cescom 10 - aircraft status report - elliott jets · 2020. 3. 11. · (eng) due 1 (eng) due 2 adj....

CESCOM 10 - Aircraft Status Report

Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015

SBM CLEANING COMPANY LLC

560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:

Aircraft Serial: 560-0096 Unit: 0096 Reg No: N10TD

3:12PM31-Aug-2015

Part Number

Part Serial No

Item Code Description C/W Time 1 TBO 1

Drawing # / Task # City Mod Lvl C/W Time 2 TBO 2Position

Remains

RemainsTSO 2

TSO 1

Maintenance Inspections

(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

055601 INSPECT WINDSHIELD INSPECTION

LEFT

SMF

31-Oct-20162409-Oct-2014MTH 14 m 0 d

6447.13006147.1HRS 108

5586LDG

055601 INSPECT WINDSHIELD INSPECTION

RIGHT

SMF

31-Oct-20162409-Oct-2014MTH 14 m 0 d

6447.13006147.1HRS 108

5586LDG

055602 INSPECT SIDE WINDOW INSPECTION

LEFT

SMF

31-Oct-20162409-Oct-2014MTH 14 m 0 d

6447.13006147.1HRS 108

5586LDG

5-12-01 PHASE 1

051201

SMF

30-Apr-20162411-Apr-2014MTH 8 m 0 d

6343.93006043.9HRS 4.8

5528LDG

5-12-02 PHASE 2

051202

SMF

30-Apr-20162411-Apr-2014MTH 8 m 0 d

6343.93006043.9HRS 4.8

5528LDG

5-12-03 PHASE 3

051203

SMF

31-Jan-20172429-Jan-2015MTH 17 m 0 d

6447.13006147.1HRS 108

5586LDG

5-12-04 PHASE 4

051204

SMF

31-Jan-20172429-Jan-2015MTH 17 m 0 d

6447.13006147.1HRS 108

5586LDG

5-12-05 PHASE 5

051205

SMF

31-May-20183622-May-2015MTH 33 m 0 d

7483.912006283.9HRS 1144.8

5674LDG

5-12-11 PHASE 11

051211

SMF

30-Nov-2015622-May-2015MTH 3 m 0 d

6283.9HRS

5674LDG

5-12-13 PHASE 13

051213

SMF

07-Jun-2007MTH

996950004969HRS 3629.9

5-12-14 PHASE 14

051214

*CF

09-Apr-1991MTH

12000120000HRS 5660.9

5-12-15 PHASE 15

051215

*CF

09-Apr-1991MTH

10000100000HRS 3660.9

5-12-16 PHASE 16

051216

*CF

09-Apr-1991MTH

10000100000HRS 3660.9

5-12-17 PHASE 17

051217

*CF

09-Apr-1991MTH

10000100000HRS 3660.9

5-12-18 PHASE 18

051218

SMF

31-Jan-20161229-Jan-2015MTH 5 m 0 d

6147.1HRS

5586LDG

PHASE 56 SHOULD BE ACCOMPLISHED IN CONJUNCTION WITH THE PHASE 18. PHASE 56 ADDED PER REV 21 TO 560 MM. OCTOBER

2005

A262003 INSPECT/WEIGH PORTABLE HALON FIRE EXTINGUISHER : PHASE 18

GH2-1/2J

V461840

CABIN

051208

SMF 31-Jan-20161228-Jan-2015MTH 5 m 0 d

A262003 INSPECT/WEIGH PORTABLE HALON FIRE EXTINGUISHER : PHASE 18

GH2-1/2J

V467489

COCKPIT

051208

SMF 31-Jan-20161228-Jan-2015MTH 5 m 0 d

5-12-20 PHASE 20

SMF

2409-Sep-2013MTH

5961.8HRS

5486LDG

A341012 PERFORM STATIC PORT HEIGHT AND SLOPE CHECK (AIRPLANES -0001 THRU -0259 CERTIFIED FOR RVSM): PHASE 20

051220 SMF 30-Sep-20152409-Sep-2013MTH 1 m 0 d

5961.8HRS

5486LDG

of 66NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from Print

Date for calendar items.


Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015

Description C/W Time 1 TBO 1

Drawing # / Task # City Mod Lvl C/W Time 2 TBO 2

Remains


Remains

TSO 1

TSO 2

Item Code Part Number

Part Serial NoPosition

(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

B341001 CALIBRATION TEST AIRSPEED INDICATOR (AIRPLANES -0001 THRU -0259) NOT CERTIFIED FOR RVSM (FAR 91.411): PHASE 20

C661063-0106

W20628

NO. 1

051220 : L-A/S

SMF 30-Sep-20152403-Sep-2013MTH 1 m 0 d

B341001 CALIBRATION TEST AIRSPEED INDICATOR (AIRPLANES -0001 THRU -0259) NOT CERTIFIED FOR RVSM (FAR 91.411): PHASE 20

C661063-0106

W27154H

NO. 2

051220 : R-A/S

SMF 30-Sep-20152403-Sep-2013MTH 1 m 0 d

B341003 CALIBRATION TEST ALTIMETER (91.411): PHASE 20

4016341-905

90116311

LEFT

051220 : L-ALT

SMF

30-Sep-20152403-Sep-2013MTH 1 m 0 d

B341003 CALIBRATION TEST ALTIMETER (91.411): PHASE 20

570-24929-013

3555

STANDBY

051220 : STDBY

SMF

30-Sep-20152403-Sep-2013MTH 1 m 0 d

B341005 LEAK TEST STATIC SYSTEM (FAR 91.411) AIRPLANES -0001 THRU -0259 NOT CERTIFIED FOR RVSM: PHASE 20

LEFT

051220 : L

SMF 30-Sep-20152403-Sep-2013MTH 1 m 0 d

B341005 LEAK TEST STATIC SYSTEM (FAR 91.411) AIRPLANES -0001 THRU -0259 NOT CERTIFIED FOR RVSM: PHASE 20

RIGHT

051220 : R

SMF 30-Sep-20152403-Sep-2013MTH 1 m 0 d

B341011 CALIBRATION TEST AIR DATA COMPUTER (FAR 91.411) AIRPLANES -0001 THRU -0259 CERTIFIED FOR RVSM: PHASE 20

7024900-30302

04060795

NO. 1

051220 : ADC

SMF 30-Sep-20152403-Sep-2013MTH 1 m 0 d

B345001 CALIBRATION TEST ATC TRANSPONDER (FAR 91.413): PHASE 20

7510774-901

900304483

NO. 1

051220 : XPDR1

SMF 30-Sep-20152403-Sep-2013MTH 1 m 0 d

B345001 CALIBRATION TEST ATC TRANSPONDER (FAR 91.413): PHASE 20

7510774-901

91120762

NO. 2

051220 : XPDR2

SMF 30-Sep-20152403-Sep-2013MTH 1 m 0 d

5-12-21 PHASE 21

SMF

2409-Oct-2014MTH

6147.1HRS

5586LDG

A237003 INSPECT CVR UNDERWATER LOCATOR BEACON : PHASE 21

DK100

SC48989

051221 : CVR

SMF

31-Oct-20162409-Oct-2014MTH 14 m 0 d

6147.1HRS

5586LDG

B237004 OPERATIONAL TEST CVR UNDERWATER LOCATOR BEACON : PHASE 21

DK100

SC48989

051221 : CVR SMF 31-Oct-20162409-Oct-2014MTH 14 m 0 d

6147.1HRS

5586LDG

5-12-28 PHASE 28

SMF

22-May-2015MTH

1006283.9HRS

5674LDG

B243002 FUNCTIONAL CHECK MAIN SHIP BATTERY MARATHON NI-CAD BATTERY (CAPACITY CHECK): PHASE 28

30978-002

11402005

SMF 22-May-2015MTH

6383.91006283.9HRS 44.8

5674LDG

5-12-30 PHASE 30

051230

SMF

09-Oct-2014MTH

6747.16006147.1HRS 408

5586LDG

5-12-32 PHASE 32

051232

*CF

09-Apr-1991MTH

15000150000LDG 9287

5-12-33 PHASE 33

051233

*CF

09-Apr-1991MTH

15000150000LDG 9287

5-12-34 PHASE 34

051234

*CF

09-Apr-1991MTH

672567250HRS 385.9

5-12-48 PHASE 48 7209-Apr-1991MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains


Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

B262004 EMPTY/INSPECT/RECHARGE PORTABLE HALON FIRE EXTINGUISHER : PHASE 48

GH2-1/2J

V461840

CABIN

051248 : A

SMF 31-Jul-20167209-Jul-2010MTH 11 m 0 d

5437.2HRS

5216LDG

B262004 EMPTY/INSPECT/RECHARGE PORTABLE HALON FIRE EXTINGUISHER : PHASE 48

GH2-1/2J

V467489

COCKPIT

051248 : F

SMF 31-Jul-20167209-Jul-2010MTH 11 m 0 d

5437.2HRS

5216LDG

5-12-49 PHASE 49

051249

SMF

31-Oct-20173609-Oct-2014MTH 26 m 0 d

7347.112006147.1HRS 1008

5586LDG

5-12-54 PHASE 54 31-Aug-201512MTH 0 d

6695.17600HRS 356.07

Over Due

5-12-56 PHASE 56

051256

SMF

31-Oct-20151209-Oct-2014MTH 2 m 0 d

6147.1HRS

5586LDG

5-12-59 PHASE 59 A/R09-Apr-1991MTH

0HRS

0LDG

A561004 PERFORM CO-PILOTS INNER WINDOW COPILOT SIDE WINDOW INSPECTION : PHASE 59

5511285-6

110104

RIGHT INBOARD A/R09-Apr-1991MTH

A561004 PERFORM CO-PILOTS OUTER WINDOW COPILOT'S SIDE WINDOW INSPECTION : PHASE 59

5511285-78

3705

RIGHT OUTBOARD A/R09-Apr-1991MTH

5-12-60 PHASE 60

SMF

09-Sep-2013MTH

6461.85005961.8HRS 122.7

5486LDG

5-12-61 PHASE 61 09-Apr-1991MTH

13200132000HRS 6860.9

5-12-62 PHASE 62 09-Apr-1991MTH

15600156000HRS 9260.9

5-12-63 PHASE 63 09-Apr-1991MTH

15600156000HRS 9260.9

5-12-64 PHASE 64

SMF

30-Nov-2015622-May-2015MTH 3 m 0 d

6283.9HRS

5674LDG

5-12-65 PHASE 65

SMF

11-Apr-2014MTH

6043.9HRS

5528LDG

5005000ACH 500

5-12-66 PHASE 66 31-Aug-2028180MTH 156 m 0 d

11956.056000HRS 5616.95

5-12-67 PHASE 67 MTH

1000010000HRS 3660.9

5-12-MC PHASE MC

0512MC

SMF

29-Jan-2015MTH

7603.114566147.1HRS 1264

5586LDG

5-12-MD PHASE MD

0512MD

SMF

17-Nov-2005MTH

728925234766HRS 949.9

5-12-ME PHASE ME

0512ME

MHR

16-Apr-2002MTH

850644504056HRS 2166.9

5-12-MF PHASE MF

0512MF

SMF

17-Nov-2005MTH

976650004766HRS 3426.9




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains


Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

5-12-MG PHASE MG 09-Apr-1991MTH

100000LDG

A325009 INSPECT NOSE GEAR FORK/PISTON NOSE LANDING GEAR FORK: PHASE MG

6642000-3

SN-UNKNOWN

0512MG *CF MTH

1000010000LDG 4287

5-12-MI PHASE MI

0512MI

SMF

25-Jun-2008MTH

1031051305180HRS 3970.9

5-12-MJ PHASE MJ

0512MJ

ICT

14-Jun-2013MTH

1180059005917.1HRS 5460.9-17.1

5466LDG

5-12-MK PHASE MK

0512MK

*CF

09-Apr-1991MTH

672567250HRS 385.9

5-12-ML PHASE ML

SMF

11-Apr-2014MTH

6343.93006043.9HRS 4.8

5528LDG

057110 MINOR INSPECTION

E1

SMF

31-Jan-20172429-Jan-2015MTH 17 m 0 d

(6415.4)6447.13006147.1HRS 108

5586LDG

057110 MINOR INSPECTION

E2

SMF

31-Jan-20172429-Jan-2015MTH 17 m 0 d

(6415.4)6447.13006147.1HRS 108

5586LDG

129999 INSPECT AIRCRAFT SURVEY

SMF

O/C31-Mar-2000MTH

3718HRS

215012 REPLACE MOTOR COMPRESSOR DRIVE MOTOR BRUSHES (COMPRESSOR MOTORS P/N 1134104-1, -5 OR FWA1134104-1, -5

ONLY)

1250150

444

SMF N/R11-Apr-2014MTH

6043.9HRS

5528LDG

263005 REPLACE (MAX LIFE) CARTRIDGE (SERVICE LIFE)

873364-1

021632

FORWARD LEFT

262003 : FL

MHR

N/AMTH 84


873364-1

051485

FORWARD RIGHT

262003 : FR

MHR

N/AMTH 84


873364-1

051474

AFT LEFT

262003 : AL

MHR

N/AMTH 84


873364-1

041409

AFT RIGHT

262003 : AR

MHR

N/AMTH 84

B262002 HYDROSTATIC TEST ENGINE FIRE BOTTLE

898066-2

92793EK

AFT

051223 : A

SMF

31-Mar-20166004-Mar-2011MTH 7 m 0 d

5568.6HRS

5282LDG

B262002 HYDROSTATIC TEST ENGINE FIRE BOTTLE

898066-2

92770EK

FORWARD

051223 : F

SMF

31-Mar-20166004-Mar-2011MTH 7 m 0 d

5568.6HRS

5282LDG

B262003 HYDROSTATIC TEST PORTABLE HALON FIRE EXTINGUISHER

GH2-1/2J

V461840

CABIN

051247 : A

SMF

30-Sep-202514406-Sep-2013MTH 121 m 0 d

B262003 HYDROSTATIC TEST PORTABLE HALON FIRE EXTINGUISHER

GH2-1/2J

V467489

COCKPIT

051247 : F

SMF

30-Sep-202514406-Sep-2013MTH 121 m 0 d

324201 NON DESTRUCTIVE TEST MLG WHEEL ASSEMBLY

3-1490-1

1677

LEFT

SMF

T/C22-May-2015MTH

6283.9HRS

5674LDG




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains


Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

324201 NON DESTRUCTIVE TEST MLG WHEEL ASSEMBLY

3-1490-1

1488/3066

RIGHT

SMF

T/C22-May-2015MTH

6283.9HRS

5674LDG

324202 NON DESTRUCTIVE TEST NOSE WHEEL ASSEMBLY

3-1418

6630

SMF

T/C22-May-2015MTH

6283.9HRS

5674LDG

B326003 HYDROSTATIC TEST PNEUMATIC BLOWDOWN/EMERGENCY BRAKE BOTTLE

212940-2

8392

051222 : GEAR SMF 31-Jan-20183627-Jan-2015MTH 29 m 0 d

341090 CALIBRATION TEST ADC ALTIMETER (91.411)

70251N02D04

04111502D

RVSM

051220 : RVSM

SMF

30-Sep-20152409-Sep-2013MTH 1 m 0 d

5961.8HRS

5486LDG

350004 HYDROSTATIC TEST OXYGEN CYLINDER

89520077

C06110084

051222 : OXY

SMF

30-Apr-20196006-Apr-2014MTH 44 m 0 d

710010 OVERHAUL

E1

23-Jul-1999MTH

(7086)701435003514HRS 674.9

710010 OVERHAUL

E2

23-Jul-1999MTH

(7086)701435003514HRS 674.9

710020 HOT SECTION INSPECTION

E1

SMF

19-Jul-2009MTH

(7180)710818005308HRS 768.9

710020 HOT SECTION INSPECTION

E2

SMF

19-Jul-2009MTH

(7180)710818005308HRS 768.9

710030 WASH ENGINE

E1

A/R09-Apr-1991DAYS

710030 WASH ENGINE

E2

A/R09-Apr-1991DAYS

720010 OIL ANALYSIS

E1

A/R09-Apr-1991MTH

720010 OIL ANALYSIS

E2

A/R09-Apr-1991MTH

731025 VISUALLY INSPECT FUEL-OIL COOLER

11438-001J

551

E1

SMF

11-Apr-2014MTH

(9512.2)9543.935006043.9HRS 3204.8

5528LDG

731025 VISUALLY INSPECT FUEL-OIL COOLER

11438-001J

513

E2

SMF

11-Apr-2014MTH

(9512.2)9543.935006043.9HRS 3204.8

5528LDG

731035 VISUALLY INSPECT MOTIVE FLOW VALVE

PN

SN-UNKNOWN

E1

09-Apr-1991MTH

(7086)7117.7350031.7HRS 778.6

731035 VISUALLY INSPECT MOTIVE FLOW VALVE

PN

SN-UNKNOWN

E2

09-Apr-1991MTH

(7086)7117.7350031.7HRS 778.6

731060 VISUAL INSPECT BLEED VALVE ACTUATOR

PN

SN-UNKNOWN

E1

SMF

31-Jan-20172429-Jan-2015MTH 17 m 0 d

(6415.4)6447.13006147.1HRS 108

5586LDG

731060 VISUAL INSPECT BLEED VALVE ACTUATOR

PN

SN-UNKNOWN

E2

SMF

31-Jan-20172429-Jan-2015MTH 17 m 0 d

(6415.4)6447.13006147.1HRS 108

5586LDG

731090 VISUALLY INSPECT FLOW DIVIDER VALVE

26395-2

259

E1

09-Apr-1991MTH

(7086)7117.7350031.7HRS 778.6

731090 VISUALLY INSPECT FLOW DIVIDER VALVE

26395-2

403

E2

09-Apr-1991MTH

(7086)7117.7350031.7HRS 778.6




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains


Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

732050 VISUAL INSPECT ELECTRONIC BLEED VALVE CONTROL

PN

SN-UNKNOWN

E1

SMF

31-Jan-20172429-Jan-2015MTH 17 m 0 d

(6415.4)6447.13006147.1HRS 108

5586LDG

732050 VISUAL INSPECT ELECTRONIC BLEED VALVE CONTROL

PN

SN-UNKNOWN

E2

SMF

31-Jan-20172429-Jan-2015MTH 17 m 0 d

(6415.4)6447.13006147.1HRS 108

5586LDG

732060 VISUAL INSPECT MAIN WIRING HARNESS

PN

SN-UNKNOWN

E1

SMF

31-Jan-20172429-Jan-2015MTH 17 m 0 d

(6415.4)6447.13006147.1HRS 108

5586LDG

732060 VISUAL INSPECT MAIN WIRING HARNESS

PN

SN-UNKNOWN

E2

SMF

31-Jan-20172429-Jan-2015MTH 17 m 0 d

(6415.4)6447.13006147.1HRS 108

5586LDG

741030 VISUAL INSPECT IGNITION EXCITER

NB01201

R5948

E1 INBOARD

SMF

31-Jan-20172429-Jan-2015MTH 17 m 0 d

(6415.4)6447.13006147.1HRS 108

5586LDG


NB01201

R5958

E1 OUTBOARD

SMF

31-Jan-20172429-Jan-2015MTH 17 m 0 d

(6415.4)6447.13006147.1HRS 108

5586LDG


305013

682

E2 INBOARD

SMF

31-Jan-20172429-Jan-2015MTH 17 m 0 d

(6415.4)6447.13006147.1HRS 108

5586LDG


CH92028

01030791

E2 OUTBOARD

SMF

31-Jan-20172429-Jan-2015MTH 17 m 0 d

(6415.4)6447.13006147.1HRS 108

5586LDG

792010 CHANGE OIL

E1

SMF

O/C09-Jul-2010MTH

5437.2HRS

5216LDG

792010 CHANGE OIL

E2

SMF

O/C09-Jul-2010MTH

5437.2HRS

5216LDG




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015

Part Number

Part Serial No



Remains

RemainsTSO 2

TSO 1

Components

(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

211002 EMERGENCY PRESSURE VALVE

27441482-06

10AF76

*CF

O/C09-Apr-1991MTH

211004 S243 PRIMARY PRESSURE SWITCH

1103P240-1

1536

SMF

O/C07-Jun-2007MTH

04969HRS

211005 S244 SECONDARY PRESSURE SWITCH

1103P240-2

SN-UNKNOWN

*CF

O/C09-Apr-1991MTH

211006 THERMAL ACTUATOR ASSEMBLY

56CD1660-9-8/13

SN-UNKNOWN

LGB

O/C01-Dec-1996MTH

02692HRS

212001 INSTRUMENT PANEL FAN

4124X

SN-UNKNOWN

*CF

O/C09-Apr-1991MTH

212002 AVIONICS BAY COOLING BOX FAN

032105

SN-UNKNOWN

*CF

O/C09-Apr-1991MTH

212004 OVERHEAD CABIN FAN

BC61A901-2

1390A

9912323-2 SMF

14-Jun-2014MTH

7078.3010006078.3HRS 739.2

5548LDG

212006 COCKPIT DEFOGGER FAN

5703-4

241

SMF

06-Jul-1997MTH

8886.72035002844HRS 2547.62

212009 FLOW DIVIDER CABIN UNDERFLOOR ACTUATOR

NYLC50466

951

*CF

O/C09-Apr-1991MTH

212010 AVIONICS BAY VANE AXIAL BLOWER

19A827

SN-UNKNOWN

*CF

O/C09-Apr-1991MTH

212011 TEMP DUCT SENSOR

27221274

SN-UNKNOWN

9912085-3 *CF

O/C09-Apr-1991MTH

213001 CABIN PRESSURE INDICATOR

C668511-0103

19209

3001J50 *CF

O/C09-Apr-1991MTH

213003 RATE OF CHANGE INDICATOR

C668513-0101

W27144H

35060-1128 *CF

O/C09-Apr-1991MTH

213006 CABIN ALTITUDE CONTROLLER

130620-2

12A0002

LGB

O/C27-Jan-1996MTH

02409HRS

213007 PRIMARY OUTFLOW VALVE

103648-14

119323

NO. 1

*CF

O/C09-Apr-1991MTH

213007 SECONDARY OUTFLOW VALVE

103648-14

119298

NO. 2

*CF

O/C09-Apr-1991MTH

213009 FLOW CONTROL PRESSURE REGULATOR VALVE

34E16-4

9900255

NO. 1 9912162-1 *CF

O/C09-Apr-1991MTH

213009 FLOW CONTROL PRESSURE REGULATOR VALVE

34E16-4

7900290

NO. 2 9912162-1 *CF

O/C09-Apr-1991MTH

213013 PNEUMATIC RELAY

130358-1

501793

*CF

O/C09-Apr-1991MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

215001 ACM REFRIGERATOR PACKAGE ASSEMBLY

782343-2

900720

9912069-26 *CF

O/C09-Apr-1991MTH

215004 AIR CYCLE MACHINE

738384-26

9906214

SMF

07-Jun-2007MTH

9969050004969HRS 3629.9

RECOMMENDED ECONOMIC OVERHAUL PERIOD DEFINED BY HAMILTON STANDARD.

