIED WITH
S RAI
93-284 TCA CF-92-03R1 - - N/A
INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
- CLOSED – SUPERSEDED BY TCCA CF-92-03R2
I Y TCA
CF-92-03R2 -
P&WC SB20957R3 SB20962R2
SB21065
30/06/94 N/A INTERNAL OIL FIRES IN
THE ICC. - CLOSED –
AD COMPLIED WITH
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0014 Manuf. date:
DECEMBER 5, 1996
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCT righr engine
A N RAI
94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94
1000⇔2000 cycles N/A
REPLACEMENT HP TURBINE DISK
- CLOSED – NOT EFFECTIVE FOR
ENGINES S/N 109022 AND SUBSEQUENT
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077R7 SB21364R1 SB21373R3
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
- CLOSED – AD COMPLIED WITH
A N ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB 21100R2
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES
FUEL HEATERS
- CLOSED – NOT APPLICABLE FOR
ENGINES S/N 109036 AND SUB’S
A N ENAC 02-090
TCA CF-2002-10 - CLOSED –
N/A AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21562R0/R1/R2
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within 2400 f/h
or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
- CLOSED – AD COMPLIED WITH
(NO REPETETIVE ACTION)
28/09/2003
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0095 Manuf. date:
DEC 2006
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCT Left Engine
I Y TCCA
CF-90-21 -
P&WC SB20355R1
SB20897 30/04/91 N/A
O-RING DETERIORATION DURING FUEL FILTER COVER INSTALLATION
- CLOSED - AD COMPLIED WITH AT
DELIVERY
I Y TCCA
CF-90-22R1 RAI 91-296
P&WC SB21018R1
30/06/94 N/A OIL SYSTEM INSPECTION
DUE TO BEARING DETERIORATION
- CLOSED - AD COMPLIED WITH AT
DELIVERY
A N TCCA
CF-91-02 -
P&WC SB20946R1
31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS - CLOSED –
N/A DUE TO ENGINE S/N
I Y TCCA
CF-91-26R1 RAI 91-347
P&WC SB20914R3
SB21053 31/03/92 N/A
TO IMPROVE THE RETENTION OF THE
P2.5/P3 TUBE ASSEMBLY.
- CLOSED - AD COMPLIED WITH AT
DELIVERY
S TCCA
CF-92-03R1 RAI 93-284 - - N/A
INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
- CLOSED – SUPERSEDED BY TCCA CF-92-03R2
I Y TCCA
CF-92-03R2 -
P&WC SB20957R3 SB20962R2
SB21065
30/06/94 N/A INTERNAL OIL FIRES IN
THE ICC.
- CLOSED - AD COMPLIED WITH AT
DELIVERY
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0095 Manuf. date:
DEC 2006
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCT Left Engine
A N TCCA
CF-94-01
FAA 94-03-02 Amdt 39-8808
RAI 94-001 P&WC SIL 307
Since 14/01/94
1000⇔2000 cycles N/A
REPLACEMENT HP TURBINE DISK
- CLOSED – NOT EFFECTIVE FOR
ENGINES S/N 109022 AND SUBSEQUENT
I Y TCCA
CF-96-22 ENAC 96-353
P&WC SB21077R7 SB21364R1 SB21373R3
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
- CLOSED - ALL SBs RELATED TO AD
EMBODIED AD COMPLIED WITH
A N TCCA
CF-2000-34 FAA 2003-16-04
ENAC 01-065 P&WC
SB 21100R2
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES
FUEL HEATERS
- CLOSED – NOT EFFECTIVE FOR
ENGINES S/N 109036 AND SUB’S
A N TCCA
CF-2002-10 ENAC 02-090
P&WC SB 21914R4
Next shop visit or before 31/12/03
Whichever occurs first
N/A PW118, PW120 and PW121
INTERCOMPRESSOR CASE FIRE
- CLOSED – N/A AS PER ENGINE MODEL
I Y TCCA
CF-2002-34 FAA 2004-20-01
ENAC 02-448
P&WC SB21562R0/R1/R2
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within 2400 f/h
or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
- CLOSED - POST SB21562
28/09/2003
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
970227 Manuff. date:
FEB 1997
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 2
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCT right propeller
I Y FAA
93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided
transfer tube
- CLOSED – AD COMPLIED WITH
P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs.
PCU INSPECTION/ MODIFICATION
OPEN: PCU COMPLIANT WITH HS-SB14SF-61-82.
CHECK COVERED BY O/H PROCEDURE (2000FH)
932.30 TO GO
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
NOT APPLICABLE FOR BLADE #1 S/N 9910019-19
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
NOT APPLICABLE FOR BLADE #2 S/N 888109-19
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
NOT APPLICABLE FOR BLADE #3 S/N 2008061377
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
NOT APPLICABLE FOR BLADE #4 S/N 200106023-19
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
970227 Manuff. date:
FEB 1997
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 2
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCT right propeller
R Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
TRANSFER TUBE INSPECTED DURING LAST
O/H. (every 2000 FH) 1394.34 FH TO GO
R Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
ACTUATOR INSPECTED DURING LAST O/H. (every
2000 FH) 1394.34 FH TO GO
R Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
PCU INSPECTED DURING LAST O/H on 16/09/03.
(every 2000 FH) 932.30 TO GO
28/09/2003
A N FAA
2006-24-07 Scheda Analisi PA Jan 3, 2007
NOT APPLICABLE AS PER PROPELLER MODEL
A N FAA
US-2011-04-02 ENAC 2011-68 ADE issued Apr 15, 2011
NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
930508 Manuf. date:
17/05/93
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 2
S Superseded N Not effective
Date:
Sep 09, 10
Prepared by:
________________________
Approved by:
________________________
I-DPCT Left Propeller
I Y FAA
93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided
transfer tube CLOSED: AD COMPLIED WITH
P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs.
PCU INSPECTION/ MODIFICATION
OPEN:
PCU INSPECTION PERFORMED EVERY O/H
(NEXT DUE WITHIN 1381.12 FH)
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLOSED: PERFORMED by SISAM ASB –A92R1 FOR
BLADE #1 S/N 879627-19
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLOSED: PERFORMED by SISAM ASB –A92R1 FOR BLADE #2 S/N 879628-19
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLOSED: PERFORMED by SISAM ASB –A92R1 FOR BLADE #3 S/N 879626-19
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #4 S/N
200105014-19
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
930508 Manuf. date:
17/05/93
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 2
S Superseded N Not effective
Date:
Sep 09, 10
Prepared by:
________________________
Approved by:
________________________
I-DPCT Left Propeller
R Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRANSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 343.00)
R Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRANSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: ACTUATOR INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 939.31)
R Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRANSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: PCU INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 1381.12
FH)
28/09/2003
A N FAA
2006-24-07 Scheda Analisi PA Jan 3, 2007
CLOSED: NOT APPLICABLE AS PER PROPELLER
MODEL
A N FAA
US-2011-04-02 ENAC 2011-68 ADE issued Apr 15, 2011
NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCT s/n 2029
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCT Components Compliance Status
A N FAA
81-21-05 - - Nov 19, 1981 N/A
ARTEX ELT Battery not usable in salt environment
CLOSED: NOT APPLICABLE – SUBJECT ELT BATTERY NOT
INSTALLED
A N TCCA
CF-96-21
FAA 72-19-04 Amdt. 39-1782
RAI 74-225 - N/A N/A
Ni-Cd batterie con celle in polistirolo
CLOSED: NOT APPLICABLE - TEMPERATURE SENSING
INSTALLED ON BATTERIES EMBODIED
S - RAI
82-113 - - - - -
CLOSED: SUPERS. BY ENAC 96-348
N N TCCA
CF-96-21
FAA 72-19-04 Amdt. 39-1782 - N/A N/A Ni-Cd batteries
CLOSED: CF96-21 ISSUED TO CANCEL THE APPLICABILITY OF
FAA 72-19-04
S - RAI
88-052 - - - - - SUPERS. BY ENAC 88-096
R Y RAI
88-096 FAR 43
Appendix E Norma di lavoro
NL-CL-34-06 19/11/2005 24 Months
ALTIMETER AND STATIC PRESSURE SYSTEM
OPEN: TEST CARRIED OUT ON JUL 29, 2010, W.O. 09/382 (NEXT
DUE WITHIN JUL 27, 2012)
I Y ENAC 96-052
FAA FAR 91.21 - N/A N/A USE OF PORTABLE
ELETTRONIC DEVICES CLOSED: AFM UPDATED – CREW
INFORMED
N N ENAC 96-348
FAA 96-20-07 Amdt 39-9773 -
Within 500 Hrs (TIS) or 12 mths from 14/11/96
100 Hrs funzion. 24 Months
COMBUSTION CHAMBER DECAY TEST (JANITROL)
CLOSED: NOT APPLICABLE - HEATER MODEL B4500
(CERAMIC COMBUSTION TUBE) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCT s/n 2029
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCT Components Compliance Status
N N ENAC 97-167
FAA 97-11-10 - - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N TCCA
CF-95-16 ENAC 97-221
Marathon Power SB 111692-014
27/07/96 N/A PCB SERIES PC-250 MODIFICATION OR
REMOVAL
CLOSED: NOT APPLICABLE AS PER INVERTER INSTALLED
(Serie MSI-800)
N N ENAC 97-274
FAA 97-18-03 - - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - AVOX OXYGEN MASKS
INSTALLED
N N ENAC 99-231
FAA 99-08-21 - - N/A
PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - AVOX OXYGEN MASKS
INSTALLED
S - ENAC 00-018
FAA 99-23-22 Norma di Lavoro
NL-CL-34-07 Apr 17, 2000 Every 90 days TRANSPONDER MODO
“C” INSPECTION/TEST
CLOSED: SUPERSEDED BY ENAC 00-209
N N ENAC 00-209
FAA 99-23-22 Amdt. 39-11686
Engineering Instruction
EI 004/00 18/05/00 N/A
TRANSPONDER MODO “C”
CLOSED: NOT APPLICABLE AD RESCINDED APR. 12, ‘00
SUPERSEDES ENAC 00-018
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCT s/n 2029
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 3 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCT Components Compliance Status
S - ENAC 01-173
FAA 2001-08-01 Scheda Analisi PA May 2, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04
CLOSED: SUPERSEDED BY ENAC 01-368
A N ENAC 01-368
FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
P/N installed on A/C: J20C30
CLOSED: NOT APPLICABLE AS PER FUEL SHUT-OFF P/N
INSTALLED Supersedes ENAC 01-173
N N ENAC 01-442
FAA 2001-18-05 - Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.
CLOSED: NOT APPLICABLE PER P/N
I Y ENAC 01-470
FAA 2001-22-14 SoREM
DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER
DISCHARGER
CLOSED: P/N AFFECTED CHECKED. WALTER KIDDE
CARTRIDGES INSTALLED ON
I Y TCCA
CF-2002-14 ENAC 02-167
BOMBARDIER SB215-3108 SB215-4234
SoREM BM-CL-61-4234
04/03/2003 N/A
PROPELLER CONTROL UNIT
BACKUP PRESSURE RELIEF VALVE
CLOSED: SB 215-4234 INCORPORATED
I Y ENAC 03-067
FAA 2003-04-06 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II
RNZ -850/ -851
CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND
7510100-731 (#2) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCT s/n 2029
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 4 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCT Components Compliance Status
28/09/2003
N N FAA
2003-23-05 ENAC 2004-003 ENAC-2004-073
- December 24, 2005 N/A Titeflex Corporation,
Tubi Flessibili
CLOSED: NOT APPLICABLE
HOSES INSTALLATI P/N 114040-4
R Y FAA
2004-21-05 Amdt.39-13826
- Scheda Analisi PA DT-CL-21-01
A 500 heater Hrs or 100 heater Hrs TIS
since 19/11/04 (whichever occurs
later)
100 Hrs (TIS) or
24 Months
PRESSURE DECAY TEST ed Operational Test del
CABIN HEATER (JANITROL)
OPEN: HEATER TIME IN SERVICE CHECKED:
309.54 HOURS TEST NOT YET PERFORMED
A N FAA
2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
CLOSED: NOT APPLICABLE AS PER HEATER INSTALLED
R Y EASA
2006-0265 -
Scheda Analisi PA ESP-4-34-001
Within Mar 13, 2007
24 Months MODE “S” and “C”
TRANSPONDERS CHECK
OPEN: CARRIED OUT DURING LAST ANNUAL CHECK W.O. 09/382 ON JUL 29, 2010 NEXT DUE
WITHIN JUL 2012
A N EASA
2006-0269 - Scheda Analisi PA - -
MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
A N FAA
2006-18-08 - Scheda Analisi AD Oct. 11, 2006 -
GOODYEAR NOSE WHEEL TIRES
CLOSED: NOT APPLICABLE AS PER
GOODYEAR TIRES NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCT s/n 2029
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 5 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCT Components Compliance Status
A N FAA
2006-19-04 - Scheda Analisi AD - -
MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER PART NUMBER NOT
INSTALLED
N N FAA
2006-22-05 ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU
CLOSED: NOT APPLICABLE AS PER
COMPONENT MODIFIED (REF TO
FAA-2003-04-06)
A N EASA
2006-0366 - Scheda Analisi PA Dec 14, 2006 - LIFE RAFT
CLOSED: NOT APPLICABLE AS PER
AIRCRAFT MODEL
A N EASA
2006-0286R1 - Scheda Analisi PA Sep 9, 2006 - Oxygen Cylinders
CLOSED: NOT APPLICABLE: P/N NOT
INSTALLED
A N EASA
2007-0256 - Scheda Analisi PA Sep 19, 2007 - Seat Restraint System
CLOSED: NOT APPLICABLE: P/N NOT
INSTALLED
A N EASA
2007-0294 ENAC 2009-060 Scheda Analisi PA - -
APU Turbine wheel life limit reduction
CLOSED: NOT EFFECTIVE AS PER
APU NOT INSTALLED ON SOREM CL415
FLEET
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCT s/n 2029
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 6 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCT Components Compliance Status
N N EASA
2009-0200 - Scheda Analisi AD Sep 22, 2010 N/A
Navigation – Mode A/C Transponder – Check /
Modification
CLOSED: NOT EFFECTIVE: P/N NOT
INSTALLED
N N FAA
2009-20-10 - Scheda Analisi AD Jan 17, 2010 N/A
Autopilot – servo motors modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
S - CF 2009-42 - SOREM ESB-4-32-4414
(SMJC 063)
Part I within 50Fh Part II: within 750 Fc Part III: every 750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
CLOSED: SUPERSEDED BY CF
2009-42R1 (PART I CARRIED OUT ON NOV
26, 2009)
R Y CF 2009-42R1 - SOREM ESB-4-32-
4414R1 - Every 750 Flight
cycles Special Inspection of
Accumulator Screw Caps
OPEN: AD COVERED BY SMJC-63
PERFORMED ON 19/04/2011 (W/O 11/066)
596 FC TO GO
A N EASA
2009-0251 - Scheda Analisi AD Nov 26, 2009 N/A
Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE: S/N NOT
INSTALLED
A N EASA
2009-0262R1 Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A
Portable Halon 1211 Fire Extinguisher
NOT EFFECTIVE: S/N NOT INSTALLED
A N EASA
2009-0278 - Scheda Analisi AD Jan 22, 2010 N/A
Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCT s/n 2029
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 7 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCT Components Compliance Status
N N TCA
CF-2009-44 - Scheda Analisi AD Jul 01, 2011 N/A
ELT-Potential Failure to Transmit the Required 406MHz Coded Signal
CLOSED: NOT EFFECTIVE: P/N NOT
INSTALLED
N N EASA
2010-003R1 - Scheda Analisi AD 18 Apr, 2010 N/A
TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE : P/N NOT
INSTALLED
Y N EASA
2010-0062R1 - Scheda Analisi AD 14 Apr 2010 N/A
Portable Halon 1211 Fire Extinguisher
NOT EFFECTIVE: P/N NOT INSTALLED
A Y FAA
2010-07-02 - Scheda Analisi AD 31 Ott 2012 N/A
Honeywell Primus II RNZ 850()/-851
INU #1 COMPLIED INU #2 TO BE
PERFOMED WITHIN OCT 31, 12”
N N EASA
2010-0067 - Scheda Analisi AD 26 Apr, 2010 N/A
TDR-94 and TDR-94D transponders
CLOSED - NOT EFFECTIVE: P/N NOT
INSTALLED
N N EASA
2010-30 Scheda Analisi SIB N/A N/A
Risks in Transporting Lithium Batteries in Cargo by
Aircraft
CLOSED - NOT APPLICABLE SINCE
INAER FLEET IS NOT OPERATING IN CARGO
TRANSPORT CONFIGURATION
N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer –
Erroneous Airspeed and Altitude Indications
CLOSED - NOT APPLICABLE AS PER A/C TYPE, REFER TO ADE ISSUED DATED
NOV 09, 2010
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCT s/n 2029
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 8 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCT Components Compliance Status
N N FAA
2011-01-09 Scheda Analisi AD 9/06/2011 N/R
B/E Aerospace protective breathing equipment P/N 119003-11 inspection for
B/A Aerospace S.B. 119003-35-6 compliance.
