ANCRA INTERNATIONAL LLC

CAGE Code 31272

601 SOUTH VINCENT AVE. • AZUSA • CALIFORNIA 91702 • USA
www.ancra.com

TO: HOLDERS OF COMPONENT MAINTENANCE MANUAL 25-52-16,

PART NUMBER 85550

This letter transmits Revision 4, dated Apr 1/21, to Component Maintenance Manual 25-52-16.
Replace revised pages and add and remove the pages as shown below.

REVISED PAGES DATED

T-1, ROR-1, RTR-1, SBL-1, LEP-1 thru -3, TOC-1 thru -3, Apr 1/21
INTRO-1, -2, 3001 thru 3010, 6001 thru 6007, 7001 thru 7014,
9001, 9002, 10007 thru 10026, 10095 thru 10108

ADD PAGES DATED

Not Applicable

REMOVE PAGES DATED

H-2 Apr 1/21

25-52-16
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PART NUMBER 85550

REVISION NO. 4 DATED APR 1/21

HIGHLIGHTS
Pages which have been revised, added, or removed are shown below with the reasons for the
changes. Add or remove these pages and record the revision number and the date on the Record
of Revisions page.

PAGE DESCRIPTION OF CHANGE

T- 1 Changed date
ROR-1 Added new Revision No. 4 and changed date
RTR-1, SBL-1 Changed date
LEP-1 thru -3 Changed date on affected pages
TOC-1 thru -3, INTRO-1, -2 Changed date
3001 thru 3010 Changed date in block of pages
3007 Revised item number in paragraph 12.C.
6001 thru 6007 Changed date in block of pages
6002 Revised P/N in CMM Table 6002
6005 Revised P/N in CMM Figure 6001
7001 thru 7014 Changed date in block of pages
7011 Revised item number in paragraph 12.Y.
9001, 9002 Changed date, revised P/N in CMM Table 9002 on page 9002
10007 thru 10026 Changed date in block of pages, revised P/Ns on page 10012
10095 thru 10108 Changed date in IPL Figure 13
10098 Revised item number in illustration
10105 Deleted item number -130. Added item number 130A.

25-52-16
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601 SOUTH VINCENT AVE. • AZUSA • CALIFORNIA 91702 • USA
www.ancra.com

COMPONENT MAINTENANCE MANUAL

WITH
ILLUSTRATED PARTS LIST

A321-200 CARGO HANDLING SYSTEM

PART NUMBERS
85550-10
85550-12

CONVERSION KIT
PART NUMBER
85550-90

Ancra International LLC proprietary rights are included in the information disclosed herein.
By accepting this document the recipient agrees that neither this document nor information
disclosed herein nor any part thereof shall be reproduced or transferred to other docu-
ments or used or disclosed to others for manufacturing, technical or for any other purpose
except as specifically authorized in writing by Ancra International LLC. Unpublished – all
rights reserved under copyright laws. © 2018, 2019, 2021 Ancra International LLC

Trademarks and trade names may be used in this document to refer to either the entities
claiming the marks and names as their own or their products. Ancra International LLC dis-
claims any proprietary interest in trademarks and trade names other than its own.

The technical data in this document (or file) is controlled for export under the Export
Administration Regulations (EAR), 15 CFR Parts 730-774, ECCN: 9E991. Violations of
these laws may be subject to fines and penalties under the Export Administration Act.

25-52-16
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RECORD OF REVISIONS
REVISION ISSUE DATE BY REVISION ISSUE DATE BY
NUMBER DATE INSERTED NUMBER DATE INSERTED

1 Dec 1/18 BK
2 Sep 1/19 BK
3 Jan 1/21 BK
4 Apr 1/21 BK

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RECORD OF TEMPORARY REVISIONS

TEMPORARY ISSUE DATE DATE DATE DATE
REVISION INSERTED/ REMOVED/ INCORPORATED
NUMBER INSERTED BY REMOVED BY

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SERVICE BULLETIN LIST

SERVICE BULLETIN/ ISSUE DATE DATE TITLE
REVISION NUMBER INCORPORATED
OR NO EFFECT

SB 85550-25-01 R00 Sep 1/19 No effect Reconfig. of CHS P/N 85550-10 to -12

SB 85550-25-02 R00 Dec 23/20 Jan 1/21 Modification of CHS P/N 85550-10, -12

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LIST OF EFFECTIVE PAGES

SUBJECT PAGE DATE SUBJECT PAGE DATE SUBJECT PAGE DATE

Title Page T-1 Apr 1/21 Repair 6005 Apr 1/21

(cont)
Rec of Rev ROR-1 Apr 1/21 Disassy 3001 Apr 1/21 6006 Apr 1/21

Temp Rev RTR-1 Apr 1/21 3002 Apr 1/21 6007 Apr 1/21

SB List SBL-1 Apr 1/21 3003 Apr 1/21

Eff.Pages LEP-1 Apr 1/21 3004 Apr 1/21 Assy 7001 Apr 1/21

LEP-2 Apr 1/21 3005 Apr 1/21 7002 Apr 1/21

LEP-3 Apr 1/21 3006 Apr 1/21 7003 Apr 1/21

3007 Apr 1/21 7004 Apr 1/21

Table Cont TOC-1 Apr 1/21 3008 Apr 1/21 7005 Apr 1/21

TOC-2 Apr 1/21 3009 Apr 1/21 7006 Apr 1/21

TOC-3 Apr 1/21 3010 Apr 1/21 7007 Apr 1/21

7008 Apr 1/21

Intro INTRO-1 Apr 1/21 7009 Apr 1/21

INTRO-2 Apr 1/21 7010 Apr 1/21

Cleaning 4001 Jan 1/21 7011 Apr 1/21

Des & Op 1001 Jan 1/21 4002 Jan 1/21 7012 Apr 1/21

1002 Jan 1/21 7013 Apr 1/21

1003 Jan 1/21 Check 5001 Jan 1/21 7014 Apr 1/21

1004 Jan 1/21 5002 Jan 1/21

1005 Jan 1/21 5003 Jan 1/21

1006 Jan 1/21 5004 Jan 1/21 Tools 9001 Apr 1/21

1007 Jan 1/21 5005 Jan 1/21 9002 Apr 1/21

1008 Jan 1/21 5006 Jan 1/21

1009 Jan 1/21 5007 Jan 1/21 IPL intro 10001 Sep 1/19

1010 Jan 1/21 5008 Jan 1/21 10002 Sep 1/19

1011 Jan 1/21 10003 Sep 1/19

1012 Jan 1/21 Repair 6001 Apr 1/21 10004 Sep 1/19

1013 Jan 1/21 6002 Apr 1/21 10005 Sep 1/19

6003 Apr 1/21 10006 Sep 1/19

6004 Apr 1/21

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SUBJECT PAGE DATE SUBJECT PAGE DATE SUBJECT PAGE DATE

Index 10007 Apr 1/21 IPL 10038 Jan 1/21 IPL 10069 Sep 1/19
(cont) (cont)
10008 Apr 1/21 10039 Jan 1/21 10070 Sep 1/19

10009 Apr 1/21 10040 Jan 1/21 10071 Sep 1/19

10010 Apr 1/21 10041 Jan 1/21 10072 Sep 1/19

10011 Apr 1/21 10042 Jan 1/21 10073 Sep 1/19

10012 Apr 1/21 10043 Jan 1/21 10074 Sep 1/19

10013 Apr 1/21 10044 Jan 1/21 10075 Sep 1/19

10014 Apr 1/21 10045 Jan 1/21 10076 Sep 1/19

10015 Apr 1/21 10046 Jan 1/21 10077 Sep 1/19

10016 Apr 1/21 10047 Sep 1/19 10078 Sep 1/19

10017 Apr 1/21 10048 Sep 1/19 10079 Sep 1/19

10018 Apr 1/21 10049 Sep 1/19 10080 Sep 1/19

10019 Apr 1/21 10050 Sep 1/19 10081 Jan 1/21

10020 Apr 1/21 10051 Sep 1/19 10082 Jan 1/21

10021 Apr 1/21 10052 Sep 1/19 10083 Jan 1/21

10022 Apr 1/21 10053 Sep 1/19 10084 Jan 1/21

10023 Apr 1/21 10054 Sep 1/19 10085 Jan 1/21

10024 Apr 1/21 10055 Sep 1/19 10086 Jan 1/21

10025 Apr 1/21 10056 Sep 1/19 10087 Jan 1/21

10026 Apr 1/21 10057 Sep 1/19 10088 Jan 1/21

IPL 10027 Jan 1/21 10058 Sep 1/19 10089 Jan 1/21

10028 Jan 1/21 10059 Sep 1/19 10090 Jan 1/21

10029 Jan 1/21 10060 Sep 1/19 10091 Sep 1/19

10030 Jan 1/21 10061 Sep 1/19 10092 Sep 1/19

10031 Jan 1/21 10062 Sep 1/19 10093 Sep 1/19

10032 Jan 1/21 10063 Sep 1/19 10094 Sep 1/19

10033 Jan 1/21 10064 Sep 1/19 10095 Apr 1/21

10034 Jan 1/21 10065 Sep 1/19 10096 Apr 1/21

10035 Jan 1/21 10066 Sep 1/19 10097 Apr 1/21

10036 Jan 1/21 10067 Sep 1/19 10098 Apr 1/21

10037 Jan 1/21 10068 Sep 1/19 10099 Apr 1/21

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SUBJECT PAGE DATE SUBJECT PAGE DATE SUBJECT PAGE DATE

IPL 10100 Apr 1/21

(cont)
10101 Apr 1/21

10102 Apr 1/21

10103 Apr 1/21

10104 Apr 1/21

10105 Apr 1/21

10106 Apr 1/21

10107 Apr 1/21

10108 Apr 1/21

10109 Sep 1/19

10110 Sep 1/19

10111 Sep 1/19

10112 Sep 1/19

10113 Sep 1/19

10114 Sep 1/19

10115 Sep 1/19

10116 Sep 1/19

10117 Sep 1/19

10118 Sep 1/19

10119 Jan 1/21

10120 Jan 1/21

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TABLE OF CONTENTS
SECTION/PARAGRAPH PAGE

Introduction............................................................................................................ Intro-1

Description and Operation

1. General...............................................................................................................1001
2. ULD Loading Arrangements ...............................................................................1002
3. Operation of the CHS components.....................................................................1003
4. Components Installation .....................................................................................1013

Testing and Fault Isolation .......................................................................Not Applicable

Schematics and Wiring Diagrams............................................................Not Applicable

Disassembly

1. General...............................................................................................................3001
2. Disassembly of the Cargo Lock Assy P/N 80004 ...............................................3001
3. Disassembly of the End Stop Assy P/N 80576...................................................3002
4. Disassembly of the Roller Rail Assy P/N 81384.................................................3002
5. Disassembly of the Side Guide Rails P/N 84021 ...............................................3003
6. Disassembly of the Increased Height Side Guide Rails P/N 84022 ...................3003
7. Disassembly of the Articulating Side Guide Rails P/N 84764.............................3003
8. Disassembly of the Increased Height Side Guide Rails P/N 86872 ...................3004
9. Disassembly of the Ball Mats P/N 86963 ...........................................................3004
10. Disassembly of the Crosstracks P/N 86974 .......................................................3005
11. Disassembly of the Crosstracks P/N 86976 .......................................................3006
12. Disassembly of the Door Sill Protector P/N 86980 .............................................3007
13. Disassembly of the Lateral Guides P/N 87008...................................................3008
14. Disassembly of the Crosstracks P/N 87226 .......................................................3010

Cleaning

1. General...............................................................................................................4001
2. Materials .............................................................................................................4001
3. Procedures .........................................................................................................4002

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SECTION/PARAGRAPH PAGE

Check

1. General...............................................................................................................5001
2. System Operational Check.................................................................................5002
3. Overhaul Inspection and Maintenance Schedule ...............................................5003
4. Component Operational Check ..........................................................................5005
5. Component Damage Limits Reference Guide....................................................5006

Repair

1. General...............................................................................................................6001
2. Content ...............................................................................................................6001
3. Materials .............................................................................................................6002
4. Tools, Fixtures, and Equipment..........................................................................6003
5. Repair of Small Surface Imperfections - REPAIR 1-1 ........................................6003
6. Restore the Anti-Skid Paint - REPAIR 2-1..........................................................6003
7. Repair of the Edge Pail - REPAIR 3-1................................................................6005
8. Repair of the Panel Skin - REPAIR 4-1 ..............................................................6006
9. Replacement of the Nameplate - REPAIR 5-1 ...................................................6007

Assembly

1. General...............................................................................................................7001
2. Assembly of the Cargo Lock Assy P/N 80004....................................................7002
3. Assembly of the End Stop Assy P/N 80576 .......................................................7004
4. Assembly of the Roller Rail Assy P/N 81384......................................................7004
5. Assembly of the Side Guide Rails P/N 84021 ....................................................7004
6. Assembly of the Increased Height Side Guide Rails P/N 84022 ........................7005
7. Assembly of the Articulating Side Guide Rails P/N 84764 .................................7005
8. Assembly of the Increased Height Side Guide Rails P/N 86872 ........................7006
9. Assembly of the Ball Mats P/N 86963 ................................................................7006
10. Assembly of the Crosstracks P/N 86974 ............................................................7007
11. Assembly of the Crosstracks P/N 86976 ............................................................7008
12. Assembly of the Door Sill Protectors P/N 86980 ................................................7009
13. Assembly of the Lateral Guides P/N 87008........................................................7011
14. Assembly of the Crosstracks P/N 87226 ............................................................7013

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SECTION/PARAGRAPH PAGE

Fits and Clearances...................................................................................Not Applicable

Special Tools, Fixtures, and Equipment

1. Special Tools, Fixtures, and Equipment .............................................................9001

2. Materials .............................................................................................................9001

Illustrated Parts List

1. Introduction.......................................................................................................10001
2. Numerical Index ...............................................................................................10007
3. Illustrated Parts List ..........................................................................................10027

FIGURE TITLE PAGE

1. A321-200 Cargo Handling System, P/N 85550-10...........................................10027

1A. A321-200 Cargo Handling System, P/N 85550-12...........................................10037
2. Wall Placard Instl, P/N 85338-10 .....................................................................10047
2A. Wall Placard Instl, P/N 85338-12 .....................................................................10050
3. Cargo Lock Assy, P/N 80004-10, -11, and - 43................................................10054
4. End Stop Assy, P/N 80576-10..........................................................................10056
5. Roller Rail Assy, P/N 81384-10, -12 thru -15, and -18 .....................................10058
6. Side Guide Rail Assy, P/N 84021-40, -41, -45, -50, -51,
-52, -54, -59, -60, -61, -75, -78 .........................................................................10061
7. Increased Height Side Guide Rail Assy, P/N 84022-47 and -49 ......................10065
8. Articulating Side Guide Rail Assy, P/N 84764-16 and -18 ...............................10067
9. Increased Height Side Guide Rail Assy, P/N 86872-11, -14, -19, -20..............10069
10. Ball Mat Assy, P/N 86963-10 thru -19 ..............................................................10071
11. Crosstrack Assy, P/N 86974-10 thru -13, -16 thru -18, -22, -23, -28................10081
12. Crosstrack Assy, P/N 86976-10 and -11 ..........................................................10091
13. Door Sill Protector Assy, P/N 86980-10 and -11 ..............................................10095
14. Lateral Guide Assy, P/N 87008-10 and -11......................................................10109
15. Crosstrack Assy, P/N 87226-10 .......................................................................10116
16. Conversion Kit, P/N 85550-90..........................................................................10119

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 COMPONENT MAINTENANCE MANUAL
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INTRODUCTION
This manual supplies data and instructions to do maintenance, tests, and repairs on the
component in the shop. The data and procedures are necessary to make sure that the
component operates satisfactorily when returned to service. This manual will be revised as
necessary to include current information. It contains:

- Technical data for the component

- Maintenance and repair procedures for the component
- An Illustrated Parts List (IPL)

Refer to the Table of Contents to find page numbers for each section.

The IPL figure and item number are used to identify parts in all sections of the manual. The
introduction to the IPL tells how to use the IPL.

All weights and measurements in the manual are in English units with metric equivalents in
parenthesis, unless stated differently.

This is a list of abbreviations and acronyms used in the manual:

AFT Rearward

AR As Required

ASSY Assembly

ATA Air Transport Association of America

CHS Cargo Handling System
CCW Counterclockwise
CMM Component Maintenance Manual
CW Clockwise
FH Flight Hours
FIG Figure
FWD Forward
INBRD Inboard

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IPL Illustrated Parts List

LEP List of Effective Pages
LH Left Hand
LOT Letter of Transmittal
LRU Line Replaceable Unit
MSDS Material Safety Data Sheets
NHA Next Higher Assembly
NO. Number
NSN National Stock Number
OUTBRD Outboard
PL Places
P/N Part Number
RH Right Hand
ROR Record of Revisions
RTR Record of Temporary Revisions
SB Service Bulletin
SBL Service Bulletin List
TOC Table of Contents
ULD Unit Load Device

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DESCRIPTION AND OPERATION

1. General
A. Ancra Cargo Handling Systems (CHS) P/N 85550-10 and -12 are designed
for installation on the main deck of A321-200 aircraft.

B. The CHS allows you to move Unit Load Devices (ULDs) on the aircraft main
cargo deck and lock them in positions.

C. Most of the components of the CHS are secured to the aircraft seat tracks
with studs, retainers, washers, and nuts. Some components are secured with
quick release fasteners.

D. The conveyor plain is approximately 1.25 in. (3.2 cm) high from the aircraft
seat tracks.

E. The CHS is manually operated.

F. To convert CHS P/N 85550-10 to P/N 85550-12 obtain the following:

(1) Ancra SB 85550-25-01

(2) One Conversion Kit P/N 85550-90

(3) Conversion Drawing 85501

G. The total weight of the CHS is approximately:

(1) P/N 85550-10..........1884 lb (854.6 kg).

(2) P/N 85550-12..........1935 lb (877.7 kg).

H. See Ancra Report 10551, Rev. C, dated Jan. 1, 2021, for Instructions For
Continued Airworthiness.

I. Refer to the Illustrated Parts List (IPL) Figures 1 and 1A to identify compo-
nents of the CHS and their arrangement in the aircraft.

J. This manual gives Ancra International’s procedures for Ancra components

only. You must refer to the Owner/Operator’s manuals for data that applies to
your aircraft.

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2. ULD Loading Arrangements

NOTE: Pallets and containers are a subset of the general term, Unit Load Device
(ULD).

A. CMM Figure 1001 shows examples of the ULD loading arrangements.

CMM Figure 1001 - Examples of the ULD Loading Arrangements

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3. Operation of the CHS components

A. Obey the safety precautions given below. The safety precautions will
decrease the risk of injury and damage.

WARNING
Risk of Injury
ULDS CAN MOVE WITHOUT WARNING
OBEY OPERATOR’S SAFETY PROCEDURES

WARNING
Risk of Injury
CAREFULLY MOVE PAWLS.
PAWLS ARE SPRING-LOADED.

WARNING
Risk of Injury
DO NOT STEP OR STAND
ON BALL UNITS.

CAUTION
Risk of Aircraft Damage
LOCK ALL ULDS TO COMPONENTS
BEFORE AIRCRAFT MOVES

CAUTION
Risk of Aircraft Damage
DO NOT USE LOCK PAWLS AS STOPS OR
BUMPERS FOR TURNING ULDS

CAUTION
Risk of Damage to Cargo
BEFORE LIFTING SILL PROTECTORS
LOCK DOWN ITS PAWLS AND SIDE GUIDES

B. If the component does not operate correctly, do the Component Operational

Check. Refer to the CHECK section of this manual.

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C. Operation of the Cargo Locks

(1) CMM Figure 1002 shows examples of the components. Refer to IPL
Figure 3 for details.

CMM Figure 1002 - Examples of the Cargo Locks

(2) The Cargo Locks lock ULDs to the aircraft floor.

(3) Operation of the pawls:

(a) Move the pawls to the UP position: Carefully lift the outer pawl.
The pawls move quickly to the UP position.

(b) Move the pawls to the DOWN position: Carefully push DOWN
the inner pawl. The pawls move quickly to the DOWN position.

(4) Some of the Cargo Locks have rollers. Move the rollers FWD and AFT:
The rollers turn quickly in both directions.

(5) Operation of the shear studs:

(a) Move the shear studs to the UP position: Turn the knob CCW.
The shear stud moves UP into the base. The bottom of the
shear stud will be flush with bottom of the base.

(b) Move the shear studs to the DOWN position: Push DOWN and
turn the knob CW. The shear stud will move DOWN below the
base.

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D. Operation of the End Stops

(1) CMM Figure 1003 shows examples of the components. Refer to IPL
Figure 4 for details.

CMM Figure 1003 - Example of the End Stop

(2) The End Stops help to restrain ULDs at the FWD and AFT of the air-
craft cargo cabin.

(3) The End Stops are equipped with a polyurethane bumper to help
absorb impact of the ULD.

(4) To install the End Stop in the seat track, release the bolt, tilt the left
and right castings and insert the bottom flanges into the seat track.
Then turn the castings together and reattach the fasteners. Torque the
fasteners 30 to 40 in. lb (3.4 to 4.7 N m).

E. Operation of the Crosstracks

(1) CMM Figure 1004 shows examples of the components. Refer to IPL
Figures 11, 12, and 15 for details.

CMM Figure 1004 - Examples of the Crosstracks

(2) The Crosstracks help to move, align, and restrain ULDs on the aircraft
floor.

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(3) P/N 86974 ONLY: Operation of the vertical restraint (flipper). Push the
flipper to the LH and RH sides: The flipper automatically returns to the
center position.

(4) P/N 86976-10 ONLY. Operation of the folding pawl:

(a) Move the folding pawl UP: Lift UP the folding pawl. The folding
pawl locks in the UP position.

(b) Move the folding pawl DOWN: The folding pawl is spring-loaded
to the DOWN position. Push DOWN the lever with serrations.
The folding pawl moves quickly to the DOWN position.

(5) P/N 86974-16 thru -18, -28 ONLY. Operation of the overrideable pawl:

(a) Move the overrideable pawl DOWN: Push DOWN the override-
able pawl. The pawl folds in the crosstrack.

(b) Move the overrideable pawl UP: The overrideable pawl is

spring-loaded to the UP position. Release the pawl. The pawl
moves quickly to the UP position.

(6) P/N 86974-16, -17 ONLY. Locking the overrideable pawl:

(a) Lock the overrideable pawl DOWN: Push DOWN the override-
able pawl. Slide the red release plunger to block the override-
able pawl. The pawl rests on the crosstrack.

(b) Unlock the overrideable pawl to the UP position: Pull on the red
release plunger. The pawl moves quickly UP.

(7) Many of the components have rollers. Move the rollers FWD and AFT:
The rollers turn quickly in both directions.

F. Operation of the Side Guide Rails

(1) CMM Figure 1005 shows examples of the components. Refer to IPL
Figures 6, 7, 8, and 9 for details.

CMM Figure 1005 - Examples of the Side Guide Rails

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(2) The Side Guide Rails help to guide ULDs along the cargo cabin.

(3) Most of the components have rollers. Move the rollers FWD and AFT:
The rollers turn quickly in both directions.

G. Operation of the Roller Rails

(1) CMM Figure 1006 shows examples of the components. Refer to IPL
Figure 5 for details.

CMM Figure 1006 - Examples of the Roller Rails

(2) The Roller Rails help to move ULDs on the aircraft floor.

(3) Rollers. Move the rollers FWD and AFT: The rollers turn quickly in both
directions.

(4) To install the Roller Rail in the seat track, release the fasteners and
remove the retainers. Tilt the Roller Rail and the retainer and insert the
bottom flanges into the seat track. Then turn the Roller Rail and the
retainer together and reattach the fasteners. Torque the fasteners 30
to 40 in. lb (3.4 to 4.7 N m).