215005 ACM BYPASS VALVE

754751-2

85102495

PIT

O/C24-Jan-2000MTH

03695HRS

215007 COMPRESSION ACTUATOR

BYLB50907

SN-UNKNOWN

9912294-1 *CF

O/C09-Apr-1991MTH

215008 DUCT OVERHEAT SENSOR

1173T42-1

SN-UNKNOWN

*CF

O/C09-Apr-1991MTH

215009 ACM OVERHEAT SWITCH

1173T0396

324

TOL

O/C17-Dec-1992MTH

01119HRS

215016 AC COMPRESSOR

1134160

2084

SMF

0O/C19-Mar-2012MTH

05725.6HRS

5363LDG

215017 AC CONDENSER

1250180-7

916

*CF

O/C09-Apr-1991MTH

215021 MOTOR

1250150

444

*CF

O/C09-Apr-1991MTH

215022 AFT EVAPORATOR

1250240-3

379

*CF

O/C09-Apr-1991MTH

215023 FWD EVAPORATOR

1250240-1

373

*CF

O/C09-Apr-1991MTH

215024 PRESSURE SWITCH

1250232-4

10742

SMF

O/C11-Apr-2014MTH

6043.9HRS

5528LDG

215026 FREON A/C-HOBBS METER

1250703-3

NSN

SMF

0O/C11-Apr-2014MTH

06043.9HRS

05528LDG

216001 CABIN TEMPERATURE SENSOR

1942T100-3

174A

TOL

O/C25-Feb-1993MTH

01203HRS

216002 CABIN TEMPERATURE CONTROLLER

754661-5

97064929

9912069-22 SAC

O/C28-Jun-2004MTH

04560HRS

216003 DUCT TEMPERATURE SENSOR

754691-3

N0032

9912069-14 SMF

O/C07-Jun-2007MTH

04969HRS

216005 CENTRIFUGAL BLOWER

3A1003-10

SN-UNKNOWN

*CF

O/C09-Apr-1991MTH

216010 DOOR ACTUATOR MOTOR ASSEMBLY

5A3032

SN-UNKNOWN

9910059-3 *CF

O/C09-Apr-1991MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

217001 WATER SEPARATOR

738386-3

900718

9912069-13 *CF

O/C09-Apr-1991MTH

221001 ROLL RATE MONITOR

4015901-920

89121729

NO. 1 RZ-220 *CF

O/C09-Apr-1991MTH

221001 ROLL RATE MONITOR

4015901-920

91011824

NO. 2 RZ-220 *CF

O/C09-Apr-1991MTH

221008 AUTOPILOT COMPUTER

4008519-952

90064435

SP-200 *CF

O/C09-Apr-1991MTH

221009 AUTOPILOT CONTROL

4018639-933

90103366

PC-500 *CF

O/C09-Apr-1991MTH

221010 SERVO

4006719-906

90105129

AILERON SM-200 *CF

O/C09-Apr-1991MTH

221010 SERVO

4006719-914

80126454

ELEVATOR SM-200 TOL

O/C05-Jun-1998MTH

4123159HRS

221010 SERVO

4006719-906

90105138

RUDDER SM-200 *CF

O/C09-Apr-1991MTH

221011 SERVO-BRACKET --

4005842

04016890

ELEVATOR

SMF

O/C06-Feb-2009MTH

05261HRS

232001 VHF COMM ANTENNA

VF10-347

3967

NO. 3

0O/C23-May-2012MTH

05743.2HRS

05371LDG


VF10-108-1

1803

NO. 2 9912084-1 *CF

O/C09-Apr-1991MTH


VFS10-90-5

2558

NO. 1

*CF

O/C09-Apr-1991MTH

232004 TRANSCEIVER PHONE

724855-801

940

PIT

O/C21-Jan-1999MTH

03391HRS

232005 HANDSET PHONE

725729-815

GH51445

CABIN

LNK

O/C17-Jul-1996MTH

02553HRS

232006 HANDSET PHONE

725729-815

MX22419

COCKPIT

LNK

O/C17-Jul-1996MTH

02553HRS

232008 VHF INTEGRATED CONTROL UNIT

7510700-901

900905501

NO. 1 RCZ-850 KALN

O/C23-May-2012MTH

5743.2HRS

5371LDG

232008 VHF INTEGRATED CONTROL UNIT

7510700-901

90010436

NO. 2 RCZ-850 KALN

O/C23-May-2012MTH

5743.2HRS

5371LDG

232010 VHF COMMUNICATION TRANSCEIVER

7510764-901

89110421

NO. 1 TR-850 TOL

O/C30-Sep-1992MTH

0983HRS

232010 VHF COMMUNICATION TRANSCEIVER

7510764-901

SN-UNKNOWN

NO. 2 TR-850 LBE

O/C18-Apr-1991MTH

029HRS




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

232013 COMM CLUSTER MODULE

7510784-901

89120443

NO. 1 XC-850 TOL

O/C30-Sep-1992MTH

0983HRS

232013 COMM CLUSTER MODULE

7510784-901

SN-UNKNOWN

NO. 2 XC-850 LBE

O/C18-Apr-1991MTH

029HRS

232018 CDBR REPEATER

724864-801

1285

LNK

O/C17-Jul-1996MTH

02553HRS

232019 MAGNASTAR DUPLEXER

620317-1

ZM048

LNK

O/C17-Jul-1996MTH

02553HRS

232020 CABIN ALERTER SWITCH

725256-801

MSL0507

LNK

O/C17-Jul-1996MTH

02553HRS

235001 AUDIO AMPLIFIER

7511001-915

90090298

NO. 1 AV-850A TOL

O/C06-Nov-1992MTH

01057HRS

235001 AUDIO AMPLIFIER

7511001-915

90090301

NO. 2 AV-850A TOL

O/C06-Nov-1992MTH

01057HRS

237001 COCKPIT VOICE RECORDER

GA100-0000

1179

GA-100 SMF

O/C09-Feb-2007MTH

44454922HRS

237006 CVR UNDERWATER LOCATOR BEACON

DK100

SC48989

SMF

31-Oct-201597209-Jul-2010MTH 2 m 0 d

5437.2HRS

5216LDG

242001 STATIC INVERTER

SPC38B

2018

NO. 1

ICT

O/C21-May-2008MTH

9575163HRS

242001 STATIC INVERTER

SPC38B

2234

NO. 2

ICT

O/C21-May-2008MTH

32105163HRS

243001 STARTER/GENERATOR

23085-004-1

96112

LEFT 9912125-3 SMF

04-Mar-2011MTH

6568.6010005568.6HRS 229.5

5282LDG

243001 STARTER/GENERATOR

23085-004-1

94100

RIGHT 9912125-3 SMF

04-Mar-2011MTH

6568.6010005568.6HRS 229.5

5282LDG

243003 GENERATOR CONTROL UNIT

51539-006F

2457AB

NO. 1 9912039-6 MCC

O/C04-Mar-2005MTH

04661HRS

243003 GENERATOR CONTROL UNIT

51539-006F

8364AB

NO. 2 9912039-6 *CF

O/C09-Apr-1991MTH

243004 AMMETER

C662501-0104

528

NO. 1

*CF

O/C09-Apr-1991MTH

243004 AMMETER

C662501-0104

532

NO. 2

*CF

O/C09-Apr-1991MTH

243005 DC VOLTMETER

C662502-0101

1739

*CF

O/C09-Apr-1991MTH

243007 MAIN SHIP BATTERY

30978-002

11402005

9914058-6 / ATSP-44 SMF

0O/C09-Oct-2014MTH

06147.1HRS

5586LDG




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

243008 BATTERY TEMP MONITOR

1529-1

1913

*CF

O/C09-Apr-1991MTH

243009 BATTERY TEMP GAGE

1229-1

1635

*CF

O/C09-Apr-1991MTH

243010 BATTERY TEMP SENSOR

1166-1

SN-UNKNOWN

*CF

O/C09-Apr-1991MTH

243011 CURRENT/VOLTAGE CONTROLLER

1301-1

447A

TOL

O/C06-Jul-1997MTH

02844HRS

243015 BATTERY DISCONNECT RELAY

A876K

CJ82764

TOL

O/C06-Nov-1992MTH

01057HRS

243016 CURRENT/VOLTAGE SENSOR

1302-1

378

LGB

O/C28-Aug-1995MTH

02247HRS

245002 CABIN ALTITUDE SWITCH

GB300NA161

8940892

9910095-6 *CF

O/C09-Apr-1991MTH

256002 EMERGENCY LOCATOR TRANSMITTER

3000-1

321459

*CF

O/C09-Apr-1991MTH

256003 EMERGENCY LOCATOR TRANSMITTER BEACON BATTERY

2020

-NSN-

2020BATTERY SMF

30-Sep-201602409-Oct-2014MTH 13 m 0 d

6147.1HRS

5586LDG

Expiration Date: 30-Sep-2016

256004 ELT ANTENNA

ELT10-177-1

920

NO. 1

*CF

O/C09-Apr-1991MTH

256004 ELT ANTENNA

ELT10-177-2

590

NO. 2

*CF

O/C09-Apr-1991MTH

261001 FIRE DETECTOR SENSOR

244-18882

SN-UNKNOWN

NO. 1 ENGINE 9912036-3 *CF

O/C09-Apr-1991MTH

261001 FIRE DETECTOR SENSOR

244-18882

SN-UNKNOWN

NO. 2 ENGINE 9912036-3 *CF

O/C09-Apr-1991MTH

261002 FIRE DETECTOR CONTROL

377-02808

9035013

NO. 1 9912036-2 *CF

O/C09-Apr-1991MTH

261002 FIRE DETECTOR CONTROL

377-02808

9035007

NO. 2 9912036-2 *CF

O/C09-Apr-1991MTH

262001 ENGINE FIRE BOTTLE

898066-2

92793EK

AFT 9912048-3 *CF

0O/C09-Apr-1991MTH

262001 ENGINE FIRE BOTTLE

898066-2

92770EK

FORWARD 9912048-3 *CF

0O/C09-Apr-1991MTH

262002 PORTABLE HALON FIRE EXTINGUISHER

GH2-1/2J

V461840

CABIN

SMF

118O/C25-Jun-2001MTH

3926HRS




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

262002 PORTABLE HALON FIRE EXTINGUISHER

GH2-1/2J

V467489

COCKPIT

SMF

118O/C25-Jun-2001MTH

3926HRS

262003 (MAX LIFE) CARTRIDGE

873364-1

051474

AFT LEFT

SMF

30-Sep-201712009-Jul-2010MTH 25 m 0 d

5437.2HRS

5216LDG

Manufacture Date: 30-Sep-2007


873364-1

041409

AFT RIGHT

SMF

30-Jun-201712009-Jul-2010MTH 22 m 0 d

5437.2HRS

5216LDG

Manufacture Date: 30-Jun-2007


873364-1

021632

FORWARD LEFT

SMF

31-Aug-201812009-Jul-2010MTH 36 m 0 d

5437.2HRS

5216LDG

Manufacture Date: 31-Aug-2008


873364-1

051485

FORWARD RIGHT

SMF

30-Sep-201712009-Jul-2010MTH 25 m 0 d

5437.2HRS

5216LDG

Manufacture Date: 30-Sep-2007

271001 AILERON TRIM ACTUATOR

5565450-72

SN-UNKNOWN

*CF

O/C09-Apr-1991MTH

272001 RUDDER TRIM ACTUATOR

5565450-71

SN-UNKNOWN

*CF

O/C09-Apr-1991MTH

273002 TRIM MIXER ACTUATOR

1U662-001

T361

SMF

O/C11-Apr-2014MTH

6043.9HRS

5528LDG

273003 ELEVATOR TRIM ACTUATOR

5565450-81

SN-UNKNOWN

LEFT

O/C07-Nov-1997MTH

02948HRS

273003 ELEVATOR TRIM ACTUATOR

5565450-82

SN-UNKNOWN

RIGHT

*CF

O/C09-Apr-1991MTH

275001 FLAP CONTROL VALVE

66720

654

*CF

O/C09-Apr-1991MTH

275003 FLAP ACTUATOR

1535000-3

2748

NO. 1 9912007-2 SMF

O/C06-Feb-2009MTH

05261HRS

275003 FLAP ACTUATOR

55800-1

681

NO. 2 9912007-1 *CF

O/C09-Apr-1991MTH

275004 AFT FLAP ROLLER

CC50380

NSN

LEFT WING LEFT

INBOARD

SMF

25-Jun-2008MTH

5180HRS

10051050005051LDG 4338


CC50380

NSN

LEFT WING LEFT

OUTBOARD

SMF

25-Jun-2008MTH

5180HRS

10051050005051LDG 4338


CC50380

-NSN-

LEFT WING RIGHT

INBOARD

SMF

17-Nov-2005MTH

4766HRS

9735050004735LDG 4022


CC50380

-NSN-

LEFT WING RIGHT

OUTBOARD

SMF

17-Nov-2005MTH

4766HRS

9735050004735LDG 4022




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -


CC50380

NSN

RIGHT WING LEFT

INBOARD

SMF

25-Jun-2008MTH

5180HRS

10051050005051LDG 4338


CC50380

NSN

RIGHT WING LEFT

OUTBOARD

SMF

25-Jun-2008MTH

5180HRS

10051050005051LDG 4338


CC50380

NSN

RIGHT WING RIGHT

INBOARD

SMF

25-Jun-2008MTH

5180HRS

10051050005051LDG 4338


CC50380

NSN

RIGHT WING RIGHT

OUTBOARD

SMF

25-Jun-2008MTH

5180HRS

10051050005051LDG 4338

276001 SPEED BRAKE ACTUATOR

55850-1

297

NO. 1 9912344-1 *CF

O/C09-Apr-1991MTH

276001 SPEED BRAKE ACTUATOR

55850-1

286

NO. 2 9912344-1 *CF

O/C09-Apr-1991MTH

276002 SPEED BRAKE FLAP CONTROL VALVE

66720

687

*CF

O/C09-Apr-1991MTH

276003 SAFETY SPDBK VALVE

68930

169

*CF

O/C09-Apr-1991MTH

282001 ELECTRIC FUEL BOOST PUMP

1C7-12

8AF122

NO. 1 9912017-2 *CF

O/C09-Apr-1991MTH

282001 ELECTRIC FUEL BOOST PUMP

1C7-12

8AF119

NO. 2 9912017-2 *CF

O/C09-Apr-1991MTH

282002 MOTOR ACTUATOR VALVE

AV24B1325C

N77639

NO. 1

*CF

O/C09-Apr-1991MTH

282002 MOTOR ACTUATOR VALVE

AV24B1325C

N77625

NO. 2

*CF

O/C09-Apr-1991MTH

282010 MOTIVE FUEL VALVE

3244850

B28224

LEFT

PIT

O/C23-Jul-1999MTH

03514HRS

282010 MOTIVE FUEL VALVE

3244850

B28191

RIGHT

PIT

O/C23-Jul-1999MTH

03514HRS

284001 FUEL LOW LEVEL SWITCH

L15H-3

SN-UNKNOWN

NO. 1

*CF

O/C09-Apr-1991MTH

284001 FUEL LOW LEVEL SWITCH

L15H-3

7141

NO. 2

SMF

O/C06-Feb-2009MTH

05261HRS

284002 FUEL QTY COMPENSATOR

300047-13001

16460T

LEFT 9912019-4 SMF

O/C19-Jul-2013MTH

5941HRS

5476LDG

284002 FUEL QTY COMPENSATOR

300047-13001

16235T

RIGHT 9912019-4 SMF

O/C19-Jul-2013MTH

5941HRS

5476LDG

284007 FUEL QTY INDICATOR

VSDL-OC403F-1

273X

9912147-26 TOL

O/C14-Mar-1999MTH

34303430HRS




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

291001 MAIN HYD RESERVOIR

40500-7

1

9912052-12 TOL

O/C09-Jan-1998MTH

02999HRS

291002 HYDRAULIC PUMP

24195-LAA

3751

LEFT 9912062-4 MHR

O/C15-Apr-2002MTH

04056HRS

291002 HYDRAULIC PUMP

24195-LAA

1642

RIGHT 9912062-4 VNY

O/C13-Feb-1996MTH

02430HRS

291005 CK VALVE HYDRAULIC FLOW SWITCH

3520020100-4

2924

NO. 1 9912194-3 *CF

O/C09-Apr-1991MTH

291005 CK VALVE HYDRAULIC FLOW SWITCH

3520020100-4

2681

NO. 2 9912194-3 *CF

O/C09-Apr-1991MTH

291008 THERMAL RELIEF VALVE

20900-1

1435

*CF

O/C09-Apr-1991MTH

291009 PRESSURE RELIEF VALVE

4614

207A

TOL

O/C26-Oct-1999MTH

03608HRS

291012 SOLENOID BYPASS VALVE

61510-1

847A

*CF

O/C09-Apr-1991MTH

301001 TEMP CONTROL SL002 SWITCH

1173T42-3

SN-UNKNOWN

LEFT

*CF

O/C09-Apr-1991MTH

301001 OUTBRD WING DEICE BOOT

P35-5D5230-01

NAF3740

NO. 1

KALN

0O/C23-May-2012MTH

05743.2HRS

5371LDG

SL560-57-01 IS MANDATORY AND NEEDS TO BE INCORPORATED WHEN DE-ICE BOOTS ARE REMOVED.

301001 OUTBRD WING DEICE BOOT

P35-5D5230-02

NAC4210

NO. 2

KALN

0O/C23-May-2012MTH

05743.2HRS

5371LDG

SL560-57-01 IS MANDATORY AND NEEDS TO BE INCORPORATED WHEN DE-ICE BOOTS ARE REMOVED.