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
N N EASA
2011-0043 Scheda Analisi AD 30/04/2013 N/R
Gables Engineering Mode S Transponder Control Panel
Modification
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N EASA
2011-0090R1 ENAC 2011-202 Scheda Analisi AD 27/07/2011 N/R Oxygen mask regulator
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N EASA
2011-0103 Scheda Analisi AD 03/12/2011 N/R
ELT TRI-BAND Antennas P/N 21-41 ( ) series Mod/Replacement
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N FAA
2011-11-04
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire
Extinguisher
NOT EFFECTIVE AS PER P/N NOT INSTALLED
N N EASA
2010-0204 ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A
TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCT s/n 2029
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE
DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 9 of 9
S Superseded N Not effective
Date:
Sep 09, 11
Prepared by:
________________________
Approved by:
________________________
I-DPCT Components Compliance Status
R Y TCCA
CF-2011-35 - ESB-4-32-A4451 Rev 01
First incorporation: Within 50 Flight Hrs
upon receipt of Bombardier SB 215-
A4451
To be repeated every 165 land landings
Inspection of the MLG Upper Member forward lug using
eddy current method
FIRST INCORPORATION:
CLOSED (REF TO WO 11/195 ON 22/07/11);
REPETITIVE ACTION: 91 LL TO GO
A Y TCCA
CF-2011-35 - ESB-4-32-A4450 Rev 01 November 11, 2011 N/A
Inspection of the MLG Upper Member forward lug using
liquid penetrant method
OPEN
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCU s/n 2030
Delivery Date: Jun ‘98
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 1 of 4 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCU Compliance Status
A N FAA 77-17-13
- - - - NLG DOORS CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY
A N FAA 77-13-05
- - - - MISSING RIVETS IN BULKHEAD
CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY
A N TCCA CF-90-11R2 FAA 93-16-06R2
Bombardier SB215-A435
SoREM Scheda analisi AD
JUNE. 10, 1994 N/A RUDDER-AILERON
INTERCONNECT TAB (TO PREVENT POSSIBILE
FLUTTER)
CLOSED: NOT EFFECTIVE AS PER POWERED AILERON SYSTEM
INSTALLED
S TCCA CF-92-22
FAA 94-04-02
Bombardier SB215-A3040
SoREM Scheda analisi AD
- N/A ENGINE REAR MOUNT STRUTS
CLOSED: SUPERSEDED BY AD CF-2003-02
I Y ENAC 95-064
TCCA CF-92-10R1
P&WC: SB20914 SB21113 SB21211 SB21314
Bombardier SB215-A3060
SoREM Scheda Analisi PA
N/A ENGINE FIRE-WIRE DETECTION LOOP
CLOSED: AD COMPLIED WITH ENGINE FIRE DETECTION SYSTEM CONNECTED TO AIRCRAFT FIRE WARNING
SYSTEM
I Y FAA 97-11-08
- - - - AFM - LIMITATION SECTION - POWER
LEVERS
CLOSED: AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION
SECTION PAGE 8
A N TCCA CF-96-02R1
ENAC 1999-268 - - - - CLOSED: AD ISSUED JUST TO CANCEL PREVIOUS REVISION
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCU s/n 2030
Delivery Date: Jun ‘98
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 2 of 4 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCU Compliance Status
R N ENAC 00-265
FAA 2004-03-13 - - - MLG AXLES CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY
A N TCCA CF-2002-14
FAA 2004-26-08 ENAC 02-167
Bombardier SB215-4234
SoREM DT CL-61-4234
MARCH 04, 2003 N/A PCU BACKUP PRESSURE VALVE
CLOSED: NOT APPLICABLE AS PER VALVE INCORPORATED AT
MANUFACTURE
R N ENAC 00-496
FAA 2002-12-12 - - - WING TO FUSELAGE FRAME ANGLES
CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY
S - FAA 2003-04-06
ENAC 03-067 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ-850/ -851
REF TO COMPONENTS
CLOSED: SUPERSEDED BY FAA 2006-22-05
R Y TCCA CF-2003-02
FAA 2004-10-04 ENAC 03-251
Bombardier SB215-A4287R2
SoREM BM-CL-71-A4287
BM-CL-71-A4287R2 SMJC 31 and 32
WITHIN 50 F/H SINCE FEBRUARY
28, 2003
EVERY 250 F/H REPETITIVE ACTION
FOLLOWED BY SoREM SMJC #31 and #32
ENGINE REAR MOUNT STRUTS
OPEN: INSPECTION COVERED BY SOREM SMJC 31 AND 32 AND
CARRIED OUT WITH W.O. 09/279. NEXT DUE WITHIN A/C FH 4279
28/09/2003
R Y FAA 2004-21-05 -
SCHEDA ANALISI Disposizione Tecnica
DT-CL-21-01
A 500 heater Hrs Total or 100 heater hrs TIS from 19/11/04
(whichever occurs later)
100 Hrs funzion. 24 Months
PRESSURE DECAY TEST and CABIN
HEATER (JANITROL)
OPERATIONAL TEST
REF TO COMPONENTS
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCU s/n 2030
Delivery Date: Jun ‘98
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 3 of 4 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCU Compliance Status
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
REGOLATORE CARBURANTE CON VALVOLE SHUTOFF
A/B/C 14D11 o A/B/C/P 23D04
REF TO COMPONENTS
R N FAA 2005-18-05
- - - - LOWER CAPS OF THE
WING FRONT SPAR AND REAR SPAR
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N EASA 2006-0375
- Scheda Analisi AD Dec. 29, 2006 - CARLING
TECHNOLOGIES SWITCHES
CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY
N N FAA 2006-22-05
EASA 2006-479 Scheda Analisi AD - N/A INTEGRATED NAVIGATION UNITS
REF TO COMPONENTS Supersedes
FAA 2003-04-06
R Y TCCA CF-2008-29
FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009
BEFORE AND AFTER EVERY FIRE SEASON
OR AT SIX MONTH INTERVAL,
WHICHEVER IS SHORTER TIME
PERIOD
RUDDER LOWER TORQUE TUBE UPPER
BEARING
OPEN: CARRIED OUT ON OCT 05, 10 (AD COVERED BY SMJC 60). EXPIRED ON APR 05, 2010 AND ALREADY PLANNED WITH W.O.
11/038
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCU s/n 2030
Delivery Date: Jun ‘98
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 4 of 4 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCU Compliance Status
R Y TCCA CF-2010-38R2
ENAC 2011-88 Bombardier SB 215 -A4424 Jun 01, 2011
FIRST INSPECTION WITHIN 50 FC FROM
20 DEC 2010; THEREAFTER REPEAT
PERRFORM AN INSPECTION BEFORE
100 FC WITH TERMINATING ACTION NOT LATER THAN Jun
01, 2011.
INSPECTION OF THE EMERGENCY WATER
DUMP PULLEY BRACKET AND STRUCTURE
OPEN: PART B, TERMINATING ACTION, PLANNED WITH W.O. 11/038
R Y TCCA CF-2011-35
Bombardier SB 215-A4450;
Bombardier SB 215-A4451
ESB-4-32-A4450 Rev 01;
ESB-4-32-A4451 Rev 01;
Ref. To AD-PA Compliance Components
Ref. To AD-PA Compliance Components
Liquid Penetrant & Eddy Current Inspection on MLG Upper Member
Forward Lug
REF. TO AD-PA COMPLIANCE COMPONENTS
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCU s/n 2030
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 1 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCQ Components Compliance Status
A N FAA 81-21-05
- - Nov 19, 1981 N/A ARTEX ELT Battery not usable in salt environment
CLOSED: NOT APPLICABLE – SUBJECT ELT BATTERY NOT
INSTALLED
A N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782
RAI 74-225 - N/A N/A Ni-Cd batterie con celle in
polistirolo
CLOSED: NOT APPLICABLE - TEMPERATURE SENSING
INSTALLED ON BATTERIES EMBODIED
S - RAI 82-113
- - - - - CLOSED: SUPERS. BY ENAC 96-348
N N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782 - N/A N/A Ni-Cd batteries
CLOSED: CF96-21 ISSUED TO CANCEL THE APPLICABILITY OF
FAA 72-19-04
S - RAI 88-052
- - - - - SUPERS. BY ENAC 88-096
R Y RAI 88-096
FAR 43 Appendix E
Norma di lavoro NL-CL-34-06 19/11/2005 24 Months ALTIMETER AND STATIC
PRESSURE SYSTEM
OPEN: CARRIED OUT DURING WITH W.O. 09/073. NEXT DUE PLANNED WITH W.O. 11/038
Supersedes ENAC 88-095
I Y ENAC 96-052
FAA FAR 91.21 - N/A N/A USE OF PORTABLE ELETTRONIC DEVICES
CLOSED: AFM UPDATED – CREW INFORMED
N N ENAC 96-348
FAA 96-20-07 Amdt 39-9773 -
Within 500 Hrs (TIS) or 12 mths from 14/11/96
100 Hrs funzion. 24 Months
COMBUSTION CHAMBER DECAY TEST (JANITROL)
CLOSED: NOT APPLICABLE - HEATER MODEL B4500
(CERAMIC COMBUSTION TUBE) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCU s/n 2030
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 2 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCQ Components Compliance Status
N N ENAC 97-167
FAA 97-11-10 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N TCCA CF-95-16
ENAC 97-221 Marathon Power SB 111692-014 27/07/96 N/A
PCB SERIES PC-250 MODIFICATION OR
REMOVAL
CLOSED: NOT APPLICABLE AS PER INVERTER INSTALLED
(Serie MSI-800)
N N ENAC 97-274
FAA 97-18-03 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N ENAC 99-231
FAA 99-08-21 - - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS CLOSED: NOT APPLICABLE -
SCOTT OXYGEN MASKS INSTALLED
S - ENAC 00-018
FAA 99-23-22 Norma di Lavoro NL-CL-34-07 Apr 17, 2000 Every 90 days
TRANSPONDER MODO “C”
INSPECTION/TEST
CLOSED: SUPERSEDED BY ENAC 00-209
N N ENAC 00-209
FAA 99-23-22 Amdt. 39-11686
Engineering InstructionEI 004/00 18/05/00 N/A TRANSPONDER MODO
“C”
CLOSED: NOT APPLICABLE AD RESCINDED APR. 12, ‘00
SUPERSEDES ENAC 00-018
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCU s/n 2030
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 3 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCQ Components Compliance Status
S - ENAC 01-173
FAA 2001-08-01 Scheda Analisi PA May 2, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04
CLOSED: SUPERSEDED BY ENAC 01-368
A N ENAC 01-368
FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04 P/N installed on A/C: J20C30
CLOSED: NOT APPLICABLE AS PER FUEL SHUT-OFF P/N
INSTALLED Supersedes ENAC 01-173
N N ENAC 01-442
FAA 2001-18-05 - Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.
CLOSED: NOT APPLICABLE PER P/N
I Y ENAC 01-470
FAA 2001-22-14 SoREM DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER
DISCHARGER
CLOSED: P/N AFFECTED CHECKED AND REMOVED.
WALTER KIDDE CARTRIDGES INSTALLED ON
FEB 05, 02
I Y TCCA CF-2002-14
ENAC 02-167
BOMBARDIER SB215-3108 SB215-4234
SoREM BM-CL-61-4234
04/03/2003 N/A
PROPELLER CONTROL UNIT
BACKUP PRESSURE RELIEF VALVE
CLOSED: SB 215-4234 INCORPORATED
I Y ENAC 03-067
FAA 2003-04-06 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ -850/ -851
CLOSED: INU#1 #2 REPLACED. NOTIFIED TO THE CREW – INFO
INSERTED IN AFM
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCU s/n 2030
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 4 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCQ Components Compliance Status
28/09/2003
N N FAA 2003-23-05
ENAC 2004-003 ENAC 2004-073 - December 24, 2005 N/A Titeflex Corporation,
Tubi Flessibili
CLOSED: NOT APPLICABLE
HOSES INSTALLED P/N 114040-4
R Y FAA
2004-21-05 Amdt.39-13826
- Scheda Analisi PA DT-CL-21-01
A 500 heater Hrs or 100 heater Hrs TIS
since 19/11/04 (whichever occurs
later)
100 Hrs (TIS) or
24 Months
PRESSURE DECAY TEST ed Operational Test del
CABIN HEATER (JANITROL)
OPEN: HEATER TIME IN SERVICE 278.00
HOURS. 222.00 HOURS TO GO TO THE TEST
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
CLOSED: NOT APPLICABLE BY
COMPONENT P/N 91E18-1 INSTALLED
R Y EASA 2006-0265 - Scheda Analisi PA
ESP-4-34-001 Within
Mar 13, 2007 24 Months MODE “S” and “C” TRANSPONDERS CHECK
OPEN: CARRIED OUT DURING
WITH W.O. 09/073. NEXT DUE PLANNED
WITH W.O. 11/038
A N EASA 2006-0269
- Scheda Analisi PA - - MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
A N FAA 2006-18-08 - Scheda Analisi AD Oct. 11, 2006 - GOODYEAR
NOSE WHEEL TIRES
CLOSED: NOT APPLICABLE AS PER
GOODYEAR TIRES P/N INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCU s/n 2030
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 5 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCQ Components Compliance Status
A N FAA 2006-19-04
- Scheda Analisi AD - - MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
N N FAA 2006-22-05
ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU
CLOSED: NOT APPLICABLE AS PER
COMPONENT MODIFIED (REF TO FAA
2003-04-06)
A N EASA 2006-0366
- Scheda Analisi PA Dec 14, 2006 - LIFE RAFT CLOSED: NOT
APPLICABLE AS PER AIRCRAFT MODEL
A N EASA 2006-0286R1
- Scheda Analisi PA Sep 9, 2006 - Oxygen Cylinders CLOSED: NOT
APPLICABLE AS PER P/N INSTALLED
A N EASA 2007-0256
- Scheda Analisi PA Sep 19, 2007 - Seat Restraint System CLOSED: NOT
APPLICABLE AS PER P/N INSTALLED
A N EASA 2007-0294
ENAC 2009-060 Scheda Analisi PA - - APU Turbine wheel life limit reduction
CLOSED: NOT EFFECTIVE AS PER
APU NOT INSTALLED ON SOREM CL415
FLEET
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCU s/n 2030
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 6 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCQ Components Compliance Status
N N EASA 2009-0200
- Scheda Analisi AD Sep 22, 2010 N/A Navigation – Mode A/C Transponder – Check /
Modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N FAA 2009-20-10
- Scheda Analisi AD Jan 17, 2010 N/A Autopilot – servo motors modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
S - CF 2009-42 - SOREM ESB-4-32-4414 (SMJC 063)
Part I within 50Fh Part II: within 750 Fc
Part III: every 750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
CLOSED: SUPERSEDED BY CF 2009-42R1 (PART
I CARRIED OUT ON NOV 2009)
R Y CF 2009-42R1 - SOREM ESB-4-32-4414 (SMJC 063)
Part I within 50Fh Part II: within 750 Fc
Part III: every 750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
CLOSED: (PART I CARRIED OUT ON NOV
2009) OPEN: PART II AND PART III - NOT YET
PERFORMED. ISSUED SMJC 063: 160 FLIGHT
CYCLES TO GO
A N EASA 2009-0251
- Scheda Analisi AD Nov 26, 2009 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER S/N
INSTALLED
Y N EASA 2009-0262R1
Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A Portable Halon 1211 Fire Extinguisher
NOT EFFECTIVE AS PER S/N NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCU s/n 2030
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 7 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCQ Components Compliance Status
N N EASA 2009-0278
- Scheda Analisi AD Jan 22, 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N TCA CF-2009-44
- Scheda Analisi AD Jul 01, 2011 N/A ELT-Potential Failure to Transmit the Required 406MHz Coded Signal
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N EASA 2010-003R1
- Scheda Analisi AD 18 Apr, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
Y N EASA
2010-0062R1
- Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
NOT EFFECTIVE AS PER P/N NOT INSTALLED
A Y FAA 2010-07-02
- Scheda Analisi AD ESB-4-34-2010-07-02 31 Oct 2012 N/A Honeywell Primus II RNZ
850()/-851
OPEN: INCORPORATION TO
BE VERIFIED. INSPECTION PLANNED
WITH W.O. 11/038
N N EASA 2010-0067
- Scheda Analisi AD 26 Apr, 2010 N/A TDR-94 and TDR-94D transponders
NOT EFFECTIVE AS PER P/N NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCU s/n 2030
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 8 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCQ Components Compliance Status
N N EASA 2010-30
Scheda Analisi SIB N/A N/A Risks in Transporting
Lithium Batteries in Cargo by Aircraft
NOT APPLICABLE SINCE SOREM FLEET IS NOT OPERATING IN CARGO TRANSPORT
CONFIGURATION
N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer –
Erroneous Airspeed and Altitude Indications
NOT APPLICABLE AS PER A/C TYPE, REFER
TO ADE ISSUED DATED NOV 09, 2010
N N FAA 2011-01-09
Scheda Analisi AD 9/06/2011 N/R
B/E Aerospace protective breathing equipment P/N 119003-11 inspection for
B/A Aerospace S.B. 119003-35-6 compliance.
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
N N EASA 2011-0043
Scheda Analisi AD 30/04/2013 N/R Gables Engineering Mode S Transponder Control Panel
Modification
CLOSED: NOT APPLICABLE AS PER
P/N NOT INSTALLED ON THE A/C TYPE
N N EASA 2011-0090R1
ENAC 2011-202 Scheda Analisi AD 27/07/2011 N/R Oxygen mask regulator CLOSED: NOT
APPLICABLE AS PER P/N NOT INSTALLED ON
THE A/C TYPE
N N EASA 2011-0103
Scheda Analisi AD 03/12/2011 N/R ELT TRI-BAND Antennas
P/N 21-41 ( ) series Mod/Replacement
CLOSED: NOT APPLICABLE AS PER
P/N NOT INSTALLED ON THE A/C TYPE
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCU s/n 2030
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective
Revision n° 1
pag. 9 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCQ Components Compliance Status
N N FAA
2011-11-04
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N EASA 2010-0204
ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N FAA 2011-14-08
Scheda Analisi AD Aug 19,2014 or
6500 FH from Aug 19,2011
N/A B/E Aerospace pax oxy mask inspection
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
R Y TCCA CF-2011-35
- ESB-4-32-A4451 Rev 01
First incorporation: Within 50 Flight Hrs
upon receipt of Bombardier SB 215-
A4451
To be repeated every 165 land landings
Inspection of the MLG Upper Member forward lug using eddy current method
FIRST INCORPORATION:
PLANNED (REF TO WO 11/038);
REPETITIVE ACTION: OPEN TO BE
CONSEQUENTLY PLANNED.
