32-12-64 Rev 35 K0654
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laudimaia32-12-64 Rev 35 K0654
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laudimaiaSAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
Cheltenham Road, Gloucester, GL2 9QH, England
Telephone: +44 (0) 1452 712424
www.safran-landing-systems.com
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COMPONENT MAINTENANCE MANUAL
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ILLUSTRATED PARTS LIST
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BOGIE ASSEMBLY
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The technical data in this document (or file) may contain US data and be controlled for export under the Export
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Administration Regulations (EAR), 15 CFR Parts 730-774, ECCN: 9E991. Violations of these laws may be
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subject to fines and penalties under the Export Administration Act.
© SAFRAN LANDING SYSTEMS 2016 (AND SUBSEQUENT REVISION PAGE DATES)
This document and all information contained herein is the sole property of Safran Landing Systems (and/or its affiliated companies).
No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be
reproduced to a third party without the express written consent of Safran Landing Systems (and/or the appropriate affiliated company).
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Initial Issue: Apr 01/05 32-12-64 Revision No. 35
Mar 20/20
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SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
SAFRAN LANDING SYSTEMS UK Ltd
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Cheltenham Road, Gloucester, GL2 9QH, England
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Telephone +44 (0) 1452 712424
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TRANSMITTAL LETTER
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PERMANENT REVISIONS:
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This transmittal letter is applicable to Component Maintenance Manual ATA 32-12-64 Revision No. 35,
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dated Mar 20/20 that supersedes the Revision No. 34, dated Nov 01/19.
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REASON FOR REVISION:
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– To update assembly. nd ern
– To update special tools, fixtures, equipment and consumables.
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INSTRUCTIONS:
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This manual is intended for use in electronic format only.
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This manual supersedes the previous issue. If printed, all the pages of the previous issue must be
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removed, destroyed and replaced by all the pages of the new revision. This is necessary to take into
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account the transferred pages which are not covered by a revision bar.
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Tasks, Subtasks and Figures have been added, revised or deleted in this revision are outlined in
HIGHLIGHTS together with the description of changes.
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Pages which have been added or revised are shown in LIST OF EFFECTIVE PAGES with the revision
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dates.
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© SAFRAN LANDING SYSTEMS 2020 (AND SUBSEQUENT REVISION PAGE DATES)
This document and all information contained herein is the sole property of Safran Landing Systems (and/or its affiliated companies).
No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be
reproduced to a third party without the express written consent of Safran Landing Systems (and/or the appropriate affiliated company).
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
HIGHLIGHTS
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Revision No.35 - Mar 20/20
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LOCATIONS DESIGNATION DESCRIPTION OF CHANGE
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TITLE PAGE R Show Latest Revision Status
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LIST OF EFFECTIVE PAGES R Show Current Pages/Dates
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ASSEMBLY
TASK 32-12-64-400-801-A01 R Updated consumables table to add cotsolv 4021,
metsolv 4021 and rocol aerospec protect spray
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SUBTASK 32-12-64-440-002-A01 nd ern R Updated the assembly procedure to add rocol
aerospec protect spray application on the axles
(3-20)
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GRAPHIC 32-12-64-991-054-A01 N Added new figure to show rocol aerospec protect
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spray application on the axles (3-20)
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SPECIAL TOOLS, FIXTURES,
EQUIPMENT AND CONSUMABLES
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TASK 32-12-64-940-804-A01 R Updated consumables table to add cotsolv 4021,
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metsolv 4021 and rocol aerospec protect spray
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HLTS
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INSERTED INSERTED
REV ISSUE REV. ISSUE
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No. DATE DATE BY No. DATE DATE BY
1 Nov 01/06 Nov 01/06 M-DL 31 Dec 07/18 Dec 07/18 SAFRAN
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4 Jul 01/08 Apr 02/08 M-DL 34 Nov 01/19 Nov 01/19 SAFRAN
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5 Oct 01/08 Jul 01/08 M-DL 35 Mar 20/20 Mar 20/20 SAFRAN
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6 Dec 22/08 Oct 01/08 M-DL
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7 Apr 02/09 Apr 02/09 M-DL
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8 Oct 01/09 Oct 01/09 M-DL
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26 Jun 30/17 Jun 30/17 SAFRAN
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27 Sep 22/17 Sep 22/17 SAFRAN
28 Dec 08/17 Dec 08/17 SAFRAN
29 Mar 23/18 Mar 23/18 SAFRAN
30 Sep 21/18 Sep 21/18 SAFRAN
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RECORD OF TEMPORARY REVISIONS
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REV. No. DATE DATE BY DATE BY
Repair No. 1-1: Page 6001 to
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32-1 Jun 20/16 Jun 20/16 SAFRAN SAFRAN
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SERVICE BULLETINS LIST
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SB DATE
SB NUMBER SB TITLE REVISION INCORPORATED COVER SB NO.
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NUMBER INTO MANUAL
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A33/34-32-283 Introduction of a new bogie and 0 Dec 22/10 -
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dressings with a new two coat
1 No effect A330-32-3237
paint procedure
A340-32-4279
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Introduction of a new bogie A330-32-3270
A33/34-32-304 0 Jun 19/15
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beam A340-32-4302
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Introduction of a new bogie A330-32-3268
A33/34-32-305 0 Jun 19/15
beam A340-32-4300
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Introduction of a new bogie A330-32-3290
A33/34-32-315 0 Mar 23/18
pivot pin A340-32-4315
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TITLE PAGE DISASSEMBLY
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1 R Mar 20/20 3001 Jun 30/17
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3002 Jun 30/17
RECORD OF REVISIONS 3003 Jun 30/17
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2 Blank Mar 20/20
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RECORD OF TEMPORARY REVISIONS
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4001 Mar 22/19
1 Sep 16/16 4002 Mar 22/19
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INSPECTION/CHECK
SERVICE BULLETIN LIST 5001 Mar 23/18
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LIST OF EFFECTIVE PAGES
1 R Mar 20/20 REPAIR
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2 R Mar 20/20 6001 Nov 01/19
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3 R Mar 20/20 6002 Nov 01/19
4 Blank Mar 20/20 6003 Nov 01/19
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TABLE OF CONTENTS 6005 Nov 01/19
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3 Mar 23/18 6008 Nov 01/19
4 Mar 23/18 6009 Nov 01/19
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LIST OF ILLUSTRATIONS 6011 Nov 01/19
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2 R Mar 20/20 6013 Nov 01/19
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LIST OF TABLES 6015 Nov 01/19
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2 Blank Sep 16/16 6017 Nov 01/19
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UNIT IDENTIFICATION CHART 6019 Nov 01/19
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2 Blank Mar 23/18 6021 Nov 01/19
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INTRODUCTION 6023 Nov 01/19
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1 Mar 22/19 6024 Nov 01/19
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2 Mar 22/19 6025 Nov 01/19
3 Mar 22/19 6026 Nov 01/19
4 Blank Mar 22/19 6027 Nov 01/19
6028 Blank Nov 01/19
DESCRIPTION AND OPERATION
1 Sep 16/16 REPAIR NO. 1-1
2 Sep 16/16 6001 Sep 16/16
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REPAIR NO. 2-1 6028 Mar 22/19
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6002 Mar 22/19 ASSEMBLY
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REPAIR NO. 3-1
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REPAIR NO. 4-1 7018 R Mar 20/20
6001 Mar 22/19
6002 Mar 22/19 FITS AND CLEARANCES
6003 Mar 22/19 8001 Mar 24/17
6004 Mar 22/19 8002 Mar 24/17
6005 Mar 22/19 8003 Mar 24/17
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SPECIAL TOOLS, FIXTURES, EQUIPMENT AND
CONSUMABLES
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9002 R Mar 20/20
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STORAGE AND TRANSPORTATION
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ILLUSTRATED PARTS LIST
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INTRO IPL
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ALPHA/NUMERIC INDEX
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UNIT IDENTIFICATION CHART ...................................................................................................... 1
1. Unit Identification Chart ............................................................................................................. 1
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INTRODUCTION .............................................................................................................................. INTRO 1
1. Introduction ............................................................................................................................... INTRO 1
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A. General .............................................................................................................................. INTRO 1
B. Reference Publications ...................................................................................................... INTRO 1
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C. Units and Abbreviations ..................................................................................................... INTRO 2
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DESCRIPTION AND OPERATION .................................................................................................. 1
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1. Description and Operation ........................................................................................................ 1
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A. General .............................................................................................................................. 1
B. Description ......................................................................................................................... 1
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C. Operation ........................................................................................................................... 1
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D. Data ................................................................................................................................... 1
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TESTING AND FAULT ISOLATION ................................................................................ NOT APPLICABLE
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SCHEMATIC AND WIRING DIAGRAMS ........................................................................ NOT APPLICABLE
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DISASSEMBLY ................................................................................................................................ 3001
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1. Disassembly .............................................................................................................................. 3001
A. Job Set-up Information ....................................................................................................... 3001
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B. Job Set-up .......................................................................................................................... 3001
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(1) General ....................................................................................................................... 3001
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C. Procedure .......................................................................................................................... 3002
(1) Bogie Assembly (1-1) ................................................................................................. 3002
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(2) Bogie Beam Subassembly (3-30) ............................................................................... 3002
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CLEANING ....................................................................................................................................... 4001
1. Cleaning .................................................................................................................................... 4001
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A. Job Set-up Information ....................................................................................................... 4001
B. Job Set-up .......................................................................................................................... 4001
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C. Procedure .......................................................................................................................... 4001
(1) Cleaning ...................................................................................................................... 4001
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(2) Paint Removal ............................................................................................................ 4002
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INSPECTION/CHECK ...................................................................................................................... 5001
1. Inspection/Check ....................................................................................................................... 5001
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A. Job Set-up Information ....................................................................................................... 5001
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B. Job Set-up .......................................................................................................................... 5001
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C. Procedure .......................................................................................................................... 5001
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(1) General ....................................................................................................................... 5001
(2) Detailed Inspection ..................................................................................................... 5001
(3) Examine Dimensions .................................................................................................. 5002
(4) Special Detailed Inspection ........................................................................................ 5002
REPAIR ............................................................................................................................................ 6001
1. Repair ........................................................................................................................................ 6001
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A. Job Set-up Information ....................................................................................................... 6001
B. Job Set-up .......................................................................................................................... 6001
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C. Procedure .......................................................................................................................... 6001
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(1) General ....................................................................................................................... 6001
(2) Repair Procedure Conditions ...................................................................................... 6003
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(3) Protective Treatment ................................................................................................... 6003
(4) Approved Repairs ....................................................................................................... 6026
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REPAIR NO. 1-1 ............................................................................................................................... 6001
1. Repair No. 1-1 Axle (3-20) ........................................................................................................ 6001
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A. Job Set-up Information ....................................................................................................... 6001
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B. Job Set-up .......................................................................................................................... 6002
C. Procedure .......................................................................................................................... 6002
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(1) Use this procedure if there is damage or wear to the chromium plate of the diameter
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A. There must not be any damage or wear to the bare metal. ................................... 6002
(2) Use this procedure if there is damage or wear to the bare metal of the diameter A. ..
nd ern 6003
(3) Use this procedure if there is damage or wear to the chromium plate of the diameter
B. There must not be any damage or wear to the bare metal. ................................... 6004
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(4) Use this procedure if there is damage or wear to the bare metal of the diameter B. .. 6005
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(5) Use this procedure if there is damage or wear to the chromium plate of the diameter
C. There must not be any damage or wear to the bare metal. ................................... 6006
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(6) Use this procedure if there is damage or wear to the bare metal of the diameter C. . 6007
(7) Use this procedure as the first repair to diameter D if there is damage or wear to the
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chromium plate. There must not be any damage or wear to the bare metal. ............. 6008
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(8) Do this procedure to diameter D, if the base metal is damaged. ................................ 6009
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REPAIR NO. 2-1 ............................................................................................................................... 6001
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1. Repair No. 2-1 Towing Bracket (2-120) ..................................................................................... 6001
A. Job Set-up Information ....................................................................................................... 6001
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B. Job Set-up .......................................................................................................................... 6002
C. Procedure .......................................................................................................................... 6002
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(1) Use this procedure if there is damage or wear to the diameter A and/or the face B
and/or face C. ............................................................................................................. 6002
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(2) Use this procedure if there is damage or wear to the diameter D and/or the face E,
and/or the face F, and/or the face G, and/or the face H. ............................................. 6004
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e
REPAIR NO. 3-1 ............................................................................................................................... 6001
ex tial
1. Repair No. 3-1 Jacking Dome (1-150 and 2-70) ....................................................................... 6001
A. Job Set-up Information ....................................................................................................... 6001
n
B. Job Set-up .......................................................................................................................... 6001
ide
C. Procedure .......................................................................................................................... 6002
nf
(1) Do this procedure as the first repair to diameter A if there is damage to the plating.
Co
The bare metal must not be damaged: ....................................................................... 6002
(2) Do this procedure to diameter A if the bare metal is damaged: .................................. 6003
REPAIR NO. 4-1 ............................................................................................................................... 6001
1. Repair No. 4-1 Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D) ................... 6001
A. Job Set-up Information ....................................................................................................... 6001
B. Job Set-up .......................................................................................................................... 6002
TOC
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TABLE OF CONTENTS (Continued)
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C. Procedure .......................................................................................................................... 6003
(1) Do this procedure only for bogie beam subassemblies (3-30), (3-30A), (3-30B),
itio 0
(3-30C) and (3-30D), if there is a wear or damage to diameter A and/or diameter B
nd 202
and/or adjacent face L and/or M: (For bogie beam subassemblies (3-30E), (3-30F),
(3-30G), (3-30H) and (3-30I), go to para (5)) .............................................................. 6003
Co ay-
(2) Do this procedure if there is wear or damage to diameters C and/or D and/or E
and/or F and/or adjacent faces N and/or P and/or Q and/or R: .................................. 6005
s & -M
(3) Do this procedure if there is wear or damage to diameter G and/or diameter H and/or
rm 12
adjacent faces S and/or T: .......................................................................................... 6006
(4) Do this procedure if there is wear or damage to diameter J and/or diameter K and/or
Te n
adjacent faces U and/or V and/or X and/or W: ........................................................... 6009
S so
(5) Do this procedure only for bogie beam subassemblies (3-30E), (3-30F), (3-30G),
(3-30H) and (3-30I) if there is a wear or damage to diameter A and/or diameter B
SL de
and/or adjacent face L and/or M:(For bogie beam subassemblies (3-30), (3-30A),
er an
(3-30B), (3-30C) and (3-30D), go to para (1)). ............................................................ 6011
nd ern
ASSEMBLY ...................................................................................................................................... 7001
1. Assembly ................................................................................................................................... 7001
lu F
A. Job Set-up Information ....................................................................................................... 7001
ga pes
B. Job Set-up .......................................................................................................................... 7003
(1) General ....................................................................................................................... 7003
or Lo
C. Procedure .......................................................................................................................... 7003
(1) Bogie Beam Subassembly (3-30) ............................................................................... 7003
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(2) Install the Axles (3-20) ................................................................................................ 7006
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(3) Towing Bracket Subassembly (2-10) .......................................................................... 7007
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(4) Bogie Assembly (1-1) ................................................................................................. 7008
(5) Paint ............................................................................................................................ 7018
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FITS AND CLEARANCES ................................................................................................................ 8001
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1. Fits and Clearances ................................................................................................................. 8001
A. General .............................................................................................................................. 8001
us nloa
B. Layout ................................................................................................................................ 8001
C. Fits and Clearances Table ................................................................................................. 8004
siv ow
e
2. Torque Values ........................................................................................................................... 8010
A. Torque Data ....................................................................................................................... 8010
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SPECIAL TOOLS, FIXTURES, EQUIPMENT AND CONSUMABLES ............................................. 9001
ex tial
1. Special Tools, Fixtures and Equipment ..................................................................................... 9001
A. General .............................................................................................................................. 9001
n
2. Consumables ............................................................................................................................ 9002
ide
A. General .............................................................................................................................. 9002
nf
Co
SPECIAL PROCEDURES ............................................................................................... NOT APPLICABLE
REMOVAL ....................................................................................................................... NOT APPLICABLE
INSTALLATION ............................................................................................................... NOT APPLICABLE
SERVICING ..................................................................................................................... NOT APPLICABLE
TOC
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TABLE OF CONTENTS (Continued)
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STORAGE AND TRANSPORTATION .............................................................................................. 15001
1. Storage Instructions .................................................................................................................. 15001
itio 0
A. Job Set-up Information ....................................................................................................... 15001
nd 202
B. Job Set-up .......................................................................................................................... 15001
C. Procedure .......................................................................................................................... 15001
Co ay-
(1) Storage ....................................................................................................................... 15001
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REWORK (SERVICE BULLETIN ACCOMPLISHMENT PROCEDURES) ...................... NOT APPLICABLE
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ILLUSTRATED PARTS LIST ............................................................................................................ 10001
Te n
1. Introduction ............................................................................................................................... 10003
S so
A. General .............................................................................................................................. 10003
B. Numerical Index (where applicable) ................................................................................... 10003
SL de
C. Detailed Parts List .............................................................................................................. 10003
er an
2. Vendor Codes, Names and Addresses ..................................................................................... 10004
3. How to Use the Illustrated Parts List .........................................................................................
nd ern 10005
Alpha/Numeric Index ................................................................................................................. 10007
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Detailed Parts List ..................................................................................................................... 10011
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LIST OF ILLUSTRATIONS
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FIGURE TITLE PAGE
ns for
1 Bogie Assembly .......................................................................................................... 2
itio 0
6001 Axle (3-20) - Protective Treatment .............................................................................. 6013
nd 202
6002 Bogie Beam Subassembly (3-30), (3-30A), (3-30B), (3-30E), (3-30F) and (3-30G) -
Protective Treatment ................................................................................................... 6015
Co ay-
6003 Bogie Beam Subassembly (3-30C), (3-30D), (3-30H) and (3-30I) - Protective
Treatment .................................................................................................................... 6016
s & -M
6004 Diaphragm (1-210 and 2-180) - Protective Treatment ................................................ 6018
6005 Bogie Beam (3-190), (3-190A) and (3-190B) - Protective Treatment ......................... 6019
rm 12
6006 Bogie Beam (3-190C) and (3-190D) - Protective Treatment ...................................... 6021
Te n
6007 Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D) - Protective
S so
Treatment .................................................................................................................... 6023
6008 Bogie beam axle spacer subassembly (2-190) - Protective Treatment ...................... 6025
SL de
6009 Approved Repairs - Key Diagram ............................................................................... 6027
er an
6001 Repair No. 1-1 - Axle (3-20) Repair Positions ............................................................ 6011
6002 Repair No. 1-1 - Diameter A .......................................................................................
nd ern 6012
6003 Repair No. 1-1 - Diameter B ....................................................................................... 6013
6004 Repair No. 1-1 - Diameter C ....................................................................................... 6014
lu F
6005 Repair No. 1-1 - Detail Z ............................................................................................. 6015
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6006 Repair No. 1-1 - Detail Y ............................................................................................ 6016
6007 Repair No. 1-1 - Sermetel and Paint Application ........................................................ 6017
or Lo
6008 Repair No. 1-1 - Sermetel Application ........................................................................ 6018
6009 Repair No. 1-1 - Diameter D ....................................................................................... 6019
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6010 Repair No. 1-1 - Detail X ............................................................................................ 6020
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6011 Repair No. 1-1 - Detail W ........................................................................................... 6021
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6001 Repair No. 2-1 - Towing Bracket (2-120) .................................................................... 6006
6002 Repair No. 2-1 - Towing Bracket (2-120) .................................................................... 6007
TA by
6001 Repair No. 3-1 - Repair to Jacking Dome ................................................................... 6004
6002 Repair No. 3-1 - Repair to Jacking Dome ................................................................... 6005
of ded
6003 Repair No. 3-1 - Repair to Jacking Dome ................................................................... 6006
6004 Repair No. 3-1 - Repair to Jacking Dome ................................................................... 6007
us nloa
6001 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
(3-190D) ...................................................................................................................... 6013
siv ow
6002 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
e
(3-190D) ...................................................................................................................... 6014
clu - D
6003 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
e
(3-190D) ...................................................................................................................... 6015
ex tial
6004 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
(3-190D) ...................................................................................................................... 6016
n
6005 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
ide
(3-190D) ...................................................................................................................... 6017
nf
6006 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
Co
(3-190D) ...................................................................................................................... 6018
6007 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
(3-190D) ...................................................................................................................... 6019
6008 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
(3-190D) ...................................................................................................................... 6020
6009 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
(3-190D) ...................................................................................................................... 6021
LOI
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LIST OF ILLUSTRATIONS (Continued)
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FIGURE TITLE PAGE
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6010 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
itio 0
(3-190D) ...................................................................................................................... 6022
nd 202
6011 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
(3-190D) ...................................................................................................................... 6023
Co ay-
6012 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
(3-190D) ...................................................................................................................... 6024
s & -M
6013 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
(3-190D) ...................................................................................................................... 6025
rm 12
6014 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
Te n
(3-190D) ...................................................................................................................... 6026
S so
6015 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
(3-190D) ...................................................................................................................... 6027
SL de
6016 Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and
er an
(3-190D) ...................................................................................................................... 6028
7001 Bogie Beam Subassembly - Preparation and Installation of Bushes (3-150) .............
nd ern 7012
7002 Bogie Beam Subassembly - Installation of Bushes (3-130, 3-120 and 3-80) ............. 7013
7003 Bogie Beam Subassembly - Installation of Bushes (3-100 or 3-110) .......................... 7014
lu F
7004 Bogie Beam Subassembly - Preparation and Installation of Bushes (3-70, 3-60 and
ga pes
3-50) ........................................................................................................................... 7015
7005 Axles (3-20) - Application of Rocol Aerospec Protect Spray ...................................... 7016
or Lo
7006 Axle Rings (1-70) - Installation .................................................................................... 7017
8001 Fits and Clearances - Key Diagram ............................................................................ 8002
r P la
8002 Fits and Clearances .................................................................................................... 8003
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8003 Fits and Clearances .................................................................................................... 8005
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8004 Fits and Clearances .................................................................................................... 8008
TA by
Detailed Parts List
of ded
1 Bogie Assembly .......................................................................................................... 10012
2 Bogie Assembly .......................................................................................................... 10016
us nloa
3 Bogie Beam and Axle Subassembly ........................................................................... 10020
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LIST OF TABLES
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TABLE TITLE PAGE
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5001 Penetrant Inspection ................................................................................................... 5003
itio 0
5002 Magnetic Inspection .................................................................................................... 5003
nd 202
6001 Protective Treatment ................................................................................................... 6004
6002 Approved Repairs ....................................................................................................... 6026
Co ay-
8001 Fits and Clearances .................................................................................................... 8004
8002 Fits and Clearances .................................................................................................... 8006
s & -M
8003 Fits and Clearances .................................................................................................... 8009
8004 Torque Data ................................................................................................................ 8010
rm 12
9001 Special Tools, Fixtures and Equipment ....................................................................... 9001
Te n
9002 Consumables .............................................................................................................. 9002
S so
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UNIT IDENTIFICATION CHART
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TASK 32-12-64-99E-801-A01
1. Unit Identification Chart
ns for
SAFRAN LANDING SYSTEMS SAFRAN LANDING SYSTEMS MOD.
itio 0
DASH
nd 202
PART NO. MODIFICATION SERVICE BULLETIN STRIKE
NO.
NUMBER NUMBER NO.
Co ay-
10-211701 000 - EIS -
10-211701 001 MAF1-0002-0149 A33/34-32-283 2
s & -M
10-211701 002 MAF1-0002-0171 A33/34-32-304 3
rm 12
10-211701 003 MAF1-0002-0172 A33/34-32-305 4
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10-211701 004 EDES2-002-0209 A33/34-32-315 -
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UNIT IDENT. CHART
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UNIT IDENT. CHART
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INTRODUCTION
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TASK 32-12-64-871-801-A01
1. Introduction
ns for
A. General
itio 0
nd 202
(1) ATA specification 2200 is used in this manual.
Co ay-
(2) ASD Simplified Technical English to ASD-STE100 is used in this manual.
s & -M
(3) This manual contains Description, Operation and Maintenance procedures. It also contains an
Illustrated Parts List (IPL). IPL Figure and Item numbers in parentheses follow the part name
rm 12
to identify them.
Te n
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(4) A Unit Identification Chart is included to show the modification status of the unit. The
modification status is related to the unit part number by the dash number: the dash number is
SL de
marked on the unit name plate adjacent to the part number.
er an
(5) All references in this manual are to the left configuration of the unit unless the instructions tell
nd ern
you differently.
lu F
(6) All dimensions and quantities in this manual are in SI units with Imperial units in parentheses. A
ga pes
comma shows a decimal part of an SI unit. A full point shows a decimal part of an Imperial unit.
(7) This manual refers to Process Specifications (M-DLPS or PCS) and Non-destructive Tests
or Lo
(M-DLNDT). These are available in the Safran Landing Systems Technical Publication on-line
service.
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(8) All the materials in this manual have a CML Ref. code identification. This is the reference item
P :P
number of the material in the Consumable Materials List. These are available within the Safran
Landing Systems Technical Publications on-line service.
TA by
(9) All the materials in this manual have a Ref. Item identification. This is the reference item number
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of the material in the Aircraft Manufacturer's Consumable Materials List.
us nloa
(10) Use approved persons and good aircraft engineering practice for all procedures in this manual.
(11) Maintenance Task Oriented Support System (MTOSS) task and subtask identification is used
siv ow
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in this manual. The maintenance tasks and other data have special MTOSS numbers for the
clu - D
use of the Electronic Data Processing (EDP).
e
(12) The repairs in this CMM have been approved under Airbus' EASA Design Organisation Approval
ex tial
No. EASA.21J.031.
n
ide
(13) On occasion a REF. CODE can be identified in the NOMENCLATURE column in the
DETAILED PARTS LIST. This is a Safran Landing Systems reference code and is used for
nf
cross-reference purposes only.
Co
B. Reference Publications
No. NOMENCLATURE PUBLICATION NUMBER
1 Safran Landing Systems UK Ltd Component 32-12-63
Maintenance Manual, Bogie and Dressings
INTRO
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C. Units and Abbreviations
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(1) Standard Units
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S.I. UNITS ABBREVIATIONS IMPERIAL UNITS ABBREVIATIONS
itio 0
Degrees Celsius °C Degrees Fahrenheit °F
nd 202
(or centigrade)
Millimeter mm Inch in
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Newton-meter N.m Pound force per foot or Pound lbf.ft or lbf.in
s & -M
force per inch
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Newton N Pound force or poundal lbf or pdl
Kilogram kg Pound (mass) lb
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Gram g Ounce oz
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Mega Pascal MPa Kilo square inch ksi
er an
Bar bar Pound square inch psi
Square centimeter cm2
nd ern Square inch in2
Cubic centimeter cm3 Cubic inch in3
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Liter l Gallon US Gal
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Volt V Volt Direct Current VDC
or Lo
MilliVolt mV Root Mean Square RMS
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(2) General Abbreviations
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AECMA European Association of Aerospace Industries
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ASD Aerospace and Defence Industries Association of Europe
ATA Air Transport Association of America
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AR As required
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CMM Component Maintenance Manual
(D) Deleted
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EASA European Aviation Safety Agency
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EDP Electronic Data Processing
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EFF. CODE Effectivity code
Fig. Figure
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ID Inside Dimension
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IPL Illustrated Parts List
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M-DLPS Messier-Dowty Limited Process Specification
M-DLNDT Messier-Dowty Limited Non-Destructive Test
MLG Main Landing Gear
MTOSS Maintenance Task Oriented Support System
INTRO
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No. Number
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NP Non-procurable Part
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OD Outside Dimension
Para Paragraph
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nd 202
PCS Process Specification
Ref. Reference
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RF Reference
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(S) Superseded
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SI System International
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SB Service Bulletin
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TBA To Be Assigned
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TBD To Be Determined
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INTRO
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INTRO
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DESCRIPTION AND OPERATION
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TASK 32-12-64-870-801-A01
1. Description and Operation
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A. General
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nd 202
(1) The bogie assembly has a bogie beam and axle subassembly and a towing bracket
subassembly.
