structural repair manualseries 100/200/440 structural repair manual volume 1 csp a−008 master...

TRANSMITTAL LETTER

This package contains the Strucutural Repair Manual, CSP−A−008, Revision 31 dated Apr 10/2011.

To bring your manual up to date, remove and insert pages according to the filing instructions. Record theinsertion of this revision on the Record of Revisions.

The following is a list of all Temporary Revisions which were incorporated into Revision 31 and are to beremoved

Please update the Record of Temporary Revisions accordingly.

51−18 51−22

51−19 51−23

51−20 53−16

51−21

Suggested Split

The suggested split is 500 sheets or 1000 pages per volume.

NOTE: Please place this Transmittal Letter prior to the Volume 1 Cover page, as this is an integral part ofyour manual.

CSTRUCTURAL REPAIR MANUAL

MasterEFFECTIVITY: ALL Transmittal

Letter

Apr 10/2011

REMOVE: INSERT:

Ch−Se−Su−Config Eff. Page Ch−Se−Su−Config Eff. Page

Intro − Effective Pages 1 Intro − Effective Pages 1

Introduction 5 Introduction 5

51 − Effective Pages 1−18 51 − Effective Pages 1−19

51 − Contents 2−40 51 − Contents 2−41

51−00−00 1−3 51−00−00 1−3

51−00−00 6−15 51−00−00 6−15

51−00−20 1−9

51−13−00 1−2 51−13−00 1−2

51−13−00 4−5 51−13−00 4−5

51−13−00 7−8 51−13−00 7−8

51−13−01 15 51−13−01 15

51−13−02 1−36

51−13−03 00 1−2

51−13−04 1−2

51−14−06 2−3 51−14−06 2−3

51−14−06 5 51−14−06 5

51−14−06 8−10 51−14−06 8−10

51−14−06 22−25 51−14−06 22−25

51−32−00 78−80 51−32−00 78−80

51−74−24 201−202 51−74−24 201−202

51−75−04 201−202 51−75−04 201−202

51−75−04 204−206 51−75−04 204−206


52 − Effective Pages 5 52 − Effective Pages 5

52−12−55 2−6 52−12−55 2−6


53 − Contents 10−14 53 − Contents 10−14

53−00−00 2 53−00−00 2

53−21−23 7−32 53−21−23 7−34



LetterPage 1

Apr 10/2011

REMOVE: INSERT:

Ch−Se−Su−Config Eff. Page Ch−Se−Su−Config Eff. Page

53−51−31 3−6 53−51−31 3−6






57−52−00 2−3 57−52−00 2−3



LetterPage 2

Apr 10/2011

51−13−01 1 Corrected thd e−mail address on one illustration. ALL

51−74−24 201 Revised page block to incorporate the RAFBA71464

ALL

51−75−04 201 Changed all the reference from aluminium tocopper. Revised the task title. Reference toaluminium oxide abrasive paper 180−grit and 400−grit added newly.

ALL

53−00−00 1 Illustration is Revised in Figure 1. FS 461.00 ischanged to FS 461.50.

ALL

53−00−00 1 Illustration is Revised in Figure 1. FS 461.00 ischanged to FS 461.50.

ALL


REVISION 31

Ch−Se−Su

Page 1Apr 10/2011

The following is a summary of changes for this revision.

PAGE BLOCK −REPAIR NO.

DESCRIPTION OF CHANGES EFFECTIVITY

HIGHLIGHTS

CModel CL−600−2B19

Series 100/200/440

STRUCTURAL REPAIR MANUAL

Volume 1

CSP A−008

MASTER

BOMBARDIER INC.BOMBARDIER AEROSPACE REGIONAL AIRCRAFT

CUSTOMER SUPPORT

123 GARRATT BLVD, TORONTO, ONTARIOCANADA M3K 1Y5

Copyright © 1992 − 2011 by Bombardier Inc.

All rights reserved. No part of this work may be reproduced or copiedin any form or by any means without written permission

of Bombardier Inc.

The Bombardier logo and Canadair are registeredtrademarks of Bombardier Inc.

Initial Issue:Revision 31:

Mar 31/1992Apr 10/2011

B

"The information, technical data and the designs disclosed herein are theexclusive property of Bombardier Inc. or contain proprietary rights of others andare not to be used or disclosed to others without the written consent ofBombardier Inc. The recipient of this document, by its retention and use, agreesto hold in confidence the technical data and designs contained herein. Theforegoing shall not apply to persons having proprietary rights to such information,technical data or such designs to the extent that such rights exist."

REVNO.

PAGESAFFECTED SUBJECT

TRANSPORT CANADAAPPROVAL/DATE

2 52−00−31, pg 101 TR 52−1 incorporated, with editorialchanges.

53−00−31, pg 101 TR 53−1 incorporated, with editorialchanges.

P.C. Newman/ 7 Nov 1992

3 52−12−55 pg 1−7 Passenger Door Stairs − StructuralIdentification Revised

52−12−57 pg 1−3 Passenger Door Handrail − StructuralIdentification Revised

52−41−27 pg 1−4 Service Door Fittings − StructuralIdentification Revised

53−00−47_101Passenger and Cargo Compartmentfloor panels − Materials Ident.Revised

57−31−14 pg 1−6 Winglet Framing Structures −Structural Identification Revised

57−41−31 pg 102,103, 105

Wing Leading Edge − AllowableDamage Revised

57−51−14 pg 1−9 Framing Structure Trailing Edge −Structural Identification Revised

P.C. Newman/ 5 Apr 1993

4 Not Affected − −

5 53−00−31_201Repair No. 1

TR 53−2 incorporated, with editorialchanges.

53−00−00_1 Page3


57−41−31_101Pages 101 to 106


P.C. Newman/ 8 Jun 1995

6 52−01−00_201 pg1−2 Repair of door seals added

53−00−31_101 pg101. 104−107

Fuselage skin and plating − allowabledamage revised

53−80−00_101pg101

Fuselage aerodynamic fairings −allowable damage added

P.C. Newman/ 8 Sep 1995

7 53−00−47_101 Page 101, Editorial change on thenote

53−62−57_101 Apu compartment − allowabledamage

53−21−03_1 Stringers FS280 − FS409

P.C. Newman/ 5 Sep 1996

8 52−10−14_1 Passenger door frame and structureidentification added.

52−21−0_1 Overwing emergency door ident.added.

52−22−00_1 Crew escape hatch identificationadded

52−30−00_1 Cargo door identification added.

DAO #93−Q−02

G.P. Jones/ 20 Feb 1997


APPROVAL LOG Page 1Dec 15/2004

REVNO.



8(Cont’d)

52−30−55_1 Cargo door step−plate ident. added.

52−41−14_1 Service door skin and frame structuralidentification added.

52−42−00_1 Main avionics door struct.identification

52−43−00_1 Aft equipment bay door structureidentification added.

52−44−32_1 Forward equipment compartmentdoors structure identification added.

52−44−37_1 ADG door struct. identification added.

52−45−01_1 Apu fault and ground air connectiondoor struct. identification added.

52−45−02_1 Refueling access door struct.identification added.

52−45−03_1 Oxygen refilling door struct.identification.

52−45−04_1 AC electrical ground power doorstruct. identification added.

52−45−05_1 External service panel door struct.identification added.

52−45−06_1 DC electrical ground door struct.identification added.

52−45−07_1 Lavatory services door struct.identification added.

52−45−08_1 Refuel/Defuel control panel doorstructural identification added.

52−45−09_1 Potable water service door struct.identification added.

52−81−00_1 Nose landing gear door struct.identification added.

52−82−00_1 Main landing gear door struct.identification added

57−21−03_1 Stringers. integral structuralidentification added.

57−21−27_1 Wing box fittings structuralidentification added.

57−21−32_1 Wing box access doors structuralidentification added.

57−21−55_1 Flap hinge boxes structuralidentification added.

57−31−31_1 Winglet skin and plating structuralidentification added.

57−31−51_1 Winglet fillets and fairings structuralidentification added.

DAO #93−Q−02




REVNO.



8(Cont’d)

57−41−12_1 Leading edge ribs structuralidentification added.

57−41−29_1 Leading edge shrouds and framesstructural identification added.

57−41−31_1 Leading edge skin and platingstructural identification added.

57−51−31_1 Trailing edge skin and platingstructural identification added.

57−52−00_1 Inboard flap and vane structuralidentification added.

57−53−00_1 Outboard flap and vane structuralidentification added.

