COMPONENT MAINTENANCE MANUAL
WITH
ILLUSTRATED PARTS LIST
AFT LOWER COWL DOOR ASSEMBLY
PART NUMBER
5930640-1, -2, -501, -502, -503, -504, -505, -506, -507, -508
BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET
Copyright © 2003 The Boeing Company
Unpublished Work - All Rights Reserved
Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable
subject matter. Boeing also claims copyright in this document as a compilation and/or collective work.
This document includes proprietary information owned by The Boeing Company and/or one or more third parties.
Treatment of the document and the information it contains is governed by contract with Boeing. For more
information, contact The Boeing Company, P.O. Box 3707, Seattle, Washington 98124.
Boeing, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, 787, Dreamliner, BBJ,
DC-8, DC-9, DC-10, KC-10, KDC-10, MD-10, MD-11, MD-80, MD-88, MD-90, P-8A, Poseidon and the Boeing
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this document unless provided in writing by Boeing.
PUBLISHED BY BOEING COMMERCIAL AIRPLANES GROUP, SEATTLE, WASHINGTON, USA
A DIVISION OF THE BOEING COMPANY
PAGE DATE: Nov 01/2017
71-10-13
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5930640
COMPONENT MAINTENANCE MANUAL
Revision No. 16
Nov 01/2017
To: All holders of Aft Lower Cowl Door Assembly 71-10-13.
Attached is the current revision to this COMPONENT MAINTENANCE MANUAL
The COMPONENT MAINTENANCE MANUAL is furnished either as a printed manual, on microfilm, or digital
products, or any combination of the three. This revision replaces all previous microfilm cartridges or digital
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Pages replaced or made obsolete by this revision should be removed and destroyed.
ATTENTION
IF YOU RECEIVE PRINTED REVISIONS, PLEASE VERIFY THAT YOU HAVE RECEIVED AND FILED THE
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71-10-13
TRANSMITTAL LETTER
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COMPONENT MAINTENANCE MANUAL
LOCATION OF CHANGE
DESCRIPTION OF CHANGE
NO HIGHLIGHTS
71-10-13
HIGHLIGHTS
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COMPONENT MAINTENANCE MANUAL
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TITLE PAGE
1
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71-10-13
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5930640
COMPONENT MAINTENANCE MANUAL
TABLE OF CONTENTS
PARAGRAPH TITLE
PAGE
DESCRIPTION AND OPERATION
1
TESTING AND FAULT ISOLATION
(NOT-APPLICABLE)
AUTOMATIC TEST REQUIREMENTS (ATLAS)
(NOT-APPLICABLE)
DISASSEMBLY
301
CLEANING
401
CHECK
501
REPAIR
601
ASSEMBLY
701
FITS AND CLEARANCES
801
SPECIAL TOOLS, FIXTURES, AND EQUIPMENT
(NOT-APPLICABLE)
ILLUSTRATED PARTS LIST
1001
71-10-13
CONTENTS
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COMPONENT MAINTENANCE MANUAL
TEMPORARY REVISION AND SERVICE BULLETIN RECORD
BOEING SERVICE
BULLETIN
BOEING
TEMPORARY
REVISION
OTHER
DIRECTIVE
DATE OF INCORPORATION
INTO MANUAL
MD80-71-025
Feb 15/1982
MD80-71-026
Feb 15/1982
MD80-54–037
Oct 15/1986
MD80-71-029
Jan 15/1988
71-10-13
TR AND SB RECORD
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COMPONENT MAINTENANCE MANUAL
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revision number in numerical order, together with the revision date, the date filed and the initials of the person
filing.
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REVISION RECORD
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date the temporary revision is inserted and the initials of the person filing.
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5930640
COMPONENT MAINTENANCE MANUAL
INTRODUCTION
1. General
A.
The Component Maintenance Manual (CMM) with Illustrated Parts List (IPL) has been prepared to
give shop maintenance procedures for components made by The Boeing Company, Long Beach,
California.
Changes will be made to each CMM when necessary, and revisions will be sent as required. Each
revision will include a Highlights page with the airplane model effectivity, revision number, publication
date, and highlights of each change.
Information not included in the CMM can be found in the Maintenance Manual, Structural Repair
Manual, Nondestructive Testing Manual, Tool and Equipment Lists, Illustrated Parts Catalog, and
Wiring Diagram Manual.
This publication complies with the Air Transport Association of America (ATA) Specification No. 100.
2. Measurement Conversion
A.
When weights, dimensions, pressure, or torque values are changed to metric equivalents, they are
shown in parentheses after the English units.
3. Standard Practices
A.
Procedures for standard practices such as nondestructive testing, stripping, plating, refinishing,
shotpeening, etc., are in ATA Chapter 20. When necessary, each CMM will refer to the applicable
location in Chapter 20 for instructions.
4. Use of the Manual
A.
Each CMM contains tests or checks that should be done to find the condition or malfunction of the
unit, and the level of maintenance necessary to return it to a serviceable condition. If overhaul is
required, use Disassembly and Assembly instructions to remove and install parts to the level
necessary.
B.
Job set-up information is located at the front of major sections of each CMM, as applicable. Job
set-up information can include the charts that follow:
• References
• Tools/Equipment*
• Consumable Materials**
NOTE: *Equivalent substitutes are permitted for the listed tools and equipment. Tools with a part
number “TE” followed by characters in ATA chapter-section-subject format (TEXX-XX-XX) are
detailed in the applicable Tool and Equipment Lists. The tool reference numbers are used to
identify if a tool is a standard tool (STD-XXXX), a commercial tool (COM-XXXX), or a special
tool (SPL-XXXX). This reference number is also used to distinguish between tools with
similar names in the same procedure. These reference numbers are for use in the
documentation only. They are not to be used for ordering tools.
NOTE: **Equivalent substitutes are permitted for the listed consumable materials. The consumable
material reference numbers are used to distinguish between materials with similar names in
the same procedure. These reference numbers are for use in the documentation only. Use
the specification number, and not the reference number, for ordering consumable materials.
71-10-13
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COMPONENT MAINTENANCE MANUAL
C.
This CMM may include references to other manuals for additional overhaul or maintenance
procedures. When another Boeing Company CMM, OHM, or SOPM is referenced, make sure to use
the correct manual for the application. In some cases, there are two Boeing Company manuals with
the same ATA number: one for Boeing Heritage products (associated with CAGE Code 81205), the
other for Boeing Long Beach products (associated with CAGE Code 88277).
D.
Every part in the IPL is assigned an item number. The item numbers in the IPL correspond to those in
the CMM text. Items that are not illustrated in the IPL are excluded from the CMM text. Left-side parts
and assemblies are usually illustrated as typical, while right-side parts and assemblies are not
illustrated if they are a reverse image of the left side. Unless otherwise noted, all instructions for the
left-side parts and assemblies also apply to the non-illustrated, right-side parts and assemblies.
E.
If a vendor component that can be repaired is in the Disassembly, Repair, or Testing and Fault
Isolation sections, the CMM will refer to the applicable vendor manual (if available) for maintenance
instructions.
5. Measurement Abbreviations
A.
The following abbreviations may be used in this manual:
C
centigrade
dia
diameter
F
fahrenheit
ft
foot
gal.
gallon
Hg
mercury
hz
hertz
ID
inside diameter
in.
inch
kg
kilogram
kPa
kilopascals
kpsi
thousand pounds per square inch
l
liter
lb
pound
max
maximum
mBar
millibar
min
minute, minimum
mm
millimeter
N—m
newton meters
no.
number
OD
outside diameter
pH
hydrogen-ion concentration
psi
pounds per square inch
scc
standard cubic centimeter
vac
volts, alternating current
vdc
volts, direct current
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COMPONENT MAINTENANCE MANUAL
6.
Hazardous Materials
A.
General
(1)
This section lists all of the hazardous material warnings used in this manual.
HZ1000 - REFER TO MSDS
REFER TO THE APPLICABLE MANUFACTURER'S OR SUPPLIER'S MSDS FOR:
• MORE PRECAUTIONARY DATA
• APPROVED SAFETY EQUIPMENT
WARNING
• EMERGENCY MEDICAL AID.
TALK WITH THE LOCAL SAFETY DEPARTMENT OR AUTHORITIES FOR THE
PROCEDURES TO DISCARD THIS HAZARDOUS AGENT.
HZ1097 - SOLVENT/MIL-PRF-680 TYPE 1 (DPM 518)
MIL-PRF-680 TYPE 1 SOLVENT IS AN AGENT THAT IS FLAMMABLE AND
POISONOUS. MAKE SURE ALL PERSONS OBEY ALL OF THE PRECAUTIONS
WHEN MIL-PRF-680 TYPE 1 SOLVENT IS USED.
• DO NOT USE IN AREAS WHERE THERE IS HIGH HEAT, SPARKS, OR FLAMES.
• USE IN AN AREA OPEN TO THE AIR.
WARNING
• CLOSE THE CONTAINER WHEN NOT USED.
• DO NOT GET MIL-PRF-680 TYPE 1 SOLVENT IN THE EYES, ON THE SKIN, OR
ON YOUR CLOTHES.
• DO NOT BREATHE THE GAS.
HZ1107 - PRIMER/FR (DMS QPL 1786)
FR PRIMER IS AN AGENT THAT IS FLAMMABLE, POISONOUS, AN IRRITANT,
AND CARCINOGENIC. MAKE SURE ALL PERSONS OBEY ALL OF THE
PRECAUTIONS WHEN FR PRIMER IS USED.
• DO NOT USE IN AREAS WHERE THERE IS HIGH HEAT, SPARKS, OR FLAMES.
• USE IN AN AREA OPEN TO THE AIR.
WARNING
• CLOSE THE CONTAINER WHEN NOT USED.
• DO NOT GET FR PRIMER IN THE EYES, ON THE SKIN, OR ON YOUR
CLOTHES.
• DO NOT BREATHE THE GAS OR MIST.
71-10-13
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COMPONENT MAINTENANCE MANUAL
HZ1117 - COMPOUND/INTEGRAL FUEL TANKS SEALING (DMS QPL 2082 B1/2 AND B2)
INTEGRAL FUEL TANKS SEALING COMPOUND (POLYSULFIDE SEALANT B1/2
AND B2) IS AN AGENT THAT IS POISONOUS AND AN IRRITANT. MAKE SURE ALL
PERSONS OBEY ALL OF THE PRECAUTIONS WHEN INTEGRAL FUEL TANKS
SEALING COMPOUND IS USED.
• GAS/AIR MIXTURES MORE THAN THE LOWER EXPLOSIVE LIMIT (LEL) CAN
CAUSE AN EXPLOSION IF HIGH HEAT, SPARKS, OR FLAMES SUPPLY
IGNITION.
WARNING
• USE IN AN AREA OPEN TO THE AIR.
• CLOSE THE CONTAINER WHEN NOT USED.
• DO NOT GET INTEGRAL FUEL TANKS SEALING COMPOUND IN THE EYES,
ON THE SKIN, OR ON YOUR CLOTHES.
• DO NOT BREATHE THE GAS.
HZ1147 - RELEASE AGENT/MS-122 FLUOROCARBON (DPM 3494)
MS-122 FLUOROCARBON RELEASE AGENT IS AN AGENT THAT IS POISONOUS,
AN ASPHYXIANT, AND AN IRRITANT. MAKE SURE ALL PERSONS OBEY ALL OF
THE PRECAUTIONS WHEN MS-122 FLUOROCARBON RELEASE AGENT IS
USED.
• DO NOT USE IN AREAS WHERE THERE IS HIGH HEAT, SPARKS, OR FLAMES.
• USE IN AN AREA OPEN TO THE AIR.
WARNING
• CLOSE THE CONTAINER WHEN NOT USED.
• DO NOT GET MS-122 FLUOROCARBON RELEASE AGENT IN THE EYES, ON
THE SKIN, OR ON YOUR CLOTHES.
• DO NOT BREATHE THE GAS.