H. Operation of the Ball Mats

(1) CMM Figure 1007 shows examples of the components. Refer to IPL
Figure 10 for details.

CMM Figure 1007 - Examples of the Ball Mats

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(2) The Ball Mats help to move and turn ULDs at the aircraft cargo door
zone.

(3) Ball Units. Turn the balls in all directions: The balls turn quickly in all
directions.

(4) Some of the Ball Mats have ramp rails. The ramp rail helps to move
ULDs on and off the Ball Mat.

(5) The Ball Mats are painted with green primer. The top has a layer of
non-skid walkway coating. The walkway coating looks and feels like
sandpaper.

J. Operation of the Lateral Guides

(1) CMM Figure 1008 shows an example of the components. Refer to IPL
Figure 14 for details.

CMM Figure 1008 - Example of the Lateral Guides

(2) The Lateral Guides help to guide ULDs at the FWD of the ball mats
area.

(3) Operation of the frame:

(a) Turn the frame DOWN with your hand until it is locks in DOWN
position below conveyor plane.

(b) Turn the frame UP: Push the release handle. The frame is
spring-loaded to the UP position. The frame turns quickly to the
UP position.

(4) Ball Units. Turn the balls in all directions: The balls turn quickly in all
directions.

(5) Rollers. Move the rollers INBRD and OUTBRD: The rollers turn quickly
in both directions.

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K. Operation of the Door Sills

(1) CMM Figure 1009 shows examples of components. Refer to IPL Fig-
ure 13 for details.

CMM Figure 1009 - Examples of the Door Sills

(2) The Door Sills are designed to protect the aircraft door area and guide
the ULDs through the aircraft cargo door.

(3) The Door Sills are in the DOWN position during ground handling oper-
ations and UP while in flight.

(a) Fold the Door Sills in the UP position. Carefully push UP on the
assembly. The Door Sills are equipped with gas springs to
ensure easy retraction.

(b) Lower the Door Sills to the DOWN position. Carefully push
DOWN on the assembly until it is parallel to the aircraft floor. Do
not let the Door Sill free-fall on door spools.

(4) The side guides provide guidance for ULDs during load and unload
and help to protect aircraft door area from damage.

(a) Fold the side guides to the DOWN position. Push the red
release lock: The side guide moves quickly to the DOWN posi-
tion.

(b) Unfold the side guide to the UP position. Pull the side guide UP:
The Side Guide locks in the UP position.

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(5) The roll back stops help to prevent ULDs from accidentally rolling back
from the aircraft. The roll back stops are spring loaded to the UP posi-
tion and are designed to automatically spring to the UP position after
the ULD passes over it. The roll back stops have a lockdown feature.

(a) Lock the roll back stop to the DOWN position. Push DOWN the
roll back stop and slide the latch to block it. The stop locks in
the DOWN position.

(b) Unlock the roll back stop to the UP position. Slide the latch out.
The roll back stop moves quickly to the UP position.

(6) Rollers: Move the rollers in both directions. The rollers turn quickly in
both directions.

L. Installation of the Door Sills:

(1) Safety Procedures for Installation of the Door Sills:

(a) Obey all aircraft Owner/Operator’s safety procedures for the

Door Sill zone.

(b) When you install or remove the Door Sill on/from the aircraft,
make sure that the ground service equipment is properly
aligned in the door area.

(c) Door Sills are heavy! To avoid injury, a minimum of two people
must lift and move a Door Sill or the component must be moved
on a wheeled cart.

(d) A minimum of three people are required to install or remove a

Door Sill. Two people hold and monitor the Door Sill, while a
third person guides the component into the seat track.

(2) Installation of the Door Sills:

(a) Make sure the Door Sills are in the correct position. The side
guides must be adjacent to the cargo door opening.

(b) Put the Door Sills in the vertical position for installation.

(c) Remove the tension studs from the Door Sill and install in cor-
rect locations below the lip of the seat track. Make sure that
each tension stud is locked below the lip of the seat track.

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(d) Carefully lower the Door Sill on the tension studs.

(e) Install the washer and the nut on each tension stud. Torque the
nuts 55 to 65 in. lb (6.2 to 7.3 N m).

(3) Adjustments of the Door Sills on the aircraft. Refer to CMM Figure
1010, below.

(a) It is important to adjust the link arms and the spool legs to
ensure the Door Sills proper operation. Both Door Sills must be
leveled with the ball mats and each other in the DOWN position
and all saddles must rest on door spools.

(b) Turn the Door Sills in the DOWN position. Visually check if the
Door Sills are leveled and all saddles are on the door spools.

(c) If the Door Sills are not leveled, loosen the jam nuts on the link
arms.

(d) Put a thin tool through the opening in the link arm and turn the
link arm until the spool leg is at correct angle to the door spools.

(e) Then loosen the jam nuts on the spool legs.

(f) Holding the saddle, turn the adjustment stud on the spool leg
until the saddle is at correct position on the door spools.

(g) Torque the jam nuts on the link arms 160 to 190 in. lb (18.1 to
21.5 N m). Torque the jam nuts on the spool legs 450 to 500 in.
lb (50.8 to 56.5 N m).

(h) Wire lock the jam nuts on the link arms and the spool legs per
Owner/Operator’s procedures. Approximately 144 in. (366 cm)
of lock wire is required.

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CMM Figure 1010 - Door Sills Adjustments Summary

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4. Components Installation
A. As a general rule, start your installation at the FWD of the aircraft and work
your way to the AFT.

B. Typical installation of the Ancra components with permanent fasteners:

(1) Remove the studs from component and install in required positions in
the seat tracks.

(2) If applicable, install the retainers or washers on top of the studs.

(3) Make sure that component is installed in correct direction. The arrows
on some of the components show direction of installation.

(4) Carefully lower the component in position.

(5) Install the washers and the nuts on the studs. Hand tighten the nuts
only.

(6) Adjust the component on the floor as required and apply torque to the
nuts. For standard torque values refer to ASSEMBLY section of this
CMM.

C. To remove Ancra components from the aircraft, reverse the installation order.

D. To install and remove the Door Sill Protectors from the aircraft refer to Para-
graph 3.L., above.

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DISASSEMBLY
1. General
A. If you need to repair or clean the component, see which parts need to be dis-
assembled. It is possible that the procedure requires only partial disassem-
bly. Partial disassembly reduces wear on parts.

B. The person doing the disassembly can make modifications to the sequence
of disassembly.

C. Replace all parts damaged during disassembly.

D. When you move a component, do not let it twist. Give symmetrical support
below it.

E. Disassembly Materials:

(1) Common Mechanic Tools

(2) Ancra Retainer Installation Tool P/N T228-10

WARNING
WEAR GLOVES, PROTECTIVE CLOTHING, AND
EYE PROTECTION DURING DISASSEMBLY.
PARTS ARE SPRING-LOADED.

2. Disassembly of the Cargo Lock Assy P/N 80004

NOTE: All item numbers refer to IPL Figure 3, unless specified differently.

A. Remove the Outer Pawl (45) and the Inner Pawl (60):

(1) Cut the Cotter Pins (20) off of each Shaft (25).

(2) Pull the Shafts (25) out while you hold the Pawls (45, 60) in the Base
(115).

(3) Lift the Washers (30), the Pawls (45, 60), and the Springs (35, 40, 50,
55) out of the Base (115).

B. P/N 80004-10, -43 ONLY. Remove the Roller Assy (80):

(1) Cut the Cotter Pin (70) off of the Roller Shaft (75).

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(2) Pull the Roller Shaft (75) out.

(3) Lift the Roller Assy (80) out of the Base (115).

CAUTION: Do not disassemble the Roller Assy (80). If damaged,

replace with the new Roller Assy (80).

C. Remove the Shear Studs (105) from the Base (115):

(1) Turn the Setscrew (90) a few turns to move it out of the Shear Stud
(105). Try not to remove the Setscrew (90) from hole in the Base
(115).

(2) Lift the Shear Stud (105) and the Spring (100) out of the Base (115).

D. Remove two Tension Studs (110) from the Base (115).

E. Do not remove the Nameplate (10) and the Cover (15) unless they are dam-
aged. Refer to the REPAIR section of this manual.

3. Disassembly of the End Stop Assy P/N 80576

NOTE: All item numbers refer to IPL Figure 4, unless specified differently.

A. Release the Bolt (40), the Washer (45), and the Nut (50) from the Castings
(60, 65).

B. Move the Castings (60, 65) apart.

NOTE: The Bumpers (20) are Adhesive (30) bonded to the Castings (60, 65).
Do not remove the Bumpers (20). If the Bumpers (20) are damaged, get a
new End Stop Assy (1).

C. Do not remove the Nameplate (10) and the Cover (15) unless they are dam-
aged. Refer to the REPAIR section of this manual.

4. Disassembly of the Roller Rail Assy P/N 81384

NOTE: All item numbers refer to IPL Figure 5, unless specified differently.

A. Release the Bolts (25) the Washers (30) and the Nuts (35) that attach the
Retainers (20) to the Roller Rail (65).

B. Cut the Cotter Pins (50) off of the Roller Rail (65) shafts.

C. Remove the Collars (55) from the Roller Rail (65) shafts.

D. Slide the Roller Assy (60) from the Roller Rail (65) shafts.

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CAUTION: Do not disassemble the Roller Assy (60) or the Roller Rail (65). If
damaged, replace with the new assembly.

E. Do not remove the Nameplate (10) and the Cover (15) unless they are dam-
aged. Refer to the REPAIR section of this manual.

5. Disassembly of the Side Guide Rails P/N 84021

NOTE: All item numbers refer to IPL Figure 6, unless specified differently.

A. Cut the Cotter Pins (20) off of the Headed Pins (25).

B. Pull the Headed Pins (25) out of the Rail (40).

C. Lift the Roller Assy (30) from the Rail (40).

CAUTION: Do not disassemble the Roller Assy (30). If damaged, replace

with the new Roller Assy (30).

D. Do not remove the Nameplate (10) and the Cover (15) unless they are dam-
aged. Refer to the REPAIR section of this manual.

6. Disassembly of the Increased Height Side Guide Rails P/N 84022

NOTE: All item numbers refer to IPL Figure 7, unless specified differently.

A. Cut the Cotter Pins (20) off of the Headed Pins (25).

B. Pull the Headed Pins (25) out of the Rail (35).

C. Lift the Roller Assy (30) from the Rail (35).

CAUTION: Do not disassemble the Roller Assy (30). If damaged, replace

with the new Roller Assy (30).

D. Do not remove the Nameplate (10) and the Cover (15) unless they are dam-
aged. Refer to the REPAIR section of this manual.

7. Disassembly of the Articulating Side Guide Rails P/N 84764

NOTE: All item numbers refer to IPL Figure 8, unless specified differently.

A. Remove the Roller Assy (25) from the Rail (70):

(1) Cut the Cotter Pins (15) off of the Headed Pins (20).

(2) Pull the Headed Pins (20) out of the Rail (70).

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(3) Lift the Roller Assy (25) from the Rail (70).

CAUTION: Do not disassemble the Roller Assy (25). If damaged,

replace with the new Roller Assy (25).

B. Release the Screw (35), the Washer (40), and the Nut (45) to remove the
Link (30) from the Hinge Support (50).

C. Release the Screws (55), the Washers (60), and the Nuts (65) to remove the
Hinge Support (50) from the Rail (70).

D. Do not remove the Nameplate (5) and the Cover (10) unless they are dam-
aged. Refer to the REPAIR section of this manual.

8. Disassembly of the Increased Height Side Guide Rails P/N 86872

NOTE: All item numbers refer to IPL Figure 9, unless specified differently.

A. Cut the Cotter Pins (20) off of the Headed Pins (25).

B. Pull the Headed Pins (25) out of the Rail (35).

C. Lift the Roller Assy (30) from the Rail (35).

CAUTION: Do not disassemble the Roller Assy (30). If damaged, replace

with the new Roller Assy (30).

D. Do not remove the Nameplate (10) and the Cover (15) unless they are dam-
aged. Refer to the REPAIR section of this manual.

9. Disassembly of the Ball Mats P/N 86963

NOTE: All item numbers refer to IPL Figure 10, unless specified differently.

A. Remove the Studs (85), the Retainers (90), the Washers (105), and the Nuts
(115) from the Panel Assy (200).

B. Remove the Ball Units (50) as follows:

(1) Turn the Setscrew (30) through the notch in the Retainer (45) until it is
below the Retainer (45).

(2) Use the Ancra Retainer Installation Tool P/N T228-10 to carefully push
DOWN and turn the Retainer (45) until it releases from the Ball Unit
(50) housing and moves UP.

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(3) Lift the Retainer (45), the Ball Unit (50), and the Spring (55) out of the
Ball Unit (50) housing.

CAUTION: Do not disassemble the Ball Unit (50). If damaged, replace

with a new Ball Unit (50).

C. P/N 86963-10, -13, -15, -17, -19 ONLY. To remove the Ramp Rail (150), drill
off the Rivet (160) heads.

D. To remove the Brackets (280), drill off the Rivet (290) heads.

CAUTION: Do not disassemble the Panel Assy (200) structure. Parts are riv-
eted and adhesive bonded together. Refer to the REPAIR section of this
manual.

E. Do not remove the Nameplate (10) and the Cover (15) unless they are dam-
aged. Refer to the REPAIR section of this manual.

10. Disassembly of the Crosstracks P/N 86974

NOTE: All item numbers refer to IPL Figure 11, unless specified differently.

A. P/N 86974-10, -12, -13, -16, -18, -22, -23, -28 ONLY. Remove the Roller
Assy (40):

(1) Cut the Cotter Pins (30) off of the Roller Shafts (35).

(2) Pull the Roller Shafts (35) out of the Roller Support Bracket (45, 50).

(3) Lift the Roller Assy (40) out of the Roller Support Bracket (45, 50).

CAUTION: Do not disassemble the Roller Assy (40). If damaged,

replace with the new Roller Assy (40).

(4) P/N 86974-10, -16 ONLY. Release the Bolts (55), the Washers (60),
and the Nuts (65) to remove the Roller Support Bracket (45) from of
the Crosstrack (300, 300D).

(5) P/N 86974-12, -13, -18, -22, -23, -28 ONLY. Release the Bolts (57)
and remove the Roller Support Bracket (50) from of the Crosstrack
(300B, 300C, 300E, 300F, 300G, 300H).

B. Remove the Vertical Restraint (100) mechanism:

(1) Release the Bolt (80), the Washer (85), and the Nut (90) from the Out-
board Restraint Body (110).

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(2) Lift the Vertical Restraint (100) and the Spring (105) from the Outboard
Restraint Body (110).

(3) Remove the Bushing (95) from top of the Vertical Restraint (100).

(4) Remove the Outboard Restraint Body (110) by releasing the Bolts
(114, 117, 120), the Washers (130), and the Nuts (140).

C. P/N 86974-16, -17, -18, -28 ONLY. Remove the Pawl (175) mechanism:

(1) Remove and discard the Retaining Rings (150) from the Shaft (155).

(2) Carefully pull the Shaft (155) out of the Crosstrack (300D, 300E, 300H)
while you hold the Pawl (175).

(3) Remove the Pawl (175), the Washers (160), and the Springs (165,
170).

D. P/N 86974-16, -17 ONLY. Remove and discard the Groove Pin (180) from
the Crosstrack (300D) and remove the Plunger (190) and the Spring (195).

E. Remove the Studs (220, 225), the Washers (250, 260), and the Nuts (280)
from the Crosstrack (300).

F. Do not remove the Nameplate (10) and the Cover (15) unless they are dam-
aged. Refer to the REPAIR section of this manual.

11. Disassembly of the Crosstracks P/N 86976

NOTE: All item numbers refer to IPL Figure 12, unless specified differently.

A. Remove the Pawl (65) mechanism:

(1) Remove and discard the Retaining Rings (30, 35) from the Shafts (40,
45).

(2) Carefully pull the Shafts (40, 45) out of the Crosstrack (300) while you
hold the Pawl (65) and the Lever (70).

(3) Remove the Pawl (65), the Lever (70), the Washers (50, 55), and the
Spring (60).

B. Remove the Studs (220, 225), the Washers (250 thru 265), and the Nuts
(280, 285) from the Crosstrack (300).

C. Do not remove the Nameplate (10) and the Cover (15) unless they are dam-
aged. Refer to the REPAIR section of this manual.

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12. Disassembly of the Door Sill Protector P/N 86980

NOTE: All item numbers refer to IPL Figure 13, unless specified differently.

A. Remove and discard the Cotter Pins (60, 100) and the Spring Pins (80) from
the Shafts (65, 85, 105).

B. Pull out the Shafts (65, 85, 105) out of the Door Sills (680 thru 695) and
remove the Rollers (70, 90, 110).

C. To remove the Gas Spring (165), remove and discard two Cotter Pins (145)
that attach the Shaft (150). Pull out the Shaft (150) and remove the Bolt
(130A) and the Spacer (140). Remove two End Fittings (155) from the Gas
Spring (165).

D. Release the Screws (180), the Washers (185), and the Nuts (190) and
remove the Spring Bracket (175).

E. Remove and discard the Cotter Pins (200, 205) from the Pins (215) and pull
out the Pins. Remove and discard the Grove Pins (220) from the Pins (222)
and pull out the Pins. Loosen the Nuts (235, 240) and remove the Rod End
Joints (225, 230), the Nuts (235, 240), the Stud (245), the Link Arm (250),
and the Rod Link (255).

F. Remove and discard the Cotter Pins (270) from the Shaft (275). Carefully pull
out the Shaft (275) and remove the Spring (280) and the Leg (325) with
attached components.

G. Remove and discard the Lock Wire (288). Loosen the Nuts (315, 320) and
remove the Saddle (305), the Nuts (315, 320), and the Stud (310) from the
Leg (325).

H. Remove the Plastic Trims (285) from the Door Sills (680 thru 695).

I. To remove the Leg Brackets (340, 345), release the Bolts (350) and the
Washers (355).

J. Remove and discard the Spring Pin (370). Carefully pull out the Shaft (375)
and lift the Springs (380, 385) and the Guide (390, 395).

K. Release the Bolts (425) and the Washers (430) and remove the Housing
Doubler (420) with attached locking mechanism. Remove the Spring Pin
(400) and take apart the Spring (415), the Plunger (410), the Doubler Hous-
ing (420), and the Handle (405).

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L. Remove and discard the Cotter Pins (465). Pull the Shaft (470) out of the
Support (490). Lift the Guide (485) with the Springs (475, 480). Release the
Bolts (495), the Washers (500), and the Nuts (505) to remove the Support
(490). Release the Screw (450), remove the Latch (455) and the Plunger
(460).

M. Release the Screw (515) and remove the Washers (520, 535), the Roller
Retainer (525), and the Pivot Roller (530) from the Pivot Roller Body (550).
Remove and discard the Cotter Pins (540) and slide the Lockhead Shaft
(545) out. Lift the Pivot Roller Body (550) out of the Hinge Bracket (590).

N. Remove and discard the Groove Pins (560). Pull the Shafts (565, 570) out
and disconnect the Hinge Brackets (580, 590) from the Door Sills (680 thru
695).

O. Remove the Studs (600 thru 610), the Washers (620 thru 630), and the Nuts
(640, 645) from the Hinge Brackets (580, 590).

P. Release the Bolts (660), the Washers (665), and the Nuts (670) and move
apart the Door Sills (680 thru 695).

Q. Do not remove the Nameplate (5), the Decals (15 thru 30), or the Covers (40
thru 50) unless they are damaged. Refer to the REPAIR section of this man-
ual.

13. Disassembly of the Lateral Guides P/N 87008

NOTE: All item numbers refer to IPL Figure 14, unless specified differently.

A. Remove the Studs (340), the Washers (345, 350), and the Nuts (355) from
the Base (400).

B. Remove the Ball Units (45) as follows:

(1) Turn the Setscrew (30) through the notch in the Retainer (40) until it is
below the Retainer (40).

(2) Use the Ancra Retainer Installation Tool T228-10 to carefully push
DOWN and turn the Retainer (40) until it releases from the Housing
(70) and moves UP.

(3) Lift the Retainer (40), the Ball Unit (45), and the Spring (50) out of the
Base (400).

NOTE: Do not disassemble the Ball Unit (45). If damaged, replace with
a new Ball Unit (45).

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(4) Release the Screws (55) and lift the Skin (60) and the Housings (70)
out of the Base (400).

C. Remove four Spring Pins (280). Remove the Blocks (285) and the Lockhead
Shafts (290) from the Base (400).

D. Remove the Spring Pins (170) out of the Base (400).

E. With the Frame (185) in the UP position, carefully remove two Shafts (175),
and the Shaft (180) out of the Base (400).

F. Lift the Frame (185) with the attached components, the Washers (195), and
the Torsion Springs (190) out off the Base (400).

G. Remove the Spring Pins (130) out of the Frame (185).

H. Pull the Shafts (135, 140) out and remove the Roller Assy (145) out of the
Frame (185).

I. Remove the Spring Pins (160) out of the Frame (185).

J. Remove the Lockhead Shafts (165) and the Link (215) with components out
of the Frame (185).

K. Release the Bolts (200) and the Washers (205). Move apart the Links (215,
295), and the Dampeners (220).

L. Remove the Spring Pin (80) out of the Handle (90).

M. Remove the Handle (90), the Release Plunger (95), and the Handle Spring
(100).

N. Release the Bolts (110) and the Washers (115) and remove the Doubler
Housing (105) form the Base (400).

O. Remove the Spring Pin (305) out of the Base (400).

P. Pull the Lockhead Shaft (310) out and remove the Roller Assy (320) out of
the Base (400).

CAUTION: Do not disassemble the Roller Assy (145, 320). If damaged,

replace with the new Roller Assy (145, 320).

Q. Do not remove the Nameplate (10) and the Cover (15) unless they are dam-
aged. Refer to the REPAIR section of this manual.

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14. Disassembly of the Crosstracks P/N 87226

NOTE: All item numbers refer to IPL Figure 15, unless specified differently.

A. Remove the Roller Assy (40):

(1) Cut the Cotter Pins (30) off of the Roller Shafts (35).

(2) Pull the Roller Shafts (35) out of the Roller Support Bracket (50).

(3) Lift the Roller Assy (40) out of the Roller Support Bracket (50).

CAUTION: Do not disassemble the Roller Assy (40). If damaged,

replace with the new Roller Assy (40).

(4) Release the Bolts (55) and remove the Roller Support Bracket (50)
from of the Crosstrack (300).

B. Release the Screws (80), the Washers (85), and the Nuts (90) from the End
Base (110).

C. Remove the End Base (110) by releasing the Bolts (115, 120), the Washers
(130), and the Nuts (140).

D. Remove the Studs (225), the Washers (250, 260), and the Nuts (280) from
the Crosstrack (300).

E. Do not remove the Nameplate (10) and the Cover (15) unless they are dam-
aged. Refer to the REPAIR section of this manual.

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CLEANING
1. General

WARNING
OBEY ALL SAFETY AND APPLICATION
INSTRUCTIONS FROM MANUFACTURER
OF CLEANING SOLUTIONS AND MSDS.
CLEANING SOLUTIONS ARE HAZARDOUS.

CAUTION
DO NOT USE CLEANING SOLUTIONS
THAT CONTAIN CHLORINE, STRONG ACIDS,
OR ALKALIS. THESE CHEMICALS CAN
DAMAGE ALUMINUM IN COMPONENTS.

2. Materials
A. Refer to CMM Table 4001 for the cleaning materials.

NOTE: Equivalent substitutes approved by engineering may be used.