DAO #93−Q−02


953−00−31_201

Fuselage, Skin and Plating − ExternalNon−Flush Repairs, new repairsadded

53−61−03_1 Stringers FS559.00+112 to FS755.00(page 3 revised, item M and N)

53−81−00_101 Radome − Allowable Damage (page1 revised)

57−00−00_1 Wings General

G.P. Jones/ 5 Oct 1997

10 53−00−00_1 Fuselage internal structure −structural identification added.

53−00−03_1 Fuselage stringers − structuralidentification added.

53−00−03_1 Fuselage skin and plating − structuralidentification added.

53−00−49_1Passenger seat and cargo tie−downtracks and structure − structuralidentification added.

53−10−00_1 Fuselage FS144.00 to FS280 −structural identification added.

53−11−00_1Fuselage main structure FS144.00 toFS280.00 − structural identificationadded.

53−11−19_1 Bulkheads, FS144.00 to FS280.00 −structural identification added.

53−11−23_1Surround structures, FS144.00 toFS280.00 − structural identificationadded.

53−11−31_1Skin and plating, FS169.00 toFS280.00 − structural identificationadded.

53−20−00_1Fuselage, FS280.00 to FS409.00 −general added.

G.P. Jones/ 20 Sep 1999



REVNO.



10(Cont’d)

53−21−00_1 Fuselage, FS280.00 to FS409.00 −structural identification added.

53−21−17_1 Intercostals, FS280.00 to FS409.00 −structural identification added.

53−21−23_1Door surround structures, FS280.00to FS409.00 − structural identificationadded.

53−21−27_1 Fittings, FS280.00 to FS409.00 −structural identification added.

53−30−00_1 Fuselage, FS490.00 to FS409.00+128 − general added.

53−31−00_1Fuselage main structure, FS490.00 toFS409.00+ 128 − structuralidentification added.

53−40−00_1 Fuselage, FS490.00+ 128 toFS559.00 − general added.

53−41−00_1Stringers, FS490.00+ 128 toFS559.00 − structural identificationadded.

53−50−00_1 Fuselage, FS599.00 to FS559.00+112 − general added.

53−51−00_1 Fuselage, FS599.00 to FS559.00+112 − structural identification added.

53−60−00_1 Fuselage, FS599.00+ 112 toFS755.00 − general added.

53−61−00_1Fuselage, FS599.00+ 112 toFS755.00 − structural identificationadded.

53−70−00_1Fuselage,FS755.00 to verticalstabilizer 67.5% spar datum − generaladded.

53−71−00_1Fuselage, FS755.00 to verticalstabilizer 67.5% spar datum −structural identification added.

G.P. Jones/ 20 Sep 1999

11 52−00−27_201 Door fittings − repairs added.

52−00−31_201 Door skin and plating − repairsadded.

52−10−27_101 Passenger−door fittings − allowabledamage

52−10−27_201 Passenger−door fittings − repairsadded.

52−10−31_201 Passenger door skin and plating −repairs added.

52−12−55_201Passenger−door stairs − repairsadded.

G.P. Jones/ 30 Nov 1999



REVNO.



11(Cont’d)

52−12−57_201 Passenger−door handrail − repairsadded.

52−21−00_201 Overwing emergency exit door −repairs added.

52−30−55_201 Cargo door step plate − repairsadded.

52−42−00_201 Main avionics door − repairs added.

52−44−32_201 Forward equipment−compartmentaccess doors − repairs added.

52−45−00_201 Servicing doors − repairs added.

52−45−01_101 Apu fault and ground air connectiondoor − allowable damage added.

52−45−02_101 Refueling access door − allowabledamage added.

52−45−04_101 Ac electrical ground power door −allowable damage added.

52−45−05_101 External service panel door −allowable damage added.

52−45−06_101 Dc electrical ground power door −allowable damage added.

52−45−08_101 Refuel / defuel control panel door −allowable damage added.

52−51−00_101 Flight compartment door − allowabledamage added.

52−51−00_201 Flight compartment door − repairsadded.

53−00−03_101 Stringers − allowable damage added.

53−00−03_201 Stringers − repairs added.

53−00−15_101 Frames − allowable damage added.

53−00−15_201 Frames − repairs added.

53−00−27_201 Fittings − repairs added.

53−00−47_201 Passenger and cargo compartmentfloor panels − repairs added.

53−00−49_1

Passenger seat and cargo tie−downtracks and structure − structuralidentification, figures amended andtable added

53−00−49_201 Passenger seat and cargo tie−downtracks and structure − repairs added.

53−11−03_201 Stringers, FS169.00 to FS280.00 −repairs added.

53−11−15_201Frames, FS144.00 to FS280.00 −repairs added.




REVNO.



11(Cont’d)

53−11−17_1 Intercostals, FS144.00 to FS280.00 −structural identification, revised figure.

53−11−17_201 Intercostals, FS144.00 to FS280.00 −repairs added.

53−11−19_201 Bulkheads, FS144.00 to FS280.00 −repairs added.

53−11−23_201 Surround structures, FS144.00 toFS280.00 − repairs added.

53−11−31_201 Skin and plating, FS169.00 to FS280.00 − repairs added.

53−11−35_201 Windshield and side window framestructure − repairs added.

53−11−43_201 Floor support structure, FS169.00 toFS280.00 − repairs added.

53−11−47_201 Floor panels, FS169.00 to FS280.00− repairs added.

53−11−49_201 Flight−compartment seat tracks −repairs added.

53−11−67_201 Nose−landing−gear support structure− repairs added.

53−12−55_201Underfloor crawlway and supportstructure, FS235.00 to FS280.00 −repairs added.

53−21−03_201 Stringers, FS280.00 to FS409.00 −repairs added.

53−21−15_201 Frames, FS280.00 to FS409.00 −repairs added.

53−21−17−201 Intercostals, FS280.00 to FS409.00 −repairs added.

53−21−23_1Door surround structures, FS280.00to FS409.00 − structural identificationwas revised

53−21−23_201 Door surround structure, FS280.00 toFS409.00 − repairs added.

53−21−27_201 Fittings, FS280.00 to FS409.00 −repairs added.

53−21−31_201 Skin and plating, FS280.00 toFS409.00 − repairs added.

53−21−43_201 Floor support structure, FS280.00 toFS409.00 − repairs added.

53−21−49_101 Seat tracks, FS280.00 to FS409.00 −allowable damage added.

53−21−49_201Seat tracks, FS280.00 to FS409.00 −repairs added.




REVNO.



11(Cont’d) 53−22−55_201

Underfloor crawlway and supportstructure, FS280.00 to FS409.00 −repairs added.

53−31−03_201 Stringers, FS409.00 to FS409.00+128− repairs added.

53−31−15_201 Frames, FS409.00 t0FS409.00.00+128 − repairs added.

53−31−23_201 Surround structures, FS409.00 toFS409.00+128 − repairs added.

53−31−31_201 Skin and plating, FS409.00 toFS409.00+128 − repairs added.

53−31−33_201 Forward longeron beam − repairsadded.

53−31−43−201 Floor structure, FS409.00 toFS409.00+128 − repairs added.

53−31−45_101 Pressure box − allowable damageadded.

53−31−45_201 Pressure box − repairs added.

53−31−49_101Seat tracks, FS409.00 toFS409.00+128 − allowable damageadded.

53−31−49_201 Seat tracks, FS409.00 toFS409.00+128 − repairs added.

53−41−03_201 Stringers, FS409.00+128 to FS559.00− repairs added.

53−41−15_201 Frames, FS409.00+128 to FS559.00− repairs added.

53−41−19_201 Bulkheads, FS409.00+128 toFS559.00 − repairs added.

53−41−23_201Surround structures − overwingemergency exits, FS409.00+128 toFS559.00 − repairs added.

53−41−31_201 Skin and plating, FS409.00+128 toFS559.00 − repairs added.

53−41−33_201 Underfloor longeron − repairs added.

53−41−43_201Floor support structure,FS409.00+128 to FS559.00 − repairsadded.

53−41−45_101Pressure floor structure,FS409.00+128 to FS559.00 −allowable damage added.

53−41−45_201

Pressure floor structure,FS409.00+128 to FS559.00 − repairsadded.




REVNO.



11(Cont’d)

53−41−49_101 Seat tracks, FS409.00+128 toFS559.00 − allowable damage added.

53−41−49_201 Seat tracks, FS409.00+128 toFS559.00 − repairs added.

53−41−55_101 Main landing gear uplock and apronstructure − allowable damage added.

