, ,

. CUSTOMIZED MAINTENANCE PROGRAMAIRWORTHINESS LIMITATIONS LISTDash 8 Series 300 - Wing IIB Flap SIN FI 530

DOT Approvedtyrolean

~Threshold Repeat

Task # Ale SIN IFIt [Fit Task Description DH Ref RemarksHours] Hours]

Ii 8-57-3314 N/A 40.000 20.000 Insp for repair of RD # 8-57-3314 This taskapplicable for

chafing on upper wingskin of the LH inboard flap

inboard nap upper SIN FI530

skin

VO-CMPI AWL-8/300Authority: TEIssued by: TE

4 1"1530.DO(, 2-FI53D

Revision # 16Page 1 of 1

Sep 01,2008

BOMBARDIERPREPARED: IB

CHECKED

DATE: May'06

RD8-57-3314SECT 1PAGE 1lSSU]l; 1

The following pages detail a Permanent Repair for Chafing on the Upper Skin ofthe LH Inboard Flap Upper Skin, 85750051, at Yw 79.0 Forward of Stringer 2,Damage is as reported in Temporary RD8-57-J312 .. Blended damage is left as is andall external repair' doubler installed ..

This repair is void if there is any damage to underlying structure.

This repair will require a special inspection as defined on Page 2. Thisinspection must be incorporated into the operators approved maintenanceprogram,

This Repairis detailed in: RD8-57~3314 Section 1

-- Approx Repair Location

Pages 1 Iss..!2 Iss.13 Iss.14 Iss.I5 Iss.1

RDISSUE 1 Title:Permanent Repair for Chafing on.-----1the Upper Skin of the LH InboardFlap Upper Skin, 85750051, atYw 79.0 Forward of Stringer 2.

DA.TE 4/May/06-----r---------+--------~DRA WN Ian BumsAPPROVED

STRESS

DAD# tOb REPORT NUMBE~

RD8-57-3314

DArE

APPLICABILITY

DHC-8-300

SIN 527LH Inboard Flap,85750002·011.SIN: FI-S30

BSS)' 91.E 9l)'IZ8-j lOO/eOO d 218-1

PREPARED: I B RD8-57-3314CHECKED BOMBARDIER SECT 1

PAGE 3DATE: May'06 ISStJ"E 1

.....-BLENDED AREA FROM RDB-57-3312LEAVE AS IS - DO NOT CUTOUT.

Yw87.35 DO NOT INSTALL RIVETS THROUGH Yw74.35I BLENDED AREA. .

Ir:;:h+ ~,'" , --Jr-II II 1~11II II II II)1+1\ )I+I!

':::."'_:-~J~'.:''::===~====='::::,::===,::=---- - --------- --- __-~~-+~~\,\.J-J ---- --------------. \.....J"-.:::.-;-

STR 1 .=============================== ===:===================.:::1+ L'+l --_- __ -:..":..":=,.-:...-:::.:::.-:.. -:::......::.;-=.:::.~~-=--=.:~"":.."::..--::~:::::.::-+ ('+"'I/?~/ ~--:..---,--1--;-=-=------------ ':\-T--r I'\. '-I- I / <: I+ I (\ I I ( FW D \ I I,I! 'I \, II'1+11 t ---_ 11+1'I , I( :_k. _k _lL_ _IL _IL I ,I11+11 7j 71 71 71 7]"- :1+11i i+ II ~ liB _k _k ___k _k. _k I: i iII I I, 71- 7J 7): 7j 7J"- II+ I iI , \ !I///,. J I , \/ I+ I', _k _k(.I'I''''''''''''>,_v + 1+'--"" , I ...._-- ;r 71'(/""///~,~ ./ t -h \-_.---'II-·-----===:::====----- ----- ......eN/,4-_.~__ ...~/' 1-" 1\ '"\ T , ----- -------....:'------ ====- ..- \+ 1 ...... .:.:::\~- ~- 1STR 2 ===.=.-::::-=:::=~~.========:::.';===;;:;=;;:;;;:;;;:;=;;:;=;;;:;;::.==.=====.=-==.=======~

-.~-..({]-------- -1--:..-=::.....::·::..:::.:-:...-:::...-:.::::::...":.:":..~~~:--~;f~-:...~*~-==--'::::::;::,+ (.jll,,;:;=l-, , I ,....------- ___lL ___lL ++ .....,.I" ,+- I / ?( 7]"- \ I+ II

\! , / \ I II11+11 DONOTINSTALL if~' ~ -t: ~ 1:+11'I 11 RIVETS THROUGH II . I'II + II STRINGER FLANGES. I' + 11I! 11 r I 'III +11 ,1+11I I I\ I I ,t11+', /1+'\

REAR =::;:::.,~+=1~~==:=,.=========~"i:;-==-~...====- ==========:;-====,;;;::J+=I:~~~-SPAR _~::T_....:~-::.~ ------.-------------~d,-~1

.------ ..-_I--------------- ............JREPAIR DOUBLER,.040", 2024·T3 CLAD, QQ-A·250/S.CORNERS .25" RADIUS MIN.FORM TO CONTOUR.