Co ay-
B. Description
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Refer to Figure 1
rm 12
(1) Bogie Beam and Axle Subassembly
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(a) The bogie beam and axle subassembly has a bogie beam subassembly and two axles.
SL de
1 The bogie beam subassembly has holes at each end to install the axles. A diaphragm
seals each end of the bogie beam subassembly. There is a jacking dome at each end
er an
of the bogie beam subassembly. One of the jacking domes attaches a towing bracket
nd ern
subassembly to the forward end of the bogie beam subassembly.
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2 A spigot and a nut hold the axles in position: locking segments lock the spigot in
ga pes
position. Spacers are installed on the inboard diameter of each axle and touch the
bogie beam subassembly. The axles have a thread at each end to attach a wheel nut.
or Lo
C. Operation
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(1) Not applicable.
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D. Data
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(1) Weight: - 425,546 Kg (937.903 lbs)
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Bogie Assembly
Figure 1/GRAPHIC 32-12-64-991-001-A01
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DISASSEMBLY
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TASK 32-12-64-000-801-A01
1. Disassembly
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A. Job Set-up Information
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nd 202
(1) Special Tools, Fixtures and Equipment
Co ay-
(a) The table below gives the special tools, fixtures and equipment necessary to disassemble
the component.
s & -M
rm 12
NOTE: It is permitted to use equivalent alternatives for the listed items.
Te n
NOTE: Refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT AND
S so
CONSUMABLES section for full details.
SL de
Part No. Description Function
er an
Local Supply Hydraulic Press Remove the axles (3-20)
nd ern
DRT66784 Lifting Equipment Lift the bogie beam and axle subassembly
(2-190)
lu F
DRT67088 Torque Spanner Remove the spigots (1-190) and (2-160)
ga pes
DRT67093 Holding Tool Hold the axle spigot nuts (1-200) and
or Lo
(2-170)
DRT68906 Spacer Removal Tool Remove the axle spacers (3-10)
r P la
tu
Ai au
HS122000 BushOut Kit Remove the bushes (3-50), (3-60), (3-70),
(3-100) and (3-110)
P :P
T14565 Crowfoot Spanner Remove the nuts (1-120) and (2-60)
TA by
T14566 Socket Hold the jacking dome subassembly (1-130)
of ded
and the jacking dome (2-70)
us nloa
(2) Consumables
Not applicable.
siv ow
e
clu - D
(3) Referenced Information
e
Reference Description
ex tial
PGBLK-32-12-64-9000-1 Special tools, fixtures, equipment and consumables
n
ide
B. Job Set-up
nf
SUBTASK 32-12-64-000-001-A01
Co
(1) General
(a) Make sure that the work area, the tools and the equipment are clean.
(b) Discard parts that you must not use again. These include split pins, sealing rings, backing
rings and lockwire (TBA).
32-12-64 Page 3001
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
C. Procedure
e
th
SUBTASK 32-12-64-040-001-A01
(1) Bogie Assembly (1-1)
ns for
(a) Remove the split pins (1-10).
itio 0
nd 202
(b) Remove the nuts (1-20), the washers (1-30) and (1-40) and the bolts (1-50).
Co ay-
(c) Remove the wheel nuts (1-60) and the axle rings (1-70).
s & -M
(d) Remove the split pin (1-80).
rm 12
(e) Remove the nut (1-90), the washers (1-100) and the bolt (1-110).
Te n
S so
(f) Use the Socket (T14566) to hold the jacking dome subassembly (1-130) and use the
Crowfoot Spanner (T14565) to remove the nut (1-120).
SL de
(g) Remove the jacking dome subassembly (1-130).
(h)
er an
Remove the bolts (1-160), the washers (1-170) and the locking segment (1-180).
nd ern
(i) Use the Holding Tool (DRT67093) to hold the axle spigot nut (1-200) and use the Torque
lu F
Spanner (DRT67088) to remove the spigot (1-190).
ga pes
(j) Remove the axle spigot nut (1-200).
or Lo
(k) Remove the diaphragm (1-210).
r P la
tu
Ai au
(l) Remove the split pin (2-20).
P :P
(m) Remove the nut (2-30), the washers (2-40) and the bolt (2-50).
TA by
(n) Use the Socket (T14566) to hold the jacking dome (2-70) and use the Crowfoot
of ded
Spanner (T14565) to remove the nut (2-60).
(o) Remove the jacking dome (2-70).
us nloa
(p) Remove the towing bracket subassembly (2-10).
siv ow
e
(q) Remove the bushes (2-100) and (2-110).
clu - D
e
(r) Remove the bolts (2-130), the washers (2-140) and the locking segment (2-150).
ex tial
(s) Use the Holding Tool (DRT67093) to hold the axle spigot nut (2-170) and use the Torque
n
Spanner (DRT67088) to remove the spigot (2-160).
ide
(t) Remove the axle spigot nut (2-170).
nf
Co
(u) Remove the diaphragm (2-180).
SUBTASK 32-12-64-040-002-A01
(2) Bogie Beam Subassembly (3-30)
(a) Use the Lifting Equipment (DRT66784) to install the bogie beam and axle subassembly
(2-190) in the Hydraulic Press.
32-12-64 Page 3002
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(b) Use the Spacer Removal Tool (DRT68906) to remove the spacers (3-10).
e
th
(c) Remove the axles (3-20).
ns for
(d) Use the Lifting Equipment (DRT66784) to remove the bogie beam and axle subassembly
(2-190) from the Hydraulic Press.
itio 0
nd 202
(e) Remove the dowels (3-40).
Co ay-
(f) Use the BushOut Kit (HS122000) to remove the bush (3-50).
s & -M
(g) Use the BushOut Kit (HS122000) to remove the bush (3-60).
rm 12
(h) Use the BushOut Kit (HS122000) to remove the bush (3-70).
Te n
S so
(i) Remove the bushes (3-80) and the saddle washer (3-90).
SL de
(j) Use the BushOut Kit (HS122000) to remove the bushes (3-100).
er an
(k) Use the BushOut Kit (HS122000) to remove the bushes (3-110).
nd ern
(l) Remove the bushes (3-120).
lu F
(m) Remove the bushes (3-130) and the saddle washer (3-140).
ga pes
(n) Remove the bushes (3-150).
or Lo
(o) Remove the lubrication fittings (3-160).
r P la
tu
Ai au
(p) Remove the adapters (3-170) and the washers (3-180).
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 3003
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CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
This page intentionally left blank.
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 3004
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SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
CLEANING
e
th
TASK 32-12-64-100-801-A01
1. Cleaning
ns for
A. Job Set-up Information
itio 0
nd 202
(1) Special Tools, Fixtures and Equipment
Co ay-
Not applicable.
s & -M
(2) Consumables
rm 12
(a) The table below gives the consumables necessary to clean the component.
Te n
S so
NOTE: It is permitted to use equivalent alternatives for the listed items.
SL de
NOTE: Refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT AND
er an
CONSUMABLES section for full details.
nd ern
CML Ref. Code Description
lu F
CM-0095 Cleaning product
ga pes
(3) Referenced Information
or Lo
Reference Description
r P la
PCS-2700 Paint stripping
tu
Ai au
PCS-2800 Temporary corrosion and damage protection of parts
P :P
PGBLK-32-12-64-6000-1 Repair
TA by
B. Job Set-up
of ded
Not applicable.
us nloa
C. Procedure
siv ow
e
WARNING: DO NOT GET CLEANING AGENTS ON YOUR SKIN, IN YOUR EYES OR NEAR A
clu - D
FLAME. DO NOT BREATHE THE FUMES. ONLY USE IN A LOCATION THAT HAS
e
A CONTINUOUS FLOW OF CLEAN AIR. CLEANING AGENTS ARE POISONOUS
AND FLAMMABLE.
ex tial
n
CAUTION: DO NOT USE CHLORINATED SOLVENTS. CHLORINATED SOLVENTS CAN MIX
ide
WITH VERY SMALL QUANTITIES OF WATER IN HYDRAULIC SYSTEMS TO MAKE
HYDROCHLORIC ACID. HYDROCHLORIC ACID WILL CAUSE CORROSION ON
nf
METAL SURFACES.
Co
SUBTASK 32-12-64-110-001-A01
(1) Cleaning
(a) Clean all the metal parts with Cleaning product (CM-0095). Make sure that you fully
remove all sealants, adhesives and jointing compounds.
32-12-64 Page 4001
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SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(b) Dry all the metal parts.
e
th
(c) Use clean PVC or polythene gloves to prevent corrosion of metal parts.
ns for
(d) Prevent corrosion of the metal parts that you do not immediately use for assembly
procedures: refer to PCS-2800.
itio 0
nd 202
SUBTASK 32-12-64-110-002-A01
(2) Paint Removal
Co ay-
WARNING: DO NOT GET PAINT STRIPPER ON YOUR SKIN, IN YOUR EYES OR NEAR A
s & -M
FLAME. DO NOT BREATHE THE FUMES. ONLY USE IN A LOCATION THAT
rm 12
HAS A CONTINUOUS FLOW OF CLEAN AIR. PAINT STRIPPER IS POISONOUS
AND FLAMMABLE.
Te n
S so
(a) Remove the damaged paint: refer to PCS-2700.
SL de
(b) Clean the part: refer to SUBTASK 32-12-64-110-001-A01.
er an
(c) Paint the part: refer to REPAIR.
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 4002
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SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
INSPECTION/CHECK
e
th
TASK 32-12-64-200-801-A01
1. Inspection/Check
ns for
A. Job Set-up Information
itio 0
nd 202
(1) Special Tools, Fixtures and Equipment
Co ay-
Not applicable.
s & -M
(2) Consumables
rm 12
Not applicable.
Te n
S so
(3) Referenced Information
SL de
Reference Description
er an
M-DLNDT3 Non destructive testing inspection of ground chrome plate
PCS-3100
nd ern
Magnetic particle inspection
PCS-3200 Fluorescent penetrant flaw detection
lu F
ga pes
PGBLK-32-12-64-8000-1 Fits and Clearances
or Lo
B. Job Set-up
r P la
Not applicable.
tu
Ai au
C. Procedure
P :P
SUBTASK 32-12-64-210-001-A01
TA by
(1) General
of ded
(a) The procedure to examine the parts is in two levels:
us nloa
1 Detailed Inspection.
2 Special Detailed Inspection.
siv ow
e
SUBTASK 32-12-64-220-001-A01
clu - D
(2) Detailed Inspection
e
ex tial
(a) Examine Parts Visually
n
ide
1 Carefully examine changes of section and areas which contact sealing rings.
nf
Co
32-12-64 Page 5001
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CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
2 Examine each part for these types of damage:
e
th
a Corrosion.
ns for
b Deterioration of protective treatment.
itio 0
c Distortion and/or cracks.
nd 202
d Wear or fretting.
Co ay-
e Scores, dents or burrs.
s & -M
f Unserviceable screw threads.
rm 12
g Parts of permanent assemblies that are not correctly attached.
Te n
S so
SUBTASK 32-12-64-220-002-A01
SL de
(3) Examine Dimensions
er an
(a) Measure all the parts that are in FITS AND CLEARANCES and compare with the
dimensions in the table.
nd ern
(b) Spring Data
lu F
ga pes
1 Not applicable.
or Lo
SUBTASK 32-12-64-280-001-A01
(4) Special Detailed Inspection
r P la
tu
Ai au
(a) Unless instructions are different:
P :P
1 Examine all parts shown in Tables 5001 and 5002 to the applicable specification
TA by
and information given.
of ded
CAUTION: YOU MUST DISASSEMBLE ALL PARTS, THIS WILL INCLUDE THE
BUSHES, THEY MUST BE REMOVED AND DISCARDED. YOU MUST
us nloa
APPLY THE NDT INSPECTION TO THE DETAIL LEVEL PART ONLY AS
IDENTIFIED IN TABLES 5001 AND 5002. IF THE BUSHES ARE NOT
REMOVED THE INSPECTION IS NOT COMPLETE FOR THE DETAIL
siv ow
e
PART AND DAMAGE CAN OCCUR.
clu - D
2 Parts that are included in Tables 5001 and 5002 must be fully disassembled to the
e
lowest detail level for NDT inspection. This includes the removal of all of the bushes.
ex tial
n
ide
nf
Co
32-12-64 Page 5002
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Penetrant Inspection
e
Table 5001
th
Fig Item
ns for
Name Material Type M-D Spec. Remarks
No.
itio 0
1-150 Jacking dome Steel, 300M to M-DLNDT3 Part 2 Chromium plated
nd 202
MTL1201 areas: refer to
Table 5002
Co ay-
1-190 and Spigot UHT Steel, M-DLNDT3 Part 2 Chromium plated
s & -M
2-160 MAT137 areas: refer to
Table 5002
rm 12
1-210 and Diaphragm Aluminium Alloy, PCS-3200 -
Te n
2-180 7010-T736,
S so
MAT210 or
7010-T7651 to
SL de
DTD 5120B
er an
2-70 Jacking dome Steel, 300M to M-DLNDT3 Part 2 Chromium plated
nd ern
MTL1201 areas: refer to
Table 5002
lu F
3-20 Axle Steel, 300M M-DLNDT3 Part 2 Chromium plated
ga pes
areas: refer to
Table 5002
or Lo
Magnetic Inspection
r P la
Table 5002
tu
Ai au
P :P
Fig Item
Name Material Type M-D Spec. Remarks
No.
TA by
1-60 Wheel nut Steel, S99 MAT123 PCS-3100 Inclusion class 2
of ded
1-120 Nut Steel, S99 MAT123 PCS-3100 Inclusion class 2
and 2-60
us nloa
1-150 Jacking dome Steel, 300M to PCS-3100 and Inclusion class 4 on areas
MTL1201 without chromium plate
siv ow
e
M-DLNDT3 Part 1 Chromium plated areas:
clu - D
refer to
e
Table 5001
ex tial
1-190 Spigot UHT Steel, PCS-3100 and Inclusion class 4 on areas
and MAT137 without chromium plate
n
ide
2-160
M-DLNDT3 Part 1 Chromium plated areas:
refer to
nf
Table 5001
Co
1-200 Axle spigot Steel, S99 MAT123 PCS-3100 Inclusion class 2
and nut
2-170
32-12-64 Page 5003
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CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Magnetic Inspection
e
Table 5002 (continued)
th
ns for
Fig Item
Name Material Type M-D Spec. Remarks
No.
itio 0
2-70 Jacking dome Steel, 300M to PCS-3100 and Inclusion class 4 on areas
nd 202
MTL1201 with out chromium plate
Co ay-
M-DLNDT3 Part 1 Chromium plated areas:
refer to
s & -M
Table 5001
rm 12
2-120 Towing Steel, 300M to PCS-3100 Inclusion class 4
bracket MTL1201
Te n
S so
3-20 Axle UHT Steel, PCS-3100 and Inclusion class 4 on areas
MTL1201 without chromium plate
SL de
M-DLNDT3 Part 1 Chromium plated areas:
er an
refer to
nd ern Table 5001
3-40 Dowel CR Steel, S145F or PCS-3100 Inclusion class 2
lu F
S145H
ga pes
3-190, Bogie beam Steel, 300M to PCS-3100 Inclusion class 4
3-190A, MTL1201
or Lo
3-190B,
3-190C
r P la
and
tu
Ai au
3-190D
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 5004
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SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
REPAIR
e
th
TASK 32-12-64-300-801-A01
1. Repair
ns for
A. Job Set-up Information
itio 0
nd 202
(1) Special Tools, Fixtures and Equipment
Co ay-
Not applicable.
s & -M
(2) Consumables
rm 12
Not applicable.
Te n
S so
(3) Referenced Information
SL de
Reference Description
er an
GUIDE-CS-001 Guide for the On-line application of a Repair Design Solution
M-DLPS102-1
nd ern
Chromic acid anodising
M-DLPS621 Application of temperature indicating paint
lu F
ga pes
M-DLPS1003-1 Standard treatments
PCS-2100 Cadmium plating of ultra high strength steel
or Lo
PCS-2101 Cadmium plating of steels UTS < 1450 MPa (210 ksi), copper
alloys and aluminium alloys
r P la
tu
Ai au
PCS-2141 Low embrittlement cadmium brush plating
P :P
PCS-2220 Protective chemical treatment of aluminium alloys
TA by
PCS-2500 Polyurethane Paint - Two Coat Process
PCS-2550 Heat resistant Metallic-ceramic Anti-corrosion coating
of ded
PCS-2800 Temporary corrosion and damage protection of parts
us nloa
PCS-7204 Anti-stone chip polysulphide coating
PGBLK-32-12-64-4000-1 Cleaning
siv ow
e
PGBLK-32-12-64-5000-1 Inspection/Check
clu - D
e
B. Job Set-up
ex tial
Not applicable.
n
ide
C. Procedure
nf
SUBTASK 32-12-64-300-001-A01
Co
(1) General
(a) Repair levels
1 There are two levels of repair procedure for parts that are found to be unserviceable
after inspection: refer to INSPECTION/CHECK.
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
a Repair of surface damage.
e
th
b Repair of wear or damage with an approved Messier-Dowty Limited or Safran
Landing Systems repair.
ns for
(b) Surface damage
itio 0
nd 202
1 Repair isolated external scores, smooth dents and abrasions, that have no cracks
and no effect on internal dimensions: refer to SUBTASK 32-12-64-350-001-A01.
Co ay-
Such damage must not be:
s & -M
a More than 19,00 mm (0.750 in) in length.
rm 12
b More than 0,76 mm (0.030 in) in depth.
Te n
S so
c Less than one diameter from a hole and less than 6,35 mm (0.250 in) from a
bearing surface.
SL de
d On a radius.
er an
2
nd ern
Remove burrs, corrosion and sharp edges: the area of damage must not be more
than 645 mm² (1.0 in²) for each 6450 mm² (10.0 in²). Subsequently, remove 0,127 mm
lu F
(0.0050 in) more of the material and repair the protective treatment.
ga pes
3 In a bore that will not seal, ignore abrasions and small scores that have no burrs. If
there are burrs, remove them plus 0,127 mm (0.0050 in) of material from the area.
or Lo
Repair the protective treatment.
r P la
4 In a bore that will seal, polish scores to remove them. Make sure that the surface
tu
Ai au
finish, concentricity and fits and clearances do not change.
P :P
5 Remove burrs from external screw threads.
TA by
CAUTION: DO NOT REPAIR A PART WITH A PROCEDURE THAT IS NOT APPROVED.
of ded
(c) Approved Repairs
us nloa
1 Approved repairs are in SUBTASK 32-12-64-350-002-A01. The repairs in this
CMM have been approved under Airbus' EASA Design Organisation Approval No.
siv ow
e
EASA.21J.031.
clu - D
2 Unless instructions are different in the approved repair, the applicable tolerances are:
e
ex tial
a General tolerance: + or - 0,25 mm (0.010 in).
n
ide
b Holes that are drilled or machined: + 0,25 to - 0,05 mm (+ 0.010 to - 0.002 in).
nf
c Angular tolerance: + or - 0,5 degree.
Co
3 Before you repair a part that is identified with a concession, salvage or repair number,
write to Safran Landing Systems for approval. Such numbers are adjacent to the
part number, for example:
a Concession - CON 14235.
32-12-64 Page 6002
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CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
b Salvage - 440015644.
e
th
c Repair - 450213024.
ns for
4 If the repairs in this manual cannot correct the wear or damage to the part, write to
Safran Landing Systems: refer to M-DLPS3002 (GUIDE-CS-001).
itio 0
nd 202
SUBTASK 32-12-64-350-001-A01
(2) Repair Procedure Conditions
Co ay-
(a) Cleaning
s & -M
1 Clean the parts after repair: refer to CLEANING.
rm 12
(b) Identification
Te n
S so
1 Identify the parts after repair with the Messier-Dowty Limited or Safran Landing
SL de
Systems Repair Number: refer to the applicable repair for instructions.
er an
SUBTASK 32-12-64-380-001-A01 nd ern
(3) Protective Treatment
lu F
(a) Protective Treatment Repair
ga pes
1 Cadmium Plated Surfaces
or Lo
a Repair damage to small areas of cadmium plated surfaces: refer to PCS-2141.
r P la
2 Anodized Surfaces
tu
Ai au
a Repair damage to small areas of anodized surfaces: refer to PCS-2220.
P :P
TA by
3 Paint Finish
of ded
a Repair damage to small areas of paint finish: refer to M-DLPS1003-1, use paint
to PCS-2500.
us nloa
(b) Protective Treatment Replacement
siv ow
1 Protective treatment replacement procedures and the applicable parts are given
e
in Table 6001.
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 6003
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CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Protective Treatment
e
Table 6001
th
Material
ns for
IPL Figure and
Name Specifica- Protective Treatment
Item No.
tion
itio 0
nd 202
1-60 Wheel nut Steel, S99 Apply cadmium plate to a thickness of between
MAT 123 0,010 and 0,015 mm (0.0004 and 0.0006 in): refer to
Co ay-
PCS-2101. Apply paint to PCS-2500: do not apply
paint to the threads and the slotted areas.
s & -M
1-120 and Nut Steel, S99 Apply cadmium plate to a thickness of between
rm 12
2-60 MAT 123 0,010 and 0,015 mm (0.0004 and 0.0006 in): refer to
PCS-2101. Apply paint to PCS-2500: do not apply
Te n
paint to the threads.
S so
1-150 and Jacking dome Steel, 300M Apply cadmium plate all over to a thickness of
SL de
2-70 to MTL1201 between 0,010 and 0,020 mm (0.0004 and 0.0008 in):
er an
refer to PCS-2100. Do not apply cadmium plate to
nd ern surfaces that have chromium plate. Apply primer paint
only to the holes for the bolts (1-110) and (2-50) and
to the undercut areas of the jacking dome shaft: refer
lu F
to PCS-2500. Apply paint all over: refer to PCS-2500.
ga pes
Do not paint the threads, the surfaces that have
chromium plate and surfaces that have primer paint
or Lo
only.
r P la
1-190 and Spigot UHT Steel, Apply cadmium plate to a thickness of between
tu
Ai au
2-160 MAT 137 0,010 and 0,020 mm (0.0004 and 0.0008 in): refer
to PCS-2101. Apply paint to PCS-2500: do not
P :P
apply paint to the threads and the surfaces that have
chromium plate.
TA by
1-200 and Nut Steel, S99 Apply cadmium plate to a thickness of between
of ded
2-170 MAT 123 0,010 and 0,015 mm (0.0004 and 0.0006 in): refer to
PCS-2101. Apply paint to PCS-2500: do not apply
us nloa
paint to the threads and the areas that make contact
with the diaphragm (1-210) and (2-180).
siv ow
e
1-210 and Diaphragm Aluminium Refer to Figure 6004. Apply chromic acid anodise
2-180 Alloy, process all over: refer to M-DLPS102-1. Apply primer
clu - D
7010T736 to paint only to the areas A: refer to PCS-2500. Apply
e
MAT210 paint: refer to PCS-2500. Do not paint the holes and
ex tial
areas B.
n
2-120 Towing bracket Steel, 300M Apply cadmium plate to a thickness of between
ide
to MTL1201 0,010 and 0,020 mm (0.0004 and 0.0008 in): refer to
PCS-2100. Apply temporary corrosion and damage
nf
protection: refer to PCS-2800.
Co
32-12-64 Page 6004
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SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Protective Treatment
e
Table 6001 (continued)
th
ns for
Material
IPL Figure and
Name Specifica- Protective Treatment
Item No.
itio 0
tion
nd 202
2-190 Bogie beam axle - Refer to Figure 6008. Before the application of rocol
spacer subassembly aerospec protect spray, clean the area of the axle with
Co ay-
METSOLV 4021 or COTSOLV 4021 and a lint free
cloth to remove the contamination products. Apply
s & -M
spray at ambient temperature with a thin uniform
rm 12
coating of rocol aerospace protect spray to the areas
A. The coating has a standby period of 30 minutes
Te n
before the installation of the spacers (3-10).
S so
3-20 Axle Steel, 300M Refer to Figure 6001. Apply Sermetel 962 and a
SL de
single top coat of 570A to a thickness of between 0,01
er an
to 0,02 mm (0.004 to 0.008 in) to the hole A and to
nd ern the threads for the wheel nuts: refer to PCS-2550.
Apply Sermetel 962 and a single top coat of 570A to
a thickness of between 0,025 to 0,050 mm (0.001
lu F
to 0.002 in) all over: refer to PCS-2550-6. Do not
ga pes
apply Sermetel 962 and top coat 570A to the areas
of chromium plate and nickel-chromium plate. Apply
or Lo
paint and make sure that the paint overlaps onto the
chromium plate runouts: refer to PCS-2500. Do not
r P la
apply paint to the areas of chromium plate, the hole A,
tu
Ai au
the areas B, the slots C (four places), the thread
P :P
undercuts and the holes D (twelve places). Paint the
areas B with temperature indicating paint: refer to
TA by
M-DLPS621.
of ded
3-30 and 3-30E Bogie beam - Refer to Figure 6002. Apply anti-stone chip
subassembly polysulphide coating, to the undersurface area A,
after primer paint and before finish paint: refer
us nloa
to PCS-7204. The thickness of the anti-stone
chip polysulphide coating must not be less than
siv ow
e
0,51 mm (0.020 in). Do not apply the anti-stone chip
polysulphide coating to the bush flanges and the
clu - D
bush bores B. Apply paint to the external surfaces:
e
refer to PCS-2500. Do not apply paint to the faces
ex tial
of the bush flanges and the bush bores B, the holes
C (eight places), the lubrication fittings (3-160), the
n
ide
adapters (3-170) and the dowels (3-40). Check the
thickness of the finish paint: refer to Figure 6007 and
nf
SB A33/34-32-283. If the measurement is not within
Co
the limits, the bogie beam must be finish painted
again. Apply corrosion preventive compound, Ardrox
AV100D, to the internal surfaces: refer to PCS-2800.
Do not apply the corrosion preventive compound to
the areas and items without paint.
32-12-64 Page 6005
Nov 01/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Protective Treatment
e
Table 6001 (continued)
th
ns for
Material
IPL Figure and
Name Specifica- Protective Treatment
Item No.
itio 0
tion
nd 202
3-30A, 3-30B, Bogie beam - Refer to Figures 6002 and 6007 and
3-30F and subassembly SB A33/34-32-283. Apply anti-stone chip
Co ay-
3-30G polysulphide coating, to the undersurface area A, after
primer paint and before finish paint: refer to PCS-7204.
s & -M
The thickness of the anti-stone chip polysulphide
rm 12
coating must not be less than 0,51 mm (0.020 in).
Do not apply the anti-stone chip polysulphide coating
Te n
to the bush flanges and the bush bores B. Apply
S so
paint to the external surfaces: refer to PCS-2500.
