Commercial 

Airplanes 737

Service Bulletin

ALERT

Number: 737-57A1218

Original Issue: July 22, 1993

Revision 6: June 09, 2011

ATA System: 5752

SUBJECT: WINGS - Trailing Edge Flaps - Outboard Flap Carriage Spindle Repair and Life Limiting

Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15

CFR 730-774). An export license may be required before it is used for development, production or use by foreign

persons from specific countries. The controller of this data has the individual responsibility to abide by all export

laws.

ECCN: 9E991

BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET

Copyright © 1993 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Unpublished Work - All Rights Reserved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 livery are all trademarks owned by The Boeing Company; and no trademark license is granted in

connection with this document unless provided in writing by Boeing.

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4.0
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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT

BLANK PAGE
Table of Contents

Revision Transmittal Sheet ............................................ 5

Summary ...................................................... 7

1. PLANNING INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

A. Effectivity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

1. Airplanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

2. Spares Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22

B. Concurrent Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

C. Reason . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

D. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24

E. Compliance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26

F. Approval . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27

G. Manpower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 28

H. Weight and Balance Changes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 28

I. Electrical Load Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 28

J. References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29

1. Existing Data: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29

2. Data supplied with this Service Bulletin: . . . . . . . . . . . . . . . . . . . . . . . . . . . 29

3. Installation Drawings Used in the Preparation of this Service Bulletin: . . . . . . . . . . . 29

K. Publications Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30

L. Interchangeability and Intermixability of Parts . . . . . . . . . . . . . . . . . . . . . . . . . . . 30

2. MATERIAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

A. Material - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

B. Industry Support Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

C. Parts Necessary For Each Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

1. Kits/Parts: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

2. Parts and Materials Supplied by the Operator: . . . . . . . . . . . . . . . . . . . . . . . . 31

3. Parts Modified and Reidentified: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

4. Parts Removed and Not Replaced: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

D. Parts Necessary to Change Spares . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

E. Special Tooling - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

F. Special Tooling Necessary to do this Service Bulletin . . . . . . . . . . . . . . . . . . . . . . . 31

3. ACCOMPLISHMENT INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33

A. GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33

B. WORK INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 34

FIGURE 1: CARRIAGE SPINDLE INSPECTION AND REPAIR . . . . . . . . . . . . . . . . . . . . . 38

FIGURE 2: MINIMUM ALLOWABLE SPINDLE DIAMETER . . . . . . . . . . . . . . . . . . . . . . . 41

FIGURE 3: APPLICATION OF CARRIAGE TEMPORARY SERIAL NUMBERS . . . . . . . . . . . . . 43

FIGURE 4: APPLICATION OF CARRIAGE PERMANENT SERIAL NUMBERS . . . . . . . . . . . . . 45

Appendix A: EXISTING PARTS ACCOUNTABILITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47

Appendix B: CARRIAGE MANUFACTURED DATES . . . . . . . . . . . . . . . . . . . . . . . . . . . . 48

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BOEING SERVICE BULLETIN 737-57A1218

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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT

BLANK PAGE
Commercial 

Airplanes 737

Service Bulletin

ALERT

Revision Transmittal Sheet Number: 737-57A1218

Original Issue: July 22, 1993

Revision 6: June 09, 2011

ATA System: 5752

SUBJECT: WINGS - Trailing Edge Flaps - Outboard Flap Carriage Spindle Repair and Life Limiting

This revision includes all pages of the service bulletin.

COMPLIANCE INFORMATION RELATED TO THIS REVISION

Federal Aviation Administration (FAA) Airworthiness Directive AD 2010-15-08 is related to this service bulletin.

No more work is necessary on the airplane(s) changed in accordance with the Revision 5 of this service bulletin.

REASON FOR REVISION

This revision is sent to change the compliance time from 48,000 flight cycles to 40,000 flight cycles in both Group

1 and Group 2 tables, and to correct the typo in the Figure 2 graphic.