VIEW LOOKLNG DOWN, LH INBOARD FLAP UPPER SKIN, 85750051.

128-: LOO/SOO d 218-1 6€Sv SL€ Slv so-\'o-so

PREPARED: I B RD8·57·3314BOMBARDIER

isuerPAGEISSUE

151DATE: May'06

GENERAL NOTES (Continued)

10)Fill voids and fillet seal around the edges ~f the repair doubler, per sketch below, withPR1422B2, or equivalent, per Structural Repair Manual, PSM 1-83-3, Chapter 51-30-26

Repair DoubJer

_-.1.t ~04011(Ref)

11)RIVET KEY* CR3214·4 New locations at .70{SO"pitch, except across stringerHole size )29/ 132" Dia. : Csk .1911 196"Dia.

I+ Reference only.

l28-: LOO/LOO d 2l8-1 sm SL¬ 9ly SO-vo-sO

i~lOS EASA PART-145 AT.145.001, FAR-AUXY103F Austrian Airlines, Oesterreichsche Luftverkehrs AG

Illt.II~1I11~VO: EASA PART-145 AT.145.030 Tyrolean Airways - Tiroler Luftfahrt GmbH W.O. Rev. 1 IAircraft/ LTM Maintenance Workorder r·'~~-\ \~;~Cust.: - \~','V·',,'~>.~.'~o A32 OB77 o MD8o A33 o CRJ o 3RD Date Issued by ATA o Pirep No.2075067o A34 o DH8 o COMP 01.Mar2006 ID VPRI S7-S0 o Mainto B73 o F70 Fit No. From Tol (Side 1 of 2) (§9o B76 o F100 ~ SchedP/r--.;

Stn INN Statistics I DBase

SIN o Canni Project ~ Struct. Damage o Insuranceo Tech. Irreg. o WarrantyMEL Ref: MEL Interval D HIL D Fit Deck Info D Cabin Info D SDC

Classification [6]ffil[g[Q] D F.B. req: D AOG Risk ETOPS Restr.: CAT Restr.:OPS Reporting Text:

List any available Fault Codes, Messages, Observations either in Description- or Action Text

PERFORM PERMANENT REPAIR ON L/H INB. FLAP UPPER SKIN. RD FORPERMANENT REPAIR NEEDED. ENGINEERING! TEMP. REPAIR C/O ACC.

c RD8-S7-3312.0

207S0S0~ REF. TO WO'5o:ill0

Aircraft Log D ETOPSILJ Entry req, Critical PathIf Taskcard Finding I Zone I I Area I Date ID t-'egpJ~edrecort Task No.:

ET-INSPECTION PERFORMED ACC. RD 8-S7-3314 ISSUE 1 ITEM 3WITHOUT FINDINGS SEE ATTACHED REPORT.

UT DISBONDING INSPECTION PERFORMED ON STRINGER AND FRAMENO DISBONDING COULD BE FOUND AT THE TIME OF INSPECTION.EQ.IJ.IPMENT USED: FOKKERBONDTESTER 80L CRYSTAL 3418J! l)TER704 SETTING SRF M1SS. OS.OSVEBN %r---

c -----------------------------_--_-----------------------0D L/H<{ PERFORMED PERMANENT REPAIR ON INB.FLAP ACC: I L! •

RD8-S7-3314 ISSUE1 04.0SVZIN fh.-~O~OS VK1E, ~

I-' A .......-

/ I

/ I

(IReference W 207S0S0 W 2079012Type / No.:w. F. CD. I. M

Valid Ex1.Codes: Combination of GTI Groundtime. MPI Manpower, TOI Tool. HAl Hangar. PWI Paperwork, PRI Partrequest and CHI Change. ICllncomplete, lSI Insufficient. NAI Not avail. WRI Wrong