A Y TCCA CF-2011-35
- ESB-4-32-A4450 Rev 01 November 11, 2011 N/A
Inspection of the MLG Upper Member forward lug
using liquid penetrant method
OPEN
EFFE
CT
pag. 1 o
I-DPCV Co
A N
A N
A N
S
I Y
I Y
A N
P.A. / A.D.
of 4 A ApR ApN NoS Su
ompliance Status
FAA 77-17-13
FAA 77-13-05
TCCA CF-90-11R2
TCCA CF-92-22
ENAC 95-064
FAA 97-11-08
TCCA CF-96-02R
A.D. C
. Other
Authorityissues
pplicable (to be pplicable Repetot Applicable uperseded
-
-
2 FAA 93-16-06R
FAA 94-04-02TCCA CF-2003
02
TCCA CF-92-10R1
-
1 ENAC 1999-26
Compli
y ISSUEDDOCUMEN
Incorp.) D Dtitive I I
Y YN N
-
-
R2
BombardieSB215-A43
SoREMScheda analis
2 3-
BombardieSB215-A304
SoREMScheda analisP&WC: SB20 SB21 SB21 SB21
BombardieSB215-A306
SoREMScheda Analis
-
68 -
ance SD NTS EXPIRA
Deleted Incorporated Yes effective Not effective
-
-
er 35
si AD
JUNE. 10
er 40
si AD
-
0914 113 211 314
er 60
si PA
-
-
Status
ATION REPEACT
Date:
Sep 09,
, 1994
A/C Type:
CaC
ETITIVE TIONS
11 Prepared
________
-
- M
N/A IN(T
N/A
N/A E
- S
-
anadair CL-415
DESCRIPTIO
by:
______________
NLG DOORS
MISSING RIVETSBULKHEAD
RUDDER-AILERONTERCONNECT TO PREVENT POSSI
FLUTTER)
ENGINE REARMOUNT STRUT
ENGINE FIRE-WIDETECTION LOO
AFM - LIMITATIOSECTION - POW
LEVERS
-
A/C Reg. :
D
ON (COMP
____
Approved b
_________
CLOSED:PER
S IN CLOSED:PER
ON TAB BILE
CLOSED: NPOWERE
R TS
CLOSEA
IRE OP
CLOSEDENGINSYSTEAIRCRA
ON WER
CLOSED:WITH THE
SE
CLOSEDCANCEL
I-DPCVs/n 20
Delivery Date: Jul
NOTES PLIANCE DAT
by:
______________
: NOT APPLICABLE AR AIRCRAFT S/N
: NOT APPLICABLE AR AIRCRAFT S/N
NOT EFFECTIVE AS PED AILERON SYSTE
INSTALLED
D: SUPERSEDED BYAD CF-2003-02
D: AD COMPLIED WITNE FIRE DETECTION EM CONNECTED TO AFT FIRE WARNING
SYSTEM
: AFM REV. 12 ISSUEE NOTE IN LIMITATIOECTION PAGE 8
: AD ISSUED JUST TPREVIOUS REVISIO
V 035 l 98
E)
___
AS
AS
PER M
Y
TH
ED ON
TO ON
EFFE
CT
pag. 2 o
I-DPCV Co
R N
A N
R N
S -
R Y
R Y
P.A. / A.D.
of 4 A ApR ApN NoS Su
ompliance Status
ENAC 00-265
TCCA CF-2002-14
ENAC 00-496
FAA 2003-04-06
TCCA CF-2003-02
FAA 2004-21-05
A.D. C
. Other
Authorityissues
pplicable (to be pplicable Repetot Applicable uperseded
FAA 2004-03-1
4 FAA 2004-26-0
ENAC 02-167
FAA 2002-12-1
6 ENAC 03-067
FAA 2006-22-0
2 FAA 2004-10-0
ENAC 03-251
5 -
Compli
y ISSUEDDOCUMEN
Incorp.) D Dtitive I I
Y YN N
13 -
08 7
BombardieSB215-423
SoREMDT CL-61-42
12 -
7 05
SoREMDT-CL-34-
DT-CL-34-0BM-CL-34-4
04 1
BombardieSB215-A4287
SoREMBM-CL-71-A4
BM-CL-71-A42SMJC 31 and
SCHEDA ANADisposizione Te
DT-CL-21-
ance SD NTS EXPIRA
Deleted Incorporated Yes effective Not effective
-
er 34
234
MARCH 04
-
-05 07R1 4343
March 16
er 7R2
4287 287R2 d 32
WITHIN 5SINCE FEB
28, 20
28
ALISI ecnica -01
A 500 hHrs Total heater hrfrom 19/
(whicheoccurs l
Status
ATION REPEACT
Date:
Sep 09,
4, 2003
6, 2003
50 F/H BRUARY 003
EVERREPETIT
FOLLOWESMJC #
8/09/2003
eater or 100 rs TIS /11/04 ever later)
100 Hr24 M
A/C Type:
CaC
ETITIVE TIONS
11 Prepared
________
-
N/A
- W
N/A IN
RY 250 F/H TIVE ACTION ED BY SoREM #31 and #32
EN
rs funzion. Months
P
O
anadair CL-415
DESCRIPTIO
by:
______________
MLG AXLES
PCU BACKUPPRESSURE VAL
WING TO FUSELAFRAME ANGLE
U Honeywell PrimRNZ-850/ -851
NGINE REAR MOSTRUTS
PRESSURE DECTEST and CABI
HEATER (JANITROL)
OPERATIONAL TE
A/C Reg. :
D
ON (COMP
____
Approved b
_________
CLOSED:PER
P VE
CLOSED:PER AIR
SE
AGE ES
CLOSED:PER
mus II
CLOSEF
OUNT OPEN: INS
SOREM CARRIED
(NEXT D
CAY N
EST
REF T
I-DPCVs/n 20
Delivery Date: Jul
NOTES PLIANCE DAT
by:
______________
: NOT APPLICABLE AR AIRCRAFT S/N
: NOT APPLICABLE ARCRAFT AND ENGINEERIAL NUMBERS
: NOT APPLICABLE AR AIRCRAFT S/N
D: SUPERSEDED BYFAA 2006-22-05
PECTION COVEREDSMJC 31 AND 32 ANOUT WITH W.O. 10/3
DUE WITHIN 55.56 FH
TO COMPONENTS
V 035 l 98
E)
___
AS
AS E
AS
Y
D BY D 344 H)
EFFE
CT
pag. 3 o
I-DPCV Co
A N 2
R N
A N
N N
R Y
P.A. / A.D.
of 4 A ApR ApN NoS Su
ompliance Status
FAA 2004-25-16R
FAA 2005-18-05
EASA 2006-0375
FAA 2006-22-05
TCCA CF-2008-29
A.D. C
. Other
Authorityissues
pplicable (to be pplicable Repetot Applicable uperseded
R1 -
5 -
5 -
5 EASA 2006-47
9 FAA 2009-05-0ENAC 2008-31
Compli
y ISSUEDDOCUMEN
Incorp.) D Dtitive I I
Y YN N
Scheda Analis
-
Scheda Analis
79 Scheda Analis
04 16 SMJC-60
ance SD NTS EXPIRA
Deleted Incorporated Yes effective Not effective
si AD Jan. 05,
-
si AD Dec. 29,
si AD -
Mar 8, 2
Status
ATION REPEACT
Date:
Sep 09,
2005
2006
2009
BEFOREEVERY F
OR AT INT
WHICSHOR
P
A/C Type:
CaC
ETITIVE TIONS
11 Prepared
________
N/A CV
A/
- LO
WIN
-
N/A N
E AND AFTER FIRE SEASON SIX MONTH
TERVAL, CHEVER IS RTER TIME ERIOD
RU
anadair CL-415
DESCRIPTIO
by:
______________
REGOLATORECARBURANTE CVALVOLE SHUTO/B/C 14D11 o A/B
23D04
OWER CAPS OF NG FRONT SPAR
REAR SPAR
CARLING TECHNOLOGIE
SWITCHES
INTEGRATEDNAVIGATION UN
UDDER LOWER TORTUBE UPPER BEARI
A/C Reg. :
D
ON (COMP
____
Approved b
_________
E CON OFF B/C/P
REF T
THE R AND CLOSED:
PER
ES CLOSED:PER
D ITS
REF TS
FA
RQUE ING
OPEN: CEXPIREA/C CU
M
I-DPCVs/n 20
Delivery Date: Jul
NOTES PLIANCE DAT
by:
______________
TO COMPONENTS
: NOT APPLICABLE AR AIRCRAFT S/N
: NOT APPLICABLE AR AD EFFECTIVITY
TO COMPONENTS Supersedes
AA 2003-04-06
COVERED BY SMJC 6ED ON SEP 29, 2010 URRENTLY UNDER
MAINTENANCE
V 035 l 98
E)
___
AS
AS
60
EFFE
CT
pag. 4 o
I-DPCV Co
R Y
R Y
P.A. / A.D.
of 4 A ApR ApN NoS Su
ompliance Status
TCCA CF-2010-38R
TCCA CF-2011-35
A.D. C
. Other
Authorityissues
pplicable (to be pplicable Repetot Applicable uperseded
R2 ENAC 2011-8
5 Bombardier SB
215-A4450; Bombardier SB
215-A4451
Compli
y ISSUEDDOCUMEN
Incorp.) D Dtitive I I
Y YN N
8 Bombardier SB -A4424
B
B
ESB-4-32-A44501;
ESB-4-32-A44501;
ance SD NTS EXPIRA
Deleted Incorporated Yes effective Not effective
215 Jun 01,
50 Rev
51 Rev
Ref. To ACompliaCompon
Status
ATION REPEACT
Date:
Sep 09,
2011
FIRST IWITHIN
20 DTHEREAF
PERRINSPECT
100 TERMINANOT LAT
01
AD-PA ance nents
Ref. TComCom
A/C Type:
CaC
ETITIVE TIONS
11 Prepared
________
NSPECTION 50 FC FROM
DEC 2010; FTER REPEAT RFORM AN TION BEFORE FC WITH
ATING ACTION TER THAN Jun 1, 2011.
INE
To AD-PA mpliance mponents
LiqCM
anadair CL-415
DESCRIPTIO
by:
______________
NSPECTION OF TMERGENCY WA
DUMP PULLEYBRACKET ANDSTRUCTURE
quid Penetrant & Current InspectionMLG Upper Mem
Forward Lug
A/C Reg. :
D
ON (COMP
____
Approved b
_________
THE ATER Y D
PART A TW
PLATERM
A/C CUM
Eddy n on ber
REF. TOC
I-DPCVs/n 20
Delivery Date: Jul
NOTES PLIANCE DAT
by:
______________
OPEN TO BE ACCOMPLISHEWITH SMJC-062
NNED PART B AS MINATING ACTION URRENTLY UNDER
MAINTENANCE
AD-PA COMPLIANCCOMPONENTS
V 035 l 98
E)
___
ED
CE
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCV s/n 2035
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
pag. 1 of 9 A Applicable (to be Incorp.) D Deleted Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________ R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective S Superseded N Not effective
I-DPCV Components Compliance Status
A N FAA 81-21-05
- - Nov 19, 1981 N/A ARTEX ELT Battery not usable in salt environment
CLOSED: NOT APPLICABLE – SUBJECT ELT BATTERY NOT
INSTALLED
A N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782
RAI 74-225 - N/A N/A Ni-Cd batterie con celle in
polistirolo
CLOSED: NOT APPLICABLE - TEMPERATURE SENSING
INSTALLED ON BATTERIES EMBODIED
S - RAI 82-113
- - - - - CLOSED: SUPERS. BY ENAC 96-348
N N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782 - N/A N/A Ni-Cd batteries
CLOSED: CF96-21 ISSUED TO CANCEL THE APPLICABILITY OF
FAA 72-19-04
S - RAI 88-052
- - - - - CLOSED: SUPERS. BY ENAC 88-096
R Y RAI 88-096
FAR 43 Appendix E
Norma di lavoro NL-CL-34-06 19/11/2005 24 Months ALTIMETER AND STATIC
PRESSURE SYSTEM
OPEN: CARRIED OUT WITH W.O. 08/422. EXPIRED ON 04/05/11
A/C CURRENTLY UNDER MAINTENANCE
I Y ENAC 96-052
FAA FAR 91.21 - N/A N/A USE OF PORTABLE ELETTRONIC DEVICES
CLOSED: AFM UPDATED – CREW INFORMED
N N ENAC 96-348
FAA 96-20-07 Amdt 39-9773 -
Within 500 Hrs (TIS) or 12 mths from 14/11/96
100 Hrs funzion. 24 Months
COMBUSTION CHAMBER DECAY TEST (JANITROL)
CLOSED: NOT APPLICABLE - HEATER MODEL B4500
(CERAMIC COMBUSTION TUBE) INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCV s/n 2035
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
pag. 2 of 9 A Applicable (to be Incorp.) D Deleted Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________ R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective S Superseded N Not effective
I-DPCV Components Compliance Status
N N ENAC 97-167
FAA 97-11-10 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N TCCA CF-95-16
ENAC 97-221 Marathon Power SB 111692-014 27/07/96 N/A
PCB SERIES PC-250 MODIFICATION OR
REMOVAL
CLOSED: NOT APPLICABLE AS PER INVERTER INSTALLED
(Serie MSI-800)
N N ENAC 97-274
FAA 97-18-03 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N ENAC 99-231
FAA 99-08-21 - - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS CLOSED: NOT APPLICABLE -
SCOTT OXYGEN MASKS INSTALLED
S - ENAC 00-018
FAA 99-23-22 Norma di Lavoro NL-CL-34-07 Apr 17, 2000 Every 90 days
TRANSPONDER MODO “C”
INSPECTION/TEST
CLOSED: SUPERSEDED BY ENAC 00-209
N N ENAC 00-209
FAA 99-23-22 Amdt. 39-11686
Engineering InstructionEI 004/00 18/05/00 N/A TRANSPONDER MODO
“C”
CLOSED: NOT APPLICABLE AD RESCINDED APR. 12, ‘00
SUPERSEDES ENAC 00-018
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCV s/n 2035
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
pag. 3 of 9 A Applicable (to be Incorp.) D Deleted Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________ R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective S Superseded N Not effective
I-DPCV Components Compliance Status
S - ENAC 01-173
FAA 2001-08-01 Scheda Analisi PA May 2, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04
CLOSED: SUPERSEDED BY ENAC 01-368
A N ENAC 01-368
FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04 P/N installed on A/C: J20C30
CLOSED: NOT APPLICABLE AS PER FUEL SHUT-OFF P/N
INSTALLED Supersedes ENAC 01-173
N N ENAC 01-442
FAA 2001-18-05 - Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.
CLOSED: NOT APPLICABLE PER P/N
I Y ENAC 01-470
FAA 2001-22-14 SoREM DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER
DISCHARGER CLOSED: P/N AFFECTED
CHECKED. WALTER KIDDE CARTRIDGES INSTALLED ON
I Y TCCA CF-2002-14
ENAC 02-167
BOMBARDIER SB215-3108 SB215-4234
SoREM BM-CL-61-4234
04/03/2003 N/A
PROPELLER CONTROL UNIT
BACKUP PRESSURE RELIEF VALVE
CLOSED: SB 215-4234 INCORPORATED
I Y ENAC 03-067
FAA 2003-04-06 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ -850/ -851
CLOSED: INU#1 #2 REPLACED ON 09/04/04
W/O SOREM 04/209 NOTIFIED TO THE CREW – INFO
INSERTED IN AFM
28/09/2003
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCV s/n 2035
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
pag. 4 of 9 A Applicable (to be Incorp.) D Deleted Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________ R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective S Superseded N Not effective
I-DPCV Components Compliance Status
N N FAA 2003-23-05
ENAC 2004-003 - December 24, 2005 N/A Titeflex Corporation, Tubi Flessibili
CLOSED: NOT APPLICABLE
HOSES INSTALLATI P/N 114040-4
N N FAA 2003-23-05
ENAC 2004-073 - December 24, 2005 N/A Titeflex Corporation, Tubi Flessibili
CLOSED: NOT APPLICABLE
HOSES INSTALLATI P/N 114040-4
R Y FAA
2004-21-05 Amdt.39-13826
- Scheda Analisi PA DT-CL-21-01
A 500 heater Hrs or 100 heater Hrs TIS
since 19/11/04 (whichever occurs
later)
100 Hrs (TIS) or
24 Months
PRESSURE DECAY TEST ed Operational Test del
CABIN HEATER (JANITROL)
OPEN: HEATER TIME IN SERVICE:
223.48 HOURS TEST NOT YET PERFORMED
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
CLOSED: NOT APPLICABLE BY
COMPONENT P/N 91E18-1 INSTALLED
R Y EASA 2006-0265 - Scheda Analisi PA
ESP-4-34-001 Within
Mar 13, 2007 24 Months MODE “S” and “C” TRANSPONDERS CHECK
OPEN: PERFORMED WITH W.O. 10/047.