Specification or Part
Name Source or CAGE Code
Number

Low Lint Cloth A-A-59323 Commercially Available

Cleaning Brush 7092T16 V3A054
Cleaning Solution FD080, Safety PrepTM, V0K209
NSN6850-01-381-5139
Isopropyl Alcohol GSL26 Commercially Available

CMM Table 4001 - Materials

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3. Procedures
A. Cleaning parts:

(1) Wash part with the Cleaning Solution.

(2) Remove dirt with the Cleaning Brush.

(3) Dry part with a clean Low Lint Cloth.

B. Cleaning surfaces before you attach the nameplate:

(1) Refer to REPAIR section of this manual.

C. Cleaning removed ball units:

(1) Soak the ball units in the Cleaning Solution for 1 hour.

(2) Air-blow the ball unit with low pressure compressed air from the ball
side to flush dirt out of the drainage hole.

(3) If necessary, repeat soaking and air-blowing until all dirt is completely
out of the ball unit.

(4) Wipe off the ball unit with Low Lint Cloth.

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CHECK
1. General
A. Types of applicable checks and inspections are listed below:

(1) Checklist for Troubleshooting During Load/Unload

(2) Visual Check at Each Loading Cycle

(3) System Operational Check

(4) Overhaul Inspection and Maintenance Schedule

(5) Component Operational Check

B. When you do the check or inspection, write the results of the differences and
identify a corrective maintenance action. Obey the Owner/Operator’s proce-
dures.

C. If a component has more damage than is permitted to be repaired in the field,

talk to Ancra Customer Service. It could be necessary to send the component
to Ancra International for the correct repair.

Procedure to Get
Condition Response
Response
1. After unload or before Prevent delays by identify- Do the Visual Check at
load ing trouble spots before load Each Loading Cycle. Refer
to the Instructions for Con-
tinued Airworthiness Man-
ual 10551, Rev. C, dated
Jan. 1, 2021.
2. ULD blocked during Release the ULD without Do the Checklist for Trou-
load / unload damage to aircraft, critical bleshooting During Load/
components, or cargo Unload. Refer to the
Instructions for Continued
Airworthiness Manual
10551, Rev. C, dated Jan.
1, 2021.
3. Component is dam- Quickly identify the cause of Do the Component Opera-
aged or does not oper- the problem tional Check. Identify if
ate replacement is necessary.

CMM Table 5001 - Conditions and Responses (Sheet 1 of 2)

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Procedure to Get
Condition Response
Response

4. Component is dam- Remove and replace with a Install component with ser-
aged or does not oper- serviceable component. viceable tag.
ate; Replacement is Refer to operator replace-
available ment procedure.
5. Component is dam- Remove component that is Refer to Damage Limits
aged or does not oper- damaged or does not oper- Reference Guide in sec-
ate; No replacement is ate, tion 5, below, and Ancra
available or mainte- Aircraft Weight and Bal-
nance must be and: Determine if the ULD ance Manual 10552, Rev.
deferred loading position must be C, dated Sep, 2019.
downloaded or voided (not
loaded),
and: write the results.
6. After you receive or Make sure that component Do the Component Opera-
repair a component is serviceable. tional Check.
7. After you install a com- Make sure that component Do the Component Opera-
ponent in aircraft is serviceable. tional Check.
8. After you install the full Make sure that components Do the System Opera-
CHS are installed in correct posi- tional Check.
tions.
9. If there is a question if See loading arrangement Make sure all restraint
the loading arrange- placard at cargo door area. devices correctly engage
ment is correct the ULD.
10. After aircraft extended Make sure that CHS has all Do the System Opera-
downtime components and all compo- tional Check.
nents are serviceable.
11. Every 72 month or Make sure that CHS has all Do the System Overhaul
18000 FH, whichever components and all compo- Inspection.
comes first nents are serviceable.

CMM Table 5001 - Conditions and Responses (Sheet 2 of 2)

2. System Operational Check

A. Do the System Operational Check after you install the CHS. Approximately
one hour is necessary to make this check.

B. First, do the Visual Check at Each Loading Cycle. Refer to the Ancra Instruc-
tions for Continued Airworthiness Manual 10551, Rev. C, dated Jan. 1, 2021.

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C. Move a ULD of each approved size through each position of the CHS.

D. Make sure that all components operate correctly.

E. Lock the ULD to each loading position. Make sure that all restraint devices
are engaged.

F. If restraint devices do not engage the ULD, check the CHS installation draw-
ing P/N 85550 and reposition the component to correct location.

G. Visually check the wall and floor markings (if applicable) and placards to
ensure they are properly affixed to the aircraft.

3. Overhaul Inspection and Maintenance Schedule

A. This inspection is required every 72 month or 18000 FH, whichever comes
first.

B. Approximately 230 man-hours are necessary to make this inspection.

C. Obey procedures in the Aircraft Maintenance Manuals and the Owner/Opera-

tor procedures.

D. Identify the CHS:

(1) Compare the CHS in the aircraft with IPL Figures 1 or 1A of this man-
ual.

(2) Compare the identification nameplate on each component with the

part numbers and installation locations shown in IPL Figures 1 or 1A.

(3) If an identification nameplate is damaged or not there, refer to the IPL

Figures 3 thru 15 to see the illustrated parts lists for each component.
If possible, identify the components by comparison to the illustrated
parts lists.

E. Remove the CHS components from the aircraft.

F. Examine the main deck and the seat tracks. If damage is discovered, refer to
the Aircraft Maintenance Manual for repair. Do not install CHS components in
damaged seat tracks.

G. Check each component of the CHS:

(1) Compare each component with its Illustrated Parts List in this manual.

(2) Make sure that all assemblies have Ancra identification nameplates.

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(3) Remove dirt, loose objects, and waste. Refer to the CLEANING sec-
tion of this manual.

(4) Do the Component Operational Check on all components. The proce-

dures are given in Section 4, below.

(5) Remove and replace components that have signs of damage. Refer to
the DISASSEMBLY, REPAIR, and ASSEMBLY sections.

H. Ball Mats:

(1) Remove all ball units from the panel. Refer to DISASSEMBLY section
of this manual.

(2) If necessary, clean the retainer, the ball unit, the spring, and the hous-
ing from dust and debris. Refer to the CLEANING section of this man-
ual.

(3) Visually check the retainer, the ball unit, and the spring for damage
and corrosion. Reassemble the ball units with serviceable compo-
nents. Refer to ASSEMBLY section of this manual.

I. Install components:

(1) Install components which are approved for installation. Approval is the
responsibility of the aircraft Owner/Operator.

(2) Install components which were approved after the Component Opera-
tional Check.

(3) Install components into clean seat tracks. If it is necessary to clean the
seat tracks, refer to procedures from the Owner/Operator or Aircraft
Manufacturer.

J. Make sure that all components are installed in the correct positions on the
main deck.

(1) Refer to the CHS installation drawing P/N 85550. You may request a
copy of installation drawing from Ancra International.

(2) The station positions given in this manual are approximate locations.

K. Do the System Operational Check.

(1) The System Operational Check makes sure that the CHS can move
and lock the ULDs correctly.

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(2) The procedure is given in Section 2, above.

L. Write the results of any problem and identify a corrective maintenance action.

4. Component Operational Check

A. Approximately one to five minutes for each component is necessary for this
check.

B. Completeness: Visually check each component for completeness. Compare

each component with its Illustrated Parts List within this manual. Check to
make sure all parts are there and each part is correctly assembled.

C. Damage: Visually check each component for damage:

(1) No parts are bent, twisted or out-of-shape.

(2) Corrosion: Refer to REPAIR section for corrosion procedures. Minor

discoloration or surface imperfections may be present from normal
use.

(3) There are no cracks or deep scrapes. Shallow scrapes are typical on
normal ULD contact surfaces and seat track surfaces.

(4) Coating is intact. Some coating will be rubbed off on normal ULD con-
tact surfaces and seat track contact surfaces.

(5) There is no leaking lubrication. Do not add lubrication.

(6) Parts fit together with no binding or wobble.

(7) Parts are not blocked by loose objects or lumps of dirt.

(8) There are no out-of-round shaft holes or burrs around shaft holes.

(9) The springs ends are engaged in components.

(10) Cotter pins are installed with one end around each side of the shaft.

(11) The floor attaching hardware is not damaged or missing and securely
attached to the main body, base, or crosstrack.

(12) The identification nameplates are attached and readable.

D. Functionality: Operate each part to ensure proper function. Refer to the

DESCRIPTION AND OPERATION section of this manual. Cycle each com-
ponent a minimum of 5 times to ensure proper function.

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E. Remove and replace parts that are damaged or do not operate. Refer to the
REPAIR section of this manual. Write the results of differences and the main-
tenance response.

F. The CHS is made to operate as a full unit. If a component is damaged or not

there, refer to the Component Damage Limits Reference Guide, below.

5. Component Damage Limits Reference Guide

A. It is possible that parts that are damaged or not there can reduce the permit-
ted maximum gross weight for that ULD loading position.

B. The Component Damage Limits Reference Guide in CMM Table 5003,

below, shows Ancra International’s required conditions for damage limits. The
guide can help you decide when you can continue to operate an incomplete
CHS in full or reduced operation.

C. For the function of this reference guide, damage limits are divided into three
categories. The categories are given in CMM Table 5002, below.

Category Description
I These are non-restraint devices; repair and replacement may be delayed
until next maintenance interval. For example, rollers, ball units, guidance
surfaces, or pivot rollers.
II These are non-restraint devices but have impact on ULD conveyance. The
operator may repair these discrepancies partially to bring it to Category 1
until next maintenance interval. For example, large number or rollers or
ball units damaged or missing in one area can be improved by moving roll-
ers or ball units from other part of the CHS.
III These are restraint devices. There is no time limitation for repairing or
replacing damaged restraint, however the ULD allowable weight will be
restricted or loading position will be voided. For more information and rem-
edies see Ancra Aircraft Weight & Balance Manual 10552, Rev. C, dated
Sep, 2019.

CMM Table 5002 - Description of Categories

D. Make an analysis of damage as a result of damage to the full ULD loading

position.

(1) The Component Damage Limits Reference Guide, below, makes an

analysis of damage to each component.

(2) If more than one type of component is damaged or missing in the

same ULD position, you must make an analysis of all damaged com-
ponents.

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Name and Description of Quantity Category

P/N Damage Damaged or Missing
Cargo Locks Damaged or missing pawls, shafts, Any III
80004 springs, cotter pins, floor attaching
hardware, or base
Damaged or missing rollers Any I
End Stops Damaged or missing castings or Any III
80576 fasteners
Crosstracks Damaged or missing pawls, levers, Any III
86974, or vertical restraints (flippers)
86976, Damaged or missing shafts, Any III
87226 springs, retaining rings on pawls
and levers, flipper, floor attaching
hardware, body, or crosstracks
Damaged or missing rollers Any I
Side Rails Damaged or missing rollers Any I
84021, Damaged or missing rail, guide, fit- Any I
84022, ting, or attaching hardware
84764,
86872
Lateral Damaged or missing rollers or ball Any I
Guides units
87008 Damaged or missing frame, fittings, Any I
base, pins, springs, or floor attach-
ing hardware
Roller Rails Damaged or missing rollers, shafts, 1 or 2 per ULD posi- I
81384 or cotter pins tion
3 or more per ULD II
position
Damaged or missing floor attaching 1 per ULD position I
hardware or rail 2 or more per ULD II
position
Door Sill Pro- Damaged or missing restraints Any III
tectors Damaged or missing guides or roll Any II
86980 back stops
Damaged or missing legs or hinges Any II
Damaged or missing latch mecha- Any II
nism
Damaged or missing rollers Any II
Damaged or missing floor attaching Any II
hardware
Damaged or missing caution decals Any I
CMM Table 5003 - Component Damage Limits Reference Guide (Sheet 1 of 2)

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Name and Description of Quantity Category

P/N Damage Damaged or Missing
Ball Mats High-density ball units (4 in. (10.2Up to 1 x 1 in. (2.5 x I
86963 cm) between ball units): Damaged 2.5 cm) area per Ball
or missing top or bottom skin Mat or ULD position
More than 1 x 1 in. II
(2.5 x 2.5 cm) area per
Ball Mat or ULD posi-
tion
Low-density ball units (6 in. (15.2 Up to 3 x 3 in. (7.6 x I
cm) between ball units): Damaged 7.6 cm) area per Ball
or missing top or bottom skin Mat or ULD position
More than 3 x 3 in. II
(7.6 X 7.6 cm) area
per Ball Mat or ULD
position
Damaged or missing non-skid walk- Up to 2 x 2 in. (5.1 x I
way coating or primer 5.1 cm) per Ball Mat or
ULD position
More than 2 x 2 in. II
(5.1 x 5.1 cm) per Ball
Mat or ULD position
Damaged or missing edge rail Up to 3 in. (7.6 cm) I
per Ball Mat or ULD
position
More than 3 in. (7.6 II
cm) per Ball Mat or
ULD position
Damaged or missing ramp rails Any I
Damaged or missing ball units Up to 10% per ULD I
(evenly spread out) position and Ball Mat
More than 10% per II
ULD position and Ball
Mat
Damaged or missing brackets or 1 or 2 per ULD posi- I
floor attaching hardware tion
3 or more per ULD II
position
Placards, Damaged, missing, illegible Any I
Nameplates,
Wall Mark-
ings

CMM Table 5003 - Component Damage Limits Reference Guide (Sheet 2 of 2)

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REPAIR
1. General

WARNING
OBEY ALL SAFETY AND APPLICATION
INSTRUCTIONS FROM MANUFACTURER
OF CHEMICAL SOLUTIONS AND MSDS.
CHEMICAL SOLUTIONS ARE HAZARDOUS.

CAUTION
DO NOT USE CLEANING SOLUTIONS
THAT CONTAIN CHLORINE, STRONG ACIDS,
OR ALKALIS. THESE CHEMICALS CAN
DAMAGE ALUMINUM IN COMPONENTS.

2. Content
A. Repair, refinish, and replacement procedures are shown in CMM Table 6001.

NOTE: The item numbers in CMM Table 6001 refer to IPL Figures 1 and 1A,
unless specified differently.

Repair
Item Number Part Name Repair Operation
Number

30 thru 370 All Repair of Small Surface 1-1

Imperfection
Restore the Non-Skid Paint 2-1
230 thru 265
Ball Mat Assy Repair of the Edge Rail 3-1
Repair of the Panel Skin 4-1
30 thru 370 All Replacement of the Name- 5-1
plate
CMM Table 6001 - Repair Procedures

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3. Materials
A. Refer to CMM Table 6002 for the materials necessary to do the repairs.

NOTE: Equivalent substitutes approved by engineering may be used.

Specification or Source or CAGE
Name Use
Part Number Code
Abrasive Pad Scotch-Brite, V52152 To remove surface
Nylon web, imperfections
aluminum oxide
Cleaning Brush 7092T16 V3A054 For general cleaning
Vacuum Cleaner No specific Commercially For general cleaning
Available
Zinc Coating ASTM B633, Type II, Commercially Protective coating
Class Fe/Zn Available
Alodine Coating MIL-C-81706, Commercially Protective coating
Class 1A Available
Low Lint Cloth A-A-59323 Commercially To wipe surfaces
Available
Isopropyl Alcohol GSL26 Commercially To clean parts
Available
Masking Tape No specific Commercially
Available
Paint Roller or No specific Commercially Restore the Anti-Skid
Paint Brush Available Paint
Light Green Primer 44GN054 V33461
Anti-Skid Paint 342-4 V0YY71
Edge Rail 80025 V31272
Aluminum Sheet 2014-T6 Commercially
Available Edge Rail Repair
Rivets MS20426AD5-5 Commercially
Available
Aluminum Sheet 2014-T4 or -T3 Commercially
Available
Rivets MS20601AD5W2 Commercially Panel Skin Repair
Available
Epoxy Adhesive 2216 V52152
CMM Table 6002 - Repair Materials

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4. Tools, Fixtures, and Equipment

A. Refer to CMM Table 6003 for the tools, fixtures, and equipment necessary to
do the repairs.

NOTE: Equivalent substitutes approved by engineering may be used.

Specification or Source or CAGE
Name Use
Part Number Code
Paint Mixer No specific Commercially
Available Restore the Anti-Skid
Paint Sprayer No specific Commercially Paint
Available
CMM Table 6003 - Repair Tools, Fixtures, and Equipment

5. Repair of Small Surface Imperfections - REPAIR 1-1

A. Clean the application area with Isopropyl Alcohol and the Cleaning Brush.

B. Polish the surface with the Abrasive Pad. Remove abrasive dust.

C. Apply a layer of protection on the polished areas:

(1) Apply Zinc Coating to ferrous parts per ASTM B633, Type II, Class Fe/
Zn.

(2) Brush-coat nonferrous parts with Alodine Coating per MIL-C-81706,

Class 1A.

6. Restore the Anti-Skid Paint - REPAIR 2-1

CAUTION
DO NOT ALLOW DIRT, ABRASIVE DUST, OR
PAINT ON BALL UNITS, RETAINERS, AND
RAMP RAIL. PROTECT THESE PARTS
WITH MASKING TAPE.

A. Cover primer/paint application borders with the Masking Tape as required.

B. Sand down surface to bare metal. Remove corrosion, scores, and scratches.

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C. Remove dirt and abrasive dust with the Vacuum Cleaner or the Cleaning
Brush.

D. Clean the area with Isopropyl Alcohol and allow to air-dry.

E. Spray-paint the Light Green Primer on the surface in uniform single coat.

F. Let the coat dry for 24 at least hours.

G. Anti-Skid Paint application:

(1) Mix the Anti-Skid Paint components according to the manufacturer

procedure.

(2) Pour the necessary amount of the mixed Anti-Skid Paint in zig-zag pat-
tern on the primed surface.

(3) Spread the liquid Anti-Skid Paint evenly on the surface with the paint
roller or the paint brush.

(4) Let the coat dry for at least 24 hours.

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7. Repair of the Edge Rail - REPAIR 3-1

A. You can repair a maximum length of 3 in. (7.6 cm) of the Edge Rail.

B. CMM Figure 6001 gives the procedures for the Edge Rail Repair.

CMM Figure 6001 - Repair of the Edge Rail

NOTE: To restore the paint refer to instructions in REPAIR 2-1

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8. Repair of the Panel Skin - REPAIR 4-1

A. Repair limits:

(1) Panels with low-density ball units (Approximately 6 in. (15.2 cm)
between ball units): You can repair a maximum area of a 3 x 3 in. (7.6
x 7.6 cm) section of the top or bottom skin.

(2) Panels with high-density ball units (Approximately 4 in. (10.2 cm)
between ball units): You can repair a maximum area of a 1 x 1 in. (2.5
x 2.5 cm) section of the top or bottom skin.

B. CMM Figure 6002 gives procedures for the Panel Skin Repair.

CMM Figure 6002 - Repair of Panel Skin

NOTE: To restore the paint refer to instructions in REPAIR 2-1

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9. Replacement of the Nameplate - REPAIR 5-1

A. If you removed the Nameplate, do not apply it again. If damaged or not there,
replace with the new.

B. Order the new Nameplate and the Clear Cover at Ancra. Make sure to give
serial number and the part number for the part.

C. Refer to the IPL Figures 3 thru 15 to get correct position for the Nameplate.

D. Clean the Nameplate application area with Isopropyl Alcohol and allow to air-
dry.

E. Peel the backing and attach the new Nameplate on component.

F. Apply the Clear Cover on top of the Nameplate.

G. CMM Figure 6003 gives condensed procedures for replacement of the

Nameplate.

CMM Figure 6003 - Replacement of the Nameplate

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ASSEMBLY
1. General
A. The person doing the assembly can make modifications to the sequence of
assembly.

B. Do not lubricate parts.

C. Replace all parts damaged during disassembly.

D. When you move a component, do not let it twist. Give symmetrical support
below it.

E. Assembly Materials:

(1) Common Mechanic Tools

(2) Ancra Retainer Installation Tool P/N T228-10

WARNING
WEAR GLOVES, PROTECTIVE CLOTHING, AND
EYE PROTECTION DURING ASSEMBLY.
PARTS ARE SPRING-LOADED.

WARNING
OBEY ALL SAFETY AND APPLICATION
INSTRUCTIONS GIVEN BY MANUFACTURERS
OF THREADLOCKER, ADHESIVE, SEALER, &
MSDS. THESE CHEMICALS ARE HAZARDOUS.

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F. Approved Torques:

(1) Use the approved torques given in CMM Table 7001, below.

Thread Size Tightening Torque*

Diameter Threads per in., lb in., (N m)
in., (cm) (cm)
0.190 (0.483) 32 (12.6) 030 to 040 (3.4 to 4.7)
0.250 (0.635) 28 (11) 055 to 065 (6.2 to 7.3)
0.312 (0.792) 24 (9.5) 125 to 155 (14.1 to 17.5)
0.375 (0.953) 24 (9.5) 160 to 190 (18.1 to 21.5)
0.500 (1.270) 20 (7.9) 450 to 500 (50.9 to 56.5)
* Unless otherwise noted in assembly instructions

CMM Table 7001 - Approved Torques

2. Assembly of the Cargo Lock Assy P/N 80004

NOTE: All item numbers refer to IPL Figure 3, unless specified differently.

A. Install the Inner Pawl (60):

(1) Align one Washer (30), the Inner Pawl (60), the Springs (50, 55), and
another Washer (30) inside the Base (115).

(2) Slide the Shaft (25) through components.

(3) Put the ends of the Springs (50, 55) in grooves on bottom of the Base
(115) and on the Inner Pawl (60).

(4) Install the new Cotter Pins (20) on the Shaft (25).

B. Install the Outer Pawl (45):

(1) Align one Washer (30), the Outer Pawl (45), the Springs (35, 40), and
another Washer (30) inside the Base (115).

(2) Slide the Shaft (25) through components.

(3) Put the ends of the Springs (35, 40) in grooves on bottom of the Base
(115) and in the holes in the Outer Pawl (45).

(4) Install the new Cotter Pins (20) on the Shaft (25).

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C. Install two Shear Studs (105) into the Base (115):

(1) Apply one drop of the Threadlocker (95) to the threads of two Set-
screws (90).

(2) Put the Setscrews (90) in hole in the Base (115). Make sure that set-
screw does not extend into the Shear Stud (105) hole.

(3) Install the Spring (100) on the Shear Stud (105). Visually check how
much the end of the Spring extends above the Shear Stud.

(4) Remove the Spring (100) from the Shear Stud (105). Cut the end of
the Spring (100) so it will be flush or slightly below top of the Shear
Stud.

(5) Put the cut end of the Spring (100) in hole in top of the Shear Stud
(105). Make sure that end of the Spring does not extend above top of
the Shear Stud.

(6) Put the Shear Stud (105) together with Spring (100) in the Base (115).

(7) Turn the Shear Stud (105) approximately 1/2-turn and push it down to
preload the Spring (100).

(8) Align groove in the Shear Stud (105) with the Setscrew (90) hole in
Base (115).

(9) Put the Setscrew (90) through the Base (115) and into groove in the
Shear Stud (105).

(10) Tighten the Setscrew (90) fully then back-off approximately one turn.

(11) If required, lightly hit the Shear Stud (105) with mallet to set the Spring
(100).

D. Attach the Tension Studs (110) to the Base (115).

E. P/N 80004-10, -43 ONLY. Install the Roller Assy (80) in the Base (115):

(1) Align the Roller Assy (80) inside the Base (115).

(2) Slide the Roller Shaft (75) through the components.

(3) Install the new Cotter Pin (70) on the Roller Shaft (75).

F. Refer to the REPAIR section of this manual to replace the adhesive backed
Nameplate (10) and the Cover (15).

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G. Check the component for proper operation. Refer to the CHECK section of
this manual.