53−41−55_201 Main landing gear uplock and apronstructure − repairs added.

53−51−03_201 Stringers, FS559.00 to FS559.00+112− repairs added.

53−51−15_201 Frames, FS559.00 to FS559.00+112− repairs added.

53−51−26_101 Surround structure, lavatory servicing− allowable damage added.

53−51−26_201 Surround structure, lavatory servicing− repairs added.

53−51−31_201 Skin and plating, FS559.00 toFS559.00+112 − repairs added.

53−51−43_1Floor support structure, FS559.00 toFS559.00+112 − structuralidentification added.

53−51−43_101Floor support structure, FS559.00 toFS559.00+112 − allowable damageadded.

53−51−43_201 Floor support structure, FS559.00 toFS559.00+112 − repairs added.

53−51−49_101Seat tracks, FS559.00 toFS559.00+112 − allowable damageadded.

53−51−49_201 Seat tracks, FS559.00 toFS559.00+112 − repairs added.

53−52−55_101Equipment support structure,FS559.00 to FS559.00+112 −allowable damage added.

53−52−55_201Equipment support structure,FS559.00 to FS559.00+112 − repairsadded.

53−61−03_201 Stringers, FS559.00+112 to FS755.00− repairs added.

53−61−15_201 Frames, FS 559.00+112 to FS 755.00− repairs added.

53−61−17_201 Intercostals, FS559.00+112 toFS755.00 − repairs added.

53−61−19_201Bulkheads, FS559.00+112 toFS755.00 − repairs added.




REVNO.



11(Cont’d) 53−61−23_201

Surround structure, cargo andaft−equipment compartment doors −repairs added.

53−61−27_101 Fittings, FS559.00+112 to FS755.00−allowable damage added.

53−61−27_201 Fittings, FS559.00+112 to FS755.00− repairs added.

53−61−31_201 Skin and plating, FS 559.00+112 toFS 755.00 − repairs added.

53−61−33−101Longeron beam structure, verticalstabilizer attach − allowable damageadded

53−61−33−201 Longeron beam structure, verticalstabilizer attach − repairs added

53−61−43_201Floor support structure,FS559.00+112 to FS755.00 − repairsadded.

53−61−49_101Cargo tie−down tracks,FS559.00+112 to FS621.00 −allowable damage added.

53−61−49_201

Cargo tie−down tracks,FS559.00+112 to FS621.00 −allowable damage added. − repairsadded.

53−61−55_201 Engine support and transverse beams− repairs added.

53−62−55_101 Equipment support structure −allowable damage added.

53−62−55_201 Equipment support structure − repairsadded.

53−62−57_201 Apu compartment − repairs added.

53−71−03_201Stringers, FS755.00 to verticalstabilizer 67.5% spar datum − repairsadded.

53−71−15_201Frames, FS755.00 to verticalstabilizer 67.5% spar datum − repairsadded.

53−71−27_101Fittings, FS755.00 to vertical stabilizer67.5% spar datum − allowabledamage added.

53−71−27_201 Fittings, FS755.00 to vertical stabilizer67.5% spar datum − repairs added.

53−71−31_201Skin and plating, FS755.00 to verticalstabilizer 67.5% spar datum − repairsadded.

53−71−55_201 Tail−bumper support structure −repairs added.




REVNO.



11(Cont’d)

53−71−79_101 Stabilizer to fuselage drag angles −allowable damage added.

53−71−79_201 Stabilizer to fuselage drag angles −repairs added.

53−80−00_201 Fuselage aerodynamic fairings −repairs added.

53−82−00_101 Outboard wing fairing panel −allowable damage added.

53−82−00_201 Outboard wing fairing panel − repairsadded.

53−82−81_201 Forward fairing (wing−to−fuselage) −repairs added.

53−82−82_201 Aft fairing (wing−to−fuselage) −repairs added.

53−82−83_101 Side access and flap stub fairings −allowable damage added.

53−82−83_201 Side access and flap stub fairings −repairs added.

53−83−00_201 Main landing−gear fairing − repairsadded.

53−84−00_201 Tail cone − repairs added.

53−85−00_101 Passenger door hinge fairing −allowable damage added.

53−85−00_201 Passenger door hinge fairing −repairs added.

54−10−31_201 Nacelle skin and plating − repairsadded.

54−11−15_101 Nose cowl frames and formers −allowable damage added.

54−11−15_201 Nose cowl frames and formers −repairs added.

54−11−31_201 Nose cowl skin and plating − repairsadded.

54−12−15_101 Tailpipe frames and formers −allowable damage added.

54−12−15_201 Tailpipe frames and formers − repairsadded.

54−12−31_101 Tailpipe skin and plating − allowabledamage added.

54−12−31_201 Tailpipe skin and plating − repairsadded.

54−13−15_101Thrust reverser frames and formers −allowable damage added.




REVNO.



11(Cont’d)

54−13−15_201 Thrust reverser frames and formers −repairs added.

54−13−31_101 Thrust reverser skins and plating −allowable damage added.

54−13−31_101 Thrust reverser skins and plating −repairs added.

54−14−00_101 Access cowl − allowable damageadded.

54−14−00_201 Access cowl − repairs added.

54−16−15_101 Core cowl frames and formers −allowable damage added.

54−16−15_201 Core cowl frames and formers −repairs added.

54−16−31_101 Core cowl skin and plating −allowable damage added.

54−16−31−201 Core cowl skin and plating − repairsadded.

54−17−00_101 Nacelle/pylon service structure −allowable damage added.

54−17−00_201 Nacelle/pylon service structure −repairs added.

54−18−00_101 Exhaust nozzle − allowable damageadded.

54−18−00_201 Exhaust nozzle − repairs added.

54−50−00−101 Pylons − main structure − allowabledamage added.

54−51−14_101 Pylon box framing structure −allowable damage added.

54−51−14_101 Pylon box framing structure − repairsadded.

54−51−27_101 Pylon−box attach/attached fittings −allowable damage added.

54−51−27_201 Pylon−box attach/attached fittings −repairs added.

54−51−31_101 Pylon box skin and plating −allowable damage added.

54−51−31_201 Pylon box skin and plating − repairsadded.

54−60−00_101 Pylons − secondary structure −allowable damage added.

54−61−14_101 Forward stucture framing − allowabledamage added.

54−61−14−201 Forward stucture framing − repairsadded.




REVNO.



11(Cont’d)

54−61−31_101 Forward stucture skin and plating −allowable damage added.

54−61−31_201 Forward stucture skin and plating −repairs added.

54−62−14−101 Aft structure framing − allowabledamage added.

54−62−14_201 Aft structure framing − repairs added.

54−62−31_101 Aft structure skin and plating −allowable damage added.

54−62−31_201 Aft structure skin and plating − repairsadded.

55−00−27_201 Stabilizer fittings − repairs added.

55−00−31_201 Stabilizer skin and plating − repairsadded.

55−11−31_201 Horizontal stabilizer skin and plating −repairs added.

55−12−00_101 Horizontal−stabilizer secondarystructure − allowable damage added.

55−12−00_201 Horizontal−stabilizer secondarystructure − repairs added.

55−12−01_201 Horizontal−stabilizer leading edge −repairs added.

55−12−51_201 Fillets and fairings, horizontalstabilizer − repairs added.

55−30−00_1 Vertical stabilizer − general added.

55−31−00_1 Vertical−stabilizer main structure −structural identification added.

55−31−00_101 Vertical−stabilizer main structure −allowable damage added.

55−31−00_201 Vertical−stabilizer main structure −repairs added.

55−31−03−201 Vertical stabilizer stringers − repairsadded.

55−31−07_201 Vertical stabilizer spars − repairsadded.

55−31−12_201 Vertical stabilizer ribs − repairsadded.

55−31−27_201 Vertical stabilizer attach/attachedfittings − repairs added.

55−31−31_201 Vertical stabilizer skin and plating −repairs added.

55−31−55_201Rudder−actuator support structure −repairs added.




REVNO.



11(Cont’d)

55−32−00_101 Vertical−stabilizer secondarystructure − allowable damage added.

55−32−00−201 Vertical−stabilizer secondarystructure − repairs added.

57−00−00_1 Wing − general revised

57−20−00_1 Wing main structure − general added.

57−21−00_101 Wing box structure − allowabledamage added.

57−21−00_201 Wing box structure − repairs added.

57−21−55_201 Flap hinge boxes − repairs added.

57−30−00_1 Wingtip − general added.