EXPIRED. A/C CURRENTLY
UNDER MAINTENANCE
A N EASA 2006-0269
- Scheda Analisi PA - - MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
A N FAA 2006-18-08 - Scheda Analisi AD Oct. 11, 2006 - GOODYEAR
NOSE WHEEL TIRES
CLOSED: NOT APPLICABLE AS PER
GOODYEAR TIRES P/N INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCV s/n 2035
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
pag. 5 of 9 A Applicable (to be Incorp.) D Deleted Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________ R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective S Superseded N Not effective
I-DPCV Components Compliance Status
A N FAA 2006-19-04
- Scheda Analisi AD - - MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
N N FAA 2006-22-05
ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU
CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND
7510100-731 (#2) INSTALLED
A N EASA 2006-0366
- Scheda Analisi PA Dec 14, 2006 - LIFE RAFT CLOSED: NOT
APPLICABLE AS PER AIRCRAFT MODEL
A N EASA 2006-0286R1
- Scheda Analisi PA Sep 9, 2006 - Oxygen Cylinders CLOSED: NOT
APPLICABLE AS PER P/N INSTALLED
A N EASA 2007-0256
- Scheda Analisi PA Sep 19, 2007 - Seat Restraint System CLOSED: NOT
APPLICABLE AS PER P/N INSTALLED
A N EASA 2007-0294
ENAC 2009-060 Scheda Analisi PA - - APU Turbine wheel life limit reduction
CLOSED: NOT EFFECTIVE AS PER
APU NOT INSTALLED ON SOREM CL415
FLEET
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCV s/n 2035
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
pag. 6 of 9 A Applicable (to be Incorp.) D Deleted Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________ R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective S Superseded N Not effective
I-DPCV Components Compliance Status
N N EASA 2009-0200
- Scheda Analisi AD Sep 22, 2010 N/A Navigation – Mode A/C Transponder – Check /
Modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N FAA 2009-20-10
- Scheda Analisi AD Jan 17, 2010 N/A Autopilot – servo motors modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
S - CF 2009-42 - SOREM ESB-4-32-4414 (SMJC 063)
Part I within 50Fh Part II: within 750 Fc
Part III: every 750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
CLOSED: SUPERSEDED BY CF 2009-42R1 (PART
I CARRIED OUT ON NOV 26, 2009)
R Y CF 2009-42R1 - SOREM ESB-4-32-
4414R1 (SMJC 063)
Part I within 50Fh Part II: within 750 Fc
Part III: every 750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
OPEN: COVERED BY SOREM ESB-4-32-4414 (SMJC 063; 59 CYCLES
TO GO)
A N EASA 2009-0251
- Scheda Analisi AD Nov 26, 2009 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER S/N
INSTALLED
Y N EASA 2009-0262R1
Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A Portable Halon 1211 Fire Extinguisher
NOT EFFECTIVE AS PER S/N NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCV s/n 2035
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
pag. 7 of 9 A Applicable (to be Incorp.) D Deleted Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________ R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective S Superseded N Not effective
I-DPCV Components Compliance Status
N N EASA 2009-0278
- Scheda Analisi AD Jan 22, 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N TCA CF-2009-44
- Scheda Analisi AD Jul 01, 2011 N/A ELT-Potential Failure to Transmit the Required 406MHz Coded Signal
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N EASA 2010-003R1
- Scheda Analisi AD 18 Apr, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
Y N EASA
2010-0062R1
- Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
A Y FAA 2010-07-02
- Scheda Analisi AD 31 Oct 2012 N/A Honeywell Primus II RNZ 850()/-851
OPEN: INU #1 COMPLIED WITH / INU #2 TO BE PERFORMED
N N EASA 2010-0067
- Scheda Analisi AD 26 Apr, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCV s/n 2035
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
pag. 8 of 9 A Applicable (to be Incorp.) D Deleted Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________ R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective S Superseded N Not effective
I-DPCV Components Compliance Status
N N EASA 2010-30
Scheda Analisi SIB N/A N/A Risks in Transporting Lithium Batteries in Cargo by Aircraft
CLOSED: NOT APPLICABLE SINCE
SOREM FLEET IS NOT OPERATING IN CARGO
TRANSPORT CONFIGURATION
N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer – Erroneous Airspeed and Altitude Indications
CLOSED: NOT APPLICABLE AS PER A/C TYPE, REFER TO ADE ISSUED DATED
NOV 09, 2010
N N FAA 2011-01-09
Scheda Analisi AD 9/06/2011 N/R
B/E Aerospace protective breathing equipment P/N 119003-11 inspection for B/A Aerospace S.B. 119003-35-6 compliance.
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
N N EASA 2011-0043
Scheda Analisi AD 30/04/2013 N/R Gables Engineering Mode S Transponder Control Panel
Modification
CLOSED: NOT APPLICABLE AS PER
P/N NOT INSTALLED ON THE A/C TYPE
N N EASA 2011-0090R1
ENAC 2011-202 Scheda Analisi AD 27/07/2011 N/R Oxygen mask regulator CLOSED: NOT
APPLICABLE AS PER P/N NOT INSTALLED ON
THE A/C TYPE
N N EASA 2011-0103
Scheda Analisi AD 03/12/2011 N/R ELT TRI-BAND Antennas P/N 21-41 ( ) series Mod/Replacement
CLOSED: NOT APPLICABLE AS PER
P/N NOT INSTALLED ON THE A/C TYPE
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCV s/n 2035
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
pag. 9 of 9 A Applicable (to be Incorp.) D Deleted Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________ R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective S Superseded N Not effective
I-DPCV Components Compliance Status
N N FAA
2011-11-04
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N EASA 2010-0204
ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N FAA 2011-14-08
Scheda Analisi AD Aug 19,2014 or 6500 FH from Aug 19,2011
N/A B/E Aerospace pax oxy mask inspection
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
R Y TCCA CF-2011-35
- ESB-4-32-A4451 Rev 01
First incorporation:
Within 50 Flight Hrs upon receipt of Bombardier SB 215-A4451
To be repeated every 165 land
landings
Inspection of the MLG Upper Member forward lug using eddy
current method
OPEN: FIRST
INCORPORATION NOT YET PERFORMED
A Y TCCA CF-2011-35
- ESB-4-32-A4450 Rev 01
November 11, 2011 N/A
Inspection of the MLG Upper Member forward lug using liquid
penetrant method OPEN
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCW s/n 2036
Delivery Date: Nov 11, 1998
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 4
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCW Compliance Status
A N FAA
77-17-13 NLG DOORS
NOT APPLICABLE AS PER AD EFFECTIVITY
A N FAA
77-13-05
MISSING RIVETS IN BULKHEAD
NOT APPLICABLE AS PER AD EFFECTIVITY
A N TCCA
CF-90-11R2 FAA 93-16-06R2
Bombardier SB215-A435
SoREM Scheda analisi AD
JUNE. 10, 1994 N/A
RUDDER-AILERON INTERCONNECT TAB (TO PREVENT POSSIBILE
FLUTTER)
NOT EFFECTIVE AS PER POWERED AILERON SYSTEM
INSTALLED
S TCCA
CF-92-22 FAA 94-04-02
Bombardier SB215-A3040
SoREM Scheda analisi AD
N/A ENGINE REAR
MOUNT STRUTS
SUPERSEDED BY AD CF-2003-02
I Y ENAC 95-064
TCCA CF-92-10R1
P&WC: SB20914 SB21113 SB21211 SB21314
Bombardier SB215-A3060
SoREM Scheda Analisi PA
N/A ENGINE FIRE-WIRE DETECTION LOOP
- CLOSED - AD COMPLIED WITH
ENGINE FIRE DETECTION SYSTEM CONNECTED TO AIRCRAFT FIRE WARNING
SYSTEM
I Y FAA
97-11-08
AFM - LIMITATION SECTION - POWER
LEVERS
- CLOSED - AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION SECTION
PAGE 8
A N TCCA
CF-96-02R1 ENAC 1999-268
AD ISSUED JUST TO CANCEL PREVIOUS REVISION
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCW s/n 2036
Delivery Date: Nov 11, 1998
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 4
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCW Compliance Status
R N ENAC 00-265
FAA 2004-03-13 MLG AXLES NOT APPLICABLE AS PER AD
EFFECTIVITY
A N TCCA
CF-2002-14 FAA 2004-26-08
ENAC 02-167
Bombardier SB215-4234
SoREM DT CL-61-4234
MARCH 04, 2003 N/A PCU BACKUP
PRESSURE VALVE
NOT APPLICABLE AS PER VALVE INCORPORATED AT
MANUFACTURE
R N ENAC 00-496
FAA 2002-12-12 WING TO FUSELAGE
FRAME ANGLES NOT APPLICABLE AS PER AD
EFFECTIVITY
S FAA
2003-04-06 ENAC 03-067
SoREM
DT-CL-34-05 DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II
RNZ-850/ -851
REF TO COMPONENTS
SUPERSEDED BY FAA 2006-22-05
A N TCCA
CF-2003-02 FAA 2004-10-04
ENAC 03-251
Bombardier SB215-A4287R2
SoREM BM-CL-71-A4287
BM-CL-71-A4287R2 SMJC 31 and 32
WITHIN 50 F/H SINCE FEBRUARY
28, 2003
EVERY 250 F/H REPETITIVE ACTION
FOLLOWED BY SoREM SMJC #31 and #32
ENGINE REAR MOUNT STRUTS
AD IS APPLIED TO REAR MOUNTS P/N 87110016-009 AND -011.
P/N 87110047-001 INSTALLED DURING PRODUCTION AD NOT APPLICABLE
28/09/2003
R Y FAA
2004-21-05 -
SCHEDA ANALISI Disposizione Tecnica
DT-CL-21-01
A 500 heater Hrs Total or 100 heater hrs TIS from 19/11/04
(whichever occurs later)
100 Hrs funzion. 24 Months
PRESSURE DECAY TEST and CABIN
HEATER (JANITROL)
OPERATIONAL TEST
REF TO COMPONENTS
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCW s/n 2036
Delivery Date: Nov 11, 1998
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 3 of 4
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCW Compliance Status
A N FAA
2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
REGOLATORE CARBURANTE CON VALVOLE SHUTOFF
A/B/C 14D11 o A/B/C/P 23D04
REF TO COMPONENTS
R N FAA
2005-18-05 -
LOWER CAPS OF THE WING FRONT SPAR AND
REAR SPAR
NOT APPLICABLE AS PER AD EFFECTIVITY
A N EASA
2006-0375 Scheda Analisi AD Dec. 29, 2006
CARLING TECHNOLOGIES
SWITCHES
NOT APPLICABLE AS PER AD EFFECTIVITY
N N FAA
2006-22-05 EASA 2006-479 Scheda Analisi AD N/A
INTEGRATED NAVIGATION UNITS
REF TO COMPONENTS
Supersedes FAA 2003-04-06
R Y TCCA
CF-2008-29 FAA 2009-05-04 ENAC 2008-316
SMJC-60 Mar 8, 2009
BEFORE AND AFTER EVERY FIRE SEASON
OR AT SIX MONTH INTERVAL,
WHICHEVER IS SHORTER TIME
PERIOD
RUDDER LOWER TORQUE TUBE UPPER BEARING
OPEN: AD COVERED BY SMJC 60 CARRIED OUT ON 27/05/2011(W/O
11/112) NEXT DUE WITHIN NOV 27, 11
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCW s/n 2036
Delivery Date: Nov 11, 1998
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 4 of 4
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCW Compliance Status
R Y TCCA
CF-2010-38R2 ENAC 2011-88
Bombardier SB 215 -A4424 Jun 01, 2011
FIRST INSPECTION WITHIN 50 FC FROM
20 DEC 2010; THEREAFTER REPEAT
PERRFORM AN INSPECTION BEFORE
100 FC WITH TERMINATING ACTION NOT LATER THAN Jun
01, 2011.
INSPECTION OF THE EMERGENCY WATER
DUMP PULLEY BRACKET AND STRUCTURE
CLOSED SB 215-A4424 PART B EMBODIED
ON 27/05/2011 (W/0 11/109)
R Y TCCA
CF-2011-35
Bombardier SB 215-A4450;
Bombardier SB 215-A4451
ESB-4-32-A4450 Rev 01;
ESB-4-32-A4451 Rev 01;
Ref. To AD-PA Compliance Components
Ref. To AD-PA Compliance Components
Liquid Penetrant & Eddy Current Inspection on MLG Upper Member
Forward Lug
REF. TO AD-PA COMPLIANCE COMPONENTS
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
109063 Manuf. date:
DEC 17, 1994
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - 109063 - Engine1 - I-DPCW
I Y TCA
CF-90-21 -
P&WC SB20355 (last R1) SB20897 (last R3)
30/04/91 N/A O-RING DETERIORATION
DURING FUEL FILTER COVER INSTALLATION
- CLOSED - AD COMPLIED BY
SB20355 AND SB20897 INCORPORATION
PRIOR TO DELIVERY
I Y RAI
91-296 TCA CF-90-22R1
P&WC SB21018 (last R6)
30/06/94 N/A OIL SYSTEM INSPECTION
DUE TO BEARING DETERIORATION
- CLOSED - AD COMPLIED BY
SB21018R1 INCORPORATION PRIOR TO DELIVERY
A N TCA
CF-91-02 -
P&WC SB20946 (last R2)
31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS CLOSED: N/A AS PER
ENGINE S/N
I Y RAI
91-347 TCA CF-91-26R1
P&WC SB20914 (last R4) SB21053 (last R2)
31/03/92 N/A ENGINE FIRE DUE TO OIL
ACCUMULATING IN THE ICC CAVITY.
- CLOSED - AD COMPLIED BY
SB20914R3 AND SB21053 INCORPORATION
PRIOR TO DELIVERY
S RAI
93-284 TCA CF-92-03R1 - - N/A
INTERNAL OIL FIRES INTERCOMPRESSOR CASE
(ICC)
SUPERSEADED BY
TCA CF-92-03R2
I Y TCA
CF-92-03R2 -
P&WC SB20957 (last R5) SB20962 (last R4) SB21065 (last R7)
21211 (last R6)
30/06/94 N/A INTERNAL OIL FIRES IN THE
ICC.
- CLOSED - AD COMPLIED BY
SB20957, SB20962 AND SB21065 INCORPORATION
PRIOR TO DELIVERY
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
109063 Manuf. date:
DEC 17, 1994
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - 109063 - Engine1 - I-DPCW
A N RAI
94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94
1000⇔2000 cycles
N/A REPLACEMENT HP
TURBINE DISK
CLOSED: NOT EFFECTIVE FOR
ENGINES S/N 109022 AND SUBSEQUENT
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077R7 SB21364R1 SB21373R3
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
- CLOSED -
ALL SBs RELATED TO AD EMBODIED PRIOR
TO DELIVERY
A N ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB 21100R2
all spare heaters within 02/03/01
installed p/n 10718
before 31/08/02
N/A ENGINE PW100 SERIES
FUEL HEATERS
CLOSED NOT APPLICABLE FOR
ENGINES S/N 109036 AND SUB’S
A N ENAC 02-090
TCA CF-2002-10 CLOSED: N/A AS PER
ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21562 (last R2)
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within
2400 f/h or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
- CLOSED - MFCU p/n: 324485715
INSTALLED. AD COMPLIED WITH
28/09/2003
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0052 Manuf. date:
SEP 1999
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - AF0052 - Engine2 - I-DPCW
I Y TCA
CF-90-21 -
P&WC SB20355 (last R1) SB20897 (last R3)
30/04/91 N/A
O-RING DETERIORATION
DURING FUEL FILTER COVER INSTALLATION
- CLOSED - AD COMPLIED WITH AT
DELIVERY
I Y TCCA
CF-90-22R1 RAI 91-296
P&WC SB21018R1
30/06/94 N/A
OIL SYSTEM INSPECTION DUE TO
BEARING DETERIORATION
- CLOSED - AD COMPLIED WITH AT
DELIVERY
A N TCA
CF-91-02 -
P&WC SB20946 (last R2)
31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS
- CLOSED – N/A DUE TO ENGINE S/N
I Y TCCA
CF-91-26R1 RAI 91-347
P&WC SB20914R3
SB21053 31/03/92 N/A
TO IMPROVE THE RETENTION OF THE
P2.5/P3 TUBE ASSEMBLY.
- CLOSED - AD COMPLIED WITH AT
DELIVERY
S TCCA
CF-92-03R1 RAI 93-284 - - N/A
INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
- CLOSED – SUPERSEDED BY TCCA CF-92-03R2
I Y TCCA
CF-92-03R2 -
P&WC SB20957R3 SB20962R2
SB21065
30/06/94 N/A INTERNAL OIL FIRES IN
THE ICC.
- CLOSED - AD COMPLIED WITH AT
DELIVERY
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0052 Manuf. date:
SEP 1999
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - AF0052 - Engine2 - I-DPCW
A N TCCA
CF-94-01
FAA 94-03-02 Amdt 39-8808
RAI 94-001 P&WC SIL 307
Since 14/01/94
1000⇔2000 cycles
N/A REPLACEMENT HP
TURBINE DISK
- CLOSED – NOT EFFECTIVE FOR
ENGINES S/N 109022 AND SUBSEQUENT
I Y TCCA
CF-96-22 ENAC 96-353
P&WC SB21077R7 SB21364R1 SB21373R3
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A
REPLACEMENT OF FUEL NOZZLES
LOCKING PLATES AND “O” RINGS
- CLOSED - ALL SBs RELATED TO AD
EMBODIED AD COMPLIED WITH
A N TCCA
CF-2000-34 FAA 2003-16-04
ENAC 01-065 P&WC
SB 21100R2
all spare heaters within 02/03/01
installed p/n 10718
before 31/08/02
N/A ENGINE PW100 SERIES
FUEL HEATERS
- CLOSED – NOT EFFECTIVE FOR
ENGINES S/N 109036 AND SUB’S
A N TCCA
CF-2002-10 ENAC 02-090
P&WC SB 21914R4
Next shop visit or before 31/12/03
Whichever occurs first
N/A
PW118, PW120 and PW121
INTERCOMPRESSOR CASE FIRE
- CLOSED – N/A AS PER ENGINE MODEL
I Y TCCA
CF-2002-34 FAA 2004-20-01
ENAC 02-448
P&WC SB21562R0/R1/R2
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within
2400 f/h or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
- CLOSED - POST SB21562
28/09/2003
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
991213 Manuf. date:
DECEMBER 1999
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - 991213 - Propeller 1 - I-DPCW
I Y FAA
93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided
transfer tube
- CLOSED – P/N 814829-1 INSTALLED AD COMPLIED WITH
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS
SB 14SF-61-82)
Shaft Torque Check
5000 Hrs
PCU INSPECTION/ MODIFICATION
OPEN: PCU COMPLIANT WITH HS-SB14SF-61-82.
CHECK COVERED BY O/H PROCEDURE (2000 FH) 208.02
FH TO GO
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #1 S/N 9912024-19
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #2 S/N 9912025-19
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #3 S/N 9912027-19
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #4 S/N 9912031-19
R Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
6000 Hrs or 3 years since February 7,
1997
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE INSPECTED DURING LAST O/H.
(every 2000 FH) 410.49 FH TO GO
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
991213 Manuf. date:
DECEMBER 1999
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - 991213 - Propeller 1 - I-DPCW
R Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
6000 Hrs or 3 years since February 7,
1997
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: ACTUATOR INSPECTED DURING LAST O/H.