HZ1215 - ADHESIVE/EPOXY RESIN EA934NA (DPM 5535-2)
EPOXY RESIN EA934NA ADHESIVE IS AN AGENT THAT IS POISONOUS AND AN
IRRITANT. MAKE SURE ALL PERSONS OBEY THE PRECAUTIONS WHEN EPOXY
RESIN EA934NA ADHESIVE IS USED.
• DO NOT USE IN AREAS WHERE THERE IS HIGH HEAT, SPARKS, OR FLAMES.
• USE IN AN AREA OPEN TO THE AIR.
WARNING
• CLOSE THE CONTAINER WHEN NOT USED.
• DO NOT GET EPOXY RESIN EA934NA ADHESIVE IN THE EYES, ON THE SKIN,
OR ON YOUR CLOTHES.
• DO NOT BREATHE THE GAS.
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COMPONENT MAINTENANCE MANUAL
HZ1294 - PUTTY/FILLER/HI-BUILD/EPOXY (DPM 5765)
EPOXY HI-BUILD FILLER PUTTY IS AN AGENT THAT IS FLAMMABLE,
EXPLOSIVE, POISONOUS, AND AN IRRITANT. MAKE SURE ALL PERSONS OBEY
THE PRECAUTIONS WHEN EPOXY HI-BUILD FILLER PUTTY IS USED.
• GAS/AIR MIXTURES MORE THAN THE LOWER EXPLOSIVE LIMIT (LEL) CAN
CAUSE AN EXPLOSION IF HIGH HEAT, SPARKS, OR FLAMES SUPPLY
IGNITION.
WARNING
• USE IN AN AREA OPEN TO THE AIR.
• CLOSE THE CONTAINER WHEN NOT USED.
• DO NOT GET EPOXY HI-BUILD FILLER PUTTY IN THE EYES, ON THE SKIN,
OR ON YOUR CLOTHES.
• DO NOT BREATHE THE GAS.
HZ1333 - EPOXY PRIMER (DMS QPL 2104 TYPE 1)
EPOXY PRIMER IS AN AGENT THAT IS FLAMMABLE, EXPLOSIVE, POISONOUS,
CARCINOGENIC, AN ASPHYXIANT, A SENSITIZER, AND AN IRRITANT. MAKE
SURE ALL PERSONS OBEY THE PRECAUTIONS WHEN EPOXY PRIMER IS
USED.
• GAS/AIR MIXTURES MORE THAN THE LOWER EXPLOSIVE LIMIT (LEL) CAN
CAUSE AN EXPLOSION IF HIGH HEAT, SPARKS, OR FLAMES SUPPLY
IGNITION.
WARNING
• USE IN AN AREA OPEN TO THE AIR.
• CLOSE THE CONTAINER WHEN NOT USED.
• DO NOT GET EPOXY PRIMER IN THE EYES, ON THE SKIN, OR ON YOUR
CLOTHES.
• DO NOT BREATHE THE GAS.
HZ1422 - COATING/ANTI-CHAFE/COMPOSITION C/GRAY & WHITE (DPM 5066-3635/-7622)
ANTI-CHAFE COATING (COMPOSITION C) IS AN AGENT THAT IS FLAMMABLE,
EXPLOSIVE, POISONOUS, AND AN IRRITANT. MAKE SURE ALL PERSONS OBEY
THE PRECAUTIONS WHEN ANTI-CHAFE COATING (COMPOSITION C) IS USED.
• GAS/AIR MIXTURES MORE THAN THE LOWER EXPLOSIVE LIMIT (LEL) CAN
CAUSE AN EXPLOSION IF HIGH HEAT, SPARKS, OR FLAMES SUPPLY
IGNITION.
WARNING
• USE IN AN AREA OPEN TO THE AIR.
• CLOSE THE CONTAINER WHEN NOT USED.
• DO NOT GET ANTI-CHAFE COATING (COMPOSITION C) IN THE EYES, ON THE
SKIN, OR ON YOUR CLOTHES.
• DO NOT BREATHE THE GAS.
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COMPONENT MAINTENANCE MANUAL
HZ1492 - PAPER/GREASEPROOF (DPM 634 - Type 2/Grade A/Class 2)
GREASEPROOF PAPER IS AN ARTICLE THAT IS A LOW HAZARD. MAKE SURE
ALL PERSONS OBEY THE PRECAUTIONS WHEN GREASEPROOF PAPER IS
USED.
WARNING
• USE IN AN AREA OPEN TO THE AIR.
• CLOSE THE CONTAINER WHEN NOT USED.
HZ1497 - CLEANER/HANDWIPE (DPM 6380-1)
HANDWIPE CLEANER IS AN AGENT THAT IS FLAMMABLE, A SENSITIZER, AN
ASPHYXIANT, AND AN IRRITANT. MAKE SURE ALL PERSONS OBEY THE
PRECAUTIONS WHEN HANDWIPE CLEANER IS USED.
• DO NOT USE IN AREAS WHERE THERE IS HIGH HEAT, SPARKS, OR FLAMES.
• USE IN AN AREA OPEN TO THE AIR.
WARNING
• CLOSE THE CONTAINER WHEN NOT USED.
• DO NOT GET HANDWIPE CLEANER IN THE EYES, ON THE SKIN, OR ON
YOUR CLOTHES.
• DO NOT BREATHE THE GAS.
HZ1690 - POLYURETHANE TOPCOAT (DPM 6456)
POLYURETHANE TOPCOAT IS AN AGENT THAT IS FLAMMABLE, AND AN
IRRITANT. MAKE SURE ALL PERSONS OBEY THE PRECAUTIONS WHEN
POLYURETHANE TOPCOAT IS USED.
• DO NOT USE IN AREAS WHERE THERE IS HIGH HEAT, SPARKS, OR FLAMES.
• USE IN AN AREA OPEN TO THE AIR.
WARNING
• CLOSE THE CONTAINER WHEN NOT USED.
• DO NOT GET POLYURETHANE TOPCOAT IN THE EYES, ON THE SKIN, OR ON
YOUR CLOTHES.
• DO NOT BREATHE THE GAS.
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COMPONENT MAINTENANCE MANUAL
DESCRIPTION AND OPERATION
1. Description
A.
The aft lower cowl door assembly (Ref. DESCRIPTION AND OPERATION, Figure 1) attaches to the
apron assembly and covers the aft lower section of the engine. The door consists of hold open strut
assemblies, snubber assembly, hinges, safety latch, latch fittings, strake, straps, seals, cable
assemblies, retainers, and composite door assembly
2. Operation
A.
The door is manually opened when access to the aft lower section of the engine is required. The
snubber assembly prevents the door from opening too far and damaging the door or fuselage. The
door is retained in the open position by hold open strut assemblies, to facilitate engine maintenance.
3. Leading Particulars
A.
The aft lower cowl door assembly weighs approximately 59 pounds (27 kilograms).
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DESCRIPTION AND OPERATION
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COMPONENT MAINTENANCE MANUAL
Aft Lower Cowl Door
Figure 1
71-10-13
DESCRIPTION AND OPERATION
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COMPONENT MAINTENANCE MANUAL
TESTING AND FAULT ISOLATION
(NOT APPLICABLE)
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TESTING AND FAULT ISOLATION
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AUTOMATIC TEST REQUIREMENTS (ATLAS)
(NOT APPLICABLE)
71-10-13
AUTOMATIC TEST REQUIREMENTS (ATLAS)
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COMPONENT MAINTENANCE MANUAL
DISASSEMBLY
1. General
A.
This section contains the data necessary to disassemble the aft lower cowl door assembly.
B.
Refer to IPL Figure 1 for the item numbers.
2. Disassembly Procedures
NOTE: Door assembly should be checked to determine extent of maintenance required (Ref. CHECK).
A.
Standard Disassembly Procedures
(1)
Remove nut (5), washer (6), screw or bolt (7) and strake (8) from door assembly (121).
(2)
Remove nuts (15), washers (16 and 17), bolts (19), spacers (18), strut assemblies (21 and 22),
and adapters (20) from bolts (25).
(3)
Remove nuts (23), washers (24), bolts (25), and spacers (26) from brackets (29).
(4)
Remove bolts (27), washers (29), and brackets (29) from door assembly (121).
NOTE: If loose laminated shims (30) exist between bracket (29) and inserts, location and
thickness should be noted to aid in repair and assembly.
(5)
If necessary, remove sleeves (31 or 33D), pins (32 or 33C), and cables (33 or 33B) from
spacers (36 or 33E).
(6)
Remove screws (34 or 34C and 34E), washers (35 and 35C), spacers (36 or 33E), and retainers
(37) from block (37A) in door assembly (121).
(7)
Remove nut (38), washer (39), bolt (40), and snubber assembly (41) from bracket (44).
(8)
Remove bolts (42), washers (43), and bracket (44) from door assembly (121).
NOTE: If laminated shims (45) exist between bracket (44) and inserts, location and thickness
should be noted to aid in repair and assembly.
(9)
Remove rollpins (46) from door assembly (121).
(10)
Remove cotter pins (46E and 46G) from latch fittings (54).
(11)
Remove bolt assemblies (47) from latch fittings (54).
(12)
For 5930640-1 and -2, remove nuts (50), washers (51), jumper (51A), bolts (52 and 53), and
latch fittings (54) from door assembly (121).
NOTE: Termination points of jumper (51A) should be noted to aid in assembly.
(13)
For other configurations, remove nuts (50), washers (51), bolts (52 and 53), and latch fittings
(54) from door assembly (121).
NOTE: If loose laminated shims (55) exist between latch fittings (54) and inserts, location and
thickness should be noted to aid in repair and assembly.
(14)
For 5930640-1 and -2, remove nuts (56 and 58B), washers (57 and 58C), bolts (58, 58D, and
59), hinge (65), and hinge assemblies (60 and 66) from door assembly (121).
(15)
For other configurations, remove nuts (56), washers (57 and 57B, if installed), bolts (58 and 59),
hinge (65), and hinge assemblies (60 and 66) from door assembly (121).
NOTE: If installed, retain chamfered bottom washers (57B) for assembly.
NOTE: If loose laminated shims (71) exist between hinges (60, 63, and 69) and inserts, location
and thickness should be noted to aid in repair and assembly.
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DISASSEMBLY
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COMPONENT MAINTENANCE MANUAL
(16)
Remove nuts (72), washers (73), screws (74), spacers (75 and 76), spring (77), and latch
assembly (78) from bracket (81).
(17)
Remove bolts (79), washers (80), and bracket (81) from door assembly (121).
NOTE: If loose laminated shims (82) exist between bracket (81) and inserts, location and
thickness should be noted to aid in repair and assembly.
(18)
Remove seals (84 through 91) from retainers (93 through 99).
(19)
If necessary, remove rivets (92) and retainers (93 through 99).
(20)
If necessary, remove rivets (101) and retainer (102).
(21)
Remove rivets (103 or 103A), retainers (104, 105, 106, 107, 108 and 109) or washers (103B),
plate (104C), retainer assemblies (104B, 105B, 106B, 107B, 108B, and 109B), seals (110, 111,
112, 113, 114 and 115 or 110B, 111B, 112B, 113B, 114B and 115B), and if installed, straps
(115C, 115E, 115F, and 115H) from door assembly (121).
(22)
If damaged, remove rivets (116B) and rubstrip (116).
71-10-13
DISASSEMBLY
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COMPONENT MAINTENANCE MANUAL
CLEANING
1. General
A.
This section contains the data necessary to clean the aft lower cowl door assembly.
2. Cleaning Procedures
A.
Consumable Materials
NOTE: It is possible that some materials in the Consumable Materials chart cannot be used for some
or all of the necessary applications. Before you use the materials, make sure the types,
quantities, and applications of the materials necessary are legally permitted in your location.
All persons must obey all applicable federal, state, local, and provincial laws and regulations
when it is necessary to work with these materials.
B.
Reference
Description
Specification
B60087
Solvent - Cleaning
DPM 518 (MIL-PRF-680,
Type 1)
G60037
Air - Pure Dry
DPM 5148
G60428
Wipers - Cleaning, Cotton, White
DMS 1820 T1A2
Standard Cleaning Procedures
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF THIS
MANUAL.