57−30−00_101 Wingtip − allowable damage added.

57−31−00_1 Winglet − structural identificationadded.

57−31−00_101 Winglet − allowable damage added.

57−31−61_101 Trailing edge − wing box extension −allowable damage added.

57−31−61_201 Trailing edge − wing box extension −repairs added.

57−40−00_1 Leading edge − general added.

57−41−00_1 Leading edge structure − structuralidentification added.

57−41−00_101 Leading edge structure − allowabledamage added.

57−50−00_1 Trailing edge and edge devices −general added.

57−51−00_1 Trailing edge structure − structuralidentification added.

57−51−00_101 Trailing edge structure − allowabledamage added.

57−51−14_101 Framing structure, trailing edge −allowable damage added.

57−51−14_201 Framing structure, trailing edge −repairs added.

57−51−31_101 Trailing edge skin and plating, −allowable damage added.

57−51−31_201 Trailing edge skin and plating −repairs added.

57−54−00_101 Flap hinge arms − allowable damageadded.

57−54−00−201 Flap hinge arms − repairs added.

57−55−00_101 Flap hinge fairings − allowabledamage added.




REVNO.



11(Cont’d)

57−55−00_201 Flap hinge fairings − repairs added.

57−60−00_101 Ailerons − allowable damage added.

57−60−00_201 Ailerons − repairs added.

57−71−00_101 Inboard ground spoiler − allowabledamage added.

57−71−00_201 Inboard ground spoiler − repairsadded.

57−72−00_101 Outboard ground spoiler − allowabledamage added.

57−72−00_201 Outboard ground spoiler − repairsadded.

57−73−00_101 Flight spoiler − allowable damageadded.

57−73−00_201 Flight spoiler − repairs added.

57−74−00_101 Spoileron − allowable damage added.

57−74−00_201 Spoileron − repairs added.


12 53−21−49_1 Seat tracks, FS280.00 to FS409.00 −structural identification added.

53−31−33_1 Forward longeron beam − structuralidentification added.

53−31−43_1Floor structure, FS490.00 toFS409.00+ 128 − structuralidentification added.

53−31−45_1 Pressure box − structuralidentification added.

53−31−49_1 Seat tracks, FS490.00 to FS409.00+128 − structural identification added.

53−41−45_1 Pressure floor structure, FS490.00+128 to FS559.00 − general

53−41−49_1Seat tracks, FS409.00+128 toFS559.00 − structural identificationadded.

53−51−26_1 Surround structure, lavatory servicing− structural identification added.

53−51−31_1Skin and plating, FS599.00 toFS559.00+ 112 − structuralidentification added.

53−51−49_1 Seat tracks, FS599.00 to FS559.00+112 − structural identification added.

53−61−23_1

Surround structure, cargo andaft−equipment doors − structuralidentification added.




REVNO.



12(Cont’d) 53−61−27_1

Attach/attached fittings, FS599.00+112 to FS755.00 − structuralidentification added.

53−61−31_1Skin and plating, FS599.00+ 112 toFS755.00 − structural identificationadded.

53−71−27_1Attach/attached fittings, FS755.00 tovertical stabilizer 67.5% spar datum −structural identification added.

55−12−00_1Horizontal stabilizer secondarystructure − structural identificationadded.

55−32−00_1 Vertical stabilizer secondary structure− structural identification added.

57−21−00_1 Wings box structure − structuralidentification added.

57−54−00_1 Flap hinge arms − structuralidentification added.

57−55−00_1 Flap hinge fairings − structuralidentification added.

57−60−00_1 Ailerons − structural identificationadded.

57−70−00_1 Spoilers − structural identificationadded.

57−71−00_1 Inboard ground spoiler − structuralidentification added.

57−72−00_1 Outboard ground spoiler − structuralidentification added.

57−73−00_1 Flight spoiler − structural identificationadded.

57−74−00_1 Spoileron − structural identificationadded.


1353−00−15_1

Fuselage frames − Repairs revisedand incorporated REO601R−53−00−028.

53−00−31_1Fuselage skin and plating −Repairsrevised and incorporated REO601R−53−00−001, −022, −023, −025.

53−21−17_1 Intercostals, FS280.00 to FS409.00 −structural identification revised.

53−21−23_1Door surround structures, FS280.00to FS409.00 − structural identificationrevised.

53−21−27_1Fittings, FS280.00 to FS409.00 −structural identification revised.

G.P. Jones/ 31 May 2000



REVNO.



13(Cont’d) 53−22−55_1

Underfloor crawlway and supportstructure, FS280.00 to FS409.00 −structural identification added.

53−22−55_101Underfloor crawlway and supportstructure, FS280.00 to FS409.00 −allowable damage added.

53−22−55_201Underfloor crawlway and supportstructure, FS280.00 to FS409.00 −repair revised.

53−61−43_1Floor support structure, FS599.00+112 to FS621.00 − structuralidentification added.

53−61−49_1Cargo tie−down tracks, FS599.00+112 to FS621.00 − structuralidentification added.

53−62−55_1 Equipment support structure −structural identification added.

53−62−57_1 APU Compartment − structuralidentification added.

53−71−31_1Skin and plating, FS755.00 to verticalstabilizer 67.5% spar datum −structural identification added.

53−80−00_1 Fuselage aerodynamic fairings −structural identification added.

53−81−00_1 Radome − structural identificationadded.

53−82−81_1 Forward fairing (wing to fuselage) −structural identification added.

53−82−82_1 Aft fairing (wing to fuselage) −structural identification added.

53−82−83_1 Side access and flap stub fairings −structural identification added.

53−85−00_1 Passenger door hinge fairing −structural identification added.

G.P. Jones/ 31 May 2000

14 52−00−00_1 Doors − general, structuralidentification revised.

52−00−27_1 Door fittings − structural identificationadded.

D. Radulescu/ 15 Dec 2000

52−00−31_1 Door skin and plating − structuralidentification added.


52−01−00_1 Door seals − structural identificationrevised.

G.P. Jones/ 1 Jun 2001



REVNO.



14(Cont’d)

52−10−14_1 Passenger−door frame structure −structural identification revised/added.

52−45−00_1 Servicing door − general fully revised.


53−00−03_201 Stringers − splice repairs revised andincorporated REO 601R53−00−029.


53−00−43_201Floor support structure − repair no. 1floorbeam flange repair revised andincorporated REO 601R53−00−027.


53−21−43_1Floor support structure, FS280.00 toFS409.00 − structural identificationadded.



53−61−43_1Floor support structure,FS559.00+112 to FS621.00 − repairsrevised.

A. Vincze/ 19 Dec 2000

53−84−00_1 Tail cone − structural identificationrevised/added.


54−00−00_1 Nacelles/pylons − general, structuralidentification revised.


54−10−00_1 Nacelles internal structure − generalrevised.


54−10−27_1 Nacelles fittings − general revised.

54−10−31_1 Nacelles skin and plating − generalrevised.


54−11−00_1 Nose cowl − general added.

54−12−00_1 Tailpipe − general added.




REVNO.



14(Cont’d)

54−12−15_1 Tailpipe frames and formers −structural identification added.

54−12−31_1 Tailpipe skin and plating − structuralidentification added.


54−14−00_1 Access cowls − structuralidentification added.

D. Radulescu/ 1 May 2001

54−17−00_1 Nacelle/pylon service structure −structural identification added.

D. Radulescu/ 1 Jun 2001

54−18−00_1 Exhaust nozzle − structuralidentification added.


55−00−00_1 Stabilizers − general revised. D. Radulescu/ 18 Dec 2000

55−00−27_1 Stabilizer fittings − structuralidentification revised.

D. Radulescu/ 3 Mar 2001

55−00−31_1 Stabilizers skin and plating − generalrevised/added.


55−11−31_1 Horizontal stabilizer skin and plating −structural identification added.

D. Radulescu/ 1 Jun 2001

56−00−00_1 Windows − general added. D. Radulescu/ 15 Dec 2000

56−00−35_201Flight compartment and passengercompartment windows − repairsadded.


56−10−00_1 Flight compartment windows −general added.




REVNO.



14(Cont’d)

56−11−00_1 Windshields − general added. A. Vincze/ 18 Dec 2000

56−11−00_101 Windshields − allowable damageadded.

56−11−00_201 Windshields − repairs added.

56−11−35_201 Loose windshield power terminalblock − repairs added.


56−11−36_201 Windshield disconnected powerterminal block − repairs added.