301001 TEMP CONTROL SR002 SWITCH

1173T42-3

SN-UNKNOWN

RIGHT

*CF

O/C09-Apr-1991MTH

301001 ANTI-ICE BLEED AIR CROSSFLOW ISOLATION VALVE

320495

SN-UNKNOWN

WING 9914121-1 *CF

O/C09-Apr-1991MTH

301002 HORIZONTAL STABILIZER DEICE BOOT

P29S-5D5225-05

NCJ6440

NO. 1

SMF

0O/C22-May-2015MTH

06283.9HRS

05674LDG

301002 HORIZONTAL STABILIZER DEICE BOOT

29S-5D5225-04

M493270

NO. 2

LNK

O/C19-Jul-1996MTH

02553HRS

301003 SURFACE DEICE TIMER

878

41

*CF

O/C09-Apr-1991MTH

301004 ANTI-ICE BLEED AIR PRESSURE REG SHUTOFF VT001 VLV

67410-2

2469

LEFT WING 9912086-4 TOL G

O/C06-Jul-1997MTH

02844HRS

301004 ANTI-ICE BLEED AIR PRESSURE REG SHUTOFF VT002 VLV

67410-2

1340

RIGHT WING 9912086-4 *CF

O/C09-Apr-1991MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

301007 RAM AIR MODULATING TEMP CONTROL VLV

27441500-01

10AF85

LEFT 9912362-1 *CF

O/C09-Apr-1991MTH

301007 RAM AIR MODULATING TEMP CONTROL VLV

27441500-01

10AF83

RIGHT 9912362-1 *CF

O/C09-Apr-1991MTH

301008 DEICE CONTROL SLV19 VLV

3D2353-06

SN-UNKNOWN

LEFT

*CF

O/C09-Apr-1991MTH

301008 DEICE CONTROL SLV18 VLV

3D2353-06

N084687

RIGHT

SMF

0O/C04-Mar-2011MTH

05568.6HRS

5282LDG

301009 TEMP CONTROL S95 SENSOR

27431501-04

4AH64

LEFT 9912362-3 TOL

O/C29-May-1992MTH

0759HRS

301009 TEMP CONTROL S94 SENSOR

27431501-04

4AH56

RIGHT 9912362-3 TOL

O/C29-May-1992MTH

0759HRS

302003 ANTI-ICE SOLENOID VLV

67410-1

1573AE

LEFT ENGINE 9912086-7 LGB

O/C06-Apr-1994MTH

01794HRS

302003 ANTI-ICE SOLENOID VLV

67410-1

811

RIGHT ENGINE 9912086-7 PIT G

O/C22-Sep-1999MTH

03575HRS

302004 INLET TEMPERATURE S95 SWITCH

M1002-505

000154

LEFT ENGINE

SMF

0O/C19-Mar-2012MTH

05725.6HRS

5363LDG

302004 INLET TEMPERATURE S94 SWITCH

21548-2-19-6

SN-UNKNOWN

RIGHT ENGINE

*CF

O/C09-Apr-1991MTH

302005 ANTI ICING VALVE

10018200C

454

LEFT 3033057 SMF

O/C22-May-2015MTH

2769.96283.9HRS

5674LDG

302005 ANTI ICING VALVE

10018200C

486

RIGHT 3033057 SMF

O/C22-May-2015MTH

2769.96283.9HRS

5674LDG

302006 BLEED VALVE ACTUATOR

800888-1

F20552

LEFT 3037074 PIT

O/C23-Jul-1999MTH

03514HRS


800888-1

F16153

RIGHT 3037074 PIT

O/C23-Jul-1999MTH

03514HRS

303001 PITOT TUBE

PH502

SN-UNKNOWN

LEFT

*CF

O/C09-Apr-1991MTH

303001 PITOT TUBE

PH502

SN-UNKNOWN

RIGHT

*CF

O/C09-Apr-1991MTH

304001 BLEED AIR MONITOR

1169-1

1379

*CF

O/C09-Apr-1991MTH

304002 ANTI-ICE BLEED AIR WNDSHLD HEAT EXCHANGER

10663A

527

9912041-4 *CF

O/C09-Apr-1991MTH

304004 ALCOHOL WINDSHIELD ANTI-ICE PUMP

476411

SN-UNKNOWN

*CF

O/C09-Apr-1991MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

304005 TEMP CONTROL VALVE

27241287

8AF94

9912085-1 *CF

O/C09-Apr-1991MTH

304006 ANTI-ICE BLEED AIR WNDSHLD TEMP XMTR26 SENSOR

27231272-10

8AF80

9912085-2 *CF

O/C09-Apr-1991MTH

304007 ANTI-ICE BLEED AIR WNDSHLD HEAT EXCHANGER PRESS S130 SWITCH

1115P25

SN-UNKNOWN

*CF O/C09-Apr-1991MTH

304009 WINDSHIELD ANTI-ICE BLEED AIR CONTROL VALVE

67410-2

3693

9912086-4 SMF

O/C06-Feb-2009MTH

05261HRS

312001 DIGITAL CLOCK

M877A5V

3358

COPILOT

*CF

O/C09-Apr-1991MTH

312001 DIGITAL CLOCK

M877A5V

3370

PILOT

*CF

O/C09-Apr-1991MTH

313001 FLIGHT HOUR RECORDER

C664503-0104

NSN

85071 ICT

O/C16-Sep-2008MTH

05233HRS

313003 ACCELEROMETER

7000992

5993

NO. 1 AG-222 *CF

O/C09-Apr-1991MTH

313003 ACCELEROMETER

7000992

6058

NO. 2 AG-222 *CF

O/C09-Apr-1991MTH

315001 MASTER WARNING ANNUNCIATOR

465-1-14

269

9912119-14 *CF

O/C09-Apr-1991MTH

321001 MAIN LANDING GEAR ASSEMBLY

6641000-15

25

LEFT

*CF

09-Apr-1991MTH

124500124500LDG 6737

321002 MAIN LANDING GEAR ASSEMBLY

6641000-16

25

RIGHT

*CF

09-Apr-1991MTH

124500124500LDG 6737

321003 TORQUE LINK BOLT

5541220-2

SN-UNKNOWN

LEFT MAIN LANDING

GEAR

*CF

09-Apr-1991MTH

103700103700LDG 4657

321003 TORQUE LINK BOLT

5541220-2

SN-UNKNOWN

RIGHT MAIN LANDING

GEAR

*CF

09-Apr-1991MTH

103700103700LDG 4657

322001 NOSE LANDING GEAR ASSEMBLY

6642000-10

8

*CF

09-Apr-1991MTH

235000235000LDG 17787

322002 NOSE SHIMMY DAMPER

5543001-8

3878

PIT

O/C15-Nov-1999MTH

3629HRS

03890LDG

322004 NOSE GEAR FORK/PISTON

6642000-3

SN-UNKNOWN

SMF

19-Mar-2012MTH

5725.65725.6HRS

136405363136405363LDG 7927

323001 MAIN LANDING GEAR ACTUATOR

1523100-3

194

LEFT 9912111-1 *CF

09-Apr-1991MTH

150000150000LDG 9287

323002 MAIN LANDING GEAR ACTUATOR

1523100-4

203B

RIGHT 9912111-2 TOL

30-Jun-1999MTH

3497HRS

153603365150003725LDG 9647




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

323003 NOSE LANDING GEAR ACTUATOR

1523200-9

1773

9912120-4 SMF

06-Feb-2009MTH

5261HRS

201110150005111LDG 14398

323004 MLG UPLOCK ACTUATOR

5527504-2

WMP1117

LEFT

TOL

O/C25-Feb-1993MTH

1203HRS

01309LDG

323004 UPLOCK ACTUATOR

5527504-2

772

NOSE

*CF

O/C09-Apr-1991MTH

323004 MLG UPLOCK ACTUATOR

5527504-2

1567

RIGHT

LGB

O/C28-Aug-1995MTH

2247HRS

02402LDG

323006 PNEUMATIC BLOWDOWN/EMERGENCY BRAKE BOTTLE

212940-2

8392

9912103-3 SMF

31-Jan-203928829-Jan-2015MTH 281 m 0 d

6147.1HRS

5586LDG

Manufacture Date: 27-Jan-2015

323007 LANDING GEAR CONTROL VALVE

66710

358

*CF

O/C09-Apr-1991MTH

323008 DUMP VALVE

AS19400-1

1632

*CF

O/C09-Apr-1991MTH

323019 EMERGENCY AIR BOTTLE GAUGE

2341128

20550D

*CF

0O/C09-Apr-1991MTH

324001 MLG WHEEL ASSEMBLY

3-1490-1

1677

LEFT 9912222-11 SMF

O/C22-May-2015MTH

6283.9HRS

27965674LDG

324001 MLG WHEEL ASSEMBLY

3-1490-1

1488/3066

RIGHT 9912222-11 SMF

O/C22-May-2015MTH

6283.9HRS

5674LDG

324002 NOSE WHEEL ASSEMBLY

3-1418

6630

9914069-2 SMF

O/C22-May-2015MTH

6283.9HRS

5674LDG

324003 MLG BRAKE ASSEMBLY

2-1529-7

1217

LEFT 9912222-17 SMF

O/C23-Jul-2007MTH

4984HRS

04910LDG

324004 MLG BRAKE ASSEMBLY

2-1529-7

3268

RIGHT 9912222-17 SMF

O/C23-Jul-2007MTH

4984HRS

04910LDG

324005 MLG TIRE

220K28-1

41132985

LEFT

SMF

0O/C22-May-2015MTH

06283.9HRS

05674LDG

324005 MLG TIRE

220K28-1

42843029

RIGHT

SMF

0O/C22-May-2015MTH

06283.9HRS

05674LDG

324006 NOSE TIRE

031-613-8

4343S00457

9914070-1 SMF

0O/C22-May-2015MTH

06283.9HRS

05674LDG

324010 MLG SHUTTLE VALVE

195-183

328R

LEFT

*CF

O/C09-Apr-1991MTH

324010 MLG SHUTTLE VALVE

195-183

413R

RIGHT

*CF

O/C09-Apr-1991MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

324011 MLG INBOARD BRAKE MASTER CYLINDER

95367-9

345

LEFT 9912050-11 *CF

O/C09-Apr-1991MTH

324011 MLG INBOARD BRAKE MASTER CYLINDER

95367-9

359

RIGHT 9912050-11 *CF

O/C09-Apr-1991MTH

324012 MLG OUTBOARD MASTER BRAKE CYLINDER

95367-10

338

LEFT 9912050-12 *CF

O/C09-Apr-1991MTH

324012 MLG OUTBOARD MASTER BRAKE CYLINDER

95367-10

363

RIGHT 9912050-12 *CF

O/C09-Apr-1991MTH

324014 EMERGENCY AIR BRAKE VALVE

895232-0875

V1232

SMF

O/C06-Feb-2009MTH

05261HRS

324019 BRAKE PRESS PUMP ASSEMBLY

634343

202242

9912166-2 *CF

O/C09-Apr-1991MTH

324021 POWER BRAKE ANTISKID VALVE

38-707-1

564

9912305-7 *CF

O/C09-Apr-1991MTH

324022 BRAKE CONTROL BOX

42-707-1

232A

9912305-6 TOL

O/C06-Jul-1997MTH

02844HRS

324023 ANTISKID ACCUMULATOR

57C57652

RH0499

*CF

O/C09-Apr-1991MTH

324024 MLG WHEEL TRANSDUCER

40-955

2394

LEFT 9912305-2 *CF

O/C09-Apr-1991MTH

324024 MLG WHEEL TRANSDUCER

40-955

2384

RIGHT 9912305-2 *CF

O/C09-Apr-1991MTH

324025 PRESSURE SWITCH

1206P25

3463

9912163-1 SMF

0O/C03-Mar-2013MTH

05873.7HRS

5439LDG

324026 POWER BRAKE ASSEMBLY MOTOR

30-2

2022

*CF

O/C09-Apr-1991MTH

324101 PARKING BRAKE VALVE

20800-6

1448

9914263-1 *CF

O/C09-Apr-1991MTH

325001 NOSE STEERING BUNGEE ASSEMBLY

5565624-19

SN-UNKNOWN

*CF

O/C09-Apr-1991MTH

326003 MAIN GEAR DOWN & LOCK SWITCH

1EN118-6

SN-UNKNOWN

LEFT

TOL

O/C03-Sep-1993MTH

1503HRS

01634LDG

326003 MAIN GEAR DOWN & LOCK SWITCH

1EN118-6

SN-UNKNOWN

RIGHT

TOL

O/C03-Sep-1993MTH

1503HRS

01634LDG

326003 NOSE GEAR DOWN & LOCK SWITCH

1EN118-6

SN-UNKNOWN

TOL

O/C03-Sep-1993MTH

1503HRS

01634LDG

326005 MAIN GEAR UP & LOCKED SWITCH

65-430087

SN-UNKNOWN

LEFT

*CF

O/C09-Apr-1991MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

326005 MAIN GEAR UP & LOCKED SWITCH

65-430087

SN-UNKNOWN

RIGHT

*CF

O/C09-Apr-1991MTH

326005 NOSE GEAR UP & LOCKED SWITCH

65-430087

SN-UNKNOWN

*CF

O/C09-Apr-1991MTH

331001 LIGHT PANEL DIMMER

1821-1

1453

NO. 1

*CF

O/C09-Apr-1991MTH


1821-1

1391

NO. 2

*CF

O/C09-Apr-1991MTH


1821-1

1434

NO. 3

*CF

O/C09-Apr-1991MTH

331011 INVT-115V EL PANEL

EM2044-1

1354

*CF

O/C09-Apr-1991MTH

332002 INDIRECT LIGHTING INVERTER

18.996

6516

AFT

*CF

O/C09-Apr-1991MTH

332002 INDIRECT LIGHTING INVERTER

18.994

2656

FORWARD

TOL

O/C06-Jul-1997MTH

02844HRS

334002 ROTATING/FLASHING BEACON

30-2140-5

2539

SMF

0O/C22-May-2015MTH

06283.9HRS

05674LDG

334003 STROBE POWER SUPPLY

60-2799-1

15587

NO. 1 9910368-2 *CF

O/C09-Apr-1991MTH

334003 STROBE POWER SUPPLY

60-2799-1

15592

NO. 2 9910368-2 *CF

O/C09-Apr-1991MTH

335001 EMERGENCY BATTERY PACK

41B0202BA01301

SN-UNKNOWN

LGB

0O/C10-Sep-1994MTH

1953HRS

341001 AIRSPEED INDICATOR

C661063-0106

W20628

NO. 1 20240-11323 LGB

O/C23-Nov-1994MTH

02030HRS

341001 AIRSPEED INDICATOR

C661063-0106

W27154H

NO. 2 20240-11323 SMF

O/C29-Aug-2007MTH

05018HRS

341005 S262 MACH/AIRSPEED WARNING SWITCH

D2RA45C-27

249

9912076-13 SMF

O/C07-Jun-2007MTH

04969HRS

341006 PITOT PRESSURE SWITCH

D45C31

115

SMF

O/C19-Jul-2009MTH

05308HRS

341008 ADC ALTIMETER

70251N02D04

04111502D

RVSM

SMF

O/C20-Apr-2005MTH

04685HRS

341010 ANGLE OF ATTACK INDICATOR

C11605-1

178

*CF

O/C09-Apr-1991MTH

341011 ANGLE OF ATTACK STALL WARNING COMPUTER

C11606-8

316

TOL

O/C05-Jun-1998MTH

03159HRS




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

341013 ANGLE OF ATTACK TRANSMITTER

1703-15

191

*CF

O/C09-Apr-1991MTH

341015 RADIO ALTIMETER ALT-55B INDICATOR

622-2937-009

2578

PILOT ALI-55 *CF

O/C09-Apr-1991MTH

341019 ALTIMETER

4016341-905

90116311

LEFT BA-141 SMF

O/C19-Jul-2009MTH

05308HRS

341019 ALTIMETER

570-24929-013

3555

STANDBY

SMF

O/C20-Apr-2005MTH

4514685HRS

341020 VNAV CONTROL

7000472-901

04031312

VN-800 SMF

O/C20-Apr-2005MTH

04685HRS

341022 OAT INDICATOR

C668510-0401

296

341025 162BL507D KALN

O/C23-May-2012MTH

5743.2HRS

5371LDG

341035 ANGLE OF ATTACK HEAT MONITOR

1703-147-1

168

*CF

O/C09-Apr-1991MTH

342001 MAGNETIC COMPASS

C660501-0301

NSN

SMF

0O/C22-May-2015MTH

06283.9HRS

05674LDG

342021 VERTICAL SPEED INDICATOR

C661006-0101

W27796H

NO. 1

*CF

O/C09-Apr-1991MTH

342021 VERTICAL SPEED INDICATOR

C661006-0101

W27800H

NO. 2 30260-1117 *CF

O/C09-Apr-1991MTH

342023 RADAR CONTROLLER

7008471-801

90061029

WC-870 *CF

O/C09-Apr-1991MTH

342041 FLIGHT DIRECTOR COMPUTER

4018369-905

91016320

NO. 1 FZ-500 SMF

O/C28-Apr-2005MTH

25284685HRS

342041 FLIGHT DIRECTOR COMPUTER

4018369-905

90106229

NO. 2 FZ-500 SMF

O/C28-Apr-2005MTH

25284685HRS

342042 MODE FLIGHT DIRECTOR SELECTOR

4020570-905

90091891

NO. 1 MS-205 *CF

O/C09-Apr-1991MTH

342042 MODE FLIGHT DIRECTOR SELECTOR

4020570-905

91102059

NO. 2 MS-205 TOL

O/C25-Feb-1993MTH

01203HRS

342043 VERTICAL FLIGHT DIRECTOR GYRO

7000622-901

81093521

NO. 1 VG-14A VNY

O/C23-Aug-1996MTH

1152605HRS

342043 VERTICAL FLIGHT DIRECTOR GYRO

7000622-901

91016765

NO. 2 VG-14A LGB

O/C29-Jan-1996MTH

24092409HRS

342044 RATE OF TURN GYRO

7007453-903

90102580

NO. 1 RG-204 *CF

O/C09-Apr-1991MTH

342044 RATE OF TURN GYRO

7007453-903

93043349

NO. 2 RG-204 LGB

O/C06-Apr-1994MTH

01794HRS




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

342048 AIR DATA COMPUTER

7024900-30302

04060795

NO. 1 AZ-252 SMF

O/C20-Apr-2005MTH

04685HRS

342049 DIRECTIONAL GYRO

4020577-3

85103701

NO. 1 C-14D ICT

O/C21-May-2008MTH

45245163HRS

342049 DIRECTIONAL GYRO

4020577-3

90084691

NO. 2 C-14D ICT

O/C21-May-2008MTH

20015163HRS

342050 FLUX DETECTOR

2594484

80104102

NO. 1 FX-220 SMF

5O/C22-May-2015MTH

06283.9HRS

05674LDG

342050 FLUX DETECTOR

2594484

98042790

NO. 2 FX-220 SMF

1O/C22-May-2015MTH

06283.9HRS

05674LDG

342052 REMOTE COMPENSATOR

2593379-1

90080224

CS-412 *CF

O/C09-Apr-1991MTH

342063 REMOTE COURSE CONTROL

4026206-974

90114353

NO. 1 RI-206S *CF

O/C09-Apr-1991MTH

342064 GYRO POWER SUPPLY

501-1228-03

1639

STANDBY PS-835C SMF

0O/C20-Apr-2005MTH

46854685HRS

342065 STANDBY GYRO

501-1197-05

4146

AI-804 *CF

O/C09-Apr-1991MTH

342066 EFIS DISPLAY

7003430-901

90091932

LEFT BOTTOM ED-600 *CF

O/C09-Apr-1991MTH

342066 EFIS DISPLAY

7003430-901

86040686

LEFT TOP ED-600 LGB

O/C01-Dec-1996MTH

02692HRS

342066 EFIS DISPLAY

7003430-901

93073157

MFD 1 ED-600 MCC

O/C24-Feb-2009MTH

15375262HRS

342066 EFIS DISPLAY

7003430-901

90091940

RIGHT BOTTOM ED-600 SMF

O/C22-May-2015MTH

6283.9HRS

5674LDG

342066 EFIS DISPLAY

7003430-901

91012072

RIGHT TOP ED-600 SMF

O/C22-May-2015MTH

6283.96283.9HRS

56745674LDG

342068 (EFIS) CONTROLLER DISPLAY

7012977-753

90090691

NO. 1 DC-811 *CF

O/C09-Apr-1991MTH

342068 (EFIS) CONTROLLER DISPLAY

7012977-753

91020850

NO. 2 DC-811 *CF

O/C09-Apr-1991MTH

342069 INCLINOMETER

7005400-901

SN-UNKNOWN

NO. 1 AY-03 *CF

O/C09-Apr-1991MTH

342069 MULTIFUNCTION DISPLAY CONTROLLER

7007062-933

90110882

MC-800 *CF

O/C09-Apr-1991MTH

342070 EFIS SYMBOL GENERATOR

7011672-606

90040415

NO. 1 SG-605 LBE

O/C18-Dec-1991MTH

0521HRS




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

342070 EFIS SYMBOL GENERATOR

7011672-606

90120655

NO. 2 SG-605 LBE

O/C09-May-1991MTH

079HRS

342071 MFD SYMBOL GENERATOR

7011673-606

90100264

MG-605 PIT

O/C03-Nov-1998MTH

33433343HRS

342072 STATIC CONVERTER

501-1318-01

3221

*CF

O/C09-Apr-1991MTH

344003 PRIMUS 650 RADAR RECEIVER/TRANSMITTER

7012640-921

97021584

WU-870 SMF

O/C11-Apr-2014MTH

6043.9HRS

5528LDG

344006 LIGHTING ANTENNA

7014062-901

90080204

AT-855 *CF

O/C09-Apr-1991MTH

344007 LIGHTING DETECT PROCESSOR

7011822-903

90060423

LP-850 *CF

O/C09-Apr-1991MTH

344021 RADIO MAGNETIC INDICATOR

622-2506-008

1075

NO. 1 RMI-36 TOL

O/C21-Aug-1991MTH

0293HRS

344021 RADIO MAGNETIC INDICATOR

622-2506-008

7065

NO. 2 RMI-36 *CF

O/C09-Apr-1991MTH

344022 RADIO ALT TRANSCEIVER

622-2855-001

7429

ALT-55B *CF

O/C09-Apr-1991MTH

344023 RECEIVER RADIO ALT ANTENNA

622-0954-001

4613

AFT

*CF

O/C09-Apr-1991MTH

344023 TRAMSMITTER RADIO ALT ANTENNA

622-0954-001

4116

FORWARD

*CF

O/C09-Apr-1991MTH

345004 TRANSPONDER ANTENNA

DMNI50-2-2

44546

AFT 85226 *CF

O/C09-Apr-1991MTH

345004 TRANSPONDER ANTENNA

DMNI50-2-2

44537

FORWARD 85226 *CF

O/C09-Apr-1991MTH

345007 DME ANTENNA

DMNI50-2-2

44512

AFT 85226 *CF

O/C09-Apr-1991MTH

345007 DME ANTENNA

DMNI50-2-2

44524

FORWARD 85226 *CF

O/C09-Apr-1991MTH

345010 NAVIGATION ANTENNA

DMN4-17-1B

35038

NO. 1

*CF

O/C09-Apr-1991MTH

345013 NAV 2 INDICATOR

066-03034-0024

19374

KI-206 *CF

O/C09-Apr-1991MTH

345014 ADF ANTENNA

7510300-901

0703C399

NO. 1 AT-860 SMF

O/C07-Jun-2007MTH

04969HRS

345017 MARKER BEACON ANTENNA

CI164

SN-UNKNOWN

*CF

O/C09-Apr-1991MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

345018 GLIDESLOPE ANTENNA

RGS10-48

A1895

*CF

O/C09-Apr-1991MTH

345027 NAV MODULE

7510134-901

90070511

NO. 1 NV-850 *CF

O/C09-Apr-1991MTH

345027 NAV MODULE

7510134-901

90080542

NO. 2 NV-850 *CF

O/C09-Apr-1991MTH

345028 ADF MODULE

7510114-901

92030802

NO. 1 DF-850 TOL

O/C06-Nov-1992MTH

01057HRS

345029 NAV CLUSTER MODULE

7510164-902

90020492

NO. 1 XN-850 *CF

O/C09-Apr-1991MTH

345029 NAV CLUSTER MODULE

7510164-902

90070585

NO. 2 XN-850 *CF

O/C09-Apr-1991MTH

345030 CLEARANCE DELIVERY CONTROL

7513000-811

442

CD-850 SMF

O/C09-Sep-2013MTH

5961.8HRS

5486LDG

345031 NAVIGATION(FMS) COMPUTER

1192-00-111101

137

SAC

O/C09-Dec-2002MTH

16154231HRS

345034 ATC TRANSPONDER

7510774-901

900304483

NO. 1 XS-850 KALN

O/C23-May-2012MTH

5743.2HRS

5371LDG

345034 ATC TRANSPONDER

7510774-901

91120762

NO. 2 XS-850 KALN

O/C23-May-2012MTH