3. Assembly of the End Stop Assy P/N 80576

NOTE: All item numbers refer to IPL Figure 4, unless specified differently.

NOTE: The Bumpers (20) must be bonded to the Castings (60, 65). If the
Bumpers (20) are damaged, get a new End Stop Assy (1).

A. Install the Bolt (40) through the Castings (60, 65).

B. Attach the Washer (45) and the Nut (50) to the Bolt (40) and hand tighten.

C. Refer to the REPAIR section of this manual to replace the adhesive backed
Nameplate (10) and the Cover (15).

D. Check the component for proper operation. Refer to the CHECK section of
this manual.

4. Assembly of the Roller Rail Assy P/N 81384

NOTE: All item numbers refer to IPL Figure 5, unless specified differently.

A. Slide the Roller Assy (60) on the Roller Rail (65) shafts.

B. Install the Collars (55) on the Roller Rail (65) shafts.

C. Install the new Cotter Pins (50) in the Roller Rail (65) shafts.

D. Attach the Retainers (20) to the Roller Rail (65) with the Bolts (25), the Wash-
ers (30), and the Nuts (35) and hand tighten.

E. Refer to the REPAIR section of this manual to replace the adhesive backed
Nameplate (10) and the Cover (15).

F. Check the component for proper operation. Refer to the CHECK section of
this manual.

5. Assembly of the Side Guide Rails P/N 84021

NOTE: All item numbers refer to IPL Figure 6, unless specified differently.

A. Align the Roller Assy (30) inside the Rail (40).

B. Slide the Headed Pins (25) through the components.

C. Install the new Cotter Pins (20) on the Headed Pins (25).

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D. Refer to the REPAIR section of this manual to replace the adhesive backed
Nameplate (10) and the Cover (15).

E. Check the component for proper operation. Refer to the CHECK section of
this manual.

6. Assembly of the Increased Height Side Guide Rails P/N 84022

NOTE: All item numbers refer to IPL Figure 7, unless specified differently.

A. Align the Roller Assy (30) inside the Rail (35).

B. Slide the Headed Pins (25) through the components.

C. Install the new Cotter Pins (20) on the Headed Pins (25).

D. Refer to the REPAIR section of this manual to replace the adhesive backed
Nameplate (10) and the Cover (15).

E. Check the component for proper operation. Refer to the CHECK section of
this manual.

7. Assembly of the Articulating Side Guide Rails P/N 84764

NOTE: All item numbers refer to IPL Figure 8, unless specified differently.

A. Attach the Roller Assy (25) to the Rail (70):

(1) Align the Roller Assy (25) inside the Rail (70).

(2) Slide the Headed Pins (20) through the components.

(3) Install the new Cotter Pins (15) on the Headed Pins (20).

B. Attach the Hinge Support (50) to the Rail (70) with the Screws (55), the
Washers (60), and the Nuts (65).

C. Attach the Link (30) to the Hinge Support (50) with the Screw (35), the
Washer (40), and the Nut (45). Torque the fasteners to allow movement of
the Link (30).

D. Refer to the REPAIR section of this manual to replace the adhesive backed
Nameplate (5) and the Cover (10).

E. Check the component for proper operation. Refer to the CHECK section of
this manual.

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8. Assembly of the Increased Height Side Guide Rails P/N 86872

NOTE: All item numbers refer to IPL Figure 9, unless specified differently.

A. Align the Roller Assy (30) inside the Rail (35).

B. Slide the Headed Pins (25) through the components.

C. Install the new Cotter Pins (20) on the Headed Pins (25).

D. Refer to the REPAIR section of this manual to replace the adhesive backed
Nameplate (10) and the Cover (15).

E. Check the component for proper operation. Refer to the CHECK section of
this manual.

9. Assembly of the Ball Mats P/N 86963

NOTE: All item numbers refer to IPL Figure 10, unless specified differently.

A. Attach the Brackets (280) to the Panel Assy (200) with the Rivets (290).

B. P/N 86963-10, -13, -15, -17, -19 ONLY. Attach the Ramp Rails (150) to the
Panel Assy (200) with the Rivets (160).

C. Install the Studs (85), the Retainers (90), the Washers (105), and the Nuts
(115) and hand tighten.

D. Install the Ball Units (50) as follows:

(1) If installed, remove the Setscrews (30) from the Ball Unit (50) hous-
ings. Refer to the CLEANING section of this manual to remove residue
of the Threadlocker (40).

(2) Install the Spring (55), the Ball Unit (50), and the Retainer (45) in the
housing. Make sure the small end of the Spring (55) points DOWN.

(3) Align the Retainer (45) pins with the grooves in the Ball Unit (50) hous-
ing.

(4) Use the Ancra Retainer Installation Tool P/N T228-10 to carefully push
DOWN and turn the Retainer (45) until it locks in the Ball Unit (50)
housing.

(5) Apply two drops of the Threadlocker (40) to the threads of the Set-
screw (30).

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(6) Install the Setscrew (30) in the Ball Unit (50) housing. Turn the Set-
screw (30) until the exposed end is flush or .15 in. (0.4 mm) below the
top surface of the Retainer (45).

E. Refer to the REPAIR section of this manual to replace the adhesive backed
Nameplate (10) and the Cover (15).

F. Check the component for proper operation. Refer to the CHECK section of
this manual.

10. Assembly of the Crosstracks P/N 86974

NOTE: All item numbers refer to IPL Figure 11, unless specified differently.

A. Attach the Outboard Restraint Body (110) to the Crosstrack (300) with the
Bolts (114, 117, 120), the Washers (130), and the Nuts (140).

B. P/N 86974-16, -17, -18, -28 ONLY. Install the Pawl (175) mechanism:

(1) Align the Pawl (175), the Washers (160), and the Springs (165, 170)
on the Crosstrack (300D, 300E, 300H).

(2) Put the Springs (165, 170) ends in the holes in the Pawl (175) and on
the Crosstrack (300D, 300E, 300H).

(3) Slide the Shaft (155) through the components.

(4) Attach the new Retaining Rings (150) on the Shaft (155).

C. P/N 86974-16, -17 ONLY. Apply the Metal Sealer (185) to the new Groove
Pin (180). Install the Plunger (190) together with the Spring (195) in the
Crosstrack (300D) and attach with the Groove Pin (180). Then add one or two
drops of the Sealant (187) to the top and bottom of the Groove Pin (180)
holes.

D. Install the Vertical Restraint (100) mechanism:

(1) Put the Spring (105) on the Outboard Restraint Body (110). Align
opening in the Spring (105) with the tongue on the Body (110).

(2) Install the Bushing (95) inside the Vertical Restraint (100).

(3) Align the Vertical Restraint (100) on the Spring (105). Align opening in
the Spring (105) with the tongue in the Vertical Restraint (100).

(4) Install the Bolt (80) through the components and attach with the
Washer (85) and the Nut (90).

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(5) Make sure that the Vertical Restraint (100) automatically moves to the
center when you turn it side-to-side.

E. P/N 86974-10, -12, -13, -16, -18, -22, -23, -28 ONLY. Install the Roller Assy
(40):

(1) P/N 86974-10, -16 ONLY. Attach the Roller Support Brackets (45) to
the Crosstrack (300, 300D) with the Bolts (55), the Washers (60), and
the Nuts (65).

(2) P/N 86974-12, -13, -18, -22, -23, -28 ONLY. Apply 2-3 drops of the
Threadlocker (70) to the threads of the Bolts (57). Attach the Roller
Support Brackets (50) to the Crosstrack (300B, 300C, 300E, 300F,
300G, 300H) with the Bolts (55).

(3) Align the Roller Assy (40) inside the Roller Support Bracket (45, 50).

(4) Slide the Roller Shaft (35) through the components.

(5) Install the new Cotter Pins (30) on the Roller Shaft (35).

F. Attach the Studs (220, 225), the Washers (250, 260), and the Nuts (280) to
the Crosstrack (300) and hand tighten.

G. Refer to the REPAIR section of this manual to replace the adhesive backed
Nameplate (10) and the Cover (15).

H. Check the component for proper operation. Refer to the CHECK section of
this manual.

11. Assembly of the Crosstracks P/N 86976

NOTE: All item numbers refer to IPL Figure 12, unless specified differently.

A. Install the Pawl (65) mechanism:

(1) Align the Pawl (65), the Lever (70), the Washers (50, 55), and the
Spring (60) on the Crosstrack (300).

(2) Put the ends of the Spring (60) on the inside groove of the Pawl (65)
and below the Lever (70).

(3) Slide the Shafts (40, 45) through the components.

(4) Attach the new Retaining Rings (30, 35) on the Shafts (40, 45).

B. Attach the Studs (220, 225), the Washers (250 thru 265), and the Nuts (280,
285) to the Crosstrack (300) and hand tighten.

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C. Refer to the REPAIR section of this manual to replace the adhesive backed
Nameplate (10) and the Cover (15).

D. Check the component for proper operation. Refer to the CHECK section of
this manual.

12. Assembly of the Door Sill Protectors P/N 86980

NOTE: All item numbers refer to IPL Figure 13, unless specified differently.

A. Align the Rollers (70, 90, 110) in the Door Sills (680 thru 695). Slide the
Shafts (65, 85, 105) through the components.

B. Install the new Cotter Pins (60, 100) on the Shafts (65, 105). Apply the Metal
Sealer (365) to the new Spring Pins (80). Attach the Shafts (85) with the
Spring Pins (80). Then add one or two drops of the Metal Sealer (365) to the
top and bottom of the Spring Pins (80) holes.

C. Attach the Door Sill (680) to the Door Sill (685) and the Door Sill (690) to the
Door Sill (695) with the Bolts (660), Washers (665), and the Nuts (670).

D. Attach the Studs (600 thru 610) to the Hinge Brackets (580, 590) with the
Washers (620 thru 630), and the Nuts (640, 645) and hand tighten.

E. Install the Hinge Brackets (580, 590) to the Door Sills (680 thru 695), align the
holes, and slide in the Shafts (565, 570).

F. Apply the Metal Sealer (365) to the new Groove Pins (560). Attach the Shafts
(565, 570) with the Groove Pins (560). Then add one or two drops of the
Metal Sealer (365) to the top and bottom of the Groove Pin (560) holes.

G. Align the Pivot Roller Body (550) in the Hinge Bracket (590). Slide the Lock-
head Shaft (545) through the components. Install the new Cotter Pins (540)
on the Pivot Roller Body (550).

H. Install the Roller Washer (535), the Pivot Roller (530), the Roller Retainer
(525), and the Washer (520) on the Pivot Roller Body (550). Apply two-three
drops of the Threadlocker (135) to the threads of the Screw (515). Install the
Screw (515) to the preassembled Pivot Roller Body (550).

I. Attach the Support (490) with the Bolts (495), the Washers (500), and the
Nuts (505).

J. Assemble the Guide (485) and the Springs (475, 480) within the Support
(490) and slide the Shaft (470) through the components. Install the new Cot-
ter Pins (465) the Shaft (470).

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K. Install the Plunger (460) flush or below bottom surface of the Latch (455).
Apply two-three drops of the Threadlocker (160) to the threads of the Screw
(450). Install the Latch (455) with the Screw (450) to allow slide fit and posi-
tive indexing on detent locations.

L. Align the Guide (390, 395) with the Springs (380, 385) within the Door Sill and
slide the Shaft (375) through the components.

M. Apply the Metal Sealer (365) to the new Spring Pins (370). Attach the Shaft
(575) with the Spring Pins (370). Then add one or two drops of the Metal
Sealer (365) to the top and bottom of the Spring Pin (370) holes.

N. Apply two drops of the Retaining Compound (435) to the new Spring Pin
(400). Assemble The Spring (415), the Plunger (410), and the Handle (405) in
the Doubler Housing (420) and attach the components with the new Spring
Pin (400).

O. Apply two-three drops of the Threadlocker (160) to the threads of the Bolts
(425). Attach the Housing (420) with assembled components to the Door Sill
with the Bolts (425) and the Washers (430).

P. Apply two drops of the Threadlocker (135) to the threads of the Bolts (350).
Attach the Leg Brackets (340, 345) with the Bolts (350) and the Washers
(355).

Q. Assemble the Leg (325), the Stud (310), the Nuts (315, 320), and Saddle
(305).

NOTE: Final Leg (325) length adjustment to be made at aircraft installation.

R. Install the Plastic Trims (285) onto the Door Sills (680 thru 695).

S. Align the assembled Leg (325) and the Spring (280) at the Leg Brackets (340,
345) and slide in the Shaft (275) through components. Install the new Cotter
Pins (270) on the Shaft (275).

T. Assemble the Rod End Joints (225, 230), the Nuts (235, 240), the Stud (245),
the Link Arm (250), and the Rod Link (255).

U. Slide the Pin (215) in the Leg (325) hole. Install the assembled link on the Pin
(215). Install the new Cotter Pins (200, 205) on the Pin (215).

V. Align the other end of the assembled link with the Hinge Bracket (580) and
slide the Pin (222) through components. Apply the Metal Sealer (365) to the
new Groove Pin (220). Attach the Pin (222) with the Groove Pin (220). Then
add one or two drops of the Metal Sealer (365) to the top and bottom of the
Groove Pin (220) holes.

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NOTE: Final Link Arm (250) length adjustment to be made at aircraft installa-
tion.

W. Attach the Spring Brackets (175) to the Door Sills (680 thru 695) with the
Screws (180), the Washers (185), and the Nuts (190).

X. Apply one drop of the Threadlocker (160) to the threads of the End Fittings
(155). Attach the End Fittings (155) to the Gas Spring (165).

Y. Apply one drop of the Threadlocker (135) to the threads of the Bolt (130A).
Install the assembled Gas Spring (165) using the Bolt (130A), the Spacer
(140), and the Shaft (150). Then install the new Cotter Pins (145) to the Shaft
(150).

Z. Refer to the REPAIR section of this manual to replace the adhesive backed
Nameplate (5), the Decals (15 thru 30), and the Covers (40 thru 50).

AA. Check the component for proper operation. Refer to the CHECK section of
this manual.

13. Assembly of the Lateral Guides P/N 87008

NOTE: All item numbers refer to IPL Figure 14, unless specified differently.

A. Install the Housings (70) in the Base (400).

B. Lower the Skin (60) on top of the Housings (70).

C. Apply one drop of the Threadlocker (35) to the threads of the Screws (55).
Attach the Skin (60) to the Base (400) with the Screws (55).

D. Install the Ball Units (45) as follows:

(1) If installed, remove the Setscrews (30) from the Housings (70). Refer
to the CLEANING section of this manual to remove residue of the
Threadlocker (35).

(2) Install the Spring (50), the Ball Unit (45), and the Retainer (40) in the
Housing (70). Make sure the small end of the Spring (50) points
DOWN.

(3) Align the Retainer (40) pins with the grooves in the Housing (70).

(4) Use the Ancra Retainer Installation Tool T228-10 to carefully push
DOWN and turn the Retainer (40) until it locks in the Housing (70).

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(5) Apply two drops of the Threadlocker (35) to the threads of the Set-
screw (30).

(6) Install the Setscrew (30) in the Housing (70). Turn the Setscrew (30)
until the exposed end is flush or .15 in. (0.4 mm) below the top surface
of the Retainer (40).

E. Install the Release Plunger (95) mechanism:

(1) Apply one-two drops of the Threadlocker (35) to the threads of the
Bolts (110).

(2) Attach the Doubler Housing (105) to the Base (400) with the Bolts
(110) and the Washers (115).

(3) Put the Handle Spring (100) on the Release Plunger (95). Install the
Release Plunger (95) with the Handle Spring (100) through the hole in
the Base (400) and Doubler Housing (105).

(4) Apply one drop of the Retaining Compound (85) to the Spring Pin (80).

(5) Align the holes on the Release Plunger (95) and the Handle (90) and
install the Spring Pin (80) through the components.

F. Align the Roller Assy (320) on the Base (400) and slide the Lockhead Shaft
(310) through the components.

G. Apply one drop of the Retaining Compound (85) to the Spring Pin (305).

H. Align the holes on the Lockhead Shaft (310) and the Base (400) and install
the Spring Pin (305) through the components.

I. Align the Roller Assy (145) on the Frame (185) and slide the Shafts (135,
140) through the components.

J. Align the holes on the Shafts (135, 140) and the Frame (185) and install the
Spring Pins (130) through the components.

K. Align the Link (215) on the Frame (185) and install two Lockhead Shafts
(165).

L. Apply one drop of the Retaining Compound (85) to the Spring Pins (160).

M. Align the holes on the Lockhead Shafts (165) and the Frame (185) and install
the Spring Pins (160) through the components.

N. Apply one-two drops of the Threadlocker (210) to threads of the Bolts (200).

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O. Attach two Dampeners (220) and the Link (295) to each Link (215) with the
Bolts (200) and the Washers (205).

P. Lower the completed Frame (185) on the Base (400). Install the Shaft (180)
with the Torsion Springs (190) and four Washers (195) through the compo-
nents.

Q. Put the ends of the Torsion Springs (190) in the holes on the Frame (185) and
the Base (400).

R. Then install two smaller Shafts (175) in the Base (400).

S. Apply one drop of the Retaining Compound (85) to the Spring Pins (170).

T. Align the holes on the Shafts (175, 180) and the Base (400) and install the
Spring Pins (170) through the components.

U. Connect the Links (295) to the Base (400) with the Lockhead Shafts (290).

V. Apply one drop of the Retaining Compound (85) to the Spring Pins (280).

W. Align the holes on the Blocks (285) and the Base (400) and install the Spring
Pins (280) through the components.

X. Install the Studs (340), the Washers (345, 350), and the Nuts (355) on the
assembly and hand tighten.

Y. Refer to the REPAIR section of this manual to replace the adhesive backed
Nameplate (10) and the Cover (15).

Z. Check the component for proper operation. Refer to the CHECK section of
this manual.

14. Assembly of the Crosstracks P/N 87226

NOTE: All item numbers refer to IPL Figure 15, unless specified differently.

A. Attach the End Base (110) to the Crosstrack (300) with the Bolts (115, 120),
the Washers (130), and the Nuts (140).

B. Attach the Screws (80), the Washers (85), and the Nuts (90) to the End Base
(110) and hand tighten.

C. Install the Roller Assy (40):

(1) Apply two-three drops of the Threadlocker (70) to the threads of the
Bolts (55). Attach the Roller Support Brackets (50) to the Crosstrack
(300) with the Bolts (55).

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(2) Align the Roller Assy (40) inside the Roller Support Bracket (50).

(3) Slide the Roller Shaft (35) through the components.

(4) Install the new Cotter Pins (30) on the Roller Shaft (35).

D. Attach the Studs (225), the Washers (250, 260), and the Nuts (280) to the
Crosstrack (300) and hand tighten.

E. Refer to the REPAIR section of this manual to replace the adhesive backed
Nameplate (10) and the Cover (15).

F. Check the component for proper operation. Refer to the CHECK section of
this manual.

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SPECIAL TOOLS, FIXTURES, AND EQUIPMENT

1. Special Tools, Fixtures, and Equipment

A. Refer to CMM Table 9001 for a list of the special tools, fixtures, and equip-
ment necessary to do maintenance on the component. Refer to the applica-
ble section (shown in the Use column) for data such as ranges, accuracy, and
power ratings for the items.

NOTE: Equivalent substitutes approved by engineering may be used.

Specification or Source or CAGE
Name Use
Part Number Code
Retainer Installation T228-10 V31272 Disassembly,
Tool Assembly
Paint Mixer No specific Commercially Repair
Available
Paint Sprayer No specific Commercially Repair
Available
CMM Table 9001 - Special Tools, Fixtures, and Equipment

2. Materials
A. Refer to CMM Table 9002 for a list of the materials necessary to do mainte-
nance on the component.

NOTE: Equivalent substitutes approved by engineering may be used.

Specification or Part Source or CAGE
Name Use
Number Code
Threadlocker 222, 242 V05972 Assembly
Adhesive 414 V05972 Assembly
Retaining Compound 680 V05972 Assembly
Metal Sealer Coricone 1700 V7Y015 Assembly
Sealant GE5050-12C V01139 Assembly
Abrasive Pad Scotch-Brite, Nylon V52152 Repair
web, Very Fine,
aluminum oxide
Alodine Coating MIL-C-81706, Commercially Repair
Class 1A Available

CMM Table 9002 - Materials (Sheet 1 of 2)

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Specification or Part Source or CAGE

Name Use
Number Code
Low Lint Cloth A-A-59323 Commercially Cleaning, Repair,
Available Assembly
Cleaning Brush 7092T16 V3A054 Cleaning
Isopropyl Alcohol GSL26 Commercially Cleaning, Repair,
Available Assembly
Cleaning Solution FD080, Safety PrepTM, V0K209 Cleaning
NSN6850-01-381-5139
Masking Tape No specific Commercially Repair
Available
Paint Roller or No specific Commercially Repair
Paint Brush Available
Light Green Primer 44GN054 V33461 Repair
Anti-Skid Paint 342-4 V0YY71 Repair
Edge Rail 80025 V31272 Repair
Aluminum Sheet 2014-T6 Commercially Repair
Available
Rivets MS20426AD5-5 Commercially Repair
Available
Aluminum Sheet 2014-T4 or -T3 Commercially Repair
Available
Rivets MS20601AD5W2 Commercially Repair
Available
Zinc Coating ASTM B633, Type II, Commercially Repair
Class Fe/Zn Available
Alodine Coating MIL-C-81706, Commercially Repair
Class 1A Available
Epoxy Adhesive 2216 V52152 Repair
CMM Table 9002 - Materials (Sheet 2 of 2)

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ILLUSTRATED PARTS LIST

1. Introduction
A. General

(1) This Illustrated Parts List (IPL) gives illustrations and a breakdown, in
disassembly sequence, of all assemblies that can be disassembled,
repaired or replaced, and reassembled.

(2) When equipment designators are used in schematics and wiring dia-
grams for electrical and electronic parts, they are shown in the illustra-
tions and the detailed parts list. They are also included in an
Equipment Designator Index.

(3) When the detailed parts list is more than five pages, a Numerical Index
is included in this section.

(4) Supplier (vendor) information includes the name, address, and CAGE
code for each Supplier.

B. Explanation and Usage

(1) The “IPL FIG. & ITEM NO.” column shows the figure and item number
for each part.The figure number is shown once in the header row.
Each part is identified by an item number. A part that is not illustrated
will have a dash (-) before the item number.

(2) Alpha variants, letters A through Z (but not I and O), are used with an
item number to show:

(a) Configuration differences

(b) Alternative parts

(c) Optional parts

(3) The PART NUMBER column shows the part number for each part.

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The true part number will be given in the NOMENCLATURE column

when:

(a) The part number contains characters that are not permitted by
ATA 2000 Specification: for example, a slash (/).

(b) The part number has more than 15 characters.

(c) The part number contains a dash (-) between a number and a
letter.

(4) The AIRLINE PART NO. column is a blank column with space for 11
characters. The airline Customer can use this space to record their
stock numbers.

(5) The NOMENCLATURE column gives this type of information about the
part:

(a) The indenture level shows how the part is related to the next-
higher assembly. For example:

1234567

Assembly

. Detail Parts for Assembly

. Subassembly

. Attaching Parts for the Subassembly

. . Detail Parts for the Subassembly

. . Sub-subassembly

. . Attaching Parts for the Sub-subassembly

. . . Detail Parts for the Sub-subassembly

(b) The full name of the part as shown on the drawing title.

(c) The true part number if not given in the part number column.

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 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

(d) ESDS designation, if the electronic part is electrostatic dis-

charge sensitive.

(e) The values and tolerances permitted for electrical and elec-
tronic parts, such as resistors and capacitors.

(f) The CAGE code for parts made by other vendors; for standard
parts (AN, MS, or NAS), no CAGE code is given.