SL de
Do not apply paint to the faces of the bush flanges
and the bush bores B, the holes C (eight places), the
er an
lubrication fittings (3-160), the adapters (3-170) and
nd ern the dowels (3-40). Check the thickness of the finish
paint: refer to Figure 6007 and SB A33/34-32-283 for
lu F
the points of measurement. Measure at each point
ga pes
(points 1 to 14), with a permascope, five times and
take the average measurement. Finish paint dry film
thickness of the bogie beam (points 1 to 14) must
or Lo
be 0,040 to 0,050 mm (0.0016 to 0.0020 in). Finish
r P la
paint thickness measurement must not include the
tu
Ai au
cadmium plate or primer paint thickness. The average
thickness of the cadmium plate at points 1 to 14 plus
P :P
the average thickness of the primer paint at points 1 to
14 must be subtracted from the average thickness of
TA by
the finish paint at points 1 to 14. If the measurement
of ded
is not within the limits, the bogie beam must be finish
painted again. Apply corrosion preventive compound,
us nloa
Ardrox AV100D, to the internal surfaces: refer to
PCS-2800. Do not apply the corrosion preventive
compound to the areas and items without paint.
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 6006
Nov 01/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Protective Treatment
e
Table 6001 (continued)
th
ns for
Material
IPL Figure and
Name Specifica- Protective Treatment
Item No.
itio 0
tion
nd 202
3-30C, 3-30D Bogie beam - Refer to Figures 6003 and 6007. Apply anti-stone
and 3-30I subassembly chip polysulphide sprayable coating PR1436G to the
Co ay-
undersurface area A, after primer paint and before
finish paint: refer to PCS-7204. The thickness of the
s & -M
anti-stone chip polysulphide coating must not be less
rm 12
than 0,51 mm (0.020 in). Do not apply the anti-stone
chip polysulphide coating to the bush flanges and the
Te n
bush bores B. Apply paint to the external surfaces:
S so
refer to PCS-2500. Do not apply paint to the faces
SL de
of the bush flanges and the bush bores B and D,
the holes C (eight places), the lubrication fittings
er an
(3-160), the adapters (3-170) and the dowels (3-40).
nd ern Make sure that the top coat of the paint overlaps
onto the chromium plate. Check the thickness of the
lu F
finish paint: refer to Figure 6007 for the points of
ga pes
measurement. Measure at each point (points 1 to
14) five times and take the average measurement. If
the measurement is not within the limits, the bogie
or Lo
beam must be finish painted again. Apply primer paint
r P la
to the chromium plate area E to fill normal porosity
tu
Ai au
and discontinuities: refer to PCS-2500. Clean the
primer paint when it is still wet and lightly polish
P :P
to remove the primer paint on top of the chromium
plate if necessary. Do not damage the top coat paint
TA by
overlap onto chromium plate termination. Apply
of ded
corrosion preventive compound, Ardrox AV100D, to
the internal surfaces: refer to PCS-2800. Do not apply
us nloa
the corrosion preventive compound to the areas and
items without paint.
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 6007
Nov 01/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Protective Treatment
e
Table 6001 (continued)
th
ns for
Material
IPL Figure and
Name Specifica- Protective Treatment
Item No.
itio 0
tion
nd 202
3-30H Bogie beam - Refer to Figures 6003 and 6007. Apply anti-stone
subassembly chip polysulphide sprayable coating PR1436G to the
Co ay-
undersurface area A, after primer paint and before
finish paint: refer to PCS-7204. The thickness of the
s & -M
anti-stone chip polysulphide coating must not be less
rm 12
than 0,51 mm (0.020 in). Do not apply the anti-stone
chip polysulphide coating to the bush flanges and the
Te n
bush bores B. Apply paint to the external surfaces:
S so
refer to PCS-2500. Do not apply paint to the faces
SL de
of the bush flanges and the bush bores B and D,
the holes C (eight places), the lubrication fittings
er an
(3-160), the adapters (3-170) and the dowels (3-40).
nd ern Make sure that the top coat of the paint overlaps
onto the chromium plate. Check the thickness of the
lu F
finish paint: refer to Figure 6007 for the points of
ga pes
measurement. Measure at each point (points 1 to
14) five times and take the average measurement. If
the measurement is not within the limits, the bogie
or Lo
beam must be finish painted again. Apply primer paint
r P la
to the chromium plate area E to fill normal porosity
tu
Ai au
and discontinuities: refer to PCS-2500. Clean the
primer paint when it is still wet and lightly polish
P :P
to remove the primer paint on top of the chromium
plate if necessary. Do not damage the top coat paint
TA by
overlap onto chromium plate termination. Apply
of ded
corrosion preventive compound, Ardrox AV100D, to
the internal surfaces: refer to PCS-2831. Do not apply
us nloa
the corrosion preventive compound to the areas and
items without paint.
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 6008
Nov 01/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Protective Treatment
e
Table 6001 (continued)
th
ns for
Material
IPL Figure and
Name Specifica- Protective Treatment
Item No.
itio 0
tion
nd 202
3-40 Dowel C.R. Steel, Apply cadmium plate all over to a thickness of
S145 between 0,010 and 0,015 mm (0.0004 and 0.0006 in):
Co ay-
refer to PCS-2101.
s & -M
3-190, 3-190A Bogie beam Steel, 300M Refer to Figure 6005. Apply cadmium plate all over:
to MTL1201 refer to PCS-2100. Cadmium plate thickness must be
rm 12
between 0,010 to 0,020 mm (0.0004 to 0.0008 in).
Check the thickness of the cadmium plate: refer to
Te n
S so
PCS-2100, Figure 6007 and SB A33/34-32-283 for the
points of measurement. Measure at each point (points
SL de
1 to 10), with a permascope, five times and take the
er an
average measurement. If the measurement is not
nd ern within these limits, the bogie beam must be cadmium
plated again. Apply primer paint all over: refer to
PCS-2500 and Figure 6005. Do not apply primer paint
lu F
to areas A and D. Apply light primer only to areas B:
ga pes
refer to PCS-2500. Apply primer paint to areas C to
a thickness between 0,040 and 0,050 mm (0.0016
or Lo
and 0.0020 in): refer to PCS-2500 and Figure 6005.
Check the thickness of the primer paint: refer to
r P la
Figure 6007 and SB A33/34-32-283 for the points
tu
Ai au
of measurement. (Measure five times at each point
P :P
(points 1 to 10) and take the average measurement).
Primer paint dry film thickness of the bogie beam
TA by
(points 1 to 8) must be 0,040 to 0,050 mm (0.0016 to
0.0020 in). Primer paint dry film thickness of the bogie
of ded
beam (points 9 and 10) must be 0,020 to 0,025 mm
(0.0008 to 0.0010 in). Primer paint thickness must not
us nloa
include the cadmium plate thickness. The average
thickness of the cadmium plate at points 1 to 10 plus
the average thickness of the primer paint at points 1 to
siv ow
e
10 must be subtracted from the average thickness of
clu - D
the primer paint at points 1 to 10. If the measurement
e
is not within the limits, the bogie beam must be primer
ex tial
painted again.
n
ide
nf
Co
32-12-64 Page 6009
Nov 01/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Protective Treatment
e
Table 6001 (continued)
th
ns for
Material
IPL Figure and
Name Specifica- Protective Treatment
Item No.
itio 0
tion
nd 202
3-190B Bogie beam Steel, 300M Refer to Figure 6005. Apply cadmium plate all over:
to MTL 1201 refer to PCS-2100. Cadmium plate thickness must be
Co ay-
between 0,010 and 0,020 mm (0.0004 to 0.0008 in).
Do not apply cadmium plate to surfaces that have
s & -M
chromium plate and make sure that the cadmium plate
rm 12
overlaps onto the chromium plate runouts. Check the
thickness of the cadmium plate: refer to Figure 6007
Te n
for the points of measurement. Measure at each
S so
point (points 1 to 14) five times and take the average
SL de
measurement. If the measurement is not within the
limit, the bogie beam must be cadmium plated again.
er an
Apply primer paint all over: refer to PCS-2500 and
nd ern Figure 6005. Do not apply primer paint to areas A,
D and the surfaces that have chromium plate. Make
lu F
sure that the primer paint overlap the cadmium plate
ga pes
onto chromium plate. Apply light primer only to areas
B: refer to PCS-2500. Apply primer paint to areas C to
a thickness between 0,040 and 0,050 mm (0.0016 and
or Lo
0.0020 in): refer to PCS-2500 and Figure 6005. Check
r P la
the thickness of the primer paint: refer to Figure 6007
tu
Ai au
for the points of measurement. Measure five times
at each point (points 1 to 14) and take the average
P :P
measurement. If the measurement is not within the
limits, the bogie beam must be primer painted again.
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 6010
Nov 01/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Protective Treatment
e
Table 6001 (continued)
th
ns for
Material
IPL Figure and
Name Specifica- Protective Treatment
Item No.
itio 0
tion
nd 202
3-190C Bogie beam Steel, 300M Refer to Figure 6006. Apply cadmium plate all over:
to MTL 1201 refer to PCS-2100. Cadmium plate thickness must be
Co ay-
between 0,010 and 0,020 mm (0.0004 to 0.0008 in).
Do not apply cadmium plate to surfaces that have
s & -M
chromium plate and make sure that the cadmium plate
rm 12
overlaps onto the chromium plate runouts. Check the
thickness of the cadmium plate: refer to Figure 6007
Te n
for the points of measurement. Measure at each
S so
point (points 1 to 14) five times and take the average
SL de
measurement. If the measurement is not within the
limit, the bogie beam must be cadmium plated again.
er an
Apply primer paint all over: refer to PCS-2500 and
nd ern Figure 6006. Do not apply primer paint to areas A,
D and the surfaces that have chromium plate. Make
lu F
sure that the primer paint overlap the cadmium plate
ga pes
onto chromium plate. Apply light primer only to areas
B: refer to PCS-2500. Apply primer paint to areas C to
a thickness between 0,040 and 0,050 mm (0.0016 and
or Lo
0.0020 in): refer to PCS-2500 and Figure 6006. Check
r P la
the thickness of the primer paint: refer to Figure 6007
tu
Ai au
for the points of measurement. Measure five times
at each point (points 1 to 14) and take the average
P :P
measurement. If the measurement is not within the
limits, the bogie beam must be primer painted again.
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 6011
Nov 01/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Protective Treatment
e
Table 6001 (continued)
th
ns for
Material
IPL Figure and
Name Specifica- Protective Treatment
Item No.
itio 0
tion
nd 202
3-190D Bogie beam Steel, 300M Refer to Figure 6006. Apply cadmium plate all over:
to MTL 1201 refer to PCS-2100. Cadmium plate thickness must be
Co ay-
between 0,010 to 0,020 mm (0.0004 to 0.0008 in).
Check the thickness of the cadmium plate: refer to
s & -M
PCS-2100, Figure 6007 and SB A33/34-32-283 for the
rm 12
points of measurement. Measure at each point (points
1 to 10), with a permascope, five times and take the
Te n
average measurement. If the measurement is not
S so
within these limits, the bogie beam must be cadmium
SL de
plated again. Apply primer paint all over: refer to
PCS-2500 and Figure 6006. Do not apply primer paint
er an
to areas A and D. Apply light primer only to areas B:
nd ern refer to PCS-2500. Apply primer paint to areas C to
a thickness between 0,040 and 0,050 mm (0.0016
lu F
and 0.0020 in): refer to PCS-2500 and Figure 6006.
ga pes
Check the thickness of the primer paint: refer to
Figure 6007 and SB A33/34-32-283 for the points
of measurement. (Measure five times at each point
or Lo
(points 1 to 10) and take the average measurement).
r P la
Primer paint dry film thickness of the bogie beam
tu
Ai au
(points 1 to 8) must be 0,040 to 0,050 mm (0.0016 to
0.0020 in). Primer paint dry film thickness of the bogie
P :P
beam (points 9 and 10) must be 0,020 to 0,025 mm
(0.0008 to 0.0010 in). Primer paint thickness must not
TA by
include the cadmium plate thickness. The average
of ded
thickness of the cadmium plate at points 1 to 10 plus
the average thickness of the primer paint at points 1 to
us nloa
10 must be subtracted from the average thickness of
the primer paint at points 1 to 10. If the measurement
is not within the limits, the bogie beam must be primer
siv ow
e
painted again.
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 6012
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
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ns for
itio 0
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Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Axle (3-20) - Protective Treatment
(Sheet 1 of 2)
Figure 6001/GRAPHIC 32-12-64-991-002-A01
32-12-64 Page 6013
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e
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ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
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ide
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Axle (3-20) - Protective Treatment
(Sheet 2 of 2)
Figure 6001/GRAPHIC 32-12-64-991-002-A01
32-12-64 Page 6014
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e
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ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Bogie Beam Subassembly (3-30), (3-30A), (3-30B), (3-30E), (3-30F) and (3-30G) - Protective Treatment
Figure 6002/GRAPHIC 32-12-64-991-003-A01
32-12-64 Page 6015
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Bogie Beam Subassembly (3-30C), (3-30D), (3-30H) and (3-30I) - Protective Treatment
(Sheet 1 of 2)
Figure 6003/GRAPHIC 32-12-64-991-032-A01
32-12-64 Page 6016
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
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ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Bogie Beam Subassembly (3-30C), (3-30D), (3-30H) and (3-30I) - Protective Treatment
(Sheet 2 of 2)
Figure 6003/GRAPHIC 32-12-64-991-032-A01
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Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
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ide
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Co
Diaphragm (1-210 and 2-180) - Protective Treatment
Figure 6004/GRAPHIC 32-12-64-991-004-A01
32-12-64 Page 6018
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ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
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ide
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Co
Bogie Beam (3-190), (3-190A) and (3-190B) - Protective Treatment
(Sheet 1 of 2)
Figure 6005/GRAPHIC 32-12-64-991-005-A01
32-12-64 Page 6019
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ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
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ide
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Co
Bogie Beam (3-190), (3-190A) and (3-190B) - Protective Treatment
(Sheet 2 of 2)
Figure 6005/GRAPHIC 32-12-64-991-005-A01
32-12-64 Page 6020
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ns for
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nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
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ide
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Bogie Beam (3-190C) and (3-190D) - Protective Treatment
(Sheet 1 of 2)
Figure 6006/GRAPHIC 32-12-64-991-033-A01
32-12-64 Page 6021
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ns for
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nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
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ide
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Bogie Beam (3-190C) and (3-190D) - Protective Treatment
(Sheet 2 of 2)
Figure 6006/GRAPHIC 32-12-64-991-033-A01
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Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
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ide
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Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D) - Protective Treatment
(Sheet 1 of 2)
Figure 6007/GRAPHIC 32-12-64-991-006-A01
32-12-64 Page 6023
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SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
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ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D) - Protective Treatment
(Sheet 2 of 2)
Figure 6007/GRAPHIC 32-12-64-991-006-A01
32-12-64 Page 6024
Nov 01/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Bogie beam axle spacer subassembly (2-190) - Protective Treatment
Figure 6008/GRAPHIC 32-12-64-991-053-A01
32-12-64 Page 6025
Nov 01/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
SUBTASK 32-12-64-350-002-A01
e
(4) Approved Repairs
th
(a) Refer to Figure 6009 and Table 6002 for all approved repairs. The tasks and paragraphs
ns for
which follow contain each of the approved repairs.
itio 0
Approved Repairs
nd 202
Table 6002
Co ay-
Messier-Dowty or Safran Landing
Repair No. Applicable Part
Systems Repair No.
s & -M
Repair No. 1-1 64-2117003-00 Axle (3-20)
rm 12
Repair No. 2-1 64-2117007-00 Towing Bracket (2-120)
Te n
S so
Repair No. 3-1 64-2117008-00 Jacking Dome (1-150) and (2-70)
Repair No. 4-1 64-2117002-00 Bogie Beam (3-190), (3-190A),
SL de
(3-190B), (3-190C) and (3-190D)
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 6026
Nov 01/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
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th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Approved Repairs - Key Diagram
Figure 6009/GRAPHIC 32-12-64-991-007-A01
32-12-64 Page 6027
Nov 01/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
This page intentionally left blank.
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
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ex tial
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ide
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32-12-64 Page 6028
Nov 01/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
REPAIR NO. 1-1
e
th
TASK 32-12-64-300-802-A01
1. Repair No. 1-1 Axle (3-20)
ns for
A. Job Set-up Information
itio 0
nd 202
(1) Special Tools, Fixtures and Equipment
Co ay-
Not applicable.
s & -M
(2) Consumables
rm 12
Not applicable.
Te n
S so
(3) Referenced Information
SL de
Reference Description
er an
GUIDE-CS-001 Guide for the On-line application of a Repair Design Solution
M-DLNDT3
nd ern Non-destructive testing inspection of ground chrome plate
M-DLPS123 Steel shot peening
lu F
ga pes
M-DLPS621 Application of temperature indicating paint
M-DLPS914 Processing Requirements for Ultra High Strength Steels
or Lo
M-DLPS1004-4-1 Machining requirements for ultra high tensile strength steels
1760 MPa (255 ksi) tensile strength and above
r P la
tu
Ai au
M-DLPS1031-1 Termination requirements for chromed surfaces overplated and
ground to size
P :P
M-DLPS3004-1 Termination requirements for nickel and chromed surfaces
TA by
overplated and ground to size
of ded
M-DLPS3140 Shot peened nickel and chrome coating for ultra high tensile
steel parts
us nloa
PCS-2110 Electrolytic hard chromium plating of steels
PCS-2500 Polyurethane paint - Two coat process
siv ow
e
PCS-2550 Heat resistant Metallic-ceramic Anti-corrosion coating
clu - D
PCS-2700 Paint stripping
e
ex tial
PCS-3002 Penetrant inspection of ground chrome plated parts
PCS-3100, inclusion class 4 Magnetic particle inspection
n
ide
PCS-3600 Etch Inspection of high strength steel parts
nf
PCS-6000-04 Marking of materials, parts and assemblies (Air Scribe)
Co
PCS-6000-07 Marking of materials, parts and assemblies (Indelible ink)
Repair No. 1-1
32-12-64 Page 6001
Sep 16/16
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
B. Job Set-up
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th
(1) Specified Damage and Material Specification.
ns for
(a) Specified Damage
itio 0
1 Damage or wear to the diameter A, and/or diameter B, and/or diameter C, and/or
nd 202
diameter D: refer to Figure 6001.
Co ay-
(b) Material Specification
s & -M
IPL Figure and Item No. Description Material Specification
rm 12
Steel, 300M to MTL1201
3-20 Axle
(UHTS > 1930 MPa)
Te n
S so
(2) Repair Parts
SL de
Not applicable.
er an
C. Procedure
nd ern
SUBTASK 32-12-64-300-002-A01
lu F
(1) Use this procedure if there is damage or wear to the chromium plate of the diameter A. There
ga pes
must not be any damage or wear to the bare metal.
Refer to Figure 6001
or Lo
Refer to Figure 6002
Refer to Figure 6005
r P la
tu
Refer to Figure 6007
Ai au
P :P
CAUTION: FOR DAMAGE MORE THAN THE LIMITS OF THIS REPAIR SCHEME, WRITE
TO MESSIER-DOWTY LIMITED: REFER TO GUIDE-CS-001.
TA by
(a) Remove the paint and the temperature indicating paint from the axle: refer to PCS-2700
of ded
and REPAIR.
us nloa
(b) Remove the Sermetel from the axle: refer to PCS-2550.
(c) Remove the chromium plate locally from diameter A: refer to PCS-2110 and Figure 6002.
siv ow
e
(d) Examine the part for flaws: refer to PCS-3600 and PCS-3100, inclusion class 4.
clu - D
e
(e) Apply chromium plate to diameter A: refer to PCS-2110, M-DLPS1031-1, Figure 6002 and
ex tial
Figure 6005. The chromium plate thickness must not be less than 0,100 mm (0.0040 in)
after grinding.
n
ide
(f) Grind diameter A to between 159,932 and 159,957 mm (6.2965 and 6.2975 in):
nf
refer to M-DLPS914, M-DLPS1004-4-1 and Figure 6002. The surface finish must be
Co
0,8 micrometers (32 micro-inches).
(g) Examine the part for flaws: refer to M-DLNDT3.
(h) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-A adjacent
to the part number: refer to PCS-6000-04.
Repair No. 1-1
32-12-64 Page 6002
Sep 16/16
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(i) Apply Sermetel: refer to PCS-2550, Figure 6002, Figure 6005, Figure 6007 and REPAIR.
e
th
(j) Apply the temperature indicating paint: refer to M-DLPS621 and REPAIR.
ns for
(k) Apply paint: refer to PCS-2500, Figure 6005, Figure 6007 and REPAIR.
itio 0
(l) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-A adjacent
nd 202
to the part number: refer to PCS-6000-07.
Co ay-
(m) Examine the part to make sure you have obeyed all the repair instruction correctly.
s & -M
SUBTASK 32-12-64-300-003-A01
(2) Use this procedure if there is damage or wear to the bare metal of the diameter A.
rm 12
Refer to Figure 6001
Te n
Refer to Figure 6002
S so
Refer to Figure 6005
Refer to Figure 6007
SL de
CAUTION: FOR DAMAGE MORE THAN THE LIMITS OF THIS REPAIR SCHEME, WRITE
er an
TO MESSIER-DOWTY LIMITED: REFER TO GUIDE-CS-001.
nd ern
(a) Remove the paint and the temperature indicating paint from the axle: refer to PCS-2700
lu F
and REPAIR.
ga pes
(b) Remove the Sermetel from the axle: refer to PCS-2550.
or Lo
(c) Remove the chromium plate locally from diameter A: refer to PCS-2110 and Figure 6002.
r P la
(d) Machine diameter A sufficiently only to remove the minimum amount of material
tu
Ai au
necessary to remove the damage or wear. Do not make diameter A less than 159,347 mm
P :P
(6.2735 in): refer to M-DLPS914 and M-DLPS1004-4-1. The surface finish must be
0,8 micrometers (32 micro-inches).
TA by
(e) Machine the radius: refer to Figure 6005.
of ded
(f) Examine the part for flaws: refer to PCS-3600 and PCS-3100, inclusion class 4.
us nloa
(g) Shot peen the machined surfaces only: refer to M-DLPS123.
siv ow
e
(h) Apply chromium plate to diameter A: refer to PCS-2110, M-DLPS1031-1, Figure 6002
and Figure 6005. The chromium plate thickness must be between 0,10 mm (0.004 in)
clu - D
and 0,305 mm (0.0120 in) after machining.
e
ex tial
(i) Grind diameter A to between 159,932 and 159,957 mm (6.2965 and 6.2975 in): refer
to M-DLPS914 and M-DLPS1004-4-1. The surface finish must be 0,8 micrometers
n
ide
(32 micro-inches).
nf
(j) Examine the part for flaws: refer to M-DLNDT3.
Co
(k) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-B adjacent
to the part number: refer to PCS-6000-04.
(l) Apply Sermetel: refer to PCS-2550, Figure 6002, Figure 6005, Figure 6007 and REPAIR.
(m) Apply the temperature indicating paint: refer to M-DLPS621 and REPAIR.
Repair No. 1-1
32-12-64 Page 6003
Sep 16/16
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(n) Apply paint: refer to PCS-2500, Figure 6005, Figure 6007 and REPAIR.
e
th
(o) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-B adjacent
to the part number: refer to PCS-6000-07.
ns for
(p) Examine the part to make sure you have obeyed all the repair instruction correctly.
itio 0
nd 202
SUBTASK 32-12-64-300-004-A01
(3) Use this procedure if there is damage or wear to the chromium plate of the diameter B. There
Co ay-
must not be any damage or wear to the bare metal.
Refer to Figure 6001
s & -M
Refer to Figure 6003
rm 12
Refer to Figure 6005
Refer to Figure 6007
Te n
S so
CAUTION: FOR DAMAGE MORE THAN THE LIMITS OF THIS REPAIR SCHEME, WRITE
TO MESSIER-DOWTY LIMITED: REFER TO GUIDE-CS-001.
SL de
er an
(a) Remove the paint and the temperature indicating paint from the axle: refer to PCS-2700
and REPAIR. nd ern
(b) Remove the Sermetel from the axle: refer to PCS-2550.
lu F
ga pes
(c) Remove the chromium plate locally from diameter B: refer to PCS-2110 and Figure 6003.
(d) Examine the part for flaws: refer to PCS-3600 and PCS-3100, inclusion class 4.
or Lo
(e) Apply chromium plate to diameter B: refer to PCS-2110 and M-DLPS1031-1, Figure 6003
r P la
tu
and Figure 6005. The chromium plate thickness must not be less than 0,100 mm
Ai au
(0.0040 in) after grinding.
P :P
(f) Grind diameter B to between 139,917 and 139,957 mm (5.5085 and 5.5101 in):
TA by
refer to M-DLPS914, M-DLPS1004-4-1 and Figure 6003. The surface finish must be
0,8 micrometers (32 micro-inches).
of ded
(g) Examine the part for flaws: refer to M-DLNDT3.
us nloa
(h) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-C adjacent
to the part number: refer to PCS-6000-04.
siv ow
e
clu - D
(i) Apply Sermetel: refer to PCS-2550, Figure 6003, Figure 6005, Figure 6007 and REPAIR.
e
(j) Apply the temperature indicating paint: refer to M-DLPS621 and REPAIR.
ex tial
(k) Apply paint: refer to PCS-2500, Figure 6005, Figure 6007 and REPAIR.
n
ide
(l) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-C adjacent
nf
to the part number: refer to PCS-6000-07.
Co
(m) Examine the part to make sure you have obeyed all the repair instruction correctly.
Repair No. 1-1
32-12-64 Page 6004
Sep 16/16
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
SUBTASK 32-12-64-300-005-A01
e
(4) Use this procedure if there is damage or wear to the bare metal of the diameter B.
th
Refer to Figure 6001
Refer to Figure 6003
ns for
Refer to Figure 6005
itio 0
Refer to Figure 6007
nd 202
CAUTION: FOR DAMAGE MORE THAN THE LIMITS OF THIS REPAIR SCHEME, WRITE
TO MESSIER-DOWTY LIMITED: REFER TO GUIDE-CS-001.
Co ay-
(a) Remove the paint and the temperature indicating paint from the axle: refer to PCS-2700
s & -M
and REPAIR.
rm 12
(b) Remove the Sermetel from the axle: refer to PCS-2550.
Te n
S so
(c) Remove the chromium plate locally from diameter B: refer to PCS-2110 and Figure 6003.
SL de
(d) Machine diameter B sufficiently only to remove the minimum amount of material
er an
necessary to remove the damage or wear. Do not make diameter B less than 139,347 mm
(5.4861 in): refer to M-DLPS914 and M-DLPS1004-4-1. The surface finish must be
nd ern
0,8 micrometers (32 micro-inches).
lu F
(e) Machine the radius: refer to Figure 6005.
ga pes
(f) Examine the part for flaws: refer to PCS-3600 and PCS-3100, inclusion class 4.
or Lo
(g) Shot peen the machined surfaces only: refer to M-DLPS123.
r P la
tu
(h) Apply chromium plate to diameter B: refer to PCS-2110, M-DLPS1031-1 Figure 6003
Ai au
and Figure 6005. The chromium plate thickness must be between 0,10 mm (0.004 in)
P :P
and 0,305 mm (0.0120 in) after machining.
TA by
(i) Grind diameter B to between 139,917 and 139,957 mm (5.5085 and 5.5101 in): refer
to M-DLPS914 and M-DLPS1004-4-1. The surface finish must be 0,8 micrometers
of ded
(32 micro-inches).
us nloa
(j) Examine the part for flaws: refer to M-DLNDT3.
(k) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-D adjacent
siv ow
e
to the part number: refer to PCS-6000-04.
clu - D
e
(l) Apply Sermetel: refer to PCS-2550, Figure 6003, Figure 6005, Figure 6007 and REPAIR.
ex tial
(m) Apply the temperature indicating paint: refer to M-DLPS621 and REPAIR.
n
ide
(n) Apply paint: refer to PCS-2500, Figure 6005, Figure 6007 and REPAIR.
nf
(o) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-D adjacent
Co
to the part number: refer to PCS-6000-07.