5743.2HRS

5371LDG

345035 DME INDICATOR

7513006-911

596

NO. 1 DI-851 *CF

O/C09-Apr-1991MTH

345035 DME INDICATOR

7513006-911

571

NO. 2 DI-851 *CF

O/C09-Apr-1991MTH

345036 DME RECEIVER TRANSMITTER

7510184-902

90040501

NO. 1 DM-850 *CF

O/C09-Apr-1991MTH

345036 DME RECEIVER TRANSMITTER

7510184-902

90080534

NO. 2 DM-850 *CF

O/C09-Apr-1991MTH

345038 INTERGRATED NAV UNIT

7510100-711

89050311

NO. 1 RNZ-850 SMF

O/C09-Sep-2013MTH

5961.8HRS

5486LDG

345038 INTERGRATED NAV UNIT

7510100-713

90090538

NO. 2 RNZ-850B SMF

O/C09-Sep-2013MTH

5961.8HRS

5486LDG

345081 CONFIGURATION MODULE

31990-1

2527

NO. 1 CMU-GNSX *CF

O/C09-Apr-1991MTH

345088 RADIO MANAGEMENT UNIT

7012100-983

90030497

NO. 1 RM-850 TOL

O/C05-Jun-1998MTH

4053159HRS

345088 RADIO MANAGEMENT UNIT

7012100-983

90110677

NO. 2 RM-850 TOL

O/C06-Nov-1992MTH

01057HRS




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

346003 TAWS COMPUTER

805-18000-001

80639

SMF

O/C20-Apr-2005MTH

04685HRS

346035 TRAFFIC ADVISORY PROCESSOR --

71-2420-7

060465

TAS620

O/C16-Jun-2006MTH

04838HRS

351001 OXYGEN PRESSURE GAUGE

C668512-0101

345

MD-97 *CF

0O/C09-Apr-1991MTH

351002 OXYGEN PRESSURE SWITCH

P24031

839

9912057-5 *CF

O/C09-Apr-1991MTH

351004 OXYGEN MASK

174045-15

7346

COPILOT

SMF

205O/C22-May-2015MTH

06283.9HRS

05674LDG

351004 OXYGEN MASK

174045-15

50732

PILOT

SMF

252O/C22-May-2015MTH

06283.9HRS

05674LDG

351005 OXYGEN SUPPLY REGULATOR

803215-03

C06100331

SMF

0O/C06-Feb-2009MTH

5261HRS

351006 OXYGEN CYLINDER

89520077

C06110084

9914067-42 SMF

31-Jul-2021018009-Feb-2007MTH 71 m 0 d

4922HRS

Manufacture Date: 01-Jul-2006

361003 PNEUMATIC REGULATOR

38E85-5C

RF-2203

9912043-2 SMF

O/C04-Mar-2011MTH

5568.6HRS

5282LDG

361008 VALVE CHECK

1553-00-18

221

NO. 1

LGB

O/C06-Apr-1994MTH

01794HRS

361008 VALVE CHECK

1553-00-18

144

NO. 2

LGB

O/C06-Apr-1994MTH

01794HRS

383002 MOTOR AND PUMP TOILET

17000-102

SN-UNKNOWN

*CF

O/C09-Apr-1991MTH

521001 CABIN DOOR SEAL

S15501-1

-NSN-

9912075-4 SMF

O/C06-Feb-2009MTH

05261HRS

521003 SECONDARY DOOR SEAL

R881515

NSN

SMF

0O/C19-Jul-2013MTH

05941HRS

05476LDG

531001 NOSE LANDING GEAR TRUNNION SUPPORT

6613056-3

SN-UNKNOWN

LEFT

*CF

09-Apr-1991MTH

120501398120500LDG 63371398

531001 NOSE LANDING GEAR TRUNNION SUPPORT

6613056-4

SN-UNKNOWN

RIGHT

*CF

09-Apr-1991MTH

120501398120500LDG 63371398

531202 ACTUATOR FITTING

6511105-1

SN-UNKNOWN

NOSE LANDING GEAR

*CF

09-Apr-1991MTH

235001398235000LDG 177871398

541001 INLET ASSEMBLY

6552500-207

SN-UNKNOWN

LEFT

TOL

O/C14-Mar-1999MTH

03430HRS




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

541001 INLET ASSEMBLY

6552500-206

SN-UNKNOWN

RIGHT

TOL

O/C14-Mar-1999MTH

03430HRS

561001 LEFTHAND MAIN WINDSHIELD

E149000-9

1665

NO. 1 9912064-11 *CF

O/C09-Apr-1991MTH

561002 RIGHTHAND MAIN WINDSHIELD

E149000-10

1476

NO. 2 9912064-12 *CF

O/C09-Apr-1991MTH

561003 FOUL WEATHER WINDOW

5511275-7

SN-UNKNOWN

*CF

O/C09-Apr-1991MTH

561005 PILOTS INNER WINDOW

5511285-5

SN-UNKNOWN

LEFT INBOARD

*CF

O/C09-Apr-1991MTH

561005 PILOTS OUTER WINDOW

5511285-3

SN-UNKNOWN

LEFT OUTBOARD

*CF

O/C09-Apr-1991MTH

561005 CO-PILOTS INNER WINDOW

5511285-6

110104

RIGHT INBOARD

O/C28-Apr-2005MTH

04685HRS

561005 CO-PILOTS OUTER WINDOW

5511285-78

3705

RIGHT OUTBOARD

O/C28-Apr-2005MTH

04685HRS

562001 CABIN DOOR WINDOW

5512207-1

SN-UNKNOWN

L1

562002 : L1

*CF

O/C09-Apr-1991MTH

562001 CABIN WINDOW

5511260-8

SN-UNKNOWN

L2

*CF

O/C09-Apr-1991MTH

562001 CABIN WINDOW

5511260-8

SN-UNKNOWN

L3

*CF

O/C09-Apr-1991MTH

562001 CABIN WINDOW

5511260-8

SN-UNKNOWN

L4

*CF

O/C09-Apr-1991MTH

562001 CABIN WINDOW

5511260-8

SN-UNKNOWN

L5

*CF

O/C09-Apr-1991MTH

562001 CABIN WINDOW

5511260-8

SN-UNKNOWN

L6

*CF

O/C09-Apr-1991MTH

562001 CABIN WINDOW

5511260-8

SN-UNKNOWN

L7

*CF

O/C09-Apr-1991MTH

562001 EMERGENCY DOOR WINDOW

5511260-8

SN-UNKNOWN

R1

*CF

O/C09-Apr-1991MTH

562001 CABIN WINDOW

5511260-8

SN-UNKNOWN

R2

*CF

O/C09-Apr-1991MTH

562001 CABIN WINDOW

5511260-8

SN-UNKNOWN

R3

*CF

O/C09-Apr-1991MTH

562001 CABIN WINDOW

5511260-8

SN-UNKNOWN

R4

*CF

O/C09-Apr-1991MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

562001 CABIN WINDOW

5511260-8

SN-UNKNOWN

R5

*CF

O/C09-Apr-1991MTH

562001 CABIN WINDOW

5511260-8

SN-UNKNOWN

R6

*CF

O/C09-Apr-1991MTH

562001 CABIN WINDOW

5511260-8

SN-UNKNOWN

R 7

*CF

O/C09-Apr-1991MTH

572001 MLG TRUNNION FITTING ASSEMBLY

5522710-15

SN-UNKNOWN

LEFT AFT

572003 : LA

*CF

09-Apr-1991MTH

258000258000LDG 20087


6522057-5

SN-UNKNOWN

LEFT FORWARD

*CF

09-Apr-1991MTH

258000258000LDG 20087


5522710-15

SN-UNKNOWN

RIGHT AFT

572003 : RA

*CF

09-Apr-1991MTH

258000258000LDG 20087


6522057-6

SN-UNKNOWN

RIGHT FORWARD

572002 : R

*CF

09-Apr-1991MTH

258001398258000LDG 200871398

574003 MLG SIDE BRACE SUPPORT FITTING

6522047-1

SN-UNKNOWN

LEFT

*CF

09-Apr-1991MTH

258000258000LDG 20087

574004 MLG SIDE BRACE SUPPORT FITTING

6522047-2

SN-UNKNOWN

RIGHT

*CF

09-Apr-1991MTH

258000258000LDG 20087

575001 FLAP

6525130-19

112C

LEFT INBOARD

ICT

O/C26-Feb-1992MTH

0591HRS

575002 FLAP

6525130-20

108C

RIGHT INBOARD

TOL

O/C11-Feb-1994MTH

01729HRS

712001 ENGINE AFT ISOLATOR

LM420SA6-1

R0160

LEFT 9912455-2 PIT

23-Jul-1999MTH

7014035003514HRS 674.9

712001 ENGINE AFT ISOLATOR

LM420SA6-1

40161

RIGHT 9912455-2 PIT

23-Jul-1999MTH

7014035003514HRS 674.9

712002 FORWARD ENGINE ISOLATOR

LM420SA-31

R0214

LEFT BOTTOM

PIT

23-Jul-1999MTH

7014035003514HRS 674.9


LM420SA-30

R0235

LEFT TOP

PIT

23-Jul-1999MTH

7014035003514HRS 674.9


LM420SA-31

R0212

RIGHT BOTTOM

PIT

23-Jul-1999MTH

7014035003514HRS 674.9


LM420SA-30

R0228

RIGHT TOP

PIT

23-Jul-1999MTH

7014035003514HRS 674.9

71EN1 ENGINE

JT15D-5A

108220

NO. 1

710001 : E1**L

3042000 PIT

E/C23-Jul-1999MTH

03514HRS

71EN2 ENGINE

JT15D-5A

108198

NO. 2

710001 : E2**R

3042000 PIT

E/C23-Jul-1999MTH

03514HRS




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

724001 COMBUSTOR LINER

3113170-01

4F110

E1

PIT

O/C23-Jul-1999MTH

03514HRS

724001 COMBUSTOR LINER

3113170-01

1F731

E2

PIT

O/C23-Jul-1999MTH

03514HRS

721010 ACESSORY DRIVE GEAR BOX

3031170

SN-UNKNOWN

E1

*CF

O/C09-Apr-1991MTH

721010 ACESSORY DRIVE GEAR BOX

3031170

SN-UNKNOWN

E2

*CF

O/C09-Apr-1991MTH

722001 OIL PUMP

3104289-01

4Y603

E1

PIT

O/C23-Jul-1999MTH

03514HRS

722001 OIL PUMP

3104289-01

4Y554

E2

PIT

O/C23-Jul-1999MTH

03514HRS

722607 LOW COMPRESSOR HUB

3037911

30A521

E1 3037911 PIT

23-Jul-1999MTH

3514HRS

(11997)120493698120003747LDG 6336

722607 LOW COMPRESSOR HUB

3037911

28A413

E2 3037911 PIT

23-Jul-1999MTH

3514HRS

(11997)120493698120003747LDG 6336

723001 LP COMPRESSOR ROTOR BALANCE ASSEMBLY

3102814-01

SN-UNKNOWN

E1

PIT

O/C23-Jul-1999MTH

03514HRS

723001 LP COMPRESSOR ROTOR BALANCE ASSEMBLY

3102814-01

SN-UNKNOWN

E2

PIT

O/C23-Jul-1999MTH

03514HRS

723020 LOW BOOST COMPRESSOR HUB

3034112

27A524

E1 3034112 PIT

23-Jul-1999MTH

3514HRS

(13997)140493698140003747LDG 8336

723020 LOW BOOST COMPRESSOR HUB

3034112

28A941

E2 3034112 PIT

23-Jul-1999MTH

3514HRS

(13997)140493698140003747LDG 8336

723705 2ND-STAGE LOW TURBINE ROTOR DISK

3022212

32A219

E1

PIT

23-Jul-1999MTH

3514HRS

(13997)140493698140003747LDG 8336

723705 2ND-STAGE LOW TURBINE ROTOR DISK

3022212

31A911

E2

PIT

23-Jul-1999MTH

3514HRS

(13997)140493698140003747LDG 8336

724006 3RD-STAGE LOW TURBINE ROTOR DISK

3036113

33A480

E1

PIT

23-Jul-1999MTH

3514HRS

(13997)140493698140003747LDG 8336

724006 3RD-STAGE LOW TURBINE ROTOR DISK

3036113

30A480

E2

PIT

23-Jul-1999MTH

3514HRS

(13997)140493698140003747LDG 8336

724706 HIGH TURBINE ROTOR DISK

3036411

34A253

E1

PIT

23-Jul-1999MTH

3514HRS

(10523)105753698105263747LDG 4862

724706 HIGH TURBINE ROTOR DISK

3036411

11A374

E2

PIT

23-Jul-1999MTH

3514HRS

(10523)105753698105263747LDG 4862

724707 HIGH TURBINE BLADES

3029601

SN-UNKNOWN

E1 3029601 PIT

O/C23-Jul-1999MTH

03514HRS




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

724707 HIGH TURBINE BLADES

3029601

SN-UNKNOWN

E2 3029601 PIT

O/C23-Jul-1999MTH

03514HRS

724825 CENTRIFUGAL IMPELLER

3033682

9D744

E1 3033682 PIT

23-Jul-1999MTH

3514HRS

(8997)9049369890003747LDG 3336

724825 CENTRIFUGAL IMPELLER

3033682

9D273

E2 3033682 PIT

23-Jul-1999MTH

3514HRS

(8997)9049369890003747LDG 3336

731004 LOW FUEL PRESSURE SWITCH

1103P92

SN-UNKNOWN

NO. 1 9912033-1 *CF

O/C09-Apr-1991MTH

731004 LOW FUEL PRESSURE SWITCH

1103P0448

3539

NO. 2 9912033-2 TOL

O/C14-Mar-1999MTH

03430HRS

733002 FUEL FLOW/QUANTITY INDICATOR

VSDL-OC208E

659

9912147-16 *CF

O/C09-Apr-1991MTH

733003 FUEL FLOW TRANSMITER

3268014-0201

1593B

NO. 1 9912031-6 LGB

O/C01-Dec-1996MTH

02692HRS

733003 FUEL FLOW TRANSMITER

3268014-0201

1604B

NO. 2 9912031-6 LGB

O/C01-Dec-1996MTH

02692HRS

731001 FUEL PUMP

717101-1

258

E1 3037078 PIT

O/C23-Jul-1999MTH

03514HRS

731001 FUEL PUMP

717100

232S

E2 3037078 PIT

O/C23-Jul-1999MTH

03514HRS

731002 FLOW DIVIDER VALVE

26395-2

259

E1 3119573-01 PIT

O/C23-Jul-1999MTH

03514HRS

731002 FLOW DIVIDER VALVE

26395-2

403

E2 3119573-01 PIT

O/C23-Jul-1999MTH

03514HRS

731005 BLEED CONTROL VALVE

800831-1-001-L7

C9510018

E1 3118876-01 PIT

O/C23-Jul-1999MTH

03514HRS

731005 BLEED CONTROL VALVE

800831-1-001-L7

92030005

E2 3118876-01 PIT

O/C23-Jul-1999MTH

03514HRS

731006 EFCU WIRING HARNESS

3112429-01

9W686

E1

PIT

O/C23-Jul-1999MTH

03514HRS

731006 EFCU WIRING HARNESS

3112429-01

9W659

E2

PIT

O/C23-Jul-1999MTH

03514HRS

731020 FUEL-OIL COOLER

11438-001J

551

E1 3033002 PIT

O/C23-Jul-1999MTH

03514HRS

731020 FUEL-OIL COOLER

11438-001J

513

E2 3033002 PIT

O/C23-Jul-1999MTH

03514HRS

731030 MOTIVE FLOW VALVE

PN

SN-UNKNOWN

E1

0O/C09-Apr-1991MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

731030 MOTIVE FLOW VALVE

PN

SN-UNKNOWN

E2

0O/C09-Apr-1991MTH


PN

SN-UNKNOWN

E1

0O/C09-Apr-1991MTH


PN

SN-UNKNOWN

E2

0O/C09-Apr-1991MTH

731085 SCHEDULE MODULATOR

PN

SN-UNKNOWN

E1

0O/C09-Apr-1991MTH

731085 SCHEDULE MODULATOR

PN

SN-UNKNOWN

E2

0O/C09-Apr-1991MTH

732001 FUEL CONTROL UNIT

3244851-7

B29562

E1 3119508-05 PIT

O/C23-Jul-1999MTH

03514HRS

732001 FUEL CONTROL UNIT

3244851-7

B29262

E2 3119508-05 PIT

O/C23-Jul-1999MTH

03514HRS

732005 N1 SPEED SENSOR

3100335-01

SN-UNKNOWN

E1

*CF

O/C09-Apr-1991MTH


3100335-01

SN-UNKNOWN

E2

*CF

O/C09-Apr-1991MTH


3032997

SN-UNKNOWN

E1 BOTTOM

*CF

O/C09-Apr-1991MTH


3032997

SN-UNKNOWN

E1 TOP

*CF

O/C09-Apr-1991MTH


3032997

SN-UNKNOWN

E2 BOTTOM

*CF

O/C09-Apr-1991MTH


3032997

SN-UNKNOWN

E2 TOP

*CF

O/C09-Apr-1991MTH

732007 IDLE SOLENOID ASSEMBLY

3242737

70770

E2

SMF

O/C31-Mar-2000MTH

03718HRS

732045 ELECTRONIC BLEED VALVE CONTROL

PN

SN-UNKNOWN

E1

0O/C09-Apr-1991MTH

732045 ELECTRONIC BLEED VALVE CONTROL

PN

SN-UNKNOWN

E2

0O/C09-Apr-1991MTH

732065 MAIN WIRING HARNESS

PN

SN-UNKNOWN

E1

0O/C09-Apr-1991MTH

732065 MAIN WIRING HARNESS

PN

SN-UNKNOWN

E2

0O/C09-Apr-1991MTH

741001 IGNITION EXCITER

NB01201

R5948

E1 INBOARD 3033378 PIT

O/C23-Jul-1999MTH

03514HRS




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -


NB01201

R5958

E1 OUTBOARD 3033378 PIT

O/C23-Jul-1999MTH

03514HRS


305013

682

E2 INBOARD 3037865 PIT

O/C23-Jul-1999MTH

03514HRS


CH92028

01030791

E2 OUTBOARD 3041996-01 SMF

O/C25-Jun-2001MTH

03926HRS

742001 IGNITER PLUG

FHE-246-4

-NSN-

E1 INBOARD 3030595 SMF

0O/C29-Jan-2015MTH

06147.1HRS

5586LDG

742001 IGNITER PLUG

FHE-246-4

-NSN-

E1 OUTBOARD 3030595 SMF

0O/C29-Jan-2015MTH

06147.1HRS

5586LDG

742001 IGNITER PLUG

FHE-246-4

-NSN-

E2 INBOARD 3030595 SMF

0O/C29-Jan-2015MTH

06147.1HRS

5586LDG

742001 IGNITER PLUG

FHE-246-4

-NSN-

E2 OUTBOARD 3030595 SMF

0O/C29-Jan-2015MTH

06147.1HRS

5586LDG

742002 IGNITER PLUG CABLE

10-395428-1

NN08084195

E1 INBOARD

SMF

0O/C04-Mar-2011MTH

05568.6HRS

5282LDG


53067-21

SN-UNKNOWN

E2 INBOARD

PIT

O/C23-Jul-1999MTH

03514HRS


53067-38.5

-NSN-

E1 OUTBOARD

SMF

O/C28-Apr-2005MTH

04685HRS


53067-38.5

-NSN-

E2 OUTBOARD

SMF

0O/C29-Jan-2015MTH

06147.1HRS

5586LDG

761002 SYNCHRONIZER CONTROL BOX

213693

2331476

*CF

O/C09-Apr-1991MTH

761003 ENGINE SYNC ACTUATOR

5485-066

2168179F

*CF

O/C09-Apr-1991MTH

771004 N1 FAN TACHOMETER INDICATOR

VSDL-OC410AE

225B

9912147-27 *CF

O/C09-Apr-1991MTH

771005 N2 TURBINE TACHOMETER INDICATOR

DDL-OC110B

228B

9912147-28 LBE

O/C31-Jul-1991MTH

0256HRS

772001 INTERSTAGE TURBINE TEMPERATURE (ITT) INDICATOR

VSDL-OC419H

559

9912147-15 *CF

O/C09-Apr-1991MTH

783001 THRUST REVERSER ASSEMBLY

262-0001-501

2412

LEFT ENGINE 9912377-1 *CF

O/C09-Apr-1991MTH

783001 THRUST REVERSER ASSEMBLY

262-0001-503

2413

RIGHT ENGINE 9912377-2 *CF

O/C09-Apr-1991MTH

783002 THRUST REVERSER CONTROL VALVE

65680

1497

LEFT ENGINE

*CF

O/C09-Apr-1991MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

783002 THRUST REVERSER CONTROL VALVE

65680

4051

RIGHT ENGINE

SAC

O/C17-Mar-2003MTH

4265HRS

04341LDG

783003 THRUST REVERSER ISOLATION VALVE

13027-4

2223

LEFT ENGINE

*CF

O/C09-Apr-1991MTH

783003 THRUST REVERSER ISOLATION VALVE

13027-4

2231

RIGHT ENGINE

*CF

O/C09-Apr-1991MTH

783005 THRUST REVERSER UPPER DOOR ASSEMBLY

202-0001-503

2412

LEFT

*CF

O/C09-Apr-1991MTH

783005 THRUST REVERSER UPPER DOOR ASSEMBLY

202-0001-504

2415

RIGHT

CKB

O/C30-Sep-1993MTH

1537HRS

01680LDG

783006 THRUST REVERSER LOWER DOOR ASSEMBLY

202-0002-505

2412

LEFT

*CF

O/C09-Apr-1991MTH

783006 THRUST REVERSER LOWER DOOR ASSEMBLY

202-0002-506

2415

RIGHT

*CF

O/C09-Apr-1991MTH

783007 THRUST REVERSER UPPER MECHANISM

225-0007-513

2412

LEFT

*CF

O/C09-Apr-1991MTH

783007 THRUST REVERSER UPPER MECHANISM

225-0007-513

2413

RIGHT

*CF

O/C09-Apr-1991MTH

783008 THRUST REVERSER LOWER MECHANISM

225-0007-515

2412

LEFT

*CF

O/C09-Apr-1991MTH

783008 THRUST REVERSER LOWER MECHANISM

225-0007-515

2413

RIGHT

*CF

O/C09-Apr-1991MTH

783009 THRUST REVERSER FAN DUCT

225-0014-507

2412

LEFT

*CF

O/C09-Apr-1991MTH

783009 THRUST REVERSER FAN DUCT

225-0014-508

2413

RIGHT

*CF

O/C09-Apr-1991MTH

783010 THRUST REVERSER ACTUATOR

62270

2948

LEFT INBOARD

*CF

O/C09-Apr-1991MTH


62270

2943

LEFT OUTBOARD

*CF

O/C09-Apr-1991MTH


62270

2949

RIGHT INBOARD

*CF

O/C09-Apr-1991MTH


62270

2946

RIGHT OUTBOARD

*CF

O/C09-Apr-1991MTH

783011 EXHAUST NOZZLE CONE

225-0016-513-V4

SN-UNKNOWN

RIGHT 9912377-3 *CF

O/C09-Apr-1991MTH

783012 EXHAUST NOZZLE

225-0016-515-V5

SN-UNKNOWN


O/C09-Apr-1991MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Components

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

793001 OIL TEMP INDICATOR

VSDL-OC219F

658

9912147-11 *CF

O/C09-Apr-1991MTH

793002 OIL TEMPERATURE TRANSMITTER

102-00083

71

LEFT ENGINE

TOL

O/C15-Dec-1993MTH

01647HRS

793002 OIL TEMPERATURE TRANSMITTER

102-00083

35

RIGHT ENGINE

TOL

O/C15-Dec-1993MTH

01647HRS

793003 OIL PRESSURE INDICATOR

VSDL-OC204N

213

9912147-30 *CF

O/C09-Apr-1991MTH

793004 OIL PRESSURE TRANSMITTER

123479

43977


O/C09-Apr-1991MTH

793004 OIL PRESSURE TRANSMITTER

123479

43933


O/C09-Apr-1991MTH

793006 LOW OIL PRESSURE SWITCH

1103P89-2

SN-UNKNOWN


O/C09-Apr-1991MTH

793006 LOW OIL PRESSURE SWITCH

1103P89-2

SN-UNKNOWN


O/C09-Apr-1991MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015

Part Number

Part Serial No



Remains

RemainsTSO 2

TSO 1

Service Bulletins

(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SL 560-03-02 R1 SUPPLEMENTAL TYPE CERTIFICATE (STC) (THIS SL IS REPLACED BY CIL-03-01, DATED JUNE 3, 2013)

INFORMATIONAL -

MOC :

SB 560-03-06 R1 OPERATIONAL CERTIFICATION REQUIREMENTS - U.S. TO CANADIAN CONVERSION

OPTIONAL -

MOC :