(g) Applicable service bulletins; PRE SB XXXX shows the initial

configuration and POST SB XXXX identifies assemblies and
parts after the service bulletin has been completed. If a service
bulletin is related to an Airworthiness Directive (AD), then the
AD number is identified as AD XXXX.

(h) Interchangeability data (how the parts relate to each other). A

list of the terms, abbreviations, and definitions is shown below
in Paragraph C.

(i) Figures or CMMs are referenced to show that more breakdown

information is available.

(6) The EFF CODE column is used to show limited interchangeability only.
It identifies different configurations in each figure and shows how parts
relate to item 1 (or an alpha variant of item 1) in that figure only. A
code letter A through Z (but not I and O) identifies each configuration.
The same code is used in this figure to show all parts for a specified
configuration. A blank space shows that the part is used on all configu-
rations in that figure.

(7) The UNITS PER ASSY column gives the quantity of the specified item
number used on one next-higher assembly, subassembly, or sub-sub-
assembly. The letters AR (as required) are for bulk items, and RF indi-
cates that the item is shown for reference only.

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 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

C. Interchangeability Terms, Abbreviations, and Definitions.

Term Abbreviation Definition

Alternate ALT The part agrees with all functional and
structural specifications, but the external
dimensions, connection installation, and/
or mounting provisions are different.
Rework or possible changes can be nec-
essary.
Optional OPT The part is fully interchangeable in form,
fit, and function with other item numbers
shown.
Preferred PRFD The part is preferred over the other
optional parts shown.
Replaced By REPLD The part is replaced and is two-way inter-
changeable with the item number shown
(old part number can replace either old or
new part number when removed).
Replaces REPLS The part replaces and is two-way inter-
changeable with the item number shown
(new part number is acceptable replace-
ment for old or new part number).
Superseded SUPSD BY The part is superseded by and is one-way
By interchangeable with the item number
shown (old part number can be used as
replacement only where old part was
installed).
Supersedes SUPSDS The part supersedes and is one-way
interchangeable with the item number
shown (new part number is acceptable
replacement for old or new part number).
Service PRE SB Identifies when a service bulletin (SB) has
Bulletins POST SB an effect on a part. PRE shows the condi-
RWK SB tion of the part before the work in the ser-
vice bulletin is done; POST shows the
condition after the work is done; RWK
shows that the part is reworked by the
service bulletin.

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 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

D. Abbreviations and Definitions

Abbreviation Definition
AR As Required
ASSY Assembly
CMM Component Maintenance Manual
EC Explanation Code
FIG Figure
FWD Forward
IPL Illustrated Parts List
LH Left Hand
LTD Limited
MFD Manufactured
NHA Next-Higher Assembly
NO. Number
OPP Opposite
P/N Part Number
RH Right Hand
RF Reference

E. Vendors (Suppliers)

V31272 Ancra International

601 S. Vincent Ave.
Azusa, CA 91702

V0U252 M.D.C. Aircraft Service

DBA Mercury International
1825 Surveyor Ave., 102
Simi Valley, CA 93063

V0YY71 WLS Coatings Inc.

13413 S. Broadway
Los Angeles, CA 90061

V01139 Momentive Performance Materials

22 Corporate Woods Blvd.
Albany, NY 12211

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 COMPONENT MAINTENANCE MANUAL
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V01599 Reid Supply Company

2265 Black Creek Rd.
Muskegon, MI 49444

V05693 Cherry Textron Inc.

1224 E. Warner Ave.
Santa Ana, CA 92705

V05972 Loctite Corporation

1001 Trout Brook Crossing,
Rocky Hill, CT 06067

V07382 Rotor Clip Company Inc.

187 Davidson Ave.
Somerset, NJ 08873

V1A699 Lee Spring Company

140 58th St., Ste 3C
Brooklyn, NY 11220

V33461 PRC-Desoto International Inc.

DBA PPG Aerospace, Deft
17451 Von Karman Ave.
Irvine, CA 92614

V3A054 McMaster-Carr Supply Company

9630 Norwalk Blvd.
Santa Fe Springs, CA 90670

V52152 3M Company
3M Ctr
Saint Paul, MN 55144

V56988 Matthew Warren Inc.

Century Spring Corp.
222 E. 16th St.
Los Angeles, CA 90015

V73957 Groov-Pin Corp.

331 Farnum Pike
Smithfield, RI 02917

V7Y015 Corro Therm Inc.

175 Philmont Ave.
Feasterville, PA 19053

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 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NUMERICAL INDEX
The Numerical Index cross-references part numbers with figures, item numbers, and quan-
tity in that figure.

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
222 3 95 AR
222 10 40 AR
222 13 160 AR
222 14 35 AR
242 11 70 AR
242 13 135 AR
242 14 210 AR
242 15 70 AR
414 4 30 AR
680 13 435 AR
680 14 85 AR
40349-10 10 90 5
40349-10 10 -90A 6
40349-10 10 -90B 4
40349-10 10 -90C 8
40349-10 10 -90D 7
40350-10 10 85 5
40350-10 10 -85A 6
40350-10 10 -85B 4
40350-10 10 -85C 8
40350-10 10 -85D 7
40361-15 11 225 2
40361-15 15 225 2
40361-17 13 610 1
40361-17 14 340 4
40361-59 11 220 2
40361-59 12 225 1
43356-21 11 250 2
43356-21 12 250 1
43356-21 13 620 1
43356-21 15 250 2
43356-32 14 345 4
5/64 X 5/8-T-HD 5 50 12
5/64 X 5/8-T-HD 5 -50A 14
5/64 X 5/8-T-HD 5 -50B 6
5/64 X 5/8-T-HD 5 -50C 4
5/64 X 5/8-T-HD 5 -50D 10

- NOT ILLUSTRATED

85550-H
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 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
60745K241-RH 13 225 3
60745K242-LH 13 230 3
80004-10 1 30 66
80004-10 1A 30 66
80004-10 3 -1 RF
80004-11 1 35 6
80004-11 1A 35 6
80004-11 3 -1A RF
80004-43 1 40 6
80004-43 1A 40 6
80004-43 3 -1B RF
80010-11 11 35 2
80010-11 11 -35A 8
80010-11 15 35 2
80012-10 3 115 1
80012-11 3 -115A 1
80012-24 3 -115B 1
80014-10 3 45 1
80015-10 3 60 1
80018-10 3 35 1
80018-11 3 40 1
80019-10 3 50 1
80019-11 3 55 1
80021-10 3 25 2
80022-10 3 100 2
80028-10 10 45 50
80028-10 10 -45A 51
80028-10 10 -45B 39
80028-10 10 -45C 33
80028-10 10 -45D 87
80028-10 10 -45E 79
80028-10 14 40 2
80031-10 10 280 5
80031-10 10 -280A 6
80031-10 10 -280B 4
80031-10 10 -280C 8
80031-10 10 -280D 7
80039-10 5 20 2
80039-10 5 -20A 1
80076-11 12 65 1

- NOT ILLUSTRATED

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 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
80076-11 12 -65A 2
80077-10 12 70 1
80077-10 12 -70A 2
80078-12 11 155 1
80078-12 12 40 1
80078-12 12 -40A 2
80078-13 12 45 1
80078-13 12 -45A 2
80115-17 13 85 2
80115-21 13 150 3
80115-22 13 65 19
80120-10 13 90 2
80166-10 11 95 1
80167-10 11 105 1
80222-10 12 60 1
80222-10 12 -60A 2
80339-14 10 150A 1
80339-35 10 150 1
80339-39 10 150B 1
80352-10 10 55 50
80352-10 10 -55A 51
80352-10 10 -55B 39
80352-10 10 -55C 33
80352-10 10 -55D 87
80352-10 10 -55E 79
80352-10 14 50 2
80423-10 14 45 2
80423-11 10 50 50
80423-11 10 -50A 51
80423-11 10 -50B 39
80423-11 10 -50C 33
80423-11 10 -50D 87
80423-11 10 -50E 79
80471-11 13 275 3
80576-10 1 50 12
80576-10 1A 50 12
80576-10 4 -1 RF
80681-10 4 60 1
80681-11 4 65 1
80682-10 4 20 2

- NOT ILLUSTRATED

85550-H
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Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
80704-11 3 110 2
80876-30 13 45 3
80876-32 13 50 1
80879-10 7 30 2
80879-10 9 30 2
80957-10 3 75 2
80957-10 3 75A 1
81011-10 3 80 2
81011-10 3 80A 1
81011-11 14 320 2
81028-10 13 15 1
81028-11 13 20 1
81028-13 13 25 1
81028-14 13 30 1
81245-19 14 165 4
81245-20 14 310 1
81384-10 1 60 68
81384-10 1A 60 68
81384-10 5 -1 RF
81384-110 5 65 1
81384-112 5 -65A 1
81384-113 5 -65B 1
81384-114 5 -65C 1
81384-115 5 -65D 1
81384-118 5 -65E 1
81384-12 1 65 4
81384-12 1A 65 4
81384-12 5 -1A RF
81384-13 1 70 72
81384-13 1 71 2
81384-13 1 71A 2
81384-13 1A 70 68
81384-13 1A 71 2
81384-13 1A 71A 2
81384-13 5 -1B RF
81384-14 1 75 64
81384-14 1 76 2
81384-14 1A 75 68
81384-14 1A 76 2
81384-14 5 -1C RF

- NOT ILLUSTRATED

85550-H
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Unauthorized Use Prohibited 25-52-16 Pg.10010
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
81384-14 16 -30 4
81384-15 1 80 4
81384-15 1A 80 4
81384-15 5 -1D RF
81384-18 1 85 12
81384-18 1 86 2
81384-18 1 86A 2
81384-18 1A 85 12
81384-18 1A 86 2
81384-18 1A 86A 2
81384-18 5 -1E RF
81394-10 5 60 12
81394-10 5 -60A 14
81394-10 5 -60B 6
81394-10 5 -60C 4
81394-10 5 -60D 10
81394-10 11 40 2
81394-10 11 -40A 8
81394-10 15 40 2
81395-10 5 55 12
81395-10 5 -55A 14
81395-10 5 -55B 6
81395-10 5 -55C 4
81395-10 5 -55D 10
81673-11 13 605 3
81673-12 12 220 D
81673-15 12 -220A 2
81673-20 13 600 13
81858-10 10 30 50
81858-10 10 -30A 51
81858-10 10 -30B 39
81858-10 10 -30C 33
81858-10 10 -30D 87
81858-10 10 -30E 79
81858-10 14 30 2
81956-13 3 10 1
81956-13 4 10 1
81956-13 5 10 1
81956-13 6 10 1
81956-13 7 10 1

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10011
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
81956-13 8 5 1
81956-13 9 10 1
81956-13 10 10 1
81956-13 11 10 1
81956-13 12 10 1
81956-13 13 5 1
81956-13 14 10 1
81956-13 15 10 1
81956-20 3 15 1
81956-20 4 15 1
81956-20 5 15 1
81956-20 6 15 1
81956-20 7 15 1
81956-20 8 10 1
81956-20 9 15 1
81956-20 10 15 1
81956-20 11 15 1
81956-20 12 15 1
81956-20 13 40 1
81956-20 14 15 1
81956-20 15 15 1
82012-12 13 545 1
82012-15 14 290 2
82087-13 13 105 7
82087-14 13 375 1
82242-13 13 470 1
83421-12 13 305 3
83422-11 13 245 3
83422-12 13 310 3
83423-13 13 325 3
83424-11 13 250 3
83425-10 13 340 3
83425-11 13 345 3
83427-10 13 175 3
83428-14 13 390 1
83428-15 13 395 1
83428-16 13 485 1
83445-10 13 215 3
83446-10 13 -130 3
83446-12 13 130A 3

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10012
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
83450-11 13 222 3
83450-11 13 565 1
83450-12 13 570 6
83456-10 8 50 1
83504-10 13 255 3
83646-11 15 110 1
83663-10 11 175 1
83665-10 11 165 1
83665-11 11 170 1
83672-13 13 490 1
83879-12 11 45 2
83879-14 11 50 2
83879-14 11 -50A 8
83879-14 15 50 2
84021-40 1 100 6
84021-40 1A 100 6
84021-40 6 -1 RF
84021-41 1 105 2
84021-41 1A 105 2
84021-41 6 -1A RF
84021-45 1 110 6
84021-45 1A 110 6
84021-45 6 -1B RF
84021-50 1 115 4
84021-50 1A 115 4
84021-50 6 -1C RF
84021-51 1 120 6
84021-51 1A 120 6
84021-51 6 -1D RF
84021-52 1 125 6
84021-52 1A 125 6
84021-52 6 -1E RF
84021-54 1 130 2
84021-54 1A 130 2
84021-54 6 -1F RF
84021-59 1 135 2
84021-59 1A 135 2
84021-59 6 -1G RF
84021-60 1 140 2
84021-60 1A 140 2

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10013
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
84021-60 6 -1H RF
84021-61 1 145 2
84021-61 1A 145 2
84021-61 6 -1J RF
84021-75 1 150 6
84021-75 1A 150 6
84021-75 6 -1K RF
84021-78 1 155 2
84021-78 1A 155 2
84021-78 6 -1L RF
84022-47 1 170 4
84022-47 1A 170 4
84022-47 7 -1 RF
84022-49 1 175 2
84022-49 1A 175 2
84022-49 7 -1A RF
84037-10 3 105 2
84041-11 11 100 1
84077-10 14 185 1
84078-11 14 295 2
84079-10 14 215 2
84081-10 13 420 1
84081-10 14 105 1
84082-10 13 410 1
84082-10 14 95 1
84083-10 14 70 2
84084-10 13 405 1
84084-10 14 90 1
84085-10 14 220 4
84095-10 14 60 1
84099-10 14 135 3
84099-10 14 175 2
84099-11 14 140 1
84099-12 14 -175A 2
84099-13 14 180 1
84100-10 14 190 2
84100-12 13 380 2
84100-13 13 385 2
84103-10 14 145 4
84106-10 13 475 1

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10014
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
84106-11 13 480 1
84112-14 13 550 1
84116-13 13 530 1
84117-11 13 525 1
84119-11 13 535 1
84120-47 7 35 1
84120-49 7 -35A 1
84120-53 9 35 1
84120-59 9 -35A 1
84120-61 9 -35B 1
84120-62 9 -35C 1
84121-40 6 40 1
84121-41 6 -40A 1
84121-45 6 -40B 1
84121-50 6 -40C 1
84121-51 6 -40D 1
84121-52 6 -40E 1
84121-54 6 -40F 1
84121-59 6 40G 1
84121-60 6 -40H 1
84121-61 6 -40J 1
84121-75 6 -40K 1
84121-78 6 -40L 1
84123-10 6 30 2
84123-10 6 -30A 1
84123-10 8 25 2
84347-11 11 190 1
84362-10 13 110 7
84673-10 11 -110A 1
84673-12 11 110 1
84755-10 8 30 1
84755-11 8 -30A 1
84761-16 8 70 1
84761-18 8 -70A 1
84764-16 1 180 1
84764-16 1A 180 1
84764-16 8 -1 RF
84764-18 1 185 1
84764-18 1A 185 1
84764-18 8 -1A RF

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10015
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
85034-11 2 40 1
85034-11 2A 40 1
85034-12 2 45 1
85034-12 2A 45 1
85034-13 2 50 1
85034-13 2A 50 1
85034-14 2 55 1
85034-14 2A 55 1
85034-15 2 60 1
85034-15 2A 60 1
85034-16 2 65 1
85034-16 2A 65 1
85034-17 2 70 1
85034-17 2A 70 1
85034-18 2 75 1
85034-18 2A 75 1
85034-19 2 80 1
85034-19 2A 80 1
85034-20 2 85 1
85034-20 2A 85 1
85034-42 2A 150 1
85034-42 16 -225 1
85034-43 2A 155 1
85034-43 16 -230 1
85034-44 2A 160 1
85034-44 16 -235 1
85034-45 2A 165 1
85034-45 16 -240 1
85034-46 2A 170 1
85034-46 16 -245 1
85034-62 2 90 1
85034-62 2A 90 1
85034-63 2 95 1
85034-63 2A 95 1
85034-64 2 100 1
85034-64 2A 100 1
85034-65 2 105 1
85034-65 2A 105 1
85334-10 2 20 1
85334-13 2A 20 1

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10016
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
85334-13 16 -210 1
85336-10 2 25 1
85336-12 2A 25 1
85336-12 16 -220 1
85338-10 1 -20 1
85338-10 2 -1 1
85338-12 1A -20 1
85338-12 2A -1 1
85338-90 16 -200 1
85550-10 1 -1 RF
85550-10 1 -1A RF
85550-12 1A -1 RF
85550-12 1A -1A RF
85550-90 1 -800 RF
85550-90 16 -1 RF
86018-10 13 280 3
86099-10 13 455 1
8672K42 13 285 3
86872-11 1 200 7
86872-11 1A 200 7
86872-11 9 -1 RF
86872-14 1 205 1
86872-14 1A 205 1
86872-14 9 -1A RF
86872-19 1 210 2
86872-19 1A 210 2
86872-19 9 -1B RF
86872-20 1 215 1
86872-20 1A 215 1
86872-20 9 -1C RF
86963-01 10 -200 1
86963-02 10 -200A 1
86963-03 10 -200B 1
86963-04 10 -200C 1
86963-05 10 -200D 1
86963-06 10 -200E 1
86963-07 10 -200F 1
86963-08 10 -200G 1
86963-09 10 -200H 1
86963-10 1 230 1

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10017
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
86963-10 10 -1 RF
86963-11 1 235 1
86963-11 10 -1A RF
86963-12 1 240 2
86963-12 1A 240 2
86963-12 10 -1B RF
86963-13 1 245 2
86963-13 1A 245 2
86963-13 10 -1C RF
86963-14 1 250 1
86963-14 1A 250 1
86963-14 10 -1D RF
86963-15 1 255 1
86963-15 1A 255 1
86963-15 10 -1E RF
86963-16 1 260 1
86963-16 1A 260 1
86963-16 10 -1F RF
86963-17 1 265 1
86963-17 1A 265 1
86963-17 10 -1G RF
86963-18 1A 230 1
86963-18 10 -1H RF
86963-18 16 -40 1
86963-19 1A 235 1
86963-19 10 -1J RF
86963-19 16 -45 1
86963-20 10 -200J 1
86966-10 14 285 2
86974-10 1 280 76
86974-10 1A 280 52
86974-10 11 -1 RF
86974-11 1 285 8
86974-11 11 -1A RF
86974-12 1 290 16
86974-12 1A 290 16
86974-12 11 -1B RF
86974-13 1 295 12
86974-13 1A 295 8
86974-13 11 -1C RF

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10018
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
86974-16 1A 298 24
86974-16 11 -1D RF
86974-16 16 -60 24
86974-17 1A 285 8
86974-17 11 -1E RF
86974-17 16 -65 8
86974-18 1A 300 4
86974-18 11 -1F RF
86974-18 16 -70 D
86974-22 1 291 16
86974-22 1 291A 16
86974-22 1A 291 16
86974-22 1A 291A 16
86974-22 11 -1G RF
86974-23 1 296 12
86974-23 1 296A 12
86974-23 1A 296 8
86974-23 1A 296A 8
86974-23 11 -1H RF
86974-28 1A 301 4
86974-28 1A 301A 4
86974-28 11 -1J RF
86974-28 16 -70A 4
86976-10 1 305 7
86976-10 12 -1 RF
86976-11 1A 305 7
86976-11 12 -1A RF
86976-11 16 -80 7
86977-10 1 315 1
86977-10 1A 315 1
86977-11 1 320 1
86977-11 1A 320 1
86980-10 1 330 1
86980-10 1A 330 1
86980-10 13 -1 RF
86980-11 1 335 1
86980-11 1A 335 1
86980-11 13 -1A RF
87003-10 14 400 1
87003-11 14 -400A 1

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10019
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
87008-10 1 350 2
87008-10 1A 350 2
87008-10 14 -1 RF
87008-11 1 355 1
87008-11 1A 355 1
87008-11 14 -1A RF
87034-10 11 300 1
87034-11 11 -300A 1
87039-10 12 300 1
87039-12 12 300A 1
87143-10 13 680 1
87143-11 13 685 1
87143-12 13 690 1
87143-13 13 695 1
87214-10 11 300B 1
87214-11 15 300 1
87214-12 11 -300C 1
87214-14 11 300E 1
87214-15 11 300D 1
87214-20 11 300F 1
87214-22 11 -300G 1
87214-24 11 300H 1
87226-10 1 370 6
87226-10 1A 370 6
87226-10 15 -1 RF
87264-10 13 580 3
87264-11 13 -580A 3
87264-12 13 590 1
87264-13 13 -590A 1
9416K15 13 165 3
9416K84 13 155 6
AN3-3A 13 425 2
AN3-3A 14 110 2
AN3-5A 5 25 2
AN3-5A 5 -25A 1
AN565C1032H6 3 90 2
CORICONE 1700 11 185 AR
CORICONE 1700 13 365 AR
CR3242-6-03 10 160 9
CR3242-6-03 10 -160A 15

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10020
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
GE5050-12C 11 187 AR
GP-24-093-875-78 11 180 1
GP-24-125-0875-72 13 220 3
GP-24-125-0875-72 13 560 7
LC-020C-4 11 195 1
MS20392-3C43 6 25 2
MS20392-3C43 6 -25A 1
MS20392-3C43 8 20 2
MS20392-4C49 7 25 2
MS20392-4C49 9 25 2
MS20426AD6-6 10 290 20
MS20426AD6-6 10 -290A 24
MS20426AD6-6 10 -290B 16
MS20426AD6-6 10 -290C 32
MS20426AD6-6 10 -290D 28
MS20995C32 13 -288 AR
MS21042-3 11 65 4
MS21042-4 1 415 130
MS21042-4 1A 415 130
MS21042-4 11 140 4
MS21042-4 13 190 9
MS21042-4 13 505 4
MS21042-4 13 640 16
MS21042-4 15 90 2
MS21042-4 15 140 2
MS21042-5 11 90 1
MS21042-5 11 280 2
MS21042-5 13 670 6
MS21042-5 15 280 2
MS21042-6 10 115 5
MS21042-6 10 -115A 6
MS21042-6 10 -115B 4
MS21042-6 10 -115C 8
MS21042-6 10 -115D 7
MS21042-6 13 645 1
MS21042-6 14 355 4
MS21042L3 4 50 1
MS21042L3 5 35 2
MS21042L3 5 -35A 1
MS21045-4 12 285 2

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10021
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
MS21045-5 12 280 1
MS24665-132 3 70 2
MS24665-132 3 70A 1
MS24665-132 6 20 2
MS24665-132 6 -20A 1
MS24665-132 8 15 2
MS24665-132 11 30 4
MS24665-132 11 -30A 16
MS24665-132 15 30 4
MS24665-281 3 20 4
MS24665-283 13 465 2
MS24665-300 7 20 2
MS24665-300 9 20 2
MS24665-300 13 60 38
MS24665-300 13 145 6
MS24665-300 13 200 3
MS24665-300 13 270 6
MS24665-300 13 540 2
MS24665-302 13 100 14
MS24665-302 13 205 3
MS24694-S113 1 400 96
MS24694-S113 1A 400 96
MS24694-S114 1 405 34
MS24694-S114 1A 405 34
MS27039-4-08 13 515 1
MS39086-119 13 400 1
MS39086-119 14 80 1
MS39086-119 14 160 4
MS39086-119 14 305 1
MS39086-131 14 280 4
MS39086-145 14 130 4
MS39086-145 14 170 3
MS39086-436 13 80 2
MS39086-436 13 370 1
MS51964-43 10 -35 50
MS51964-43 10 -35A 51
MS51964-43 10 -35B 39
MS51964-43 10 -35C 33
MS51964-43 10 -35D 87
MS51964-43 10 -35E 79