These sections were changed:

1. In Section 1.E. Compliance, the compliance time was reduced from 48,000 flight cycles to 40,000 flight

cycles in both Group 1 and Group 2 tables, added reference to AD 2010-15-08

2. In Section 1.F. Approval, added the alternative method of compliance paragraph for AD 2010-15-08.

3. In Section 1.K. Publication Affected , added the Damage tolerance statement.

4. In Section 3.A. General Information, updated the general notes.

5. In Section 3.B. Work Instruction, updated the instructions to use the current refer to & in accordance with

terminology.

6. In Figure 2, the -27 was moved from the Outboard spindle view to the Inboard spindle view to agree with

the tables in Figure 2 and the Description Section.

Vertical lines are put on the left edge of each page, except in Paragraph 1.A., Effectivity, to show the location

of important changes.

Pages with no vertical lines have no important changes.

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REVISION HISTORY

Original Issue: July 22, 1993

Revision 1: August 15, 1996

Revision 2: September 30, 1999

Revision 3: July 25, 2002

Revision 4: June 19, 2007

Revision 5: February 09, 2009

Revision 6:

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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT
Commercial 

Airplanes 737

Service Bulletin

ALERT

Summary Number: 737-57A1218

Original Issue: July 22, 1993

Revision 6: June 09, 2011

ATA System: 5752

SUBJECT: WINGS - Trailing Edge Flaps - Outboard Flap Carriage Spindle Repair and Life Limiting

THIS BULLETIN IS SENT TO THE OPERATORS OF RECORD OF THE AIRPLANES SHOWN IN PARAGRAPH

1.A., EFFECTIVITY. IF AN AIRPLANE HAS BEEN LEASED OR SOLD, SEND THIS SERVICE BULLETIN TO

THE NEW OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS SERVICE BULLETIN TO

THE NEW OWNER.

CONCURRENT REQUIREMENTS

None

BACKGROUND

This service bulletin provides instructions for removal, inspection and overhaul/rework of the outboard midflap

carriage spindle. This is to make sure that any corrosion is found and repaired before fractures occur. This

service bulletin also provides instructions to add a serial number to the carriage for tracking purposes. Outboard

midflap carriages are made life limited and must be tracked.

Fractures that resulted from stress corrosion and pitting have been reported along the length of the spindle and

spindle diameter. Several operators have reported thirty five outboard carriage spindle fractures that resulted

from corrosion since 1969. The most critical fractures occur at the forward end of the spindle through the large

diameter. Of the thirty five reported fractures due to corrosion, three have occurred at this critical location. These

fractures occurred on 737 -100 through -500 airplanes.

Several operators have also reported seven carriage spindle fractures that resulted from fatigue, eight of which

occurred at the critical location. These fractures occurred on 737-200 and -300 airplanes.

There also have been many additional reports of corrosion on the outboard flap carriage spindles. One fractured

carriage spindle can be compensated for by the pilot with inputs to the aileron and/or rudder. However fractures

of both the inboard and outboard spindles (at the critical location) on a given outboard flap may preclude continued

safe flight and landing of the airplane.

Boeing Service Related Problem (SRP) 737-57-0147 is related to this service bulletin.

ACTION (PRR 35005-260RS)

Remove the outboard flaps, and disassemble the outboard flap carriages. Look for corrosion, pitting and/or

cracks. Refer to the 737-100/-200/-200C Overhaul Manual (OHM) 57-53-35 or the 737-300/-400/-500 Component

Maintenance Manual (CMM) 57-53-36 for repair, overhaul and assembly instructions. If the damage is beyond

the repair limits for diameters shown in this service bulletin, then the carriage must be discarded.

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If a carriage with a documented history has exceeded its life limitations detailed in this service bulletin, or if the

carriage history cannot be documented, discard and replace the carriage with a life limited, serialized part within

the time shown in Paragraph 1.E., Compliance. If a carriage is within the limits of its documented life, serialize

it or use the existing serial number and begin tracking the carriage within the time shown in Paragraph 1.E.,

Compliance.