(every 2000 FH) 410.49 FH TO GO
R Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
6000 Hrs or 3 years since February 7,
1997
10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: PCU INSPECTED DURING LAST SHOP VISIT.
(every 2000 FH) 208.02 FH TO GO
28/09/2003
A N FAA
2006-24-07 Scheda Analisi PA Jan 3, 2007
NOT APPLICABLE AS PER PROPELLER MODEL
A N FAA
US-2011-04-02 ENAC 2011-68 ADE issued Apr 15, 2011
NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
950205 Manuf. date:
Feb 20, 1995
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 1 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
__________________
Approved by:
____________________
AD-PA Compliance Status Report - 950205 - Propeller 2 - I-DPCW
I Y FAA
93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided
transfer tube
- CLOSED – P/N 814829-1 INSTALLED AD COMPLIED WITH
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check
5000 Hrs
PCU INSPECTION/ MODIFICATION
OPEN: PCU COMPLIANT WITH HS-SB14SF-61-82.
CHECK COVERED BY O/H PROCEDURE (2000 FH) 1774.09
FH TO GO
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
- CLOSED – NOT APPLICABLE AS PER
BLADE S/N 2009090165
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
- CLOSED - BLADE #2 S/N 879794
MODIFIED BY ASB-A92.R1
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
- CLOSED – BLADE #3 S/N 879997
MODIFIED BY ASB-A92.R1
A N ENAC
96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles
BLADE INSPECTION / MODIFICATION
- CLOSED - BLADE #4 S/N 880299
MODIFIED BY ASB-A92.R1
R Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
6000 Hrs or 3 years since
February 7, 1997 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE INSPECTED DURING LAST O/H.
(every 2000 FH) 537.37 FH TO GO
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand
14SF-19
Prop. S/N. :
950205 Manuf. date:
Feb 20, 1995
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective pag. 2 of 2
S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
__________________
Approved by:
____________________
AD-PA Compliance Status Report - 950205 - Propeller 2 - I-DPCW
R Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
6000 Hrs or 3 years since
February 7, 1997 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: ACTUATOR INSPECTED DURING LAST O/H.
(every 2000 FH) 537.37 FH TO GO
R Y ENAC
97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
6000 Hrs or 3 years since
February 7, 1997 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: PCU INSPECTED DURING LAST SHOP VISIT.
(every 2000 FH) 1774.09 FH TO GO
28/09/2003
A N FAA
2006-24-07 Scheda Analisi PA Jan 3, 2007
NOT APPLICABLE AS PER PROPELLER MODEL
A N FAA
US-2011-04-02 ENAC 2011-68 ADE issued Apr 15, 2011
NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCW s/n 2036
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 2
pag. 1 of 9 S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCW Components Compliance Status
A N FAA
81-21-05 Nov 19, 1981 N/A
ARTEX ELT Battery not usable in salt environment
APPLICABLE ELT BATTERY NOT INSTALLED
A N TCCA
CF-96-21
FAA 72-19-04 Amdt. 39-1782
RAI 74-225 N/A N/A
Ni-Cd batterie con celle in polistirolo
TEMPERATURE SENSING INSTALLED ON BATTERIES
EMBODIED
S RAI
82-113 SUPERS. BY ENAC 96-348
N N TCCA
CF-96-21
FAA 72-19-04 Amdt. 39-1782 - N/A N/A Ni-Cd batteries
CF96-21 ISSUED TO CANCEL THE APPLICABILITY OF
FAA 72-19-04
S RAI
88-052 SUPERS. BY ENAC 88-096
R Y RAI
88-096 FAR 43
Appendix E Norma di lavoro
NL-CL-34-06 19/11/2005 24 Months
ALTIMETER AND STATIC PRESSURE SYSTEM
CARRIED OUT DURING ACCOMPLISHMENT OF AD EASA
2006-0265 (MAR 8, 2011, W.O 11/09)
I Y ENAC 96-052
FAA FAR 91.21 N/A N/A USE OF PORTABLE
ELETTRONIC DEVICES
- CLOSED - AFM UPDATED – CREW
INFORMED
N N ENAC 96-348
FAA 96-20-07 Amdt 39-9773 -
Within 500 Hrs (TIS) or 12 mths from 14/11/96
100 Hrs funzion. 24 Months
COMBUSTION CHAMBER DECAY TEST (JANITROL)
NOT APPLICABLE HEATER MODEL B4500
(CERAMIC COMBUSTION TUBE)
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCW s/n 2036
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 2
pag. 2 of 9 S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCW Components Compliance Status
N N ENAC 97-167
FAA 97-11-10 - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS
NOT APPLICABLE SCOTT OXYGEN MASKS
INSTALLED
N N TCCA
CF-95-16 ENAC 97-221
Marathon Power SB 111692-014
27/07/96 N/A PCB SERIES PC-250 MODIFICATION OR
REMOVAL
NOT APPLICABLE AS PER INVERTER INSTALLED
(Serie MSI-800)
N N ENAC 97-274
FAA 97-18-03 - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS
NOT APPLICABLE SCOTT OXYGEN MASKS
INSTALLED
N N ENAC 99-231
FAA 99-08-21 - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS
NOT APPLICABLE SCOTT OXYGEN MASKS
INSTALLED
S ENAC 00-018
FAA 99-23-22 Norma di Lavoro
NL-CL-34-07 Apr 17, 2000 Every 90 days TRANSPONDER MODO
“C” INSPECTION/TEST
Superseded by ENAC 00-209
N N ENAC 00-209
FAA 99-23-22 Amdt. 39-11686
Engineering Instruction
EI 004/00 18/05/00 N/A
TRANSPONDER MODO “C”
NOT APPLICABLE AD RESCINDED APR. 12, ‘00
Supersedes ENAC 00-018
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCW s/n 2036
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 2
pag. 3 of 9 S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCW Components Compliance Status
S ENAC 01-173
FAA 2001-08-01 Scheda Analisi PA May 2, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04
NOT APPLICABLE AS PER HEATER INSTALLED
Supers. By ENAC 01-368
A N ENAC 01-368
FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
P/N installed on A/C: J20C30
NOT APPLICABLE AS PER HEATER INSTALLED
Supersedes ENAC 01-173
N N ENAC 01-442
FAA 2001-18-05 Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.
NOT APPLICABLE PER P/N
I Y ENAC 01-470
FAA 2001-22-14 SoREM
DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER
DISCHARGER
- CLOSED - P/N AFFECTED CHECKED.
WALTER KIDDE CARTRIDGES INSTALLED ON
I Y TCCA
CF-2002-14 ENAC 02-167
BOMBARDIER SB215-3108 SB215-4234
SoREM BM-CL-61-4234
04/03/2003 N/A
PROPELLER CONTROL UNIT
BACKUP PRESSURE RELIEF VALVE
- CLOSED - SB215-4234 IS INCORPORATED
DURING PRODUCTION
I Y ENAC 03-067
FAA 2003-04-06
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II
RNZ -850/ -851
- CLOSED - INU P/N 7510100-732 (#1) AND 7510100-731 (#2) INSTALLED
28/09/2003
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCW s/n 2036
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 2
pag. 4 of 9 S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCW Components Compliance Status
N N FAA
2003-23-05 ENAC 2004-003 -
December 24, 2005
N/A Titeflex Corporation,
Tubi Flessibili
NOT APPLICABLE HOSES INSTALLATI
P/N 114040-4
N N FAA
2003-23-05 ENAC 2004-073 -
December 24, 2005
N/A Titeflex Corporation,
Tubi Flessibili
NOT APPLICABLE HOSES INSTALLATI
P/N 114040-4
R Y FAA
2004-21-05 Amdt.39-13826
- Scheda Analisi PA DT-CL-21-01
A 500 heater Hrs or 100 heater Hrs
TIS since 19/11/04
(whichever occurs later)
100 Hrs (TIS) or
24 Months
PRESSURE DECAY TEST ed Operational Test del CABIN
HEATER (JANITROL)
HEATER TIME IN SERVICE CHECKED:
258,00 HOURS TEST NOT YET PERFORMED
A N FAA
2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
P/N installed on A/C: J20C30
NOT APPLICABLE AS PER HEATER INSTALLED
R Y EASA
2006-0265 -
Scheda Analisi PA NL CL-34-04 Ed. 2
Within Mar 13, 2007
24 Months MODE “S” and “C”
TRANSPONDERS CHECK
CARRIED OUT DURING LAST ANNUAL CHECK
W.O. 11/053 ON SEP 01, 2011 NEXT DUE WITHIN
AUG 31, 2013
A N EASA
2006-0269 - Scheda Analisi PA MODE “S” TRANSPONDERS
N/A AS PER MODEL NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCW s/n 2036
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 2
pag. 5 of 9 S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCW Components Compliance Status
A N FAA
2006-18-08 Scheda Analisi AD Oct. 11, 2006
GOODYEAR NOSE WHEEL TIRES
NOT APPLICABLE AS PER
GOODYEAR TIRES NOT INSTALLED
A N FAA
2006-19-04 Scheda Analisi AD MODE “S” TRANSPONDERS
N/A AS PER PART NUMBER NOT
INSTALLED
N N FAA
2006-22-05 ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU
NOT APPLICABLE AS PER COMPONENT MODIFIED (REF TO
FAA-2003-04-06)
A N EASA
2006-0366 Scheda Analisi PA Dec 14, 2006 LIFE RAFT
NOT APPLICABLE AS PER AIRCRAFT MODEL
A N EASA
2006-0286R1 Scheda Analisi PA Sep 9, 2006 Oxygen Cylinders
NOT APPLICABLE AS PER P/N NOT INSTALLED
A N EASA
2007-0256 Scheda Analisi PA Sep 19, 2007 Seat Restraint System
NOT APPLICABLE AS PER P/N NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCW s/n 2036
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 2
pag. 6 of 9 S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCW Components Compliance Status
A N EASA
2007-0294 ENAC 2009-060 Scheda Analisi PA
APU Turbine wheel life limit reduction
NOT EFFECTIVE AS PER APU NOT
INSTALLED ON SOREM CL415 FLEET
N N EASA
2009-0200 Scheda Analisi AD Sep 22, 2010 N/A
Navigation – Mode A/C Transponder – Check /
Modification
NOT EFFECTIVE AS PER P/N NOT INSTALLED
N N FAA
2009-20-10 Scheda Analisi AD Jan 17, 2010 N/A
Autopilot – servo motors modification
NOT EFFECTIVE AS PER P/N NOT INSTALLED
S - CF 2009-42 - SOREM ESB-4-32-
4414 (SMJC 063)
Part I within 50Fh Part II: within 750
Fc Part III: every
750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
CLOSED: SUPERSEDED BY CF
2009-42R1 (PART I CARRIED OUT ON NOV
26, 2009)
R Y CF 2009-42R1 Enac 2010-183
FAA 2011-03-08 SOREM ESB-4-32-
4414R1 Every 750 Flight
cycles Special Inspection of Accumulator
Screw Caps
CLOSED PART II:: PERFORMED WITH WO 10/293 ON SEP 1, 2010;
OPEN: PART III: 621 FLIGHT CYCLES TO GO
Y N EASA
2009-0251 Scheda Analisi AD Nov 26, 2009 N/A
Portable Halon 1211 Fire Extinguisher
NOT EFFECTIVE AS PER S/N NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCW s/n 2036
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 2
pag. 7 of 9 S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCW Components Compliance Status
Y N EASA
2009-0262R1 Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A
Portable Halon 1211 Fire Extinguisher
NOT EFFECTIVE AS PER S/N NOT INSTALLED
N N EASA
2009-0278 - Scheda Analisi AD Jan 22, 2010 N/A
Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N TCA
CF-2009-44 Scheda Analisi AD Jul 1, 2011 N/A
ELT-Potential Failure to Transmit the Required 406MHz Coded
Signal
NOT EFFECTIVE AS PER P/N NOT INSTALLED
N N EASA
2010-003R1 Scheda Analisi AD 18 Apr, 2010 N/A
TDR-94 and TDR-94D transponders
NOT EFFECTIVE AS PER P/N NOT INSTALLED
Y N EASA
2010-0062
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire
Extinguisher
NOT EFFECTIVE AS PER P/N NOT INSTALLED
A Y FAA
2010-07-02 Scheda Analisi AD 31 Ott 2012 N/A
Honeywell Primus II RNZ 850()/-851
OPEN: NOT YET PERFOMED
INU 1 AND INU 2 TO BE MODIFIED”
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCW s/n 2036
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 2
pag. 8 of 9 S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCW Components Compliance Status
N N EASA
2010-0067 Scheda Analisi AD 26 Apr, 2010 N/A
TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N EASA
2010-30 Scheda Analisi SIB N/A N/A
Risks in Transporting Lithium Batteries in Cargo by Aircraft
CLOSED: NOT APPLICABLE SINCE
SOREM FLEET IS NOT OPERATING IN CARGO
TRANSPORT CONFIGURATION
N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer – Erroneous Airspeed and Altitude Indications
CLOSED: NOT APPLICABLE AS PER A/C TYPE, REFER TO ADE ISSUED DATED
NOV 09, 2010
N N FAA
2011-01-09 Scheda Analisi AD 9/06/2011 N/R
B/E Aerospace protective breathing equipment P/N 119003-11 inspection for B/A Aerospace S.B. 119003-35-6 compliance.
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
N N EASA
2011-0043 Scheda Analisi AD 30/04/2013 N/R
Gables Engineering Mode S Transponder Control Panel
Modification
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N EASA
2011-0090R1 ENAC 2011-202 Scheda Analisi AD 27/07/2011 N/R Oxygen mask regulator
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCW s/n 2036
Components
EF
FE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS
EXPIRATION REPETITIVE
ACTIONS DESCRIPTION
NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted
R Applicable Repetitive I Incorporated
N Not Applicable Y Yes effective
Revision n° 2
pag. 9 of 9 S Superseded N Not effective
Date:
Sep 09, 2011
Prepared by:
________________________
Approved by:
________________________
I-DPCW Components Compliance Status
N N EASA
2011-0103 Scheda Analisi AD 03/12/2011 N/R
ELT TRI-BAND Antennas P/N 21-41 ( ) series Mod/Replacement
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N FAA
2011-11-04
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire
Extinguisher
NOT EFFECTIVE AS PER P/N NOT INSTALLED
N N EASA
2010-0204 ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A
TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
R Y TCCA
CF-2011-35 -
ESB-4-32-A4451 Rev 01
First incorporation:
Within 50 Flight Hrs upon receipt of Bombardier SB 215-A4451
To be repeated every 165 land
landings
Inspection of the MLG Upper Member forward lug using eddy
current method
FIRST INCORPORATION:
CLOSED (REF TO WO 11/053R2);
REPETITIVE ACTION: 151 LL TO GO
A Y TCCA
CF-2011-35 -
ESB-4-32-A4450 Rev 01
November 11, 2011
N/A Inspection of the MLG Upper
Member forward lug using liquid penetrant method
OPEN
A.D. Compliance Status A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCY s/n 2047
Delivery Date: May 00
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 3 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCY Compliance Status
A N FAA 77-17-13
- - - - NLG DOORS CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N FAA 77-13-05
- - - - MISSING RIVETS IN BULKHEAD
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N TCCA CF-90-11R2 FAA 93-16-06R2
Bombardier SB215-A435
SoREM Scheda analisi AD
JUNE. 10, 1994 N/A RUDDER-AILERON
INTERCONNECT TAB (TO PREVENT POSSIBILE
FLUTTER)
CLOSED: NOT EFFECTIVE AS PER POWERED AILERON SYSTEM
INSTALLED
S TCCA CF-92-22
FAA 94-04-02 TCCA CF-2003-
02
Bombardier SB215-A3040
SoREM Scheda analisi AD
- N/A ENGINE REAR MOUNT STRUTS
CLOSED: SUPERSEDED BY AD CF-2003-02
I Y ENAC 95-064
TCCA CF-92-10R1
P&WC: SB20914 SB21113 SB21211 SB21314
Bombardier SB215-A3060
SoREM Scheda Analisi PA
N/A ENGINE FIRE-WIRE DETECTION LOOP
CLOSED: AD COMPLIED WITH ENGINE FIRE DETECTION SYSTEM CONNECTED TO AIRCRAFT FIRE WARNING
SYSTEM
I Y FAA 97-11-08
- - - - AFM - LIMITATION SECTION - POWER
LEVERS
CLOSED: AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION
SECTION PAGE 8
A N TCCA CF-96-02R1
ENAC 1999-268 - - - - CLOSED: AD ISSUED JUST TO CANCEL PREVIOUS REVISION
A.D. Compliance Status A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCY s/n 2047
Delivery Date: May 00
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 3 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCY Compliance Status
R N ENAC 00-265
FAA 2004-03-13 - - - MLG AXLES CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N TCCA CF-2002-14
FAA 2004-26-08 ENAC 02-167
Bombardier SB215-4234
SoREM DT CL-61-4234
MARCH 04, 2003 N/A PCU BACKUP PRESSURE VALVE
CLOSED: NOT APPLICABLE AS PER AIRCRAFT AND ENGINE
SERIAL NUMBERS
R N ENAC 00-496
FAA 2002-12-12 - - - WING TO FUSELAGE FRAME ANGLES
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
S - FAA 2003-04-06
ENAC 03-067 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ-850/ -851
CLOSED: SUPERSEDED BY FAA 2006-22-05
R Y TCCA CF-2003-02
FAA 2004-10-04 ENAC 03-251
Bombardier SB215-A4287R2
SoREM BM-CL-71-A4287
BM-CL-71-A4287R2 SMJC 31 and 32
WITHIN 50 F/H SINCE FEBRUARY
28, 2003
EVERY 250 F/H REPETITIVE ACTION
FOLLOWED BY INAER SMJC #31 and #32
ENGINE REAR MOUNT STRUTS
OPEN: CARRIED OUT WITH SMJC 31 & SMJC 32 WO 10/273 – 29.05
FH TO GO
R Y FAA 2004-21-05 -
SCHEDA ANALISI Disposizione Tecnica
DT-CL-21-01
A 500 heater Hrs Total or 100 heater hrs TIS from 19/11/04
(whichever occurs later)
100 Hrs funzion. 24 Months
PRESSURE DECAY TEST and CABIN
HEATER (JANITROL)
OPERATIONAL TEST
REF TO COMPONENTS
A.D. Compliance Status A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCY s/n 2047
Delivery Date: May 00
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 3 of 3 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCY Compliance Status
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
REGOLATORE CARBURANTE CON VALVOLE SHUTOFF
A/B/C 14D11 o A/B/C/P 23D04
REF TO COMPONENTS
R N FAA 2005-18-05
- - - - LOWER CAPS OF THE
WING FRONT SPAR AND REAR SPAR
CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N
A N EASA 2006-0375
- Scheda Analisi AD Dec. 29, 2006 - CARLING
TECHNOLOGIES SWITCHES
CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY
N N FAA 2006-22-05
EASA 2006-479 Scheda Analisi AD - N/A INTEGRATED NAVIGATION UNITS
REF TO COMPONENTS Supersedes
FAA 2003-04-06
R Y TCCA CF-2008-29
FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009
BEFORE AND AFTER EVERY FIRE SEASON
OR AT SIX MONTH INTERVAL,
WHICHEVER IS SHORTER TIME
PERIOD
RUDDER LOWER TORQUE TUBE UPPER BEARING
OPEN: CARRIED OUT WITH W.O. 11/100 (AD COVERED BY SMJC
60) NEXT DUE NOV 29, 2011
A.D. Compliance Status Eng. Type:
PW123AF
Eng. S/N. :
AF0023 Manuf. date: May 1997
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 2011 Prepared by:
________________________
Approved by:
________________________
AD Compliance Status – AF0023
I Y TCA CF-90-21 -
P&WC SB20355R1
SB20897 30/04/91 N/A
O-RING DETERIORATION DURING FUEL FILTER COVER INSTALLATION
CLOSED: AD COMPLIED BY SB20355 AND SB20897
INCORPORATION PRIOR TO DELIVERY
(SEE ENGINE TECHNICAL LOG)
I Y RAI 91-296
TCA CF-90-22R1 P&WC SB21018R1 30/06/94 N/A
OIL SYSTEM INSPECTION DUE TO BEARING DETERIORATION
CLOSED: AD COMPLIED BY SB21018R1 INCORPORATION
PRIOR TO DELIVERY (SEE ENGINE TECHNICAL LOG)
I N TCA CF-91-02
- P&WC SB20946R1 31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS
CLOSED: AD COMPLIED BY SB20946R1 INCORPORATION
PRIOR TO DELIVERY (SEE ENGINE TECHNICAL LOG)
I Y RAI 91-347
TCA CF-91-26R1 P&WC
SB20914R3 SB21053
31/03/92 N/A TO IMPROVE THE
RETENTION OF THE P2.5/P3 TUBE ASSEMBLY.