Repair No. 1-1
32-12-64 Page 6005
Sep 16/16
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(p) Examine the part to make sure you have obeyed all the repair instruction correctly.
e
th
SUBTASK 32-12-64-300-006-A01
(5) Use this procedure if there is damage or wear to the chromium plate of the diameter C. There
ns for
must not be any damage or wear to the bare metal.
Refer to Figure 6001
itio 0
nd 202
Refer to Figure 6004
Refer to Figure 6005
Refer to Figure 6006
Co ay-
Refer to Figure 6007
s & -M
Refer to Figure 6008
rm 12
CAUTION: FOR DAMAGE MORE THAN THE LIMITS OF THIS REPAIR SCHEME, WRITE
TO MESSIER-DOWTY LIMITED: REFER TO GUIDE-CS-001.
Te n
S so
(a) Remove the paint and the temperature indicating paint from the axle: refer to PCS-2700
and REPAIR.
SL de
er an
(b) Remove the Sermetel from the axle: refer to PCS-2550.
nd ern
(c) Remove the chromium plate locally from diameter C: refer to PCS-2110 and Figure 6004.
lu F
(d) Examine the part for flaws: refer to PCS-3600 and PCS-3100, inclusion class 4.
ga pes
(e) Apply chromium plate to diameter C: refer to PCS-2110, M-DLPS1031-1, Figure 6004 to
or Lo
Figure 6006. The chromium plate thickness must not be less than 0,10 mm (0.004 in)
after grinding.
r P la
tu
Ai au
(f) Grind diameter C to between 133,917 and 133,957 mm (5.2723 and 5.2739 in):
refer to M-DLPS914, M-DLPS1004-4-1 and Figure 6004. The surface finish must be
P :P
0,8 micrometers (32 micro-inches).
TA by
(g) Examine the part for flaws: refer to M-DLNDT3.
of ded
(h) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-E adjacent
to the part number: refer to PCS-6000-04.
us nloa
(i) Apply Sermetel: refer to PCS-2550, Figure 6004 to Figure 6008 and REPAIR.
siv ow
e
(j) Apply the temperature indicating paint: refer to M-DLPS621 and REPAIR.
clu - D
e
(k) Apply paint: refer to PCS-2500, Figure 6005, Figure 6006, Figure 6007 and REPAIR.
ex tial
(l) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-E adjacent
n
to the part number: refer to PCS-6000-07.
ide
(m) Examine the part to make sure you have obeyed all the repair instruction correctly.
nf
Co
Repair No. 1-1
32-12-64 Page 6006
Sep 16/16
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
SUBTASK 32-12-64-300-007-A01
e
(6) Use this procedure if there is damage or wear to the bare metal of the diameter C.
th
Refer to Figure 6001
Refer to Figure 6004
ns for
Refer to Figure 6005
itio 0
Refer to Figure 6006
nd 202
Refer to Figure 6007
Refer to Figure 6008
Co ay-
CAUTION: FOR DAMAGE MORE THAN THE LIMITS OF THIS REPAIR SCHEME, WRITE
s & -M
TO MESSIER-DOWTY LIMITED: REFER TO GUIDE-CS-001.
rm 12
(a) Remove the paint and the temperature indicating paint from the axle: refer to PCS-2700
and REPAIR.
Te n
S so
(b) Remove the Sermetel from the axle: refer to PCS-2550.
SL de
(c) Remove the chromium plate locally from diameter C: refer to PCS-2110 and Figure 6004.
er an
(d) Machine diameter C sufficiently only to remove the minimum amount of material
nd ern
necessary to remove the damage or wear. Do not make diameter C less than 133,347 mm
(5.2499 in): refer to M-DLPS914 and M-DLPS1004-4-1. The surface finish must be
lu F
0,8 micrometers (32 micro-inches).
ga pes
(e) Machine the radius: refer to Figure 6005 and Figure 6006.
or Lo
(f) Examine the part for flaws: refer to PCS-3600 and PCS-3100, inclusion class 4.
r P la
tu
Ai au
(g) Shot peen the machined surfaces only: refer to M-DLPS123.
P :P
(h) Apply chromium plate to diameter C: refer to PCS-2110, M-DLPS1031-1, Figure 6004
to Figure 6006. The chromium plate thickness must be between 0,10 mm (0.004 in)
TA by
and 0,305 mm (0.0120 in) after machining.
of ded
(i) Grind diameter C to between 133,917 and 133,957 mm (5.2723 and 5.2739 in): refer
to M-DLPS914 and M-DLPS1004-4-1. The surface finish must be 0,8 micrometers
us nloa
(32 micro-inches).
siv ow
(j) Examine the part for flaws: refer to M-DLNDT3.
e
clu - D
(k) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-F adjacent
e
to the part number: refer to PCS-6000-04.
ex tial
(l) Apply Sermetel: refer to PCS-2550, Figure 6004 to Figure 6008 and REPAIR.
n
ide
(m) Apply the temperature indicating paint: refer to M-DLPS621 and REPAIR.
nf
(n) Apply paint: refer to PCS-2500, Figure 6005, Figure 6006, Figure 6007 and REPAIR.
Co
(o) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-F adjacent
to the part number: refer to PCS-6000-07.
Repair No. 1-1
32-12-64 Page 6007
Sep 16/16
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(p) Examine the part to make sure you have obeyed all the repair instruction correctly.
e
th
SUBTASK 32-12-64-300-012-A01
(7) Use this procedure as the first repair to diameter D if there is damage or wear to the chromium
ns for
plate. There must not be any damage or wear to the bare metal.
Refer to Figure 6009
itio 0
nd 202
Refer to Figure 6010
CAUTION: FOR DAMAGE MORE THAN THE LIMITS OF THIS REPAIR SCHEME, WRITE
Co ay-
TO MESSIER-DOWTY LIMITED: REFER TO GUIDE-CS-001.
s & -M
(a) Remove the paint and the temperature indicating paint from the axle: refer to PCS-2700.
rm 12
(b) Remove the Sermetel from the axle: refer to PCS-2550.
Te n
S so
(c) Remove the shot peened nickel and chromium plate locally from diameter D: refer to
M-DLPS3140 and Figure 6009.
SL de
(d) Examine the part for flaws: refer to PCS-3100 inclusion class 4 and PCS-3600.
er an
(e)
nd ern
Apply shot peened nickel and chromium plate to diameter D. The total plating thickness
must be sufficient to allow for a minimum thickness of 0,10 mm (0.004 in) after grinding:
lu F
refer to M-DLPS3140, M-DLPS3004-1, Figure 6009 and Figure 6010.
ga pes
(f) Grind diameter D to between 165,210 to 165,235 mm (6.5043 to 6.5053 in). The surface
finish must be 0,8 micrometres (32 micro-inches): refer to M-DLPS914, M-DLPS1004-4-1,
or Lo
Figure 6009 and Figure 6010.
r P la
tu
(g) Examine the part for flaws: refer to PCS-3100 inclusion class 4 and PCS-3002.
Ai au
P :P
(h) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-G adjacent
to the existing part number: refer to PCS-6000-04.
TA by
(i) Apply sermetel: refer to PCS-2550, Figure 6006, Figure 6007, Figure 6009 and
of ded
Figure 6010.
us nloa
(j) Apply the temperature indicating paint: refer to M-DLPS621 and REPAIR.
(k) Apply paint where shown: refer to PCS-2500, Figure 6007, Figure 6009, Figure 6010
siv ow
e
and REPAIR.
clu - D
(l) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-G adjacent
e
to the existing part number: refer to PCS-6000-07.
ex tial
(m) Examine the part to make sure that you have obeyed all the repair instructions correctly.
n
ide
nf
Co
Repair No. 1-1
32-12-64 Page 6008
Sep 16/16
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
SUBTASK 32-12-64-300-013-A01
e
(8) Do this procedure to diameter D, if the base metal is damaged.
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Refer to Figure 6009
Refer to Figure 6010
ns for
Refer to Figure 6011
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CAUTION: FOR DAMAGE MORE THAN THE LIMITS OF THIS REPAIR SCHEME, WRITE
TO MESSIER-DOWTY LIMITED: REFER TO GUIDE-CS-001.
Co ay-
(a) Remove the paint and the temperature indicating paint from the axle: refer to PCS-2700.
s & -M
(b) Remove the Sermetel from the axle: refer to PCS-2550.
rm 12
(c) Remove the shot peened nickel and chromium plate locally from diameter D: refer to
Te n
M-DLPS3140 and Figure 6009.
S so
(d) Machine diameter D to remove damage or wear. Remove the minimum amount of
SL de
material necessary. Do not reduce diameter D to less than 164,625 mm (6.4813 in).
er an
The surface finish must be 0,8 micrometres (32 micro-inches): refer to M-DLPS914,
M-DLPS1004-4-1 and Figure 6011.
nd ern
NOTE: It is permissible to machine diameter D complete across both journals
lu F
at the same time including centre section of axle, in which case
ga pes
requirements of Figure 6011 do not apply. Do not reduce diameter D to
less than 164,625 mm (6.4813 in). Reinstate edge break radius R0,30 to
or Lo
0,70 mm (0.012 to 0.028 in) at intersection between OD and 44,59 mm
(1.756 in) diameter hole. The surface finish must be 0,8 micrometres
r P la
(32 micro-inches): refer to M-DLPS914, M-DLPS1004-4-1, Figure 6009 and
tu
Ai au
Figure 6010.
P :P
(e) Machine the radii: refer to M-DLPS914, M-DLPS1004-4-1 and Figure 6009 to Figure 6011.
TA by
(f) Examine the part for flaws: refer to PCS-3100 inclusion class 4 and PCS-3600.
of ded
(g) Shot peen the machined surface only: refer to M-DLPS123.
us nloa
(h) Apply shot peened nickel and chromium plate to diameter D. The plating thickness must
be sufficient to allow for final machining, resulting in a maximum finish plate thickness
siv ow
e
of 0,305 mm (0.0120 in) and a minimum of 0,10 mm (0.004 in) after machining: refer to
M-DLPS3140, M-DLPS3004-1 and Figure 6009 to Figure 6011.
clu - D
e
(i) Grind diameter D to between 165,210 to 165,235 mm (6.5043 to 6.5053 in). The surface
ex tial
finish must be 0,8 micrometres (32 micro-inches): refer to M-DLPS914, M-DLPS1004-4-1
and Figure 6009 to Figure 6011.
n
ide
(j) Examine the part for flaws: refer to PCS-3100 inclusion class 4 and PCS-3002.
nf
(k) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-H adjacent
Co
to the existing part number: refer to PCS-6000-04.
(l) Apply sermetel: refer to PCS-2550, Figure 6006, Figure 6007, Figure 6009 to Figure 6011
and REPAIR.
(m) Apply the temperature indicating paint: refer to M-DLPS621 and REPAIR.
Repair No. 1-1
32-12-64 Page 6009
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SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(n) Apply paint where shown: refer to PCS-2500, Figure 6007, Figure 6009 to Figure 6011
e
and REPAIR.
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(o) Identify the part with the Messier-Dowty Limited repair number 64-2117003-00-H adjacent
ns for
to the existing part number: refer to PCS-6000-07.
itio 0
(p) Examine the part to make sure that you have obeyed all the repair instructions correctly.
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Repair No. 1-1
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Repair No. 1-1 - Axle (3-20) Repair Positions
Figure 6001/GRAPHIC 32-12-64-991-008-A01
Repair No. 1-1
32-12-64 Page 6011
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Repair No. 1-1 - Diameter A
Figure 6002/GRAPHIC 32-12-64-991-009-A01
Repair No. 1-1
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Repair No. 1-1 - Diameter B
Figure 6003/GRAPHIC 32-12-64-991-010-A01
Repair No. 1-1
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Repair No. 1-1 - Diameter C
Figure 6004/GRAPHIC 32-12-64-991-011-A01
Repair No. 1-1
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Repair No. 1-1 - Detail Z
Figure 6005/GRAPHIC 32-12-64-991-012-A01
Repair No. 1-1
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Repair No. 1-1 - Detail Y
Figure 6006/GRAPHIC 32-12-64-991-013-A01
Repair No. 1-1
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Repair No. 1-1 - Sermetel and Paint Application
Figure 6007/GRAPHIC 32-12-64-991-030-A01
Repair No. 1-1
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Repair No. 1-1 - Sermetel Application
Figure 6008/GRAPHIC 32-12-64-991-031-A01
Repair No. 1-1
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Repair No. 1-1 - Diameter D
Figure 6009/GRAPHIC 32-12-64-991-034-A01
Repair No. 1-1
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Repair No. 1-1 - Detail X
Figure 6010/GRAPHIC 32-12-64-991-035-A01
Repair No. 1-1
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Repair No. 1-1 - Detail W
Figure 6011/GRAPHIC 32-12-64-991-036-A01
Repair No. 1-1
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REPAIR NO. 2-1
e
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TASK 32-12-64-300-803-A01
1. Repair No. 2-1 Towing Bracket (2-120)
ns for
A. Job Set-up Information
itio 0
nd 202
(1) Special Tools, Fixtures and Equipment
Co ay-
(a) The table below gives the special tools, fixtures and equipment necessary to repair the
component.
s & -M
rm 12
NOTE: It is permitted to use equivalent alternatives for the listed items.
Te n
NOTE: Refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT AND
S so
CONSUMABLES section for full details.
SL de
Part No. Description Function
er an
460004330/19 Press Pad Install the Repair Bushes 201485608B
nd ern
460004330/210 Press Pad Install the Repair Bushes 61-2117017-00
lu F
460004331/3 Drift Install the Repair Bushes 61-2117017-00
ga pes
(2) Consumables
or Lo
(a) The table below gives the consumables necessary to repair the component.
r P la
tu
Ai au
NOTE: It is permitted to use equivalent alternatives for the listed items.
P :P
NOTE: Refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT AND
TA by
CONSUMABLES section for full details.
of ded
CML Ref. Code Description
TBA Zinc loaded Molykote DX, PCS-7305
us nloa
TBA Sealant, PCS-7200
siv ow
e
(3) Referenced Information
clu - D
Reference Description
e
ex tial
AMS-2700 Passivation treatment
M-DLPS123 Steel shot peening
n
ide
M-DLPS914 Processing requirements for ultra high strength steels
nf
M-DLPS1004-4-1 Requirements for ultra high tensile strength steel 1760 MPa (255
Co
ksi) tensile strength and above
PCS-2100 Cadmium plating of ultra high strength steel
PCS-2101 Cadmium plating of steels UTS < 1450 MPa (210 ksi), copper
alloys and aluminium alloys
PCS-2500 Polyurethane paint - Two coat process
Repair No. 2-1
32-12-64 Page 6001
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SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Reference Description
e
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PCS-2700 Paint stripping
ns for
PCS-3100, inclusion class 2 Magnetic particle inspection
PCS-3100, inclusion class 4 Magnetic particle inspection
itio 0
nd 202
PCS-3600 Etch inspection of high strength steel parts
PCS-5100 Assembly of bushes in steel components using Molykote DX
Co ay-
OR Zinc Loaded Molykote DX
s & -M
PCS-6000-04 Marking of materials, parts and assemblies (Air Scribe)
rm 12
PCS-6000-06 Marking of materials, parts and assemblies (Electrolytic)
PCS-6000-07 Marking of materials, parts and assemblies (Indelible ink)
Te n
S so
PCS-7200 Elastomeric filleting sealant
SL de
PCS-7305 Zinc Loaded Molykote DX
er an
B. Job Set-up nd ern
(1) Specified Damage and Material Specification.
lu F
(a) Specified Damage
ga pes
1 Damage or wear to the diameter A, and/or the face B, and/or the face C: refer to
or Lo
Figures 6001 and 6002.
r P la
2 Damage or wear to the diameter D and/or the face E, and/or the face F, and/or the
tu
Ai au
face G, and/or the face H: refer to Figures 6001 and 6002.
P :P
(b) Material Specification
TA by
IPL Figure and Item No. Description Material Specification
of ded
Steel, 300M to MTL1201
(2-120) Towing Bracket
(UHTS > 1800 MPa)
us nloa
(2) Repair Parts
siv ow
e
Part No. Repair Part Material Specification
clu - D
e
201485608B Repair Bush Stainless Steel, S145
ex tial
61-2117017-00 Repair Bush CRES, 17-4PH to AMS 5643
n
ide
C. Procedure
nf
SUBTASK 32-12-64-300-008-A01
Co
(1) Use this procedure if there is damage or wear to the diameter A and/or the face B and/or face C.
Refer to Figure 6001
Refer to Figure 6002
(a) Remove the paint: refer to PCS-2700.
(b) Remove the cadmium plate: refer to PCS-2100.
Repair No. 2-1
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(c) Machine diameter A to remove the minimum amount of material necessary to remove the
e
damage or wear. Diameter A must not be more than 65,630 mm (2.5839 in). The surface
th
finish must be 0,8 micrometers (32 micro-inches): refer to M-DLPS914, M-DLPS1004-4-1
and Figure 6001.
ns for
(d) Measure and record diameter A: refer to Figure 6001.
itio 0
nd 202
(e) Machine faces B and/or C. Remove the minimum amount of material necessary to remove
the wear or damage. The surface finish must be 1,6 micrometers (63 micro-inches): refer
Co ay-
to M-DLPS914, M-DLPS1004-4-1 and Figure 6001.
s & -M
NOTE: For the first and any repairs that follow, do not remove more than a total
rm 12
of 1,0 mm (0.04 in) from any face.
Te n
(f) Make sure that the width of the flange between face B and face C is not less than
S so
72,350 mm (2.8484 in).
SL de
(g) Machine the chamfers and radii as shown: refer to Figure 6001.
er an
(h) Examine the part for flaws: refer to PCS-3100 inclusion class 4 and PCS-3600.
nd ern
(i) Shot peen the machined areas: refer to M-DLPS123.
lu F
ga pes
(j) Identify the part with the Messier-Dowty Limited repair number 64-2117007-00-A adjacent
to the part number: refer to PCS-6000-06 or PCS-6000-04.
or Lo
(k) Apply cadmium plate all over: refer to PCS-2100. The thickness of the cadmium plate
r P la
must be between 0,010 and 0,020 mm (0.0004 and 0.0008 in).
tu
Ai au
(l) Calculate diameter V of the repair bushes 201485608B, use the formula:
P :P
V = A (as measured) + 0,023 to 0,042 mm (0.0009 to 0.0016 in). Refer to Figure 6001.
TA by
(m) Machine the repair bushes 201485608B to the dimension shown and calculated. Make
the surface finish 1,6 micrometers (63 micro-inches).
of ded
(n) Machine the inner face U of the repair bushes 201485608B to get the correct dimension
us nloa
after assembly. Make the surface finish 1,6 micrometers (63 micro-inches).
(o) Examine the part for flaws: refer to PCS-3100 inclusion class 2.
siv ow
e
clu - D
(p) Apply passivation process to the repair bushes: refer to AMS-2700.
e
(q) Apply cadmium plate all over the repair bushes: refer to PCS-2101. The thickness of the
ex tial
cadmium plate must be between 0,010 and 0,015 mm (0.0004 and 0.0006 in).
n
ide
(r) Apply primer paint to the bracket where the bush flanges will install: refer to PCS-2500.
nf
(s) Use the Press Pad (460004330/19) and zinc loaded Molykote DX to install the repair
Co
bushes: refer to PCS-5100 and PCS-7305.
(t) Apply sealant around the outer flanges of the bushes: refer to PCS-7200.
(u) Apply paint to the bracket, but not where shown: refer to PCS-2500 and Figure 6002.
Repair No. 2-1
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(v) Identify the part with the Messier-Dowty Limited repair number 64-2117007-00-A adjacent
e
to the part number: refer to PCS-6000-07.
th
(w) Examine the part to make sure you have obeyed all the repair instructions correctly.
ns for
SUBTASK 32-12-64-300-009-A01
itio 0
(2) Use this procedure if there is damage or wear to the diameter D and/or the face E, and/or the
nd 202
face F, and/or the face G, and/or the face H.
Refer to Figure 6001
Co ay-
Refer to Figure 6002
s & -M
(a) Remove the paint: refer to PCS-2700.
rm 12
(b) Remove the cadmium plate: refer to PCS-2100.
Te n
S so
(c) Machine diameter(s) D to remove the minimum amount of material necessary to remove
the damage or wear. Diameter(s) D must not be more than 37,925 mm (1.4931 in).
SL de
The surface finish must be 0,8 micrometers (32 micro-inches): refer to M-DLPS914,
er an
M-DLPS1004-4-1 and Figure 6001.
nd ern
(d) Measure and record diameter(s) D.
lu F
(e) Machine the face E, and/or the face F, and/or the face G, and/or the face H. Remove the
ga pes
minimum amount of material necessary to remove the wear or damage. The surface
finish must be 1,6 micrometers (63 micro-inches): refer to M-DLPS914, M-DLPS1004-4-1
or Lo
and Figure 6001.
r P la
NOTE: For the first and any repairs that follow, do not remove more than a total
tu
Ai au
of 1,0 mm (0.04 in) from any face.
P :P
(f) Make sure that the width of the flange between the face E and the face F or between the
TA by
face G and the face H is not less than 13,550 mm (0.5335 in): refer to Figure 6001.
of ded
(g) Machine the chamfers and radii as shown: refer to Figure 6001.
(h) Examine the part for flaws: refer to PCS-3100 inclusion class 4 and PCS-3600.
us nloa
(i) Shot peen the machined areas: refer to M-DLPS123.
siv ow
e
(j) Identify the part with the Messier-Dowty Limited repair number 64-2117007-00-B adjacent
clu - D
to the part number: refer to PCS-6000-06 or PCS-6000-04.
e
(k) Apply cadmium plate all over: refer to PCS-2100. The thickness of the cadmium plate
ex tial
must be between 0,010 and 0,020 mm (0.0004 and 0.0008 in).
n
ide
(l) Calculate diameter T of the repair bushes 61-2117017-00, use the formula:
T = D (as measured) + 0,009 to 0,025 mm (0.0004 to 0.0010 in). Refer to Figure 6002.
nf
Co
(m) Machine the repair bushes 61-2117017-00 to the dimension shown and calculated. Make
the surface finish 1,6 micrometers (63 micro-inches).
(n) Machine the inner face S of the repair bushes 61-2117017-00 to get the correct dimension
after assembly. Make the surface finish 1,6 micrometers (63 micro-inches): refer to
Figure 6002.
Repair No. 2-1
32-12-64 Page 6004
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SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(o) Examine the part for flaws: refer to PCS-3100 inclusion class 2.
e
th
(p) Apply passivation process to the repair bushes: refer to AMS-2700.
ns for
(q) Apply cadmium plate all over the repair bushes: refer to PCS-2101. The thickness of the
cadmium plate must be between 0,010 and 0,015 mm (0.0004 and 0.0006 in).
itio 0
nd 202
(r) Apply primer paint to the bracket where the bush flanges will install: refer to PCS-2500.
Co ay-
(s) Use the Press Pad (460004330/210), Drift (460004331/3) and zinc loaded Molykote DX to
install the repair bushes: refer to PCS-5100 and PCS-7305.
s & -M
(t) Check hone the inner diameters of the repair bushes to between 33,000 and 33,039 mm
rm 12
(1.2992 and 1.3007 in) by hand only. Do not machine. Refer to Figure 6002.
Te n
S so
(u) Apply sealant around the outer flanges of the bushes: refer to PCS-7200.
SL de
(v) Apply paint to the bracket, but not where shown: refer to PCS-2500 and Figure 6002.
er an
(w) Identify the part with the Messier-Dowty Limited repair number 64-2117007-00-B adjacent
nd ern
to the part number: refer to PCS-6000-07.
lu F
(x) Examine the part to make sure you have obeyed all the repair instruction correctly.
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
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e
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e
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Repair No. 2-1
32-12-64 Page 6005
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r P la
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Repair No. 2-1 - Towing Bracket (2-120)
Figure 6001/GRAPHIC 32-12-64-991-014-A01
Repair No. 2-1
32-12-64 Page 6006
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
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or Lo
r P la
tu
Ai au
P :P
TA by
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us nloa
siv ow
e
clu - D
e
ex tial
n
ide
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Repair No. 2-1 - Towing Bracket (2-120)
Figure 6002/GRAPHIC 32-12-64-991-015-A01
Repair No. 2-1
32-12-64 Page 6007
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SAFRAN LANDING SYSTEMS UK Ltd
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or Lo
r P la
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Ai au
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us nloa
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e
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e
ex tial
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Repair No. 2-1
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SAFRAN LANDING SYSTEMS UK Ltd
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
REPAIR NO. 3-1
e
th
TASK 32-12-64-300-804-A01
1. Repair No. 3-1 Jacking Dome (1-150 and 2-70)
ns for
A. Job Set-up Information
itio 0
nd 202
(1) Special Tools, Fixtures and Equipment
Co ay-
Not applicable.
s & -M
(2) Consumables
rm 12
Not applicable.
Te n
S so
(3) Referenced Information
SL de
Reference Description
er an
M-DLNDT3 Non-destructive testing inspection of ground chrome plate
M-DLPS914
nd ern Processing requirements for ultra high strength steels
M-DLPS1004-4-1 Machining requirements for ultra high tensile strength steels
lu F
1760 Mpa (255 ksi) tensile strength and above
ga pes
M-DLPS1031-2 Termination requirements for chromed surfaces overplated and
ground to size
or Lo
M-DLPS1031-6 Termination requirements for chromed surfaces overplated and
r P la
ground to size
tu
Ai au
M-DLPS3002 Guide for the On-line application of a Repair Design Solution
P :P
PCS-2100 Cadmium plating of ultra high strength steel
TA by
PCS-2110 Electrolytic hard chromium plating of steels
of ded
PCS-2300 Steel shot peening
PCS-2500 Polyurethane paint - Two coat process
us nloa
PCS-2700 Paint stripping
siv ow
PCS-3100, inclusion class 4 Magnetic particle inspection
e
PCS-3600 Etch inspection of high strength steel parts
clu - D
e
PCS-6000-04 Marking of materials, parts and assemblies (Air Scribe)
ex tial
PCS-6000-06 Marking of materials, parts and assemblies (Electrolytic)
n
PCS-6000-07 Marking of materials, parts and assemblies (Indelible ink)
ide
nf
B. Job Set-up
Co
(1) Specified Damage and Material Specification.
(a) Specified Damage
1 Damage or wear to the diameter A: refer to Figures 6001 to 6004.
Repair No. 3-1
32-12-64 Page 6001
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SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(b) Material Specification
e
th
IPL Figure and Item No. Description Material Specification
ns for
Steel, 300M to MTL1201
(1-150) and (2-70) Jacking Dome
(UHTS > 1800 MPa)
itio 0
nd 202
(2) Repair Parts
Co ay-
Not applicable.
s & -M
C. Procedure
rm 12
CAUTION: FOR DAMAGE MORE THAN THE LIMITS OF THIS REPAIR SCHEME, WRITE TO
Te n
M-DL GLOUCESTER: REFER TO M-DLPS3002.
S so
SUBTASK 32-12-64-300-010-A01
SL de
(1) Do this procedure as the first repair to diameter A if there is damage to the plating. The bare
er an
metal must not be damaged:
Refer to Figure 6001 nd ern
Refer to Figure 6002
Refer to Figure 6003
lu F
Refer to Figure 6004
ga pes
(a) Remove the paint from the jacking dome: refer to PCS-2700.
or Lo
(b) Remove the cadmium plate from the jacking dome: refer to PCS-2100.
r P la
tu
(c) Remove the chromium plate from diameter A: refer to PCS-2110 and Figures 6001 and
Ai au
6002.