EFFECTIVITY

737-100/ -200/ -200C/ -300/ -400/ and -500 Airplanes line numbers 1 through 3132.

COMPLIANCE

Federal Aviation Administration (FAA) Airworthiness Directive AD 2010-15-08 is related to this service bulletin.

Refer to Paragraph 1.E., Compliance.

INDUSTRY SUPPORT INFORMATION

Boeing warranty remedies are not available for the inspection and repair procedures given in this service bulletin.

MANPOWER

Refer to Paragraph 1.G., Manpower.

MATERIAL INFORMATION

Operator Supplied Parts/Materials.

Refer to Paragraph 2.A., Material - Price and Availability.

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BOEING SERVICE BULLETIN 737-57A1218

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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT

BLANK PAGE
Commercial 

Airplanes 737

Service Bulletin

ALERT

Number: 737-57A1218

Original Issue: July 22, 1993

Revision 6: June 09, 2011

ATA System: 5752

SUBJECT: WINGS - Trailing Edge Flaps - Outboard Flap Carriage Spindle Repair and Life Limiting

THIS BULLETIN IS SENT TO THE OPERATORS OF RECORD OF THE AIRPLANES SHOWN IN PARAGRAPH

1.A., EFFECTIVITY. IF AN AIRPLANE HAS BEEN LEASED OR SOLD, SEND THIS SERVICE BULLETIN TO

THE NEW OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS SERVICE BULLETIN TO

THE NEW OWNER.

1. PLANNING INFORMATION

A. Effectivity

1. Airplanes

Refer to Service Bulletin Index Document D6-19567, Part 3 for Airplane Variable Number, Line

Number, and Serial Number data.

This service bulletin is for the airplanes shown below.

GROUP CONFIGURATION DESCRIPTION

1 - 737-100, -200 and -200C airplanes, line numbers 1 through 1585.

2 - 737-300, -400 and -500 airplanes, line numbers 1001 through 3132.

Airplane Models:

737-100, 737-200, 737-200C, 737-300, 737-400, 737-500

Variable Number Group

PA001 - PA022 1

PA099 1

PA231 - PA232 1

PC001 - PC005 1

PG001 - PG075 1

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Variable Number Group

PG199 1

PG201 - PG230 1

PG251 - PG255 1

PG271 - PG279 1

PG301 - PG314 1

PG331 - PG332 1

PG351 - PG356 1

PG375 1

PG401 - PG403 1

PG431 - PG442 1

PG471 - PG475 1

PG501 - PG505 1

PG571 - PG586 1

PG621 - PG630 1

PG651 - PG652 1

PG701 - PG705 1

PH001 1

PH011 - PH013 1

PH021 - PH024 1

PH701 - PH715 1

PH731 - PH732 1

PH741 - PH743 1

PJ001 - PJ009 1

PJ031 - PJ032 1

PJ071 - PJ072 1

PJ101 - PJ119 1

PJ201 - PJ219 1

PJ301 - PJ302 2

PJ551 - PJ561 2

PJ601 - PJ615 2

PJ811 2

PJ816 - PJ817 2

PK026 - PK029 1

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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT
Variable Number Group

PK041 - PK053 1

PK061 - PK070 1

PK081 - PK082 1

PK091 - PK099 1

PK101 - PK103 1

PK111 - PK120 1

PK141 - PK146 1

PK201 - PK204 1

PK211 - PK223 1

PK231 - PK241 1

PK251 - PK258 1

PK271 - PK274 1

PK281 - PK289 1

PK291 1

PK301 - PK318 1

PK341 1

PK351 - PK361 1

PK391 1

PK431 - PK433 1

PK451 - PK452 1

PK461 - PK469 1

PK495 1

PK501 - PK504 1

PK511 - PK515 1

PK519 1

PK521 - PK528 1

PK541 - PK565 1

PK581 1

PK591 - PK599 1

PK601 - PK617 1

PK621 - PK637 1

PK641 - PK642 1

PK661 - PK666 1

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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT
Variable Number Group