SB 560-03-06 OPERATIONAL CERTIFICATION REQUIREMENTS - U.S. TO CANADIAN CONVERSION

OPTIONAL -

MOC :

SL CIL-03-01 SUPPLEMENTAL TYPE CERTIFICATE (STC)

INFORMATIONAL

-

MOC :

SL CIL-99-01 R1 USE OF CORROSION INHIBITING COMPOUNDS

INFORMATIONAL

-

MOC :

SL CIL-99-01 USE OF CORROSION INHIBITING COMPOUNDS

INFORMATIONAL

-

MOC :

SL CIL-99-02 AVOID OPERATIONS ON RUNWAYS TREATED WITH RUNWAY DE-ICE (RDI) FLUIDS. AIRCRAFT WASHING RECOMMENDED

AFTER EXPOSURE TO RDI FLUIDS

RECOMMENDED -MTH

MOC :

SL CIL-99-03 R1 CORROSION PREVENTION AND CONTROL PROGRAM (CPCP)

RECOMMENDED

-

MOC :

SL CIL-99-03 CORROSION PREVENTION AND CONTROL PROGRAM (CPCP)

RECOMMENDED

-MTH

MOC :

SL 560-99-02 R6 CESCOM PRICES (THIS SL CANCELS SL560-99-02 R5 AND PREVIOUS)

INFORMATIONAL -

MOC :

SL 560-99-04 MISCELLANEOUS - CESSNA PART NUMBER SUFFIXES FOR REMANUFACTURED PARTS

INFORMATIONAL A/R

MOC :

SL 560-99-05 MISCELLANEOUS - CESSNA SERVICE DOCUMENT CHANGE NOTIFICATION

INFORMATIONAL A/R

MOC :

SB 560-11-02 FLAP NO STEP PLACARD INSTALLATION

RECOMMENDED

11SB-02

TOL

-25-Feb-1993MTH Complete

1203HRS

COMPLIED WITHMOC :

SB 560-11-04 FIRE EXTINGUISHER PLACARD INSTALLATION

OPTIONAL

11SB-04

-MTH

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SB 560-12-01 ADDITIONAL APPROVED FUEL ANTI-ICE ADDITIVES

INFORMATIONAL

-

MOC :

SL CIL-99-01 R2 USE OF CORROSION INHIBITING COMPOUNDS

INFORMATIONAL

-

MOC :

SL CIL-20-01 R2 STANDARD PRACTICES - CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL

INFORMATIONAL -

MOC :

SL CIL-20-01 CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL

INFORMATIONAL -

MOC :

SL 560-20-01 R25 STANDARD PRACTICES - CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL

INFORMATIONAL A/R

MOC :

SB 560-21-06 TAILCONE PRESSURE VALVE ACTUATOR WIRING MODIFICATION

OPTIONAL21SB-06 -MTH

MOC :

SB 560-21-08 R1 P-10 PANEL ACCESS AIR DUCT MODIFICATION

OPTIONAL

21SB-08 : 560R1

-MTH

MOC :

SB 560-21-10 ADDITIONAL OUTFLOW VALVE REPLACEMENT

SUPERSEDED

21SB-10

LGB

A/R28-Aug-1995MTH Complete

2247HRS

COMPLIED WITHMOC :

SB 560-21-12 R1 RAM AIR DUCT IMPROVEMENT

OPTIONAL

21SB-12 : 560R1

-MTH

MOC :

SB 560-21-12 R2 RAM AIR DUCT IMPROVEMENT

OPTIONAL

A/R

MOC :

SB 560-21-15 COCKPIT SIDE WINDOW DEFOG SYSTEM MODIFICATION

OPTIONAL

21SB-15

-MTH

MOC :

SB 560-21-16 R1 CABIN FAN AND DEFOT BLOWER WIRING IMPROVEMENT

DISCRETIONARY

21SB-16 : 560R1

-MTH

MOC :

SB 560-21-30 CABIN ALTITUDE BAROMETRIC SWITCH IMPROVEMENT

OPTIONAL

21SB-30

A/RMTH

MOC :

SB 560-21-35 TEMPERATURE CONTROLLER IMPROVEMENT

OPTIONAL

A/RMTH

MOC :

SL CIL-21-01 COMPRESSOR MOTOR BRUSH LIFE LIMIT

INFORMATIONAL

-

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SL CIL-21-02 R1 ENVIRONMENTAL HOUR METER INSTALLATION

MANDATORY

SMF

-29-Jan-2015MTH Complete

6147.1HRS

5586LDG

COMPLIED WITH - COMPLIED WITH CIL-21-02 REVISION 1 BY INSTALLING AN HOUR METER FOR THE

COMPRESSOR MOTOR.

MOC :

SL CIL-21-02 ENVIRONMENTAL HOUR METER INSTALLATION

OPTIONAL

SMF

-11-Apr-2014MTH Complete

6043.9HRS

5528LDG

COMPLIED WITH - COMPLIED WITH CIL-21-02 BY INSTALLING AN AC HOUR METER PER THE

ACCOMPLISHMENT INSTRUCTIONS.

MOC :

SL 560-21-02 AIR CONDITIONING - COMPRESSOR DRIVE MOTOR BRUSH INSPECTION/REPLACEMENT (FORT WORTH AIRWORKS INC. -

ZEPHYR AIR CONDITIONING)

RECOMMENDED21SL-02 TOL -29-May-1992MTH Complete

759HRS

COMPLIED WITHMOC :

SL 560-21-03 EMERGENCY PRESSURIZATION SUPPLY LINE INSPECTION/MODIFICATION


759HRS

COMPLIED WITHMOC :

SL 560-21-05 COUPLING INSPECTION AND TORQUE REQUIREMENTS

RECOMMENDED

21SL-05

TOL

-25-May-1993MTH Complete

1346HRS

COMPLIED WITHMOC :

SL 560-21-06 R1 VENTILATION BOX ASSEMBLY FORWARD FLANGE INSPECTION/REPAIR

RECOMMENDED21SL-06 : 560R1 LGB A/R28-Aug-1995MTH Complete

2247HRS

COMPLIED WITHMOC :


RECOMMENDED21SL-06 : 560R2 TOL A/R08-Jan-1998MTH Complete

2999HRS

COMPLIED WITHMOC :


RECOMMENDED21SL-06 : 560R3 TOL -14-Mar-1999MTH Complete

3430HRS

COMPLIED WITHMOC :

SL 560-21-06 VENTILATION BOX ASSEMBLY FORWARD FLANGE INSPECTION/REPAIR

RECOMMENDED21SL-06 TOL A/R15-Dec-1993MTH Complete

1647HRS

COMPLIED WITHMOC :

SL 560-21-09 EVAPORATOR MODULE INSTALLATION 1250240 AND 1134240 SERIES

RECOMMENDED21SL-09 -MTH

MOC :

SL 560-21-10 OUTFLOW VALVE STATIC PRESSURE LINE INSPECTION/REPLACEMENT


MOC :

SL 560-21-11 R1 RAM AIR INLET DRAIN LINE INSPECTION

RECOMMENDED

21SL-11 : 560R1

SAC

-28-Jun-2004MTH Complete

4560HRS

COMPLIED WITH - NOT APPLICABLEMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SL 560-21-16 AIR CONDITIONING - AIR CONDITIONING EXHAUST DOOR SHAFT SPACER INSPECTION

DISCRETIONARY21SL-16 A/RMTH

MOC :

SB 560-23-09 R1 HONEYWELL EFIS SYMBOL GENERATOR INTERPOSER FILTER INSTALLATION

OPTIONAL23SB-09 : 560R1 ICT A/R26-Feb-1992MTH Complete

591HRS

COMPLIED WITHMOC :

SB 560-23-10 CABIN PASSENGER ADDRESS MODIFICATION

RECOMMENDED

23SB-10

TOL

A/R25-Feb-1993MTH Complete

1203HRS

COMPLIED WITHMOC :

SB 560-23-12 PRIMUS II SIMULCOM WIRING ADDITION

RECOMMENDED

23SB-12

TOL


1346HRS

COMPLIED WITHMOC :

SB 560-23-14 FLITEFONE VI ANTENNA CABLE REPLACEMENT

RECOMMENDED

23SB-14

TOL

A/R03-Sep-1993MTH Complete

1503HRS

COMPLIED WITHMOC :

SB 560-23-16 STATIC WICK REPLACEMENT

OPTIONAL

23SB-16

*CF

-MTH

MOC :

SB 560-23-19 R1 ELECTRICAL BONDING FLAP AND SPEED BRAKE PUSHRODS

RECOMMENDED

23SB-19 : 560R1

TOL

A/R14-Mar-1999MTH Complete

3430HRS

COMPLIED WITHMOC :

SB 560-23-19 R2 ELECTRICAL BONDING FLAP AND SPEED BRAKE PUSHRODS

RECOMMENDED

23SB-19 : 560R2

SAC


4560HRS

COMPLIED WITHMOC :

SB 560-23-19 ELECTRICAL BONDING FLAP AND SPEED BRAKE PUSHRODS

RECOMMENDED

23SB-19

TOL

A/R08-Jan-1998MTH Complete

2999HRS

COMPLIED WITHMOC :

SB 560-23-25 R1 HONEYWELL 8.33 KHZ COMMUNICATION RADIO INSTALLATION

OPTIONAL23SB-25 : 560R1 -MTH

MOC :

SB 560-23-26 R1 COLLINS 8.33 KHZ COMMUNICATION RADIO INSTALLATION

OPTIONAL

23SB-26 : 560R1

-MTH

MOC :

SB 560-23-30 R1 VLF NOISE FILTER CAPACITOR REMOVAL/REPLACEMENT

MANDATORY

23SB-30 : 560R1

SMF


3718HRS

COMPLIED WITHMOC :

SB 560-23-32 R1 RNZ-850 NAVIGATION RADIO UPGRADE

MANDATORY

23SB-32 : 560R1

SAC


4531HRS

COMPLIED WITHMOC :

SB 560-23-38 R2 COMMUNICATIONS - RADIO MANAGEMENT UNIT (RM855) INSTALLATION

OPTIONAL -

MOC :

SB 560-23-38 COMMUNICATIONS - RADIO MANAGEMENT UNIT (RM855) INSTALLATION

OPTIONAL A/RMTH

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SL 560-23-15 TRANSMITTAL OF AIRSHOW SERVICE BULLETIN 920720-1 AIRSHOW 400 DIGITAL INTERFACE UNIT

RECOMMENDED23SL-15 -DAYS 55

MOC :

SL 560-23-16 R1 AIRSHOW RELIABILITY IMPROVEMENTS AND SERVICE PACK SOFTWARE UPGRADE

RECOMMENDED23SL-16 : 560R1 A/RMTH

MOC :

SB 560-24-03 R1 MAIN LANDING GEAR AXLE ANTISKID WIRE BUNDLE PROTECTION

RECOMMENDED24SB-03 : 560R1 TOL -29-May-1992MTH Complete

759HRS

COMPLIED WITHMOC :

SB 560-24-03 MAIN LANDING GEAR AXLE ANTISKID WIRE BUNDLE PROTECTION

RECOMMENDED24SB-03 TOL A/R29-May-1992MTH Complete

759HRS

COMPLIED WITHMOC :

SB 560-24-04 R3 LIGHT DIMMING AND TEST PRINTED CIRCUIT BOARD MODIFICATION

RECOMMENDED24SB-04 : 560R3 LGB -28-Aug-1995MTH Complete

2247HRS

COMPLIED WITHMOC :

SB 560-24-04 LIGHT DIMMING AND TEST PRINTED CIRCUIT BOARD MODIFICATION

RECOMMENDED24SB-04 TOL A/R06-Nov-1992MTH Complete

1057HRS

COMPLIED WITHMOC :

SB 560-24-05 DUAL FLIGHT DIRECTORS CIRCUIT BREAKER BUSSING INSPECTION/MODIFICATION

MANDATORY24SB-05 TOL A/R21-Aug-1991MTH Complete

293HRS

COMPLIED WITHMOC :

SB 560-24-08 WING WIRE BUNDLE ROUTING MODIFICATION

RECOMMENDED

24SB-08

TOL

A/R29-May-1992MTH Complete

759HRS

COMPLIED WITHMOC :

SB 560-24-10 NOSE AVIONICS GROUND BLOCK MODIFICATION

RECOMMENDED

24SB-10

LGB

A/R12-Nov-1994MTH Complete

2020HRS

COMPLIED WITHMOC :

SB 560-24-11 LIGHT DIMMING CIRCUIT J-BOX SCREW AND DIODE MODIFICATION

OPTIONAL24SB-11 A/RMTH

MOC :

SB 560-24-12 R3 AVIONICS POWER RELAYS REPLACEMENT

OPTIONAL

24SB-12 : 560R3

-MTH

MOC :

SB 560-24-14 WING TIP WIRE BUNDLE PROTECTIVE COVER INSTALLATION

RECOMMENDED24SB-14 LGB -10-Sep-1994MTH Complete

1953HRS

COMPLIED WITHMOC :

SB 560-24-15 R1 ELECTRICAL CABLE CHAFING PROTECTION INSTALLATION WS 44.0 AND 54.07

RECOMMENDED24SB-15 : 560R1 LGB -18-Mar-1996MTH Complete

2448HRS

COMPLIED WITHMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SB 560-24-15 ELECTRICAL CABLE CHAFING PROTECTION INSTALLATION WS 44.0 AND 54.07

RECOMMENDED24SB-15 VNY A/R02-Mar-1995MTH Complete

2104HRS

COMPLIED WITHMOC :

SB 560-24-16 TRIM PC BOARD MODIFICATION AND ELEVATOR ELECTRIC TRIM MOTOR MODIFICATION

SUPERSEDED24SB-16 TOL -08-Jan-1998MTH Complete

2999HRS

COMPLIED WITHMOC :

SB 560-24-19 R1 OVERVOLTAGE MONITOR SYSTEM INSTALLATION

OPTIONAL

24SB-19 : 560R1

-MTH

MOC :

SB 560-24-20 BATTERY DISCONNECT RELAY ACCESS IMPROVEMENT

OPTIONAL

24SB-20

-MTH

- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :

SB 560-24-22 CIRCUIT BREAKER TERMINAL SCREW LENGTH INSPECTION/REPLACEMENT

RECOMMENDED24SB-22 -MTH

MOC :

SB 560-24-27 R1 WING WIRE ROUTING IMPROVEMENT/FLAP HYDRAULIC LINE INSPECTION

RECOMMENDED24SB-27 : 560R1 -MTH

MOC :

SB 560-24-29 NO SMOKING LIGHT WIRING MODIFICATION

OPTIONAL

24SB-29

-MTH

MOC :

SB 560-24-37 R3 MAIN POWER WIRE ANCHOR IMPROVEMENT

RECOMMENDED

24SB-37 : 560R3

-MTH

MOC :

SB 560-24-39 SEALED LEAD ACID BATTERY INSTALLATION

OPTIONAL

24SB-39

-MTH

MOC :

SB 560-24-42 RELAY SHIELD INSTALLATION

MANDATORY

24SB-42

SMF

-17-Nov-2005MTH Complete

4766HRS

COMPLIED WITHMOC :

SB 560-24-45 ELECTRICAL POWER - MAGNETIC CIRCUIT BREAKER REPLACEMENT

OPTIONAL A/R

MOC :

SL 560-24-05 ANTI-ICE RELAY BASE ORIENTATION MODIFICATION

RECOMMENDED

24SL-05

TOL

A/R30-Oct-1991MTH Complete

451HRS

COMPLIED WITHMOC :

SL 560-24-06 MFD SYMBOL GENERATOR WIRE BUNDLE SUPPORT INSTALLATION

OPTIONAL24SL-06 TOL -29-May-1992MTH Complete

759HRS

COMPLIED WITHMOC :

SL 560-24-07 HARTMAN BATTERY DISCONNECT RELAY PART NUMBER A876K INSPECTION/REPLACE

RECOMMENDED24SL-07 TOL A/R06-Nov-1992MTH Complete

1057HRS

COMPLIED WITHMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SB 560-25-09 PASSENGER SEAT BACK PIVOT PLATE ASSEMBLY INSPECTION/REPLACEMENT

RECOMMENDED25SB-09 TOL A/R15-Dec-1993MTH Complete

1647HRS

COMPLIED WITHMOC :

SB 560-25-16 R1 WINDOW TRIM INSULATION IMPROVEMENTS

RECOMMENDED

25SB-16 : 560R1

TOL


3159HRS

COMPLIED WITHMOC :

SB 560-25-16 WINDOW TRIM INSULATION IMPROVEMENTS

RECOMMENDED

25SB-16

LGB


2448HRS

COMPLIED WITHMOC :

SB 560-25-19 TSO C91A EMERGENCY LOCATOR TRANSMITTER INSTALLATION

CANCELLED25SB-19 A/RMTH

MOC :

SB 560-25-23 FLIGHT CREW SEAT PAN REINFORCEMENT

OPTIONAL

25SB-23

-MTH

MOC :

SB 560-25-26 R1 EQUIPMENT/FURNISHINGS - ARTEX C406-2 THREE-FREQUENCY EMERGENCY LOCATOR TRANSMITTER (ELT)

SUPERSEDED25SB-26 : 560R1 A/R

- SERVICE BULLETIN ON HOLD.MOC :

SB 560-25-26 R3 ARTEX C406-2 THREE-FREQUENCY EMERGENCY LOCATORTRANSMITTER (ELT)

OPTIONAL A/R

MOC :

SB 560-25-29 R1 GLARESHIELD LEATHER STRIP INSTALLATION

OPTIONAL

25SB-29 : 560R1

-MTH

MOC :

SB 560-25-32 R1 EQUIPMENT/FURNISHINGS - TOILET TRAY AND PAD INSTALLATION

OPTIONAL25SB-32 : 560R1 A/RMTH

MOC :

SL 560-25-03 LIFE PRESERVERS AND INDIVIDUAL FLOTATION DEVICES REPLACEMENT

MANDATORY25SL-03 PIT A/R27-Sep-1997MTH Complete

2912HRS

COMPLIED WITH - NOT APPLICABLE BY DATE OF MANUFACTUREMOC :

SL 560-25-04 GLARESHIELD ATTACHMENT SCREW(S) INSPECTION/REPLACEMENT


MOC :

SL 560-25-09 EQUIPMENT/FURNISHINGS - TRANSMITTAL OF PACIFIC SCIENTIFIC AEROSPACE SERVICE BULLETIN SB 25-1111432,

INFORMATION REGARDING THE POTENTIAL FAILURE OF THE GUARDED ROTARYBUCKLE PLASTIC HANDLE

MANDATORY25SL-09 SMF A/R25-Jun-2008MTH Complete

5180HRS

COMPLIED WITHMOC :

SB 560-26-01 FIRE BOTTLE WIRE IDENTIFICATION SLEEVE INSTALLATION

MANDATORY26SB-01 SMF A/R17-Nov-2005DAYS Complete

4766HRS

COMPLIED WITHMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

ASL 560-26-01 FIRE PROTECTION - TRANSMITTAL OF MEGGITT SAFETY SYSTEMS SERVICE BULLETIN 26-36 - THERMISTORS DETECTORS

MANDATORY26ASL-01 SMF A/R25-Jun-2008MTH Complete

5180HRS

COMPLIED WITHMOC :

SB 560-27-05 R1 FLIGHT CONTROLS - EXTENDED PEDESTAL AILERON PULLEY BRACKET MODIFICATION

SUPERSEDED27SB-05 : 560R1 ICT A/R26-Feb-1992MTH Complete

591HRS

COMPLIED WITHMOC :

SB 560-27-07 R1 ELEVATOR SERVO CABLE INSTALLATION MODIFICATION

SUPERSEDED

27SB-07 : 560R1

LGB

A/R06-Apr-1994MTH Complete

1794HRS

COMPLIED WITHMOC :

SB 560-27-07 R4 ELEVATOR SERVO CABLE INSTALLATION MODIFICATION

OPTIONAL

27SB-07 : 560R4

-MTH

MOC :

SB 560-27-09 IMPROVED ELEVATOR TRIM SECTOR INSTALLATION

SUPERSEDED

27SB-09

LGB


2448HRS

COMPLIED WITHMOC :

SB 560-27-11 AILERON/RUDDER INTERCONNECT CLAMP MODIFICATION

RECOMMENDED

27SB-11

TOL


3159HRS

COMPLIED WITHMOC :

SB 560-27-13 TRIM TAB ACTUATOR GREASE FITTING INSTALLATION

OPTIONAL

27SB-13

-MTH

MOC :

SB 560-27-22 FLIGHT CONTROLS - RUDDER PEDAL SUPPORT IMPROVEMENT

DISCRETIONARY27SB-22 A/RMTH

MOC :

SB 560-27-23 FLIGHT CONTROLS - ELEVATOR BELLCRANK SUPPORT BRACKET INSPECTION AND REPAIR

MANDATORY A/RMTH N/A

NOT APPLICABLE - BY SERIAL NUMBER APPLICABLE TO SERIAL NUMBERS -0539 THRU -0815.MOC :

SL 560-27-03 FLAP HYDRAULIC HOSE FITTING CLOCKING INSPECTION/ADJUSTMENT

RECOMMENDED27SL-03 TOL -15-Dec-1993MTH Complete

1647HRS

COMPLIED WITHMOC :

SL 560-27-05 AILERON/RUDDER INTERCONNECT RIGGING INSPECTION

RECOMMENDED

27SL-05

TOL


2999HRS

COMPLIED WITHMOC :

SL 560-27-06 RUDDER/AILERON INTERCONNECT BOLT INSPECTION

SUPERSEDED

27SL-06

TOL


2999HRS

COMPLIED WITHMOC :

SL 560-27-08 LOWER CABLE GUARD INSPECTION

RECOMMENDED

27SL-08

-MTH

MOC :

SB 560-28-02 WING LEADING EDGE RIB FLAPPER VALVES INSTALLATION

OPTIONAL

28SB-02

LBE

-MTH





Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SB 560-28-03 MOTIVE FLOW FUEL LINE INSPECTION AND SUPPORT INSTALLATION

RECOMMENDED28SB-03 TOL -25-May-1993MTH Complete

1346HRS

COMPLIED WITHMOC :

SB 560-28-04 FUEL SYS PLUMBING CLAMP ADDITIONS

RECOMMENDED

28SB-04

LGB

-18-Mar-1996MTH Complete

2448HRS

COMPLIED WITHMOC :

SB 560-28-05 IMPROVED FUEL CROSSFEED SELECT KNOB AVAILABILITY

OPTIONAL

28SB-05

-MTH

MOC :

SB 560-28-07 FUEL LINE SUPPORT INSTALLATION

RECOMMENDED

28SB-07

TOL

-26-Oct-1999MTH Complete

3608HRS

COMPLIED WITHMOC :

SB 560-28-10 WING FUEL BOOST PUMP WIRE ROUTING IMPROVEMENT

MANDATORY

28SB-10

SAC


4560HRS

COMPLIED WITHMOC :

SB 560-28-14 R1 FUEL - FUEL CHECK VALVE MODIFICATION

RECOMMENDED

-MTH

MOC :

SB 560-28-14 FUEL - FUEL CHECK VALVE MODIFICATION

RECOMMENDED

28SB-14

A/RMTH 4

MOC :

SL 560-28-01 R1 FUEL COMPENSATOR INSTALLATION ATTACHMENT INSPECTION

SUPERSEDED28SL-01 : 560R1 TOL A/R06-Nov-1992MTH Complete

1057HRS

COMPLIED WITHMOC :

SL 560-28-01 FUEL QUANTITY COMPENSATOR INSTALLATION ATTACHMENT INSPECTION

RECOMMENDED28SL-01 ICT -26-Feb-1992MTH Complete

591HRS

COMPLIED WITHMOC :

SLA 560-28-03 TRANSMITTAL OF PARKER HANNIFIN CORPORATION - AIRBORNE AIR & FUEL PRODUCTS NO. 41, RAPCO FLEET SUPPORT INC.