CLOSED: AD COMPLIED BY SB20914R3 AND SB21053
INCORPORATION PRIOR TO DELIVERY
(SEE ENGINE TECHNICAL LOG)
S RAI 93-284
TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
CLOSED: SUPERSEADED BY TCA CF-92-03R2
I Y TCA CF-92-03R2
- P&WC
SB20957R3 SB20962R2
SB21065
30/06/94 N/A INTERNAL OIL FIRES IN THE ICC.
CLOSED: AD COMPLIED BY SB20957, SB20962 AND SB21065
INCORPORATION PRIOR TO DELIVERY
(SEE ENGINE TECHNICAL LOG)
A.D. Compliance Status Eng. Type:
PW123AF
Eng. S/N. :
AF0023 Manuf. date: May 1997
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 2011 Prepared by:
________________________
Approved by:
________________________
AD Compliance Status – AF0023
A N RAI 94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94 1000⇔2000 cycles N/A REPLACEMENT HP
TURBINE DISK
CLOSED: NOT EFFECTIVE FOR ENGINES S/N 109022
AND SUBSEQUENT
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077R7 SB21364R1 SB21373R3
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
CLOSED: ALL SBs RELATED TO AD EMBODIED PRIOR
TO DELIVERY (SEE ENGINE TECHNICAL LOG)
A N ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB 21100R2
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES FUEL HEATERS
CLOSED: : NOT APPLICABLE FOR ENGINES S/N 109036
AND SUB’S
N N ENAC 02-090
TCA CF-2002-10 P&WC SB 20914 R4
At the next scheduled engine
shop visit, or before 31 December 2003, whichever occurs
first
N/A PW118, PW120 and PW121
INTERCOMPRESSOR CASE FIRE
CLOSED: N/A AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21562R0/R1/R2
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within 2400 f/h
or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
CLOSED: FINAL MODIFICATION COMPLIED BY
SB21562 INCORPORATION DATED 21/06/04 W.O.
CV005/04-24
A.D. Compliance Status Eng. Type:
PW123AF
Eng. S/N. :
AF0079 Manuf. date: Nov 2000
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 2011 Prepared by:
________________________
Approved by:
________________________
AD Compliance Status – AF0079
I Y TCA CF-90-21 -
P&WC SB20355R1
SB20897 30/04/91 N/A
O-RING DETERIORATION DURING FUEL FILTER COVER INSTALLATION
CLOSED: AD COMPLIED BY SB20355 AND SB20897
INCORPORATION PRIOR TO DELIVERY
(SEE ENGINE TECHNICAL LOG)
I Y RAI 91-296
TCA CF-90-22R1 P&WC SB21018R1 30/06/94 N/A
OIL SYSTEM INSPECTION DUE TO BEARING DETERIORATION
CLOSED: AD COMPLIED BY SB21018R1 INCORPORATION
PRIOR TO DELIVERY (SEE ENGINE TECHNICAL LOG)
I N TCA CF-91-02
- P&WC SB20946R1 31/10/91 N/A TO PREVENT IN FLIGHT
TORQUE FLUCTUATIONS
CLOSED: AD COMPLIED BY SB20946R1 INCORPORATION
PRIOR TO DELIVERY (SEE ENGINE TECHNICAL LOG)
I Y RAI 91-347
TCA CF-91-26R1 P&WC
SB20914R3 SB21053
31/03/92 N/A TO IMPROVE THE
RETENTION OF THE P2.5/P3 TUBE ASSEMBLY.
CLOSED: AD COMPLIED BY SB20914R3 AND SB21053
INCORPORATION PRIOR TO DELIVERY
(SEE ENGINE TECHNICAL LOG)
S RAI 93-284
TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
SUPERSEADED BY
TCA CF-92-03R2
I Y TCA CF-92-03R2
- P&WC
SB20957R3 SB20962R2
SB21065
30/06/94 N/A INTERNAL OIL FIRES IN THE ICC.
CLOSED: AD COMPLIED BY SB20957, SB20962 AND SB21065
INCORPORATION PRIOR TO DELIVERY
(SEE ENGINE TECHNICAL LOG)
A.D. Compliance Status Eng. Type:
PW123AF
Eng. S/N. :
AF0079 Manuf. date: Nov 2000
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 2011 Prepared by:
________________________
Approved by:
________________________
AD Compliance Status – AF0079
A N RAI 94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94 1000⇔2000 cycles N/A REPLACEMENT HP
TURBINE DISK
CLOSED: NOT EFFECTIVE FOR ENGINES S/N 109022
AND SUBSEQUENT
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077R7 SB21364R1 SB21373R3
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A REPLACEMENT OF FUEL
NOZZLES LOCKING PLATES AND “O” RINGS
CLOSED: ALL SBs RELATED TO AD EMBODIED PRIOR
TO DELIVERY (SEE ENGINE TECHNICAL LOG)
A N ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB 21100R2
all spare heaters within 02/03/01
installed p/n 10718 before 31/08/02
N/A ENGINE PW100 SERIES FUEL HEATERS
CLOSED: NOT APPLICABLE FOR ENGINES S/N 109036
AND SUB’S
N N ENAC 02-090
TCA CF-2002-10 P&WC SB 20914 R4
At the next scheduled engine
shop visit, or before 31 December 2003, whichever occurs
first
N/A PW118, PW120 and PW121
INTERCOMPRESSOR CASE FIRE
CLOSED: N/A AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21562R0/R1/R2
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within 2400 f/h
or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
CLOSED: ENGINE IS POST SB 21562, NO FURTHER ACTION
REQUIRED (SEE ENGINE TECHNICAL LOG)
A.D. Compliance Status Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
20010810 Manuf. date:
Aug 17, 2001
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09 , 11 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report prop1 sn 20010810
I Y FAA 93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided transfer tube
CLOSED: P/N 814829-1 INSTALLED
AD COMPLIED WITH
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs.
PCU INSPECTION/ MODIFICATION
PCU HOURS: 749.27 INSPECTION PERFORMED
EVERY O/H (NEXT DUE WITHIN 1250.33)
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #1 S/N
200107049-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #2 S/N
200107050-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #3 S/N
200108010-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #4 S/N
200210034-19
A.D. Compliance Status Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
20010810 Manuf. date:
Aug 17, 2001
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09 , 11 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report prop1 sn 20010810
I Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRANSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE HOURS: TTSN: N/A; TSO:
1444.57 INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 555.03)
I Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRANSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: ACTUATOR HOURS: TTSN: N/A; TSO: 1444.57
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 555.03)
I Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: PCU HOURS (TSN): 749.27
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 1250.33)
A N FAA 2006-24-07
Scheda Analisi PA Jan 3, 2007 CLOSED: NOT APPLICABLE
AS PER PROPELLER MODEL
A N FAA US-2011-04-02
ENAC 2011-68 ADE issued Apr 15, 2011 CLOSED: NOT APPLICABLE
AS PER PROPELLER MODEL
A.D. Compliance Status Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
20010411 Manuf. date:
May 07, 2001
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09,11 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report prop2 sn 20010411
I Y FAA 93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided transfer tube
CLOSED: P/N 814829-1 INSTALLED
AD COMPLIED WITH
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs.
PCU INSPECTION/ MODIFICATION
OPEN: PCU HOURS: 1618.41
INSPECTION PERFORMED EVERY O/H
(NEXT DUE WITHIN 381.19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #1 S/N
200105010-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #2 S/N
200105012-10
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #3 S/N
2007080733-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
CLOSED: NOT APPLICABLE FOR BLADE #4 S/N 889088-19
A.D. Compliance Status Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
20010411 Manuf. date:
May 07, 2001
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09,11 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report prop2 sn 20010411
I Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRANSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE TTSN: N/A; TSO: 884.49
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 1115.11)
I Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRANSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: ACTUATOR HOURS TTSN: N/A; TSO: 884.49
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 1115.11)
I Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRANSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: PCU HOURS (TSN): 1618.41
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 381.19)
A N FAA 2006-24-07
Scheda Analisi PA Jan 3, 2007 CLOSED: NOT APPLICABLE
AS PER PROPELLER MODEL
A N FAA US-2011-04-02
ENAC 2011-68 ADE issued Apr 15, 2011 CLOSED: NOT APPLICABLE
AS PER PROPELLER MODEL
A.D. Compliance Status A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCY s/n 2047
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCY Components Compliance Status
A N FAA 81-21-05
- - Nov 19, 1981 N/A ARTEX ELT Battery not usable in salt environment
CLOSED: NOT APPLICABLE – SUBJECT ELT BATTERY NOT
INSTALLED
A N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782
RAI 74-225 - N/A N/A Ni-Cd batterie con celle in
polistirolo
CLOSED: NOT APPLICABLE - TEMPERATURE SENSING
INSTALLED ON BATTERIES EMBODIED
S - RAI 82-113
- - - - - CLOSED: SUPERS. BY ENAC 96-348
N N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782 - N/A N/A Ni-Cd batteries
CLOSED: CF96-21 ISSUED TO CANCEL THE APPLICABILITY OF
FAA 72-19-04
S - RAI 88-052
- - - - - SUPERS. BY ENAC 88-096
R Y RAI 88-096
FAR 43 Appendix E
Norma di lavoro NL-CL-34-06R2 19/11/2005 24 Months ALTIMETER AND STATIC
PRESSURE SYSTEM OPEN: TEST CARRIED OUT ON DEC 13 2009 WITH W.O. 09/380
(NEXT DUE WITHIN DEC 07, 2011)
I Y ENAC 96-052
FAA FAR 91.21 - N/A N/A USE OF PORTABLE ELETTRONIC DEVICES
CLOSED: AFM UPDATED – CREW INFORMED
N N ENAC 96-348
FAA 96-20-07 Amdt 39-9773 -
Within 500 Hrs (TIS) or 12 mths from 14/11/96
100 Hrs funzion. 24 Months
COMBUSTION CHAMBER DECAY TEST (JANITROL)
CLOSED: NOT APPLICABLE - HEATER MODEL B4500
(CERAMIC COMBUSTION TUBE) INSTALLED
A.D. Compliance Status A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCY s/n 2047
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCY Components Compliance Status
N N ENAC 97-167
FAA 97-11-10 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N TCCA CF-95-16
ENAC 97-221 Marathon Power SB 111692-014 27/07/96 N/A
PCB SERIES PC-250 MODIFICATION OR
REMOVAL
CLOSED: NOT APPLICABLE AS PER INVERTER INSTALLED
(Serie MSI-800)
N N ENAC 97-274
FAA 97-18-03 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS
INSTALLED
N N ENAC 99-231
FAA 99-08-21 - - N/A PURITAIN-BENNETT
CREW OXYGEN MASKS CLOSED: NOT APPLICABLE -
SCOTT OXYGEN MASKS INSTALLED
S - ENAC 00-018
FAA 99-23-22 Norma di Lavoro NL-CL-34-07 Apr 17, 2000 Every 90 days
TRANSPONDER MODO “C”
INSPECTION/TEST
CLOSED: SUPERSEDED BY ENAC 00-209
N N ENAC 00-209
FAA 99-23-22 Amdt. 39-11686
Engineering InstructionEI 004/00 18/05/00 N/A TRANSPONDER MODO
“C”
CLOSED: NOT APPLICABLE AD RESCINDED APR. 12, ‘00
SUPERSEDES ENAC 00-018
A.D. Compliance Status A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCY s/n 2047
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 3 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCY Components Compliance Status
S - ENAC 01-173
FAA 2001-08-01 Scheda Analisi PA May 2, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04
CLOSED: SUPERSEDED BY ENAC 01-368
A N ENAC 01-368
FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04 P/N installed on A/C: J20C30
CLOSED: NOT APPLICABLE AS PER FUEL SHUT-OFF P/N
INSTALLED Supersedes ENAC 01-173
N N ENAC 01-442
FAA 2001-18-05 - Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.
CLOSED: NOT APPLICABLE PER P/N
I Y ENAC 01-470
FAA 2001-22-14 SoREM DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER
DISCHARGER CLOSED: P/N AFFECTED
CHECKED. WALTER KIDDE CARTRIDGES INSTALLED ON
I Y TCCA CF-2002-14
ENAC 02-167
BOMBARDIER SB215-3108 SB215-4234
SoREM BM-CL-61-4234
04/03/2003 N/A
PROPELLER CONTROL UNIT
BACKUP PRESSURE RELIEF VALVE
CLOSED: SB 215-4234 INCORPORATED
I Y ENAC 03-067
FAA 2003-04-06 FAA 2006-22-05
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ -850/ -851
CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND
7510100-731 (#2) INSTALLED
A.D. Compliance Status A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCY s/n 2047
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 4 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCY Components Compliance Status
28/09/2003
N N FAA 2003-23-05
ENAC 2004-003 ENAC 2004-073 - December 24, 2005 N/A Titeflex Corporation,
Tubi Flessibili
CLOSED: NOT APPLICABLE
HOSES INSTALLATI P/N 114040-4
R Y FAA
2004-21-05 Amdt.39-13826
- Scheda Analisi PA DT-CL-21-01
A 500 heater Hrs or 100 heater Hrs TIS
since 19/11/04 (whichever occurs
later)
100 Hrs (TIS) or
24 Months
PRESSURE DECAY TEST ed Operational Test del
CABIN HEATER (JANITROL)
OPEN: HEATER TIME IN SERVICE CHECKED:
300.06 HOURS TEST NOT YET PERFORMED
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
CLOSED: NOT APPLICABLE BY
COMPONENT P/N 91E18-1 INSTALLED
R Y EASA 2006-0265 - Scheda Analisi PA
NL-34-004 Within
Mar 13, 2007 24 Months MODE “S” and “C” TRANSPONDERS CHECK
OPEN: CARRIED OUT DURING ANNUAL CHK; LAST WITH WO 11/020. NEXT DUE APR 27, 2012
A N EASA 2006-0269
- Scheda Analisi PA - - MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
A N FAA 2006-18-08 - Scheda Analisi AD Oct. 11, 2006 - GOODYEAR
NOSE WHEEL TIRES
CLOSED: NOT APPLICABLE AS PER
GOODYEAR TIRES P/N INSTALLED
A.D. Compliance Status A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCY s/n 2047
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 5 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCY Components Compliance Status
A N FAA 2006-19-04
- Scheda Analisi AD - - MODE “S” TRANSPONDERS
CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED
N N FAA 2006-22-05
ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU
CLOSED: NOT APPLICABLE AS PER
COMPONENT MODIFIED (REF TO
SCHEDA ANALISI 2006-22-05)
A N EASA 2006-0366
- Scheda Analisi PA Dec 14, 2006 - LIFE RAFT CLOSED: NOT
APPLICABLE AS PER AIRCRAFT MODEL
A N EASA 2006-0286R1
- Scheda Analisi PA Sep 9, 2006 - Oxygen Cylinders CLOSED: NOT
APPLICABLE AS PER P/N INSTALLED
A N EASA 2007-0256
- Scheda Analisi PA Sep 19, 2007 - Seat Restraint System CLOSED: NOT
APPLICABLE AS PER P/N INSTALLED
A N EASA 2007-0294
ENAC 2009-060 Scheda Analisi PA - - APU Turbine wheel life limit reduction
CLOSED: NOT EFFECTIVE AS PER
APU NOT INSTALLED ON SOREM CL415
FLEET
A.D. Compliance Status A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCY s/n 2047
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 6 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCY Components Compliance Status
N N EASA 2009-0200
- Scheda Analisi AD Sep 22, 2010 N/A Navigation – Mode A/C Transponder – Check /
Modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N FAA 2009-20-10
- Scheda Analisi AD Jan 17, 2010 N/A Autopilot – servo motors modification
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
S - CF 2009-42 - SOREM ESB-4-32-4414 (SMJC 063)
Part I within 50Fh Part II: within 750 Fc
Part III: every 750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
CLOSED: SUPERSEDED BY CF 2009-42R1 (PART
I CARRIED OUT ON NOV 26, 2009)
R Y CF 2009-42R1 - SOREM ESB-4-32-4414 SMJC 063 - Every 750 Flight
cycles Special Inspection of
Accumulator Screw Caps
OPEN: PERFORMED:WITH W.O. 10/136-PART 2; PART III DUE WITHIN
490 FC
A N EASA 2009-0251
- Scheda Analisi AD Nov 26, 2009 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER S/N
INSTALLED
Y N EASA 2009-0262R1
Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER S/N
NOT INSTALLED
A.D. Compliance Status A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCY s/n 2047
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 7 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCY Components Compliance Status
N N EASA 2009-0278
- Scheda Analisi AD Jan 22, 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N TCA CF-2009-44
- Scheda Analisi AD Jul 01, 2011 N/A ELT-Potential Failure to Transmit the Required 406MHz Coded Signal
CLOSED: NOT EFFECTIVE AS PER P/N
INSTALLED
N N EASA 2010-003R1
- Scheda Analisi AD 18 Apr, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
Y N EASA
2010-0062R1
- Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
A Y FAA 2010-07-02
- Scheda Analisi AD 31 Oct 2012 N/A Honeywell Primus II RNZ 850()/-851
OPEN: INU #1 , INU #2 TO BE PERFORMED
N N EASA 2010-0067
- Scheda Analisi AD 26 Apr, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
A.D. Compliance Status A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCY s/n 2047
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 8 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCY Components Compliance Status
N N EASA 2010-30
Scheda Analisi SIB N/A N/A Risks in Transporting
Lithium Batteries in Cargo by Aircraft
CLOSED: NOT APPLICABLE SINCE
SOREM FLEET IS NOT OPERATING IN CARGO
TRANSPORT CONFIGURATION
N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer –
Erroneous Airspeed and Altitude Indications
CLOSED: NOT APPLICABLE AS PER A/C TYPE, REFER TO ADE ISSUED DATED
NOV 09, 2010
N N FAA 2011-01-09
Scheda Analisi AD 9/06/2011 N/R
B/E Aerospace protective breathing equipment P/N 119003-11 inspection for
B/A Aerospace S.B. 119003-35-6 compliance.