P :P
(d) Examine the part for flaws: refer to PCS-3100 inclusion class 4 and PCS-3600.
TA by
(e) Apply chromium plate to diameter A. The plating thickness must be sufficient to
of ded
give a minimum thickness of 0,10 mm (0.004 in) after grinding: refer to PCS-2110,
M-DLPS1031-2, M-DLPS1031-6 and Figures 6001 to 6004.
us nloa
(f) Grind diameter A to between 32,936 and 32,975 mm (1.2967 and 1.2982 in). The surface
finish must be 0,8 micrometers (32 micro-inches): refer to M-DLPS914, M-DLPS1004-4-1
siv ow
e
and Figure 6002.
clu - D
e
(g) Examine the part for flaws: refer to M-DLNDT3.
ex tial
(h) Identify the part with the Messier-Dowty Limited repair number 64-2117008-00-VAR-A
n
adjacent to the part number: refer to PCS-6000-06 or PCS-6000-04.
ide
(i) Apply cadmium plate all over, but not where chromium plated. The thickness of the plating
nf
must be between 0,010 and 0,020 mm (0.0004 and 0.0008 in): refer to PCS-2100.
Co
Cadmium plate overlap onto chromium plate is permitted. Bare metal is not permitted.
(j) Apply paint all over, but not where shown: refer to PCS-2500 and Figure 6002.
(k) Identify the part with the Messier-Dowty Limited repair number 64-2117008-00-VAR-A
adjacent to the part number: refer to PCS-6000-07.
Repair No. 3-1
32-12-64 Page 6002
Mar 24/17
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(l) Examine the part to make sure that you have obeyed all the repair instructions correctly.
e
th
SUBTASK 32-12-64-300-011-A01
(2) Do this procedure to diameter A if the bare metal is damaged:
ns for
Refer to Figure 6001
Refer to Figure 6002
itio 0
nd 202
Refer to Figure 6003
Refer to Figure 6004
Co ay-
(a) Remove the paint from the jacking dome: refer to PCS-2700.
s & -M
(b) Remove the cadmium plate from the jacking dome: refer to PCS-2100.
rm 12
(c) Remove the chromium plate from diameter A: refer to PCS-2110, Figures 6001 and 6002.
Te n
S so
(d) Machine diameter A to remove damage or wear. Remove the minimum amount of material
necessary. Do not make diameter A less than 32,365 mm (1.2742 in). The surface finish
SL de
must be 0,8 micrometers (32 micro-inches): refer to M-DLPS914, M-DLPS1004-4-1
er an
and Figure 6002.
nd ern
(e) Machine the chamfer as shown: refer to Figure 6003.
lu F
(f) Examine the part for flaws: refer to PCS-3100 inclusion class 4 and PCS-3600.
ga pes
(g) Shot peen the machined surface: refer to PCS-2300.
or Lo
(h) Apply chromium plate to diameter A. The plating thickness must be sufficient for
machining: the total thickness of plate must be between 0,100 and 0,305 mm (0.0040
r P la
tu
and 0.0120 in) after machining: refer to PCS-2110, M-DLPS1031-2, M-DLPS1031-6
Ai au
and Figures 6001 to 6004.
P :P
(i) Grind diameter A to between 32,936 and 32,975 mm (1.2967 and 1.2982 in). The surface
TA by
finish must be 0,8 micrometers (32 micro-inches): refer to M-DLPS914, M-DLPS1004-4-1
and Figure 6002.
of ded
(j) Examine the part for flaws: refer to M-DLNDT3.
us nloa
(k) Identify the part with the Messier-Dowty Limited repair number 64-2117008-00-VAR-B
adjacent to the part number: refer to PCS-6000-06 or PCS-6000-04.
siv ow
e
clu - D
(l) Apply cadmium plate all over, but not where chromium plated. The thickness of the plating
e
must be between 0,010 and 0,020 mm (0.0004 and 0.0008 in): refer to PCS-2100.
Cadmium plate overlap onto chromium plate is permitted. Bare metal is not permitted.
ex tial
n
(m) Apply paint all over, but not where shown: refer to PCS-2500 and Figure 6002.
ide
(n) Identify the part with the Messier-Dowty Limited repair number 64-2117008-00-VAR-B
nf
adjacent to the part number: refer to PCS-6000-07.
Co
(o) Examine the part to make sure that you have obeyed all the repair instructions correctly.
Repair No. 3-1
32-12-64 Page 6003
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
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r P la
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Ai au
P :P
TA by
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e
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e
ex tial
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Co
Repair No. 3-1 - Repair to Jacking Dome
Figure 6001/GRAPHIC 32-12-64-991-016-A01
Repair No. 3-1
32-12-64 Page 6004
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SAFRAN LANDING SYSTEMS UK Ltd
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
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nd 202
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SL de
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or Lo
r P la
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Ai au
P :P
TA by
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ex tial
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ide
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Co
Repair No. 3-1 - Repair to Jacking Dome
Figure 6002/GRAPHIC 32-12-64-991-017-A01
Repair No. 3-1
32-12-64 Page 6005
Mar 24/17
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
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ns for
itio 0
nd 202
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s & -M
rm 12
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SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Repair No. 3-1 - Repair to Jacking Dome
Figure 6003/GRAPHIC 32-12-64-991-018-A01
Repair No. 3-1
32-12-64 Page 6006
Mar 24/17
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
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itio 0
nd 202
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s & -M
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SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
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Co
Repair No. 3-1 - Repair to Jacking Dome
Figure 6004/GRAPHIC 32-12-64-991-019-A01
Repair No. 3-1
32-12-64 Page 6007
Mar 24/17
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
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or Lo
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Repair No. 3-1
32-12-64 Page 6008
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SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
REPAIR NO. 4-1
e
th
TASK 32-12-64-300-805-A01
1. Repair No. 4-1 Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
ns for
A. Job Set-up Information
itio 0
nd 202
(1) Special Tools, Fixtures and Equipment
Co ay-
(a) The table below gives the special tools, fixtures and equipment necessary to repair the
component.
s & -M
rm 12
NOTE: It is permitted to use equivalent alternatives for the listed items.
Te n
NOTE: Refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT AND
S so
CONSUMABLES section for full details.
SL de
Part No. Description Function
er an
DRT68052/12 Press Pad To install the bushes 61-2117015-00 and
nd ern 61-1217005-00
DRT68052/13 Press Pad To install the bush 61-2117013-00
lu F
DRT68052/14 Press Pad To install the bushes 61-2117011-00 and
ga pes
61-2117035-00
or Lo
DRT68052/15 Press Pad To install the bush 61-2117006-00
DRT68052/16 Press Pad To install the bush 201272625B
r P la
tu
Ai au
DRT68052/17 Press Pad To install the bush 61-2117016-00
P :P
(2) Consumables
TA by
(a) The table below gives the consumables necessary to repair the component.
of ded
NOTE: Refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT AND
us nloa
CONSUMABLES section for full details.
CML Ref. Code Description
siv ow
e
AM-0470 Sealant
clu - D
e
PC-0190 Coating
ex tial
TBA Zinc Loaded Molykote DX, PCS-7305
n
ide
(3) Referenced Information
nf
Reference Description
Co
M-DLPS914 Processing requirements for ultra high strength steels
Machining requirements for ultra high tensile strength steels
M-DLPS1004-4-1
1760 Mpa (255 ksi) tensile strength and above
M-DLPS1011-14 Assembly of bushes - Wet primer
PCS-2100 Cadmium plating of ultra high strength steel
Repair No. 4-1
32-12-64 Page 6001
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Reference Description
e
th
Cadmium plating of steels UTS < 1450 MPa (210 ksi), copper
PCS-2101
alloys and aluminium alloys
ns for
PCS-2110 Electrolytic hard chromium plating of steels
itio 0
PCS-2141 LHE cadmium brush plating
nd 202
PCS-2300 Steel shot peening
Co ay-
PCS-2500 Polyurethane paint - Two coat process
s & -M
PCS-2700 Paint stripping
rm 12
PCS-3100 Magnetic particle inspection
PCS-3600 Etch inspection of high strength steel parts
Te n
S so
Assembly of bushes in steel components using Molykote DX
PCS-5100
or Zinc Loaded Molykote DX
SL de
PCS-6000 Marking of materials, parts and assemblies
er an
PCS-7200 Elastomeric filleting sealant
nd ern
PCS-7204 Anti-stone chip polysulphide coating
lu F
PCS-7305 Zinc Loaded Molykote DX
ga pes
B. Job Set-up
or Lo
(1) Specified Damage and Material Specification.
r P la
tu
Ai au
(a) Specified Damage
P :P
1 Damage or corrosion to diameters A, B, C, D, E, F, G, H, J and K (both ends) and
TA by
faces L, M, N, P, Q, R, S, T, U, V, W (both ends) and X (both ends).
of ded
(b) Material Specification
IPL Figure and Item No. Description Material Specification
us nloa
3-190, 3-190A, 3-190B, Steel, 300M to MTL1201
Bogie Beam
3 -190C and 3-190D (UTS > 1930 MPa)
siv ow
e
clu - D
(2) Repair Parts
e
(a) These repair parts are necessary:
ex tial
n
Part No. Description Material Specification
ide
61-2117011-00 Repair Bush Aluminium Bronze to AMS 4590 or
nf
AMS 4881 centrifugally cast
Co
61-2117006-00 Repair Bush Aluminium Bronze to AMS 4640 or
AMS 4880 or AMS 4590 or AMS 4881
centrifugally cast
61-2117015-00 Repair Bush Aluminium Bronze to AMS 4640 or
AMS 4880
Repair No. 4-1
32-12-64 Page 6002
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Part No. Description Material Specification
e
th
61-1217005-00 Repair Bush CRES 17-4PH condition H1025
to AMS 5643
ns for
61-2117013-00 Repair Bush Aluminium Bronze to AMS 4590 or
itio 0
AMS 4881 centrifugally cast
nd 202
201272625B Repair Bush Stainless Steel to S 145
Co ay-
61-2117016-00 Repair Bush CRES 17-4PH condition H1025 to
AMS 5643
s & -M
61-2117035-00 Repair Bush Copper Alloy Toughmet 3 AT110 to
rm 12
AMS 4596
Te n
C. Procedure
S so
SL de
CAUTION: FOR DAMAGE MORE THAN THE LIMITS OF THIS REPAIR SCHEME, WRITE TO
M-DL GLOUCESTER: REFER TO M-DLPS3002.
SUBTASK 32-12-64-300-014-A01
er an
nd ern
(1) Do this procedure only for bogie beam subassemblies (3-30), (3-30A), (3-30B), (3-30C) and
lu F
(3-30D), if there is a wear or damage to diameter A and/or diameter B and/or adjacent face
L and/or M: (For bogie beam subassemblies (3-30E), (3-30F), (3-30G), (3-30H) and (3-30I),
ga pes
go to para (5))
Refer to Figure 6001
or Lo
Refer to Figure 6002
Refer to Figure 6003
r P la
tu
Refer to Figure 6006
Ai au
Refer to Figure 6007
P :P
Refer to Figure 6008
Refer to Figure 6013
TA by
(a) Remove the paint from the bogie beam: refer to PCS-2700.
of ded
(b) Remove the coating (PC-0190): refer to PCS-7204.
us nloa
(c) Remove the cadmium plate from the bogie beam: refer to PCS-2100.
siv ow
e
(d) Machine diameters A and/or B to remove the minimum amount of material to remove the
clu - D
wear or damage. Do not increase diameter A and/or diameter B to more than 157,64 mm
e
(6.206 in). The surface finish must be 0,8 micrometres (32 micro-inches). Measure
and record diameter A and/or diameter B: refer to M-DLPS914, M-DLPS1004-4-1 and
ex tial
Figures 6001, 6002 and 6003.
n
ide
(e) Machine faces L and/or M to remove the minimum amount of material to remove the
wear or damage. The surface finish must be 1,6 micrometres (63 micro-inches): refer to
nf
M-DLPS914, M-DLPS1004-4-1 and Figures 6001, 6002 and 6003.
Co
(f) After you have machined face(s) L and M, the lug width ZC must not be less than
342,00 mm (13.465 in): refer to Figure 6003.
(g) Machine chamfer(s) and radii as shown: refer to M-DLPS914, M-DLPS1004-4-1 and
Figure 6003.
Repair No. 4-1
32-12-64 Page 6003
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(h) Examine the part for damage: refer to PCS-3100 inclusion class 4 and PCS-3600.
e
th
(i) Identify the part with the Messier-Dowty Limited repair number 64-2117002-00-A adjacent
to the existing part number with large rotary nib of 0,70 to 0,80 mm (0.028 to 0.031 in)
ns for
radius to a maximum depth of 0,20 mm (0.008 in): refer to PCS-6000-04 and Figure 6002.
itio 0
(j) Shot peen the reworked surface(s) and engraved repair number only: refer to PCS-2300.
nd 202
(k) Apply cadmium plate all over. The plating thickness must be from 0,010 to 0,020 mm
Co ay-
(0.0004 to 0.0008 in): refer to PCS-2110.
s & -M
(l) Do a check of the cadmium plating thickness: refer to REPAIR.
rm 12
(m) Apply primer paint to the bogie beam but not where shown: refer to REPAIR, PCS-2500
Te n
and Figures 6003 and 6008.
S so
(n) Do a check of the primer paint thickness: refer to REPAIR.
SL de
(o) Prepare the repair bush 61-2117011-00 (Qty 2) for installation with the dimensions that
er an
follow: refer to Figure 6013.
nd ern
1 Machine diameter AA, use the formula:
lu F
Diameter AA = Diameters A and/or B (as measured) + 0,240 to + 0,305 mm (+ 0.0094
ga pes
to + 0.0120 in).
or Lo
2 Machine face AZ to get the correct dimension after assembly. Do not damage the
chromium plating on the front flange face of the repair bush: refer to Figures 6003
r P la
and 6007.
tu
Ai au
P :P
3 Apply cadmium plate to the repair bush but not where shown. The plating thickness
must be between 0,010 to 0,015 mm (0.0004 to 0.0006 in): refer to PCS-2101 and
TA by
PCS-2141.
of ded
(p) Use Press Pad (DRT68052/14) and Zinc Loaded Molykote DX to install the repair
bush(es) with wet primer. Apply a light coat of wet primer paint under the repair bush
us nloa
flanges and along the outside diameter of the repair bush: refer to PCS-7305, PCS-5100,
M-DLPS1011-14 and Figures 6007 and 6008.
siv ow
e
(q) Hone the bore of the repair bush(es) if necessary: refer to Figure 6007.
clu - D
(r) Apply a fillet of sealant to the repair bush: refer to PCS-7200, Type 2 and Figure 6007.
e
ex tial
(s) Apply coating (PC-0190). The minimum thickness must be 0,51 mm (0.020 in): refer to
REPAIR, PCS-7204 and Figures 6006 and 6007.
n
ide
(t) Apply paint but not where shown: refer to REPAIR, PCS-2500 and Figures 6002 to 6012.
nf
(u) Do a check of the paint thickness: refer to REPAIR.
Co
(v) Identify the part with the Messier-Dowty Limited repair number 64-2117002-00-A adjacent
to the existing part number: refer to PCS-6000-07.
Repair No. 4-1
32-12-64 Page 6004
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(w) Examine the part to make sure that you have obeyed all the repair instructions correctly.
e
th
SUBTASK 32-12-64-300-015-A01
(2) Do this procedure if there is wear or damage to diameters C and/or D and/or E and/or F and/or
ns for
adjacent faces N and/or P and/or Q and/or R:
Refer to Figure 6001
itio 0
nd 202
Refer to Figure 6002
Refer to Figure 6003
Refer to Figure 6006
Co ay-
Refer to Figure 6009
s & -M
Refer to Figure 6013
rm 12
(a) Remove the paint from the bogie beam: refer to PCS-2700.
Te n
(b) Remove the coating (PC-0190): refer to PCS-7204.
S so
(c) Remove the cadmium plate from the bogie beam: refer to PCS-2100.
SL de
er an
(d) Machine diameters C and/or D and/or E and/or F to remove the minimum amount of
material to remove the wear or damage. Do not increase diameters C and/or D and/or E
nd ern
and/or F to more than 173,34 mm (6.824 in). The surface finish must be 0,8 micrometres
(32 micro-inches). Measure and record diameter C and/or D and/or E and/or F: refer to
lu F
M-DLPS914, M-DLPS1004-4-1 and Figures 6001, 6002 and 6003.
ga pes
(e) Machine faces N and/or P and/or Q and/or R to remove the minimum amount of
or Lo
material to remove the wear or damage. The surface finish must be 1,6 micrometres
(63 micro-inches): refer to M-DLPS914, M-DLPS1004-4-1 and Figures 6001, 6002 and
r P la
6003.
tu
Ai au
(f) After you have machined face(s) N and P, the width ZA must not be less than 308,845 mm
P :P
(12.1593 in) over spotface: refer to Figure 6003.
TA by
(g) After you have machined face(s) Q and R, the width ZB must not be less than 308,845 mm
of ded
(12.1593 in) over spotface: refer to Figure 6003.
(h) Machine chamfer(s) and radii as shown: refer to M-DLPS914, M-DLPS1004-4-1 and
us nloa
Figure 6003.
siv ow
e
(i) Examine the part for damage: refer to PCS-3100 inclusion class 4 and PCS-3600.
clu - D
(j) Identify the part with the Messier-Dowty Limited repair number 64-2117002-00-B adjacent
e
to the existing part number with large rotary nib of 0,70 to 0,80 mm (0.028 to 0.031 in)
ex tial
radius to a maximum depth of 0,20 mm (0.008 in): refer to PCS-6000-04 and Figure 6002.
n
(k) Shot peen the reworked surface(s) and engraved repair number only: refer to PCS-2300.
ide
(l) Apply cadmium plate all over. The plating thickness must be from 0,010 to 0,020 mm
nf
(0.0004 to 0.0008 in): refer to PCS-2100.
Co
(m) Do a check of the cadmium plating thickness: refer to REPAIR.
(n) Apply primer paint to the bogie beam but not where shown: refer to REPAIR, PCS-2500
and Figure 6003.
(o) Do a check of the primer paint thickness: refer to REPAIR.
Repair No. 4-1
32-12-64 Page 6005
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(p) Prepare the repair bush 61-2117006-00 (Qty 4) for installation in accordance with the
e
dimensions that follow: refer to Figure 6013.
th
1 Machine diameter BB, use the formula:
ns for
Diameter BB = Diameters C and/or D and/or E and/or F (as measured) + 0,270 to
itio 0
+ 0,335 mm (+ 0.0106 to + 0.0132 in).
nd 202
2 Machine face BZ to get the correct dimension after assembly: refer to Figure 6009.
Co ay-
3 Apply cadmium plate to the repair bush but not where shown. The plating thickness
s & -M
must be between 0,010 to 0,015 mm (0.0004 to 0.0006 in): refer to PCS-2101.
rm 12
(q) Use the Press Pad (DRT68052/15) and Zinc Loaded Molykote DX to install the repair
Te n
bush(es): refer to PCS-7305, PCS-5100 and Figure 6009.
S so
(r) Do a check of the bore of the repair bush(es). Do not machine. Check hone or hand
SL de
ream only if necessary: refer to Figure 6009.
er an
NOTE: Complete cleanup of bore after assembly is not necessary. Clean up area
nd ern
referes to supported area of the repair bush only.
lu F
(s) Apply a fillet of sealant to the repair bush: refer to PCS-7200, Type 2 and Figure 6009.
ga pes
(t) Apply coating (PC-0190). The minimum thickness must be 0,51 mm (0.020 in): refer to
REPAIR, PCS-7204 and Figures 6006 and 6009.
or Lo
(u) Apply paint but not where shown: refer to REPAIR, PCS-2500 and Figures 6002 to 6012.
r P la
tu
Ai au
(v) Do a check of the paint thickness: refer to REPAIR.
P :P
(w) Identify the part with the Messier-Dowty Limited repair number 64-2117002-00-B adjacent
TA by
to the existing part number: refer to PCS-6000-07.
of ded
(x) Examine the part to make sure that you have obeyed all the repair instructions correctly.
us nloa
SUBTASK 32-12-64-300-016-A01
(3) Do this procedure if there is wear or damage to diameter G and/or diameter H and/or adjacent
faces S and/or T:
siv ow
e
Refer to Figure 6001
clu - D
Refer to Figure 6002
e
Refer to Figure 6004
Refer to Figure 6006
ex tial
Refer to Figure 6010
n
Refer to Figure 6011
ide
Refer to Figure 6014
Refer to Figure 6015
nf
Co
(a) Remove the paint from the bogie beam: refer to PCS-2700.
(b) Remove the coating (PC-0190): refer to PCS-7204.
(c) Remove the cadmium plate from the bogie beam: refer to PCS-2100.
Repair No. 4-1
32-12-64 Page 6006
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(d) Machine diameter G to remove the minimum amount of material to remove the wear or
e
damage. Do not increase diameter G to more than 74,63 mm (2.938 in). The surface
th
finish must be 0,8 micrometres (32 micro-inches). Measure and record diameter G: refer
to M-DLPS914, M-DLPS1004-4-1 and Figures 6001, 6002 and 6004.
ns for
(e) Machine diameter H to remove the minimum amount of material to remove the wear or
itio 0
nd 202
damage. Do not increase diameter H to more than 81,13 mm (3.194 in). The surface
finish must be 0,8 micrometres (32 micro-inches). Measure and record diameter H: refer
to M-DLPS914, M-DLPS1004-4-1 and Figures 6001, 6002 and 6004.
Co ay-
(f) Machine faces S and/or T to remove the minimum amount of material to remove the
s & -M
wear or damage. The surface finish must be 1,6 micrometres (63 micro-inches): refer to
rm 12
M-DLPS914, M-DLPS1004-4-1 and Figures 6001, 6002 and 6004.
Te n
(g) After you have machined face(s) S and T, the lug width ZD must not be less than
S so
34,75 mm (1.368 in) over spotface: refer to Figure 6004.
SL de
(h) Machine chamfer(s) and radii as shown: refer to M-DLPS914, M-DLPS1004-4-1 and
er an
Figure 6004.
nd ern
(i) Examine the part for damage: refer to PCS-3100 inclusion class 4 and PCS-3600.
lu F
(j) Identify the part with the Messier-Dowty Limited repair number 64-2117002-00-C adjacent
ga pes
to the existing part number with large rotary nib of 0,70 to 0,80 mm (0.028 to 0.031 in)
radius to a maximum depth of 0,20 mm (0.008 in): refer to PCS-6000-04 and Figure 6002.
or Lo
(k) Shot peen the reworked surface(s) and engraved repair number only: refer to PCS-2300.
r P la
tu
Ai au
(l) Apply cadmium plate all over. The plating thickness must be from 0,010 to 0,020 mm
(0.0004 to 0.0008 in): refer to PCS-2110.
P :P
(m) Do a check of the cadmium plating thickness: refer to REPAIR.
TA by
(n) Apply primer paint to the bogie beam but not where shown: refer to REPAIR, PCS-2500
of ded
and Figures 6002, 6010 and 6011.
us nloa
(o) Do a check of the primer paint thickness: refer to REPAIR.
(p) Prepare the repair bush 61-2117015-00 for installation in accordance with the dimensions
siv ow
e
that follow: refer to Figure 6014.
clu - D
e
1 Machine diameter CC, use the formula:
ex tial
Diameter CC = Diameter G (as measured) + 0,072 to + 0,121 mm (+ 0.0028 to
n
+ 0.0048 in).
ide
2 Machine face CZ to get the correct dimension after assembly: refer to Figure 6010.
nf
Co
3 Apply cadmium plate to the repair bush but not where shown. The plating thickness
must be between 0,010 to 0,015 mm (0.0004 to 0.0006 in): refer to PCS-2101.
Repair No. 4-1
32-12-64 Page 6007
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(q) Prepare the repair bush 61-1217005-00 for installation in accordance with the dimensions
e
that follow: refer to Figure 6014.
th
1 Machine diameter DD, use the formula:
ns for
Diameter DD = Diameter G (as measured) + 0,072 to + 0,121 mm (+ 0.0028 to
itio 0
+ 0.0048 in).
nd 202
2 Machine face DZ to get the correct dimension after assembly: refer to Figure 6010.
Co ay-
3 Apply cadmium plate to the repair bush but not where shown. The plating thickness
s & -M
must be between 0,010 to 0,015 mm (0.0004 to 0.0006 in): refer to PCS-2101.
rm 12
(r) Prepare the repair bush 61-2117013-00 for installation in accordance with the dimensions
Te n
that follow: refer to Figure 6015.
S so
1 Machine diameter EE, use the formula:
SL de
Diameter EE = Diameter H (as measured) + 0,072 to + 0,121 mm (+ 0.0028 to
er an
+ 0.0048 in). nd ern
2 Machine the taper as shown.
lu F
3 Apply cadmium plate to the repair bush but not where shown. The plating thickness
ga pes
must be between 0,010 to 0,015 mm (0.0004 to 0.0006 in): refer to PCS-2101.
or Lo
(s) Use Zinc Loaded Molykote DX to install the repair bush(es) with wet primer. Use Press
Pad (DRT68052/12) to install the repair bushes 61-2117015-00 and 61-1217005-00 and
r P la
Press Pad (DRT68052/13) to install the repair bush 61-2117013-00. Apply a light coat of
tu
Ai au
wet primer paint under the repair bush flanges and along the outside diameter of the repair
P :P
bush(es): refer to PCS-7305, PCS-5100, M-DLPS1011-14 and Figures 6010 and 6011.
TA by
(t) Do a check of the bore of the repair bush(es). Do not machine. Check hone or hand
ream only if necessary: refer to Figure 6010.
of ded
(u) Apply a fillet of sealant to the repair bush(es): refer to PCS-7200, Type 2 and Figure 6010.
us nloa
(v) Apply coating (PC-0190). The minimum thickness must be 0,51 mm (0.020 in): refer to
REPAIR, PCS-7204 and Figures 6006 and 6010.
siv ow
e
(w) Apply paint but not where shown: refer to REPAIR, PCS-2500 and Figures 6002 to 6012.
clu - D
e
(x) Do a check of the paint thickness: refer to REPAIR.
ex tial
(y) Identify the part with the Messier-Dowty Limited repair number 64-2117002-00-C adjacent
n
ide
to the existing part number: refer to PCS-6000-07.
nf
(z) Examine the part to make sure that you have obeyed all the repair instructions correctly.
Co
Repair No. 4-1
32-12-64 Page 6008
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
SUBTASK 32-12-64-300-017-A01
e
(4) Do this procedure if there is wear or damage to diameter J and/or diameter K and/or adjacent
th
faces U and/or V and/or X and/or W:
Refer to Figure 6001
ns for
Refer to Figure 6002
itio 0
Refer to Figure 6005
nd 202
Refer to Figure 6006
Refer to Figure 6012
Co ay-
Refer to Figure 6015
Refer to Figure 6016
s & -M
(a) Remove the paint from the bogie beam: refer to PCS-2700.
rm 12
(b) Remove the coating (PC-0190): refer to PCS-7204.
Te n
S so
(c) Remove the cadmium plate from the bogie beam: refer to PCS-2110.