WARNING
HAZMAT 1097, SOLVENT/MIL-PRF-680 TYPE 1 (DPM 518)
HAZMAT 1000, REFER TO MSDS
CAUTION
DO NOT USE STRIPPING SOLUTIONS ON COMPOSITE MATERIALS.
STRIPPING SOLUTIONS ATTACK BONDING AGENTS, AND DELAMINATION
MAY RESULT.
DO NOT USE CHLORINATED SOLVENTS ON TITANIUM PARTS. (TITANIUM
PARTS ARE IDENTIFIED WITH A (T) IN THE ILLUSTRATED PARTS LIST).
CAUTION
CAREFULLY CLEAN PARTS THAT HOUSE BEARINGS. DO NOT ALLOW
SOLVENT TO CONTACT SEALED LUBRICANT.
CAUTION
(1)
Clean parts thoroughly with cleaning solvent, B60087.
(2)
Rinse parts with clean cleaning solvent, B60087.
(3)
Dry parts immediately with clean, dry white cotton cleaning wipers, G60428 or pure dry air,
G60037.
NOTE: Parts must be free of dirt, grease, oil, and other contaminants.
71-10-13
CLEANING
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COMPONENT MAINTENANCE MANUAL
CHECK
1. General
A.
This section contains the data necessary to check the aft lower cowl door assembly.
B.
Refer to IPL Figure 1 for the item numbers.
2. Check Procedures
A.
B.
C.
References
Reference
Title
THE BOEING COMPANY
NDTSPM Part 07
Magnetic Particle Check
THE BOEING COMPANY
NDTSPM Part 08
Penetrant Check
General Visual Check
(1)
Check parts for cracks, corrosion, gouges, and other damage or deterioration.
(2)
Check threaded parts for stripping, cross-threading, and wear.
(3)
Check bearing housings of hinge assemblies (60 and 66). Housings must be free of nicks,
scratches, burrs, and corrosion.
(4)
Check seals (83 through 91 and 110 through 115B) for cracking, gouges, distortion, and
deterioration.
(5)
Check condition of cadmium plating on bolts (49).
Nondestructive Check
(1)
Magnetic-particle check latch fitting (54) and hinges (63, 65, and 69), refer to THE BOEING
COMPANY NDTSPM Part 07.
(2)
Fluorescent-penetrant check following parts, refer to THE BOEING COMPANY NDTSPM Part
08:
• Bracket (29)
• Spring (77)
• Extension assemblies (117 and 119)
D.
Check Spring (77)
(1)
E.
Check spring (77) for correct torque values, 10 to 12 inch-pounds shall be required to move
spring to initial position, and 11 to 13 inch-pounds shall be required to move spring to final
position (Ref. CHECK, Figure 501).
Check Snubber Assembly (41)
(1)
Check snubber assembly (41) for damage and proper operation.
(2)
Check spring tension on cables as follows:
(a)
Tension must be 5 pounds minimum with cable at full extension.
(b)
Tension must be 2 pounds minimum with cable at the cowl door closed position.
71-10-13
CHECK
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COMPONENT MAINTENANCE MANUAL
Spring Tension
Figure 501
71-10-13
CHECK
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COMPONENT MAINTENANCE MANUAL
F.
Check Strakes (8 and 9)
(1)
(2)
Check strakes (8 and 9) for damage. Acceptable damage limits are as follows:
(a)
Damage that does not reduce platform area more than 3 percent is acceptable.
(b)
Waviness along edges no greater than 0.250 inch (high point to low point) is acceptable.
(c)
Dents no greater than 0.250 inch deep in surface are acceptable.
Refer to REPAIR for instructions concerning damage that exceeds acceptable limits.
71-10-13
CHECK
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COMPONENT MAINTENANCE MANUAL
REPAIR
1. General
A.
This section contains the data necessary to repair the aft lower cowl door assembly.
B.
Refer to IPL Figure 1 for the item numbers.
2. Repair Procedures
A.
Tools/Equipment
NOTE: Equivalent substitutes may be used.
B.
Reference
Description
STD-128
Brush - Paint
STD-151
Cap - Air, No. 30
STD-152
Cap - Air, No. 765
STD-549
Knife - Putty, Broad Blade
STD-554
Lamp - Heat
STD-610
Non-metallic
STD-611
Nozzle and Needle - No. E
STD-612
Nozzle and Needle - No. FX
STD-4276
MBC Spray Gun with No. 514 Spray Assembly
STD-6634
Knife - Plastic
Consumable Materials
NOTE: It is possible that some materials in the Consumable Materials chart cannot be used for some
or all of the necessary applications. Before you use the materials, make sure the types,
quantities, and applications of the materials necessary are legally permitted in your location.
All persons must obey all applicable federal, state, local, and provincial laws and regulations
when it is necessary to work with these materials.
Reference
Description
Specification
A60017
Adhesive - Epoxy (Non-asbestos Filler)
DPM 5535-2
A60077
Compound - Sealing, Integral Fuel Tanks and Fuel
Cell Cavities
DMS 2082
A60172
Putty - Filler, Hi-Build, Epoxy 467-9 with CA-41B
Hardener
DPM 5765
B60016
Cleaner - Hand Wipe
DPM 6380-1
B60064
Release - Mold, Fluorocarbon
DPM 3494
C60066
Primer - Epoxy
DMS 2104, Type 1
C60068
Primer - Fluid Resistant
DMS 1786
C60168
Topcoat - Exterior Polyurethane, High Solids
DPM 6456
C60173
Coating - Anti-chafe, Composition C, White (DN 7622) DPM 5066
G60205
Paper - Abrasive, Silicon Carbide, Waterproof, 240
Grit
DPM 923
G60207
Paper - Abrasive, Silicon Carbide, Waterproof, 320
Grit
DPM 923
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REPAIR - GENERAL
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COMPONENT MAINTENANCE MANUAL
(Continued)
C.
D.
Reference
Description
Specification
G60215
Paper - Kraft, Neutral
DPM 640 (MIL-P-17667, Type
1)
G60248
Sandpaper - 280 Grit
DPM 919
G60350
Tape - Masking; Paper, Pressure Sensitive
DMS 1861 Type 2
G60428
Wipers - Cleaning, Cotton, White
DMS 1820 T1A2
G60884
Paper - Abrasive, Silicon Carbide, Waterproof, 280 to
320 Grit
DPM 923
References
Reference
Title
THE BOEING COMPANY
NDTSPM Part 08
Penetrant Check
THE BOEING COMPANY
SOPM 20-10-6
Repair of Plated Steel Parts Heat Treated 200 to 305 KPSI
THE BOEING COMPANY
SOPM 20-10-7
Bearing and Bushing Removal, Installation, and General Staking
DC9/MD80 SRM 51
Structural Repair Manual
General
(1)
Replace parts that do not meet requirements and cannot be reconditioned.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1107, PRIMER/FR (DMS QPL 1786)
HAZMAT 1000, REFER TO MSDS
(2)
Replace all loose or missing fasteners. Install all fasteners and shims in dissimilar metals in wet
condition; using paint brush, STD-128, brush apply or dip fasteners in fluid resistant primer,
C60068 prior to installation.
NOTE: If, after fastener removal or during installation, it is observed that installation hole or
countersink is oversize, the next larger fastener and/or countersink size may be used.
Washers should be used under expanded or bucked side of rivet, under bolt and screw
heads, and under nuts where composites provide the base material, to prevent
delamination at edge of fastener holes.
(3)
E.
Plating
(1)
F.
Repair damaged composite structure in accordance with DC9/MD80 SRM 51.
If necessary, recondition cadmium plating on all surfaces of bolts (49) (Ref. THE BOEING
COMPANY SOPM 20-10-6).
Repair Hinge Assemblies (60 and 66) and Hinge (65), if Necessary
NOTE: Damage exceeding the following maximum limits should be referred to Boeing Long Beach
Service Engineering for determination.
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G.
(1)
Any two damages to hinge or fitting should be at least 1 inch apart.
(2)
Nicks, scratches, and gouges 0.020 inch deep by 0.250 inch long maximum are allowed on
hinge surface without repair.
(3)
Nicks, scratches, and gouges deeper than 0.020 inch but not deeper than 0.040 inch and not
more than 0.350 inch long must be repaired by blending to remove sharp edges and abrupt
surface changes.
(4)
Cracks of any size are not allowed on bearing hole or pin bearing surface.
(5)
On hinge assemblies (60 and 66) a maximum of 0.813 inch diameter wear is allowed on bearing
hole. Install bearings (62 and 68) in hinges (63 and 69), refer to THE BOEING COMPANY
SOPM 20-10-7.
(6)
On hinge (65) a maximum of 0.010 inch deep wear and gouges is allowed on pin bearing
surface.
Repair Rubstrip (116), if Necessary
(1)
Remove rivets (116B) and rubstrip (116) from door assembly (121).
(2)
Install new rubstrip (116) on door assembly (121) using rivet (116B).
NOTE: Install rivets (116B) with manufactured head near side. Hand squeeze installation, no
bucking bar. Far side must be flush with 82 degree countersink, using 1.5 to 2.5 inch
spacing.
H.
Repair Anti-Chafe Coating, if Necessary
(1)
Scratches and gouges of any length in anti-chafe coating may be repaired, providing there is no
evidence of damage to composite structure. If damage to composite structure is evident, refer to
DC9/MD80 SRM 51.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1497, CLEANER/HANDWIPE (DPM 6380-1)
HAZMAT 1000, REFER TO MSDS
(2)
Thoroughly clean area to be repaired with white cotton cleaning wipers, G60428 moistened with
hand wipe cleaner, B60016.
(3)
Abrade area with 320 grit abrasive paper, G60207 to a matte appearance.
(4)
Clean area with white cotton cleaning wipers, G60428 dampened with hand wipe cleaner,
B60016, and dry with clean, dry white cotton cleaning wipers, G60428.
(5)
Mask off area to be repaired with neutral kraft paper, G60215 and masking tape, G60350.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1107, PRIMER/FR (DMS QPL 1786)
HAZMAT 1000, REFER TO MSDS
71-10-13
REPAIR - GENERAL
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(WARNING PRECEDES)
(6)
Using paint brush, STD-128, apply one uniform light coat of fluid resistant primer, C60068.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1422, COATING/ANTI-CHAFE/COMPOSITION C/GRAY & WHITE
(DPM 5066-3635/-7622)
HAZMAT 1000, REFER TO MSDS
(7)
Using paint brush, STD-128, apply two uniform wet brush coats of anti-chafe coating, C60173 to
obtain a dry film thickness of 0.008 to 0.010 inch. Allow coating to dry approximately 15 minutes
between coats.
NOTE: Refer to manufacturer's instructions for mixing and application procedures, chemical
reaction and drying times, and usable pot life.
NOTE: Coating may be spray appliedspray gun, STD-4276, No. E needle and nozzle, STD-611,
and No. 30 air cap, STD-151. If sprayed, apply 3 crosscoats to build a film thickness of
0.008 to 0.010 inch.
(8)
Allow anti-chafe coating, C60173 to air-dry for 24 hours at ambient temperature, or force-dry at
115° to 145°F (46° to 63°C) for 2 1/2 hours after 60 minutes air-dry.
NOTE: Anti-chafe coating must be free of pinholes, sags, runs, and dirt.
I.
Repair Liquid Shim Under Hinges and Latches, if Necessary
(1)
Damaged liquid shim may be repaired or replaced, providing there is no evidence of damage to
composite structure. If damage to composite structure is evident, refer to DC9/MD80 SRM 51.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1497, CLEANER/HANDWIPE (DPM 6380-1)
HAZMAT 1000, REFER TO MSDS
(2)
Clean surface thoroughly with white cotton cleaning wipers, G60428 moistened with hand wipe
cleaner, B60016; do not allow hand wipe cleaner, B60016 to evaporate on surface, wipe dry with
clean, dry white cotton cleaning wipers, G60428.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1147, RELEASE AGENT/MS-122 FLUOROCARBON (DPM 3494)
HAZMAT 1000, REFER TO MSDS
(3)
Apply two coats of fluorocarbon mold release, B60064 to mating surface of hinge or latch, and
allow to air-dry a minimum of 15 minutes.