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10022
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
NAS1149C0532R 11 160 2
NAS1149C0832R 14 195 4
NAS1149D0516H 3 30 4
NAS1149D0532H 12 50 2
NAS1149D0532H 12 -50A 4
NAS1149D0632H 12 55 2
NAS1149D0632H 12 -55A 4
NAS1149F0332P 4 45 1
NAS1149F0332P 5 30 2
NAS1149F0332P 5 -30A 1
NAS1149F0332P 11 60 4
NAS1149F0332P 13 430 2
NAS1149F0332P 14 115 2
NAS1149F0432P 1 410 130
NAS1149F0432P 1A 410 130
NAS1149F0432P 11 130 4
NAS1149F0432P 12 265 2
NAS1149F0432P 13 185 9
NAS1149F0432P 13 500 4
NAS1149F0432P 13 520 1
NAS1149F0432P 13 625 16
NAS1149F0432P 14 205 6
NAS1149F0432P 15 85 2
NAS1149F0432P 15 130 2
NAS1149F0463P 8 40 1
NAS1149F0463P 8 60 2
NAS1149F0532P 11 85 1
NAS1149F0532P 11 260 2
NAS1149F0532P 12 260 1
NAS1149F0532P 13 355 12
NAS1149F0532P 13 665 6
NAS1149F0532P 15 260 2
NAS1149F0632P 10 105 5
NAS1149F0632P 10 -105A 6
NAS1149F0632P 10 -105B 4
NAS1149F0632P 10 -105C 8
NAS1149F0632P 10 -105D 7
NAS1149F0632P 13 630 1
NAS1149F0632P 14 350 4
NAS43DD5-20A 13 140 3

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10023
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED
NAS509-6 13 240 6
NAS509-8 13 320 3
NAS509L6 13 235 6
NAS509L8 13 315 3
NAS517-3-0 14 55 6
NAS517-4-18 8 35 1
NAS517-4-21 8 55 2
NAS517-4-3 13 180 9
NAS517-4-6 15 80 2
NAS601-7 13 450 D
NAS602-7P 13 -450A 1
NAS6203-5 11 57 4
NAS6203-5 11 -57A 16
NAS6203-5 15 55 4
NAS6203-7 11 55 4
NAS6204-10 11 114 2
NAS6204-12 13 495 4
NAS6204-14 11 117 2
NAS6204-42 15 120 1
NAS6204-54 15 115 1
NAS6204-6 14 200 6
NAS6204-9 11 120 4
NAS6205-11 11 80 1
NAS6205-5 13 350 12
NAS6205-8 13 660 6
NAS6703-2 4 40 1
NAS679A4 8 45 1
NAS679A4 8 65 2
QQ-67 13 415 1
QQ-67 14 100 1
SH-37STZD 12 35 2
SH-37STZD 12 -35A 4
SHM-31STZD 11 150 2
SHM-31STZD 12 30 2
SHM-31STZD 12 -30A 4
X4A-N 13 460 1

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10024
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10025
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

FIGURE ITEM TOTAL

P/N AIRLINE P/N
NUMBER NUMBER REQUIRED

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10026
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

A321-200 Cargo Handling System, P/N 85550-10

Figure 1 (Sheet 1 of 6)

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10027
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

A321-200 Cargo Handling System, P/N 85550-10

Figure 1 (Sheet 2 of 6)

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10028
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

A321-200 Cargo Handling System, P/N 85550-10

Figure 1 (Sheet 3 of 6)

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10029
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

A321-200 Cargo Handling System, P/N 85550-10

Figure 1 (Sheet 4 of 6)

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10030
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

A321-200 Cargo Handling System, P/N 85550-10

Figure 1 (Sheet 5 of 6)

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10031
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

A321-200 Cargo Handling System, P/N 85550-10

Figure 1 (Sheet 6 of 6)

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10032
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

PART AIRLINE NOMENCLATURE USAGE UNITS

FIG PER
ITEM NUMBER PART NO. 1234567 CODE
ASSY
1
-1 85550-10 CARGO HANDLING SYSTEM, A RF
A321-200
(RWK SB 85550-25-02)
(MSNS 1238, 1250 ONLY)
-1A 85550-10 CARGO HANDLING SYSTEM, B RF
A321-200
(SUBS MSNS ONLY)
-20 85338-10 . PLACARD INSTL, WALL 1
(SEE IPL FIGURE 2 FOR DETAILS)
30 80004-10 . LOCK ASSY, CARGO 66
(SEE IPL FIGURE 3 FOR DETAILS)
35 80004-11 . LOCK ASSY, CARGO 6
(SEE IPL FIGURE 3 FOR DETAILS)
40 80004-43 . LOCK ASSY, CARGO 6
(SEE IPL FIGURE 3 FOR DETAILS)
50 80576-10 . STOP ASSY, END 12
(SEE IPL FIGURE 4 FOR DETAILS)
60 81384-10 . RAIL ASSY, ROLLER 68
(SEE IPL FIGURE 5 FOR DETAILS)
65 81384-12 . RAIL ASSY, ROLLER 4
(SEE IPL FIGURE 5 FOR DETAILS)
70 81384-13 . RAIL ASSY, ROLLER 72
(SEE IPL FIGURE 5 FOR DETAILS)
71 81384-13 . RAIL ASSY, ROLLER A 2
(SEE IPL FIGURE 5 FOR DETAILS)
(POST SB 85550-25-02)
(SUPSDS ITEM 76)
71A 81384-13 . RAIL ASSY, ROLLER B 2
(SEE IPL FIGURE 5 FOR DETAILS)
75 81384-14 . RAIL ASSY, ROLLER 64
(SEE IPL FIGURE 5 FOR DETAILS)
76 81384-14 . RAIL ASSY, ROLLER A 2
(SEE IPL FIGURE 5 FOR DETAILS)
(PRE SB 85550-25-02)
(SUPSD BY ITEM 71)
80 81384-15 . RAIL ASSY, ROLLER 4
(SEE IPL FIGURE 5 FOR DETAILS)
85 81384-18 . RAIL ASSY, ROLLER 12
(SEE IPL FIGURE 5 FOR DETAILS)
86 81384-18 . RAIL ASSY, ROLLER A 2
(SEE IPL FIGURE 5 FOR DETAILS)

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10033
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NOMENCLATURE UNITS
FIG PART AIRLINE USAGE
PER
ITEM NUMBER PART NO. 1234567 CODE ASSY
1
(POST SB 85550-25-02)
86A 81384-18 . RAIL ASSY, ROLLER B 2
(SEE IPL FIGURE 5 FOR DETAILS)
100 84021-40 . RAIL ASSY, SIDE GUIDE 6
(SEE IPL FIGURE 6 FOR DETAILS)
105 84021-41 . RAIL ASSY, SIDE GUIDE 2
(SEE IPL FIGURE 6 FOR DETAILS)
110 84021-45 . RAIL ASSY, SIDE GUIDE 6
(SEE IPL FIGURE 6 FOR DETAILS)
115 84021-50 . RAIL ASSY, SIDE GUIDE 4
(SEE IPL FIGURE 6 FOR DETAILS)
120 84021-51 . RAIL ASSY, SIDE GUIDE 6
(SEE IPL FIGURE 6 FOR DETAILS)
125 84021-52 . RAIL ASSY, SIDE GUIDE 6
(SEE IPL FIGURE 6 FOR DETAILS)
130 84021-54 . RAIL ASSY, SIDE GUIDE 2
(SEE IPL FIGURE 6 FOR DETAILS)
135 84021-59 . RAIL ASSY, SIDE GUIDE 2
(SEE IPL FIGURE 6 FOR DETAILS)
140 84021-60 . RAIL ASSY, SIDE GUIDE 2
(SEE IPL FIGURE 6 FOR DETAILS)
145 84021-61 . RAIL ASSY, SIDE GUIDE 2
(SEE IPL FIGURE 6 FOR DETAILS)
150 84021-75 . RAIL ASSY, SIDE GUIDE 6
(SEE IPL FIGURE 6 FOR DETAILS)
155 84021-78 . RAIL ASSY, SIDE GUIDE 2
(SEE IPL FIGURE 6 FOR DETAILS)
170 84022-47 . RAIL ASSY, INCREASED HEIGHT 4
SIDE GUIDE
(SEE IPL FIGURE 7 FOR DETAILS)
175 84022-49 . RAIL ASSY, INCREASED HEIGHT 2
SIDE GUIDE
(SEE IPL FIGURE 7 FOR DETAILS)
180 84764-16 . RAIL ASSY, ARTICULATING 1
SIDE GUIDE
(SEE IPL FIGURE 8 FOR DETAILS)
185 84764-18 . RAIL ASSY, ARTICULATING 1
SIDE GUIDE
(SEE IPL FIGURE 8 FOR DETAILS)
200 86872-11 . RAIL ASSY, INCREASED HEIGHT 7
SIDE GUIDE
(SEE IPL FIGURE 9 FOR DETAILS)

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10034
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NOMENCLATURE UNITS
FIG PART AIRLINE USAGE
PER
ITEM NUMBER PART NO. 1234567 CODE ASSY
1
205 86872-14 . RAIL ASSY, INCREASED HEIGHT 1
SIDE GUIDE
(SEE IPL FIGURE 9 FOR DETAILS)
210 86872-19 . RAIL ASSY, INCREASED HEIGHT 2
SIDE GUIDE
(SEE IPL FIGURE 9 FOR DETAILS)
215 86872-20 . RAIL ASSY, INCREASED HEIGHT 1
SIDE GUIDE
(SEE IPL FIGURE 9 FOR DETAILS)
230 86963-10 . MAT ASSY, BALL 1
(SEE IPL FIGURE 10 FOR DETAILS)
235 86963-11 . MAT ASSY, BALL 1
(SEE IPL FIGURE 10 FOR DETAILS)
240 86963-12 . MAT ASSY, BALL 2
(SEE IPL FIGURE 10 FOR DETAILS)
245 86963-13 . MAT ASSY, BALL 2
(SEE IPL FIGURE 10 FOR DETAILS)
250 86963-14 . MAT ASSY, BALL 1
(SEE IPL FIGURE 10 FOR DETAILS)
255 86963-15 . MAT ASSY, BALL 1
(SEE IPL FIGURE 10 FOR DETAILS)
260 86963-16 . MAT ASSY, BALL 1
(SEE IPL FIGURE 10 FOR DETAILS)
265 86963-17 . MAT ASSY, BALL 1
(SEE IPL FIGURE 10 FOR DETAILS)
280 86974-10 . CROSSTRACK ASSY 76
(SEE IPL FIGURE 11 FOR DETAILS)
285 86974-11 . CROSSTRACK ASSY 8
(SEE IPL FIGURE 11 FOR DETAILS)
290 86974-12 . CROSSTRACK ASSY A 16
(SEE IPL FIGURE 11 FOR DETAILS)
(PRE SB 85550-25-02)
(SUPSD BY ITEM 291)
291 86974-22 . CROSSTRACK ASSY A 16
(SEE IPL FIGURE 11 FOR DETAILS)
(POST SB 85550-25-02)
(SUPSDS ITEM 290)
291A 86974-22 . CROSSTRACK ASSY B 16
(SEE IPL FIGURE 11 FOR DETAILS)
295 86974-13 . CROSSTRACK ASSY A 12
(SEE IPL FIGURE 11 FOR DETAILS)
(PRE SB 85550-25-02)

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10035
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NOMENCLATURE UNITS
FIG PART AIRLINE USAGE
PER
ITEM NUMBER PART NO. 1234567 CODE ASSY
1
(SUPSD BY ITEM 296)
296 86974-23 . CROSSTRACK ASSY A 12
(SEE IPL FIGURE 11 FOR DETAILS)
(POST SB 85550-25-02)
(SUPSDS ITEM 295)
296A 86974-23 . CROSSTRACK ASSY B 12
(SEE IPL FIGURE 11 FOR DETAILS)
305 86976-10 . CROSSTRACK ASSY 7
(SEE IPL FIGURE 12 FOR DETAILS)
315 86977-10 . RAIL 1
320 86977-11 . RAIL 1
330 86980-10 . PROTECTOR ASSY, DOOR SILL 1
(SEE IPL FIGURE 13 FOR DETAILS)
335 86980-11 . PROTECTOR ASSY, DOOR SILL 1
(SEE IPL FIGURE 13 FOR DETAILS)
350 87008-10 . GUIDE ASSY, LATERAL 2
(SEE IPL FIGURE 14 FOR DETAILS)
355 87008-11 . GUIDE ASSY, LATERAL 1
(SEE IPL FIGURE 14 FOR DETAILS)
370 87226-10 . CROSSTRACK ASSY 6
(SEE IPL FIGURE 15 FOR DETAILS)
400 MS24694S113 . SCREW 96
(TRUE P/N IS MS24694-S113)
405 MS24694S114 . SCREW 34
(TRUE P/N IS MS24694-S114)
410 NAS1149F0432P . WASHER 130
415 MS21042-4 . NUT 130
-800 85550-90 KIT, CONVERSION RF
(SEE IPL FIGURE 16 FOR DETAILS)

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10036
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

A321-200 Cargo Handling System, P/N 85550-12

Figure 1A (Sheet 1 of 6)

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10037
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

A321-200 Cargo Handling System, P/N 85550-12

Figure 1A (Sheet 2 of 6)

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10038
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

A321-200 Cargo Handling System, P/N 85550-12

Figure 1A (Sheet 3 of 6)

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10039
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

A321-200 Cargo Handling System, P/N 85550-12

Figure 1A (Sheet 4 of 6)

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10040
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

A321-200 Cargo Handling System, P/N 85550-12

Figure 1A (Sheet 5 of 6)

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10041
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

A321-200 Cargo Handling System, P/N 85550-12

Figure 1A (Sheet 6 of 6)

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10042
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

PART AIRLINE NOMENCLATURE USAGE UNITS

FIG PER
ITEM NUMBER PART NO. 1234567 CODE
ASSY
1A
-1 85550-12 CARGO HANDLING SYSTEM, A RF
A321-200
(RWK SB 85550-25-02)
(MSNS 835, 1017 ONLY)
-1A 85550-12 CARGO HANDLING SYSTEM, B RF
A321-200
(SUBS MSNS ONLY)
-20 85338-12 . PLACARD INSTL, WALL 1
(SEE IPL FIGURE 2A FOR DETAILS)
30 80004-10 . LOCK ASSY, CARGO 66
(SEE IPL FIGURE 3 FOR DETAILS)
35 80004-11 . LOCK ASSY, CARGO 6
(SEE IPL FIGURE 3 FOR DETAILS)
40 80004-43 . LOCK ASSY, CARGO 6
(SEE IPL FIGURE 3 FOR DETAILS)
50 80576-10 . STOP ASSY, END 12
(SEE IPL FIGURE 4 FOR DETAILS)
60 81384-10 . RAIL ASSY, ROLLER 68
(SEE IPL FIGURE 5 FOR DETAILS)
65 81384-12 . RAIL ASSY, ROLLER 4
(SEE IPL FIGURE 5 FOR DETAILS)
70 81384-13 . RAIL ASSY, ROLLER 68
(SEE IPL FIGURE 5 FOR DETAILS)
71 81384-13 . RAIL ASSY, ROLLER A 2
(SEE IPL FIGURE 5 FOR DETAILS)
(POST SB 85550-25-02)
(SUPSDS ITEM 76)
71A 81384-13 . RAIL ASSY, ROLLER B 2
(SEE IPL FIGURE 5 FOR DETAILS)
75 81384-14 . RAIL ASSY, ROLLER 68
(SEE IPL FIGURE 5 FOR DETAILS)
76 81384-14 . RAIL ASSY, ROLLER A 2
(SEE IPL FIGURE 5 FOR DETAILS)
(PRE SB 85550-25-02)
(SUPSD BY ITEM 71)
80 81384-15 . RAIL ASSY, ROLLER 4
(SEE IPL FIGURE 5 FOR DETAILS)
85 81384-18 . RAIL ASSY, ROLLER 12
(SEE IPL FIGURE 5 FOR DETAILS)
86 81384-18 . RAIL ASSY, ROLLER A 2
(SEE IPL FIGURE 5 FOR DETAILS)

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10043
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NOMENCLATURE UNITS
FIG PART AIRLINE USAGE
PER
ITEM NUMBER PART NO. 1234567 CODE ASSY
1A
(POST SB 85550-25-02)
86A 81384-18 . RAIL ASSY, ROLLER B 2
(SEE IPL FIGURE 5 FOR DETAILS)
100 84021-40 . RAIL ASSY, SIDE GUIDE 6
(SEE IPL FIGURE 6 FOR DETAILS)
105 84021-41 . RAIL ASSY, SIDE GUIDE 2
(SEE IPL FIGURE 6 FOR DETAILS)
110 84021-45 . RAIL ASSY, SIDE GUIDE 6
(SEE IPL FIGURE 6 FOR DETAILS)
115 84021-50 . RAIL ASSY, SIDE GUIDE 4
(SEE IPL FIGURE 6 FOR DETAILS)
120 84021-51 . RAIL ASSY, SIDE GUIDE 6
(SEE IPL FIGURE 6 FOR DETAILS)
125 84021-52 . RAIL ASSY, SIDE GUIDE 6
(SEE IPL FIGURE 6 FOR DETAILS)
130 84021-54 . RAIL ASSY, SIDE GUIDE 2
(SEE IPL FIGURE 6 FOR DETAILS)
135 84021-59 . RAIL ASSY, SIDE GUIDE 2
(SEE IPL FIGURE 6 FOR DETAILS)
140 84021-60 . RAIL ASSY, SIDE GUIDE 2
(SEE IPL FIGURE 6 FOR DETAILS)
145 84021-61 . RAIL ASSY, SIDE GUIDE 2
(SEE IPL FIGURE 6 FOR DETAILS)
150 84021-75 . RAIL ASSY, SIDE GUIDE 6
(SEE IPL FIGURE 6 FOR DETAILS)
155 84021-78 . RAIL ASSY, SIDE GUIDE 2
(SEE IPL FIGURE 6 FOR DETAILS)
170 84022-47 . RAIL ASSY, INCREASED HEIGHT 4
SIDE GUIDE
(SEE IPL FIGURE 7 FOR DETAILS)
175 84022-49 . RAIL ASSY, INCREASED HEIGHT 2
SIDE GUIDE
(SEE IPL FIGURE 7 FOR DETAILS)
180 84764-16 . RAIL ASSY, ARTICULATING 1
SIDE GUIDE
(SEE IPL FIGURE 8 FOR DETAILS)
185 84764-18 . RAIL ASSY, ARTICULATING 1
SIDE GUIDE
(SEE IPL FIGURE 8 FOR DETAILS)
200 86872-11 . RAIL ASSY, INCREASED HEIGHT 7
SIDE GUIDE
(SEE IPL FIGURE 9 FOR DETAILS)

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10044
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NOMENCLATURE UNITS
FIG PART AIRLINE USAGE
PER
ITEM NUMBER PART NO. 1234567 CODE ASSY
1A
205 86872-14 . RAIL ASSY, INCREASED HEIGHT 1
SIDE GUIDE
(SEE IPL FIGURE 9 FOR DETAILS)
210 86872-19 . RAIL ASSY, INCREASED HEIGHT 2
SIDE GUIDE
(SEE IPL FIGURE 9 FOR DETAILS)
215 86872-20 . RAIL ASSY, INCREASED HEIGHT 1
SIDE GUIDE
(SEE IPL FIGURE 9 FOR DETAILS)
230 86963-18 . MAT ASSY, BALL 1
(SEE IPL FIGURE 10 FOR DETAILS)
235 86963-19 . MAT ASSY, BALL 1
(SEE IPL FIGURE 10 FOR DETAILS)
240 86963-12 . MAT ASSY, BALL 2
(SEE IPL FIGURE 10 FOR DETAILS)
245 86963-13 . MAT ASSY, BALL 2
(SEE IPL FIGURE 10 FOR DETAILS)
250 86963-14 . MAT ASSY, BALL 1
(SEE IPL FIGURE 10 FOR DETAILS)
255 86963-15 . MAT ASSY, BALL 1
(SEE IPL FIGURE 10 FOR DETAILS)
260 86963-16 . MAT ASSY, BALL 1
(SEE IPL FIGURE 10 FOR DETAILS)
265 86963-17 . MAT ASSY, BALL 1
(SEE IPL FIGURE 10 FOR DETAILS)
280 86974-10 . CROSSTRACK ASSY 52
(SEE IPL FIGURE 11 FOR DETAILS)
285 86974-17 . CROSSTRACK ASSY 8
(SEE IPL FIGURE 11 FOR DETAILS)
290 86974-12 . CROSSTRACK ASSY A 16
(SEE IPL FIGURE 11 FOR DETAILS)
(PRE SB 85550-25-02)
(SUPSD BY ITEM 291)
291 86974-22 . CROSSTRACK ASSY A 16
(SEE IPL FIGURE 11 FOR DETAILS)
(POST SB 85550-25-02)
(SUPSDS ITEM 290)
291A 86974-22 . CROSSTRACK ASSY B 16
(SEE IPL FIGURE 11 FOR DETAILS)
295 86974-13 . CROSSTRACK ASSY A 8
(SEE IPL FIGURE 11 FOR DETAILS)
(PRE SB 85550-25-02)

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10045
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NOMENCLATURE UNITS
FIG PART AIRLINE USAGE
PER
ITEM NUMBER PART NO. 1234567 CODE ASSY
1A
(SUPSD BY ITEM 296)
296 86974-23 . CROSSTRACK ASSY A 8
(SEE IPL FIGURE 11 FOR DETAILS)
(POST SB 85550-25-02)
(SUPSDS ITEM 295)
296A 86974-23 . CROSSTRACK ASSY B 8
(SEE IPL FIGURE 11 FOR DETAILS)
298 86974-16 . CROSSTRACK ASSY 24
(SEE IPL FIGURE 11 FOR DETAILS)
300 86974-18 . CROSSTRACK ASSY A 4
(SEE IPL FIGURE 11 FOR DETAILS)
(PRE SB 85550-25-02)
(SUPSD BY ITEM 301)
301 86974-28 . CROSSTRACK ASSY A 4
(SEE IPL FIGURE 11 FOR DETAILS)
(POST SB 85550-25-02)
(SUPSDS ITEM 300)
301A 86974-28 . CROSSTRACK ASSY B 4
(SEE IPL FIGURE 11 FOR DETAILS)
305 86976-11 . CROSSTRACK ASSY 7
(SEE IPL FIGURE 12 FOR DETAILS)
315 86977-10 . RAIL 1
320 86977-11 . RAIL 1
330 86980-10 . PROTECTOR ASSY, DOOR SILL 1
(SEE IPL FIGURE 13 FOR DETAILS)
335 86980-11 . PROTECTOR ASSY, DOOR SILL 1
(SEE IPL FIGURE 13 FOR DETAILS)
350 87008-10 . GUIDE ASSY, LATERA 2
(SEE IPL FIGURE 14 FOR DETAILS)
355 87008-11 . GUIDE ASSY, LATERAL 1
(SEE IPL FIGURE 14 FOR DETAILS)
370 87226-10 . CROSSTRACK ASSY 6
(SEE IPL FIGURE 15 FOR DETAILS)
400 MS24694S113 . SCREW 96
(TRUE P/N IS MS24694-S113)
405 MS24694S114 . SCREW 34
(TRUE P/N IS MS24694-S114)
410 NAS1149F0432P . WASHER 130
415 MS21042-4 . NUT 130

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10046
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Wall Placard Instl, P/N 85338-10

Figure 2 (Sheet 1 of 2)

85338-A
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10047
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Wall Placard Instl, P/N 85338-10

Figure 2 (Sheet 2 of 2)