PK671 - PK681 1

PK691 - PK697 1

PK711 - PK716 1

PK731 - PK765 1

PK771 - PK779 1

PK801 - PK804 1

PK819 - PK827 1

PK830 1

PK861 - PK863 1

PK871 - PK874 1

PK881 - PK884 1

PK901 - PK938 1

PK971 - PK974 1

PL001 - PL028 1

PL061 1

PL081 1

PL101 - PL113 1

PL151 1

PL171 - PL172 1

PL201 - PL203 1

PL221 1

PL401 - PL417 1

PL421 1

PL441 1

PL451 - PL456 1

PL471 1

PL491 1

PL501 - PL506 1

PL551 - PL562 1

PL581 1

PL601 - PL603 1

PL611 1

PL621 - PL626 1

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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT
Variable Number Group

PL631 - PL632 1

PL711 - PL712 1

PL716 - PL747 1

PL756 1

PL758 1

PL761 - PL770 1

PL781 - PL788 1

PL793 1

PL801 - PL803 1

PM001 - PM006 1

PM016 - PM017 1

PM021 - PM023 1

PM051 - PM066 1

PM101 - PM119 1

PM141 - PM142 1

PM171 1

PM181 1

PM251 - PM255 1

PM281 - PM283 1

PM381 - PM399 2

PM401 - PM417 2

PM541 - PM564 2

PN001 - PN002 1

PN021 - PN043 1

PN081 - PN086 1

PN101 - PN117 1

PN131 - PN163 1

PN401 - PN420 1

PN431 - PN433 1

PN451 - PN456 1

PN471 - PN474 1

PN481 1

PN491 - PN493 1

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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT
Variable Number Group

PN501 - PN502 1

PN511 - PN512 1

PN521 1

PP001 - PP054 2

PP101 - PP169 2

PP181 - PP199 2

PP201 - PP205 2

PP221 2

PP231 - PP243 2

PP281 - PP286 2

PP301 - PP305 2

PP351 - PP353 2

PP376 - PP384 2

PP391 - PP393 2

PP401 - PP440 2

PP471 - PP475 2

PP501 - PP522 2

PP631 - PP634 2

PP651 - PP652 2

PP671 - PP699 2

PP701 - PP733 2

PP771 - PP779 2

PP801 - PP808 2

PP821 - PP827 2

PP831 - PP848 2

PP851 - PP852 2

PP861 - PP877 2

PP891 - PP899 2

PP901 - PP936 2

PP946 - PP948 2

PP951 - PP952 2

PP961 - PP967 2

PP981 - PP991 2

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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT
Variable Number Group

PP993 2

PQ001 - PQ016 2

PQ026 - PQ041 2

PQ051 - PQ092 2

PQ101 - PQ199 2

PQ201 - PQ202 2

PQ221 - PQ237 2

PQ241 - PQ243 2

PQ251 - PQ267 2

PQ281 - PQ299 2

PQ301 - PQ307 2

PQ331 - PQ332 2

PQ341 - PQ348 2

PQ361 - PQ373 2

PQ391 - PQ395 2

PQ401 - PQ418 2

PQ421 2

PQ431 - PQ438 2

PQ447 - PQ448 2

PQ451 2

PQ454 2

PQ471 - PQ475 2

PQ479 - PQ481 2

PQ486 - PQ487 2

PQ491 - PQ493 2

PQ771 - PQ772 2

PQ791 - PQ793 2

PQ801 - PQ805 2

PQ931 - PQ935 2

PQ951 2

PQ971 - PQ997 2

PR001 - PR017 2

PR021 - PR034 2

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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT
Variable Number Group