56−12−00_1 Side windows − general added. D. Radulescu/ 19 Dec 2000

56−12−00_101 Side windows − allowable damageadded.

56−12−00_201 Side windows − repairs added.


56−20−00_1 Passenger compartment windows −general added.


56−20−00_101 Passenger compartment windows −allowable damage added.

56−20−00_201 Passenger compartment windows −repairs added.


15 53−00−31_201 Fuselage skin and plating − repairNo.6 added.


16 51−00−16_1 GLOSSARY

51−21−16_1 FINISH CODES

51−22−00_1 BONDING AND ATTACHING PARTSWITH ADHESIVE

51−22−21_1 ATTACHING OF PHENOLICPLASTICS WITH ADHESIVE

51−22−24_1 ATTACHING COTTON CLOTH TOALUMINUM WITH ADHESIVE

51−22−26_1 ATTACHING SYNTHETIC RUBBERWITH ADHESIVE

51−22−28_1 ATTACHING SILICONE RUBBERWITH ADHESIVES

G.P. jones/18 Feb 2003



REVNO.



16(Cont’d)

51−22−34_1 ATTACHING FLUOROSILICONERUBBER WITH ADHESIVES

51−22−36_1

ATTACHING SYNTHETIC RUBBERAND PHENOLIC SHEET WITH JETA1 FUESL−RESISTANTADHESIVES

51−22−38_1

ATTACHING NYLON GROMMETSAND NYLONCATERPILLAR−PROTECTORSTRIPS WITH ADHESIVES

51−22−41_1

GENERAL NON−STRUCTURALBONDING OF DIFFERENTMATERIALS FOR OPERATIONALTEMPERATURES OF −55°C (−67°F)TO 71°C (160°F)

51−22−46_1 ATTACHING PARTS WITHCONDUCTIVE ADHESIVE

51−22−52_1 ATTACHING TEFLON WITHADHESIVE/SEALANT

51−22−56_1ATTACHING COMPOSITELAMINATES AND ALUMINUM WITHFLUID−RESISTANT ADHESIVE

51−22−61_1ATTACHING TITANIUM TOGRAPHITE−EPOXY LAMINATESWITH ADHESIVE

51−22−66_1ATTACHING NYLON AND FLEXIBLEPOLYVINYL CHLORIDE (PVC) WITHADHESIVES

51−22−72_1ATTACHING SPONGE ANDCLOSED−CELL RUBBER WITHADHESIVE

51−22−76_1 ATTACHING VELCRO TAPE WITHADHESIVE

51−23−01_1 FUSELAGE PRESSURE LEAKAGE− TESTING AND REPAIR

51−23−02_1 FUEL TANK LEAKAGE − TESTINGAND REPAIR

51−27−19_1 ABRASION RESISTANT FILMINSTALLATION PROCEDURE

51−32−00_1 NON−METALLIC ANDMISCELLANEOUS MATERIALS

51−35−00_1 TOOLS AND EQUIPMENT

51−42−02_1 FASTENER CODE SYSTEM

52−10−14_201PASSENGER− DOOR FRAMESTRUCTURE

52−10−27_201 PASSENGER−DOOR FITTINGS




REVNO.



16(Cont’d)

52−10−31_201 PASSENGER−DOOR SKIN ANDPLATING

52−12−55_201 PASSENGER−DOOR STAIRS

52−30−00_201 CARGO DOOR

52−81−00_201 NOSE LANDING GEAR DOOR

53−00−31_201FUSELAGE SKIN AND PLATING −REPAIR NO. 7 − SKIN REPAIRNON−FLUSH

53−11−15_201 FRAMES, FS144.00 TO FS280.00

53−11−17_201 INTERCOSTALS, FS144.00 TOFS280.00

53−11−19_201 BULKHEADS, FS144.00 TOFS280.00

53−11−23_201 SURROUND STRUCTURES,FS144.00 TO FS280.00

53−11−31_201 SKIN AND PLATING, FS169.00 TOFS280.00

53−11−47_201 FLOOR PANELS, FS169.00 TOFS280.00

53−21−23_201 DOOR SURROUND STRUCTURES,FS280.00 TO FS409.00

53−21−31_201 SKIN AND PLATING, FS280.00 TOFS409.00

53−21−31_201−01

SKIN AND PLATING, FS280.00 TOFS409.00 − REPAIR NO. 1 −REPAIR TO FUSELAGE SKINAROUND PASSENGER DOORCUT−OUT

53−21−31_201−02

SKIN AND PLATING, FS280.00 TOFS409.00 − REPAIR NO. 2 −REPAIR TO FUSELAGE SKINAROUND SERVICE DOORCUT−OUT

53−21−43_201 FLOOR SUPPORT STRUCTURE,FS280.00 TO FS409.00

53−31−43_201 FLOOR SUPPORT STRUCTURE,FS409.00 TO FS409.00+128

53−31−45_201 PRESSURE BOX

53−41−19_201 BULKHEADS, FS409.00+128 TOFS559.00

53−41−43_201 FLOOR SUPPORT STRUCTURE,FS409.00+128 TO FS559.00

53−41−47_201FLOOR PANELS, FS409.00+128 TOFS559.00




REVNO.



16(Cont’d)

53−51−43_201 FLOOR SUPPORT STRUCTURE,FS559.00 TO FS559.00+112

53−61−15_201 FRAMES, FS559.00+112 TOFS755.00

53−61−31_201 SKIN AND PLATING, FS559.00_112TO FS755.00

53−81−00_201 RADOME

53−82−83_201 SIDE ACCESS AND FLAP STUBFAIRINGS

53−83−00_201 MAIN LANDING−GEAR FAIRING

53−84−00_201 TAIL CONE

57−21−12_201 WING BOX RIBS

57−21−31_201 WING BOX SKIN AND PLATING

57−31−14_201 WINGLET FRAMING STRUCTURE

57−31−51_201 FILLETS AND FAIRINGS, WINGLET

57−51−31_201 TRAILING EDGE SKIN ANDPLATING

57−52−00_101 INBOARD FLAP AND VANE

57−53−00_201 OUTBOARD FLAP AND VANE

57−60−00_201 AILERONS


17 51−00−18_1 ABREVIATIONS AND ACRONYMS

51−22−16_1 ATTACHINGABRASION−RESISTANT FILM

51−42−07_1 BIMETAL SOLID RIVETS

53−21−31_201 SKIN AND PLATING, FS280.00 TOFS409.00 − REPAIRS

53−21−31_201−01


53−21−31_201−02


53−81−00_101 RADOME − ALLOWABLE DAMAGE

54−11−15_101 NOSE COWL FRAME ANDFORMERS − ALLOWABLE DAMAGE

54−11−31_101 NOSE AND COWL SKIN ANDPLATING − ALLOWABLE DAMAGE

54−12−15_101 TAILPIPE FRAMES AND FORMERS− ALLOWABLE DAMAGE

G.P. Jones/17 Jun 2003



REVNO.



17(Cont’d)

54−12−31_101 TAILPIPE SKIN AND PLATING −ALLOWABLE DAMAGE

54−14−00_101 ACCESS COWL − ALLOWABLEDAMAGE

54−16−15_101 CORE COWL FRAMES ANDFORMERS − ALLOWABLE DAMAGE

54−16−31_101 CORE COWL SKIN AND PLATING −ALLOWABLE DAMAGE

54−17−00_101NACELLE/PYLON SERVICESTRUCTURE − ALLOWABLEDAMAGE

54−18−00_101 EXHAUST NOZZLE − ALLOWABLEDAMAGE

57−21−32_201 WING BOX ACCESS DOORS −REPAIRS

G.P. Jones/17 Jun 2003

19 51−25−16_1 FLUID RESISTANT (FR)POLYURETHANE TOPCOAT

53−00−31_201−01

SKIN AND PLATING − REPAIR NO.1 − EXTERNAL NON−FLUSHPERMANENT REPAIRS −PRESSURIZED AREA

53−00−31_201−02

SKIN AND PLATING − REPAIR NO.2 EXTERNAL NON−FLUSHTEMPORARY REPAIRS −PRESSURIZED AREA

53−00−31_201−03

SKIN AND PLATING − REPAIR NO.3 − EXTERNAL NON−FLUSHPERMANENT REPAIRS −NON−PRESSURIZED AREA

53−00−31_201−04

SKIN AND PLATING − REPAIR NO.4 − EXTERNAL NON−FLUSHTEMPORARY REPAIRS −NON−PRESSURIZED AREA

53−00−31_201−05

SKIN AND PLATING − REPAIR NO.5 − EXTERNAL FLUSHPERMANENT REPAIRS −PRESSURIZED AREA

53−00−31_201−06SKIN AND PLATING − REPAIR NO.6 − FUSELAGE SKIN SPLICEREPAIRS

53−00−31_201−07

SKIN AND PLATING − REPAIR NO.7 − GENERIC SKIN REPAIR,NON−FLUSH, AROUNDPASSENGER CABIN WINDOWCUT−OUT

53−31−43_201FLOOR SUPPORT STRUCTUREFS409.00 TO 409.00+128 −REPAIRS

G.P. Jones/22 Dec 2003



REVNO.