SL de
(d) Machine diameter J to remove the minimum amount of material to remove the wear or
er an
damage. Do not increase diameter J to more than 34,939 mm (1.3756 in). The surface
finish must be 1,6 micrometres (63 micro-inches). Measure and record diameter J: refer
nd ern
to M-DLPS914, M-DLPS1004-4-1 and Figures 6001, 6002 and 6005.
lu F
(e) Machine diameter K to remove the minimum amount of material to remove the wear or
ga pes
damage. Do not increase diameter K to more than 37,939 mm (1.4937 in). The surface
finish must be 1,6 micrometres (63 micro-inches). Measure and record diameter K: refer
or Lo
to M-DLPS914, M-DLPS1004-4-1 and Figures 6001, 6002 and 6005.
r P la
(f) Machine face U and/or spotface V to remove the minimum amount of material to remove
tu
Ai au
the wear or damage. The surface finish must be 1,6 micrometres (63 micro-inches): refer
to M-DLPS914, M-DLPS1004-4-1 and Figures 6001, 6002 and 6005.
P :P
TA by
(g) After you have machined face(s) U and V, the web thickness ZG must not be less than
15,75 mm (0.620 in): refer to Figure 6005.
of ded
(h) Machine face(s) X and/or face W to remove the minimum amount of material to remove
us nloa
the wear or damage. The surface finish must be 1,6 micrometres (63 micro-inches): refer
to M-DLPS914, M-DLPS1004-4-1 and Figures 6001, 6002 and 6005.
siv ow
e
(i) After you have machined face(s) X and W, the length ZF must not be less than 29,75 mm
(1.171 in): refer to Figure 6005.
clu - D
e
(j) Machine chamfer(s) and radii as shown: refer to M-DLPS914, M-DLPS1004-4-1 and
ex tial
Figure 6005.
n
(k) Examine the part for damage: refer to PCS-3100 inclusion class 4 and PCS-3600.
ide
(l) Identify the part with the Messier-Dowty Limited repair number 64-2117002-00-D adjacent
nf
to the existing part number with large rotary nib of 0,70 to 0,80 mm (0.028 to 0.031 in)
Co
radius to a maximum depth of 0,20 mm (0.008 in): refer to PCS-6000-04 and Figure 6002.
(m) Shot peen the reworked surface(s) and engraved repair number only: refer to PCS-2300.
(n) Apply cadmium plate all over. The plating thickness must be from 0,010 to 0,020 mm
(0.0004 to 0.0008 in): refer to PCS-2110.
Repair No. 4-1
32-12-64 Page 6009
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(o) Do a check of the cadmium plating thickness: refer to REPAIR.
e
th
(p) Apply primer paint to the bogie beam but not where shown: refer to REPAIR, PCS-2500
and Figure 6005.
ns for
(q) Do a check of the primer paint thickness: refer to REPAIR.
itio 0
nd 202
(r) Prepare the repair bush 201272625B (Qty 2) for installation in accordance with the
dimensions that follow: refer to Figure 6015.
Co ay-
1 Machine diameter FF, use the formula:
s & -M
Diameter FF = Diameter J (as measured) - 0,005 to + 0,050 mm (- 0.0002 to
rm 12
+ 0.0020 in).
Te n
S so
2 Machine face FZ to get the correct dimension after assembly: refer to Figure 6012.
SL de
3 Apply cadmium plate to the repair bush but not where shown. The plating thickness
must be between 0,010 to 0,015 mm (0.0004 to 0.0006 in): refer to PCS-2101.
er an
(s)
nd ern
Prepare the repair bush 61-2117016-00 (Qty 4) for installation in accordance with the
dimensions that follow: refer to Figure 6016.
lu F
1 Machine diameter GG, use the formula:
ga pes
Diameter GG = Diameters K (as measured) - 0,005 to + 0,050 mm (- 0.0002 to
or Lo
+ 0.0020 in).
r P la
2 Machine face GZ to get the correct dimension after assembly: refer to Figure 6012.
tu
Ai au
3 Passivate the repair bush: refer to AMS 2700.
P :P
TA by
4 Apply cadmium plate to the repair bush but not where shown. The plating thickness
must be between 0,010 to 0,015 mm (0.0004 to 0.0006 in): refer to PCS-2101.
of ded
(t) Prepare the saddle washer 55-2117021-00 (Qty 2) for installation in accordance with the
us nloa
dimensions that follow: refer to Figure 6016.
1 Locally remove cadmium plate from washer bore: refer to PCS-2101.
siv ow
e
2 Machine diameter S, use the formula:
clu - D
e
Diameter S = Diameters K (as measured) + 0,081 to + 0,159 mm (+ 0.0032 to
ex tial
+ 0.0063 in)
n
3 Machine the chamfer as shown.
ide
4 Apply cadmium plate to the machined faces. The plating thickness must be between
nf
0,010 to 0,015 mm (0.0004 to 0.0006 in): refer to PCS-2101.
Co
(u) Use Zinc Loaded Molykote DX to install the repair bush(es). Use Press Pad (DRT68052/16)
to install the repair bushes 201272625B and Press Pad (DRT68052/17) to install the
repair bushes 61-2117016-00 and saddle washer 55-2117021-00: refer to PCS-7305,
PCS-5100 and Figure 6012.
Repair No. 4-1
32-12-64 Page 6010
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(v) Do a check of the bore of the repair bush(es). Do not machine. Check hone or hand
e
ream only if necessary: refer to Figure 6012.
th
(w) Apply a fillet of sealant to the repair bush(es): refer to PCS-7200, Type 2 and Figure 6012.
ns for
(x) Apply coating (PC-0190). The minimum thickness must be 0,51 mm (0.020 in): refer to
itio 0
REPAIR, PCS-7204 and Figures 6006 and 6012.
nd 202
(y) Apply paint but not where shown: refer to REPAIR, PCS-2500 and Figures 6002 to 6012.
Co ay-
(z) Do a check of the paint thickness: refer to REPAIR.
s & -M
(aa) Identify the part with the Messier-Dowty Limited repair number 64-2117002-00-D adjacent
rm 12
to the existing part number: refer to PCS-6000-07.
Te n
S so
(ab) Examine the part to make sure that you have obeyed all the repair instructions correctly.
SL de
SUBTASK 32-12-64-300-018-A01
(5) Do this procedure only for bogie beam subassemblies (3-30E), (3-30F), (3-30G), (3-30H) and
er an
(3-30I) if there is a wear or damage to diameter A and/or diameter B and/or adjacent face L
nd ern
and/or M:(For bogie beam subassemblies (3-30), (3-30A), (3-30B), (3-30C) and (3-30D), go to
para (1)).
lu F
Refer to Figure 6001
ga pes
Refer to Figure 6002
Refer to Figure 6003
or Lo
Refer to Figure 6006
Refer to Figure 6007
r P la
Refer to Figure 6008
tu
Ai au
Refer to Figure 6013
P :P
(a) Remove the paint from the bogie beam: refer to PCS-2700.
TA by
(b) Remove the coating (PC-0190): refer to PCS-7204.
of ded
(c) Remove the cadmium plate from the bogie beam: refer to PCS-2100.
us nloa
(d) Machine diameters A and/or B to remove the minimum amount of material to remove the
wear or damage. Do not increase diameter A and/or diameter B to more than 157,64 mm
siv ow
(6.206 in). The surface finish must be 0,8 micrometres (32 micro-inches). Measure
e
and record diameter A and/or diameter B: refer to M-DLPS914, M-DLPS1004-4-1 and
clu - D
Figures 6001, 6002 and 6003.
e
ex tial
(e) Machine faces L and/or M to remove the minimum amount of material to remove the
wear or damage. The surface finish must be 1,6 micrometres (63 micro-inches): refer to
n
M-DLPS914, M-DLPS1004-4-1 and Figures 6001, 6002 and 6003.
ide
(f) After you have machined face(s) L and M, the lug width ZC must not be less than
nf
342,00 mm (13.465 in): refer to Figure 6003.
Co
(g) Machine chamfer(s) and radii as shown: refer to M-DLPS914, M-DLPS1004-4-1 and
Figure 6003.
(h) Examine the part for damage: refer to PCS-3100 inclusion class 4 and PCS-3600.
Repair No. 4-1
32-12-64 Page 6011
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(i) Identify the part with the Messier-Dowty Limited repair number 64-2117002-00-E adjacent
e
to the existing part number with large rotary nib of 0,70 to 0,80 mm (0.028 to 0.031 in)
th
radius to a maximum depth of 0,20 mm (0.008 in): refer to PCS-6000-04 and Figure 6002.
ns for
(j) Shot peen the reworked surface(s) and engraved repair number only: refer to PCS-2300.
itio 0
(k) Apply cadmium plate all over. The plating thickness must be from 0,010 to 0,020 mm
nd 202
(0.0004 to 0.0008 in): refer to PCS-2110.
Co ay-
(l) Do a check of the cadmium plating thickness: refer to REPAIR.
s & -M
(m) Apply primer paint to the bogie beam but not where shown: refer to REPAIR, PCS-2500
rm 12
and Figures 6003 and 6008.
Te n
(n) Do a check of the primer paint thickness: refer to REPAIR.
S so
(o) Prepare the repair bush 61-2117035-00 (Qty 2) for installation with the dimensions that
SL de
follow: refer to Figure 6013.
er an
1 Machine diameter AA, use the formula:
nd ern
Diameter AA = Diameters A and/or B (as measured) + 0,240 to + 0,305 mm (+ 0.0094
lu F
to + 0.0120 in).
ga pes
2 Machine face AZ to get the correct dimension after assembly. Do not damage the
chromium plating on the front flange face of the repair bush: refer to Figures 6003
or Lo
and 6007.
r P la
3 Apply cadmium plate to the repair bush but not where shown. The plating thickness
tu
Ai au
must be between 0,010 to 0,015 mm (0.0004 to 0.0006 in): refer to PCS-2101 and
P :P
PCS-2141.
TA by
(p) Use Press Pad (DRT68052/14) and Zinc Loaded Molykote DX to install the repair
bush(es) with wet primer. Apply a light coat of wet primer paint under the repair bush
of ded
flanges and along the outside diameter of the repair bush: refer to PCS-7305, PCS-5100,
M-DLPS1011-14 and Figures 6007 and 6008.
us nloa
(q) Hone the bore of the repair bush(es) if necessary: refer to Figure 6007.
siv ow
e
(r) Apply a fillet of sealant to the repair bush: refer to PCS-7200, Type 2 and Figure 6007.
clu - D
(s) Apply coating (PC-0190). The minimum thickness must be 0,51 mm (0.020 in): refer to
e
REPAIR, PCS-7204 and Figures 6006 and 6007.
ex tial
(t) Apply paint but not where shown: refer to REPAIR, PCS-2500 and Figures 6002 to 6012.
n
ide
(u) Do a check of the paint thickness: refer to REPAIR.
nf
(v) Identify the part with the Messier-Dowty Limited repair number 64-2117002-00-E adjacent
Co
to the existing part number: refer to PCS-6000-07.
(w) Examine the part to make sure that you have obeyed all the repair instructions correctly.
Repair No. 4-1
32-12-64 Page 6012
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6001/GRAPHIC 32-12-64-991-037-A01
Repair No. 4-1
32-12-64 Page 6013
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6002/GRAPHIC 32-12-64-991-038-A01
Repair No. 4-1
32-12-64 Page 6014
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6003/GRAPHIC 32-12-64-991-039-A01
Repair No. 4-1
32-12-64 Page 6015
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6004/GRAPHIC 32-12-64-991-040-A01
Repair No. 4-1
32-12-64 Page 6016
Mar 22/19
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
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Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6005/GRAPHIC 32-12-64-991-041-A01
Repair No. 4-1
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Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6006/GRAPHIC 32-12-64-991-042-A01
Repair No. 4-1
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Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6007/GRAPHIC 32-12-64-991-043-A01
Repair No. 4-1
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Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6008/GRAPHIC 32-12-64-991-044-A01
Repair No. 4-1
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Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6009/GRAPHIC 32-12-64-991-045-A01
Repair No. 4-1
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Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6010/GRAPHIC 32-12-64-991-046-A01
Repair No. 4-1
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Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6011/GRAPHIC 32-12-64-991-047-A01
Repair No. 4-1
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CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
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Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6012/GRAPHIC 32-12-64-991-048-A01
Repair No. 4-1
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Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6013/GRAPHIC 32-12-64-991-049-A01
Repair No. 4-1
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Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6014/GRAPHIC 32-12-64-991-050-A01
Repair No. 4-1
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CAGE: K0654
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Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6015/GRAPHIC 32-12-64-991-051-A01
Repair No. 4-1
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CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
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Repair No. 4-1 - Repair to Bogie Beam (3-190), (3-190A), (3-190B), (3-190C) and (3-190D)
Figure 6016/GRAPHIC 32-12-64-991-052-A01
Repair No. 4-1
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
ASSEMBLY
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TASK 32-12-64-400-801-A01
1. Assembly
ns for
A. Job Set-up Information
itio 0
nd 202
(1) Special Tools, Fixtures and Equipment
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(a) The table below gives the special tools, fixtures and equipment necessary to assemble
the component.
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NOTE: It is permitted to use equivalent alternatives for the listed items.
Te n
NOTE: Refer to the SPECIAL TOOLS, FIXTURES, EQUIPMENT AND
S so
CONSUMABLES section for full details.
SL de
Part No. Description Function
er an
Local Supply Oven Heat the bogie beam (3-190) and the axle
nd ern spacers (3-10)
Local Supply Freezing Chamber Cool the axles (3-20)
lu F
DRT66784 Lifting Equipment Lift the the axles (3-20) and bogie beam
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subassembly (3-30)
or Lo
DRT67035 Punch Install the lubrication adapters (3-170)
DRT67088 Torque Spanner Torque the spigots (1-190) and (2-160)
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tu
Ai au
DRT67093 Holding Tool Hold the axle spigot nuts (1-200) and
(2-170)
P :P
DRT67958-13 Line Up Pin Check the alignment of the bushes (3-50),
TA by
(3-60) and (3-70)
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DRT68004-1 Axle Stops Set axle on center line of bogie
DRT68052/12 Press Pad Install the bushes (3-50) and (3-60)
us nloa
DRT68052/13 Press Pad Install the bush (3-70)
DRT68052/14 Press Pad Install the bushes (3-150)
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e
DRT68052/15 Press Pad Install the bushes (3-100) and (3-110)
clu - D
e
DRT68052/16 Press Pad Install the bushes (3-120)
ex tial
DRT68052/17 Press Pad Install the bushes (3-80) and (3-130)
n
DRT68782 Bogie Beam Locator Align the rear axle (3-20) in the bogie beam
ide
(3-190)
nf
DRT68806 Bogie Beam Locator Align the forward axle (3-20) in the bogie
Co
beam (3-190)
DRT68843 Punch Install the dowels (3-40)
T14565 Crowfoot Spanner Torque the nuts (1-120) and (2-60)
T14566 Socket Hold the jacking dome subassembly (1-130)
and the jacking dome (2-70
32-12-64 Page 7001
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(2) Consumables
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(a) The table below gives the consumables necessary to assemble the component.
ns for
NOTE: It is permitted to use equivalent alternatives for the listed items.
itio 0
nd 202
CML Ref. code Description
TBA Lockwire, PCS-7610
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TBA Liquid nitrogen
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TBA Zinc loaded Molykote DX, PCS-7305
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LM-0100A Grease
LM-0060A Grease
Te n
S so
PC-0680 Corrosion Preventive Compound
SL de
AM-0165 Adhesive
er an
TBA Sealant, PCS-7200
TBA
nd ern
Cotsolv 4021
TBA Metsolv 4021
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TBA Rocol Aerospec Protect Spray
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(3) Referenced Information
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Reference Description
tu
Ai au
M-DLPS1011-14 Assembly of bushes - Wet primer
P :P
M-DLPS1011-20 Assembly of bushes in steel components - Zinc loaded mastinox
TA by
D40
PCS-2141 LHE cadmium Brush Plating
of ded
PCS-2500 Polyurethane paint - Two coat process
us nloa
PCS-5100 Assembly of bushes in steel components using Molykote DX
or Zinc Loaded Molykote DX
siv ow
e
PCS-6000-05 Marking of materials, parts and assemblies (Vibrating engraver)
clu - D
PCS-7200 Elastomeric filleting sealant
e
PCS-7302 Molykote DX mineral oil based jointing compound
ex tial
PCS-7305 Zinc Loaded Molykote DX
n
PCS-7610 Locking of threaded components
ide
PGBLK-32-12-64-4000-1 Cleaning
nf
PGBLK-32-12-64-6000-1 Repair
Co
PGBLK-32-12-64-8000-1 Fits and clearances
PGBLK-32-12-64-9000-1 Special tools, fixtures, equipment and consumables
32-12-64 Page 7002
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
B. Job Set-up
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SUBTASK 32-12-64-400-001-A01
(1) General
ns for
(a) Make sure that all of the parts are clean: refer to CLEANING.
itio 0
nd 202
(b) Make sure that the work area, the tools and the equipment are clean.
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(c) Make sure that all of the parts are correct to the data given in FITS AND CLEARANCES.
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(d) Torque all the parts that have threads: refer to M-DLPS1002-1, unless different torque
values are in FITS AND CLEARANCES.
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(e) Unless otherwise stated, lubricate all threads, thread undercuts, splines, bolt shanks
Te n
S so
(other than chromium plated pin diameters lubricated with grease), cavities, voids and
between the interfaces of mating parts with Corrosion Preventive Compound (PC-0680),
SL de
before you install them: refer to PCS-7302.
er an
(f) When you apply sealant or Corrosion Preventive Compound (PC-0680), make sure that
nd ern
you get a good seal. The layer must be continuous; there must be no space between the
surfaces after assembly to allow contamination or corrosion.
lu F
ga pes
C. Procedure
SUBTASK 32-12-64-440-001-A01
or Lo
(1) Bogie Beam Subassembly (3-30)
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(a) Install the bushes (3-150) (Refer to Figure 7001)
tu
Ai au
P :P
1 Machine the faces of the bushes (3-150) that will be against the bogie beam (3-190)
so that:
TA by
a There will be a dimension of between 349,99 and 350,16 mm (13.779 and
of ded
13.785 in) across the outer flange faces when they are assembled.
us nloa
b There is not more than 0,10 mm (0.004 in) in difference in thickness between
the flanges.
siv ow
e
c The surface finish must be 1,6 micrometers (63 micro-inches).
clu - D
2 Refer to PCS-6000-05. Identify the bushes (3-150) with their part numbers. Put the
e
part numbers on the faces that you have machined. Remove the burrs and make
ex tial
sure that the faces are flat.
n
ide
3 Apply cadmium plate to the machined surfaces: refer to PCS-2141. The thickness of
the cadmium plate must be 0,010 to 0,015 mm (0.0004 to 0.0006 in).
nf
4 Make sure that the surfaces of the bogie beam (3-190) are primer painted where the
Co
bushes (3-150) are to be installed: refer to REPAIR and PCS-2500.
5 Apply wet primer paint under the flange and between 24,0 and 26,0 mm (0.94 and
1.02 in) of the outside diameter of the bushes (3-150): refer to M-DLPS1011-14. Do
not get primer paint in the bush bores or on the flanges.
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
6 Apply zinc loaded Molykote DX to the bogie beam (3-190): refer to PCS-7305 and
e
Figure 7001.
th
7 Install the bushes (3-150) in the bogie beam (3-190): refer to PCS-5100. Use the
ns for
Press Pad (DRT68052/14).
itio 0
8 Check ream the bushes (3-150) to between 149,225 and 149,265 mm (5.8750 to
nd 202
5.8766 in): the surface finish must be 0,8 micrometers (32 micro-inches).
Co ay-
9 Apply sealant around the flanges of the bushes (3-150): refer to PCS-7200.
s & -M
(b) Install the bushes (3-80) and (3-130) (Refer to Figure 7002)
rm 12
1 Use Press Pad (DRT68052/17) and zinc loaded Molykote DX to install the bushes
Te n
(3-80) and (3-130) and the saddle washers (3-90) and (3-140) in the bogie beam
S so
(3-190): refer to PCS-5100 and PCS-7305.
SL de
2 Measure the dimension over the flanges of the bushes (3-80) and (3-130).
er an
3 Machine the flange faces of the bushes (3-80) and (3-130) so that:
nd ern
a The dimension across the flange faces is between 40,300 and 40,350 mm
lu F
(1.5866 and 1.5886 in)
ga pes
b There is not more than 0,10 mm (0.004 in) difference in thickness between the
flange faces
or Lo
c The surface finish is 1,6 micrometers (63 micro-inches).
r P la
tu
Ai au
4 Check dimension. Do not machine. Check hone or hand ream the bushes (3-80) and
P :P
(3-130) to between 33,000 and 33,039 mm (1.2992 and 1.3007 in): the surface finish
must be 1,6 micrometers (63 micro-inches).
TA by
5 Apply sealant around the bushes and between the end faces of the bushes (3-80)
of ded
and (3-130): refer to PCS-7200 and Figure 7002.
us nloa
(c) Install the bushes (3-120) (Refer to Figure 7002)
1 Make sure that the surfaces of the bogie beam (3-190) are primer painted where the
siv ow
e
bushes (3-120) are to be installed: refer to REPAIR and PCS-2500.
clu - D
2 Install the bushes (3-120) in the bogie beam (3-190). Refer to PCS-5100 and
e
PCS-7305 and use zinc loaded Molykote DX. Use the Press Pad (DRT68052/16).
ex tial
3 Check dimension. Do not machine. Check hone or hand ream the bushes (3-120)
n
ide
to between 30,000 and 30,052 mm (1.1811 and 1.1831 in): the surface finish must
be 1,6 micrometers (63 micro-inches).
nf
4 Apply sealant around the bushes and between the end faces of the bushes (3-120):
Co
refer to PCS-7200 and Figure 7002.
(d) Install the bushes (3-100) and (3-110) (Refer to Figure 7003)
1 Install the bushes (3-100) and (3-110) in the bogie beam (3-190). Refer to PCS-5100
and PCS-7305 and use zinc loaded Molykote DX. Use the Press Pad (DRT68052/15).
32-12-64 Page 7004
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
2 Machine the flange faces of the bushes (3-100) and (3-110) so that:
e
th
a The dimension is between 158,400 and 158,500 mm (6.2362 and 6.2401 in)
from the center line of the bogie beam (3-190) to the flange face of each bush
ns for
(3-100) and (3-110).
itio 0
b The surface finish is 1,6 micrometers (63 micro-inches).
nd 202
3 Check dimension. Do not machine. Check hone or hand ream the bushes (3-100)
Co ay-
and (3-110) to between 165,040 and 165,080 mm (6.4976 and 6.4992 in): the surface
finish must be 1,6 micrometers (63 micro-inches).
s & -M
rm 12
4 Apply sealant around the bushes (3-100) and (3-110): refer to PCS-7200.
Te n
(e) Install the bush (3-70) (Refer to Figure 7004)
S so
1 Make sure that the internal surfaces of the bogie beam (3-190) are primer painted
SL de
where the bush (3-70) is to be installed: refer to REPAIR and PCS-2500.
er an
2 Apply wet primer paint under the flange for a length of 23,000 to 25,000 mm (0.9055
nd ern
to 0.9843 in) of the outside diameter of the bush (3-70): refer to M-DLPS1011-14. Do
not get primer paint in the bush bore or on the flange.
lu F
ga pes
3 Apply zinc loaded Molykote DX to the bogie beam (3-190): refer to PCS-7305 and
Figure 7004. Use the Press Pad (DRT68052/13) to install the bush (3-70) in the
bogie beam (3-190): refer to PCS-5100 and PCS-7305.
or Lo
4 Check dimension. Do not machine. Check hone or hand ream the bush (3-70) to
r P la
tu
between 73,000 and 73,030 mm (2.8740 and 2.8751 in). The surface finish must be
Ai au
0,8 micrometers (32 micro-inches). Use the Line Up Pin (DRT67958-13) to check the
P :P
alignment of the bush (3-70).
TA by
5 Apply sealant around the bush (3-70): refer to PCS-7200.
of ded
(f) Install the bushes (3-50) and (3-60) (Refer to Figure 7004)
us nloa
1 Make sure that the internal surfaces of the bogie beam (3-190) are primer painted
where the bushes (3-50) and (3-60) are to be installed: refer to REPAIR and
PCS-2500.
siv ow
e
clu - D
2 Apply wet primer paint under the flange for a length of 6,00 to 8,00 mm (0.236
e
to 0.315 in) of the outside diameter of the bushes (3-50) and (3-60): refer to
M-DLPS1011-14. Do not get primer paint in the bores or on the flanges of the bushes.
ex tial
n
3 Apply zinc loaded Molykote DX, to the bogie beam (3-190): refer to PCS-7305 and
ide
Figure 7004. Use the Press Pad (DRT68052/12) to install the bushes (3-50) and
(3-60) in the bogie beam (3-190): refer to PCS-5100 and PCS-7305.
nf
Co
4 Check dimension. Do not machine. Check hone or hand ream the bushes (3-50) and
(3-60) to between 66,600 and 66,646 mm (2.6220 and 2.6238 in): the surface finish
must be 0,8 micrometers (32 micro-inches). Use the Line Up Pin (DRT67958-13) to
check the alignment of the bushes (3-50) and (3-60).
5 Apply sealant around the bushes and between the end faces of the bushes (3-50)
and (3-60): refer to PCS-7200.
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
(g) Install the lubrication adapters (3-170) and the dowels (3-40)
e
th
1 Apply adhesive (AM-0165) to the lubrication adapters (3-170): refer to PCS-5303.
ns for
2 Install the washers (3-180). Use the Punch (DRT67035) to install the lubrication
adapters (3-170). Install the lubrication fittings (3-160). Align the lubrication fittings
itio 0
(3-160) to face the towing bracket subassembly (2-10).
nd 202
3 PRE SB A33/34-32-315. Lubricate through the lubrication fittings (3-160) with
Co ay-
Grease (LM-0060A), make sure that the grease comes through to the bushes
(3-150): refer to M-DLPS1005-1.
s & -M
rm 12
4 POST SB A33/34-32-315. Lubricate through the lubrication fittings (3-160) with
Grease (LM-0100A), make sure that the grease comes through to the bushes
Te n
(3-150A): refer to M-DLPS1005-1.
S so
5 Apply primer paint to the holes for the dowels (3-40): refer to M-DLPS1011-20 and
SL de
PCS-2500.
er an
6 Apply zinc loaded Molykote DX to the diameter of the dowels (3-40) that will be in the
nd ern
bogie beam (3-190): refer to PCS-7305.
lu F
7 Use the Punch (DRT68843) to install the dowels (3-40): make sure that between 7,75
ga pes
and 8,75 mm (0.305 and 0.344 in) of the dowel (3-40) shows.
SUBTASK 32-12-64-440-002-A01
or Lo
(2) Install the Axles (3-20)
r P la
tu
WARNING: WEAR PROTECTIVE CLOTHING WHEN YOU HANDLE HOT COMPONENTS.
Ai au
P :P
(a) Put the bogie beam subassembly (3-30) in the oven and apply heat at 60 °C (140 °F)
for four hours.
TA by
NOTE: Use the Lifting Equipment (DRT66784) as necessary to lift the bogie beam
of ded
subassembly (3-30).
us nloa
WARNING: WEAR PROTECTIVE CLOTHING WHEN YOU USE LIQUID NITROGEN.
siv ow
(b) Fill the Freezing Chamber with liquid nitrogen, Material Ref. Item TBA, and put the axles
e
(3-30) into it. Keep the axles (3-30) in the Freezing Chamber until the liquid nitrogen stops
clu - D
boiling: add liquid nitrogen, Material Ref. Item TBA as necessary to keep the freezing
e
chamber full. The minimum temperature of the axle must be -183 °C (-297.4 °F).
ex tial
WARNING: WEAR PROTECTIVE CLOTHING WHEN YOU HANDLE HOT COMPONENTS.
n
ide
(c) Remove the bogie beam subassembly (3-30) from the oven.
nf
WARNING: WEAR PROTECTIVE CLOTHING WHEN YOU USE LIQUID NITROGEN.