PR041 - PR045 2

PR061 - PR072 2

PR077 - PR082 2

PR091 - PR092 2

PR096 2

PR101 2

PR121 - PR122 2

PR131 - PR132 2

PR141 - PR143 2

PR161 - PR172 2

PR181 2

PS601 - PS631 2

PS636 - PS638 2

PS641 - PS644 2

PS651 - PS657 2

PS666 - PS669 2

PS691 - PS692 2

PS701 - PS706 2

PS751 - PS799 2

PS811 2

PS836 - PS837 2

PS841 - PS846 2

PS851 - PS852 2

PS856 2

PS861 - PS863 2

PS866 - PS868 2

PS871 - PS874 2

PS896 - PS897 2

PS901 - PS941 2

PS956 - PS957 2

PS961 - PS963 2

PS971 - PS978 2

PT001 - PT015 2

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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT
Variable Number Group

PT021 - PT031 2

PT041 - PT064 2

PT101 - PT105 2

PT121 - PT138 2

PT146 - PT148 2

PT161 - PT170 2

PT181 - PT188 2

PT211 - PT220 2

PT295 2

PT301 - PT309 2

PT331 - PT360 2

PT381 - PT399 2

PT401 - PT438 2

PT501 - PT517 2

PT561 - PT565 2

PT581 - PT586 2

PT611 - PT621 2

PT641 - PT644 2

PT651 - PT656 2

PT671 - PT672 2

PT681 - PT685 2

PT701 - PT703 2

PT716 - PT717 2

PT721 - PT725 2

PT801 - PT834 2

PT851 - PT854 2

PT871 - PT886 2

PT901 - PT930 2

PT971 - PT973 2

PT981 - PT985 2

PT996 2

PU001 - PU025 2

PU301 2

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BOEING SERVICE BULLETIN 737-57A1218

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Variable Number Group

PU311 - PU313 2

PV001 - PV055 2

PV201 - PV209 2

PV226 - PV229 2

PV231 - PV237 2

PV271 - PV272 2

PV281 - PV287 2

PV296 2

PV301 - PV302 2

PV351 2

PV356 - PV357 2

PW001 - PW054 2

PW061 - PW068 2

PW072 2

PW086 - PW088 2

PW091 - PW094 2

PW101 - PW102 2

PW106 2

PW111 - PW120 2

PW156 - PW157 2

PW161 - PW171 2

PW201 - PW252 2

PW261 - PW268 2

PW271 - PW276 2

PW278 2

PW281 - PW293 2

PW296 2

PW301 - PW327 2

PW401 - PW408 2

PW411 - PW418 2

PW421 - PW424 2

PW431 - PW435 2

PW441 - PW450 2

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BOEING SERVICE BULLETIN 737-57A1218

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Variable Number Group

PW461 - PW467 2

PW501 - PW504 2

PW511 - PW522 2

PW524 - PW550 2

PW556 - PW557 2

PW561 - PW564 2

PW571 - PW576 2

PW591 - PW596 2

PW611 - PW622 2

PW631 - PW637 2

PW661 - PW662 2

PW681 - PW683 2

PW701 - PW702 2

PW711 - PW717 2

PW741 - PW742 2

PW761 2

PW771 2

PW831 2

PW851 - PW856 2

PX071 1

PX701 1

PY001 - PY008 1

PY021 - PY022 1

PY031 1

PY036 - PY037 1

PY046 - PY048 1

PY051 - PY053 1

PY056 - PY057 1

PY101 - PY103 1

PY111 - PY113 1

PY131 - PY135 1

PY141 - PY143 1

PY151 - PY154 1

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ALERT ALERT
Variable Number Group

PY156 - PY157 1

PY161 - PY162 1

PY166 1

PY191 1

PY201 1

PY221 - PY222 1

PY231 1

PY241 - PY244 1

PY270 - PY275 1

PY281 1

PY286 1

PY301 - PY304 1

PY321 - PY323 1

PY341 - PY346 1

PY361 - PY362 1

PY381 1

PY401 1

PY409 - PY411 1

PY421 - PY422 1

PY441 1

PY451 1

PY461 - PY463 1

PY591 - PY595 1

PY611 - PY612 1

PY621 1

PY631 1

PY651 1

PY671 - PY672 1

PY721 1

PY741 1

2. Spares Affected

None. However, spare carriages are subject to the requirements of paragraph 1.E., Compliance.