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
N N EASA 2011-0043
Scheda Analisi AD 30/04/2013 N/R Gables Engineering Mode S Transponder Control Panel
Modification
CLOSED: NOT APPLICABLE AS PER
P/N NOT INSTALLED ON THE A/C TYPE
N N EASA 2011-0090R1
ENAC 2011-202 Scheda Analisi AD 27/07/2011 N/R Oxygen mask regulator CLOSED: NOT
APPLICABLE AS PER P/N NOT INSTALLED ON
THE A/C TYPE
N N EASA 2011-0103
Scheda Analisi AD 03/12/2011 N/R ELT TRI-BAND Antennas
P/N 21-41 ( ) series Mod/Replacement
CLOSED: NOT APPLICABLE AS PER
P/N NOT INSTALLED ON THE A/C TYPE
A.D. Compliance Status A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCY s/n 2047
Components
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
(COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 9 of 9 S Superseded N Not effective
Date:
Sep 09, 11 Prepared by:
________________________
Approved by:
________________________
I-DPCY Components Compliance Status
N N FAA
2011-11-04
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N EASA 2010-0204
ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N FAA 2011-14-08
Scheda Analisi AD Aug 19,2014 or
6500 FH from Aug 19,2011
N/A B/E Aerospace pax oxy mask inspection
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
R Y TCCA CF-2011-35
- ESB-4-32-A4451 Rev 01
First incorporation: Within 50 Flight Hrs
upon receipt of Bombardier SB 215-
A4451
To be repeated every 165 land landings
Inspection of the MLG Upper Member forward lug using eddy current method
FIRST INCORPORATION:
CLOSED (REF TO WO 11/196);
REPETITIVE ACTION: OPEN; TO GO: 76
LANDINGS
A Y TCCA CF-2011-35
- ESB-4-32-A4450 Rev 01 November 11, 2011 N/A
Inspection of the MLG Upper Member forward lug
using liquid penetrant method
OPEN
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCZ s/n 2048
Delivery Date: April 2000
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 4 S Superseded N Not effective
Date:
Sep 09,2011 Prepared by:
________________________
Approved by:
________________________
I-DPCZ Compliance Status
A N FAA 77-17-13
NLG DOORS - CLOSED -
NOT APPLICABLE AS PER AD EFFECTIVITY
A N FAA 77-13-05
MISSING RIVETS IN BULKHEAD
- CLOSED - NOT APPLICABLE AS PER AD
EFFECTIVITY
A N TCCA CF-90-11R2 FAA 93-16-06R2
Bombardier SB215-A435
SoREM Scheda analisi AD
JUNE. 10, 1994 N/A RUDDER-AILERON
INTERCONNECT TAB (TO PREVENT POSSIBILE
FLUTTER)
- CLOSED - NOT EFFECTIVE AS PER
POWERED AILERON SYSTEM INSTALLED
S TCCA CF-92-22
FAA 94-04-02
Bombardier SB215-A3040
SoREM Scheda analisi AD
N/A ENGINE REAR MOUNT STRUTS
- CLOSED - SUPERSEDED BY
AD CF-2003-02
I Y ENAC 95-064
TCCA CF-92-10R1
P&WC: SB20914 SB21113 SB21211 SB21314
Bombardier SB215-A3060
SoREM Scheda Analisi PA
N/A ENGINE FIRE-WIRE DETECTION LOOP
- CLOSED - AD COMPLIED WITH
ENGINE FIRE DETECTION SYSTEM CONNECTED TO AIRCRAFT FIRE WARNING
SYSTEM
I Y FAA 97-11-08
AFM - LIMITATION SECTION - POWER
LEVERS
- CLOSED - AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION SECTION
PAGE 8
A N TCCA CF-96-02R1
ENAC 1999-268 - CLOSED -
AD ISSUED JUST TO CANCEL PREVIOUS REVISION
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCZ s/n 2048
Delivery Date: April 2000
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 4 S Superseded N Not effective
Date:
Sep 09,2011 Prepared by:
________________________
Approved by:
________________________
I-DPCZ Compliance Status
R N ENAC 00-265
FAA 2004-03-13 MLG AXLES - CLOSED -
NOT APPLICABLE AS PER AD EFFECTIVITY
A N TCCA CF-2002-14
FAA 2004-26-08 ENAC 02-167
Bombardier SB215-4234
SoREM DT CL-61-4234
MARCH 04, 2003 N/A PCU BACKUP PRESSURE VALVE
- CLOSED - NOT APPLICABLE AS PER VALVE
INCORPORATED AT MANUFACTURE
R N ENAC 00-496
FAA 2002-12-12 WING TO FUSELAGE FRAME ANGLES
- CLOSED - NOT APPLICABLE AS PER AD
EFFECTIVITY
S FAA 2003-04-06
ENAC 03-067
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ-850/ -851
- CLOSED - REF TO COMPONENTS
SUPERSEDED BY
FAA 2006-22-05
R Y TCCA CF-2003-02
FAA 2004-10-04 ENAC 03-251
Bombardier SB215-A4287R2
SoREM BM-CL-71-A4287
BM-CL-71-A4287R2 SMJC 31 and 32
WITHIN 50 F/H SINCE FEBRUARY
28, 2003
EVERY 250 F/H REPETITIVE ACTION
FOLLOWED BY SoREM SMJC #31 and #32
ENGINE REAR MOUNT STRUTS
- OPEN - CARRIED OUT WITH SMJC 31 & 32
WITH W.O. 11/225, 76.11 FH TO GO
28/09/2003
R Y FAA 2004-21-05 -
SCHEDA ANALISI Disposizione Tecnica
DT-CL-21-01
A 500 heater Hrs Total or 100 heater hrs TIS from 19/11/04
(whichever occurs later)
100 Hrs funzion. 24 Months
PRESSURE DECAY TEST and CABIN
HEATER (JANITROL)
OPERATIONAL TEST
REF TO COMPONENTS
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCZ s/n 2048
Delivery Date: April 2000
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 3 of 4 S Superseded N Not effective
Date:
Sep 09,2011 Prepared by:
________________________
Approved by:
________________________
I-DPCZ Compliance Status
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
REGOLATORE CARBURANTE CON VALVOLE SHUTOFF
A/B/C 14D11 o A/B/C/P 23D04
REF TO COMPONENTS
R N FAA 2005-18-05
- LOWER CAPS OF THE
WING FRONT SPAR AND REAR SPAR
- CLOSED - NOT APPLICABLE AS PER AD
EFFECTIVITY
A N EASA 2006-0375
Scheda Analisi AD Dec. 29, 2006 CARLING
TECHNOLOGIES SWITCHES
- CLOSED - NOT APPLICABLE AS PER AD
EFFECTIVITY
N N FAA 2006-22-05
EASA 2006-479 Scheda Analisi AD N/A INTEGRATED NAVIGATION UNITS
REF TO COMPONENTS Supersedes
FAA 2003-04-06
R Y TCCA CF-2008-29
FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009
BEFORE AND AFTER EVERY FIRE SEASON
OR AT SIX MONTH INTERVAL,
WHICHEVER IS SHORTER TIME
PERIOD
RUDDER LOWER TORQUE TUBE UPPER BEARING
- OPEN - COVERED BY SMJC 60; TO BE
PERFORMED WITHIN 31/10/2011
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCZ s/n 2048
Delivery Date: April 2000
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 4 of 4 S Superseded N Not effective
Date:
Sep 09,2011 Prepared by:
________________________
Approved by:
________________________
I-DPCZ Compliance Status
R Y TCCA
CF-2010-38R2
ENAC 2011-88 Bombardier SB 215 -A4424 Jun 01, 2011
FIRST INSPECTION WITHIN 50 FC FROM
20 DEC 2010; THEREAFTER REPEAT
PERRFORM AN INSPECTION BEFORE
100 FC WITH TERMINATING ACTION NOT LATER THAN Jun
01, 2011.
INSPECTION OF THE EMERGENCY WATER DUMP
PULLEY BRACKET AND STRUCTURE
-CLOSED- TERMINATING ACTION
COMPLETED WITH WO 11/070
R Y TCCA CF-2011-35
Bombardier SB 215-A4450;
Bombardier SB 215-A4451
ESB-4-32-A4450 Rev 01;
ESB-4-32-A4451 Rev 01;
Ref. To AD-PA Compliance Components
Ref. To AD-PA Compliance Components
LIQUID PENETRANT & EDDY CURRENT INSPECTION ON
MLG UPPER MEMBER FORWARD LUG
REF. TO AD-PA COMPLIANCE COMPONENTS
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0055 Manuf. date:
OTT 1999
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09,2011
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - AF0055 - Engine1 - I-DPCZ
I Y TCA CF-90-21 -
P&WC SB20355 (last R1) SB20897 (last R3)
30/04/91 N/A
O-RING DETERIORATION
DURING FUEL FILTER COVER INSTALLATION
-CLOSED- AD COMPLIED WITH AT
DELIVERY
I Y RAI 91-296
TCA CF-90-22R1 P&WC SB21018 (last R6) 30/06/94 N/A
OIL SYSTEM INSPECTION DUE TO
BEARING DETERIORATION
-CLOSED- AD COMPLIED WITH AT
DELIVERY
A N TCA CF-91-02
- P&WC SB20946 (last R2) 31/10/91 N/A
TO PREVENT IN FLIGHT TORQUE
FLUCTUATIONS
-CLOSED- N/A DUE TO ENGINE S/N AD COMPLIED WITH AT
DELIVERY
I Y RAI 91-347
TCA CF-91-26R1 P&WC
SB20914 (last R4) SB21053 (last R2)
31/03/92 N/A ENGINE FIRE DUE TO
OIL ACCUMULATING IN THE ICC CAVITY.
-CLOSED- AD COMPLIED WITH AT
DELIVERY
S RAI 93-284
TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
CLOSED- SUPERSEDED BY TCA CF-
92-03R2
I Y TCA CF-92-03R2
- P&WC
SB20957 (last R5) SB20962 (last R4) SB21065 (last R7)
21211 (last R6)
30/06/94 N/A INTERNAL OIL FIRES IN THE ICC.
-CLOSED- AD COMPLIED WITH AT
DELIVERY
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0055 Manuf. date:
OTT 1999
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09,2011
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - AF0055 - Engine1 - I-DPCZ
A N RAI 94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94
1000⇔2000 cycles
N/A REPLACEMENT HP TURBINE DISK
-CLOSED- NOT EFFECTIVE FOR
ENGINES S/N 109022 AND SUBSEQUENT
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077 (last R8) SB21364 (last R1) SB21373 (last R3)
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A
REPLACEMENT OF FUEL NOZZLES
LOCKING PLATES AND “O” RINGS
-CLOSED- AD COMPLIED WITH AT
DELIVERY
A N ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB21100 (last R3)
all spare heaters within 02/03/01
installed p/n 10718
before 31/08/02
N/A ENGINE PW100 SERIES FUEL HEATERS
-CLOSED- NOT EFFECTIVE FOR
ENGINES S/N 109036 AND SUBSEQUENT
A N ENAC 02-090
TCA CF-2002-10 -CLOSED- N/A AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21562 (last R2)
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within
2400 f/h or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
-CLOSED- AD COMPLIED WITH AT
DELIVERY (NO REPETITIVE ACTION)
28/09/2003
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0080 Manuf. date:
DEC 2000
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09,2011
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - AF0080 - Engine2 - I-DPCZ
I Y TCA CF-90-21 -
P&WC SB20355 (last R1) SB20897 (last R3)
30/04/91 N/A
O-RING DETERIORATION
DURING FUEL FILTER COVER INSTALLATION
-CLOSED- AD COMPLIED WITH AT
DELIVERY
I Y RAI 91-296
TCA CF-90-22R1 P&WC SB21018 (last R6) 30/06/94 N/A
OIL SYSTEM INSPECTION DUE TO
BEARING DETERIORATION
-CLOSED- AD COMPLIED WITH AT
DELIVERY
A N TCA CF-91-02
- P&WC SB20946 (last R2) 31/10/91 N/A
TO PREVENT IN FLIGHT TORQUE
FLUCTUATIONS
-CLOSED- N/A DUE TO ENGINE S/N AD COMPLIED WITH AT
DELIVERY
I Y RAI 91-347
TCA CF-91-26R1 P&WC
SB20914 (last R4) SB21053 (last R2)
31/03/92 N/A ENGINE FIRE DUE TO
OIL ACCUMULATING IN THE ICC CAVITY.
-CLOSED- AD COMPLIED WITH AT
DELIVERY
S RAI 93-284
TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES INTERCOMPRESSOR
CASE (ICC)
CLOSED- SUPERSEDED BY TCA CF-
92-03R2
I Y TCA CF-92-03R2
- P&WC
SB20957 (last R5) SB20962 (last R4) SB21065 (last R7)
21211 (last R6)
30/06/94 N/A INTERNAL OIL FIRES IN THE ICC.
-CLOSED- AD COMPLIED WITH AT
DELIVERY
A.D. Compliance Status
Eng. Type:
PW123AF
Eng. S/N. :
AF0080 Manuf. date:
DEC 2000
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09,2011
Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - AF0080 - Engine2 - I-DPCZ
A N RAI 94-001
TCA CF 94-01 FAA 94-03-02 Amdt 39-8808
P&WC SIL 307 Since 14/01/94
1000⇔2000 cycles
N/A REPLACEMENT HP TURBINE DISK
-CLOSED- NOT EFFECTIVE FOR
ENGINES S/N 109022 AND SUBSEQUENT
I Y ENAC 96-353
TCA CF-96-22
P&WC SB21077 (last R8) SB21364 (last R1) SB21373 (last R3)
First nozzle replacement or within 30/11/98
Whichever occurs first
N/A
REPLACEMENT OF FUEL NOZZLES
LOCKING PLATES AND “O” RINGS
-CLOSED- AD COMPLIED WITH AT
DELIVERY
A N ENAC 01-065
TCA CF-2000-34 FAA 2003-16-04
P&WC SB21100 (last R3)
all spare heaters within 02/03/01
installed p/n 10718
before 31/08/02
N/A ENGINE PW100 SERIES FUEL HEATERS
-CLOSED- NOT EFFECTIVE FOR
ENGINES S/N 109036 AND SUBSEQUENT
A N ENAC 02-090
TCA CF-2002-10 -CLOSED- N/A AS PER ENGINE MODEL
I Y ENAC 02-448
TCA CF-2002-34 FAA 2004-20-01
P&WC SB21562 (last R2)
SB21669 SOREM DT-CL-73-04
Within 400 f/h or “C/2” Inspection
1200 f/h or 3A Final Action within
2400 f/h or 23/8/2004
INSPECTION /MODIFICATION OF MECHANICAL FUEL
CONTROL UNIT
-CLOSED- AD COMPLIED WITH AT
DELIVERY (NO REPETITIVE ACTION)
28/09/2003
EASA/TCA/FAA/ENAC
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
991014 Manuff. date:
OCT 28, 1999
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09, 2011 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report Propeller 1 I-DPCZ
I Y FAA 93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided transfer tube
- CLOSED - AD COMPLIED WITH
P/N 814829-1
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS SB
14SF-61-82)
Shaft Torque Check 5000 Hrs.