OVERHAUL OF AIRBORNE FUEL PUMPS

SUPERSEDED28SLA03 LGB A/R01-Dec-1996MTH Complete

2692HRS

COMPLIED WITHMOC :

SB 560-29-01 ECOLOGY (OVERFLOW) BOTTLE INSTALLATION

OPTIONAL

29SB-01

-MTH

MOC :

SB 560-29-02 IMPROVED HYDRAULIC PUMP PRESSURE HOSE INSTALLATION

RECOMMENDED29SB-02 LGB -01-Dec-1996MTH Complete

2692HRS

COMPLIED WITHMOC :

SB 560-29-04 R1 HYDRAULIC TUBE REPLACEMENT

MANDATORY

29SB-04 : 560R1

SMF


4766HRS

COMPLIED WITHMOC :

SB 560-29-08 R1 HYDRAULIC PRESSURE LINE ROUTING IMPROVEMENT

RECOMMENDED

A/R

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SB 560-29-08 HYDRAULIC PRESSURE LINE ROUTING IMPROVEMENT

RECOMMENDED

A/R

MOC :

SB 560-30-02 ANTI-ICE TEMPERATURE SENSOR SUPPORT ANGLE MODIFICATION

SUPERSEDED30SB-02 TOL A/R29-May-1992MTH Complete

759HRS

COMPLIED WITHMOC :

SB 560-30-03 ENGINE BLEED AIR ANTI-ICE TEMPERATURE SENSORS REPLACEMENT

RECOMMENDED30SB-03 TOL -29-May-1992MTH Complete

759HRS

COMPLIED WITHMOC :

SB 560-30-04 TAILCONE DEICE LINES SUPPORT INSPECTION/INSTALLATION

RECOMMENDED30SB-04 TOL -03-Sep-1993MTH Complete

1503HRS

COMPLIED WITHMOC :

SB 560-30-06 PICCOLO TUBE INSTALLATION INSPECTION AND MODIFICATION

SUPERSEDED30SB-06 LGB A/R10-Sep-1994MTH Complete

1953HRS

COMPLIED WITHMOC :

SB 560-30-10 WINDSHIELD ANTI-ICE BLEED AIR SWITCH INSPECTION/REPLACEMENT

MANDATORY30SB-10 SAC -28-Jun-2004MTH Complete

4560HRS


SB 560-30-15 ICE AND RAIN PROTECTION - ENGINE INLET ANTI-ICE VALVE SUPPORT BRACKET INSTALLATION

RECOMMENDED30SB-15 A/RMTH

MOC :

SL CIL-30-01 R1 APPROVED DEICING PROGRAM UPDATES

INFORMATIONAL

-

MOC :

SL 560-30-05 R1 ENGINE ANTI-ICE VALVE INSPECTION

RECOMMENDED

30SL-05 : 560R1

LGB


1953HRS

COMPLIED WITHMOC :

SL 560-30-05 ENGINE ANTI-ICE VALVE INSPECTION

SUPERSEDED

30SL-05

LGB


1794HRS

COMPLIED WITHMOC :

SB 560-31-09 INADVERTENT POWER BRAKE LOW PRESSURE ANNUNCIATION

RECOMMENDED

31SB-09

-MTH

MOC :

SB 560-31-15 INDICATING/RECORDING SYSTEMS - INSTRUMENT PANEL MODIFICATION FOR AOA TEST SWITCH

OPTIONAL31SB-15 A/RMTH

MOC :

SB 560-32-03 R5 GRAVEL RUNWAY PROTECTION

OPTIONAL

32SB-03 : 560R5

-MTH

MOC :

SB 560-32-06 BFGOODRICH BRAKE BLEEDER BLOCK INSTALLATION AND HOSE REPLACEMENT

OPTIONAL32SB-06 VNY -02-Mar-1995MTH Complete

2104HRS

COMPLIED WITHMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SB 560-32-07 NOSE GEAR DOORS TORQUE TUBE INSTALLATION INSP/MOD

RECOMMENDED

32SB-07

TOL


1203HRS

COMPLIED WITHMOC :

SB 560-32-09 MLG WHEEL WELL AFT SPAR BOX HYDRAULIC/PNEUMATIC LINES GROMMET REPLACEMENT

RECOMMENDED32SB-09 TOL -25-Feb-1993MTH Complete

1203HRS

COMPLIED WITHMOC :

SB 560-32-10 ANTI-SKID WIRING MODIFICATION

SUPERSEDED

32SB-10

LGB


2448HRS

COMPLIED WITHMOC :

SB 560-32-11 UPLOCK SWITCH COVER MOD

RECOMMENDED

32SB-11

LGB

-28-Aug-1995MTH Complete

2247HRS

COMPLIED WITHMOC :

SB 560-32-15 ANTI-SKID DRIVE CLIP REPLACEMENT

RECOMMENDED

32SB-15

LGB

-01-Dec-1996MTH Complete

2692HRS

COMPLIED WITHMOC :

SB 560-32-16 TRANSMITTAL OF BFGOODRICH SB195-183-32-1, MAIN BRAKE SHUTTLE VALVE IMPROVEMENTS

RECOMMENDED32SB-16 TOL -08-Jan-1998MTH Complete

2999HRS

COMPLIED WITHMOC :

SB 560-32-17 POWER BRAKE HYDRAULIC PUMP SCREW REPLACEMENT

SUPERSEDED

32SB-17

TOL


2999HRS

COMPLIED WITHMOC :

SB 560-32-18 ANTI-SKID SYSTEM DIODE REMOVAL

RECOMMENDED

32SB-18

TOL


3159HRS

COMPLIED WITHMOC :

SB 560-32-19 BRAKE MOTOR COUPLING REPLACEMENT

RECOMMENDED

32SB-19

TOL


3159HRS

COMPLIED WITHMOC :

SB 560-32-20 R1 BRAKE LINE REPLACEMENT

RECOMMENDED

32SB-20 : 560R1

-MTH

MOC :

SB 560-32-22 R3 LANDING GEAR ON GROUND OPERATION AND MODIFICATION

RECOMMENDED

32SB-22 : 560R3

-MTH

MOC :

SB 560-32-31 R1 PARKING BRAKE CABLE REPLACEMENT

OPTIONAL

32SB-31 : 560R1

A/RMTH

MOC :

SB 560-32-39 LANDING GEAR - NLG ACTUATOR REPLACEMENT

MANDATORY

32SB-39

SMF

A/R19-Jul-2009MTH Complete

5308HRS

COMPLIED WITHMOC :

SB 560-32-42 R1 REPLACEMENT OF BLEEDER SCREWS AND FITTINGS WITH BLEEDER PLUGS

RECOMMENDED 6264.27300HRS -74.83

Over Due

MOC :

SB 560-32-42 REPLACEMENT OF BLEEDER SCREWS AND FITTINGS WITH BLEEDER PLUGS

RECOMMENDED -

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SL CIL-32-01 IMPROVED NOSE WHEEL GREASE SEAL

INFORMATIONAL

-

MOC :

SL CIL-32-03 NLG UPLOCK ROLLER BRACKET INSPECTION

RECOMMENDED

MTH

6459.05300HRS 119.95

MOC :

SL CIL-32-04 WIRELESS TIRE PRESSURE MONITORING SYSTEM INSTALLATION

INFORMATIONAL -

MOC :

SL 560-32-08 R1 STRUT EXTENSION INSPECTION AND PISTON UPPER BEARING RETENTION IMPROVEMENT

RECOMMENDED32SL-08 : 560R1 TOL A/R06-Nov-1992MTH Complete

1057HRS

COMPLIED WITHMOC :

SL 560-32-17 BRAKE AND SPOILER/SPEEDBRAKE EXTEND HYDRAULIC LINES(S) ROUTING INSPECTION/MODIFICATION


759HRS

COMPLIED WITHMOC :

SL 560-32-18 NOSE GEAR TRUNNION FINISH INSPECTION/REFINISH

RECOMMENDED

32SL-18

TOL


1057HRS

COMPLIED WITHMOC :

SL 560-32-24 MAIN LANDING GEAR WHEEL WELL BRAKE LINE INSPECTION

MANDATORY32SL-24 LBE A/R13-Jan-1993MTH Complete

1150HRS

COMPLIED WITHMOC :

SL 560-32-25 R1 TEIJIN SEIKI MAIN AND NOSE LANDING GEAR ACTUATOR DOWN AND LOCKED SWITCH INSPECTION/REPLACEMENT

SUPERSEDED32SL-25 : 560R1 TOL A/R03-Sep-1993MTH Complete

1503HRS

COMPLIED WITHMOC :

SL 560-32-29 NOSE LANDING GEAR WHEEL WELL AND TIRE ASSEMBLY AND WIDE DOOR ATTACH HARDWARE INSPECTION/REPLACEMENT

RECOMMENDED32SL-29 LGB -12-Nov-1994MTH Complete

2020HRS

COMPLIED WITHMOC :

SL 560-32-31 MAIN LANDING GEAR EXTEND PNEUMATIC LINE CLEARANCE INSPECTION

SUPERSEDED32SL-31 LGB A/R28-Aug-1995MTH Complete

2247HRS

COMPLIED WITHMOC :

SL 560-32-34 NOSE GEAR STEERING BUNGEE INSPECTION

RECOMMENDED

32SL-34

TOL


3430HRS

COMPLIED WITHMOC :

SL 560-32-40 R1 NOSE LANDING GEAR ICE PROTECTION BOOT INSTALLATION

OPTIONAL32SL-40 : 560R1 -MTH

MOC :

SL 560-32-41 GOODRICH NOSE WHEEL INSPECTION/REPLACEMENT

MANDATORY

32SL-41

SMF


4922HRS

COMPLIED WITHMOC :

SL 560-32-50 LANDING GEAR - EMERGENCY GEAR RELEASE INSPECTION

MANDATORY

32SL-50

SMF

A/R19-Jul-2009MTH Complete

5308HRS

COMPLIED WITHMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SL 560-32-51 LANDING GEAR - UNAPPROVED NOSE LANDING GEAR TIRE INSPECTION

RECOMMENDED A/R

MOC :

SB 560-33-04 R1 LANDING LIGHT BULB PROTECTION

OPTIONAL

33SB-04 : 560R1

LBE


29HRS

COMPLIED WITHMOC :

SB 560-33-06 R1 EXIT SIGN REPLACEMENT

OPTIONAL

33SB-06 : 560R1

*CF

-MTH

MOC :

SB 560-33-07 TAIL FLOODLIGHT INSTALLATION

OPTIONAL

33SB-07

A/RMTH

MOC :

SB 560-33-08 R1 WINGTIP NAV/COLLISION LIGHT MODIFICATION

OPTIONAL

33SB-08 : 560R1

LGB


2020HRS

COMPLIED WITHMOC :

SB 560-33-09 WING TIP LANDING LIGHT INSTALLATION

SUPERSEDED

33SB-09

*CF

A/RMTH

MOC :

SB 560-33-11 LANDING LIGHT CIRCUIT SWITCH MODULE INSTALLATION

OPTIONAL

33SB-11

-MTH

MOC :

SB 560-33-14 TAIL NAVIGATION LIGHT SOCKET MODIFICATION

SUPERSEDED

33SB-14

LGB


2247HRS

COMPLIED WITHMOC :

SB 560-33-15 INDIRECT LIGHTING LAMP AND CONNECTOR UPGRADE

OPTIONAL

33SB-15

-MTH

MOC :

SB 560-33-16 R3 EMERGENCY LIGHTING BATTERY PACK UPGRADE

OPTIONAL

33SB-16 : 560R3

A/RMTH

MOC :

SB 560-33-16 R4 EMERGENCY LIGHTING BATTERY PACK UPGRADE

OPTIONAL

-

MOC :

SB 560-33-22 LIGHTS - LED TAIL POSITION LIGHT INSTALLATION

OPTIONAL

33SB-22

A/RMTH

MOC :

SB 560-33-31 LED TAIL FLOODLIGHT UPGRADE

OPTIONAL

33SB-31

A/RMTH

MOC :

SB 560-33-32 LED REPLACEMENT LIGHT FOR THE BAGGAGE COMPARTMENT

OPTIONAL

A/R

MOC :

SB 560-33-33 R1 LED REPLACEMENT LIGHT FOR THE WING LANDING/TAXI LIGHT ASSEMBLY

OPTIONAL -

MOC :

SB 560-33-35 LED LANDING GEAR INDICATION LIGHT INSTALLATION

OPTIONAL

A/R

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SL CIL-33-01 TRANSMITTAL OF RADIANT POWER CORP. SB-RPC-001, PROCEDURE TO REPLACE OBSOLETE CONNECTOR ASSEMBLY FOR

CBS28 EMERGENCY BATTERY

INFORMATIONAL -

MOC :

SL 560-33-02 R1 CABIN INDIRECT LIGHTING SYSTEM INSPECTION

SUPERSEDED

33SL-02 : 560R1

LGB


2409HRS

COMPLIED WITHMOC :

SL 560-33-02 R2 CABIN INDIRECT LIGHTING SYSTEM INSPECTION

RECOMMENDED

33SL-02 : 560R2

TOL

-06-Jul-1997MTH Complete

2844HRS

COMPLIED WITHMOC :

SL 560-33-05 R1 LANDING LIGHT SWITCH INSPECTION/REPLACEMENT

MANDATORY

33SL-05 : 560R1

TOL


1647HRS

COMPLIED WITHMOC :

SB 560-34-109 5 AMP-HOUR STANDBY GYRO BATTERY INSTALLATION

OPTIONAL

34SB-109

-MTH

MOC :

SB 560-34-112 R3 MARK VIII ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) INSTALLATION


MOC :

SB 560-34-113 R1 NAVIGATION - TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS) II AND HONEYWELL TRANSPONDER UPGRADE FOR

ELEMENTARY SURVEILLANCE


MOC :

SB 560-34-116 TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS) II AND MST-67A TRANSPONDER FOR ELEMENTARY SURVEILLANCE

SUPERSEDED34SB-116 A/RMTH

MOC :

SB 560-34-121 SANDEL ST3400 TAWS INSTALLATION

OPTIONAL

34SB-121

-MTH

MOC :

SB 560-34-143 R1 NAVIGATION - SPEED LIMITATION PLACARD INSTALLATION

MANDATORY34SB-143 : 560R1 MCC A/R15-Jan-2008MTH Complete

5071HRS

COMPLIED WITHMOC :

SB 560-34-156 NAVIGATION - UNIVERSAL SOLID STATE DATA TRANSFER UNIT (SSDTU) UPGRADE

OPTIONAL A/R

MOC :

SB 560-34-23 VN212 SIGNAL GROUND WIRING MODIFICATION

OPTIONAL

34SB-23

-MTH

MOC :

SB 560-34-27 FMS/COMM2 NOISE REDUCTION IMPROVEMENTS

SUPERSEDED

34SB-27

LGB


1794HRS

COMPLIED WITHMOC :

SB 560-34-28 GLOBAL NAVIGATION MANAGEMENT UNIT UPGRADE

OPTIONAL

34SB-28

-MTH

- NOT APPLICABLE-EQUIPMENT NOT INSTALLEDMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SB 560-34-32 GNS-X OFFSET WAYPOINT S/W UPGRADE

RECOMMENDED

34SB-32

TOL


1057HRS

COMPLIED WITHMOC :

SB 560-34-34 MULTIFUNCTION DISPLAY SYMBOL GENERATOR WIRE BUNDLE ROUTING MODIFICATION

OPTIONAL34SB-34 PCT -17-Sep-1998MTH Complete

3288HRS

COMPLIED WITHMOC :

SB 560-34-36 HONEYWELL PRIMUS RADIO RACK COAX CONNECTOR REPLACEMENT

SUPERSEDED34SB-36 LGB A/R12-Nov-1994MTH Complete

2020HRS

COMPLIED WITHMOC :

SB 560-34-37 HONEYWELL PRIMUS RADIO ADF SYSTEM IMPROVEMENTS

RECOMMENDED

34SB-37

LGB


2020HRS

COMPLIED WITHMOC :

SB 560-34-40 R1 P870 RADAR RECEIVER/TRANSMITTER REPLACEMENT (FOR REDUCED COMM RADIO INTERFERENCE)

OPTIONAL34SB-40 : 560R1 VNY -07-Dec-1994MTH Complete

2043HRS

COMPLIED WITHMOC :

SB 560-34-44 KOLLSMAN AIRSPEED INDICATOR SERVICE TEST

OPTIONAL

34SB-44

-MTH

MOC :

SB 560-34-46 HONEYWELL RMU SOFTWARE UPDATE

SUPERSEDED

34SB-46

A/RMTH

MOC :

SB 560-34-50 R1 INTERMITTENT RUDDER KICK CORRECTION MODIFICATION

RECOMMENDED

34SB-50 : 560R1

LGB


2247HRS

COMPLIED WITHMOC :

SB 560-34-54 AIRSPEED INDICATOR WITH OVERSPEED/LOW SPEED WARNING SWITCHES INSTALLATION


MOC :

SB 560-34-59 COPILOT ALTIMETER INSTALLATION - KOLLSMAN

OPTIONAL

34SB-59

-MTH

MOC :

SB 560-34-60 PRIMUS 870 RADAR GERMAN CERTIFICATIOON UPGRADE

OPTIONAL

34SB-60

-MTH

MOC :

SB 560-34-69 R1 SAFE FLIGHT ANGLE-OF-ATTACK COMPUTER MODIFICATION

SUPERSEDED

34SB-69 : 560R1

TOL

A/R05-Jun-1998MTH Complete

3159HRS

COMPLIED WITHMOC :

SB 560-34-70 TELEDYNE ANGLE-OF-ATTACK COMPUTER MODIFICATION

SUPERSEDED

34SB-70

PIT


3296HRS

COMPLIED WITH - NOT APPLICABLE-EQUIPMENT NOT INSTALLEDMOC :

SB 560-34-75 R1 STATIC PORT INSPECTION/MODIFICATION

OPTIONAL

34SB-75 : 560R1

SMF


4685HRS

COMPLIED WITHMOC :

SB 560-34-89 UNS-1K 603.4 SOFTWARE UPGRADE

RECOMMENDED

34SB-89

-MTH

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SB 560-34-97 R1 REDUCED VERTICAL SEPARATION MINIMUM (RVSM) MODIFICATION

OPTIONAL34SB-97 : 560R1 SMF -20-Apr-2005MTH Complete

4685HRS

COMPLIED WITHMOC :

ASL 560-34-21 TRANSMITTAL OF HONEYWELL TECHNICAL NEWSLETTER A23-3850-001

MANDATORY34ASL21 SMF A/R17-Nov-2005MTH Complete

4766HRS

COMPLIED WITHMOC :

ASL 560-34-34 R3 NAVIGATION - STALL WARNING SYSTEM CALIBRATION ADJUSTMENT AND IN-FLIGHT TEST PROCEDURES

SUPERSEDED34ASL-34 : 560R3 SMF A/R25-Jun-2008MTH Complete

5180HRS

COMPLIED WITHMOC :

ASL 560-34-35 R3 NAVIGATION - STALL WARNING SYSTEM CALIBRATION, ADJUSTMENT, AND IN-FLIGHT TEST PROCEDURES

SUPERSEDED34ASL-35 : 560R3 SMF A/R25-Jun-2008MTH N/A

5180HRS

NOT APPLICABLEMOC :

SL CIL-34-02 TRANSMITTAL OF HONEYWELL SIL D201301000032, PRIMUS II INTEGRATED RADIO SYSTEM

MANDATORYSMF -09-Sep-2013MTH Complete

5961.8HRS

5486LDG

COMPLIED WITH - COMPLIED WITH CIL-34-02, BY COMPLYING WITH A MORE COMPREHENSIVE

INSPECTION CRITERIA TO ASSURE COMPLIANCE WITH AD2010-07-02.

MOC :

SL 560-34-06 GNS-X NAV MANAGEMENT UNIT COVER REPLACEMENT

RECOMMENDED

34SL-06

5OL


1203HRS

COMPLIED WITHMOC :

SL 560-34-23 R1 GNS-XL FLIGHT MANAGEMENT SYSTEM (FMS) MOD 4 UPGRADE

RECOMMENDED -

MOC :

SL 560-34-28 HONEYWELL SOFTWARE BULLETIN SWB TPU 67A-SW8

DISCRETIONARY

34SL-28

-MTH

MOC :

SL 560-34-36 NAVIGATION - TRANSMITTAL OF HONEYWELL SWB MST 67A-SW5

RECOMMENDED34SL-36 A/RMTH

MOC :

SB 560-35-01 R4 EROS OXYGEN MASK INSTALLATION

OPTIONAL

35SB-01 : 560R4

LBE

-MTH


SB 560-35-04 CHAFING PROTECTION INSTALLATION OF TAILCONE LINES AND WIRE BUNDLES

RECOMMENDED35SB-04 LGB -18-Mar-1996MTH Complete

2448HRS

COMPLIED WITHMOC :

SB 560-35-09 R1 EROS MLD20-506 OXYGEN MASK INSTALLATION

OPTIONAL

35SB-09 : 560R1

-MTH

MOC :

SB 560-35-12 EROS MLD20-510 OXYGEN MASK INSTALLATION

OPTIONAL

35SB-12

-MTH

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SL 560-35-04 PORTABLE OXYGEN CYLINDER MASK INSPECTION/REPLACEMENT


MOC :

SL 560-35-06 OXYGEN - OXYGEN BOTTLE INSPECTION

INFORMATIONAL

A/RMTH

MOC :

SL 560-35-07 R1 TRANSMITTAL OF INTERTECHNIQUE SERVICE BULLETIN MXH-35-240

MANDATORYKALN -23-May-2012MTH Complete

5743.2HRS

5371LDG

COMPLIED WITH - ACCOMPLISHED THE SL560-35-07REV1 PER THE SL INSTRUCTIONS. THE INSTALLED

CREW O2 MASKS DO NOT APPLY TO THIS SL.