71-10-13
REPAIR - GENERAL
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USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1215, ADHESIVE/EPOXY RESIN EA934NA (DPM 5535-2)
HAZMAT 1000, REFER TO MSDS
(4)
Fill damaged areas, gaps, and mismatches with epoxy adhesive, A60017, and install hinge or
latch while epoxy adhesive, A60017 is still wet.
NOTE: Refer to manufacturer's instructions for mixing and application procedures, chemical
reaction and drying times, and usable pot life.
NOTE: If loose laminated shims exist between inserts and latch or hinge, install as noted during
disassembly.
(5)
J.
K.
L.
Allow epoxy adhesive, A60017 to cure for 7 days at room temperature, or force-cure for 1 hour
at 200°F (93°C) or 2 hours at 150°F (66°C).
Repair Latch Assembly (78)
(1)
If necessary, remove rivets (78B) and cap (78C) from latch (78E).
(2)
Install serviceable cap (78C) on latch (78E) with rivets (78B).
Repair Strakes (8 and 9), if Necessary
(1)
If waviness along edges exceeds acceptable limits (Ref. CHECK), minor cold-forming may be
performed to restore strakes (8 and 9) to serviceable condition.
(2)
If dents in surface of strakes (8 and 9) exceed acceptable limits (Ref. CHECK), minor
cold-forming may be performed to restore strakes (8 and 9) to serviceable condition.
(3)
After all cold-forming operations, strakes (8 and 9) must be penetrant checked in accordance
with THE BOEING COMPANY NDTSPM Part 08.
Exterior Surface Paint
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF THIS
MANUAL.
WARNING
HAZMAT 1690, POLYURETHANE TOPCOAT (DPM 6456)
HAZMAT 1000, REFER TO MSDS
(1)
Repair or overcoating of exterior polyurethane topcoat, C60168 must be cured for a minimum of
45 days at ambient temperature or with an optional air-cure of 2 hours at ambient temperature
followed by heat-cure of 3 hours minimum at 160° to 180°F (71° to 82°C) prior to installation
onto aircraft and engine runup.
NOTE: Refer to manufacturer's instructions for mixing and application procedures, chemical
reaction and drying times, and usable pot life.
71-10-13
REPAIR - GENERAL
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COMPONENT MAINTENANCE MANUAL
M.
Repair Exterior Paint Cracks
(1)
Visible cracks in exterior paint around removable and hinged doors readily noticeable from a
distance of 5 feet and generally 1/2 to 4 inches long may be repaired in accordance with
following steps.
(2)
Remove foreign material from crack with a sharp non-metallic tool, STD-610.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
HAZMAT 1497, CLEANER/HANDWIPE (DPM 6380-1)
WARNING
HAZMAT 1117, COMPOUND/INTEGRAL FUEL TANKS SEALING
(DMS QPL 2082 B1/2 AND B2)
HAZMAT 1000, REFER TO MSDS
(3)
Clean area with clean white cotton cleaning wipers, G60428 moistened with hand wipe cleaner,
B60016, and wipe dry with clean, dry white cotton cleaning wipers, G60428 before it
evaporates.
(4)
Fill crack with sealing compound, A60077. Allow sealing compound, A60077 to air-cure 2 hours,
and finish curing at 140° to 160°F (60° to 71°C) for 90 minutes.
NOTE: Refer to manufacturer's instructions for mixing and application procedures, chemical
reaction and drying times, and usable pot life.
NOTE: Cure time at room temperature of 75° to 79°F (24° to 26°C) is 30 hours.
(5)
After sealing compound, A60077 has cured, abrade area and blend using 240 grit abrasive
paper, G60205 or finer.
(6)
Clean abraded area with clean white cotton cleaning wipers, G60428 moistened with hand wipe
cleaner, B60016, and wipe dry with clean, dry white cotton cleaning wipers, G60428 before it
evaporates.
(7)
If required, repair or replace aerodynamic, refer to REPAIR-GENERAL, Paragraph 2.N.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1333, EPOXY PRIMER (DMS QPL 2104 TYPE 1)
HAZMAT 1000, REFER TO MSDS
(8)
Apply epoxy primer, C60066 over repaired area, and allow to air-cure for 1 to 3 hours prior to
applying exterior polyurethane topcoat, C60168.
NOTE: Refer to manufacturer's instructions for mixing and application procedures, chemical
reaction and drying times, and usable pot life.
71-10-13
REPAIR - GENERAL
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USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1690, POLYURETHANE TOPCOAT (DPM 6456)
HAZMAT 1000, REFER TO MSDS
(9)
Apply one uniform wet overlapping single spray coat of exterior polyurethane topcoat, C60168
on repair area using spray gun, STD-4276, No. FX needle and nozzle, STD-612, and No. 765
air cap, STD-152, so as to blend in with adjacent area. Allow to air-cure 30 minutes to 2 hours
before applying additional coating. Air-cure coating at ambient temperature for 1 hour, and
heat-cure at 150° to 170°F (66° to 77°C) for 90 minutes.
NOTE: Refer to manufacturer's instructions for mixing and application procedures, chemical
reaction and drying times, and usable pot life.
(10)
N.
Blend in repair area by buffing.
Repair or Replace Aerodynamic Sealant, if Necessary
(1)
Damaged, missing, or loose aerodynamic sealant may be repaired or replaced, providing there
is no evidence of damage to composite structure. If damage to composite structure is evident,
refer to DC9/MD80 SRM 51.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1497, CLEANER/HANDWIPE (DPM 6380-1)
HAZMAT 1000, REFER TO MSDS
(2)
Clean surfaces to be repaired thoroughly with white cotton cleaning wipers, G60428 moistened
with hand wipe cleaner, B60016; do not allow hand wipe cleaner, B60016 to evaporate dry on
surfaces, wipe dry with clean white cotton cleaning wipers, G60428.
(3)
Mask off area to be repaired with neutral kraft paper, G60215 and masking tape, G60350.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1215, ADHESIVE/EPOXY RESIN EA934NA (DPM 5535-2)
HAZMAT 1000, REFER TO MSDS
(4)
Apply epoxy adhesive, A60017 to area being repaired, and tool flush to 0.002 inch below
surrounding surfaces. Remove excess epoxy adhesive, A60017 with white cotton cleaning
wipers, G60428 moistened with hand wipe cleaner, B60016.
NOTE: Refer to manufacturer's instructions for mixing and application procedures, chemical
reaction and drying times, and usable pot life.
71-10-13
REPAIR - GENERAL
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O.
Repair Exterior Paint Surfaces
(1)
Composite cowling exterior paint repair procedure.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1497, CLEANER/HANDWIPE (DPM 6380-1)
HAZMAT 1000, REFER TO MSDS
(a)
Remove loose and flaking coating. Wash surface with hand wipe cleaner, B60016 and
wipe dry. Feather sand edges of the peripheral coating as required. Sand the surface of
the laminate to be coated using 280 grit sandpaper, G60248 or finer. Remove sanding
residue.
(b)
Wash surface with hand wipe cleaner, B60016 and wipe dry.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1333, EPOXY PRIMER (DMS QPL 2104 TYPE 1)
HAZMAT 1000, REFER TO MSDS
(c)
Apply one coat of epoxy primer, C60066 as specified in the applicable finish specification.
Primer will air-dry in 1 hour at 70°F (21°C) minimum.
NOTE: Refer to manufacturer's instructions for application procedures, chemical reaction
and drying times, and usable pot life.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1690, POLYURETHANE TOPCOAT (DPM 6456)
HAZMAT 1000, REFER TO MSDS
(d)
Within 24 hours of applying epoxy primer, C60066, apply two coats of exterior
polyurethane topcoat, C60168 as specified in the applicable finish specification.
NOTE: Refer to manufacturer's instructions for mixing and application procedures,
chemical reaction and drying times, and usable pot life.
(e)
(2)
Air-dry for a minimum of 1 hour, followed by local application of heat lamps 160° to 180°F
(71° to 82°C) for a minimum of 2 hours.
Alternate procedure for composite exterior paint repair:
NOTE: If cosmetic surface fill is desired due to damage repair or other surface irregularities, the
following optional procedure may be utilized.
71-10-13
REPAIR - GENERAL
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COMPONENT MAINTENANCE MANUAL
(a)
Remove loose and flaking coating. Wash surface with hand wipe cleaner, B60016 and
wipe dry. Feather sand edges of the peripheral coating as required. Sand the surface of
the laminate to be coated using 280 grit sandpaper, G60248 or finer. Remove sanding
residue. Wash with hand wipe cleaner, B60016 and wipe dry.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1294, PUTTY/FILLER/HI-BUILD/EPOXY (DPM 5765)
HAZMAT 1000, REFER TO MSDS
(b)
Fill undesired surface irregularities by applying filler putty, A60172 with a broad blade putty
knife, STD-549 or plastic knife, STD-6634. Apply minimum amount of material. Remove
excess filler putty, A60172 before it dries.
(c)
Air-dry filler putty, A60172 for 45 minutes, followed by a force-cure at 160° to 180°F (71° to
82°C) for 1 hour.
(d)
Abrade surface with 280 to 320 grit abrasive paper, G60884.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1497, CLEANER/HANDWIPE (DPM 6380-1)
HAZMAT 1000, REFER TO MSDS
(e)
Wash with hand wipe cleaner, B60016 and wipe dry.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1333, EPOXY PRIMER (DMS QPL 2104 TYPE 1)
HAZMAT 1000, REFER TO MSDS
(f)
Apply one coat of epoxy primer, C60066 as specified in the applicable finish specification.
The epoxy primer, C60066 will air-dry in 1 hour at 70°F (21°C) minimum.
NOTE: Refer to manufacturer's instructions for mixing and application procedures,
chemical reaction and drying times, and usable pot life.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1690, POLYURETHANE TOPCOAT (DPM 6456)
HAZMAT 1000, REFER TO MSDS
71-10-13
REPAIR - GENERAL
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COMPONENT MAINTENANCE MANUAL
(WARNING PRECEDES)
(g)
Within 24 hours of applying epoxy primer, C60066, apply two coats of exterior
polyurethane topcoat, C60168 as specified in the applicable finish specification.
NOTE: Refer to manufacturer's instructions for mixing and application procedures,
chemical reaction and drying times, and usable pot life.
(h)
Air-dry for a minimum of 1 hour, followed by local application of heat lamps, STD-554, 160°
to 180°F (71° to 82°C) for a minimum of 2 hours.
71-10-13
REPAIR - GENERAL
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COMPONENT MAINTENANCE MANUAL
ASSEMBLY
1. General
A.
This section contains the data necessary to assemble the aft lower cowl door assembly.
B.
Refer to IPL Figure 1 for the item numbers.
2. Assembly Procedures
A.
Consumable Materials
NOTE: It is possible that some materials in the Consumable Materials chart cannot be used for some
or all of the necessary applications. Before you use the materials, make sure the types,
quantities, and applications of the materials necessary are legally permitted in your location.
All persons must obey all applicable federal, state, local, and provincial laws and regulations
when it is necessary to work with these materials.
B.
Reference
Description
Specification
A60077
Compound - Sealing, Integral Fuel Tanks and Fuel
Cell Cavities
DMS 2082
C60068
Primer - Fluid Resistant
DMS 1786
Dissimilar Metals Protection
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF THIS
MANUAL.
WARNING
HAZMAT 1107, PRIMER/FR (DMS QPL 1786)
HAZMAT 1000, REFER TO MSDS
(1)
Install all fasteners, except as noted in ASSEMBLY, Paragraph 2.B.(2), and shims in dissimilar
metals in wet condition. Dip fasteners in fluid resistant primer, C60068 or brush apply fluid
resistant primer, C60068 to holes prior to installation of fasteners.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1117, COMPOUND/INTEGRAL FUEL TANKS SEALING
(DMS QPL 2082 B1/2 AND B2)
HAZMAT 1000, REFER TO MSDS
(2)
C.