Transfer Due Date TAH TAC Prio Ext. Codes ID Sign

0 PIC for MEL Dispatch

16'16S 3 PWNA VPRI

b AcrrunistratonWorkorder,noMaintenanceReleaserequired E va Only:workoroer Completion- CRSto be issued in TAL

o This aircraft or airframeidentif,iedabovewas repairedand inspectedin accordancewithcurrent Regulationsof the Fe~eralAviationAdministrationand is approvedfor returnto service~_~1'~lrs,gned for the Austrian Airlines FAR 145 Approved Repair Stauon, Certificate Number: AUXY 103F at Austrran Airlines Technical Base A·1300 Vienna Airport, Austria, Europe

o C~ )hat the workspecifiedexceptas otherwisespecifiedwascarried out in accordancewithPART-145and in respectto thatwork the aircraft/aircraftcomponentis consideredreadyfor releasetoservl....c::

Approval No.: DoS EASA PART-145 AT 145001 D VO EASA PART-145 AT.145.030 D Other

Closing Closing Time UTC Last Fit No. Hrs: 16' 002 Rel~lD Dbllnsp.ID (if req) ~Station Date Sign@,j Sign .

INN OS.May.2006 OS288 Cyc: 17'448 -:c ~\ IIf) RA

printed by WARTUNG on Friday. the 5 May 2006 at 1944 out of database prod_vo hosted on amosp.vie.aua.com ~ pcedbY AMOS wwwmYAMOSCO~4505 .

~ OS'. EASA PART-145 AT145.001, FAR-AUXY103F Austrian Airlines, Oesterreichsche Luftverkehrs AG

IIIIIIIJIIII~~ VO: EASA PART-145AT.145.030 Tyrolean Airways - Tiroler Luftfahrt GmbH W.O. Rev. 1

Aircraft! , LTM F'"'' r~\Cust.: Maintenance Workorder :.Q/ .~,lI"F";'

o A32 OB77 o MD8 Dateo A33 o CRJ o 3RD Issued by ATA o Pirep No.2075067o A34 o DH8 o COMP 01.Mar2006 10 VPRI 57-50 o Mainto B73 o F70o B7 o F100 Fit No. From Tol ~ Sched (Side 1 of 2) , ~

i,/

PINStn INN Statistic~ DBase

SINo Canni Project ~ Struct. Damage o Insurance

o Tech. Irreg.:"

o Warranty

I MEL Ref: MEL Interval o HIL o Fit Deck Info o Cabin l~fO ". o SOC

Classification [6JffiJ[9[_QJ o F.B. req. o AOG Risk ETOPS Restr.: CAT Restr.:I, OPS Reporting Text:

List any available Fault Codes, Messages, Observations either in Description-or Action Text

PERFORM PERMANENT REPAIR ON L/H INB. FLAP UPPER' SKIN. RD FOR

PERMANENT REPAIR NEEDED. ENGINEERING! TEMP. REPAIR C/O ACC; 'tl' "'; .'c: RD8-57-3312.

:r.j ,..." •. " -;'M·,· "'

0

"g REF. TO WO 2075050 .' .,..

o(f) "

",',o0

1].Aircraft Log OJ 0 ETOPs/Entry req. Cnticat Path

If Taskcard Finding I IZone I IArea I Date 10 l'egPdlre0reoort Task No.:

ET-INSPECTION PERFORMED ACC. RD 8-57-3314 'ISSUE 1 'ITEM 3

WITHOUT FINDINGS SEE ATTACHED REPORT. -=- .,.

,.ye.

UT DISBONDING INSPECTION PERFORMED ON STRINGER"AND FRAME

NO DISBONDING COULD BE FOUND AT THE.TIME OF INSPECTION.o~

.~~PMENT USED: FOKKERBONDTESTER 80L CRYSTAL 3418 ." ~~

(;-;{.MC TECUAvlPTER 704 SETTING SRF M155. ,'., 05.05 VEBN X<~-1.

c:II ~''':7

0--------------------------------------------------------

·u<t:

~

,. 0 ,.

• 0 ,"."

.....

J, 0' .• ,,<C,h'" ,:.;, ' : ' )-

Ic

Reference W 2075050 W 2079012Type / No.: I

W.F.CD.I.MValid Ext. Codes: Combination of GTI Groundtime. MPI Manoower. TOI Tool. HAl Hanoar. PWI Paperwork. PRI Partreauest and CHI cnance. ICI Incom

ete, IS/Insufficient. NAI Not avail, WRI Wren

Transfer DueDate TAH TAC Prio Ext. Codes 10 Sign

-:" o PIC for MEL Dispatch

16'165 3 PWNA VPRI

5Administration Workorder, no Maintenance Release requiredo VO Only, WorMrder Completion - CRS to be issued in TAL

0ircraft or alrtrame identified above was repaired and inspected in accordance Withcurrent Regulations of the Federal Aviation Administration and is approved for retum to service.dersigned for the Austrian Airlines FAR 145 Approved Repair Station. Certificate Number AUXY 103F at Auslrian Airlines Technical Base A·1300 Vienna Airport. Austna. Europe.

tcJ Certifies that the worl<specified except as otherwise specified was carried out in accordance with PART- '45 and In respect to that work the aircrafVaircraft component is considered ready for release to

service.