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ALERT ALERT
B. Concurrent Requirements

None.

C. Reason

This service bulletin provides instructions for removal, inspection and overhaul/rework of the outboard

midflap carriage spindle. This is to make sure that any corrosion is found and repaired before fractures

occur. This service bulletin also provides instructions to add a serial number to the carriage for tracking

purposes. Outboard midflap carriages are made life limited and must be tracked.

Fractures that resulted from stress corrosion and pitting have been reported along the length of the

spindle and spindle diameter. Several operators have reported thirty five outboard carriage spindle

fractures that resulted from corrosion since 1969. The most critical fractures occur at the forward end

of the spindle through the large diameter. Of the thirty five reported fractures due to corrosion, three

have occurred at this critical location. These fractures occurred on 737 -100 through -500 airplanes.

Several operators have also reported seven carriage spindle fractures that resulted from fatigue, five

of which occurred at the critical location. These fractures occurred on 737-200 and -300 airplanes.

There also have been many additional reports of corrosion on the outboard flap carriage spindles. One

fractured carriage spindle can be compensated for by the pilot with inputs to the aileron and/or rudder.

However fractures of both the inboard and outboard spindles (at the critical location) on a given outboard

flap may preclude continued safe flight and landing of the airplane.

Boeing Service Related Problem (SRP) 737-57-0147 is related to this service bulletin.

Revision 1 was sent to reference the overhaul manual and component maintenance manual for repair

instruction in paragraph 3., Accomplishment Instruction.

Revision 2 was sent to:

— Add compliance information to Paragraph 1. E., Compliance and Summary page 1.

— Add Maintenance Manual Subjects for 737-300/-400/-500 in steps A and B in paragraph 3. E.,

Accomplishment Instructions.

— Remove sulfamate-nickel plating in paragraph 3. E., Accomplishment Instructions. This will give

more selections in the referenced overhaul manual and component maintenance manual.

Revision 3 was sent to:

— Upgrade the Service Bulletin to Alert status.

— Update the compliance information, by reducing the interval to 12,000 cycles or 8 years of service,

which ever comes first, in Paragraph 1. E., Compliance and Summary page 1.

— Updated inspection requirements to cover the entire spindle for corrosion, pitting and cracks.

— Update the service findings information in the Background Section.

— Added airplane line numbers 2450 - 3132.

Revision 4 is sent to put a life limit on the outboard midflap carriages to prevent fractures of the carriage

spindle. Fractures of both the inboard and outboard spindles (at the critical location) on a given outboard

flap may preclude continued safe flight and landing of the airplane.

This revision also gives instructions on how to serialize the outboard midflap carriages and how to

determine the accumulated flight cycles for undocumented carriages.

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ALERT ALERT
Changes in this revision include:

— Planning Section - New compliance information is added.

— Accomplishment Instructions - New instructions are added (Part 2) to instruct operators how to

apply a serial number to a carriage and how to determine the accumulated flight cycles of an

undocumented carriage.

— Figures - Figure 2 is added to measure the carriage spindle diameter.

— Figures - Figure 3 is added to show how and where to apply a temporary serial number to a

carriage.

— Figures - Figure 4 is added to show how and where to apply a permanent serial number to a

carriage.

— Appendices - Appendix A (Parts Accountability) is deleted. All carriages are subject to the

requirements of paragraph 1.E., Compliance.

— Appendices - Appendix B is added to list some of the applicable carriage serial numbers with their

date of manufacture dating back to 1995. Records of carriages prior to 1995 are no longer available

at Boeing.

The data given in Information Notice 737-57A1218 IN 01 is included in this revision.