PCU INSPECTION/ MODIFICATION
OPEN: PCU HOURS: 31.03
INSPECTION PERFORMED EVERY O/H
(NEXT DUE WITHIN 1968.57)
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION NOT APPLICABLE FOR
BLADE #1 S/N
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION NOT APPLICABLE FOR
BLADE #2 S/N
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION NOT APPLICABLE FOR
BLADE #3 S/N
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or within
28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION NOT APPLICABLE FOR
BLADE #4 S/N
EASA/TCA/FAA/ENAC
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
991014 Manuff. date:
OCT 28, 1999
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09, 2011 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report Propeller 1 I-DPCZ
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE HOURS: TTSN :N/A; TSO:
566.58 INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 1433.02)
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: ACTUATOR HOURS: TTSN :N/A; TSO:
566.58 INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 1433.02)
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
PCU mod –A48 10.500 Hrs 10.500 Hours
CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,
ACTUATOR ASSEMBLY
OPEN: PCU HOURS (TSO): 31.03
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 1968.57)
28/09/2003
A N FAA 2006-24-07
Scheda Analisi PA Jan 3, 2007 NOT APPLICABLE AS PER PROPELLER MODEL
A N FAA US-2011-04-02
ENAC 2011-68 ADE issued Apr 15, 2011 NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
20000125 Manuf. date:
JAN 30, 2000
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective
Date:
Sep 09,2011 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - 20000125 - Propeller 2 - I-DPCZ
I Y FAA 93-06-06 - H.S.
ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided transfer tube
-CLOSED- P/N 814829-1 INSTALLED
AD COMPLIED WITH
R Y ENAC 96-004
supersedes 95-046
FAA 95-22-12 Amdt 39-9420
H.S. ASB 14SF-61-A59R6
SB -67R2/-81R2/-82R1
5000 Hrs (PostMod HS
SB 14SF-61-82)
Shaft Torque Check
5000 Hrs
PCU INSPECTION/ MODIFICATION
OPEN: PCU HOURS: 516.12
INSPECTION PERFORMED EVERY O/H
(NEXT DUE WITHIN 1483.48)
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
-CLOSED- NOT APPLICABLE FOR BLADE
#1 S/N 882399-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
-CLOSED- NOT APPLICABLE FOR BLADE
#2 S/N 890123-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
-CLOSED- NOT APPLICABLE FOR BLADE
#3 S/N 890124-19
A N ENAC 96-177
FAA 96-08-02 Amdt 39-9568
H.S. ASB 14SF-61-A95R1/-
A93/A92R1
since 09/05/96 300 cycles or
within 28/02/97 500 cycles BLADE INSPECTION /
MODIFICATION
-CLOSED- NOT APPLICABLE FOR BLADE
#4 S/N 890126-19
A.D. Compliance Status
Prop. Type:
Hamilton Sundstrand 14SF-19
Prop. S/N. :
20000125 Manuf. date:
JAN 30, 2000
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 2 S Superseded N Not effective
Date:
Sep 09,2011 Prepared by:
________________________
Approved by:
________________________
AD-PA Compliance Status Report - 20000125 - Propeller 2 - I-DPCZ
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
6000 Hrs or 3 years since February 7,
1997
10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: TRANSFER TUBE HOURS: TTSN :N/A; TSO: 1625.34
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 374.19)
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
6000 Hrs or 3 years since February 7,
1997
10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: ACTUATOR HOURS TTSN :N/A; TSO: 1625.34
INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)
AD COMPLIED WITH (NEXT DUE WITHIN 374.19)
R Y ENAC 97-034
FAA 96-25-20 Amdt 39-9863
H.S. ASB 14SF-61-70R2
6000 Hrs or 3 years since February 7,
1997
10.500 Hours
CRITICAL PARTS INSPECTION: PCU,
TRNSFER TUBE, ACTUATOR ASSEMBLY
OPEN: PCU HOURS (TSO): 516.12 INSPECTION SCHEDULED EVERY
2000 FH (prop. O/H) AD COMPLIED WITH
(NEXT DUE WITHIN 1483.48) 28/09/2003
A N FAA 2006-24-07
Scheda Analisi PA Jan 3, 2007 -CLOSED-
NOT APPLICABLE AS PER PROPELLER MODEL
A N FAA US-2011-04-02
ENAC 2011-68 ADE issued Apr 15, 2011 CLOSED: NOT APPLICABLE AS PER PROPELLER MODEL
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCZ s/n 2048
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 9 S Superseded N Not effective
Date:
Sep 09 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCZ Components Compliance Status
A N FAA 81-21-05
Nov 19, 1981 N/A ARTEX ELT Battery not usable in salt environment
CLOSED: NOT APPLICABLE, SUBJECT ELT BATTERY NOT
INSTALLED
A N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782
RAI 74-225 N/A N/A Ni-Cd batterie con celle in
polistirolo
CLOSED: NOT APPLICABLE - TEMPERATURE SENSING
INSTALLED ON BATTERIES EMBODIED
S RAI 82-113
- CLOSED - SUPERS. BY ENAC 96-348
N N TCCA CF-96-21
FAA 72-19-04 Amdt. 39-1782 - N/A N/A Ni-Cd batteries
- CLOSED - CF96-21 ISSUED TO CANCEL THE
APPLICABILITY OF FAA 72-19-04
S RAI 88-052
- CLOSED - SUPERS. BY ENAC 88-096
R Y RAI 88-096
FAR 43 Appendix E
Norma di lavoro NL-CL-34-06 19/11/2005 24 Months ALTIMETER AND STATIC
PRESSURE SYSTEM - OPEN -
CARRIED OUT ON JAN 28, 2010; NEXT DUE WITHIN JAN 26, 2012
I Y ENAC 96-052
FAA FAR 91.21 N/A N/A USE OF PORTABLE ELETTRONIC DEVICES
- CLOSED - AFM UPDATED – CREW
INFORMED
N N ENAC 96-348
FAA 96-20-07 Amdt 39-9773 -
Within 500 Hrs (TIS) or 12 mths from 14/11/96
100 Hrs funzion. 24 Months
COMBUSTION CHAMBER DECAY TEST (JANITROL)
- CLOSED - NOT APPLICABLE
HEATER MODEL B4500 (CERAMIC COMBUSTION TUBE)
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCZ s/n 2048
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 2 of 9 S Superseded N Not effective
Date:
Sep 09 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCZ Components Compliance Status
N N ENAC 97-167
FAA 97-11-10 - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
- CLOSED - NOT APPLICABLE
SCOTT OXYGEN MASKS INSTALLED
N N TCCA CF-95-16
ENAC 97-221 Marathon Power SB 111692-014 27/07/96 N/A
PCB SERIES PC-250 MODIFICATION OR
REMOVAL
- CLOSED - NOT APPLICABLE AS PER
INVERTER INSTALLED (Serie MSI-800)
N N ENAC 97-274
FAA 97-18-03 - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
- CLOSED - NOT APPLICABLE
SCOTT OXYGEN MASKS INSTALLED
N N ENAC 99-231
FAA 99-08-21 - N/A PURITAIN-BENNETT CREW OXYGEN MASKS
- CLOSED - NOT APPLICABLE
SCOTT OXYGEN MASKS INSTALLED
S ENAC 00-018
FAA 99-23-22 Norma di Lavoro NL-CL-34-07 Apr 17, 2000 Every 90 days
TRANSPONDER MODO “C”
INSPECTION/TEST
- CLOSED - Superseded by ENAC 00-209
N N ENAC 00-209
FAA 99-23-22 Amdt. 39-11686
Engineering InstructionEI 004/00 18/05/00 N/A TRANSPONDER MODO
“C”
- CLOSED - NOT APPLICABLE
AD RESCINDED APR. 12, ‘00
Supersedes ENAC 00-018
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCZ s/n 2048
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 3 of 9 S Superseded N Not effective
Date:
Sep 09 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCZ Components Compliance Status
S ENAC 01-173
FAA 2001-08-01 Scheda Analisi PA May 2, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04
- CLOSED - NOT APPLICABLE AS PER
HEATER INSTALLED
Supers. By ENAC 01-368
A N ENAC 01-368
FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A FUEL SHUT-OFF VALVES
P/N 14D11 o 23D04 P/N installed on A/C: J20C30
- CLOSED - NOT APPLICABLE AS PER
HEATER INSTALLED
Supersedes ENAC 01-173
N N ENAC 01-442
FAA 2001-18-05 Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.
- CLOSED - NOT APPLICABLE PER P/N
I Y ENAC 01-470
FAA 2001-22-14 SoREM DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER
DISCHARGER
- CLOSED - P/N AFFECTED CHECKED.
WALTER KIDDE CARTRIDGES INSTALLED ON
I Y TCCA CF-2002-14
ENAC 02-167
BOMBARDIER SB215-3108 SB215-4234
SoREM BM-CL-61-4234
04/03/2003 N/A
PROPELLER CONTROL UNIT
BACKUP PRESSURE RELIEF VALVE
- CLOSED - SB215-4234 IS INCORPORATED
DURING PRODUCTION
I Y ENAC 03-067
FAA 2003-04-06
SoREM DT-CL-34-05
DT-CL-34-07R1 BM-CL-34-4343
March 16, 2003 N/A INU Honeywell Primus II RNZ -850/ -851
- CLOSED - INU P/N 7510100-732 (#1) AND 7510100-731 (#2) INSTALLED
28/09/2003
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCZ s/n 2048
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 4 of 9 S Superseded N Not effective
Date:
Sep 09 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCZ Components Compliance Status
N N FAA 2003-23-05
ENAC 2004-003 - December 24, 2005 N/A Titeflex Corporation,
Tubi Flessibili
- CLOSED - NOT APPLICABLE
HOSES INSTALLATI P/N 114040-4
N N FAA 2003-23-05
ENAC 2004-073 - December 24, 2005 N/A Titeflex Corporation,
Tubi Flessibili
- CLOSED - NOT APPLICABLE
HOSES INSTALLATI P/N 114040-4
R Y FAA
2004-21-05 Amdt.39-13826
- Scheda Analisi PA DT-CL-21-01
A 500 heater Hrs or 100 heater Hrs
TIS since 19/11/04
(whichever occurs later)
100 Hrs (TIS) or
24 Months
PRESSURE DECAY TEST ed Operational Test del CABIN
HEATER (JANITROL)
- OPEN - HEATER TIME IN
SERVICE CHECKED: 126.36 HOURS AT JAN
20, 2010; TEST NOT YET PERFORMED
A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A
FUEL SHUT-OFF VALVES P/N 14D11 o 23D04
P/N installed on A/C: J20C30
- CLOSED - NOT APPLICABLE AS
PER HEATER INSTALLED
R Y EASA 2006-0265 - Scheda Analisi PA
ESP-4-34-001 Within
Mar 13, 2007 24 Months MODE “S” and “C” TRANSPONDERS CHECK
- OPEN - CARRIED OUT DURING LAST ANNUAL CHECK:
(CRS DATED: 13/06/2011)
A N EASA 2006-0269
- Scheda Analisi PA MODE “S” TRANSPONDERS - CLOSED -
N/A AS PER MODEL NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCZ s/n 2048
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 5 of 9 S Superseded N Not effective
Date:
Sep 09 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCZ Components Compliance Status
A N FAA 2006-18-08 Scheda Analisi AD Oct. 11, 2006 GOODYEAR
NOSE WHEEL TIRES
- CLOSED - NOT APPLICABLE AS
PER GOODYEAR TIRES NOT
INSTALLED
A N FAA 2006-19-04
Scheda Analisi AD MODE “S” TRANSPONDERS - CLOSED -
N/A AS PER PART NUMBER NOT
INSTALLED
N N FAA 2006-22-05
ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU
- CLOSED - NOT APPLICABLE AS
PER COMPONENT MODIFIED (REF TO
FAA-2003-04-06)
A N EASA 2006-0366
Scheda Analisi PA Dec 14, 2006 LIFE RAFT - CLOSED -
NOT APPLICABLE AS PER AIRCRAFT MODEL
A N EASA 2006-0286R1
Scheda Analisi PA Sep 9, 2006 Oxygen Cylinders - CLOSED -
NOT APPLICABLE AS PER P/N NOT INSTALLED
A N EASA 2007-0256
Scheda Analisi PA Sep 19, 2007 Seat Restraint System - CLOSED -
NOT APPLICABLE AS PER P/N NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCZ s/n 2048
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 6 of 9 S Superseded N Not effective
Date:
Sep 09 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCZ Components Compliance Status
A N EASA 2007-0294
ENAC 2009-060 Scheda Analisi PA APU Turbine wheel life limit reduction
- CLOSED - NOT EFFECTIVE AS
PER APU NOT INSTALLED ON SOREM
CL415 FLEET
N N EASA 2009-0200
Scheda Analisi AD Sep 22, 2010 N/A Navigation – Mode A/C Transponder – Check /
Modification
- CLOSED - NOT EFFECTIVE AS
PER P/N NOT INSTALLED
N N FAA 2009-20-10
Scheda Analisi AD Jan 17, 2010 N/A Autopilot – servo motors modification
- CLOSED - NOT EFFECTIVE AS
PER P/N NOT INSTALLED
S - CF 2009-42 - SOREM ESB-4-32-
4414 (SMJC 063)
Part I within 50FhPart II: within 750
Fc Part III: every
750 Fc
Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
- CLOSED - SUPERSEDED BY CF
2009-42R1 (PART I CARRIED OUT ON NOV
26, 2009)
R Y CF 2009-42R1 Enac 2010-183 Scheda Analisi AD Every 750 Flight cycles
Special Inspection of Accumulator Screw Caps
- OPEN - CARRIED OUT WITH
ESB-4-32-4414R1 (SMJC 63 PERFORMED ON JUL 22, 2010); NEXT DUE: 547 CYCLES
Y N EASA 2009-0251
Scheda Analisi AD Nov 26, 2009 N/A Portable Halon 1211 Fire Extinguisher
- CLOSED - NOT EFFECTIVE AS
PER S/N NOT INSTALLED
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCZ s/n 2048
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 7 of 9 S Superseded N Not effective
Date:
Sep 09 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCZ Components Compliance Status
Y N EASA 2009-0262R1
Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A Portable Halon 1211 Fire Extinguisher
- CLOSED - NOT EFFECTIVE AS
PER S/N NOT INSTALLED
N N EASA 2009-0278
- Scheda Analisi AD Jan 22, 2010 N/A Portable Halon 1211 Fire Extinguisher
- CLOSED - NOT EFFECTIVE AS PER P/N INSTALLED
N N TCA CF-2009-44
Scheda Analisi AD Jul 1, 2011 N/A ELT-Potential Failure to Transmit
the Required 406MHz Coded Signal
- CLOSED - NOT EFFECTIVE AS
PER P/N NOT INSTALLED
N N EASA 2010-003R1
Scheda Analisi AD 18 Apr, 2010 N/A TDR-94 and TDR-94D transponders
- CLOSED - NOT EFFECTIVE AS
PER P/N NOT INSTALLED
Y N EASA
2010-0062R1
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
- CLOSED - NOT EFFECTIVE AS
PER P/N NOT INSTALLED
A Y FAA 2010-07-02
Scheda Analisi AD 31 Ott 2012 N/A Honeywell Primus II RNZ 850()/-851
- OPEN - TO BE INTRODUCED ON BOTH INU 1 & 2.
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCZ s/n 2048
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 8 of 9 S Superseded N Not effective
Date:
Sep 09 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCZ Components Compliance Status
N N EASA 2010-0067
Scheda Analisi AD 26 Apr, 2010 N/A TDR-94 and TDR-94D transponders
- CLOSED - NOT EFFECTIVE AS
PER P/N NOT INSTALLED
N N EASA 2010-30
Scheda Analisi SIB N/A N/A Risks in Transporting Lithium Batteries in Cargo by Aircraft
- CLOSED - NOT APPLICABLE
SINCE SOREM FLEET IS NOT OPERATING IN CARGO TRANSPORT
CONFIGURATION
N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer – Erroneous Airspeed and Altitude Indications
- CLOSED - NOT APPLICABLE AS
PER A/C TYPE, REFER TO ADE ISSUED DATED
NOV 09, 2010
N N FAA 2011-01-09
Scheda Analisi AD 9/06/2011 N/R
B/E Aerospace protective breathing equipment P/N 119003-11 inspection for B/A Aerospace S.B. 119003-35-6 compliance.
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
N N EASA 2011-0043
Scheda Analisi AD 30/04/2013 N/R Gables Engineering Mode S Transponder Control Panel
Modification
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N EASA 2011-0090R1
ENAC 2011-202 Scheda Analisi AD 27/07/2011 N/R Oxygen mask regulator CLOSED: NOT
APPLICABLE AS PER P/N NOT INSTALLED ON
THE A/C TYPE
A.D. Compliance Status
A/C Type:
Canadair CL-415
A/C Reg. :
I-DPCZ s/n 2048
Componenti
EFFE
CT
P.A. / A.D. Other
Authority issues
ISSUED DOCUMENTS EXPIRATION REPETITIVE
ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)
A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 9 of 9 S Superseded N Not effective
Date:
Sep 09 2011 Prepared by:
________________________
Approved by:
________________________
I-DPCZ Components Compliance Status
N N EASA 2011-0103
Scheda Analisi AD 03/12/2011 N/R ELT TRI-BAND Antennas P/N 21-41 ( ) series Mod/Replacement
CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED
ON THE A/C TYPE
N N FAA
2011-11-04
Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N EASA 2010-0204
ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A TDR-94 and TDR-94D transponders
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
N N FAA 2011-14-08
Scheda Analisi AD Aug 19,2014 or 6500 FH from Aug 19,2011
N/A B/E Aerospace pax oxy mask inspection
CLOSED: NOT EFFECTIVE AS PER P/N
NOT INSTALLED
R Y TCCA CF-2011-35
- ESB-4-32-A4451 Rev 01
First incorporation:
Within 50 Flight Hrs upon receipt of Bombardier SB 215-A4451
To be repeated every 165 land
landings
Inspection of the MLG Upper Member forward lug using eddy
current method
FIRST INCORPORATION:
CLOSED (REF TO WO 11/197);
REPETITIVE ACTION: OPEN; TO GO: 74
LANDINGS
A Y TCCA CF-2011-35
- ESB-4-32-A4450 Rev 01
November 11, 2011 N/A
Inspection of the MLG Upper Member forward lug using liquid
penetrant method OPEN