19(Cont’d)

53−61−31_201 SKIN AND PLATING, FS559.00+112TO FS755.00 − REPAIRS

53−61−33_201LONGERON BEAM STRUCTUREVERTICAL STABILIZER ATTACH −REPAIRS

55−12−01_201 HORIZONTAL STABILIZERLEADING EDGE − REPAIRS

G.P. Jones/22 Dec 2003

20 51−14−06_1 AERODYNAMIC SMOOTHNESS −AIRFRAME

51−21−11_1 CORROSION PREVENTIONPROCEDURES

51−23−00_1PRESSURE, ENVIRONMENTAL,FUEL TANK AND FIREWALLSEALING

51−24−39_1

COLD WORK OF COUNTERSUNKFASTENER HOLES AROUND THECABIN WINDOWS (TO BE USEDONLY FOR THE INCORPORATIONOF SB 601R−53−025)

51−42−02_1 FASTENER CODE SYSTEM −GENERAL

51−42−26_201 COMPOSI−LOK FASTENERS

51−74−24_201−01 KEVLAR FACE SHEET DISBONDTO NOMEX CORE − REPAIRS

52−82−00_101 MAIN LANDING GEAR DOORS −ALLOWABLE DAMAGE

53−00−49_101

FLIGHT COMPARTMENT SEAT,PASSENGER SEAT AND CARGOTIE−DOWN TRACKS ANDSTRUCTURE − ALLOWABLEDAMAGE

53−11−43_101FLOOR SUPPORT STRUCTURE,FS169.00 TO FS280.00 −ALLOWABLE DAMAGE

53−11−49_101 FLIGHT COMPARTMENT SEATTRACKS − ALLOWABLE DAMAGE

53−11−67_101NOSE LANDING GEAR SUPPORTSTRUCTURE − ALLOWABLEDAMAGE

53−12−55_101

UNDERFLOOR CRAWLWAY ANDSUPPORT STRUCTURE, FS144.00TO FS280.00 − ALLOWABLEDAMAGE

53−21−49_101 SEAT TRACKS, FS280.00 TOFS409.00 − ALLOWABLE DAMAGE

53−31−33_101 FORWARD LONGERON BEAM −ALLOWABLE DAMAGE




REVNO.



20(Cont’d) 53−31−49_101

SEAT TRACKS, FS409.00 TOFS409.00+128 − ALLOWABLEDAMAGE

53−41−17_101 INTERCOSTALS, FS409.00+128 TOFS559.00 − ALLOWABLE DAMAGE

53−41−33_101 UNDERFLOOR LONGERON −ALLOWABLE DAMAGE

53−41−43_101FLOOR SUPPORT STRUCTURE,FS409.00+128 TO FS559.00 −ALLOWABLE DAMAGE

53−41−45_101PRESSURE FLOOR STRUCTURE,FS409.00+128 TO FS559.00 −ALLOWABLE DAMAGE

53−41−46_101 PRESSURE BOX − ALLOWABLEDAMAGE

53−41−49_101 SEAT TRACKS, FS409.00+128 TOFS559.00 − ALLOWABLE DAMAGE

53−51−43_101FLOOR SUPPORT STRUCTURE,FS559.00 TO FS559.00+112 −ALLOWABLE DAMAGE

53−51−49_101SEAT TRACKS, FS559.00 TOFS559.00+112 − ALLOWABLEDAMAGE

53−52−55_101

EQUIPMENT SUPPORTSTRUCTURE, FS559.00 TOFS559.00+112 − ALLOWABLEDAMAGE

53−61−31_201 SKIN AND PLATING, FS559.00+112TO FS755.00 − REPAIRS

53−61−31_201−01

SKIN AND PLATING, FS559.00+112TO FS755.00 − REPAIR NO. 1 −PERMANENT REPAIRS FORFUSELAGE AROUND THEBAGGAGE COMPARTMENT DOORCUT−OUT

53−61−49_101CARGO TIE−DOWN TRACKS,FS559.00 TO FS559.00+112 −ALLOWABLE DAMAGE

53−61−55_101ENGINE SUPPORT STRUCTUREAND TRANSVERSE BEAMS −ALLOWABLE DAMAGE

53−62−57_101 APU COMPARTMENT −ALLOWABLE DAMAGE

53−71−03_101

STRINGERS, FS755.00 TOVERTICAL STABILIZER 67.5%SPAR DATUM − ALLOWABLEDAMAGE




REVNO.



20(Cont’d) 53−71−15

FRAMES, FS755.00 TO VERTICALSTABILIZER 67.5% SPAR DATUM −ALLOWABLE DAMAGE

53−71−17–101

INTERCOSTALS, FS755.00 TOVERTICAL STABILIZER 67.5%SPAR DATUM − ALLOWABLEDAMAGE

53−71−19_101 BULKHEADS − ALLOWABLEDAMAGE

53−71−31_101

SKIN AND PLATING, FS755.00 TOVERTICAL STABILIZER 67.5%SPAR DATUM − ALLOWABLEDAMAGE

54−00−00_101 NACELLES/PYLONS − ALLOWABLEDAMAGE

54−13−15_101 THRUST REVERSER FRAMES ANDFORMERS − ALLOWABLE DAMAGE

54−13−31_101 THRUST REVERSER SKINS ANDPLATING − ALLOWABLE DAMAGE

54−50−00_101 PYLONS MAIN STRUCTURE −ALLOWABLE DAMAGE

54−51−14_101PYLON BOX FRAMINGSTRUCTURE − ALLOWABLEDAMAGE

54−51−31_101 PYLON BOX SKIN AND PLATING −ALLOWABLE DAMAGE

54−60−00_101PYLONS − SECONDARYSTRUCTURE − ALLOWABLEDAMAGE

54−61−14_101 FORWARD STRUCTURE FRAMING− ALLOWABLE DAMAGE

54−61−31−101 FORWARD STRUCTURE SKIN ANDPLATING − ALLOWABLE DAMAGE

54−62−14_101 AFT STRUCTURE FRAMING −ALLOWABLE DAMAGE

55−11−03_101HORIZONTAL STABILIZERSTRINGERS − ALLOWABLEDAMAGE

55−11−07_101 HORIZONTAL STABILIZER SPARS− ALLOWABLE DAMAGE

55−11−12_101 HORIZONTAL STABILIZER RIBS −ALLOWABLE DAMAGE

55−11−31_101HORIZONTAL STABILIZER SKINAND PLATING − ALLOWABLEDAMAGE

55−11−31_201 HORIZONTAL STABILIZER SKINAND PLATING − REPAIRS




REVNO.



20(Cont’d)

55−11−32_101 HORIZONTAL STABILIZER ACCESSPANELS − ALLOWABLE DAMAGE

55−12−01_101HORIZONTAL STABILIZERLEADING EDGE − ALLOWABLEDAMAGE

55−20−00_101 ELEVATORS − ALLOWABLEDAMAGE

55−20−00_201 ELEVATOR − REPAIRS

55−31−03_101VERTICAL STABILIZERSTRINGERS − ALLOWABLEDAMAGE

55−31−07_101 VERTICAL STABILIZER SPARS −ALLOWABLE DAMAGE

55−31−12_101 VERTICAL STABILIZER RIBS −ALLOWABLE DAMAGE

55−31−31_101 VERTICAL STABILIZER SKIN ANDPLATING − ALLOWABLE DAMAGE

55−31−31_201 VERTICAL STABILIZER SKIN ANDPLATING − REPAIRS

55−31−32_101 VERTICAL STABILIZER ACCESSPANELS − ALLOWABLE DAMAGE

55−31−55_101VERTICAL STABILIZER SUPPORTSTRUCTURE − ALLOWABLEDAMAGE

55−32−01_101 VERTICAL STABILIZER LEADINGEDGE − ALLOWABLE DAMAGE

55−32−01_201 VERTICAL STABILIZER LEADING −REPAIRS

55−32−51_101

FILLETS AND FAIRINGS, VERTICALSTABILIZER TO HORIZONTALSTABILIZER − ALLOWABLEDAMAGE

55−40−00–101 RUDDER − ALLOWABLE DAMAGE

55−40−00_201 RUDDER – REPAIR TO RUDDERSKIN, NON−FLUSH

56−11−01_101 WINDSHIELDS − ALLOWABLEDAMAGE

56−11−02_101 SIDE WINDOWS − ALLOWABLEDAMAGE

56−20−00_101 PASSENGER COMPARTMENTWINDOWS − ALLOWABLE DAMAGE

57−00−00_101 WINGS − ALLOWABLE DAMAGE

57−00−31_101WING SKIN AND PLATING −ALLOWABLE DAMAGE




REVNO.