Revision 5 is sent to revise the variable/group listing in the Effectivity section for 737-200C to Group 1

airplanes, as stated through out the service bulletin. Two new dash numbers, -29 and -31were added

to Group 2 Outboard and Inboard carriage part numbers in Table 1 of the Description section of this

service bulletin. The minimum allowable diameter "C" was changed to 0.9046 two places for

737-300/400/500 outboard spindles in Figure 2.

Revision 6 is sent to change the compliance time from 48,000 flight cycles to 40,000 flight cycles in

both Group 1 and Group 2 tables, and to correct the typo in the Figure 2 graphic.

D. Description

Remove the outboard flaps, and disassemble the outboard flap carriages. Look for corrosion, pitting

and/or cracks. Refer to the 737-100/-200/-200C Overhaul Manual (OHM) 57-53-35 or the

737-300/-400/-500 Component Maintenance Manual (CMM) 57-53-36 for repair, overhaul and assembly

instructions. If the damage is beyond the repair limits for diameters shown in this service bulletin, the

carriage must be discarded.

If a carriage with a documented history has exceeded its life limitations detailed in this service bulletin,

or if the carriage history cannot be documented, discard and replace the carriage with a life limited,

serialized part within the time shown in Paragraph 1.E., Compliance. If a carriage is within the limits of

its documented life, serialize it or use the existing serial number and begin tracking the carriage within

the time shown in Paragraph 1.E., Compliance.

The airplane effectivity is divided in 2 groups because of differences in carriage configuration. Group

1 airplanes are 737-100, -200 and -200C, Group 2 airplanes are 737-300, -400, and -500. The airplanes

are divided as shown in table 1 below.

Table 1.

Carriage Part NumberGroup Carriage Location Carriage Assembly Part Number

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ALERT ALERT
Table 1.

65-46481-1, -11, -12, -15, -16, -17, -18, 65-47821-6, -8,

-21, -22, -23, -24, -27, -28, -31, -32, -33,

-34, -37, -38, -39, -40, -41, -42, -45, -46,

-49, -50, -51, -52, -53, -54, -55, -56, -57,

-58, -59, -60, -61, -62, -65, -66, -67, -69,

-70, -72, -73, -74, -75, -76, -81, -82, -85,

-86, -95, -96, -137, -138, -139

Inboard (WBL 254) and

Outboard (WBL 355)

Group 1

-10, -12, -16, -20, -

22, -24, -26, -28, -

30

65-79949-1, -2, -3, -4, -5, -6, -7, -8, -9,

-10

65-67159-1, -5, -7,

-9

65-46481-13, -14, -19, -20, -25, -26, -

63, -64, -68, -83, -84, -153, -154

Inboard (WBL 254) and

Outboard (WBL 355)

Group 1

65C27409-5, -9, -

13, -17, -25, -29

65-46481-87, -88, -91, -92, -97, -98, -

101, -102, -111, -112, -115, -116, -121,

-122, -123, -124, -135, -136, -145, -146,

-149, -150

Group 2 Outboard (WBL 355)

65C27409-6, -10, -

18, -21, -23, -27, -

31

65-46481-89, -90, -93, -94, -103, -104,

-105, -106, -107, -108, -109, -110, -113,

-114, -117, -118, -119, -120, -133, -134,

-143, -144, -147, -148

Group 2 Inboard (WBL 254)

Revision 1 - no more work is necessary on airplanes changed as shown in the initial release of this

service bulletin.

Revision 2 - no more work is necessary on airplanes changed as shown in the initial release of this

service bulletin. See section 1. E., Compliance for subsequent overhauls.

Revision 3 - more work is necessary on airplanes inspected as shown in the initial release, Revision

1 or 2 of this service bulletin. See section 1. E., Compliance for subsequent inspection and overhaul

requirements.

Revision 4 - more work is necessary on airplanes changed as shown in the initial release, Revision 1,

Revision 2 or Revision 3 of this service bulletin. Outboard midflap carriages should have serial numbers

applied to them so their accumulated flight cycles can be tracked. Outboard midflap carriages are now

life limited.