MOC :

SL 560-35-07 R2 OXYGEN - TRANSMITTAL OF INTERTECHNIQUE SERVICE BULLETIN MXH-35-240

MANDATORY -

MOC :

SL 560-35-07 OXYGEN - TRANSMITTAL OF INTERTECHNIQUE SERVICE BULLETIN MXH-35-240

MANDATORY -

MOC :

SB 560-36-01 TAILCONE BLEED AIR CHECK VALVE REPLACEMENT

RECOMMENDED

36SB-01

LGB


1794HRS

COMPLIED WITHMOC :

SB 560-36-02 R1 DOOR SEAL VALVE REPLACEMENT AND WATER TRAP INSTALLATION


MOC :

SB 560-36-03 R3 PNEUMATIC - WIDE CARGO DOOR SEAL LINE WATER TRAP INSTALLATION


MOC :

SB 560-52-02 ENTRY DOOR STEP CATCH COVER (W/STD DOOR & STEP INSTL)

RECOMMENDED52SB-02 TOL -03-Sep-1993MTH Complete

1503HRS

COMPLIED WITHMOC :

SB 560-52-04 R1 WIDE DOOR MODIFICATION INSTALLATION

OPTIONAL

52SB-04 : 560R1

-MTH

MOC :

SB 560-52-04 R2 WIDE DOOR MODIFICATION INSTALLATION

OPTIONAL

-

MOC :

SB 560-52-08 R4 COMPOSITE DOOR STEP INSTALLATION

OPTIONAL

-

MOC :

SB 560-52-18 INSTALLATION OF NOSE LANDING GEAR DOOR DEFLECTORS

OPTIONAL

52SB-18

-MTH

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

ASL 560-52-05 DOORS - EMERGENCY EXIT INSPECTION

MANDATORY

SMF

A/R04-Mar-2011DAYS Complete

5568.6HRS

5282LDG

COMPLIED WITH - COMPLIED WITH ASL560-52-05 BY INSPECTING THE EMERGENCY EXIT SEAL PER

ACCOMPLISHMENT INSTRUCTIONS. NO DEFECTS NOTED.

MOC :

SL 560-52-01 CABIN DOOR SECONDARY SEAL FUNCTIONAL CHECK

RECOMMENDED

52SL-01

TOL

A/R29-May-1992MTH Complete

759HRS

COMPLIED WITHMOC :

SL 560-52-02 EMERGENCY EXIT INNER HANDLE ATTACH SCREW INSPECTION/REPLACEMENT

MANDATORY52SL-02 LBE -14-Apr-1992MTH Complete

683HRS

COMPLIED WITHMOC :

SB 560-53-07 R1 TAILCONE BALLAST INSTALLATION

SUPERSEDED

53SB-07 : 560R1

A/RMTH

MOC :

SB 560-53-11 FRAME BRACE INSPECTION/INSTALLATION

SUPERSEDED

53SB-11

TOL


1203HRS

COMPLIED WITHMOC :

SB 560-53-12 W/S CANTED FRAME & UPPER STRINGER INSP/MOD

MANDATORY

53SB-12

TOL


1203HRS

COMPLIED WITHMOC :

SB 560-53-14 CABIN INTERIOR ATTACH/CONTACT POINT CORROSION PROTECTION

SUPERSEDED53SB-14 5OL A/R25-Feb-1993MTH Complete

1203HRS

COMPLIED WITHMOC :

SB 560-53-15 FLIGHT CREW SEAT RAIL AND BEAM RIVET INSPECTION/INSTALLATION

SUPERSEDED53SB-15 LGB A/R06-Apr-1994MTH Complete

1794HRS

COMPLIED WITHMOC :

SB 560-53-16 MAP COMPARTMENT ASSEMBLY INSPECTION/REPLACEMENT

RECOMMENDED

53SB-16

VNY


2104HRS

COMPLIED WITHMOC :

SB 560-53-18 DORSAL FIN INSTALLATION AND MATERIAL IMPROVEMENT

OPTIONAL

53SB-18

-MTH

MOC :

SB 560-53-20 AN3-5A BOLT INSPECTION/REPLACEMENT

RECOMMENDED

53SB-20

TOL


3430HRS

COMPLIED WITHMOC :

SB 560-53-21 R1 COCKPIT LEFT SIDE WINDOW RIVET INSPECTION

SUPERSEDED

53SB-21 : 560R1

TOL


3159HRS

COMPLIED WITHMOC :

SB 560-53-21 R2 COCKPIT LEFT SIDE WINDOW RIVET INSPECTION

RECOMMENDED

53SB-21 : 560R2

TOL


3430HRS

COMPLIED WITHMOC :

SB 560-53-23 R1 WING MAIN SPAR CARRY THRU LUGS INSPECTION/REPAIR

RECOMMENDED

53SB-23 : 560R1

TOL


3430HRS

COMPLIED WITHMOC :

SB 560-53-25 TAILCONE BAGGAGE COMPARTMENT SUPPORT IMPROVEMENT

SUPERSEDED

53SB-25

TOL


3159HRS

COMPLIED WITHMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SB 560-53-26 R1 LOWER STUB WING SKIN INSPECTION/REPAIR

SUPERSEDED

53SB-26 : 560R1

TOL


3608HRS

COMPLIED WITHMOC :

SB 560-53-26 R2 LOWER STUB WING SKIN INSPECTION/REPAIR

RECOMMENDED

53SB-26 : 560R2

-MTH

MOC :

SB 560-53-27 CABIN ENTRANCE AFT DOORPOST INSPECTION/REPAIR

RECOMMENDED

53SB-27

MHR


4056HRS

COMPLIED WITHMOC :

SB 560-53-28 FUSELAGE MOISTURE DRAIN INSTALLATION

OPTIONAL

53SB-28

-MTH

MOC :

SB 560-53-29 R2 NOSE WHEEL STEERING BRACKET REPLACEMENT

MANDATORY

53SB-29 : 560R2

MHR


4056HRS

COMPLIED WITHMOC :

SB 560-53-29 NOSE WHEEL STEERING BRACKET REPLACEMENT

SUPERSEDED

53SB-29

SMF


3718HRS

COMPLIED WITHMOC :

SB 560-53-34 WHEEL WELL BOX/SKIN GAP IMPROVEMENT

OPTIONAL

53SB-34

-MTH

MOC :

SL 560-53-05 DORSAL FIN VANE INSPECTION

RECOMMENDED

53SL-05

-MTH

MOC :

SL 560-53-06 R1 INTERCOSTAL DRAINAGE PATH INSPECTION

RECOMMENDED

53SL-06 : 560R1

A/RMTH

MOC :

SB 560-54-01 R1 NEW DESIGN INLET INSTALLATION

SUPERSEDED

54SB-01 : 560R1

TOL


3430HRS

COMPLIED WITHMOC :

SB 560-54-03 R2 ENGINE INLET DOUBLER INSTALLATION

RECOMMENDED

54SB-03 : 560R2

-MTH

MOC :

SB 560-55-04 STABILIZERS - ELEVATOR TIP BONDING STRIP INSTALLATION

DISCRETIONARY55SB-04 A/RMTH

MOC :

SL 560-55-02 HORIZONTAL STABILIZER ATTACH BOLT/NUT TORQUE VERIFICATION

RECOMMENDED55SL-02 TOL A/R05-Jun-1998MTH Complete

3159HRS

COMPLIED WITHMOC :

SL 560-55-03 R1 STABILIZERS - HORIZONTAL STABILIZER RIB BORESCOPE INSPECTION

MANDATORYSMF -22-May-2015MTH Complete

6283.9HRS

5674LDG

COMPLIED WITH - COMPLIED WITH SL560-55-03 R1, ACCOMPLISHEMENT OF TASK 55-10-01-290 PER

INSTRUCTIONS

MOC :

SL 560-55-03 R2 HORIZONTAL STABILIZER RIB BORESCOPE INSPECTION

MANDATORY

-MTH

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SL 560-55-03 HORIZONTAL STABILIZER RIB BORESCOPE INSPECTION

MANDATORY

-MTH

MOC :

SB 560-57-02 R1 WINGS - STUB WING FASTENER INSPECTION/INSTALLATION

SUPERSEDED57SB-02 : 560R1 TOL A/R29-May-1992MTH Complete

759HRS

COMPLIED WITHMOC :

SB 560-57-03 R1 OUTBOARD FLAP ISLAND DOUBLER INSTALLATION

SUPERSEDED

57SB-03 : 560R1

LGB


2020HRS

COMPLIED WITHMOC :

SB 560-57-07 FLAP VENT HOLES INSTALL

RECOMMENDED

57SB-07

LNK


2553HRS

COMPLIED WITHMOC :

SL 560-57-01 R1 NOTIFICATION OF LEADING EDGE SKIN REWORK REQUIREMENT WHEN A DEICE BOOT IS REMOVED

MANDATORYKALN -23-May-2012MTH Complete

5743.2HRS

5371LDG

COMPLIED WITH - ACCOMPLISHED THE SL560-57-01REV1 TO THE LH & RH WING STATION 91 PER THE

SRM INSTRUCTIONS.

MOC :

ASL 560-30-07 APPROACH AND LANDING IN ICING CONDITIONS ADDITION TO FLIGHT MANUAL

SUPERSEDED30SLA07 PIT A/R22-Aug-1997MTH Complete

2879HRS

COMPLIED WITHMOC :

SB 560-71-03 LOWER COWL DOOR FIRESEAL INSPECTION/INSTALLATION

SUPERSEDED

71SB-03

LGB

A/R01-Dec-1996MTH Complete

2692HRS

COMPLIED WITHMOC :

SL 560-71-03 REPLACEMENT OF FUEL CONTROL UNIT IDLE SOLENOID

SUPERSEDED

71SL-03

BTV


898HRS

COMPLIED WITHMOC :

SB 560-72-01 R3 ENGINE COWLING MODIFICATION TO ACCOMODATE PRATT & WHITNEY CANADA ENGINE FUEL ACCUMULATOR INSTALLATION

RECOMMENDED72SB-01 : 560R3 TOL -14-Mar-1999MTH Complete

3430HRS

COMPLIED WITHMOC :

SL 560-72-05 R1 TRANSMITTAL OF P&WC SB JT15D-72-7458, REVISION 3, INSPECTION OF FCU - MINIMUM FUEL FLOW, AND SERVICE LETTER

7077 JT15D-012, FCU METERING VALVE (SB7458) CLARIFICATION

SUPERSEDED72SL-05 : 560R1 TOL A/R06-Jul-1997MTH Complete

2844HRS

COMPLIED WITHMOC :

SL 560-72-11 TRANSMITTAL OF P&WC SB JT15D-72-7495 TURBOFAN ENGINE - FUEL CONTROL UNIT - INSPECTION OF DECEL SCHEDULE

INFORMATIONAL72SL-11 TOL A/R05-Jun-1998MTH Complete

3159HRS

COMPLIED WITHMOC :

SL 560-72-16 TRANSMITTAL OF P&WC SERVICE LETTER JT15D-023

RECOMMENDED

72SL-16

PIT


3514HRS

COMPLIED WITHMOC :

SB JT15D-72-7001

R25

APPROVED LISTING OF (SYNTHETIC) LUBRICATING OILS

RECOMMENDED

E1

-

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SB JT15D-72-7001

R25

APPROVED LISTING OF (SYNTHETIC) LUBRICATING OILS

RECOMMENDED

E2

-

MOC :

SB JT15D-72-7002

R42

SERVICE LIVES - ROTOR COMPONENTS

E1

A/R

MOC :

SB JT15D-72-7002

R42

SERVICE LIVES - ROTOR COMPONENTS

E2

A/R

MOC :

SB JT15D-72-7003

R35

ENGINE OPERATING TIME BETWEEN OVERHAULS AND HOT SECTION INSPECTION FREQUENCY

RECOMMENDED

E1

-

MOC :

SB JT15D-72-7003

R35


RECOMMENDED

E2

-

MOC :

SB JT15D-72-7003

R36


RECOMMENDED

E1

-

MOC :

SB JT15D-72-7003

R36


RECOMMENDED

E2

-

MOC :

SB JT15D-72-7003

R37


RECOMMENDED

E1

-

MOC :

SB JT15D-72-7003

R37


RECOMMENDED

E2

-

MOC :

SB JT15D-72-7003

R38


RECOMMENDED

E1

-

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SB JT15D-72-7003

R38


RECOMMENDED

E2

-

MOC :

SB JT15D-72-7144

R20

ENGINE FUELS AND ADDITIVES - REQUIREMENTS AND APPROVED LISTING

RECOMMENDED

E1

-

MOC :

SB JT15D-72-7144

R20

ENGINE FUELS AND ADDITIVES - REQUIREMENTS AND APPROVED LISTING

RECOMMENDED

E2

-

MOC :

SB JT15D-72-7315

R1

TURBINE SHAFT LOCKING BOLT - REPLACEMENT/MODIFICATION OF

RECOMMENDED

E1

A/R

MOC :

SB JT15D-72-7315

R1

TURBINE SHAFT LOCKING BOLT - REPLACEMENT/MODIFICATION OF

RECOMMENDED

E2

A/R

MOC :

SB JT15D-72-7369

R2

LOW COMPRESSOR STATOR/CASE ASSEMBLY - IMPROVED RETENTION

RECOMMENDED

E1

A/R

MOC :

SB JT15D-72-7369

R2

LOW COMPRESSOR STATOR/CASE ASSEMBLY - IMPROVED RETENTION

RECOMMENDED

E2

A/R

MOC :

SB JT15D-72-7459

R1

REPLACEMENT OF IGNITER

OPTIONAL

E1

A/R

MOC :

SB JT15D-72-7459

R1


OPTIONAL

E2

A/R

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SB JT15D-72-7493

R4

MODIFICATION/REPLACEMENT OF FUEL NOZZLE (SUPERSEDED BY SB JT15D-72-7526 R3)

CATEGORY 8

E1

-

MOC :

SB JT15D-72-7493

R4

MODIFICATION/REPLACEMENT OF FUEL NOZZLE (SUPERSEDED BY SB JT15D-72-7526 R3)

CATEGORY 8

E2

-

MOC :

SB JT15D-72-7493

R5

MODIFICATION / REPLACEMENT OF FUEL NOZZLE (SUPERSEDED BY SB JT15D-72-7526 R3)

CATEGORY 8

E1

-

MOC :

SB JT15D-72-7493

R5

MODIFICATION / REPLACEMENT OF FUEL NOZZLE (SUPERSEDED BY SB JT15D-72-7526 R3)

CATEGORY 8

E2

-

MOC :

SB JT15D-72-7526

R2

MODIFICATION/REPLACEMENT OF FUEL NOZZLES

CATEGORY 7

E1

-

MOC :

SB JT15D-72-7526

R2

MODIFICATION/REPLACEMENT OF FUEL NOZZLES

CATEGORY 7

E2

-

MOC :

SB JT15D-72-7526

R3

MODIFICATION / REPLACEMENT OF FUEL NOZZLES

CATEGORY 7

E1

-

MOC :

SB JT15D-72-7526

R3

MODIFICATION / REPLACEMENT OF FUEL NOZZLES

CATEGORY 7

E2

-

MOC :

SB JT15D-72-7571

R2

NEW LOW TURBINE DISC ASSEMBLY - INTRODUCTION OF

INFORMATIONAL

E1

A/R

MOC :

SB JT15D-72-7571

R2

NEW LOW TURBINE DISC ASSEMBLY - INTRODUCTION OF

INFORMATIONAL

E2

A/R

MOC :

SB JT15D-72-7588

R2

REPLACEMENT/MODIFICATION OF ACCESSORY GEARBOX INPUT DRIVE GEAR

OPTIONAL

E1

-

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SB JT15D-72-7588

R2

REPLACEMENT/MODIFICATION OF ACCESSORY GEARBOX INPUT DRIVE GEAR

OPTIONAL

E2

-

MOC :

SB JT15D-72-7625

R1

REPLACEMENT OF GASKET

RECOMMENDED

E1

A/R

MOC :

SB JT15D-72-7625

R1

REPLACEMENT OF GASKET

RECOMMENDED

E2

A/R

MOC :

SB JT15D-72-7625 REPLACEMENT OF GASKET

RECOMMENDED

E1

A/R

MOC :

SB JT15D-72-7625 REPLACEMENT OF GASKET

RECOMMENDED

E2

A/R

MOC :

SB JT15D-72-7627 REPLACEMENT OF LOW PRESSURE TURBINE INTERSTAGE ROTOR AIR SEAL AND ROTOR AIR SEAL

RECOMMENDEDE1 -

MOC :

SB JT15D-72-7627 REPLACEMENT OF LOW PRESSURE TURBINE INTERSTAGE ROTOR AIR SEAL AND ROTOR AIR SEAL

RECOMMENDEDE2 -

MOC :

SB JT15D-72-7628

R1

REPLACEMENT/MODIFICATION OF GAS GENERATOR CASE ASSEMBLY

CATEGORY 6

E1

-

MOC :

SB JT15D-72-7628

R1


CATEGORY 6

E2

-

MOC :

SB JT15D-72-7628

R2


CATEGORY 6

E1

-

MOC :

SB JT15D-72-7628

R2


CATEGORY 6

E2

-

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SB JT15D-72-7628

R3


CATEGORY 6

E1

-

MOC :

SB JT15D-72-7628

R3


CATEGORY 6

E2

-

MOC :

SB JT15D-72-7628 REPLACEMENT/MODIFICATION OF GAS GENERATOR CASE ASSEMBLY

E1 -

MOC :

SB JT15D-72-7628 REPLACEMENT/MODIFICATION OF GAS GENERATOR CASE ASSEMBLY

E2 -

MOC :

SB JT15D-72-7630 INSPECTION/REPLACEMENT OF FUEL COOLED OIL COOLER

E1

SMF

-09-Oct-2014MTH N/A

6147.1HRS

5586LDG

NOT APPLICABLE - COMPLIED WITH PWCSB72-7630 FUEL COOLED OIL COOLER INSPECTION AND

FOUND TO NOT BE APPLICABLE BY PART NUMBER.

MOC :

SB JT15D-72-7630 INSPECTION/REPLACEMENT OF FUEL COOLED OIL COOLER

E2

SMF

-09-Oct-2014MTH N/A

6147.1HRS

5586LDG

NOT APPLICABLE - COMPLIED WITH PWCSB72-7630 FUEL COOLED OIL COOLER INSPECTION AND

FOUND TO NOT BE APPLICABLE BY PART NUMBER.

MOC :

SB JT15D-72-7634 REPLACEMENT OF SHIPPING CAPS FOR SHIPPING CONTAINERS

CATEGORY 3E1 -

MOC :

SB JT15D-72-7634 REPLACEMENT OF SHIPPING CAPS FOR SHIPPING CONTAINERS

CATEGORY 3E2 -

MOC :

SL 560-73-03 FLOW DIVIDER START VALVE REPLACEMENT

RECOMMENDED

73SL-03

LBE


1150HRS

COMPLIED WITHMOC :

SL 560-73-04 TRANSMITTAL OF PRATT & WHITNEY CANADA SERVICE INFORMATION LETTER SIL 7067 FLOW DIVIDER VALVE

RECOMMENDED73SL-04 VNY A/R22-Jun-1994MTH Complete

1871HRS

COMPLIED WITHMOC :

SL 560-73-05 TRANSMITTAL OF PRATT & WHITNEY CANADA SERVICE BULLLETIN JT15D-72-7467 FLOW DIVIDER VALVE -

REPLACEMENT/MODIFICATION OF

RECOMMENDED73SL-05 LGB A/R05-Jun-1996MTH Complete

2540HRS

COMPLIED WITHMOC :

SL 560-73-06 SIL JT15D-021 AND SB JT15D-72-7561

RECOMMENDED

73SL-06

PIT


3514HRS

COMPLIED WITHMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SLA 560-73-02 R1 FLOW DIVIDER DIAPHRAGM

MANDATORY

73SLA02 : 560R1

LBE


1067HRS

COMPLIED WITHMOC :

SL CIL-74-01 R1 INSPECTION OF IGNITION CABLE AND THROTTLE LINKAGE

MANDATORY

SMF

-09-Sep-2013DAYS Complete

5961.8HRS

5486LDG

COMPLIED WITH - COMPLIED WITH SL CIL-74-01 R1, BY VISUAL INSPECTION OF THE IGNITION LEAD

ELBOW POSITION AND MAKE CORRECTION AS NESSARY PER ACCOMPLISHMENT INSTRUCTIONS.

OPERATIONAL CHECK NORMAL.

MOC :

SL CIL-74-01 INSPECTION OF IGNITION CABLE AND THROTTLE LINKAGE

MANDATORY

-DAYS

MOC :

SL 560-74-02 P&W SB 7567R1

RECOMMENDED

74SL-02

-MTH

MOC :

SB JT15D-72-7459

R2


OPTIONAL

E1

A/R

MOC :

SB JT15D-72-7459

R2


OPTIONAL

E2

A/R

MOC :

SB 560-76-01 R2 ENGINE SYNCHRONIZER CONTROLLER MODIFICATION

RECOMMENDED

76SB-01 : 560R2

-MTH

MOC :

SB 560-78-02 THRUST REVERSER THROTTLE LOAD LIMITER MODIFICATION

RECOMMENDED78SB-02 TOL -30-Oct-1991MTH Complete

451HRS

COMPLIED WITHMOC :

SB 560-78-03 UPPER THRUST REVERSER DOOR MODIFICATION

RECOMMENDED

78SB-03

VNY


2104HRS

COMPLIED WITHMOC :

SB 560-78-04 THRUST REVERSER THROTTLE STOP SOLENOID GROUND IMPROVEMENT


MOC :

SL 560-78-01 R2 THRUST REVERSER SYSTEM OPERATIONAL TEST

RECOMMENDED

78SL-01 : 560R2

LGB


2409HRS

COMPLIED WITHMOC :

SL 560-78-03 THRUST REVERSER STANG FAIRING SUPPORT FORMER REPLACEMENT

RECOMMENDED78SL-03 TOL A/R15-Dec-1993MTH Complete

1647HRS

COMPLIED WITHMOC :

SL 560-78-04 EXHAUST NOZZLE I. D. INSPECTION/REPLACEMENT

SUPERSEDED

78SL-04

LGB


2020HRS

COMPLIED WITHMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains

Service Bulletins

Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

SL 560-78-06 TRANSMITTAL OF NORDAM CITV 78-2, EXHAUST - THRUST REVERSER - REPLACEMENT OF THRUST REVERSER STANG

FAIRING SUPPORT FORMER

SUPERSEDED78SL-06 SMF A/R25-Jun-2001MTH Complete

3926HRS

COMPLIED WITHMOC :

SB 560-79-01 OIL TEMPERATURE PROBE REPLACEMENT

SUPERSEDED

79SB-01

TOL

A/R15-Dec-1993MTH Complete

1647HRS

COMPLIED WITHMOC :

SB 560-80-03 R2 APC P/N 9912125-2 STARTER/GENERATOR INSPECTION/REPLACEMENT

RECOMMENDED80SB-03 : 560R2 TOL -05-Jun-1998MTH Complete

3159HRS

COMPLIED WITHMOC :

SB 560-80-04 REPLACEMENT OF SUPPRESSION DIODE WITH TRANSZORB

OPTIONAL

80SB-04

-MTH

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015

Part Number

Part Serial No



Remains

RemainsTSO 2

TSO 1

Airworthiness Directives

(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

FAA 1996-24-06 ICING COND ADDITION TO FM

SUPERSEDED

30AD-01

PIT


2879HRS

COMPLIED WITHMOC :

FAA 1997-05-03 APPLIANCE AD - GNS-XLS AND GNS-XL GPS

SUPERSEDED

34AD-07

TOL


2844HRS

COMPLIED WITH - NOT APPLICABLE-EQUIPMENT NOT INSTALLEDMOC :

FAA 1998-04-38 SEVERE ICING PROCEDURES

MANDATORY

30AD-02

PIT


3086HRS

COMPLIED WITHMOC :

FAA 1998-25-10 APPLIANCE AD - AIRCRAFT BELTS, INC.