Approval No.: DOS EASA PART-145 AT.145.001 o vo EASA PART-145AT.145.030 o Other

rrime UTev. Release 10 Obi Insp.ID (if req)

Closing Closing Last Fit No. Hrs:

Station DateSign Sign

Cyc:

printed by VEBN on Fnday. the S.May 2006 at 13:14 out of database prod_vo hosted on amosp.vle.aua.comproduced by AMOS www.myAMOS.com

Tyrolean AirwaysTiroler Luftfahrt GmbHFUrstenweg 190, 6026 InnsbruckDepartment Technik rolean

_~ _ _E!)DyCDRRENT INSPECTION REPORT----"~ --~

Partnumber: NIA Task: ----

Serialnumber : None

Technique Nr.: PSM 1-83-7A 51-00-01 Rev. 8 Dec 01/04 WO#: 2075067

r- " --- -- --- - ~ :---:--~~::c-----_Instrume~ used :Elotes_!_B1.3 SDMVersio_!l2.04, SerialnumberJl.1575 , Next Cal. Due: 17-02-2009=-= -Reference: ~ Standard calibration block Nfe

0 Calibration Block TP10 BFG testblock

other:

Calibration: )l'_ SCB: FSD at 1,OmmslotAlarm at 0,5mm slot

0 Calibration Block TP1 FSD at defect 0,5 mmAlarm at 50% FSD

0 Rotarytestblock : FSD at defectAlarm at 50% FSD

other:

Area of examination Probe Frequency Gain XJY I Preamp. Filter Phase

1. Acc. RD8-57-3314 KAS 66-3 800 kHz 50/30 dBI HF 0 dB LP 65 Hz 2720r-~~=-_ - ~__-_-=~_.~_-_-_ _=_- - .~_-~i-=-----~.-=- -=-~_=__=_-~_=_ --" . _3.------ .___ _! I I

_4.____ ~ . ~! -.=-=---=--=-=-l-----~-=-,~-:: ------~ - "_- 1 - -1- - ---I +-- --:---7.--- -i--~ -I---T 1--'-

Standard setting slightly varyfied for each application

Result of examination: Findings: 0 Yes ~ No

No surface discontinuity indications, which exceeds the rejection criteria, could be found at thetime of inspection

Additional information: NoneAll NOTwork done in accordance with applicable NOT Procedures and Tasks as shown above and approvedunder Austrian MOT Nr.: AT.145.030, 01 Rating for TYROLEAN AIRWAYS.

Inspectiondone by: Franz EBNER Qualification: EN 4179 Level II

Signature 1 License: Date: 05.05.2006

Form 12058Rev.1

SECTION 2.2

Bombardier AerospaceDASH 8

SPECIFIC AIRWORTHINESS LIMITATION

IN·SERVICEDEVIATIONINSPECTIONREQUIREMENTS]

The following task is a specific Airworthiness Lirnftatlon. Compliance with this task isrequired to ensure continuIng compliance with the airworthiness standards of theDHC-8 basis of Type Approval,

The count for the threshold commences upon incorporation of the deviation specifiedin the reference document.

Task No Threshold(flights)

40000

RepeatInterval(flights)

20000

OH Ref. Task Procedure

RO 8-57-3314 Low Frequency Eddy CurrentIssue 1 for basic aircraft structure

(sub-surface) and standardHigh Frequency EddyCurrent for repair patch(surface).Refer to NDT Manual, PSM1-83-7A, Section 51-00-06,

DAD Slgnature:_lI~",iI:....;;......!>Jd~_,;___#_~_o_G._and Number

APPROVED IN ACCORDANCE WITH TRANSPORT CANADADAO #93-0-02

APPROVAL PAGE

(RD 8-57-3314, Issue 1)

A copy of this page must be inserted in the SDIR manual.

SOIR 8 - 527.