85338-A
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10048
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

PART AIRLINE NOMENCLATURE USAGE UNITS

FIG PER
ITEM NUMBER PART NO. 1234567 CODE
ASSY
2
-1 85338-10 PLACARD INSTL, WALL 1
(SEE IPL FIGURE 1 FOR NHA)
20 85334-10 . NAMEPLATE 1
25 85336-10 . PLACARD, LOADING 1
40 85034-11 . PLACARD, WALL 1
45 85034-12 . PLACARD, WALL 1
50 85034-13 . PLACARD, WALL 1
55 85034-14 . PLACARD, WALL 1
60 85034-15 . PLACARD, WALL 1
65 85034-16 . PLACARD, WALL 1
70 85034-17 . PLACARD, WALL 1
75 85034-18 . PLACARD, WALL 1
80 85034-19 . PLACARD, WALL 1
85 85034-20 . PLACARD, WALL 1
90 85034-62 . PLACARD, WALL 1
95 85034-63 . PLACARD, WALL 1
100 85034-64 . PLACARD, WALL 1
105 85034-65 . PLACARD, WALL 1

- NOT ILLUSTRATED

85338-A
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10049
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Wall Placard Instl, P/N 85338-12

Figure 2A (Sheet 1 of 3)

85338-B
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10050
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Wall Placard Instl, P/N 85338-12

Figure 2A (Sheet 2 of 3)

85338-B
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10051
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Wall Placard Instl, P/N 85338-12

Figure 2A (Sheet 3 of 3)

85338-B
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10052
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

PART AIRLINE NOMENCLATURE USAGE UNITS

FIG PER
ITEM NUMBER PART NO. 1234567 CODE
ASSY
2A
-1 85338-12 PLACARD INSTL, WALL 1
(SEE IPL FIGURE 1A FOR NHA)
20 85334-13 . NAMEPLATE 1
25 85336-12 . PLACARD, LOADING 1
40 85034-11 . PLACARD, WALL 1
45 85034-12 . PLACARD, WALL 1
50 85034-13 . PLACARD, WALL 1
55 85034-14 . PLACARD, WALL 1
60 85034-15 . PLACARD, WALL 1
65 85034-16 . PLACARD, WALL 1
70 85034-17 . PLACARD, WALL 1
75 85034-18 . PLACARD, WALL 1
80 85034-19 . PLACARD, WALL 1
85 85034-20 . PLACARD, WALL 1
90 85034-62 . PLACARD, WALL 1
95 85034-63 . PLACARD, WALL 1
100 85034-64 . PLACARD, WALL 1
105 85034-65 . PLACARD, WALL 1
150 85034-42 . PLACARD, WALL 1
155 85034-43 . PLACARD, WALL 1
160 85034-44 . PLACARD, WALL 1
165 85034-45 . PLACARD, WALL 1
170 85034-46 . PLACARD, WALL 1

- NOT ILLUSTRATED

85338-B
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10053
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

45
30 35

40
60

30
50
55
80
80A
20 105
10
15

20 70
70 75
105 70A 80

115
20

25

100
75
75A

25

90
95

110
80004-AF-1

Cargo Lock Assy, P/N 80004-10, -11, and - 43

Figure 3

80004-AF
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10054
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

AIRLINE NOMENCLATURE USAGE UNITS

FIG PART NUMBER PER
ITEM PART NO. 1234567 CODE
ASSY
3
-1 80004-10 LOCK ASSY, CARGO A RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1A 80004-11 LOCK ASSY, CARGO B RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1B 80004-43 LOCK ASSY, CARGO C RF
(SEE IPL FIGURES 1, 1A FOR NHA)
10 81956-13 . NAMEPLATE 1
15 81956-20 . COVER 1
20 MS24665-281 . PIN, COTTER 4
25 80021-10 . SHAFT, LOCK HEAD 2
30 NAS1149D0516H . WASHER 4
35 80018-10 . SPRING, TORSION 1
40 80018-11 . SPRING, TORSION 1
45 80014-10 . PAWL, OUTER 1
50 80019-10 . SPRING, TORSION 1
55 80019-11 . SPRING, TORSION 1
60 80015-10 . PAWL, INNER 1
70 MS24665-132 . PIN, COTTER A 2
70A MS24665-132 . PIN, COTTER C 1
75 80957-10 . SHAFT ASSY, ROLLER A 2
75A 80957-10 . SHAFT ASSY, ROLLER C 1
80 81011-10 . ROLLER ASSY A 2
80A 81011-10 . ROLLER ASSY C 1
90 AN565C1032H6 . SETSCREW 2
95 222 . THREADLOCKER (V05972) AR
100 80022-10 . SPRING, SHEAR STUD 2
105 84037-10 . STUD, SHEAR 2
110 80704-11 . STUD, TENSION 2
115 80012-10 . BASE, W/ ROLLERS A 1
-115A 80012-11 . BASE, W/O ROLLERS B 1
-115B 80012-24 . BASE, W/ONE ROLLER C 1

– NOT ILLUSTRATED

80004-AF
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10055
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

End Stop Assy, P/N 80576-10

Figure 4

80576-M
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10056
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

PART AIRLINE USAGE UNITS

FIG NOMENCLATURE PER
ITEM NUMBER PART NO. 1234567 CODE
ASSY
4
-1 80576-10 STOP ASSY, END RF
(SEE IPL FIGURES 1, 1A FOR NHA)
10 81956-13 . NAMEPLATE 1
15 81956-20 . COVER 1
20 80682-10 . BUMPER 2
30 414 . ADHESIVE (V05972) AR
40 NAS6703-2 . BOLT 1
45 NAS1149F0332P . WASHER 1
50 MS21042L3 . NUT 1
60 80681-10 . CASTING 1
65 80681-11 . CASTING 1

- NOT ILLUSTRATED

80576-M
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10057
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Roller Rail Assy, P/N 81384-10, -12 thru -15, and -18
Figure 5

81384-M
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10058
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

AIRLINE NOMENCLATURE USAGE UNITS

FIG PART NUMBER PER
ITEM PART NO. 1234567 CODE
ASSY
5
-1 81384-10 RAIL ASSY, ROLLER A RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1A 81384-12 RAIL ASSY, ROLLER B RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1B 81384-13 RAIL ASSY, ROLLER C RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1C 81384-14 RAIL ASSY, ROLLER D RF
(SEE IPL FIGURES 1, 1A, 16 FOR
NHA)
-1D 81384-15 RAIL ASSY, ROLLER E RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1E 81384-18 RAIL ASSY, ROLLER F RF
(SEE IPL FIGURES 1, 1A FOR NHA)
10 81956-13 . NAMEPLATE 1
15 81956-20 . COVER 1
20 80039-10 . RETAINER A, B, C, 2
E
-20A 80039-10 . RETAINER D, F 1
ATTACHING PARTS
25 AN3-5A . BOLT A, B, C, 2
E
-25A AN3-5A . BOLT D, F 1
30 NAS1149F0332P . WASHER A, B, C, 2
E
-30A NAS1149F0332P . WASHER D, F 1
35 MS21042L3 . NUT A, B, C, 2
E
-35A MS21042L3 . NUT D, F 1
---*---
50 5-64X5-8T-HD . PIN, COTTER (V0U252) A 12
(TRUE P/N IS 5/64 X 5/8-T-HD)
-50A 5-64X5-8T-HD . PIN, COTTER (V0U252) B 14
(TRUE P/N IS 5/64 X 5/8-T-HD)
-50B 5-64X5-8T-HD . PIN, COTTER (V0U252) C 6
(TRUE P/N IS 5/64 X 5/8-T-HD)
-50C 5-64X5-8T-HD . PIN, COTTER (V0U252) D, F 4
(TRUE P/N IS 5/64 X 5/8-T-HD)
-50D 5-64X5-8T-HD . PIN, COTTER (V0U252) E 10
(TRUE P/N IS 5/64 X 5/8-T-HD)
55 81395-10 . COLLAR A 12
-55A 81395-10 . COLLAR B 14
-55B 81395-10 . COLLAR C 6
-55C 81395-10 . COLLAR D, F 4
– NOT ILLUSTRATED

81384-M
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10059
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NOMENCLATURE UNITS
FIG AIRLINE USAGE
PART NUMBER PER
ITEM PART NO. 1234567 CODE ASSY
5
-55D 81395-10 . COLLAR E 10
60 81394-10 . ROLLER ASSY A 12
-60A 81394-10 . ROLLER ASSY B 14
-60B 81394-10 . ROLLER ASSY C 6
-60C 81394-10 . ROLLER ASSY D, F 4
-60D 81394-10 . ROLLER ASSY E 10
65 81384-110 . RAIL WITH SHAFTS, 32 IN. LONG A 1
-65A 81384-112 . RAIL WITH SHAFTS, 38 IN. LONG B 1
-65B 81384-113 . RAIL WITH SHAFTS, 14 IN. LONG C 1
-65C 81384-114 . RAIL WITH SHAFTS, 8 IN. LONG D 1
-65D 81384-115 . RAIL WITH SHAFTS, 26 IN. LONG E 1
-65E 81384-118 . RAIL WITH SHAFTS, 6 IN. LONG F 1

– NOT ILLUSTRATED

81384-M
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10060
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Side Guide Rail Assy, P/N 84021-40, -41, -45, -50, -51,
-52, -54, -59, -60, -61, -75, -78
Figure 6 (Sheet 1 of 2)

84021-AH
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10061
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Side Guide Rail Assy, P/N 84021-40, -41, -45, -50, -51,
-52, -54, -59, -60, -61, -75, -78
Figure 6 (Sheet 2 of 2)

84021-AH
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10062
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

AIRLINE NOMENCLATURE USAGE UNITS

FIG PART NUMBER PER
ITEM PART NO. 1234567 CODE
ASSY
6
-1 84021-40 RAIL ASSY, SIDE GUIDE A RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1A 84021-41 RAIL ASSY, SIDE GUIDE B RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1B 84021-45 RAIL ASSY, SIDE GUIDE C RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1C 84021-50 RAIL ASSY, SIDE GUIDE D RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1D 84021-51 RAIL ASSY, SIDE GUIDE E RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1E 84021-52 RAIL ASSY, SIDE GUIDE F RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1F 84021-54 RAIL ASSY, SIDE GUIDE G RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1G 84021-59 RAIL ASSY, SIDE GUIDE H RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1H 84021-60 RAIL ASSY, SIDE GUIDE J RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1J 84021-61 RAIL ASSY, SIDE GUIDE K RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1K 84021-75 RAIL ASSY, SIDE GUIDE L RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1L 84021-78 RAIL ASSY, SIDE GUIDE M RF
(SEE IPL FIGURES 1, 1A FOR NHA)
10 81956-13 . NAMEPLATE 1
15 81956-20 . COVER 1
20 MS24665-132 . PIN, COTTER A thru G, 2
J thru L
-20A MS24665-132 . PIN, COTTER H, M 1
25 MS20392-3C43 . PIN, HEADED A thru G, 2
J thru L
-25A MS20392-3C43 . PIN, HEADED H, M 1
30 84123-10 . ROLLER ASSY A thru G, 2
J thru L
-30A 84123-10 . ROLLER ASSY H, M 1
40 84121-40 . RAIL, GUIDE A 1
-40A 84121-41 . RAIL, GUIDE B 1
-40B 84121-45 . RAIL, GUIDE C 1
-40C 84121-50 . RAIL, GUIDE D 1
-40D 84121-51 . RAIL, GUIDE E 1
-40E 84121-52 . RAIL, GUIDE F 1
-40F 84121-54 . RAIL, GUIDE G 1

– NOT ILLUSTRATED

84021-AH
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10063
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NOMENCLATURE UNITS
FIG AIRLINE USAGE
PART NUMBER PER
ITEM PART NO. 1234567 CODE ASSY
6
40G 84121-59 . RAIL, GUIDE H 1
-40H 84121-60 . RAIL, GUIDE J 1
-40J 84121-61 . RAIL, GUIDE K 1
-40K 84121-75 . RAIL, GUIDE L 1
-40L 84121-78 . RAIL, GUIDE M 1

– NOT ILLUSTRATED

84021-AH
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10064
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Increased Height Side Guide Rail Assy, P/N 84022-47 and -49
Figure 7

84022-L
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10065
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

AIRLINE NOMENCLATURE USAGE UNITS

FIG PART NUMBER PER
ITEM PART NO. 1234567 CODE
ASSY
7
-1 84022-47 RAIL ASSY, INCREASED HEIGHT A RF
SIDE GUIDE
(SEE IPL FIGURES 1, 1A FOR NHA)
-1A 84022-49 RAIL ASSY, INCREASED HEIGHT B RF
SIDE GUIDE
(SEE IPL FIGURES 1, 1A FOR NHA)
10 81956-13 . NAMEPLATE 1
15 81956-20 . COVER 1
20 MS24665-300 . PIN, COTTER 2
25 MS20392-4C49 . PIN, HEADED 2
30 80879-10 . ROLLER ASSY 2
35 84120-47 . RAIL, GUIDE A 1
-35A 84120-49 . RAIL, GUIDE B 1

– NOT ILLUSTRATED

84022-L
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10066
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Articulating Side Guide Rail Assy, P/N 84764-16 and -18

Figure 8

84764-F
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10067
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

AIRLINE NOMENCLATURE USAGE UNITS

FIG PART NUMBER PER
ITEM PART NO. 1234567 CODE
ASSY
8
-1 84764-16 RAIL ASSY, ARTICULATING A RF
SIDE GUIDE
(SEE IPL FIGURES 1, 1A FOR NHA)
-1A 84764-18 RAIL ASSY, ARTICULATING B RF
SIDE GUIDE
(SEE IPL FIGURES 1, 1A FOR NHA)
5 81956-13 . NAMEPLATE 1
10 81956-20 . COVER 1
15 MS24665-132 . PIN 2
20 MS20392-3C43 . PIN 2
25 84123-10 . ROLLER ASSY 2
30 84755-10 . LINK A 1
-30A 84755-11 . LINK B 1
ATTACHING PARTS
35 NAS517-4-18 . SCREW 1
40 NAS1149F0463P . WASHER 1
45 NAS679A4 . NUT 1
---*---
50 83456-10 . SUPPORT, HINGE 1
ATTACHING PARTS
55 NAS517-4-21 . SCREW 2
60 NAS1149F0463P . WASHER 2
65 NAS679A4 . NUT 2
---*---
70 84761-16 . RAIL A 1
-70A 84761-18 . RAIL B 1

– NOT ILLUSTRATED

84764-F
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10068
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Increased Height Side Guide Rail Assy, P/N 86872-11, -14, -19, -20
Figure 9

86872-E
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10069
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

AIRLINE NOMENCLATURE USAGE UNITS

FIG PART NUMBER PER
ITEM PART NO. 1234567 CODE
ASSY
9
-1 86872-11 RAIL ASSY, INCREASED HEIGHT A RF
SIDE GUIDE
(SEE IPL FIGURES 1, 1A FOR NHA)
-1A 86872-14 RAIL ASSY, INCREASED HEIGHT B RF
SIDE GUIDE
(SEE IPL FIGURES 1, 1A FOR NHA)
-1B 86872-19 RAIL ASSY, INCREASED HEIGHT C RF
SIDE GUIDE
(SEE IPL FIGURES 1, 1A FOR NHA)
-1C 86872-20 RAIL ASSY, INCREASED HEIGHT D RF
SIDE GUIDE
(SEE IPL FIGURES 1, 1A FOR NHA)
10 81956-13 . NAMEPLATE 1
15 81956-20 . COVER 1
20 MS24665-300 . PIN, COTTER 2
25 MS20392-4C49 . PIN, HEADED 2
30 80879-10 . ROLLER ASSY 2
35 84120-53 . RAIL, GUIDE A 1
-35A 84120-59 . RAIL, GUIDE B 1
-35B 84120-61 . RAIL, GUIDE C 1
-35C 84120-62 . RAIL, GUIDE D 1

– NOT ILLUSTRATED

86872-E
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10070
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Ball Mat Assy, P/N 86963-10 thru -19

Figure 10 (Sheet 1 of 7)

86963-B
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10071
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Ball Mat Assy, P/N 86963-10 thru -19

Figure 10 (Sheet 2 of 7)

86963-B
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10072
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Ball Mat Assy, P/N 86963-10 thru -19

Figure 10 (Sheet 3 of 7)

86963-B
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10073
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Ball Mat Assy, P/N 86963-10 thru -19

Figure 10 (Sheet 4 of 7)

86963-B
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10074
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Ball Mat Assy, P/N 86963-10 thru -19

Figure 10 (Sheet 5 of 7)

86963-B
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10075
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Ball Mat Assy, P/N 86963-10 thru -19

Figure 10 (Sheet 6 of 7)

86963-B
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10076
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Ball Mat Assy, P/N 86963-10 thru -19

Figure 10 (Sheet 7 of 7)

86963-B
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10077
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NOMENCLATURE UNITS
FIG PART NUMBER AIRLINE USAGE PER
ITEM PART NO. 1234567 CODE
ASSY
10
-1 86963-10 MAT ASSY, BALL A RF
(SEE IPL FIGURE 1 FOR NHA)
-1A 86963-11 MAT ASSY, BALL B RF
(SEE IPL FIGURE 1 FOR NHA)
-1B 86963-12 MAT ASSY, BALL C RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1C 86963-13 MAT ASSY, BALL D RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1D 86963-14 MAT ASSY, BALL E RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1E 86963-15 MAT ASSY, BALL F RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1F 86963-16 MAT ASSY, BALL G RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1G 86963-17 MAT ASSY, BALL H RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1H 86963-18 MAT ASSY, BALL J RF
(SEE IPL FIGURES 1A, 16 FOR NHA)
-1J 86963-19 MAT ASSY, BALL K RF
(SEE IPL FIGURES 1A, 16 FOR NHA)
10 81956-13 . NAMEPLATE 1
15 81956-20 . COVER 1
30 81858-10 . SETSCREW A, J, K 50
(ALT TO ITEM -35)
-30A 81858-10 . SETSCREW B 51
(ALT TO ITEM -35A)
-30B 81858-10 . SETSCREW C 39
(ALT TO ITEM -35B)
-30C 81858-10 . SETSCREW D, E, F 33
(ALT TO ITEM -35C)
-30D 81858-10 . SETSCREW G 87
(ALT TO ITEM -35D)
-30E 81858-10 . SETSCREW H 79
(ALT TO ITEM -35E)
-35 MS51964-43 . SETSCREW A, J, K 50
(ALT TO ITEM 30)
-35A MS51964-43 . SETSCREW B 51
(ALT TO ITEM -30A)
-35B MS51964-43 . SETSCREW C 39
(ALT TO ITEM -30B)
-35C MS51964-43 . SETSCREW D, E, F 33
(ALT TO ITEM -30C)

– NOT ILLUSTRATED

86963-B
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10078
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NOMENCLATURE UNITS
FIG AIRLINE USAGE
PART NUMBER PER
ITEM PART NO. 1234567 CODE ASSY
10
-35D MS51964-43 . SETSCREW G 87
(ALT TO ITEM -30D)
-35E MS51964-43 . SETSCREW H 79
(ALT TO ITEM -30E)
40 222 . THREADLOCKER (V05972) AR
45 80028-10 . RETAINER A, J, K 50
-45A 80028-10 . RETAINER B 51
-45B 80028-10 . RETAINER C 39
-45C 80028-10 . RETAINER D, E, F 33
-45D 80028-10 . RETAINER G 87
-45E 80028-10 . RETAINER H 79
50 80423-11 . BALL UNIT A, J, K 50
-50A 80423-11 . BALL UNIT B 51
-50B 80423-11 . BALL UNIT C 39
-50C 80423-11 . BALL UNIT D, E, F 33
-50D 80423-11 . BALL UNIT G 87
-50E 80423-11 . BALL UNIT H 79
55 80352-10 . SPRING A, J, K 50
-55A 80352-10 . SPRING B 51
-55B 80352-10 . SPRING C 39
-55C 80352-10 . SPRING D, E, F 33
-55D 80352-10 . SPRING G 87
-55E 80352-10 . SPRING H 79
85 40350-10 . STUD A 5
-85A 40350-10 . STUD B 6
-85B 40350-10 . STUD C, D, E, F 4
-85C 40350-10 . STUD G 8
-85D 40350-10 . STUD H 7
90 40349-10 . RETAINER A, K 5
-90A 40349-10 . RETAINER B, J 6
-90B 40349-10 . RETAINER C, D, E, F 4
-90C 40349-10 . RETAINER G 8
-90D 40349-10 . RETAINER H 7
105 NAS1149F0632P . WASHER A, K 5
-105A NAS1149F0632P . WASHER B, J 6
-105B NAS1149F0632P . WASHER C, D, E, F 4
-105C NAS1149F0632P . WASHER G 8
-105D NAS1149F0632P . WASHER H 7
115 MS21042-6 . NUT A, K 5
-115A MS21042-6 . NUT B, J 6
-115B MS21042-6 . NUT C, D, E, F 4
-115C MS21042-6 . NUT G 8
-115D MS21042-6 . NUT H 7
– NOT ILLUSTRATED

86963-B
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10079
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NOMENCLATURE UNITS
FIG AIRLINE USAGE
PART NUMBER PER
ITEM PART NO. 1234567 CODE ASSY
10
150 80339-35 . RAMP, RAIL A, H, K 1
150A 80339-14 . RAMP, RAIL D, F 1
150B 80339-39 . RAMP, RAIL H 1
ATTACHING PARTS
160 CR3242-6-03 . RIVET (V05693) A, D, F, K 9
-160A CR3242-6-03 . RIVET (V05693) H 15
---*---
-200 86963-01 . PANEL ASSY A 1
-200A 86963-02 . PANEL ASSY B 1
-200B 86963-03 . PANEL ASSY C 1
-200C 86963-04 . PANEL ASSY D 1
-200D 86963-05 . PANEL ASSY E 1
-200E 86963-06 . PANEL ASSY F 1
-200F 86963-07 . PANEL ASSY G 1
-200G 86963-08 . PANEL ASSY H 1
-200H 86963-09 . PANEL ASSY J 1
-200J 86963-20 . PANEL ASSY K 1
280 80031-10 . . BRACKET A, K 5
-280A 80031-10 . . BRACKET B, J 6
-280B 80031-10 . . BRACKET C, D, E, F 4
-280C 80031-10 . . BRACKET G 8
-280D 80031-10 . . BRACKET H 7
ATTACHING PARTS
290 MS20426AD6-6 . . RIVET A, K 20
-290A MS20426AD6-6 . . RIVET B, J 24
-290B MS20426AD6-6 . . RIVET C, D, E, F 16
-290C MS20426AD6-6 . . RIVET G 32
-290D MS20426AD6-6 . . RIVET H 28
---*---

– NOT ILLUSTRATED

86963-B
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10080
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Crosstrack Assy, P/N 86974-10 thru -13, -16 thru -18, -22, -23, -28
Figure 11 (Sheet 1 of 7)

86974-F
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10081
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Crosstrack Assy, P/N 86974-10 thru -13, -16 thru -18, -22, -23, -28
Figure 11 (Sheet 2 of 7)

86974-F
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10082
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Crosstrack Assy, P/N 86974-10 thru -13, -16 thru -18, -22, -23, -28
Figure 11 (Sheet 3 of 7)

86974-F
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10083
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Crosstrack Assy, P/N 86974-10 thru -13, -16 thru -18, -22, -23, -28
Figure 11 (Sheet 4 of 7)

86974-F
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10084
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Crosstrack Assy, P/N 86974-10 thru -13, -16 thru -18, -22, -23, -28
Figure 11 (Sheet 5 of 7)

86974-F
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10085
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Crosstrack Assy, P/N 86974-10 thru -13, -16 thru -18, -22, -23, -28
Figure 11 (Sheet 6 of 7)