Install all fasteners attaching retainers and strake (8) in wet condition using sealing compound,
A60077.
Assembly Procedures
NOTE: If, after removal or during installation, it is observed that installation hole or countersink is
oversize, the next larger fastener and/or countersink size may be used. Washers should be
used under expanded or bucked side of rivets, under bolt and screw heads, and under nuts
where composites provide the base material, to prevent delamination at edge of fastener
holes.
(1)
If removed, install straps (115C, 115E, 115F, and 115H).
71-10-13
ASSEMBLY
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COMPONENT MAINTENANCE MANUAL
(2)
Install seals (110, 111, 112, 113, 114 and 115 or 110B, 111B, 112B, 113B, 114B and 115B) and
retainers (104, 105, 106, 107, 108, and 109) or washers (103B), plate (104C), and retainer
assemblies (104B, 105B, 106B, 107B, 108B, and 109B) on door assembly (121) with rivets (103
or 103A).
(3)
If removed, install retainer (102) on extension assemblies (117) with rivets (101).
(4)
If removed, install retainers (93 through 99) on door assembly (121) with rivets (92).
(5)
Install seals (83 through 91) in retainers (93 through 99).
(6)
Install bracket (81) on door assembly (121) with washers (80) and bolts (79). Torque bolts (79)
30 to 42 inch-pounds.
NOTE: If laminated shims (82) exist between inserts and bracket (81), install as noted during
disassembly.
(7)
Install latch assembly (78), spring (77), and spacers (75 and 76) on bracket (81) with screws
(74), washers (73), and nuts (72). Torque nuts (72) 20 to 25 inch-pounds.
(8)
For 5930640-1 and -2, install hinge (65) and hinge assemblies (60 and 66) on door assembly
(121) with bolts (58, 58D, and 59), washers (57 and 58C), and nuts (56 and 58B). Torque bolts
(59) 30 to 42 inch-pounds and nuts (56 and 58B) 50 to 70 inch-pounds.
(9)
For other configurations, install hinge (65) and hinge assemblies (60 and 66) on door assembly
(121) with bolts (58 and 59), washers (57 and 57B, if removed) and nuts (56). Torque bolts (59)
30 to 42 inch-pounds and nuts (56) 50 to 70 inch-pounds.
NOTE: If removed, install chamfered bottom washers (57B) with chamfer against fillet radius of
hinge (65).
NOTE: If loose laminated shims (71) exist between inserts and hinge (65) or hinge assemblies
(60 and 66), install as noted during disassembly.
(10)
For 5930640-1 and -2, install latch fittings (54) on door assembly (121) with bolts (52 and 53),
washers (51), jumper (51A), and nuts (50). Torque bolts (53) 30 to 42 inch-pounds and nuts (50)
50 to 70 inch-pounds.
(11)
For other configurations, install latch fittings (54) on door assembly (121) with bolts (52 and 53),
washers (51), and nuts (50). Torque bolts (53) 30 to 42 inch-pounds and nuts (50) 50 to 70
inch-pounds.
NOTE: If loose laminated shims (55) exist between inserts and latch fittings (54), install as
noted during disassembly.
(12)
Install bolt assemblies (47) in latch fittings (54).
(13)
Install rollpins (46) in door assembly (121).
(14)
For 5930640-503, -504, -505, and -506, install cotter pins (46E and 46G) in latch fittings (54).
Bend one leg of pin (46G) over casting step to prevent pin rotation (Ref. ASSEMBLY, Figure
701).
(15)
Install bracket (44) on door assembly (121) with washers (43) and bolts (42). Torque bolts (42)
30 to 42 inch-pounds.
NOTE: If laminated shims (45) exist between inserts and bracket (44), install as noted during
disassembly.
(16)
Install snubber assembly (41) on bracket (44) with bolt (40), washer (39), and nut (38). Torque
nut (38) 100 to 140 inch-pounds.
71-10-13
ASSEMBLY
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COMPONENT MAINTENANCE MANUAL
(17)
Install retainers (37) with spacers (33E and 36), washers (35 and 35C), and screws (34 or 34C
and 34E) through block (37A) on door assembly (121). Torque screws (34 or 34C and 34E) 30
to 42 inch-pounds.
(18)
If removed, install cables (33 or 33B), pins (32 or 33C), and sleeves (31 or 33D) on spacers (36
or 33E).
(19)
Install brackets (29) on door assembly (121) with washers (28) and bolts (27). Torque bolts (27)
30 to 42 inch-pounds.
(20)
Install spacers (26), bolts (25), washers (24), and nuts (23) on brackets (29). Torque nuts (23)
100 to 140 inch-pounds.
(21)
Install adapters (20) and strut assemblies (21 and 22) on bolts (25) with spacers (18), bolts (19),
washers (16 and 17), and nuts (15). Torque nuts (15) 20 to 25 inch-pounds.
(22)
Install strake (8) on door assembly (121) with bolts (7), washers (6), and nuts (5). Torque nuts
(5) 50 to 70 inch-pounds.
(23)
If removed, install serviceable rubstrip (116) with rivets (116B).
71-10-13
ASSEMBLY
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COMPONENT MAINTENANCE MANUAL
Cotter Pin Installation
Figure 701
71-10-13
ASSEMBLY
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5930640
COMPONENT MAINTENANCE MANUAL
3. Storage Instructions
A.
Consumable Materials
NOTE: It is possible that some materials in the Consumable Materials chart cannot be used for some
or all of the necessary applications. Before you use the materials, make sure the types,
quantities, and applications of the materials necessary are legally permitted in your location.
All persons must obey all applicable federal, state, local, and provincial laws and regulations
when it is necessary to work with these materials.
B.
Reference
Description
Specification
G60213
Paper - Greaseproof, Waterproof
DPM 634 (MIL-PRF-121,
Type 2, Grade A, Class 2)
G60295
Tag - Identification
DMS 2409, Class 1
Storage Procedures
(1)
Mark part number on two identification tags, G60295. Attach one identification tag, G60295 to
unit and one identification tag, G60295 to exterior of container.
USE THE HAZARDOUS MATERIAL WARNINGS GIVEN BELOW FOR THE
STEPS THAT FOLLOW.
HAZMAT WARNINGS ARE LISTED IN THE INTRODUCTION SECTION OF
THIS MANUAL.
WARNING
HAZMAT 1492, PAPER/GREASEPROOF (DPM 634 - Type 2/Grade A/Class 2)
HAZMAT 1000, REFER TO MSDS
(2)
Wrap cowl door in barrier material, G60213, and place in suitable container.
(3)
Store unit in clean, dry area.
71-10-13
ASSEMBLY
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5930640
COMPONENT MAINTENANCE MANUAL
FITS AND CLEARANCES
1. General
A.
This section contains the torque value data for the aft lower cowl door assembly.
B.
Refer to IPL Figure 1 for the item numbers.
2. Fits and Clearances Procedures
A.
Torque Values
NOTE: Fasteners tighten from the head end must be tightened to the high value of the torque range.
(1)
Refer to FITS AND CLEARANCES, Table 801 for torque values.
Table 801: Torque Values
Item
Torque Values
Nuts (15 and 72)
20 to 25 inch-pounds
Bolts (27, 42, 53, 59, and 79)
30 to 42 inch-pounds
Screw (34, 34C, and 34E)
30 to 42 inch-pounds
Nuts (5, 50, 56, and 58B)
50 to 70 inch-pounds
Nuts (23 and 38)
100 to 140 inch-pounds
71-10-13
FITS AND CLEARANCES
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5930640
COMPONENT MAINTENANCE MANUAL
SPECIAL TOOLS, FIXTURES, AND EQUIPMENT
(NOT APPLICABLE)
71-10-13
SPECIAL TOOLS, FIXTURES, AND EQUIPMENT
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5930640
COMPONENT MAINTENANCE MANUAL
ILLUSTRATED PARTS LIST
1. Introduction
A.
General
(1)
The Illustrated Parts List is a breakdown, in disassembly order, of assemblies and detail parts
that make up the unit identified in the manual.
The item numbers shown in the parts list are the same as the item numbers on the exploded
view illustration(s). To find a part number, find the part on the illustration(s) and look at the item
number. Find the item number in the parts list and read the correct part number.
B.
Abbreviations
(1)
The following abbreviations are used in the parts list:
Term
Abbreviation
Definition
Post All Operator Letter
POST AOL
The part replaces or is added by the
noted All Operator Letter.
Post Service Bulletin
POST SB
The part replaces or is added by the
noted Service Bulletin.
Post Service Letter
POST SL
The part replaces or is added by the
noted Service Letter.
Specification
SPEC
The vendor part meets the requirements
defined in the noted Boeing Specification
Control Drawing.
Pre All Operator Letter
PRE AOL
The part is replaced or deleted by the
noted All Operator Letter.
Pre Service Bulletin
PRE SB
The part is replaced or deleted by the
noted Service Bulletin.
Pre Service Letter
PRE SL
The part is replaced or deleted by the
noted Service Letter.
Interchangeable with
INTCHG/W
The old part MAY be used
interchangeably with the new part.
Not interchangeable with
NOT INTCHG/W
The old part MAY NOT be used
interchangeably with the new part.
Optional part
OPT
The optional part can be used as an
alternate for the original part.
For Next Higher Assembly see FOR NHA SEE
Cross references the locations of a
subassembly and its next higher
assembly.
Reworked by Service Bulletin
REWORKED BY SB
The part has been modified by the noted
Service Bulletin or drawing.
Select as required
SELECT AR
Select the part from a range of sizes to
meet assembly requirements.
Titanium Part
T
The part is made of titanium and should
not be cleaned with chlorinated solvents.
Left Hand
LH
Left-hand part
Right Hand
RH
Right-hand part
71-10-13
ILLUSTRATED PARTS LIST
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5930640
COMPONENT MAINTENANCE MANUAL
C.
Installation Parts
Items listed under the heading “INSTALLATION PARTS” are not part of the assembly but may be
attached at the time of overhaul.
D.
Usage Codes
When more than one configuration is shown in the parts list, usage codes identify the different detail
parts used on different configurations. No usage code is used for detail parts and subassemblies
used on all configurations.
In addition to usage codes, which show the relationship of detail parts and assemblies to the end item
production configuration, parenthetical notes are placed in the NOMENCLATURE column to reflect
replacement of parts and interchangeability of parts.
E.
Units Per Assembly
The UNITS PER ASSEMBLY column shows the total number of units used per assembly. The letters
AR are used for as required bulk items or adjustable quantity items such as shims, spacers, or similar
items. If the item is listed for reference purposes, the letters RF are used.
F.
Illustrations
A view of each assembly or subassembly, exploded as necessary to show the component parts, is
provided to illustrate the parts included in the parts list. Items preceded by a dash (-) in the parts list
are not illustrated.
G.
Assembly Indenture System
The relation of each item to its next higher assembly (NHA) is shown in the NOMENCLATURE
column. Use the indenture system that follows:
H.
1
2
.
Detail parts
3
4
.
Assembly
.
Attaching parts for assembly
5
6
7
.
.
Detail parts for assembly
.
.
Subassembly
.
.
Attaching parts for subassembly
.
.
.
Detail parts for subassembly
.
.
.
Sub-subassembly
.
.
.
Attaching parts for sub-subassembly
.
.
.
.
Detail parts for sub-subassembly
Service Bulletin Incorporation
Part numbers deleted by service bulletins will include the note (PRE SB XX-XXX) in the
NOMENCLATURE column.
Part numbers added by service bulletins will include the note (POST SB XX-XXX) in the
NOMENCLATURE column.
I.
Numerical Index
For manuals in a pageblock format, a numerical index is provided.
J.
Reference Designator Index
Whenever electrical and electronic components are listed in the parts list, a reference designator to
part number index is provided.
71-10-13
ILLUSTRATED PARTS LIST
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COMPONENT MAINTENANCE MANUAL
K.