[Z8-~ LOO/ZOO'd Z[8-1 6E9v9LE9lv ~S8a diSH ~~81 - S~EdSOJ9V J9!PJeqwo8-WOJ~ 90-vO-90

PREPARED: I B

BOMBARDIERCHECKED

DATE; May'06

RD8-57-3314SECT 1PAGE 1ISSUE 1

The following pages detail a Permanent Repair for Chafing on the Upper Skin ofthe LH Inboard Flap Upper Skin, 85750051, at Yw 79.0 Forward of Stringer 2.Damage is as reported in Temporary RD8-57-3312. Blended damage is left as is andan external repair doubler installed.

Thls repair is void if there is any damage to underlying structure.

This repair will require a special inspection as defined on Page 2. Thisinspection must be incorporated into the operators approved maintenanceprogram.

This Repair is detailed in: RD8-57-3314 Section 1 Pages 1 Iss.l2 155.13 155.14 Iss. 15 155.1

Title:~--------4---------~---------4 ~Permanent Repair for Chafing on~--------4---------~---- -+ ~the Upper Skin of the LH Inboard

I------I---~~~---+-------I Flap Upper Skin, 85750051, atYw 79.0 Forward of Stringer 2.

REPORT ~'lJMBER. APPLICABILITY

RD8-57-3314

~S9a disH y~81 - 9~edSOJ9V J9!PJeqwo8-wOJ~

DHC-8-300

SIN 527LH Inboard Flap,85750002-011.SIN: FI-530

90-vO-SO

PREPARED: I B

SECTPAGEISSUE

121

RD8 ..57 ·3314

BOMBARDIERCHECKED

DATE: Mlly'06

INSPECTION REQUIREMENTS

This repair affects the airworthiness limitations document and requires anadditional task. The inspection requirements for this task, which are shownbelow, are Transport Canada approved. The operator must incorporate thisadditional task as an amendment in the airworthiness limitations document forthe affected aircraft serial number. It is the operator's responsibility to obtainapproval of the amended airworthiness limitations document from his regulatoryauthority and to incorporate the added inspection task in the maintenanceprogram for the affected aircraft. The time for threshold inspection Is measuredfrom the time of the incorporation of this repair.

Threshold: 40000 Flights

Repeat: 20000 Flights

The above inspection times were determined in Report AEROC 8.4.AC.12,Section 57-0054..1.

Inspection Method: Low frequency Eddy Current for basicaircraft structure (subsurface) and standardhigh frequency Eddy Current for RepairDoubler (surface).

Inspection Procedures: NDT Manual, PSM :I..83y7A, Chapter51-00..06.

128-~ 100/vOO'd 218-1 6ESv SlE 91v 90-vO-90

PREPARED: In RD8-57 -3314BOMBARDIERCHECKED SECT 1

PAGE 3DATE: May'06 ISSUE 1

Yw87.35

BLENDED AREA FROM RDf3-57-3312.LEAVE AS IS - DO NOT CUT OUT.DO NOT INSTALL RIVETS THROUGHBLENDED AREA. Yw74.35

j

1r'n+111/ IIII II!I+II

/ I 1\,/ I 1\,

-- I / ....-_~_____ , ,_ ,---r+-r~---------~=~==========----------- -~/'+I\,.... ...J ----.-----------..... ~....J '-.:::.-;-

==;;;;;;;;;;;;;;;;;;;;;;;;;==:;;;;=::=================== ===:===============;;;:;;;:;;;:==1+ L+1 ------.... (..-...,--~--:"'--1~- -;:-.=..."::.-::...~-::...~-::...~-=--===--::..."=--::.."=.,-:::.:::.-=- -::.."=.,~-::.-::...-::..~.:::---- - - .......~<~T:-+I;'....-" / . I / \- I I /

\ I + 1/ FWD' \ I + III' II \ I 1/11+11 ~ 11+11II [I ~ _lL _k. II II11+111 71 ~ 7J~ 7( ~ 111+11I I I 1/II , I liB _lL .._k .JL II I I

JI I + 1 I 71- 71 ~ -t :f- II+ i I

, I \ !I///,. J I I \/ 1+' \., .JL ....k(NN"/>,~ ~ / I + I._/ I I <,----_______ 71 7j '(//////'1 .. -+--h \---1+,....,.-----____ ----- --- __ -V(////,~__ ,/ / I 1\'

\. 1 ---------- ------~----=== =::==::/\+ 1 '-"::..\,- ~-STR2 =:=~.L~~=~==~~~==T====~===========~~~~~~~~~~~::==:=(~=::~

<; I ;i-~;-.=.-=--:..-=--=--:. --:..-==--:.:~-=--=-*-:::.r~·-;j2--f -::\-I~-r//\ I 1/ \ I "11+11 DONOTINSTALL if * t- * ~ il+11I I :: RIVETS THROUGH I: II: I+ II STRINGER FLANGES II + III II . II II11+/1 11+11

REAR =,:~:/~;:~k~~",,,,,,,.,,,,====...,=...,========-~============...,-=;;~~if~~;'1-SPAR -~---:::..-::.---------------------- ------- -..--------------':..---~I

STR 1

REPAIR DOUBLER,.04011, 2024-T3 CLAD, QQ-A-250/5.CORNERS .25" RADJUS MIN.FORM TO CONTOUR.