SUPERSEDED

25AD-02

TOL


3430HRS

COMPLIED WITHMOC :

FAA 1999-08-21 APPLIANCE AD - PURITAN-BENNETT AERO SYSTEM CO

MANDATORY

35AD-03

PIT


3514HRS

COMPLIED WITH - NOT APPLICABLE BY TYPE MANUFACTURERMOC :

FAA 2000-03-09 ICING COND FM INFORMATION

MANDATORY

34AD-09

MHR


3836HRS

COMPLIED WITHMOC :

FAA 2006-04-10 THIS AD REQUIRES INSTALLING IDENTIFICATION SLEEVES ON THE WIRES FOR THE POSITIVE AND NEGATIVE STUDS OF THE

ENGINE AND/ OR (APU) FIRE EXTINGUISHING BOTTLES, AS APPICABLE, AND RECONNECTING THE WIRES TO THE CORRECT

TERMINAL STUDS.

MANDATORY26AD-02 SMF -09-Feb-2007MTH Complete

4922HRS

COMPLIED WITHMOC :

FAA 2006-06-03 PREVENT FUEL VAPOR IGNITION

MANDATORY

28AD-01

SMF


4922HRS

COMPLIED WITHMOC :

FAA 2006-16-18 APPLIANCE AD - SANDEL AVIONICS INCORPORATED MODEL ST3400 TERRAIN AWARENESS WARNING SYSTEM/RADIO

MAGNETIC INDICATOR(TAWS/RMI)

MANDATORY34AD-16 SMF A/R09-Feb-2007MTH N/A

4922HRS

NOT APPLICABLEMOC :

FAA 2006-19-04

PARA(F)

REVISE HONEYWELL RCZ-833J/K, -851J/K AND 854J COMMUNICATION (COM) UNITS, EQUIPPED WITH XS-852E/F MODE S

TRANSPONDERS; AND HONEYWELL XS-856A/B AND -857A MODE S TRANSPONDERS AIRPLANE FLIGHT MANUAL (AFM)

MANDATORY

34AD-17

A/R09-Feb-2007MTH N/A

4922HRS

NOT APPLICABLEMOC :

FAA 1995-25-10 OUTFLOW AND SAFETY VALUES

MANDATORY

21AD-01

LNK


2553HRS

COMPLIED WITH - NOT APPLICABLE BY COMPONENT SERIAL NUMBER.MOC :

FAA 2013-09-11 (G) AIR CONDITIONING - REPLACEMENT OF THE BRUSHES ON A/C COMPRESSOR MOTORS, PART NOS. 1134104-1/1134104-5, OR

DEACTIVATION OF THE A/C SYSTEM INSPECTION FOR PART NUMBER (P/N)

MANDATORY

SMF -09-Sep-2013DAYS N/A

5961.8HRS

5486LDG

NOT APPLICABLE - COMPLIED WITH AD2013-09-11, EFFECTIVE DATE JULY 5, 2013, BY INSPECTION OF

THE A/C COMPRESSOR MOTOR AND DETERMINED PART NUMBER INSTALLED IS NOT APPLICABLE AS

PER PARAGRAPH (G) OF THIS

AD. NO FURTHER ACTION REQUIRED

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains


Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

FAA 2013-09-11 (H) AIR CONDITIONING - REPLACEMENT OF THE BRUSHES ON A/C COMPRESSOR MOTORS, PART NOS. 1134104-1/1134104-5, OR

DEACTIVATION OF THE A/C SYSTEM INSPECTION A\C COMPRESSOR HOUR METER AND MAINTENANCE RECORDS

MANDATORY


5961.8HRS

5486LDG





MOC :

FAA 2013-09-11 (I) &

(J)

AIR CONDITIONING - REPLACEMENT OF THE BRUSHES ON A/C COMPRESSOR MOTORS, PART NOS. 1134104-1/1134104-5, OR

DEACTIVATION OF THE A/C SYSTEM REPLACEMENT OF A/C COMPRESSOR MOTOR BRUSHES AND RELATED MAINTENANCE

MANUAL INFORMATION

MANDATORY

SMF -09-Sep-2013MTH N/A

5961.8HRS

5486LDG

NOT APPLICABLEMOC :

FAA 2013-09-11 (K) AIR CONDITIONING - REPLACEMENT OF THE BRUSHES ON A/C COMPRESSOR MOTORS, PART NOS. 1134104-1/1134104-5, OR

DEACTIVATION OF THE A/C SYSTEM DEACTIVATION OF A/C SYSTEM

MANDATORY

SMF A/R09-Sep-2013MTH N/A

5961.8HRS

5486LDG

NOT APPLICABLEMOC :

FAA 2013-09-11 (L) AIR CONDITIONING - REPLACEMENT OF THE BRUSHES ON A/C COMPRESSOR MOTORS, PART NOS. 1134104-1/1134104-5, OR

DEACTIVATION OF THE A/C SYSTEM REACTIVATION OF A/C SYSTEM

MANDATORY

SMF A/R09-Sep-2013MTH N/A

5961.8HRS

5486LDG

NOT APPLICABLEMOC :

FAA 2013-09-11 (M) AIR CONDITIONING - REPLACEMENT OF THE BRUSHES ON A/C COMPRESSOR MOTORS, PART NOS. 1134104-1/1134104-5, OR

DEACTIVATION OF THE A/C SYSTEM PARTS RETURN AND REPORTING REQUIREMENTS

MANDATORY


5961.8HRS

5486LDG

NOT APPLICABLEMOC :

FAA 2013-09-11 AIR CONDITIONING - REPLACEMENT OF THE BRUSHES ON A/C COMPRESSOR MOTORS, PART NOS. 1134104-1/1134104-5, OR

DEACTIVATION OF THE A/C SYSTEM

MANDATORYSMF -09-Sep-2013MTH N/A

5961.8HRS

5486LDG





MOC :

FAA 2015-17-12

PARA (G)

INSPECT THE A/C COMPRESSOR MOTOR TO DETERMINE WHETHER P/N FWA1134104-1 OR P/N FWA1134104-5 IS INSTALLED

MANDATORY

29-Oct-201530DAYS New Req

6361.410HRS

MOC :

FAA 2015-17-12

PARA (H)

DETERMINE THE HOUR READING ON THE A/C COMPRESSOR HOUR METER (IF, DURING THE INSPECTION REQUIRED BY PARA

(G) OF THIS AD, ANY A/C COMPRESSOR MOTOR HAVING P/N FWA1134104-1 OR P/N FWA1134104-5 IS FOUND

MANDATORY


6361.410HRS

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains


Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

FAA 2015-17-12

PARA (I)

REPLACE THE A/C COMPRESSOR MOTOR BRUSHES WITH NEW BRUSHES (USING THE HOUR READING ON THE A/C

COMPRESSOR HOUR METER DETERMINED IN PARA (H) OF THIS AD)

MANDATORY

BF/FMTH New Req

BF/F

MOC :

FAA 2015-17-12

PARA (K)

DEACTIVATE THE A/C SYSTEM (IN LIEU OF REPLACING THE A/C COMPRESSOR MOTOR BRUSHES AS REQUIRED BY THIS AD)

MANDATORY

-

MOC :

FAA 2015-17-12

PARA (L)

IF THE A/C SYSTEM IS DEACTIVATED, AS SPECIFIED IN PARA (K), PRIOR TO THE A/C SYSTEM BEING REACTIVATED: PERFORM

THE INSPECTION SPECIFIED IN PARA (H), AND DO THE REPLACEMENTS SPECIFIED IN PARA (I), AT THE TIMES SPECIFIED IN

PARA (I). RETURN THE A/C SYSTEM TO SERVICE

MANDATORY

-

MOC :

FAA 2015-17-12

PARA (M)

SEND THE REMOVED BRUSHES TO CESSNA AIRCRAFT COMPANY

MANDATORY


MOC :

FAA 2015-17-12 AIR CONDITIONING - INSPECTIONS TO DETERMINE IF CERTAIN A/C COMPRESSOR MOTORS ARE INSTALLED AND TO

DETERMINE THE ACCUMULATED HOURS ON CERTAIN A/C COMPRESSOR MOTOR ASSEMBLIES; AND REPETITIVE

REPLACEMENT OF THE BRUSHES IN THE A/C COMPRESSOR MOTOR ASSEMBLY, OR, AS AN OPTION TO THE BRUSH

REPLACEMENT, DEACTIVATION OF THE A/C SYSTEM AND PLACARD INSTALLATION; AND RETURN OF REPLACED BRUSHES TO

CESSNA

MANDATORY -MTH New Req

MOC :

FAA 1995-22-01 APPLIANCE AD - TO PREVENT SMOKE, FIRE, ELECTRICAL SHOCK AND POSSIBLE ELECTROMAGNETIC INTERFERENCE

CAUSED BY HIGH VOLTAGE ARCING

MANDATORY33AD-03 SMF A/R17-Nov-2005MTH Complete

4766HRS

COMPLIED WITHMOC :

FAA 1974-08-09 R3 LAVATORY PAPER OR LINEN WASTE RECEPTACLE FIRE PREVENTION

MANDATORY -

MOC :

FAA 2015-10-02 (G) GENERAL VISUAL INSPECTION FOR CRACKING OF SEAT BACKREST LINKS HAVING PART NUMBER (P/N) 90-000200-104-1, P/N

90-000200-104-2, P/N 90-000202-104-1 AND P/N 90-000202-104-2

MANDATORY

-

MOC :

FAA 2015-10-02 (H) CORRECTIVE ACTIONS - CRACKING IS FOUND ON THE LINK

MANDATORY

-

MOC :

FAA 2015-10-02 (I) REPLACE ALL SEAT BACKREST LINKS, HAVING P/N 90-000200-104-1, P/N 90-000200-104-2, P/N 90-000202-104-1 AND P/N

90-000202-104-2, WITH NEW LINKS

MANDATORY

-

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains


Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

FAA 2015-10-02 APPLIANCE AD - EQUIPMENT/FURNISHINGS - ZODIAC SEATS FRANCE - INSPECTION/REPLACEMENT

MANDATORY -MTH

MOC :

FAA 2007-11-17 IDENTIFY WIRES FOR FIRE EXTINGUISHING BOTTLES

MANDATORY

26AD-03

SMF


5180HRS

COMPLIED WITHMOC :

FAA 2010-04-16 (G) REPLACE TYPE H1-10 AIR HALON 1211 (BCF) PORTABLE FIRE EXTINGUISHERSMANUFACTURED BY SICLI WITH SERVICABLE

UNIT

MANDATORY

26AD-07

A/R09-Jul-2010DAYS N/A

5437.2HRS

5216LDG

NOT APPLICABLE - COMMENTS: COMPLIED WITH AD2010-01-16, EFFECTIVE DATE MARCH 8, 2010 BY

INSPECTION. PORTABLE FIRE EXTINGUISHERS ON BOARD AIRCRAFT NOT AFFECTED BY THIS AD DUE

TO MANUFACTURE AND MODEL TYPE. NO

FURTHER ACTION REQUIRED.

MOC :

FAA 2010-04-16 APPLIANCE AD - TYPE H1-10 AIR HALON 1211 (BCF) PORTABLE FIRE EXTINGUISHERSMANUFACTURED BY SICLI

MANDATORY26AD-07 SMF A/R09-Jul-2010DAYS N/A

5437.2HRS

5216LDG

NOT APPLICABLE - COMMENTS: COMPLIED WITH AD2010-01-16, EFFECTIVE DATE MARCH 8, 2010 BY

INSPECTION. PORTABLE FIRE EXTINGUISHERS ON BOARD AIRCRAFT NOT AFFECTED BY THIS AD DUE

TO MANUFACTURE AND MODEL TYPE. NO

FURTHER ACTION REQUIRED.

MOC :

FAA 2007-23-13 INSPECT - ADJUSTMENT OF STALL WARNING SYSTEM

SUPERSEDED

34AD-19

SMF


5180HRS

COMPLIED WITHMOC :

FAA 2008-26-04 INSTALL WARNING PLACARDS, PERFORM FUNCTIONAL TEST OF ANGLE OF ATTACK SYSTEM AND ADJUST CALIBRATION

SETTINGS OF AOA SYSTEM AS REQUIRED.

AIRWORTHINESS34AD-24 SMF A/R06-Feb-2009MTH Complete

5261HRS

COMPLIED WITHMOC :

FAA 1994-01-04 APPLIANCE AD - TO PREVENT COLLISIONS OR NEAR MISSES

MANDATORY34AD-03 LGB A/R10-Sep-1994MTH Complete

1953HRS

COMPLIED WITHMOC :

FAA 1998-25-02 APPLIANCE AD - TO PREVENT THE DISPLAY OF TARGET INDICATORS ON THE WRONG SIDE OF THE AIRCRAFT CAUSED BY

AN INTERNAL COMPONENT FAILURE IN THE SKY497 INSTALLATIONS

MANDATORY34AD-08 TOL A/R14-Mar-1999MTH Complete

3430HRS

COMPLIED WITHMOC :

FAA 2001-23-17 APPLIANCE AD - TO PREVENT INACCURATE COURSE DEVIATION DISPLAYS IN THE GNS 430 UNIT

MANDATORY34AD-10 SAC A/R28-Jun-2004MTH Complete

4560HRS


FAA 2003-04-06 APPLIANCE AD - HONEYWELL PRIMUS RNZ-850/851 NM

SUPERSEDED

34AD-13

SAC


4531HRS

COMPLIED WITHMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains


Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

FAA 2006-22-05 APPLIANCE AD - HONEYWELL PRIMUS RNZ-850/851 NM

MANDATORY

34AD-18

SMF


5961.8HRS

5486LDG

COMPLIED WITH - COMPLIED WITH AD-2010-07-02 EFFECTIVE DATE 05/03/2010 BY COMPLIANCE OF

CESSNA CIL-34-02, UNIT UPGRADE AS PER SECTION (I) OF AD. OPERATIONAL CHECK NORMAL. SEE

SECTION 3 FOR

COMPONENT INFORMATION.

MOC :

FAA 2010-07-02 APPLIANCE AD - PERFORM A ONE-TIME GENERAL VISUAL INSPECTION OF THE MODIFICATION PLATE FOR THE HONEYWELL

PRIMUS II NV-850 NAVIGATION RECEIVER MODULE (NRM)

MANDATORY A/R09-Jul-2010MTH Complete

5437.2HRS

5216LDG

COMPLIED WITH - COMPLIED WITH STEPS (H), (L) AND (L)(2) OF AD2010-07-02 DATED MAY 3, 2010. #1

NAV RECEIVER MODULE (NRM); P/N 7510134-701 AND #2 (NRM); P/N 7510134-701 DOES NOT HAVE MOD

L OR

T INSTALLED PER AD. OPERATOR WILL COMPLY WITH HONEYWELL SERVICE BULLETIN

7510100-34-0037 WITHIN 30 MONTHS FROM THE DATE OF THIS AD. INCORPORATED FLIGHT

LIMITATIONS INTO THE AFM.

MOC :

FAA 2012-02-08 APPLIANCE AD - AVIATION COMMUNICATION AND SURVEILLANCE SYSTEMS (ACSS) TRAFFICALERT AND COLLISION

AVOIDANCE SYSTEM (TCAS) UNITS

MANDATORYSMF -29-Jan-2015MTH N/A

6147.1HRS

5586LDG

NOT APPLICABLE - COMPLIED WITH AD 2012-02-08 EFFECTIVE ON MARCH 13, 2012 BY INSPECTING

AIRCRAFT. FOUND AFFECTED ACSS EQUIPMENT NOT INSTALLED IN THIS AIRCRAFT.

MOC :

FAA 2014-18-01 APPLIANCE AD - NAVIGATION - ROCKWELL COLLINS, INC. MODE S TRANSPONDERS - INSPECTION / MODIFICATION

MANDATORY -MTH

MOC :

FAA 2015-10-51-E APPLIANCE AD - AVIDYNE INTEGRATED FLIGHT DISPLAY (IFD)- INCORPORATE OPERATIONAL LIMITATIONS INTO LIMITATIONS

SECTION OF THE AFM OR AFMS.

MANDATORY -MTH

MOC :

FAA 2015-10-51 APPLIANCE AD - AVIDYNE INTEGRATED FLIGHT DISPLAY (IFD)- INCORPORATE OPERATIONAL LIMITATIONS INTO LIMITATIONS

SECTION OF THE AFM OR AFMS

MANDATORY -

MOC :

FAA 1994-19-06 APPLIANCE AD - TO PREVENT THE FLIGHT CREW FROM EXPERIENCING DIFFICULTY IN EXHALING

MANDATORY35AD-01 VNY A/R23-Nov-1994MTH Complete

2030HRS

COMPLIED WITHMOC :

FAA 2015-08-07

PARA (G)

INSPECT THE INFLATABLE HARNESS FITTED TO EACH FLIGHTCREW OXYGEN MASK REGULATOR TO DETERMINE IF THE

INFLATABLE HARNESS IS INSTALLED WITH A PART NUMBER AND A BATCH NUMBER IDENTIFIED IN APPENDIX I OF ZODIAC

AEROSPACE SERVICE BULLETIN MXH-35-240, REVISION 7, DATED SEPTEMBER 1, 2011

MANDATORY

16-Jun-201724MTH 21 m 16 d

MOC :

FAA 2015-08-07

PARA (H)

REPLACE THE INFLATABLE HARNESS IDENTIFIED IN PAPRGRAPH G WITH A NEW OR RE-IDENTIFIED HARNESSES

MANDATORY

16-Jun-201724MTH 21 m 16 d

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015



Remains


Remains

TSO 1

TSO 2



(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

FAA 2015-08-07 APPLIANCE AD - OXYGEN - ZODIAC AEROTECHNICS (FORMERLY INTERTECHNIQUE AIRCRAFT SYSTEMS) FLIGHTCREW

OXYGEN MASK REGULATORS - INSPECTION / REPLACEMENT OF INFLATABLE HARNESSES

MANDATORY -

MOC :

FAA 1992-22-15 SUPERSEDED BY AD 93-19-03

SUPERSEDED

73AD-01

LBE


1067HRS

COMPLIED WITHMOC :

FAA 1993-19-03 TO PREVENT DETERIORATION OF THE FLOW DIVIDER START VALVE DIAPHRAGM DUE TO HIGHT TEMPERATURE

MANDATORY73AD-02 LBE A/R19-Nov-1993MTH Complete

1615HRS

COMPLIED WITHMOC :

FAA 1993-05-15 THRUST REVERSERS

MANDATORY

78AD-01

LBE


1332HRS

COMPLIED WITHMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .576339.1 5713 25-Aug-2015

ENG 1 .576307.4 5661 25-Aug-2015

ENG 2 .576307.4 5661 25-Aug-2015


560 - CITATION V

09-Apr-1991

Aircraft Model:

Owner:

Airworthiness:

Print Date:


3:12PM31-Aug-2015

Part Number

Part Serial No



Remains

RemainsTSO 2

TSO 1

Factory Installed

(ENG) DUE 1

(ENG) DUE 2

Adj.

+ or -

21FO-02 560 COOLING/FREON SUPPLEMEMTAL FACTORY OPTION

15A

FO

21FO-02 : 560

*CF

-09-Apr-1991MTH

25FO-01 560 LOCATOR BEACON-EMERG FACTORY OPTION

175

FO

25FO-01 : 560

*CF

-09-Apr-1991MTH

31FO-01 560 CLOCK/DIGITAL RH FACTORY OPTION

182A

FO

31FO-01 : 560

*CF

-09-Apr-1991MTH

34FO-06 560/C FMS DATA LOADER(PORTABLE) GLOBAL GNS-X FACTORY OPTION

695C

FO

34FO-06 : 560/C PIT -09-Apr-1991MTH

EQUIPMENT REMOVED BY OPERATOR SUBSEQUENT TO DELIVERY.

34FO-07 560 ALTITUDE REPORTING DUAL W/IDC ENCODING FACTORY OPTION

625

FO

34FO-07 : 560 *CF -09-Apr-1991MTH

34FO-08 560/R DME 2-HNYWL DM-850 ONLY W/OPT PACKAGE FACTORY OPTION

681R

FO

34FO-08 : 560/R *CF -09-Apr-1991MTH

34FO-09 560/X FM SYS-5TUBE HONEYWL EFIS FACTORY OPTION

685X

FO

34FO-09 : 560/X

*CF

-09-Apr-1991MTH

34FO-10 560 PRIMUS II RADIO PKG HONEYWELL SRZ-850 FACTORY OPTION

607D

FO

34FO-10 : 560 *CF -09-Apr-1991MTH

34FO-12 560/K RADAR-PRIMUS 870 W/MFD FACTORY OPTION

627K

FO

34FO-12 : 560/K

*CF

-09-Apr-1991MTH

34FO-14 560 VLF/OMEGA GLOBAL GNS-X FACTORY OPTION

693G

FO

34FO-14 : 560

PIT

-09-Apr-1991MTH

EQUIPMENT REMOVED BY OPERATOR SUBSEQUENT TO DELIVERY.



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