How to use the Parts List
When the part number is known, look in the parts list for the item number, nomenclature, effectivity,
quantity, etc. Refer to the applicable illustration for a view and location of the part.
When the part number is not known, find the part and its item number in the illustration. Refer to the
applicable parts list for the part number, nomenclature, effectivity, quantity, etc.
L.
Vendor Parts
Parts manufactured by companies other than The Boeing Company will show the manufacturer’s
code preceded by the letter V, and enclosed in parentheses, following the nomenclature. If required, a
reference to the vendor manual will follow the vendor code. Example: (V99250) (Ref. 29-09-09). The
vendor code is obtained from Defense Logistics Cataloging Handbook H4/H8, Commercial and
Government Entity (CAGE). Each manual contains a list of vendors that appear in the manual.
Vendors are listed in the Illustrated Parts List section numerically by code, along with their name and
address. Vendors that have no assigned code will be arranged in alphabetical order by name at the
beginning of the list of vendors.
VENDOR CODES
Code
Name
08844
MARATHONNORCO AEROSPACE, INC., NORCO
8301 IMPERIAL DR
WACO, TX 76712-6524
09455
RBC TRANSPORT DYNAMICS CORP
3131 W SEGERSTROM AVE
SANTA ANA, CALIFORNIA 92704-5872
FORMERLY TRANSPORT DYNAMICS AEROSPACE DIV; FABROID DIV
TRANSPORT DYNAMICS V17571 & LEAR SEIGLER INC TRANSPORT DIV
V98076; FORMERLY BFM TRANSPORT DYNAMICS
17446
HUCK INTL INC AEROSPACE FASTENER DIV
900 WATSON CENTER ROAD
CARSON, CALIFORNIA 90745-4201
FORMERLY V32134 REXNORD INC; FORMERLY V97928 HUCK INTL
17816
SPECTRA LUX CORP.
11825 120TH AVENUE NE
KIRKLAND, WASHINGTON 98034
FORMERLY JENSEN, RAYMOND W INDUSTRIES IN SEGUNDO
CALIFORNIA
29372
ALCOA GLOBAL FASTENERS INC DBA ALCOA FASTENERS SYSTEMS DIV
3000 WEST LOMITA BLVD
TORRANCE CALIFORNIA 90505-5103
FORMERLY CALFAX INC V11907; NEWTON INSERT CO V98004;REXNORD
INC SPECIALTY FASTERNER DIV AND DELRON CO V82831; REXNORD
INC TRIDAIR IND; FORMERLY FAIRCHAIDL IND INC
32134
REXNORD INC ROCKFORD AEROSPACE PRODUCTS INC
SANTA ANA, CALIFORNIA 92714
FACILITIES DISCONTINUED
73197
HI-SHEAR TECHNOLOGY CORP
2600 SKYPARK DRIVE
TORRANCE, CALIFORNIA 90509
71-10-13
ILLUSTRATED PARTS LIST
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5930640
COMPONENT MAINTENANCE MANUAL
Code
Name
76691
NATIONAL TELEPHONE SUPPLY COMPANY
5100 SUPERIOR AVENUE
CLEVELAND, OHIO 44103-1240
71-10-13
ILLUSTRATED PARTS LIST
Page 1004
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5930640
COMPONENT MAINTENANCE MANUAL
NUMERICAL INDEX
FIGURE
ITEM
UNITS PER
ASSEMBLY
1
62
1
1
68
1
1
31
4
1
33D
2
2959085-501
1
20
2
3938112-1
1
44
1
3938180-1
1
29
2
4938067-1
1
77
1
4938093-1
1
76
2
4958704-1
1
37
2
4959138-1
1
17
4
5930639-11
1
78E
1
5930639-141
1
78
1
5930639-143
1
78E
1
5930639-145
1
78C
1
5930639-147
1
81
1
5930639-201
1
104C
1
5930639-3
1
78
1
5930639-59
1
78C
1
5930639-9
1
81
1
1
81
1
5930640-1
1
1
RF
5930640-100
1
95A
1
5930640-101
1
96
1
5930640-103
1
98A
1
5930640-104
1
98A
1
5930640-105
1
99
1
5930640-107
1
89
1
5930640-109
1
88
1
5930640-111
1
87
1
5930640-113
1
86
1
5930640-115
1
85
1
5930640-117
1
84
1
5930640-119
1
83
1
5930640-13
1
93
1
PART NUMBER
03-505-06E015
28-1C
AIRLINE PART NUMBER
71-10-13
ILLUSTRATED PARTS LIST
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5930640
COMPONENT MAINTENANCE MANUAL
FIGURE
ITEM
UNITS PER
ASSEMBLY
5930640-133
1
91
1
5930640-135
1
46
3
5930640-137
1
110
1
5930640-139
1
111
1
5930640-141
1
112
1
5930640-143
1
113
1
5930640-145
1
114
1
5930640-147
1
115
1
5930640-149
1
110
1
5930640-151
1
111
1
5930640-153
1
112
1
5930640-155
1
113
1
5930640-157
1
114
1
5930640-159
1
115
1
5930640-161
1
46
3
5930640-163
1
116
1
5930640-165
1
46
3
5930640-167
1
110B
1
5930640-169
1
111B
1
5930640-17
1
96
1
5930640-171
1
112B
1
5930640-173
1
113B
1
5930640-175
1
114B
1
5930640-177
1
115B
1
5930640-179
1
104B
1
5930640-181
1
105B
1
5930640-183
1
106B
1
5930640-185
1
107B
1
5930640-187
1
108B
1
5930640-189
1
109B
1
5930640-2
1
2
RF
5930640-215
1
46
3
5930640-217
1
115H
4
5930640-219
1
115E
1
1
115F
2
1
115C
2
PART NUMBER
5930640-221
AIRLINE PART NUMBER
71-10-13
ILLUSTRATED PARTS LIST
Page 1006
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIGURE
ITEM
UNITS PER
ASSEMBLY
5930640-223
1
115C
2
5930640-225
1
115F
2
5930640-227
1
37A
1
5930640-23
1
46
3
5930640-25
1
89
1
5930640-27
1
99
1
5930640-3
1
116
1
5930640-41
1
104
1
5930640-43
1
105
1
5930640-49
1
108
1
5930640-5
1
83
1
5930640-501
1
2
RF
5930640-502
1
2
RF
5930640-503
1
2
RF
5930640-504
1
2
RF
5930640-505
1
2
RF
5930640-506
1
2
RF
5930640-507
1
2
RF
5930640-508
1
2
RF
5930640-51
1
109
1
5930640-53
1
102
1
5930640-57
1
91
1
5930640-59
1
106
1
5930640-63
1
107
1
5930640-67
1
33
2
5930640-69
1
84
1
5930640-71
1
85
1
5930640-73
1
87
1
5930640-75
1
88
1
5930640-77
1
94
1
5930640-79
1
95
1
5930640-81
1
97
1
5930640-83
1
98
1
5930640-85
1
104
1
5930640-87
1
105
1
5930640-89
1
106
1
PART NUMBER
AIRLINE PART NUMBER
71-10-13
ILLUSTRATED PARTS LIST
Page 1007
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIGURE
ITEM
UNITS PER
ASSEMBLY
5930640-9
1
86
1
5930640-91
1
107
1
5930640-93
1
108
1
5930640-95
1
109
1
5930640-97
1
93
1
5930640-99
1
95A
1
5930649-71
1
33B
1
5930649-73
1
33A
2
5938073-1
1
121
1
5938084-1
1
54
3
5938084-501
1
54
3
5938085-1
1
60
1
5938085-2
1
61
1
5938085-5
1
63
1
5938085-6
1
64
1
5938086-1
1
65
1
5938087-1
1
66
1
5938087-2
1
67
1
5938087-5
1
69
1
5938087-6
1
70
1
5938118-503
1
117
1
5938118-504
1
118
1
5938118-505
1
119
1
5938118-506
1
120
1
5938118-509
1
117
1
5938118-510
1
118
1
5938118-511
1
119
1
5938118-512
1
120
1
5938118-513
1
119
1
1
120
1
5938122-21
1
14
1
5938122-23
1
12
1
5938122-25
1
11
2
5938122-3
1
11
2
5938122-5
1
12
1
5938122-501
1
3
1
PART NUMBER
AIRLINE PART NUMBER
71-10-13
ILLUSTRATED PARTS LIST
Page 1008
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIGURE
ITEM
UNITS PER
ASSEMBLY
5938122-502
1
4
1
5938122-505
1
3
1
5938122-506
1
4
1
5938122-6
1
13
1
5938122-7
1
14
1
5938123-501
1
8
1
5938123-502
1
9
1
5938136-1
1
121
1
5938219-1
1
121
1
5938219-2
1
121
1
703100-2
1
41
1
7958530-511
1
41
1
A2711-5
1
21
1
A2711-9
1
22
1
AN45C5A
1
25
2
AN960-3L
1
73A
2
AN960-516
1
24
2
AN960C10L
1
35
2
AN960C416
1
35C
2
AN960C416L
1
28
4
1
35
2
1
43
2
1
51
12
1
57
11
1
57
15
1
57B
2
1
80
2
AN960C516L
1
39
1
AN960D4
1
103B
2
AN960D416
1
6
14
AN960JD10LL
1
16
8
AN960PD10L
1
16
8
CSR904B5
1
116B
AR
D169HE365-16
1
37B
2
D169HE465-16
1
45A
2
1
55A
6
PART NUMBER
AIRLINE PART NUMBER
71-10-13
ILLUSTRATED PARTS LIST
Page 1009
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIGURE
ITEM
UNITS PER
ASSEMBLY
1
71B
9
1
82B
2
D16HE465-16
1
30A
4
HL10V8-5
1
58D
4
MS20426AD4
1
92
AR
1
103A
AR
MS20426AD5
1
103
AR
MS20470B4
1
116B
AR
MS206153M
1
78B
AR
MS20615M3
1
101
2
MS21042L3
1
72
2
MS21042L4
1
5
14
MS21042L5
1
38
1
MS21043-3
1
15
2
MS21043-4
1
50
6
1
56
10
1
23
2
1
38
1
1
15
2
1
15
2
1
50
6
1
50
6
1
56
2
1
56
10
1
23
2
1
23
2
1
38
1
1
38
1
MS24665-195
1
46E
6
MS24665-304
1
46E
3
MS24665-306
1
46G
3
MS25083-2CC6
1
51A
1
NAS1097AD5
1
116B
AR
NAS1149C0332R
1
35
2
NAS1149C0432R
1
28
4
1
35
2
PART NUMBER
D169HE465-16 (Cont.)
MS21043-5
MS21043L3
MS21043L4
MS21043L5
AIRLINE PART NUMBER
71-10-13
ILLUSTRATED PARTS LIST
Page 1010
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIGURE
ITEM
UNITS PER
ASSEMBLY
1
43
2
1
51
12
1
57
11
1
57
15
1
57B
2
1
80
2
NAS1149C0463R
1
35C
2
NAS1149C0532R
1
39
1
NAS1149D0316J
1
16
8
NAS1149D0463H
1
6
14
NAS1149DN432H
1
103B
2
NAS1149F0563P
1
24
2
NAS1149FN316P
1
73A
2
NAS1739M5
1
100
8
NAS1739M5-3
1
10
AR
NAS334CPA6
1
7
14
NAS43HT3-80
1
75
2
NAS43HT5-8
1
26
2
NAS463TC10
1
33E
1
NAS463TC416
1
33E
1
1
36
2
1
52
6
1
58
2
1
58
6
NAS6205-32
1
40
1
NAS623-3-2
1
34E
1
NAS623-3-23
1
74
2
NAS623-3-3
1
34
2
1
34E
1
NAS623-3-4
1
34C
1
NAS623-3-8
1
34C
1
NAS623-4-3
1
34
2
NAS6403U7
1
19
2
NAS6404U3
1
27
4
1
42
2
1
53
6
PART NUMBER
NAS1149C0432R (Cont.)