VIEW LOOKJNG DOWN, LH INBOARD FLAP UPPER SKIN, 85750051,

12S-~ lOO/SOO·d 218-1 6SSv SlS 9lv 90-vO-SO

'.

PREI'ARED: I B RDS-S7 ·3314CHECKED BOMBARDIER SECT 1

J>AGE 4DATE: May'U6 ISSUE 1

GENERAL NOTES

1) This repair is void if there is any damage to underlying structure.

2) Before installation of the repair, ultrasonic inspection of the bonded skin, waffle doubler andstringers is required Laensure that no disbanding indications are present in the repair area. Ifdisbonding is found contact Bombardier Aerospace Regional Aircraft before proceedingfurther. Ultrasonic testing is the preferred method of inspection for skin/waffle/stringerdisboriding. If the preferred method is impractical, or j f' ultrasonic test facilities are notavailable, an alternative non-destructive inspection procedure may be used provided it isapproved by an appropriate airworthiness authority and is performed by an operator withdemonstrated expertise.

3) Crack detect using preferred Eddy Current method, per NDT Manual, PSM 1-83-7A,Chapter 51-00-06, or fluorescent dye penetrant method. No crack indications permitted.

4) All cut edges to be smooth and nick free.

5) Maintain a minimum of two (2) times the fastener diameter edge distance un1ess otherwisespecified. Edge distance is measured from the centre of the hole to the nearest materialedge. The minimum edge distance, or better, must be maintained on all parts, includingwaffle doublers where applicable, through which the fasteners pass,

6) When drilling off new fastener locations, near existing structure or waffle doubler edges,take care to locate hole centres far enough from existing: edges to provide clearance forinstalling rivets (.20" for -4 diameter rivets.).

7) All new P81ts and bare metal to be finished with Alodine, Epoxy Primer and Enamel.i) Alodine per Structural Repair Manual, PSM 1-83-3, Chapter 51-20-16.ii) Epoxy Prime per Structural Repair Manual, PSM 1-83-3, Chapter 51-20-36.iii) Externally, apply a coat of Polyurethane Enamel (F24) per Structural Repair Manual,

PSM 1-83-3, Chapter 51-20-51, except on mating surfaces.

8) Fay seal all mating surfaces with Pro-Seal 870C, or equivalent per Structural RepairManual, PSM 1-83-3, Chapter 51-30-26.

9) Install all fasteners wet with Pro-Seal 870C, or equivalent per Structural Repair Manual,PSM 1-83-3, Chapter 51-30-26.

ContinuedNext Page...

IZ8-~ lOO/SOO'd Z18-1 6£5v 5LS Slv

I

PREPARED: IB RD8·57·3314CIII~CIn:.D BOMBARDIER SECT 1

[ PAGE 5DATE: May'06 ISSlJE 1

I

GENERAL NOTES (Continued)

10)Fill voids and fillet seal around the edges ~fthe repair doubler, per sketch below, withPR1422B2, or equivalent, per Structural Repair Manual, PSM 1-83-3, Chapter 51-30-26.

.40/.50" ,---- Repair Doubler

_---1.t_.04011 (Ref)

11)RIVET KEY

-t CR3214~4 New locations at .7°1.80" pitch, except across stringer.Hole size .129/.132"Dia. • C'sk .191/.l96'1 Dia.

+ Reference only.

IZ8-d lOOllOO d Z18-1 6ESv SlS 9lv

J ~

~1yrolean Aircraft- Equipment- List VFLO 07 .Apr .201108:52 Page 18/27

Aircraft- Equipment- List of Aircraft LTM SIN 527Only rotables with requirements with subtrees, group by 2 char. on ATA-Chapter ( AlC Data: 24'949/H, 27'009/C )

. :. '; Descri):itioD. ;Padno . ;, Y senabio Ih',. .' ."ibescript'ion . . I ·Relea~tlU)./.La~1 no.""",,;.:(.;. [:: .. ,TSN:: ".1.: :eSN,;,..ATA 't; '" :: Pos. .: lost-Date

85410282-105 TDP550 PIN, ENDS RH I 0/1010735 23.Dec.1998 24949 27009.. ,I!'J;r:~."':Require.;n~t .. ·''raske.rel: '.;..:~':!:,,;irti : "Ioterval; ;,/1',"tSR,,,i';;::' " "Togq;.: ,',.. ...