Co
CAUTION: USE CARE TO MOVE THE AXLES (3-20), FREEZING MAKES THEM BRITTLE
AND MAKES IT EASY TO DAMAGE THEM.
(d) Remove the axles (3-20) from the Freezing Chamber.
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(e) Apply a minimum quantity of Corrosion Preventive Compound (PC-0680), to the internal
e
diameter of the bushes (3-110) and (3-100): refer to PCS-7302.
th
(f) Use the Lifting Equipment (DRT66784) to install the axles (3-20) in the bogie beam
ns for
subassembly (3-30). Use the Axle Stops (DRT68004-1) and the Bogie Beam
Locators (DRT68782 and DRT68806) to align the axles (3-20): the holes in the axles
itio 0
nd 202
must be concentric with the internal diameter of the bogie beam subassembly (3-30) to
0,10 mm (0.004 in).
Co ay-
(g) Remove the Axle Stops (DRT68004-1) and the Bogie Beam Locators (DRT68782 and
DRT68806).
s & -M
rm 12
(h) Allow the temperature of the bogie beam and axle subassembly (2-190) to stabilize.
Te n
(i) Use Metsolv 4021 (TBA) or Cotsolv 4021 (TBA) to clean the area of the axles (3-20)
S so
where the axle spacers (3-10) will install. Use lint free wipes to remove the remaining
Metsolv 4021 or Cotsolv 4021 from the axles.
SL de
er an
(j) Apply a thin uniform coat of Rocol Aerospec Protect Spray (TBA) to the area of the axles
(3-20) at an ambient temperature: refer to Figure 7005. Let the coating for 30 minutes to
nd ern
dry before install the axle spacers (3-10).
lu F
WARNING: WEAR PROTECTIVE CLOTHING WHEN YOU HANDLE HOT COMPONENTS.
ga pes
(k) Put the axle spacers (3-10) in the oven and apply heat to 150 °C (302 °F).
or Lo
(l) Remove the axle spacers (3-10) from the oven.
r P la
tu
Ai au
(m) Install the axle spacers (3-10) over the axles (3-20) and that the axle spacers touch the
bush flanges. Make sure one pair of the drain holes are aligned at ninety degrees to the
P :P
length of the bogie beam subassembly.
TA by
SUBTASK 32-12-64-440-003-A01
of ded
(3) Towing Bracket Subassembly (2-10)
(a) Make sure the surfaces of the towing bracket (2-120) that will be under the flanges of the
us nloa
bushes (2-110) and (2-100) are primer painted before bush installation: refer to PCS-2500.
siv ow
(b) Install the bushes (2-110)
e
clu - D
1 Use zinc loaded Molykote DX to install the bushes (2-110) in the towing bracket
e
(2-120): refer to PCS-5100 and PCS-7305.
ex tial
2 Measure the dimension across the flanges of the bushes (2-110): it must be
n
78,900 mm (3.1063 in). This is a reference dimension do not machine it.
ide
3 Apply sealant all around the bushes (2-110) and between the end faces of the
nf
bushes: refer to PCS-7200.
Co
(c) Install the bushes (2-100)
1 Use zinc loaded Molykote DX to install the bushes (2-100) in the towing bracket
(2-120): refer to PCS-5100 and PCS-7305.
2 Machine the flange faces of the inner bushes (2-100) so that:
32-12-64 Page 7007
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
a There is a dimension of between 40,400 and 40,450 mm (1.5905 and 1.5925 in)
e
between the flange faces
th
b There is not more than 0,25 mm (0.010 in) in difference in thickness between
ns for
the flange faces
itio 0
c The surface finish is 1,6 micrometers (63 micro-inches).
nd 202
3 Machine the flange faces of the outer bushes (2-100) so that:
Co ay-
a There is a dimension of between 77,450 and 77,550 mm (3.0492 and 3.0531 in)
s & -M
across the flange faces
rm 12
b There is not more than 0,25 mm (0.010 in) in difference in thickness between
Te n
the flange faces
S so
c The surface finish is 1,6 micrometers (63 micro-inches).
SL de
4 Measure the internal diameter of the bushes (2-100). The dimension must be between
er an
33,000 and 33,039 mm (1.2992 and 1.3007 in). Check dimension. Do not machine.
nd ern
Hone or ream by hand. The surface finish must be 0,8 micrometers (32 micro-inches).
lu F
5 Apply sealant all around the flanges of the bushes (2-100): refer to PCS-7200.
ga pes
SUBTASK 32-12-64-440-004-A01
(4) Bogie Assembly (1-1)
or Lo
(a) Refer to PCS-7302. Apply Corrosion Preventive Compound (PC-0680) to:
r P la
tu
Ai au
1 The face of the spigot (2-160) that will be against the diaphragm (2-180).
P :P
2 The thread of the spigot (2-160).
TA by
3 The rounded part of the axle spigot nut (2-170).
of ded
(b) Refer to PCS-7302. Apply Corrosion Preventive Compound (PC-0680) to:
us nloa
1 The threads of the bolt (2-130).
siv ow
e
2 The face of the locking segment (2-150) that will be against the diaphragm (2-180).
clu - D
3 The curved surface of the diaphragm (2-180), where it will touch the axle (3-20).
e
ex tial
(c) Refer to PCS-7200. Apply sealant to the external diameter of the diaphragm (2-180),
where it will touch the bogie beam and axle subassembly (2-190).
n
ide
(d) Install the diaphragm (2-180) in the bogie beam and axle subassembly (2-190). Remove
all of the unwanted sealant from the joint.
nf
Co
(e) Use the Holding Tool (DRT67093) to install the axle spigot nut (2-170) in the axle (3-20)
and hold it in position.
(f) Install the spigot (2-160) through the diaphragm (2-180) and the axle (3-20) into the
axle spigot nut (2-170).
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(g) Use the Torque Spanner (DRT67088) to torque the spigot (2-160) to between 100 and
e
120 N m (73.80 and 88.56 lbf ft).
th
(h) Remove the Holding Tool (DRT67093) from the axle spigot nut (2-170).
ns for
(i) Install the locking segment (2-150), the washers (2-140) and the bolts (2-130).
itio 0
nd 202
(j) Torque the bolts (2-130) to between 3 and 4 N m (27 and 36 lbf in).
Co ay-
(k) Safety the bolts (2-130): refer to PCS-7610.
s & -M
(l) Refer to PCS-7200. Apply sealant to:
rm 12
1 The heads of the bolts (2-130).
Te n
S so
2 The joint between the diaphragm (2-180) and the bogie beam subassembly (3-30).
SL de
(m) Refer to PCS-7302. Apply Corrosion Preventive Compound (PC-0680) to:
er an
1 The diameter and threads of the jacking dome (2-70).
nd ern
2 The face of the jacking dome (2-70) that will touch the towing bracket subassembly
(2-10).
lu F
ga pes
3 The threads of the bolt (2-50).
or Lo
(n) Install the towing bracket subassembly (2-10).
r P la
(o) Install the jacking dome (2-70) through the bogie beam subassembly (3-30) and the
tu
Ai au
towing bracket subassembly (2-10).
P :P
(p) Install the nut (2-60).
TA by
(q) Hold the jacking dome (2-70) with the Socket (T14566). Use the Crowfoot
of ded
Spanner (T14565) to torque the nut (2-60) to 136 N m (100 lbf ft) and then reduce the
torque to zero.
us nloa
(r) Do para (q) two more times.
siv ow
(s) Use the Crowfoot Spanner (T14565) to torque the nut (2-60) to 81 N m (60 lbf ft).
e
clu - D
NOTE: You can increase the torque to a maximum of 339 N m (250 lbf ft) to let
e
you install the bolt (2-50).
ex tial
(t) Install the bolt (2-50), the washers (2-40) and the nut (2-30).
n
ide
(u) Torque the nut (2-30) to between 2,70 and 3,15 N m (24 and 28 lbf in).
nf
(v) Install the split pin (2-20) and safety: refer to PCS-7610.
Co
(w) Refer to PCS-7200. Apply sealant to:
1 The hexagonal nut of the jacking dome (2-70).
2 The nut (2-60).
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
3 The bolt (2-50), the washers (2-40), the nut (2-30) and the split pin (2-20).
e
th
(x) Refer to PCS-7302. Apply Corrosion Preventive Compound (PC-0680) to:
ns for
1 The face of the spigot (1-190) that will be against the diaphragm (1-210).
itio 0
2 The thread of the spigot (1-190).
nd 202
3 The rounded part of the axle spigot nut (1-200).
Co ay-
(y) Refer to PCS-7302. Apply Corrosion Preventive Compound (PC-0680) to:
s & -M
1 The threads of the bolt (1-160).
rm 12
2 The face of the locking segment (1-180) that will be against the diaphragm (1-210).
Te n
S so
3 The curved surface of the diaphragm (1-210), where it will touch the axle (3-20).
SL de
(z) Refer to PCS-7200. Apply sealant to the external diameter of the diaphragm (1-210),
er an
where it will touch the bogie beam and axle subassembly (2-190).
nd ern
(aa) Install the diaphragm (1-210) in the bogie beam and axle subassembly (2-190). Remove
all of the unwanted sealant from the joint.
lu F
ga pes
(ab) Use the Holding Tool (DRT67093) to install the axle spigot nut (1-200) into the axle (3-20)
and hold it in position.
or Lo
(ac) Install the spigot (1-190) through the diaphragm (1-210) and the axle (3-20) into the
r P la
axle spigot nut (1-200).
tu
Ai au
(ad) Use the Torque Spanner (DRT67088) to torque the spigot (1-190) to between 100 and
P :P
120 N m (73.80 and 88.56 lbf ft).
TA by
(ae) Remove the Holding Tool (DRT67093) from the axle spigot nut (1-200).
of ded
(af) Install the locking segment (1-180), the washers (1-170) and the bolts (1-160).
us nloa
(ag) Torque the bolts (1-160) to between 3 and 4 N m (27 and 36 lbf in).
siv ow
(ah) Safety the bolts (1-160): refer to PCS-7610.
e
clu - D
(ai) Refer to PCS-7200. Apply sealant to:
e
1 The heads of the bolts (1-160).
ex tial
n
2 The joint between the diaphragm (1-210) and the bogie beam subassembly (3-30).
ide
(aj) Refer to PCS-7302. Apply Corrosion Preventive Compound (PC-0680) to:
nf
Co
1 The diameter and threads of the jacking dome subassembly (1-130)
2 The threads of the bolt (1-110).
(ak) Install the jacking dome subassembly (1-130) through the bogie beam subassembly
(3-30).
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(al) Install the nut (1-120).
e
th
(am) Hold the jacking dome subassembly (1-130) with the Socket (T14566). Use the Crowfoot
Spanner (T14565) to torque the nut (1-120) to 136 N m (100 lbf ft) and then reduce the
ns for
torque to zero.
itio 0
(an) Do para (am) two more times.
nd 202
(ao) Use the Crowfoot Spanner (T14565) to torque the nut (1-120) to 81 N m (60 lbf ft).
Co ay-
NOTE: You can increase the torque to a maximum of 339 N m (250 lbf ft) to let
s & -M
you install the bolt (1-110).
rm 12
(ap) Install the bolt (1-110), the washers (1-100) and the nut (1-90).
Te n
S so
(aq) Torque the nut (1-90) to between 2,70 and 3,15 N m (24 and 28 lbf in).
SL de
(ar) Install the split pin (1-80) and safety: refer to PCS-7610.
er an
(as) Refer to PCS-7200. Apply sealant to:
nd ern
1 The hexagonal nut of the jacking dome subassembly (1-130).
lu F
2 The nut (1-120).
ga pes
3 The bolt (1-110), the washers (1-100), the nut (1-90) and the split pin (1-80).
or Lo
(at) Apply Corrosion Preventive Compound (PC-0680), to the threads of the wheel nuts (1-60).
r P la
Install the axle rings (1-70) and the wheel nuts (1-60): refer to Figure 7006.
tu
Ai au
P :P
NOTE: Install the axle rings (1-70) with the notch to the bogie beam subassembly
(3-30).
TA by
(au) Temporarily install the bolts (1-50), the washers (1-30) and (1-40) and the nuts (1-20),
of ded
with the maximum of three washers (1-30) in each position.
us nloa
(av) Install the split pins (1-10) and open sufficiently to hold in position.
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 7011
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e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Bogie Beam Subassembly - Preparation and Installation of Bushes (3-150)
Figure 7001/GRAPHIC 32-12-64-991-020-A01
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e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Bogie Beam Subassembly - Installation of Bushes (3-130, 3-120 and 3-80)
Figure 7002/GRAPHIC 32-12-64-991-021-A01
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e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Bogie Beam Subassembly - Installation of Bushes (3-100 or 3-110)
Figure 7003/GRAPHIC 32-12-64-991-022-A01
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e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Bogie Beam Subassembly - Preparation and Installation of Bushes (3-70, 3-60 and 3-50)
Figure 7004/GRAPHIC 32-12-64-991-023-A01
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e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Axles (3-20) - Application of Rocol Aerospec Protect Spray
Figure 7005/GRAPHIC 32-12-64-991-054-A01
32-12-64 Page 7016
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e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Axle Rings (1-70) - Installation
Figure 7006/GRAPHIC 32-12-64-991-024-A01
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
SUBTASK 32-12-64-440-005-A01
e
(5) Paint
th
(a) Examine the paint finish for damage: if there is damage, repair it. Refer to REPAIR.
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 7018
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
FITS AND CLEARANCES
e
th
TASK 32-12-64-940-801-A01
1. Fits and Clearances
ns for
A. General
itio 0
nd 202
Not applicable.
Co ay-
B. Layout
s & -M
(1) Fits and Clearances Definitions, Refer to Tables 8001 to 8003.
rm 12
(a) Initial Manufacturing Limits
Te n
S so
1 Dimension
SL de
a These figures are the maximum and minimum dimensions of new parts. The
difference between the two dimensions is the tolerance.
er an
2
nd ern
Assembly Clearance
a These figures are the maximum and minimum clearances when two parts are
lu F
assembled together. A minus sign (-) shows an interference fit.
ga pes
(b) In-service Wear Limits
or Lo
1 Dimension Limits
r P la
tu
Ai au
a These figures are the dimensions to which parts can wear and be used: the
difference between the two dimensions must not be more than the allowable
P :P
clearance.
TA by
2 Allowable Clearance
of ded
a This figure is the maximum allowable clearance between the two parts which are
assembled together. A minus sign (-) shows an interference fit.
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 8001
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e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Fits and Clearances - Key Diagram
Figure 8001/GRAPHIC 32-12-64-991-025-A01
32-12-64 Page 8002
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e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Fits and Clearances
Figure 8002/GRAPHIC 32-12-64-991-026-A01
32-12-64 Page 8003
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SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
SUBTASK 32-12-64-998-001-A01
e
C. Fits and Clearances Table
th
Fits and Clearances
ns for
Table 8001
itio 0
nd 202
Initial Manufacturing Limits In-Service Wear Limits
Mating
Fig
IPL Allowable
8004 Dimension Assembly Clearance Dimension Limits
Co ay-
Figure Clearance
Ref. mm (in) mm (in) mm (in)
and Item mm (in)
Ltr.
s & -M
No.
MIN MAX MIN MAX MIN MAX MAX
rm 12
(3-190) 170,960 171,020 170,960 171,020
ID (6.7307) (6.7331) (6.7307) (6.7331)
Te n
-0,405 -0,310 -0,310
S so
A (3-100)
171,330 171,365 (-0.0159) (-0.0122) 171,330 171,365 (-0.0122)
(3-110)
SL de
(6.7453) (6.7467) (6.7453) (6.7467)
OD
er an
(3-30) 165,040 165,080 nd ern 165,040 165,080
ID (6.4976) (6.4992) -0,195 -0,130 (6.4976) (6.4992) -0,130
B
(3-20) 165,210 165,235 (-0.0077) (-0.0051) 165,210 165,235 (-0.0051)
lu F
OD (6.5043) (6.5053) (6.5043) (6.5053)
ga pes
(3-190) 155,260 155,020 155,260 155,320
or Lo
ID (6.1126) (6.1150) -0,375 -0,280 (6.1126) (6.1150) -0,280
C
(3-150) 155,600 155,635 (-0.0148) (-0.0110) 155,600 155,635 (-0.0110)
r P la
OD (6.1260) (6.1274) (6.1260) (6.1274)
tu
Ai au
349,990 350,160 0,210 0,560 349,977 350,160 0,840
P :P
(3-150)
(13.7791) (13.7858) (0.0083) (0.0220) (13.7786) (13.7858) (0.0331)
D
TA by
Dimension across bush faces
of ded
(3-190) End float End float End float
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 8004
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e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Fits and Clearances
Figure 8003/GRAPHIC 32-12-64-991-027-A01
32-12-64 Page 8005
Mar 24/17
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Fits and Clearances
e
Table 8002
th
Initial Manufacturing Limits In-Service Wear Limits
ns for
Mating
Fig
IPL Allowable
8003 Dimension Assembly Clearance Dimension Limits
itio 0
Figure Clearance
nd 202
Ref. mm (in) mm (in) mm (in)
and Item mm (in)
Ltr.
No.
MIN MAX MIN MAX MIN MAX MAX
Co ay-
(1-210)
s & -M
and 44,600 44,700 44,600 44,863
(2-180) (1.7559) (1.7598) (1.7559) (1.7662)
rm 12
ID 0,150 0,275 0,413
A
Te n
(1-190) (0.0059) (0.0108) (0.0162)
S so
and 44,425 44,450 44,187 44,450
SL de
(2-160) (1.7490) (1.7500) (1.7396) (1.7500)
OD
er an
(3-20) 44,525 44,595nd ern 44,525 44,705
ID (1.7530) (1.7557) (1.7530) (1.7600)
0,075 0,170 0,255
lu F
B (1-190)
and 44,425 44,450 (0.0030) (0.0067) 44,270 44,450 (0.0100)
ga pes
(2-160) (1.7490) (1.7500) (1.7429) (1.7500)
OD
or Lo
(2-120) 63,460 63,510 63,460 63,510
r P la
ID (2.4984) (2.5004) -0,142 -0,063 (2.4984) (2.5004) -0,063
tu
Ai au
C
(2-110) 63,573 63,602 (-0.0056) (-0.0025) 63,573 63,602 (-0.0025)
P :P
OD (2.5029) (2.5040) (2.5029) (2.5040)
TA by
(3-190) 32,960 33,019 32,960 33,019
ID (1.2976) (1.3000) -0,120 -0,035 (1.2976) (1.3000) -0,035
of ded
D
(3-120) 33,054 33,080 (-0.0047) (-0.0014) 33,054 33,080 (-0.0014)
OD (1.3013) (1.3024) (1.3013) (1.3024)
us nloa
(3-90) and
36,090 36,139 36,090 36,208
(3-140)
siv ow
(1.4209) (1.4228) (1.4209) (1.4255)
e
ID 0,010 0,085 0,128
E
clu - D
(3-80) and (0.0004) (0.0033) (0.0050)
36,054 36,080 35,962 36,080
e
(3-130)
(1.4194) (1.4205) (1.4158) (1.4205)
ex tial
OD
(3-190) 35,960 36,019 35,960 36,019
n
ide
ID (1.4157) (1.4181) (1.4157) (1.4181)
-0,120 -0,035 -0,035
F (3-80) and
nf
36,054 36,080 (-0.0047) (-0.0014) 36,054 36,080 (-0.0014)
(3-130)
Co
(1.4194) (1.4205) (1.4194) (1.4205)
OD
(2-120) 35,960 36,005 35,960 36,005
ID (1.4157) (1.4175) -0,120 -0,049 (1.4157) (1.4175) -0,049
G
(2-100) 36,054 36,080 (-0.0047) (-0.0019) 36,054 36,080 (-0.0019)
OD (1.4194) (1.4205) (1.4194) (1.4205)
32-12-64 Page 8006
Mar 24/17
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Fits and Clearances
e
Table 8002 (continued)
th
ns for
Initial Manufacturing Limits In-Service Wear Limits
Mating
Fig
IPL Allowable
itio 0
8003 Dimension Assembly Clearance Dimension Limits
Figure Clearance
nd 202
Ref. mm (in) mm (in) mm (in)
and Item mm (in)
Ltr.
No.
Co ay-
MIN MAX MIN MAX MIN MAX MAX
(3-30) 33,000 33,039 33,000 33,052
s & -M
ID (1.2992) (1.3007) 0,025 0,103 (1.2992) (1.3012) 0,129
H
rm 12
(2-70) 32,936 32,975 (0.0010) (0.0041) 32,923 32,975 (0.0051)
OD (1.2967) (1.2982) (1.2962) (1.2982)
Te n
S so
(2-10) 33,000 33,039 33,000 33,052
ID (1.2992) (1.3007) (1.2992) (1.3012)
SL de
0,025 0,103 0,129
I
(2-70) 32,936 32,975 (0.0010) (0.0041) 32,923 32,975 (0.0051)
er an
OD (1.2967) (1.2982)
nd ern (1.2962) (1.2982)
(3-30) 33,000 33,039 33,000 33,052
ID (1.2992) (1.3007) (1.2992) (1.3012)
lu F
0,025 0,103 0,129
J
(0.0010) (0.0041) (0.0051)
ga pes
(1-150) 32,936 32,975 32,923 32,975
OD (1.2967) (1.2982) (1.2962) (1.2982)
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 8007
Mar 24/17
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Fits and Clearances
Figure 8004/GRAPHIC 32-12-64-991-028-A01
32-12-64 Page 8008
Mar 24/17
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Fits and Clearances
e
Table 8003
th
Initial Manufacturing Limits In-Service Wear Limits
ns for
Mating
Fig
IPL Allowable
8004 Assembly Clearance Dimension Limits
itio 0
Figure Dimension mm (in) Clearance
nd 202
Ref. mm (in) mm (in)
and Item mm (in)
Ltr.
No.
MIN MAX MIN MAX MIN MAX MAX
Co ay-
(3-190) 78,960 79,010 78,960 79,010
s & -M
ID (3.1087) (3.1106) (3.1087) (3.1106)
-0,191 -0,112 -0,112
rm 12
A
(-0.0075) (-0.0044) (-0.0044)
(3-70) 79,122 79,151 79,122 79,151
Te n
S so
OD (3.1150) (3.1162) (3.1150) (3.1162)
(3-190) 72,460 72,510 72,460 72,510
SL de
ID (2.8528) (2.8547) (2.8528) (2.8547)
er an
-0,191 -0,112 -0,112
B
nd ern (-0.0075) (-0.0044) (-0.0044)
(3-60) 72,622 72,651 72,622 72,651
OD (2.8591) (2.8603) (2.8591) (2.8603)
lu F
(3-190) 72,460 72,510 72,460 72,510
ga pes
ID (2.8528) (2.8547) (2.8528) (2.8547)
-0,191 -0,112 -0,112
or Lo
C
(-0.0075) (-0.0044) (-0.0044)
(3-50) 72,622 72,651 72,622 72,651
r P la
OD (2.8591) (2.8603) (2.8591) (2.8603)
tu
Ai au
(3-190) 19,460 19,501 19,460 19,501
P :P
ID (0.7661) (0.7678) (0.7661) (0.7678)
-0,103 -0,045 -0,045
TA by
D
(-0.0041) (-0.0018) (-0.0018)
(3-40) 19,546 19,563 19,546 19,563
of ded
OD (0.7695) (0.7702) (0.7695) (0.7702)
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 8009
Mar 24/17
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
TASK 32-12-64-940-802-A01
e
2. Torque Values
th
A. Torque Data
ns for
(1) Torque the parts in Table 8004 to their applicable values.
itio 0
nd 202
Torque Data
Table 8004
Co ay-
IPL Figure Torque Torque
s & -M
Name
and Item No. N m lbf ft or lbf in
rm 12
(1-90) Nut 2,70 to 3,15 (24 to 28 lbf in)
Te n
(1-120) Nut 81 (60 lbf ft)
S so
(1-160) Bolt 3 to 4 (27 to 36 lbf in)
SL de
(1-190) Spigot 100 to 120 (73.80 to 88.56 lbf ft)
er an
(2-30) Nut 2,70 to 3,15 (24 to 28 lbf in)
nd ern
(2-60) Nut 81 (60 lbf ft)
lu F
(2-130) Bolt 3 to 4 (27 to 36 lbf in)
ga pes
(2-160) Spigot 100 to 120 (73.80 to 88.56 lbf ft)
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 8010
Mar 24/17
SAFRAN LANDING SYSTEMS UK Ltd
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
SPECIAL TOOLS, FIXTURES, EQUIPMENT AND CONSUMABLES
e
th
TASK 32-12-64-940-803-A01
1. Special Tools, Fixtures and Equipment
ns for
A. General
itio 0
nd 202
(1) These special tools are necessary:
Co ay-
NOTE: It is permitted to use equivalent alternatives for the listed items.
s & -M
Special Tools, Fixtures and Equipment
rm 12
Table 9001
Te n
Part No. Description Function
S so
Heat the bogie beam (3-190) and the axle
Local Supply Oven
SL de
spacers (3-10)
er an
Local Supply Freezing Chamber Cool the axles (3-20)
Local Supply Hydraulic Press
nd ern Remove the axles (3-20)
Lift the bogie beam and axle subassembly
lu F
DRT66784 Lifting Equipment (2-190), the axles (3-20) and the bogie
ga pes
beam subassembly (3-30)
DRT67035 Punch Install the lubrication adapters (3-170)
or Lo
Remove/torque the spigots (1-190) and
DRT67088 Torque Spanner
r P la
(2-160)
tu
Ai au
DRT67093 Holding Tool Hold the nuts (1-200) and (2-170)
P :P
DRT67958-13 Line Up Pin Check the alignment of the bushes (3-50),
TA by
(3-60) and (3-70)
DRT68004-1 Axle Stops Set axle on center line of bogie
of ded
DRT68052/12 Press Pad Install the bushes (3-50) and (3-60)
us nloa
DRT68052/13 Press Pad Install the bush (3-70)
DRT68052/14 Press Pad Install the bushes (3-150)
siv ow
e
DRT68052/15 Press Pad Install the bushes (3-100) and (3-110)
clu - D
DRT68052/16 Press Pad Install the bushes (3-120)
e
DRT68052/17 Press Pad Install the bushes (3-80) and (3-130)
ex tial
Align the rear axle (3-20) in the bogie beam
n
DRT68782 Bogie Beam Locator
(3-190)
ide
Align the forward axle (3-20) in the bogie
nf
DRT68806 Bogie Beam Locator
beam (3-190)
Co
DRT68843 Punch Install the dowels (3-40)
DRT68906 Spacer Removal Tool Remove the axle spacers (3-10)
Remove the bushes (3-50), (3-60), (3-70),
HS122000 BushOut Kit
(3-100) and (3-110)
32-12-64 Page 9001
Mar 20/20
SAFRAN LANDING SYSTEMS UK Ltd
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
Special Tools, Fixtures and Equipment
e
Table 9001 (continued)
th
ns for
Part No. Description Function
Remove and torque the nuts (1-120) and
itio 0
T14565 Crowfoot Spanner
(2-60)
nd 202
Hold the jacking dome subassembly
T14566 Socket
Co ay-
(1-130) and the jacking dome (2-70)
s & -M
TASK 32-12-64-940-804-A01
rm 12
2. Consumables
Te n
A. General
S so
(1) These consumables are necessary.