NAS4904U3
AIRLINE PART NUMBER
71-10-13
ILLUSTRATED PARTS LIST
Page 1011
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIGURE
ITEM
UNITS PER
ASSEMBLY
1
59
9
1
79
2
1
40
1
1
40
1
NAS679A4W
1
58B
4
NAS7304U5
1
7
14
NO. 2
1
32
2
1
33C
1
RA22045
1
47
3
RA22045-5
1
49
1
RA22045-7
1
48
1
S1026614-3-007
1
18
4
S124682-4R10-3
1
58C
4
S2431221-4C8F
1
30
AR
1
45
AR
1
55
AR
1
71
AR
1
82
AR
PART NUMBER
NAS6404U3 (Cont.)
NAS6405U32
AIRLINE PART NUMBER
71-10-13
ILLUSTRATED PARTS LIST
Page 1012
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
Aft Lower Cowl Door Assembly
IPL Figure 1 (Sheet 1 of 3)
71-10-13
ILLUSTRATED PARTS LIST
Page 1013
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
Aft Lower Cowl Door Assembly
IPL Figure 1 (Sheet 2 of 3)
71-10-13
ILLUSTRATED PARTS LIST
Page 1014
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
Aft Lower Cowl Door Assembly
IPL Figure 1 (Sheet 3 of 3)
71-10-13
ILLUSTRATED PARTS LIST
Page 1015
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIG/
ITEM
PART NUMBER
1–
AIRLINE
PART
NUMBER
NOMENCLATURE
1234567
USAGE
CODE
UNITS
PER
ASSY
AFT LOWER COWL DOOR ASSEMBLY
–1
5930640-1
DOOR ASSY-AFT LOWER COWL LH
A
RF
–2
5930640-2
DOOR ASSY-AFT LOWER COWL RH
B
RF
–2
5930640-501
DOOR ASSY-AFT LOWER COWL LH
C
RF
–2
5930640-502
DOOR ASSY-AFT LOWER COWL RH
D
RF
–2
5930640-503
DOOR ASSY-AFT LOWER COWL LH
E
RF
–2
5930640-504
DOOR ASSY-AFT LOWER COWL RH
F
RF
–2
5930640-505
DOOR ASSY-AFT LOWER COWL LH
G
RF
–2
5930640-506
DOOR ASSY-AFT LOWER COWL RH
H
RF
–2
5930640-507
DOOR ASSY-AFT LOWER COWL LH
I
RF
–2
5930640-508
DOOR ASSY-AFT LOWER COWL RH
J
RF
3
5938122-501
. STRAKE INSTL-LH
A
1
3
5938122-505
. STRAKE INSTL-LH
C, E, G
1
–4
5938122-502
. STRAKE INSTL-RH
B
1
–4
5938122-506
. STRAKE INSTL-RH
D, F, H
1
5
MS21042L4
. . NUT
A-H
14
6
NAS1149D0463H
. . WASHER
(OPT AN960D416)
A-H
14
7
NAS334CPA6
. . SCREW
(PRE SB MD80-54-037)
A-B
14
7
NAS7304U5
. . BOLT-(T)
(POST SB MD80-54-037)
C-H
14
8
5938123-501
. . STRAKE
A, C, E, G
1
–9
5938123-502
. . STRAKE
B, D, F, H
1
10
NAS1739M5-3
. . RIVET
A-H
AR
11
5938122-3
. . BRACKET
A-B
2
11
5938122-25
. . BRACKET
C-H
2
12
5938122-5
. . BRACKET
A
1
12
5938122-23
. . BRACKET
C-H
1
–13
5938122-6
. . BRACKET
B
1
14
5938122-7
. . BRACKET
A-B
1
14
5938122-21
. . BRACKET
C-H
1
15
MS21043L3
. NUT
A-B
2
15
MS21043L3
. NUT
(REPLACED BY MS21043-3)
C-F
2
15
MS21043-3
. NUT
C-J
2
71-10-13
– Item not Illustrated
ILLUSTRATED PARTS LIST
Page 1016
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIG/
ITEM
PART NUMBER
1–
AIRLINE
PART
NUMBER
NOMENCLATURE
USAGE
CODE
1234567
UNITS
PER
ASSY
AFT LOWER COWL DOOR ASSEMBLY
16
AN960PD10L
. WASHER
(REPLACED BY NAS1149D0316J)
8
16
NAS1149D0316J
. WASHER
(OPT AN960JD10LL)
8
17
4959138-1
. WASHER
4
18
S1026614-3-007
. SPACER
4
19
NAS6403U7
. BOLT-(T)
2
20
2959085-501
. ADAPTER
2
21
A2711-5
. STRUT ASSY
(V08844)
1
22
A2711-9
. STRUT ASSY
(V08844)
1
23
MS21043L5
. NUT
A-B
2
23
MS21043L5
. NUT
(REPLACED BY MS21043-5)
C-H
2
23
MS21043-5
. NUT
C-J
2
24
NAS1149F0563P
. WASHER
(OPT AN960-516)
2
25
AN45C5A
. BOLT
2
26
NAS43HT5-8
. SPACER
2
27
NAS6404U3
. BOLT-(T)
4
28
NAS1149C0432R
. WASHER
(OPT AN960C416L)
4
29
3938180-1
. BRACKET
2
30
S2431221-4C8F
. SHIM-LAMINATED
AR
–30A
D16HE465-16
. INSERT
(V29372)
4
31
28-1C
. SLEEVE
(V76691)
A-B
4
32
NO. 2
. PIN
A-B
2
33
5930640-67
. CABLE
A-B
2
33A
5930649-73
. CABLE ASSY
C-J
2
33B
5930649-71
. . CABLE
C-J
1
33C
NO. 2
. . PIN
C-J
1
33D
28-1C
. . SLEEVE
(V76691)
C-J
2
33E
NAS463TC416
. . SPACER
(REPLACED BY NAS463TC10)
C-J
1
71-10-13
– Item not Illustrated
ILLUSTRATED PARTS LIST
Page 1017
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIG/
ITEM
PART NUMBER
1–
AIRLINE
PART
NUMBER
NOMENCLATURE
1234567
USAGE
CODE
UNITS
PER
ASSY
AFT LOWER COWL DOOR ASSEMBLY
33E
NAS463TC10
. . SPACER
C-J
1
34
NAS623-4-3
. SCREW
(USED WITH D169HE465-16)
(REPLACED BY NAS623-3-3)
A-B
2
34
NAS623-3-3
. SCREW
(USED WITH D169HE365-16)
C-F
2
34C
NAS623-3-4
. SCREW
(USED WITH D169HE365-16)
(REPLACED BY NAS623-3-8)
G-J
1
34C
NAS623-3-8
. SCREW
(USED WITH D169HE365-16)
G-J
1
34E
NAS623-3-3
. SCREW
(USED WITH D169HE365-16)
(REPLACED BY NAS623-3-2)
G-J
1
34E
NAS623-3-2
. SCREW
(USED WITH D169HE365-16)
G-J
1
35
NAS1149C0432R
. WASHER
(OPT AN960C416L)
(REPLACED BY NAS1149C0332R)
A-B
2
35
NAS1149C0332R
. WASHER
(OPT AN960C10L)
(USED WITH NAS623-3-3)
(USED WITH NAS623-3-4)
C-J
2
35C
NAS1149C0463R
. WASHER
(OPT AN960C416)
C-J
2
36
NAS463TC416
. SPACER
A-B
2
37
4958704-1
. RETAINER
37A
5930640-227
. BLOCK
–37B
D169HE365-16
. INSERT
(V29372)
38
MS21043L5
. NUT
A-B
1
38
MS21043L5
. NUT
(REPLACED BY MS21043-5)
C-H
1
38
MS21043-5
. NUT
C-H
1
38
MS21042L5
. NUT
E-J
1
39
NAS1149C0532R
. WASHER
(OPT AN960C516L)
40
NAS6405U32
. BOLT-(T)
A-B
1
40
NAS6405U32
. BOLT
(REPLACED BY NAS6205-32)
C-H
1
40
NAS6205-32
. BOLT
C-J
1
2
G-J
1
2
1
71-10-13
– Item not Illustrated
ILLUSTRATED PARTS LIST
Page 1018
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIG/
ITEM
PART NUMBER
1–
AIRLINE
PART
NUMBER
NOMENCLATURE
USAGE
CODE
1234567
UNITS
PER
ASSY
AFT LOWER COWL DOOR ASSEMBLY
41
703100-2
. SNUBBER ASSY
(V17816)
(SPEC 7958530-511)
1
42
NAS6404U3
. BOLT-(T)
2
43
NAS1149C0432R
. WASHER
(OPT AN960C416L)
2
44
3938112-1
. BRACKET
1
45
S2431221-4C8F
. SHIM-LAMINATED
AR
–45A
D169HE465-16
. INSERT
(V29372)
2
46
5930640-23
. ROLLPIN
(PRE SB MD80-71-025)
A-B
3
46
5930640-135
. ROLLPIN
(REPLACED BY AND NOT INTCHG/W
5930640-161)
(PRE SB MD80-71-025)
C-D
3
46
5930640-161
. ROLLPIN
(REPLACES 5930640-135)
(REPLACED BY AND INTCHG/W
5930640-165)
(POST SB MD80-71-025)
C-D
3
46
5930640-165
. ROLLPIN
(REPLACES 5930640-161)
(REPLACED BY 5930640-215)
E-H
3
46
5930640-215
. ROLLPIN
(SPARES ONLY)
C-F
3
46E
MS24665-195
. PIN-COTTER
(REPLACED BY MS24665-304)
(REPLACED BY MS24665-306)
E-H
6
46E
MS24665-304
. PIN-COTTER
E-J
3
46G
MS24665-306
. PIN-COTTER
E-J
3
47
RA22045
. BOLT ASSY
(V17446)
(POST SB MD80-71-025)
3
48
RA22045-7
. . WASHER
(V32134)
1
49
RA22045-5
. . BOLT
(V17446)
1
50
MS21043L4
. NUT
A-B
6
50
MS21043L4
. NUT
(REPLACED BY MS21043-4)
C-F
6
50
MS21043-4
. NUT
C-J
6
71-10-13
– Item not Illustrated
ILLUSTRATED PARTS LIST
Page 1019
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIG/
ITEM
PART NUMBER
1–
AIRLINE
PART
NUMBER
NOMENCLATURE
USAGE
CODE
1234567
UNITS
PER
ASSY
AFT LOWER COWL DOOR ASSEMBLY
51
NAS1149C0432R
. WASHER
(OPT AN960C416L)
12
51A
MS25083-2CC6
. JUMPER
52
NAS4904U3
. BOLT-(T)
6
53
NAS6404U3
. BOLT-(T)
6
54
5938084-1
. LATCH FITTING
(REPLACED BY AND NOT INTCHG/W
5938084-501)
A-D
3
54
5938084-501
. LATCH FITTING
(REPLACES 5938084-1)
E-J
3
55
S2431221-4C8F
. SHIM-LAMINATED
AR
–55A
D169HE465-16
. INSERT
(V29372)
6
56
MS21043L4
. NUT
A-B
2
56
MS21043L4
. NUT
(REPLACED BY MS21043-4)
C-J
10
56
MS21043-4
. NUT
C-J
10
57
NAS1149C0432R
. WASHER
(OPT AN960C416L)
A-B
11
57
NAS1149C0432R
. WASHER
(OPT AN960C416L)
C-J
15
57B
NAS1149C0432R
. WASHER
(OPT AN960C416L)
G, J
2
58
NAS4904U3
. BOLT-(T)
A-B
2
58
NAS4904U3
. BOLT-(T)
C-J
6
58B
NAS679A4W
. NUT
A-B
4
58C
S124682-4R10-3
. WASHER
A-B
4
58D
HL10V8-5
. BOLT
(V73197)
A-B
4
59
NAS6404U3
. BOLT-(T)
60
5938085-1
. HINGE ASSY
A, C, E, G,
I
1
–61
5938085-2
. HINGE ASSY
B, D, F, H, J
1
62
03-505-06E015
. . BEARING
(V09455)
63
5938085-5
. . HINGE
A, C, E, G,
I
1
–64
5938085-6
. . HINGE
B, D, F, H, J
1
65
5938086-1
. HINGE
A-B
1
9
1
1
71-10-13