LIFE LIMITATION 69300/C 27009/C 42291/C85410930-105 6907BB PIN,CENTER RH I 0/1010736 23.Dec.1998 24949 27009

'::"~l:::·,- '.. ' 'ReqiJirentent, 1 , ." . . . I' .. : i:~:Taskcard '". ·,·····.i ', llitemll'-; , , .'ISRi;:, .. Togo. 'wLIFE LIMIT ATION 69300/C 27009/C 42291/C

85410930-105 6907KK PIN, CENTER LH I 0/1010737 23.Dec.1998 24949 27009,.. ..RequIrethen·t.· . " Taskcard miervll TSR :TogoLIFE LIMITATION 69300/C 27009/C 42291/C

85411782-005 791417CTA6 FITTING, ASSY-MLG ACTUATOR LH I L-I089648 I 1089648 22.Jan.20 10 26788 29274Requirement Taskcard [nterval TSR Togo

INSPECTION 3230/18 (RH); 3230/18 (LH) 5000/C 701/C 4299/C85411782-005 MLG78201-P FITTING, ASSY-MLG ACTUATOR RH I L-I066169 11066169 o l.F eb.2008 21290 23173

Requirement ," Tlskcard Interval TSR : Togoi::.INSPECTION 3230/18 (RH); 3230/18 (LH) SOOO/C 260/C 4740/C

8Z5082-003 88610663918-AO 14 SHROUD, ASSY-EXHAUST OUTL RH IAAL-311/20 I0 I 1103045 21.Dec.2010 34445 35418,~,<:!.:iiX:, :Requiren:uint . .. , I,·:. Task~, .,; ,: ' i~.;i_wterval ! ;tSR ".;' i. ,:,1'O:J~C). ,>'<

INSPECTION 7810/509 (LH); 78101509 (RH) 250M .. 11H 24991H56 WINDOWS 171900-06 1636 WlNDOW, ASSY-SIDE RH RH I 1D041458 1 1039622 04.Feb.200S 11725 12550

,:! ','~: :::'~!~.equiremeDf·":c., : ril,,';'; .- l'asktatd, ,. . ,;'l!F;:nrui~:,'!!I,IilteiY.iil: i, •[: .:,ISR\'[';;;' ·:j!;·J'q,.P;tI:'~;';i.::_•. ,,:

INSPECTION 5310/07C (RH) 4650/C 3362/C I288/CNP157902-13 08253HI407 WINDOW, ASSY-SIDE LH LH I NI120J 1082374 15.May.2010 49 52

i'ii .:,.,'i;;:ii;~tqulrelneDt. 'c; , . : . Taskcardi!{ : ' . lIi~~l.\.;;; , , TSI\,L: ,,;~,To,i6:· ,;c ,

INSPECTION 5310/07C (LH) 96451C 52/C 9S93/C57 WINGS 85711439-001 505583BJ FITTING, ASSY-LUG CENTRE LH I 0/1010770 21.Dec.1998 24949 27009

--'" .' 'Rtqulre!beiif '.;,~ '1'lskcjrd' . liJUfiiaiJr;,:"1 j TSR .To,go"~."

LIFE LIMIT ATION 36000JC 27009/C 89911C85711439-001 505583BK FITTING, ASSY-LUG CENTRE RH I 0/1010771 21.Dec.1998 24949 27009

. :~equiremeDf Taskcard Interval TSR To'goLIFE LIMITATION 36000/C 27009/C 8991/C

85750002-011 FI530 FLAP, WING INBD LH LH IB I 0/1010801 21.Dec.1998 24949 27009.. ~produced by AMOS www.swiss-es.com

;> J J, ~, 1yrolean Air ~aft- Equipment- ::!ist VFLO 07.Apr.2011

, 08:52 Page 19127

Aircraft- Equipment -List of Aircraft LTM SIN 527I Only rotables with requirements with subtrees, group by 2 char. on ATA-Chapter (AIC Data: 24'9491H, 27'OO9/C)I