SL de
NOTE: It is permitted to use equivalent alternatives for the listed items.
er an
nd ern Consumables
Table 9002
lu F
ga pes
CML Ref. code Description
AM-0165 Adhesive
or Lo
AM-0470 Sealant
r P la
AM-0610 Insulating compound
tu
Ai au
AM-0850 Pressure sensitive adhesive tape
P :P
CM-0095 Cleaning product
TA by
LM-0060A Grease
of ded
LM-0100A Grease
MM-0520 Green PVC sheet
us nloa
MM-0525 Wax paper
LM-0550 Grease
siv ow
e
PC-0680 Corrosion Preventive Compound
clu - D
e
PC-0770 Corrosion preventive compound
ex tial
PC-0190 Coating
n
TBA Lockwire, PCS-7610
ide
TBA Liquid nitrogen
nf
TBA Zinc loaded Molykote DX, PCS-7305
Co
TBA Sealant, PCS-7200
TBA Cotsolv 4021
TBA Metsolv 4021
TBA Rocol Aerospec Protect Spray
32-12-64 Page 9002
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
STORAGE AND TRANSPORTATION
e
th
TASK 32-12-64-500-801-A01
1. Storage Instructions
ns for
A. Job Set-up Information
itio 0
nd 202
(1) Special Tools, Fixtures and Equipment
Co ay-
Not applicable.
s & -M
(2) Consumables
rm 12
(a) These consumables are necessary to prevent damage to the unit during usual storage
conditions.
Te n
S so
NOTE: It is permitted to use equivalent alternatives for the listed items.
SL de
CML Ref. Code Description
er an
MM-0520 Green PVC sheet
nd ern
AM-0610 Insulating compound
lu F
AM-0850 Pressure sensitive adhesive tape
ga pes
MM-0525 Wax paper
or Lo
LM-0550 Grease
r P la
(3) Referenced Information
tu
Ai au
P :P
Reference Description
M-DLPS1016-1-1 General Storage Information
TA by
M-DLPS1016-8-2 Storage and Preservation of Main Landing Gear
of ded
PCS-2800 Temporary corrosion and damage protection of parts
us nloa
B. Job Set-up
siv ow
e
Not applicable.
clu - D
C. Procedure
e
ex tial
SUBTASK 32-12-64-550-001-A01
(1) Storage
n
ide
(a) PRE SB A33/34-32-315. Use the consumables in para 1. A. (2). for preservation: refer to
M-DLPS1016-1-1 and M-DLPS1016-8-2.
nf
Co
(b) POST SB A33/34-32-315. Use the consumables in para 1. A. (2). for preservation:
refer to PCS-2800.
32-12-64 Page 15001
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SAFRAN LANDING SYSTEMS UK Ltd
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
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itio 0
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Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
This page intentionally left blank.
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 15002
Mar 22/19
Co
nf
ide
n
ex tial
clu - D
siv ow
e
us nloa
e
of ded
TA by
P :P
Ai au
r P la
or Lo
tu
ga pes
lu F
nd ern
er an
SL de
S so
Te n
ILLUSTRATED PARTS LIST
rm 12
s & -M
Co ay-
nd 202
itio 0
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
32-12-64
ns for
th
e
Sep 21/18
Page 10001
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SAFRAN LANDING SYSTEMS UK Ltd
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
This page intentionally left blank.
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 10002
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
TASK 32-12-64-871-802-A01
e
1. Introduction
th
A. General
ns for
(1) This parts list illustrates and identifies each part of the component in this CMM. Use it to identify
itio 0
parts and to help with provisioning.
nd 202
(2) The Illustrated Parts List contains:
Co ay-
(a) a Numerical Index (where applicable)
s & -M
rm 12
(b) a Detailed Parts List
Te n
(c) all necessary data for the procurement of parts.
S so
B. Numerical Index (where applicable)
SL de
(1) The Numerical Index is to help you find part numbers in the Detailed Parts List.
er an
(2)
nd ern
Deleted or superseded part numbers have these identifications:
lu F
(a) Deleted - (D)
ga pes
(b) Superseded - (S)
or Lo
(3) The Total Required column (TTL REQ) shows the total necessary each time the part number is
shown in the Detailed Parts List.
r P la
tu
Ai au
C. Detailed Parts List
P :P
(1) In general part numbers are in the DISASSEMBLY sequence. The parts are indented to show
TA by
that they are related to the next higher assembly (NHA).
of ded
(2) The Effectivity Code (EFF. CODE) agrees with that of the next higher assembly. The effectivity
code also shows if subassemblies and details are applicable to their next higher assembly or
us nloa
subassembly. When an item is applicable to all units the Effectivity Code column will be empty.
The effectivity code usage is specific to the IPL figure to which it applies.
siv ow
e
(3) The quantity in the Units per Assembly column is the quantity necessary for the next higher
assembly. AR in the Units per Assembly column shows that the quantity of parts to be used is
clu - D
as required. RF in the Units per Assembly column shows that the part is for reference only.
e
ex tial
(4) The Part Numbers that are shown (NP) in the Detailed Parts List are non-procurable items.
Unless the part has been superseded the next higher assembly must be installed.
n
ide
nf
Co
32-12-64 Page 10003
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
TASK 32-12-64-980-801-A01
e
2. Vendor Codes, Names and Addresses
th
NOTE: Below you will find a list of vendor codes associated to this Component Maintenance
ns for
Manual. For the latest vendor name and address details associated to these codes
itio 0
please refer to the master list of Vendor Codes, Names and Addresses that is available
nd 202
within the Safran Landing Systems Technical Publications on-line service - document
titled - ‘List of Contacts’.
Co ay-
A. Not applicable.
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 10004
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
TASK 32-12-64-879-801-A01
e
3. How to Use the Illustrated Parts List
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 10005
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
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itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
This page intentionally left blank.
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 10006
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
ALPHA/NUMERIC INDEX
e
th
ns for
PART NUMBER AIRLINE FIGURE ITEM TOTAL
itio 0
STOCK NUMBER NUMBER REQ'D
nd 202
NUMBER
Co ay-
AS15001-4C 003 –160B 2
s & -M
AS15001-4P 003 –160A 2
rm 12
MS15001-4 003 160 2
Te n
S so
MS17825-3 001 090 1
002 030 1
SL de
MS17825-4 001 020 8
er an
MS21209F4-15P
nd ern 001 –140 1
002 –080 -
lu F
MS24665-153 001 010 8
ga pes
080 1
002 020 1
or Lo
NAS1149F0363P 001 100 2
r P la
002 040 2
tu
Ai au
P :P
NAS1149F0432P 001 030 16
170 2
TA by
002 140 2
of ded
NAS1149F0463P 001 040 8
us nloa
NAS6603D27 001 110 1
002 050 1
siv ow
e
NAS6604D9 001 050 8
clu - D
NAS6604H2 001 160 2
e
002 130 2
ex tial
P332602 003 180 2
n
ide
10-211701-000 001 –001 RF
nf
002 –001 RF
Co
10-211701-001 001 –001A RF
002 –001A RF
10-211701-002 001 –001B RF
002 –001B RF
32-12-64 Page 10007
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SAFRAN LANDING SYSTEMS UK Ltd
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10-211701 SERIES COMPONENT MAINTENANCE MANUAL
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th
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PART NUMBER AIRLINE FIGURE ITEM TOTAL
STOCK NUMBER NUMBER REQ'D
itio 0
NUMBER
nd 202
10-211701-003 001 –001C RF
Co ay-
002 –001C RF
s & -M
10-211701-004 001 –001D RF
rm 12
002 –001D RF
Te n
201272606 001 190 1
S so
002 160 1
SL de
201272609 001 200 1
er an
002 170 1
nd ern
201272619 001 180 1
002 150 1
lu F
ga pes
201272621 001 120 1
002 060 1
or Lo
201272625 003 120 2
r P la
tu
201272639 001 070 4
Ai au
P :P
201485608 002 110 2
TA by
30-2117002-00 003 –030 1
of ded
30-2117002-01 003 –030A 1
us nloa
30-2117002-02 003 –030D 1
30-2117004-00 002 190 1
siv ow
e
003 –001 RF
clu - D
30-2117004-01 002 –190A 1
e
003 –001A RF
ex tial
30-2117004-02 002 –190D 1
n
ide
003 –001D RF
nf
30-2117007-00 002 –010 1
Co
30-2117008-00 001 –130 1
30-2117032-00 003 –030B 1
30-2117032-01 003 –030C 1
32-12-64 Page 10008
Dec 07/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
PART NUMBER AIRLINE FIGURE ITEM TOTAL
STOCK NUMBER NUMBER REQ'D
itio 0
NUMBER
nd 202
30-2117032-02 003 –030H 1
Co ay-
30-2117034-00 002 –190B 1
s & -M
003 –001B RF
rm 12
30-2117034-01 002 –190C 1
Te n
003 –001C RF
S so
30-2117034-02 002 –190H 1
SL de
003 –001H RF
er an
30-2117037-00 nd ern 003 –030E 1
30-2117037-01 003 –030F 1
lu F
ga pes
30-2117037-02 003 –030I 1
30-2117038-00 002 –190E 1
or Lo
003 –001E RF
r P la
30-2117038-01 002 –190F 1
tu
Ai au
003 –001F RF
P :P
30-2117038-02 002 –190I 1
TA by
003 –001I RF
of ded
30-2117039-00 003 –030G 1
us nloa
30-2117040-00 002 –190G 1
003 –001G RF
siv ow
e
50-2117002-00 003 190 1
clu - D
50-2117002-01 003 –190A 1
e
ex tial
50-2117002-02 003 –190D 1
n
50-2117032-00 003 –190B 1
ide
50-2117032-01 003 –190C 1
nf
Co
55-1217005-00 003 060 1
55-2117003-00 003 020 2
55-2117005-00 003 010 4
32-12-64 Page 10009
Dec 07/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
PART NUMBER AIRLINE FIGURE ITEM TOTAL
STOCK NUMBER NUMBER REQ'D
itio 0
NUMBER
nd 202
55-2117007-00 002 120 1
Co ay-
55-2117008-00 001 150 1
s & -M
rm 12
55-2117009-00 002 070 1
–090 -
Te n
S so
55-2117010-00 003 040 2
SL de
55-2117012-00 001 210 1
002 180 1
er an
55-2117021-00
nd ern 003 090 1
140 1
lu F
ga pes
55-2117022-00 001 060 4
65-2117006-00 003 100 2
or Lo
110 2
r P la
65-2117011-00 003 150 2
tu
Ai au
P :P
65-2117013-00 003 070 1
TA by
65-2117015-00 003 050 1
of ded
65-2117016-00 003 080 2
130 2
us nloa
65-2117017-00 002 100 4
siv ow
e
65-2117035-00 003 –150A 2
clu - D
899005010 003 170 2
e
ex tial
n
ide
nf
Co
32-12-64 Page 10010
Dec 07/18
Co
nf
ide
n
ex tial
clu - D
siv ow
e
us nloa
e
of ded
TA by
P :P
Ai au
r P la
or Lo
tu
ga pes
lu F
nd ern
er an
SL de
S so
Te n
DETAILED PARTS LIST
rm 12
s & -M
Co ay-
nd 202
itio 0
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
32-12-64
ns for
th
e
Sep 21/18
Page 10011
CAGE: K0654
SAFRAN LANDING SYSTEMS UK Ltd
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Bogie Assembly
Figure 1/GRAPHIC 32-12-64-991-901-A01
32-12-64 Page 10012
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
th
STOCK 1234567 CODE PER
ns for
NUMBER ASSY
itio 0
1 – 001 10-211701-000 BOGIE ASSEMBLY A RF
nd 202
SEE CMM 32-12-63 FOR NHA
(PRE SB A33/34-32-283)
Co ay-
– 001A 10-211701-001 BOGIE ASSEMBLY B RF
s & -M
SEE CMM 32-12-63 FOR NHA
rm 12
(POST SB A33/34-32-283,
PRE SB A33/34-32-304)
Te n
S so
– 001B 10-211701-002 BOGIE ASSEMBLY C RF
SEE CMM 32-12-63 FOR NHA
SL de
(POST SB A33/34-32-304,
er an
PRE SB A33/34-32-305)
nd ern
– 001C 10-211701-003 BOGIE ASSEMBLY D RF
SEE CMM 32-12-63 FOR NHA
lu F
(POST SB A33/34-32-305,
ga pes
PRE SB A33/34-32-315)
or Lo
– 001D 10-211701-004 BOGIE ASSEMBLY E RF
SEE CMM 32-12-63 FOR NHA
r P la
(POST SB A33/34-32-315)
tu
Ai au
010 MS24665-153 . PIN, SPLIT 8
P :P
020 MS17825-4 . NUT 8
TA by
030 NAS1149F0432P . WASHER 16
of ded
040 NAS1149F0463P . WASHER 8
us nloa
050 NAS6604D9 . BOLT 8
siv ow
e
060 55-2117022-00 . NUT, WHEEL 4
clu - D
070 201272639 . RING, AXLE 4
e
ex tial
080 MS24665-153 . PIN, SPLIT 1
n
ide
090 MS17825-3 . NUT 1
nf
100 NAS1149F0363P . WASHER 2
Co
110 NAS6603D27 . BOLT 1
120 201272621 . NUT 1
– 130 30-2117008-00 . DOME SUBASSEMBLY, JACKING 1
– 140 MS21209F4-15P . . INSERT, WIRE 1
– ITEM NOT ILLUSTRATED
32-12-64 Page 10013
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
e
STOCK 1234567 CODE PER
th
NUMBER ASSY
ns for
1 150 55-2117008-00 . . DOME, JACKING NP 1
itio 0
nd 202
160 NAS6604H2 . BOLT 2
Co ay-
170 NAS1149F0432P . WASHER 2
s & -M
180 201272619 . SEGMENT, LOCKING 1
rm 12
190 201272606 . SPIGOT 1
Te n
200 201272609 . NUT, AXLE SPIGOT 1
S so
210 55-2117012-00 . DIAPHRAGM 1
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
– ITEM NOT ILLUSTRATED
32-12-64 Page 10014
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
This page intentionally left blank.
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
32-12-64 Page 10015
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Bogie Assembly
Figure 2/GRAPHIC 32-12-64-991-902-A01
32-12-64 Page 10016
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
th
STOCK 1234567 CODE PER
ns for
NUMBER ASSY
itio 0
2 – 001 10-211701-000 BOGIE ASSEMBLY A RF
nd 202
SEE CMM 32-12-63 FOR NHA
(PRE SB A33/34-32-283)
Co ay-
– 001A 10-211701-001 BOGIE ASSEMBLY B RF
s & -M
SEE CMM 32-12-63 FOR NHA
rm 12
(POST SB A33/34-32-283,
PRE SB A33/34-32-304)
Te n
S so
– 001B 10-211701-002 BOGIE ASSEMBLY C RF
SEE CMM 32-12-63 FOR NHA
SL de
(POST SB A33/34-32-304,
er an
PRE SB A33/34-32-305)
nd ern
– 001C 10-211701-003 BOGIE ASSEMBLY D RF
SEE CMM 32-12-63 FOR NHA
lu F
(POST SB A33/34-32-305,
ga pes
PRE SB A33/34-32-315)
or Lo
– 001D 10-211701-004 BOGIE ASSEMBLY E RF
SEE CMM 32-12-63 FOR NHA
r P la
(POST SB A33/34-32-315)
tu
Ai au
– 010 30-2117007-00 . TOWING BRACKET 1
P :P
SUBASSEMBLY
TA by
ATTACHING PARTS
of ded
020 MS24665-153 . PIN, SPLIT 1
us nloa
030 MS17825-3 . NUT 1
040 NAS1149F0363P . WASHER 2
siv ow
e
clu - D
050 NAS6603D27 . BOLT 1
e
060 201272621 . NUT 1
ex tial
***
n
ide
070 55-2117009-00 . DOME, JACKING 1
nf
– 080 MS21209F4-15P *** DELETED *** -
Co
– 090 55-2117009-00 *** DELETED *** -
100 65-2117017-00 . . BUSH 4
110 201485608 . . BUSH 2
– ITEM NOT ILLUSTRATED
32-12-64 Page 10017
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
e
STOCK 1234567 CODE PER
th
NUMBER ASSY
ns for
2 120 55-2117007-00 . . BRACKET, TOWING 1
itio 0
nd 202
130 NAS6604H2 . BOLT 2
Co ay-
140 NAS1149F0432P . WASHER 2
s & -M
150 201272619 . SEGMENT, LOCKING 1
rm 12
160 201272606 . SPIGOT 1
Te n
170 201272609 . NUT, AXLE SPIGOT 1
S so
180 55-2117012-00 . DIAPHRAGM 1
SL de
er an
190 30-2117004-00 . BEAM AND AXLE SUBASSEMBLY, A 1
BOGIE
nd ern
SEE FIGURE 3 FOR DET
(PRE SB A33/34-32-283,
lu F
PRE SB A33/34-32-304,
ga pes
PRE SB A33/34-32-305,
PRE SB A33/34-32-315)
or Lo
– 190A 30-2117004-01 . BEAM AND AXLE SUBASSEMBLY, B 1
r P la
BOGIE
tu
Ai au
SEE FIGURE 3 FOR DET
(POST SB A33/34-32-283,
P :P
PRE SB A33/34-32-304,
TA by
PRE SB A33/34-32-305,
PRE SB A33/34-32-315)
of ded
– 190B 30-2117034-00 . BEAM AND AXLE SUBASSEMBLY, C 1
us nloa
BOGIE
SEE FIGURE 3 FOR DET
(POST SB A33/34-32-304,
siv ow
e
PRE SB A33/34-32-305,
clu - D
PRE SB A33/34-32-315)
e
– 190C 30-2117034-01 . BEAM AND AXLE SUBASSEMBLY, D 1
ex tial
BOGIE
n
SEE FIGURE 3 FOR DET
ide
(POST SB A33/34-32-305,
PRE SB A33/34-32-315)
nf
Co
– 190D 30-2117004-02 . BEAM AND AXLE SUBASSEMBLY, D 1
BOGIE
SEE FIGURE 3 FOR DET
(POST SB A33/34-32-305,
PRE SB A33/34-32-315)
– ITEM NOT ILLUSTRATED
32-12-64 Page 10018
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
e
STOCK 1234567 CODE PER
th
NUMBER ASSY
ns for
2 – 190E 30-2117038-00 . BEAM AND AXLE SUBASSEMBLY, A 1
itio 0
BOGIE
nd 202
SEE FIGURE 3 FOR DET
(POST SB A33/34-32-315)
Co ay-
– 190F 30-2117038-01 . BEAM AND AXLE SUBASSEMBLY, B 1
s & -M
BOGIE
SEE FIGURE 3 FOR DET
rm 12
(POST SB A33/34-32-315)
Te n
S so
– 190G 30-2117040-00 . BEAM AND AXLE SUBASSEMBLY, C 1
BOGIE
SL de
SEE FIGURE 3 FOR DET
(POST SB A33/34-32-315)
er an
– 190H 30-2117034-02
nd ern. BEAM AND AXLE SUBASSEMBLY, E 1
BOGIE
lu F
SEE FIGURE 3 FOR DET
ga pes
(POST SB A33/34-32-315)
– 190I 30-2117038-02 . BEAM AND AXLE SUBASSEMBLY, E 1
or Lo
BOGIE
r P la
SEE FIGURE 3 FOR DET
tu
Ai au
(POST SB A33/34-32-315)
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
– ITEM NOT ILLUSTRATED
32-12-64 Page 10019
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
th
ns for
itio 0
nd 202
Co ay-
s & -M
rm 12
Te n
S so
SL de
er an
nd ern
lu F
ga pes
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
Bogie Beam and Axle Subassembly
Figure 3/GRAPHIC 32-12-64-991-903-A01
32-12-64 Page 10020
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
e
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
th
STOCK 1234567 CODE PER
ns for
NUMBER ASSY
itio 0
3 – 001 30-2117004-00 BEAM AND AXLE SUBASSEMBLY, A RF
nd 202
BOGIE
SEE FIGURE 2 FOR NHA
Co ay-
(PRE SB A33/34-32-283,
PRE SB A33/34-32-304,
s & -M
PRE SB A33/34-32-305,
rm 12
PRE SB A33/34-32-315)
Te n
– 001A 30-2117004-01 BEAM AND AXLE SUBASSEMBLY, B RF
S so
BOGIE
SEE FIGURE 2 FOR NHA
SL de
(POST SB A33/34-32-283,
er an
PRE SB A33/34-32-304,
nd ern PRE SB A33/34-32-305,
PRE SB A33/34-32-315)
lu F
– 001B 30-2117034-00 BEAM AND AXLE SUBASSEMBLY, C RF
ga pes
BOGIE
SEE FIGURE 2 FOR NHA
or Lo
(POST SB A33/34-32-304,
PRE SB A33/34-32-305,
r P la
PRE SB A33/34-32-315)
tu
Ai au
– 001C 30-2117034-01 BEAM AND AXLE SUBASSEMBLY, D RF
P :P
BOGIE
TA by
SEE FIGURE 2 FOR NHA
(POST SB A33/34-32-305,
of ded
PRE SB A33/34-32-315)
us nloa
– 001D 30-2117004-02 BEAM AND AXLE SUBASSEMBLY, E RF
BOGIE
SEE FIGURE 2 FOR NHA
siv ow
e
(POST SB A33/34-32-305,
clu - D
PRE SB A33/34-32-315)
e
– 001E 30-2117038-00 BEAM AND AXLE SUBASSEMBLY, F RF
ex tial
BOGIE
n
SEE FIGURE 2 FOR NHA
ide
(POST SB A33/34-32-315)
nf
– 001F 30-2117038-01 BEAM AND AXLE SUBASSEMBLY, G RF
Co
BOGIE
SEE FIGURE 2 FOR NHA
(POST SB A33/34-32-315)
– ITEM NOT ILLUSTRATED
32-12-64 Page 10021
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
e
STOCK 1234567 CODE PER
th
NUMBER ASSY
ns for
3 – 001G 30-2117040-00 BEAM AND AXLE SUBASSEMBLY, H RF
itio 0
BOGIE
nd 202
SEE FIGURE 2 FOR NHA
(POST SB A33/34-32-315)
Co ay-
– 001H 30-2117034-02 BEAM AND AXLE SUBASSEMBLY, I RF
s & -M
BOGIE
SEE FIGURE 2 FOR NHA
rm 12
(POST SB A33/34-32-315)
Te n
S so
– 001I 30-2117038-02 BEAM AND AXLE SUBASSEMBLY, J RF
BOGIE
SL de
SEE FIGURE 2 FOR NHA
(POST SB A33/34-32-315)
er an
010 55-2117005-00
nd ern
. SPACER, AXLE 4
lu F
020 55-2117003-00 . AXLE 2
ga pes
– 030 30-2117002-00 . BEAM SUBASSEMBLY, BOGIE A 1
(PRE SB A33/34-32-283,
or Lo
PRE SB A33/34-32-304,
PRE SB A33/34-32-305,
r P la
tu
PRE SB A33/34-32-315)
Ai au
P :P
– 030A 30-2117002-01 . BEAM SUBASSEMBLY, BOGIE B 1
(POST SB A33/34-32-283,
TA by
PRE SB A33/34-32-304,
PRE SB A33/34-32-305,
of ded
PRE SB A33/34-32-315)
us nloa
– 030B 30-2117032-00 . BEAM SUBASSEMBLY, BOGIE C 1
(POST SB A33/34-32-304,
siv ow
PRE SB A33/34-32-305,
e
PRE SB A33/34-32-315)
clu - D
e
– 030C 30-2117032-01 . BEAM SUBASSEMBLY, BOGIE D 1
ex tial
(POST SB A33/34-32-305,
PRE SB A33/34-32-315)
n
ide
– 030D 30-2117002-02 . BEAM SUBASSEMBLY, BOGIE E 1
(POST SB A33/34-32-305,
nf
PRE SB A33/34-32-315)
Co
– 030E 30-2117037-00 . BEAM SUBASSEMBLY, BOGIE F 1
(POST SB A33/34-32-315)
– 030F 30-2117037-01 . BEAM SUBASSEMBLY, BOGIE G 1
(POST SB A33/34-32-315)
– ITEM NOT ILLUSTRATED
32-12-64 Page 10022
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
e
STOCK 1234567 CODE PER
th
NUMBER ASSY
ns for
3 – 030G 30-2117039-00 . BEAM SUBASSEMBLY, BOGIE H 1
itio 0
(POST SB A33/34-32-315)
nd 202
– 030H 30-2117032-02 . BEAM SUBASSEMBLY, BOGIE I 1
Co ay-
(POST SB A33/34-32-315)
s & -M
– 030I 30-2117037-02 . BEAM SUBASSEMBLY, BOGIE J 1
(POST SB A33/34-32-315)
rm 12
040 55-2117010-00 . . DOWEL 2
Te n
S so
050 65-2117015-00 . . BUSH 1
SL de
060 55-1217005-00 . . BUSH 1
er an
070 65-2117013-00 . . BUSH
nd ern 1
080 65-2117016-00 . . BUSH 2
lu F
ga pes
090 55-2117021-00 . . WASHER, SADDLE 1
or Lo
100 65-2117006-00 . . BUSH 2
r P la
110 65-2117006-00 . . BUSH 2
tu
Ai au
120 201272625 . . BUSH 2
P :P
130 65-2117016-00 . . BUSH 2
TA by
140 55-2117021-00 . . WASHER, SADDLE 1
of ded
150 65-2117011-00 . . BUSH A to E 2
us nloa
(PRE SB A33/34-32-315)
– 150A 65-2117035-00 . . BUSH F to J 2
siv ow
e
(POST SB A33/34-32-315)
clu - D
160 MS15001-4 . . FITTING, LUBRICATION 2
e
ex tial
– 160A AS15001-4P . . FITTING, LUBRICATION 2
(ALTERNATIVE TO ITEM 160)
n
ide
– 160B AS15001-4C . . FITTING, LUBRICATION 2
nf
(ALTERNATIVE TO ITEMS 160
Co
AND 160A)
170 899005010 . . ADAPTER, LUBRICATION 2
180 P332602 . . WASHER 2
– ITEM NOT ILLUSTRATED
32-12-64 Page 10023
Sep 21/18
SAFRAN LANDING SYSTEMS UK Ltd
CAGE: K0654
10-211701 SERIES COMPONENT MAINTENANCE MANUAL
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
e
STOCK 1234567 CODE PER
th
NUMBER ASSY
ns for
3 190 50-2117002-00 . . BEAM, BOGIE A, F 1
itio 0
(PRE SB A33/34-32-283,
nd 202
PRE SB A33/34-32-304,
PRE SB A33/34-32-305)
Co ay-
– 190A 50-2117002-01 . . BEAM, BOGIE B, G 1
s & -M
(POST SB A33/34-32-283,
PRE SB A33/34-32-304,
rm 12
PRE SB A33/34-32-305)
Te n
S so
– 190B 50-2117032-00 . . BEAM, BOGIE C, H 1
(POST SB A33/34-32-304,
SL de
PRE SB A33/34-32-305)
er an
– 190C 50-2117032-01 . . BEAM, BOGIE
nd ern D, I 1
(POST SB A33/34-32-305)
lu F
– 190D 50-2117002-02 . . BEAM, BOGIE E, J 1
ga pes
(POST SB A33/34-32-305)
or Lo
r P la
tu
Ai au
P :P
TA by
of ded
us nloa
siv ow
e
clu - D
e
ex tial
n
ide
nf
Co
– ITEM NOT ILLUSTRATED
32-12-64 Page 10024
Sep 21/18
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