20(Cont’d) 57−21−03_101

WING PLANK INTEGRALSTRINGERS − ALLOWABLEDAMAGE

57−21−07_101 WING BOX SPARS − ALLOWABLEDAMAGE

57−21−12_101 WING BOX RIBS − ALLOWABLEDAMAGE

57−21−17_101 WING BOX INTERCOSTALS

57−21−32_101 WING BOX ACCESS DOORS −ALLOWABLE DAMAGE

57−21−32_201 WING BOX ACCESS DOORS −REPAIRS

57−21−55_101 FLAP HINGE BOXES − ALLOWABLEDAMAGE

57−31−14_101 WINGLET FRAMING STRUCTURES− ALLOWABLE DAMAGE

57−31−31_101 SKIN AND PLATING, WINGLET −ALLOWABLE DAMAGE

57−41−12_101 RIBS, WING LEADING EDGE −ALLOWABLE DAMAGE

57−41−29_101 LEADING EDGE SHROUD ANDFRAME − ALLOWABLE DAMAGE

57−41−31_201 WING LEADING EDGE − REPAIRS

57−51−14_101 FRAMING STRUCTURE, TRAILINGEDGE − ALLOWABLE DAMAGE

57−51−31_101 SKIN AND PLATING, TRAILINGEDGE − ALLOWABLE DAMAGE

57−52−00_101 INBOARD FLAP AND VANE −ALLOWABLE DAMAGE

57−52−00_201−01INBOARD FLAP AND VANE −REPAIR NO. 1 − REPAIR TO FLAPVANE SKIN

57−52_201−02INBOARD FLAP AND VANE −REPAIR NO. 2 − FLUSH REPAIR TOINBOARD FLAP SKIN

57−52−00_201−03INBOARD FLAP AND VANE −REPAIR NO. 3 − NON−FLUSHREPAIR TO INBOARD FLAP SKIN

57−53−00_101 OUTBOARD FLAP AND VANE −ALLOWABLE DAMAGE

57−53−00_201−01

OUTBOARD FLAP AND VANE −REPAIR NO. 1 − REPAIR TOOUTBOARD FLAP VANE SKIN




REVNO.



20(Cont’d) 57−53−00_201−02

OUTBOARD FLAP AND VANE −REPAIR NO. 2 − FLUSH REPAIR TOOUTBOARD FLAP SKIN

57−53−00_201−03OUTBOARD FLAP AND VANE −REPAIR NO. 3 − NON−FLUSHREPAIR TO OUTBOARD FLAP SKIN

57−54−00_101 FLAP HINGE ARMS − ALLOWABLEDAMAGE

57−60−00_101 AILERONS − ALLOWABLE DAMAGE

57−60−00_201−01AILERON − REPAIR NO. 1 −REAPIR TO AILERON SKIN ANDPLATING

57−71−00_101 INBOARD GROUND SPOILER −ALLOWABLE DAMAGE

57−72−00_101 OUTBOARD GROUND SPOILER −ALLOWABLE DAMAGE

57−73−00_101 FLIGHT SPOILER − ALLOWABLEDAMAGE

57−74−00_101 SPOILERON − ALLOWABLEDAMAGE



54−00−31_101 NACELLES/PYLONS SKIN ANDPLATING − ALLOWABLE DAMAGE

57−21−31_201 WING BOX SKIN AND PLATING −REPAIRS

57−21−32_201 WING−BOX ACCESS DOORS −REPAIRS

G.P. Jones/ 15 Dec 2004

23 51−00−00_1 STRUCTURES− GENERAL G.P. Jones/15 Mar 2005

52−44−32_101FORWARD EQUIPMENT −COMPARTMENT ACCESS DOORS− ALLOWABLE DAMAGE

52−44−37_01 AIR−DRIVEN GENERATOR (ADG)DOOR − ALLOWABLE DAMAGE

52−81−00_01 NOSE LANDING−GEAR DOORS −ALLOWABLE DAMAGE

David Patterson/15 Mar 2005

53−00−15_201−02 FRAMES − REPAIR NO. 2 FRAMEOUTER FLANGE REPAIRS

53−00−31_201SKIN AND PLATING − REPAIRS −INTRODUCTION

G.P. Jones/15 Mar 2005


APPROVAL LOG Page 29Apr 10/2005

REVNO.



23(Cont’d) 53−00−31_201−01

SKIN AND PLATING − REPAIR NO.1 − EXTERNAL NON−FLUSHPERMANENT REPAIRS −PRESSURIZED AREA

53−00−31_201−03


53−00−43_201−01FLOOR SUPPORT STRUCTURE −REPAIR NO. 1 FLOOR BEAMFLANGE REPAIR

53−00−43_201−02FLOOR SUPPORT STRUCTURE −REPAIR NO. 2 FLOOR BEAMSPLICE REPAIR


53−22−55_101

UNDERFLOOR CRAWLWAY ANDSUPPORT STRUCTURE, FS280.00TO FS409.00 − ALLOWABLEDAMAGE

53−81−00_101 RADOME − ALLOWABLE DAMAGE

53−82−83_101 SIDE ACCESS AND FLAP STUBFAIRINGS − ALLOWABLE DAMAGE

53−83−00_101 MAIN LANDING−GEAR FAIRING −ALLOWABLE DAMAGE

54−62−31_101 AFT STRUCTURE SKIN ANDPLATING − ALLOWABLE DAMAGE


55−11−31_201 HORIZONTAL STABILIZER SKINAND PLATING − REPAIRS


55−12−51_101FILLETS AND FAIRINGS,HORIZONTAL STABILIZER −ALLOWABLE DAMAGE


55−20−00_201 ELEVATORS − REPAIRS

55−31−31_201 VERTICAL STABILIZER SKIN ANDPLATING − REPAIRS


55−32−51_101

FILLETS AND FAIRINGS,VERTICAL−TO−HORIZONTALSTABILIZERS − ALLOWABLEDAMAGE

55−32−52_101 RAM AIR INTAKE AND DORSALFAIRING − ALLOWABLE DAMAGE


55−40−00_201 RUDDER − REPAIR TO RUDDERSKIN, NON−FLUSH



APPROVAL LOG Page 30Apr 10/2005

REVNO.



23(Cont’d)

53−84−00_101 TAIL CONE − ALLOWABLEDAMAGE


57−21−55_101 FLAP HINGE BOXES − ALLOWABLEDAMAGE


57−31−51_101 FILLETS AND FAIRINGS, WINGLET− ALLOWABLE DAMAGE

57−51−31_101 SKIN AND PLATING, TRAILINGEDGE − ALLOWABLE DAMAGE


57−52−00_201−01INBOARD FLAP AND VANE −REPAIR NO. 1 − REPAIR TO FLAPVANE SKIN

57−52−00_201−02INBOARD FLAP AND VANE −REPAIR NO. 2 − FLUSH REPAIR TOINBOARD FLAP SKIN

57−52−00_201−03INBOARD FLAP AND VANE −REPAIR NO. 3 − NON−FLUSHREPAIR TO INBOARD FLAP SKIN

57−53−00_201−01OUTBOARD FLAP AND VANE −REPAIR NO. 1 − REPAIR TO FLAPVANE SKIN

57−53−00_201−02OUTBOARD FLAP AND VANE −REPAIR NO. 2 − FLUSH REPAIR TOOUTBOARD FLAP SKIN

57−53−00_201−03OUTBOARD FLAP AND VANE −REPAIR NO. 3 − NON−FLUSHREPAIR TO OUTBOARD FLAP SKIN


57−55−00_101 FLAP HINGE FAIRINGS −ALLOWABLE DAMAGE


57−60−00_201−01AILERON − REPAIR NO. 1 −REPAIR TO AILERON SKIN ANDPLATING



53−00−31−201−02

SKIN AND PLATING − REPAIR NO.2 − EXTERNAL NON−FLUSHTEMPORARY REPAIRS −PRESSURIZED AREA

G.P. Jones/10 Aug 2005


APPROVAL LOG Page 31Aug 10/2005

REVNO.