86974-F
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10086
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Crosstrack Assy, P/N 86974-10 thru -13, -16 thru -18, -22, -23, -28
Figure 11 (Sheet 7 of 7)

86974-F
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10087
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

PART AIRLINE USAGE UNITS

FIG NOMENCLATURE PER
ITEM NUMBER PART NO. 1234567 CODE
ASSY
11
-1 86974-10 CROSSTRACK ASSY A RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1A 86974-11 CROSSTRACK ASSY B RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1B 86974-12 CROSSTRACK ASSY C RF
(SEE IPL FIGURES 1, 1A FOR NHA)
(PRE SB 85550-25-02)
(SUPSD BY ITEM -1G)
-1C 86974-13 CROSSTRACK ASSY D RF
(SEE IPL FIGURES 1, 1A FOR NHA)
(PRE SB 85550-25-02)
(SUPSD BY ITEM -1H)
-1D 86974-16 CROSSTRACK ASSY E RF
(SEE IPL FIGURES 1A, 16 FOR NHA)
-1E 86974-17 CROSSTRACK ASSY F RF
(SEE IPL FIGURES 1A, 16 FOR NHA)
-1F 86974-18 CROSSTRACK ASSY G RF
(SEE IPL FIGURE 1A FOR NHA)
(PRE SB 85550-25-02)
(SUPSD BY ITEM -1J)
-1G 86974-22 CROSSTRACK ASSY H RF
(SEE IPL FIGURES 1, 1A FOR NHA)
(POST SB 85550-25-02)
(SUPSDS ITEM -1B)
-1H 86974-23 CROSSTRACK ASSY J RF
(SEE IPL FIGURES 1, 1A FOR NHA)
(POST SB 85550-25-02)
(SUPSDS ITEM -1C)
-1J 86974-28 CROSSTRACK ASSY K RF
(SEE IPL FIGURES 1A, 16 FOR NHA)
(POST SB 85550-25-02)
(SUPSDS ITEM -1F)
10 81956-13 . NAMEPLATE 1
15 81956-20 . COVER 1
30 MS24665-132 . PIN, COTTER A, C, D, 4
E, G
-30A MS24665-132 . PIN, COTTER H, J, K 16
35 80010-11 . SHAFT, ROLLER A, C, D, 2
E, G
-35A 80010-11 . SHAFT, ROLLER H, J, K 8
40 81394-10 . ROLLER ASSY A, C, D, 2
E, G

– NOT ILLUSTRATED

86974-F
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10088
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

UNITS
FIG PART AIRLINE NOMENCLATURE USAGE
PER
ITEM NUMBER PART NO. 1234567 CODE ASSY
11
-40A 81394-10 . ROLLER ASSY H, J, K 8
45 83879-12 . BRACKET, ROLLER SUPPORT A, E 2
50 83879-14 . BRACKET, ROLLER SUPPORT C, D, G 2
-50A 83879-14 . BRACKET, ROLLER SUPPORT H, J, K 8
ATTACHING PARTS
55 NAS6203-7 . BOLT A, E 4
57 NAS6203-5 . BOLT C, D, G 4
-57A NAS6203-5 . BOLT H, J, K 16
60 NAS1149F0332P . WASHER A, E 4
65 MS21042-3 . NUT A, E 4
---*---
70 242 . THREADLOCKER (V05972) C, D, G, AR
H, J, K
80 NAS6205-11 . BOLT 1
85 NAS1149F0532P . WASHER 1
90 MS21042-5 . NUT 1
95 80166-10 . BUSHING 1
100 84041-11 . RESTRAINT, VERTICAL 1
105 80167-10 . SPRING 1
110 84673-12 . BODY, OUTBOARD RESTRAINT A, C, D, 1
E, F, G,
H, J, K
-110A 84673-10 . BODY, OUTBOARD RESTRAINT B 1
ATTACHING PARTS
114 NAS6204-10 . BOLT C, D, G, 2
H, J, K
117 NAS6204-14 . BOLT C, D, G, 2
H, J, K
120 NAS6204-9 . BOLT A, B, E, 4
F
130 NAS1149F0432P . WASHER 4
140 MS21042-4 . NUT 4
---*---
150 SHM31STZD . RING, RETAINING (V07382) E, F, G, 2
K
(TRUE P/N IS SHM-31STZD)
155 80078-12 . SHAFT E, F, G, 1
K
160 NAS1149C0532R . WASHER E, F, G, 2
K
165 83665-10 . SPRING E, F, G, 1
K
170 83665-11 . SPRING E, F, G, 1
K

– NOT ILLUSTRATED

86974-F
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10089
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

UNITS
FIG PART AIRLINE NOMENCLATURE USAGE
PER
ITEM NUMBER PART NO. 1234567 CODE ASSY
11
175 83663-10 . PAWL E, F, G, 1
K
180 GP24-093-875-78 . PIN, GROOVE (V73957) E, F 1
(TRUE P/N IS GP-24-093-875-78)
185 C0RIC0NE1700 . SEALER, METAL (V7Y015) E, F AR
(TRUE P/N IS CORICONE 1700)
187 GE5050-12C . SEALANT (V01139) E, F AR
190 84347-11 . PLUNGER E, F 1
195 LC020C4 . SPRING, COMPRESSION (V1A699) E, F 1
(TRUE P/N IS LC-020C-4)
220 40361-59 . STUD A, B, E, 2
F
225 40361-15 . STUD C, D, G, 2
H, J, K
250 43356-21 . WASHER 2
260 NAS1149F0532P . WASHER 2
280 MS21042-5 . NUT 2
300 87034-10 . CROSSTRACK A 1
-300A 87034-11 . CROSSTRACK B 1
300B 87214-10 . CROSSTRACK C 1
-300C 87214-12 . CROSSTRACK D 1
300D 87214-15 . CROSSTRACK E, F 1
300E 87214-14 . CROSSTRACK G 1
300F 87214-20 . CROSSTRACK H 1
-300G 87214-22 . CROSSTRACK J 1
300H 87214-24 . CROSSTRACK K 1

– NOT ILLUSTRATED

86974-F
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10090
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Crosstrack Assy, P/N 86976-10 and -11

Figure 12 (Sheet 1 of 2)

86976-C
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10091
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Crosstrack Assy, P/N 86976-10 and -11

Figure 12 (Sheet 2 of 2)

86976-C
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10092
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

PART AIRLINE USAGE UNITS

FIG NOMENCLATURE PER
ITEM NUMBER PART NO. 1234567 CODE
ASSY
12
-1 86976-10 CROSSTRACK ASSY A RF
(SEE IPL FIGURE 1 FOR NHA)
-1A 86976-11 CROSSTRACK ASSY B RF
(SEE IPL FIGURES 1A, 16 FOR NHA)
10 81956-13 . NAMEPLATE 1
15 81956-20 . COVER 1
30 SHM31STZD . RING, RETAINING (V07382) A 2
(TRUE P/N IS SHM-31STZD)
-30A SHM31STZD . RING, RETAINING (V07382) B 4
(TRUE P/N IS SHM-31STZD)
35 SH37STZD . RING, RETAINING (V07382) A 2
(TRUE P/N IS SH-37STZD)
-35A SH37STZD . RING, RETAINING (V07382) B 4
(TRUE P/N IS SH-37STZD)
40 80078-12 . SHAFT A 1
-40A 80078-12 . SHAFT B 2
45 80078-13 . SHAFT A 1
-45A 80078-13 . SHAFT B 2
50 NAS1149D0532H . WASHER A 2
-50A NAS1149D0532H . WASHER B 4
55 NAS1149D0632H . WASHER A 2
-55A NAS1149D0632H . WASHER B 4
60 80222-10 . SPRING A 1
-60A 80222-10 . SPRING B 2
65 80076-11 . PAWL A 1
-65A 80076-11 . PAWL B 2
70 80077-10 . LEVER A 1
-70A 80077-10 . LEVER B 2
220 81673-12 DELETED D
-220A 81673-15 . STUD, TENSION 2
225 40361-59 . STUD 1
250 43356-21 . WASHER 1
260 NAS1149F0532P . WASHER 1
265 NAS1149F0432P . WASHER 2
280 MS21045-5 . NUT 1
285 MS21045-4 . NUT 2
300 87039-10 . CROSSTRACK A 1
300A 87039-12 . CROSSTRACK B 1

– NOT ILLUSTRATED

86976-C
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10093
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

THIS PAGE INTENTIONALLY LEFT BLANK

86976-C
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10094
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Door Sill Protector Assy, P/N 86980-10 and -11

Figure 13 (Sheet 1 of 10)

86980-D
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10095
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Door Sill Protector Assy, P/N 86980-10 and -11

Figure 13 (Sheet 2 of 10)

86980-D
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10096
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Door Sill Protector Assy, P/N 86980-10 and -11

Figure 13 (Sheet 3 of 10)

86980-D
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10097
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Door Sill Protector Assy, P/N 86980-10 and -11

Figure 13 (Sheet 4 of 10)

86980-D
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10098
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Door Sill Protector Assy, P/N 86980-10 and -11

Figure 13 (Sheet 5 of 10)

86980-D
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10099
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Door Sill Protector Assy, P/N 86980-10 and -11

Figure 13 (Sheet 6 of 10)

86980-D
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10100
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Door Sill Protector Assy, P/N 86980-10 and -11

Figure 13 (Sheet 7 of 10)

86980-D
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10101
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Door Sill Protector Assy, P/N 86980-10 and -11

Figure 13 (Sheet 8 of 10)

86980-D
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10102
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Door Sill Protector Assy, P/N 86980-10 and -11

Figure 13 (Sheet 9 of 10)

86980-D
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10103
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Door Sill Protector Assy, P/N 86980-10 and -11

Figure 13 (Sheet 10 of 10)

86980-D
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10104
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

AIRLINE NOMENCLATURE USAGE UNITS

FIG PART NUMBER PER
ITEM PART NO. 1234567 CODE
ASSY
13
-1 86980-10 PROTECTOR ASSY, DOOR SILL A RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1A 86980-11 PROTECTOR ASSY, DOOR SILL B RF
(SEE IPL FIGURES 1, 1A FOR NHA)
5 81956-13 . NAMEPLATE 1
15 81028-10 . DECAL 1
20 81028-11 . DECAL 1
25 81028-13 . DECAL 1
30 81028-14 . DECAL 1
40 81956-20 . COVER 1
45 80876-30 . COVER 3
50 80876-32 . COVER 1
60 MS24665-300 . PIN, COTTER 38
65 80115-22 . SHAFT, ROLLER 19
80 MS39086-436 . PIN, SPRING 2
85 80115-17 . SHAFT 2
90 80120-10 . ROLLER ASSY 2
100 MS24665-302 . PIN, COTTER 14
105 82087-13 . SHAFT 7
110 84362-10 . ROLLER 7
-130 83446-10 DELETED D
130A 83446-12 . BOLT, SHEAR 3
135 242 . THREADLOCKER (V05972) AR
140 NAS43DD5-20A . SPACER 3
145 MS24665-300 . PIN, COTTER 6
150 80115-21 . SHAFT 3
155 9416K84 . FITTING, END (V3A054) 6
160 222 . THREADLOCKER (V05972) AR
165 9416K15 . SPRING ASSY, GAS (V3A054) 3
175 83427-10 . BRACKET, SPRING 3
ATTACHING PARTS
180 NAS517-4-3 . SCREW 9
185 NAS1149F0432P . WASHER 9
190 MS21042-4 . NUT 9
---*---
200 MS24665-300 . PIN, COTTER 3
205 MS24665-302 . PIN, COTTER 3
215 83445-10 . PIN 3
220 GP24-125-0875-72 . PIN, GROOVE (V73957) 3
(TRUE P/N IS GP-24-125-0875-72)
222 83450-11 . PIN 3

– NOT ILLUSTRATED

86980-D
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10105
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NOMENCLATURE UNITS
FIG AIRLINE USAGE
PART NUMBER PER
ITEM PART NO. 1234567 CODE ASSY
13
225 60745K241RH . JOINT, ROD END (V3A054) 3
(TRUE P/N IS 60745K241-RH)
230 60745K242LH . JOINT, ROD END (V3A054) 3
(TRUE P/N IS 60745K242-LH)
235 NAS509L6 . NUT 6
240 NAS509-6 . NUT 6
245 83422-11 . STUD, THREADED 3
250 83424-11 . ARM, LINK 3
255 83504-10 . LINK, ROD 3
270 MS24665-300 . PIN, COTTER 6
275 80471-11 . SHAFT 3
280 86018-10 . SPRING, TORSION 3
285 8672K42 . TRIM, PLASTIC, 2.4 IN. (V3A054) 3
-288 MS20995C32 . WIRE, LOCK AR
305 83421-12 . SADDLE 3
310 83422-12 . STUD, THREADED 3
315 NAS509L8 . NUT 3
320 NAS509-8 . NUT 3
325 83423-13 . LEG 3
340 83425-10 . BRACKET, LEG 3
345 83425-11 . BRACKET, LEG 3
ATTACHING PARTS
350 NAS6205-5 . BOLT 12
355 NAS1149F0532P . WASHER 12
---*---
365 C0RIC0NE1700 . SEALER, METAL (V7Y015) AR
(TRUE P/N IS CORICONE 1700)
370 MS39086-436 . PIN, SPRING 1
375 82087-14 . SHAFT 1
380 84100-12 . SPRING B 2
385 84100-13 . SPRING A 2
390 83428-14 . GUIDE B 1
395 83428-15 . GUIDE A 1
400 MS39086-119 . PIN, SPRING 1
405 84084-10 . HANDLE, LATERAL GUIDE 1
410 84082-10 . PLUNGER 1
415 QQ67 . SPRING, COMPRESSION (V56988) 1
(TRUE P/N IS QQ-67)
420 84081-10 . HOUSING, DOUBLER 1
ATTACHING PARTS
425 AN3-3A . BOLT 2
430 NAS1149F0332P . WASHER 2
---*---
– NOT ILLUSTRATED

86980-D
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10106
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NOMENCLATURE UNITS
FIG AIRLINE USAGE
PART NUMBER PER
ITEM PART NO. 1234567 CODE ASSY
13
435 680 . COMPOUND, RETAINING (V05972) AR
450 NAS601-7 DELETED D
-450A NAS602-7P . SCREW 1
455 86099-10 . LATCH 1
460 X4AN . PLUNGER, BALL (V01599) 1
(TRUE P/N IS X4A-N)
465 MS24665-283 . PIN, COTTER 2
470 82242-13 . SHAFT 1
475 84106-10 . SPRING, TORSION 1
480 84106-11 . SPRING, TORSION 1
485 83428-16 . GUIDE 1
490 83672-13 . SUPPORT 1
ATTACHING PARTS
495 NAS6204-12 . BOLT 4
500 NAS1149F0432P . WASHER 4
505 MS21042-4 . NUT 4
---*---
515 MS27039-4-08 . SCREW 1
520 NAS1149F0432P . WASHER 1
525 84117-11 . RETAINER, ROLLER 1
530 84116-13 . ROLLER, PIVOT 1
535 84119-11 . WASHER, ROLLER 1

540 MS24665-300 . PIN, COTTER 2

545 82012-12 . SHAFT, LOCKHEAD 1
550 84112-14 . BODY, PIVOT ROLLER 1
560 GP24-125-0875-72 . PIN, GROOVE (V73957) 7
(TRUE P/N IS GP-24-125-0875-72)
565 83450-11 . SHAFT 1
570 83450-12 . SHAFT 6
580 87264-10 . BRACKET, HINGE A 3
-580A 87264-11 . BRACKET, HINGE B 3
590 87264-12 . BRACKET, HINGE A 1
-590A 87264-13 . BRACKET, HINGE B 1
600 81673-20 . STUD, TENSION 13
605 81673-11 . STUD, TENSION 3
610 40361-17 . STUD 1
620 43356-21 . WASHER 1
625 NAS1149F0432P . WASHER 16
630 NAS1149F0632P . WASHER 1
640 MS21042-4 . NUT 16
645 MS21042-6 . NUT 1
660 NAS6205-8 . BOLT 6
– NOT ILLUSTRATED

86980-D
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10107
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NOMENCLATURE UNITS
FIG AIRLINE USAGE
PART NUMBER PER
ITEM PART NO. 1234567 CODE ASSY
13
665 NAS1149F0532P . WASHER 6
670 MS21042-5 . NUT 6
680 87143-10 . SILL, DOOR A 1
685 87143-11 . SILL, DOOR A 1
690 87143-12 . SILL, DOOR B 1
695 87143-13 . SILL, DOOR B 1

– NOT ILLUSTRATED

86980-D
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10108
Apr 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Lateral Guide Assy, P/N 87008-10 and -11

Figure 14 (Sheet 1 of 5)

87008-A
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10109
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Lateral Guide Assy, P/N 87008-10 and -11

Figure 14 (Sheet 2 of 5)

87008-A
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10110
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Lateral Guide Assy, P/N 87008-10 and -11

Figure 14 (Sheet 3 of 5)

87008-A
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10111
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Lateral Guide Assy, P/N 87008-10 and -11

Figure 14 (Sheet 4 of 5)

87008-A
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10112
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Lateral Guide Assy, P/N 87008-10 and -11

Figure 14 (Sheet 5 of 5)

87008-A
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10113
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

AIRLINE NOMENCLATURE USAGE UNITS

FIG PART NUMBER PER
ITEM PART NO. 1234567 CODE
ASSY
14
-1 87008-10 GUIDE ASSY, LATERAL A RF
(SEE IPL FIGURES 1, 1A FOR NHA)
-1A 87008-11 GUIDE ASSY, LATERAL B RF
(SEE IPL FIGURES 1, 1A FOR NHA)
10 81956-13 . NAMEPLATE 1
15 81956-20 . COVER 1
30 81858-10 . SETSCREW 2
35 222 . THREADLOCKER (V05972) AR
40 80028-10 . RETAINER 2
45 80423-10 . BALL UNIT 2
50 80352-10 . SPRING 2
55 NAS517-3-0 . SCREW 6
60 84095-10 . SKIN 1
70 84083-10 . HOUSING 2
80 MS39086-119 . PIN, SPRING 1
85 680 . COMPOUND, RETAINING (V05972) AR
90 84084-10 . HANDLE 1
95 84082-10 . PLUNGER, RELEASE 1
100 QQ67 . SPRING, HANDLE (V56988) 1
(TRUE P/N IS QQ-67)
105 84081-10 . HOUSING, DOUBLER 1
ATTACHING PARTS
110 AN3-3A . BOLT 2
115 NAS1149F0332P . WASHER 2
---*---
130 MS39086-145 . PIN, SPRING 4
135 84099-10 . SHAFT 3
140 84099-11 . SHAFT 1
145 84103-10 . ROLLER ASSY 4
160 MS39086-119 . PIN, SPRING 4
165 81245-19 . SHAFT, LOCKHEAD 4
170 MS39086-145 . PIN, SPRING 3
175 84099-10 . SHAFT A 2
-175A 84099-12 . SHAFT B 2
180 84099-13 . SHAFT 1
185 84077-10 . FRAME 1
190 84100-10 . SPRING, TORSION 2
195 NAS1149C0832R . WASHER 4
200 NAS6204-6 . BOLT 6
205 NAS1149F0432P . WASHER 6
210 242 . THREADLOCKER (V05972) AR

– NOT ILLUSTRATED

87008-A
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10114
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

NOMENCLATURE UNITS
FIG AIRLINE USAGE
PART NUMBER PER
ITEM PART NO. 1234567 CODE ASSY
14
215 84079-10 . LINK 2
220 84085-10 . DAMPENER 4
280 MS39086-131 . PIN, SPRING 4
285 86966-10 . BLOCK 2
290 82012-15 . SHAFT, LOCKHEAD 2
295 84078-11 . LINK 2
305 MS39086-119 . PIN, SPRING 1
310 81245-20 . SHAFT, LOCKHEAD 1
320 81011-11 . ROLLER ASSY 2
340 40361-17 . STUD 4
345 43356-32 . WASHER 4
350 NAS1149F0632P . WASHER 4
355 MS21042-6 . NUT 4
400 87003-10 . BASE A 1
-400A 87003-11 . BASE B 1

– NOT ILLUSTRATED

87008-A
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10115
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Crosstrack Assy, P/N 87226-10

Figure 15 (Sheet 1 of 2)

87226-A
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10116
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

Crosstrack Assy, P/N 87226-10

Figure 15 (Sheet 2 of 2)

87226-A
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10117
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

PART AIRLINE USAGE UNITS

FIG NOMENCLATURE PER
ITEM NUMBER PART NO. 1234567 CODE
ASSY
15
-1 87226-10 CROSSTRACK ASSY RF
(SEE IPL FIGURES 1, 1A FOR NHA)
10 81956-13 . NAMEPLATE 1
15 81956-20 . COVER 1
30 MS24665-132 . PIN, COTTER 4
35 80010-11 . SHAFT, ROLLER 2
40 81394-10 . ROLLER ASSY 2
50 83879-14 . BRACKET, ROLLER SUPPORT 2
ATTACHING PARTS
55 NAS6203-5 . BOLT 4
---*---
70 242 . THREADLOCKER (V05972) AR
80 NAS517-4-6 . SCREW 2
85 NAS1149F0432P . WASHER 2
90 MS21042-4 . NUT 2
110 83646-11 . BASE, END 1
ATTACHING PARTS
115 NAS6204-54 . BOLT 1
120 NAS6204-42 . BOLT 1
130 NAS1149F0432P . WASHER 2
140 MS21042-4 . NUT 2
---*---
225 40361-15 . STUD 2
250 43356-21 . WASHER 2
260 NAS1149F0532P . WASHER 2
280 MS21042-5 . NUT 2
300 87214-11 . CROSSTRACK 1

– NOT ILLUSTRATED

87226-A
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10118
Sep 1/19
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

IPL FIG. 16 NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10119
Jan 1/21
 COMPONENT MAINTENANCE MANUAL
PART NUMBER 85550

PART AIRLINE NOMENCLATURE USAGE UNITS

FIG PER
ITEM NUMBER PART NO. 1234567 CODE
ASSY
16
-1 85550-90 KIT, CONVERSION RF
(SEE IPL FIGURE 1 FOR NHA)
-30 81384-14 . RAIL ASSY, ROLLER 4
(SEE IPL FIGURE 5 FOR DETAILS)
-40 86963-18 . MAT ASSY, BALL 1
(SEE IPL FIGURE 10 FOR DETAILS)
-45 86963-19 . MAT ASSY, BALL 1
(SEE IPL FIGURE 10 FOR DETAILS)
-60 86974-16 . CROSSTRACK ASSY 24
(SEE IPL FIGURE 11 FOR DETAILS)
-65 86974-17 . CROSSTRACK ASSY 8
(SEE IPL FIGURE 11 FOR DETAILS)
-70 86974-18 DELETED D
(SEE IPL FIGURE 11 FOR DETAILS)
-70A 86974-28 . CROSSTRACK ASSY 4
(SEE IPL FIGURE 11 FOR DETAILS)
-80 86976-11 . CROSSTRACK ASSY 7
(SEE IPL FIGURE 12 FOR DETAILS)
-200 85338-90 . KIT, WALL PLACARD 1
-210 85334-13 . . NAMEPLATE 1
-220 85336-12 . . PLACARD, LOADING 1
-225 85034-42 . . PLACARD, WALL 1
-230 85034-43 . . PLACARD, WALL 1
-235 85034-44 . . PLACARD, WALL 1
-240 85034-45 . . PLACARD, WALL 1
-245 85034-46 . . PLACARD, WALL 1

- NOT ILLUSTRATED

85550-H
ANCRA PROPRIETARY
Unauthorized Use Prohibited 25-52-16 Pg.10120
Jan 1/21