– Item not Illustrated
ILLUSTRATED PARTS LIST
Page 1020
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIG/
ITEM
PART NUMBER
1–
AIRLINE
PART
NUMBER
NOMENCLATURE
USAGE
CODE
1234567
UNITS
PER
ASSY
AFT LOWER COWL DOOR ASSEMBLY
66
5938087-1
. HINGE ASSY
A, C, E, G,
I
1
–67
5938087-2
. HINGE ASSY
B, D, F, H, J
1
68
03-505-06E015
. . BEARING
(V09455)
69
5938087-5
. . HINGE
A, C, E, G,
I
1
–70
5938087-6
. . HINGE
B, D, F, H, J
1
71
S2431221-4C8F
. SHIM-LAMINATED
AR
–71B
D169HE465-16
. INSERT
(V29372)
9
72
MS21042L3
. NUT
2
73
1
. DELETED
73A
NAS1149FN316P
. WASHER
(OPT AN960-3L)
2
74
NAS623-3-23
. SCREW
2
75
NAS43HT3-80
. SPACER
2
76
4938093-1
. SPACER
2
77
4938067-1
. SPRING
1
78
5930639-3
. LATCH ASSY
A-B
1
78
5930639-141
. LATCH ASSY
C-J
1
78B
MS206153M
. . RIVET
78C
5930639-59
. . CAP
A-B
1
78C
5930639-145
. . CAP
C-J
1
78E
5930639-11
. . LATCH-SAFETY
A-B
1
78E
5930639-143
. . LATCH-SAFETY
C-J
1
79
NAS6404U3
. BOLT-(T)
2
80
NAS1149C0432R
. WASHER
(OPT AN960C416L)
2
81
5930639-9
. BRACKET
A-B
1
81
5930639-9
. BRACKET
(REPLACED BY 5930639-147)
C-F
1
81
5930639-147
. BRACKET
C-J
1
82
S2431221-4C8F
. SHIM-LAMINATED
AR
–82B
D169HE465-16
. INSERT
(V29372)
2
83
5930640-5
. SEAL
AR
A-B
1
71-10-13
– Item not Illustrated
ILLUSTRATED PARTS LIST
Page 1021
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIG/
ITEM
PART NUMBER
1–
AIRLINE
PART
NUMBER
NOMENCLATURE
1234567
USAGE
CODE
UNITS
PER
ASSY
AFT LOWER COWL DOOR ASSEMBLY
83
5930640-119
. SEAL
C-J
1
84
5930640-69
. SEAL
A-B
1
84
5930640-117
. SEAL
C-J
1
85
5930640-71
. SEAL
A-B
1
85
5930640-115
. SEAL
C-J
1
86
5930640-9
. SEAL
A-B
1
86
5930640-113
. SEAL
C-J
1
87
5930640-73
. SEAL
A-B
1
87
5930640-111
. SEAL
C-J
1
88
5930640-75
. SEAL
A-B
1
88
5930640-109
. SEAL
C-J
1
89
5930640-25
. SEAL
A-B
1
89
5930640-107
. SEAL
C-J
1
90
. DELETED
91
5930640-57
. SEAL
A-B
1
91
5930640-133
. SEAL
C-J
1
92
MS20426AD4
. RIVET
93
5930640-13
. RETAINER
A-B
1
93
5930640-97
. RETAINER
C-J
1
94
5930640-77
. RETAINER
A-B
1
95
5930640-79
. RETAINER
A-B
1
95A
5930640-99
. RETAINER
C, E, G, I
1
95A
5930640-100
. RETAINER
D, F, H, J
1
96
5930640-17
. RETAINER
A-B
1
96
5930640-101
. RETAINER
C-J
1
97
5930640-81
. RETAINER
A-B
1
98
5930640-83
. RETAINER
A-B
1
98A
5930640-103
. RETAINER
C, E, G, I
1
98A
5930640-104
. RETAINER
D, F, H, J
1
99
5930640-27
. RETAINER
A-B
1
99
5930640-105
. RETAINER
C-J
1
100
NAS1739M5
. RIVET
C-J
8
101
MS20615M3
. RIVET
AR
2
71-10-13
– Item not Illustrated
ILLUSTRATED PARTS LIST
Page 1022
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIG/
ITEM
PART NUMBER
1–
AIRLINE
PART
NUMBER
NOMENCLATURE
USAGE
CODE
1234567
UNITS
PER
ASSY
AFT LOWER COWL DOOR ASSEMBLY
102
5930640-53
. RETAINER
1
103
MS20426AD5
. RIVET
(REPLACED BY MS20426AD4)
A-F
AR
103A
MS20426AD4
. RIVET
E-J
AR
103B
NAS1149DN432H
. WASHER
(OPT AN960D4)
E-J
2
104
5930640-41
. RETAINER
A-B
1
104
5930640-85
. RETAINER
(REPLACED BY 5930640-179)
(PRE SB MD80-71-029)
C-F
1
104B
5930640-179
. RETAINER ASSY
(POST SB MD80-71-029)
E-J
1
104C
5930639-201
. PLATE
E-J
1
105
5930640-43
. RETAINER
A-B
1
105
5930640-87
. RETAINER
(REPLACED BY 5930640-181)
(PRE SB MD80-71-029)
C-F
1
105B
5930640-181
. RETAINER ASSY
(POST SB MD80-71-029)
E-J
1
106
5930640-59
. RETAINER
A-B
1
106
5930640-89
. RETAINER
(REPLACED BY 5930640-183)
(PRE SB MD80-71-029)
C-F
1
106B
5930640-183
. RETAINER ASSY
(POST SB MD80-71-029)
E-J
1
107
5930640-63
. RETAINER
A-B
1
107
5930640-91
. RETAINER
(REPLACED BY 5930640-185)
(PRE SB MD80-71-029)
C-F
1
107B
5930640-185
. RETAINER ASSY
(POST SB MD80-71-029)
E-J
1
108
5930640-49
. RETAINER
A-B
1
108
5930640-93
. RETAINER
(REPLACED BY 5930640-187)
(PRE SB MD80-71-029)
C-F
1
108B
5930640-187
. RETAINER ASSY
(POST SB MD80-71-029)
E-J
1
109
5930640-51
. RETAINER
A-B
1
109
5930640-95
. RETAINER
(REPLACED BY 5930640-189)
(PRE SB MD80-71-029)
C-F
1
71-10-13
– Item not Illustrated
ILLUSTRATED PARTS LIST
Page 1023
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIG/
ITEM
PART NUMBER
1–
AIRLINE
PART
NUMBER
NOMENCLATURE
1234567
USAGE
CODE
UNITS
PER
ASSY
AFT LOWER COWL DOOR ASSEMBLY
109B
5930640-189
. RETAINER ASSY
(POST SB MD80-71-029)
E-J
1
110
5930640-137
. SEAL
(REPLACED BY 5930640-149)
(PRE SB MD80-71-029)
A-D
1
110
5930640-149
. SEAL
(REPLACED BY 5930640-167)
(POST SB MD80-71-026)
(PRE SB MD80-71-029)
C-F
1
110B
5930640-167
. SEAL
(POST SB MD80-71-029)
E-J
1
111
5930640-139
. SEAL
(REPLACED BY 5930640-151)
(PRE SB MD80-71-029)
A-D
1
111
5930640-151
. SEAL
(REPLACED BY 5930640-169)
(POST SB MD80-71-026)
(PRE SB MD80-71-029)
C-F
1
111B
5930640-169
. SEAL
(POST SB MD80-71-029)
E-J
1
112
5930640-141
. SEAL
(REPLACED BY 5930640-153)
(PRE SB MD80-71-029)
A-D
1
112
5930640-153
. SEAL
(REPLACED BY 5930640-171)
(POST SB MD80-71-026)
(PRE SB MD80-71-029)
C-F
1
112B
5930640-171
. SEAL
(POST SB MD80-71-029)
E-J
1
113
5930640-143
. SEAL
(REPLACED BY 5930640-155)
(PRE SB MD80-71-029)
A-D
1
113
5930640-155
. SEAL
(REPLACED BY 5930640-173)
(POST SB MD80-71-026)
(PRE SB MD80-71-029)
C-F
1
113B
5930640-173
. SEAL
(POST SB MD80-71-029)
E-J
1
114
5930640-145
. SEAL
(REPLACED BY 5930640-157)
(PRE SB MD80-71-029)
A-D
1
114
5930640-157
. SEAL
(REPLACED BY 5930640-175)
(POST SB MD80-71-026)
(PRE SB MD80-71-029)
C-F
1
114B
5930640-175
. SEAL
(POST SB MD80-71-029)
E-J
1
71-10-13
– Item not Illustrated
ILLUSTRATED PARTS LIST
Page 1024
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIG/
ITEM
PART NUMBER
1–
AIRLINE
PART
NUMBER
NOMENCLATURE
1234567
USAGE
CODE
UNITS
PER
ASSY
AFT LOWER COWL DOOR ASSEMBLY
115
5930640-147
. SEAL
(REPLACED BY 5930640-159)
(PRE SB MD80-71-029)
A-D
1
115
5930640-159
. SEAL
(REPLACED BY 5930640-177)
(POST SB MD80-71-026)
(PRE SB MD80-71-029)
C-F
1
115B
5930640-177
. SEAL
(POST SB MD80-71-029)
E-J
1
115C
5930640-221
. STRAP
(REPLACED BY 5930640-223)
G-H
2
115C
5930640-223
. STRAP
G-J
2
115E
5930640-219
. STRAP
G-J
1
115F
5930640-219
. STRAP
(REPLACED BY 5930640-225)
G-H
2
115F
5930640-225
. STRAP
G-J
2
115H
5930640-217
. STRAP
G-J
4
116
5930640-3
. RUBSTRIP
A-D
1
116
5930640-163
. RUBSTRIP
E-J
1
116B
CSR904B5
. RIVET
(REPLACED BY NAS1097AD5)
E-F
AR
116B
NAS1097AD5
. RIVET
(REPLACED BY MS20470B4)
E-F
AR
116B
MS20470B4
. RIVET
E-J
AR
117
5938118-503
. EXTENSION ASSY
A
1
117
5938118-509
. EXTENSION ASSY
C, E, G, I
1
–118
5938118-504
. EXTENSION ASSY
B
1
–118
5938118-510
. EXTENSION ASSY
D, F, H, J
1
119
5938118-505
. EXTENSION ASSY
A
1
119
5938118-511
. EXTENSION ASSY
(REPLACED BY AND NOT INTCHG/W
5938118-513)
C, E, I,
1
119
5938118-513
. EXTENSION ASSY
(REPLACES 5938118-511)
G-J
1
–120
5938118-506
. EXTENSION ASSY
B
1
–120
5938118-512
. EXTENSION ASSY
(REPLACED BY AND NOT INTCHG/W
5938118-513)
D, F, H, J
1
–120
5938118-513
. EXTENSION ASSY
(REPLACES 5938118-512)
G-J
1
71-10-13
– Item not Illustrated
ILLUSTRATED PARTS LIST
Page 1025
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
5930640
COMPONENT MAINTENANCE MANUAL
FIG/
ITEM
PART NUMBER
1–
AIRLINE
PART
NUMBER
NOMENCLATURE
1234567
USAGE
CODE
UNITS
PER
ASSY
AFT LOWER COWL DOOR ASSEMBLY
121
5938073-1
. DOOR ASSY-COMPOSITE
A-B
1
121
5938136-1
. DOOR ASSY-COMPOSITE
C-F
1
121
5938219-1
. DOOR ASSY-COMPOSITE
G, I
1
121
5938219-2
. DOOR ASSY-COMPOSITE
H, J
1
71-10-13
– Item not Illustrated
ILLUSTRATED PARTS LIST
Page 1026
Sep 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details