24(Cont’d)

53−00−31−201−07

SKIN AND PLATING − REPAIR NO.7 − GENERIC SKIN REPAIR,NON−FLUSH, AROUNDPASSENGER CABIN WINDOWCUT−OUT

53−00−31−201−03


53−61−31−201−01

SKIN AND PLATING, FS559.00+112− REPAIR NO. 1 − PERMANENTREPAIRS FOR FUSELAGEAROUND THE BAGGAGECOMPARTMENT DOOR CUT−OUT

55−12−01−201 HORIZONTAL−STABILIZERLEADING EDGE − REPAIRS

55−32−01−201−01

VERTICAL−STABILIZER LEADINGEDGE − REPAIR NO. 1 − REPAIRTO THE LEADING EDGE OF THEVERTICAL STABILIZER

57−41−31−201 WING LEADING EDGE SKINS −REPAIRS

G.P. Jones/10 Aug 2005

25 51−21−00−01 CORROSION CONTROL

53−00−31−201−04

SKIN AND PLATING − REPAIR NO.4− EXTERNAL NON−FLUSHTEMPORARY REPAIRS −NON−PRESSURIZED AREA

53−21−31−201−01



26 51−11−11−001 MECHANICAL HARDNESSTESTING

51−13−01−001DEFECT AND DAMAGE REPAIRREQUESTS − REPORTPROCEDURE

51−22−00−001 BONDING AND ATTACHING PARTSWITH ADHESIVES

51−23−00−001PRESSURE, ENVIRONMENTAL,FUEL TANK AND FIREWALLSEALING

51−24−11−001 SHOT PEENING

51−24−41−001 RAIN−EROSION RESISTANTCOATING

51−25−34−001 INTEGRAL FUEL TANK COATING

51−25−46−001 CONDUCTIVE COATINGS

G.P. Jones/Jul 10, 2006


APPROVAL LOG Page 32Jul 10/2006

REVNO.



26(Cont’d)

51−25−52−001 COMPOSITE − LAMINATECOATINGS

51−25−56−001 LIGHT REFLECTIVE COATING

51−31−59−001 EXTRUDED AND FORMEDSECTIONS

51−74−00−001 KEVLAR − GENERAL

51−74−14−201 KEVLAR EDGE DELAMINATION −REPAIR

51−74−18−201SINGLE KEVLAR SKIN ANDHONEYCOMB PUNCTURED −REPAIRS

52−10−31−201 PASSENGER DOOR SKIN ANDPLATING − REPAIRS

52−21−00−101 OVERWING EMERGENCY EXITDOORS

53−21−23−201−01DOOR SURROUND STRUCTURE −REPAIR NO. 1 − REPLACEMENTOF THE PASSENGER DOOR HINGE

53−21−31−201−02


53−51−43−101FLOOR SUPPORT STRUCTURE,FS559.00 TO FS559+112 −ALLOWABLE DAMAGE

57−60−00−201−01AILERON − REPAIR NO. 1 −REPAIR TO AILERON SKIN ANDPLATING


2751−23−00−001

PRESSURE, ENVIRONMENTAL,FUEL TANK AND FIREWALLSEALING

51−24−38−001 COLD WORKING OF FASTENERHOLES

51−25−26−001 TEFLON−FILLEDABRASION−RESISTANT COATING

51−32−00−001 NON−METALLIC ANDMISCELLANEOUS MATERIALS

51−42−10−001 BLIND RIVETS − GENERAL

51−42−11−001 CHERRYLOCK AND OLYMPIC−LOKBLIND RIVETS (NAS1398/NAS1399)

51−42−12−001 CHERRYBULB BLIND RIVETS(NAS1738/NAS1739)

51−42−14−001 HUCK BULBED BLIND RIVETS

51−74−00−001 KEVLAR − GENERAL

G.P. Jones/Jun 10, 2007


APPROVAL LOG Page 33Jun 10/2007

REVNO.



27(Cont’d) 51−75−00−001

GRAPHITE LAMINATE ANDGRAPHITE LAMINATE − FACEDHONEYCOMB REPAIR

51−75−08−201 DELAMINATED GRAPHITEAROUND HOLES − REPAIR

51−75−16−201 DAMAGED GRAPHITE PLIES −REPAIR

53−00−15−201−1 FRAMES − REPAIR NO. 1 SPLICEREPAIRS

53−00−31−201−1

SKIN AND PLATING − REPAIR NO.1 − EXTERNAL NON−FLUSHPERMANENT REPAIRS −PRESSURIZED AREAS

53−00−31−201−5SKIN AND PLATING − REPAIR NO.5 − FUSELAGE SKIN SPLICEFLUSH REPAIRS

53−00−31−201−6

SKIN AND PLATING − REPAIR NO.6 − EXTERNAL FLUSHPERMANENT REPAIRS −PRESSURIZED REPAIRS

53−00−31−201−7

SKIN AND PLATING − REPAIR NO.7− GENERIC SKIN REPAIR,NON−FLUSH, AROUNDPASSENGER CABIN WINDOWCUT−OUT

53−21−31−201−1

SKIN AND PLATING, FS280.00 TOFS409.00 − REPAIR NO. 1− REPAIRTO FUSELAGE SKIN AROUNDPASSENGER DOOR CUT−OUT

53−61−31−201−1

SKIN AND PLATING, FS559.00+112TO FS755.00 − REPAIR NO. 1PERMANENT REPAIRS FORFUSELAGE AROUND THEBAGGAGE COMPARTMENT DOORCUT−OUT

54−11−31−101 NOSE COWL SKIN AND PLATING −ALLOWABLE DAMAGE


28 51−14−06 AERODYNAMIC SMOOTHNESS −AIRFRAME


2953−00−43

FLOOR SUPPORT STRUCTURE −REPAIR NO. 2 FLOOR BEAMSPLICE REPAIR



APPROVAL LOG Page 34Jun 10/2009

STRUCTURAL REPAIR MANUAL

RECORD OF REVISIONS

* BCSG: Bombardier Customer Service Group Page 1 Apr 10/2011 RECORD OF REVISIONS CSP A-008 - MASTER

EFFECTIVITY: **ON A/C ALL

Record the date you insert and remove each Revision in your manual. REV NO.

ISSUE DATE

DATE INSERTED

INSERTED BY

1 Oct 01/92 Oct 01/92 BCSG

2 Jan 04/93 Jan 04/93 BCSG

3 Apr 05/93 Apr 05/93 BCSG

4 Jul 05/94 Jul 05/94 BCSG

5 Jun 08/95 Jun 08/95 BCSG

6 Jan 15/96 Jan 15/96 BCSG

7 Sep 05/96 Sep 05/96 BCSG

8 Dec 05/96 Dec 05/96 BCSG

9 Apr 30/98 Apr 30/98 BCSG

10 Sep 20/99 Sep 20/99 BCSG

11 Nov 30/99 Nov 30/99 BCSG

12 Feb 28/00 Feb 28/00 BCSG

13 May 31/00 May 31/00 BCSG

14 Feb 28/01 Feb 28/01 BCSG

15 Aug 24/01 Aug 24/01 BCSG

16 Feb 18/03 Feb 18/03 BCSG

17 Jun 17/03 Jun 17/03 BCSG

18 Sep 16/03 Sep 16/03 BCSG

19 Dec 22/03 Dec 22/03 BCSG

20 Jun 22/04 Jun 22/04 BCSG

21 Sep 28/04 Sep 28/04 BCSG

22 Dec 15/04 Dec 15/04 BCSG

23 Apr 10/05 Apr 10/05 BCSG

24 Aug 10/05 Aug 10/05 BCSG

25 Mar 10/06 Mar 10/06 BCSG

REVNO.

ISSUE DATE

DATE INSERTED

INSERTED BY

26 Jul 10/06 Jul 10/06 BCSG

27 Jun 10/07 Jun 10/07 BCSG

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29 Jun 10/09 Jun 10/09 BCSG

30 May 10/10 May 10/10 BCSG

31 Apr 10/11 Apr 10/11 BCSG

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