ATA: ; i! ':".Di!!mption.r- ,,', .' ,.",_" , i D_riPtipn

'hO< ·rRelellli!:ttoL,l :IiAi)ij00.' "'t§N\'i1!::, . CSN .'J Partno ' :iO,::: >;,\, SerbillfO "'1',' i' Pot. Inst-'Date.. : .tiq'i'lRm~ TaskCal-d ' Interval :TSI,l !~~. Togo':i~~:

_,,1 INSPECTION 40000/C 9S61/C 30439/C- 61 PROPELLERS 782490-47 910722 CONTROL, PROPELLER UNIT (T( #2 I 4332892/1083240 31.1an.2009 UNKNOWN UNKNOWN':Reqwr_e.t'" .'" ~ .: ;~:fi'. ,i ''i','j,,]'ukafd,

..':,,·,~~I.'I; .~~~_'i:~.:lF';· ',I, <1'0:&0"

_" .

CRITICAL PART INSPECTION6120/S06 (2) (RH); 6120/506 (1)

10S001H 48641H S6361H(RH)

INSPECTION 61201502 (RH) SOOO/H IIH 49991H782490A47 970S18 CONTROL, PROPELLER UNIT (N( #1 I L-I077211/1077211 26.Aug.2010 247S0 27044

; . :','KeqaWmeilt·.· .. ,

,Tas~;",il::'~l!' Interval ' 'TSR r~r,;", Tog!»,. ,",,~l,

CRITICAL PART INSPECTION6120/S06 (J) (LH); 6120/506 (2)

105001H 71981H 3302IH(LH)

INSPECTION 61201502 (LH) 50001H 2329/H 26711H790180-3 960819 PROPELLER ACTUATOR ASSY V #2 I BOl1/2010 /1095709 22.1an.2010 26594 28881

~,;(i;',' ,~remeat " . :':}; ';';~T.lIkc)lHl ::.,','1 ,:,I.Mi~iIJ, TSR . T,PI~ii!!'~;1OVERHAUL 1RESTORATION 6110/505 (LH); 6110/505 (RH) 25551D 17.Apr.2007 l104/DOVERHAUL / RESTORA TION 6110/505 (LH); 6110/505 (RH) 105001H 62001H 4300iH

790180-3 980414 PROPELLER ACTUA TOR ASSY V #1 I B009/20 10 / 1095661 2 J.Jan.201 0 23392 UNKNOWN'" ,~ "~ ,_ ,v " eDtr lir;~ "':~;r~~':I'" TaSlu:ard :.. ",',,, ",'.. " .. IDte~'L ,c.TSR'i':·, :,,!fogO'i ~>'~..: lj, I',

OVERHAUL IRESTORATION 6110/S05 (LH); 6110/505 (RH) 255510 13.lul.2007 119110OVERHAUL / RESTORA TION 61101505 (LH); 6110/505 (RH) 10500/H 56591H 48411H

802396-1 000412-23 BARREL,PROPELLER #1 ~C:L-I089187 /1088600 04.Jun.2009 19120 20612i! ,;;,,{::.': ,:' !~~ubimi~d,;I:i;'.,:,,'.;\H~:"'; :.". "':i:':Tas1t~,;k;,ni;;:~·i'i,:,i:ii:t!!': Interval' •;:;H':T~It::;!::,i:: "::"'1'0&0: ':OVERHAUL / RESTORA TION 6110/09 (LH); 6110/09 (RH) 255510 08.May.2009 185610OVERHAUL / RESTORA nON 6110/09 (LH); 6110/09 (RH) 105001H 1989/H 85111H

802396-1 862-23 BARREL,PROPELLER #2 ~C:L-I069814 /1069266 16.Aug.2007 26677 29102. :::lii,;: ·;;i'ieciU1remeD:t \ ::;' [;;,'E: ,!!~ '~',l!i.", ,;;'tuktil'il)!i'!'" " " ,Itttern.t::,,;i, ' ,Tjl;::r,SR ~'., " '"'to go.',;",", .. ;" - ' "",, ,

OVERHAUL / RESTORATION 6110/09 (LH); 6110/09 (RH) 255510 16.1ul.2007 119410OVERHAUL / RESTORATION 6110/09 (LH); 6110/09 (RH) 105001H 60111H 44891H

806700-1 20000514 PROPELLER,ASSY #1 I L-I089187/1089187 04.Jun.2009 19120 20612Requirement' " TaSkcard Interval TSR " Tc)'go.

REPLACEMENT 6110/506 (LH); 6110/506 (RH) 40001H 6361H 33641H

produced by AMOS www.swrss-es.ccm