Revision 5 - no more work is necessary on airplanes changed as shown in revision 4 of this service

bulletin.

Revision 6 - no more work is necessary on airplanes changed as shown in revision 5 of this service

bulletin.

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ALERT ALERT
NOTE: Due to common access requirements Boeing recommends operators work service

bulletin 737-57A1256 at the same time as this bulletin for 737-100/-200 and -200C

airplanes.

1.

2. Due to common access requirements Boeing recommends operators work service

bulletin 737-57A1277 at the same time as this bulletin.

3. Inspection and maintenance instructions are shown in Section 3.,

ACCOMPLISHMENT INSTRUCTIONS.

4. If the damage is beyond the repair limits shown in Figure 2 of this service bulletin

the carriage must be removed from service, discarded, and replaced with a serialized

carriage.

The work in this service bulletin is done in the maintenance zone(s) given below.

Group 1:

Affected Maintenance Zones

Model Zone

737-100, 737-200, 737-200C 3-7, 4-7

Group 2:

Affected Maintenance Zones

Model Zone

737-300, 737-400, 737-500 307, 407

E. Compliance

Federal Aviation Administration (FAA) Airworthiness Directive AD 2010-15-08 is related to this service

bulletin.

Boeing recommends that the operator do an initial inspection and overhaul at 12,000 flight cycles or 8

years or service, whichever comes first. This is from the most recent carriage overhaul or installation

of a new carriage or airplane delivery.

If the carriage has completed more than 12,000 flight cycles or 8 years of service since an overhaul or

a new carriage was installed, Boeing recommends the following inspection and overhaul times:

— For 737-100/-200 and -200C: Within 1 year of the release date of revision 3 to this service bulletin.

— For 737-300/-400 and -500: Within 2 years of the release date of revision 3 to this service bulletin.

After the initial inspection and overhaul as given in Revision 3 to this service bulletin, continue regular

scheduled inspection and overhauls at 12,000 flight cycles or 8 years of service, whichever comes first.

Boeing recommends that all 737 Classic carriages are replaced as follows:

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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT
Group 1:

737-100/-200 and -200C airplanes. Outboard Flap (Inboard Carriage WBL 254 and Outboard Carriage

WBL 355)

Condition Action Compliance Time

Within 3 years from the release of Revision 4 of this

service bulletin OR within 7,500 flight cycles from the

release of Revision 4 of this service bulletin, whichever

occurs first.

Replace the carriage with

a new or documented

carriage. (a)

Airplanes with an undocumented carriage

or a documented carriage having over

40,000 total flight cycles. (a)

Prior to the carriage accumulating 40,000 flight cycles

OR as defined by one of the compliance criteria from

above, whichever is later. New (zero time) carriages

shall not go over 40,000 flight cycles.

Replace the carriage with

a new or documented

carriage. (a)

Airplanes with a documented carriage having

under 40,000 total flight

cycles. (a)

(a) A documented carriage is a carriage where the service life, in flight cycles, is known. A documented

carriage must have less than 40,000 total flight cycles on it to be considered serviceable. An undocumented

carriage is a carriage where the service life, in flight cycles, is unknown.

Group 2:

737-300/-400 and -500 airplanes. Outboard Flap (Inboard Carriage WBL 254 and Outboard Carriage

WBL 355)

Condition Action Compliance Time

Within 6 years from the release of Revision 4 of this

service bulletin. OR within 15,000 flight cycles from

the release of Revision 4 of this service bulletin,

whichever occurs first.

Replace the carriage with

a new or documented

carriage. (a)

Airplanes with an undocumented carriage

or a documented carriage having over

40,000 total flight cycles. (a)

Prior to the carriage accumulating 40,000 flight cycles

OR as defined by one of the compliance criteria from

above, whichever is later. New (zero time) carriages

shall not go over 40,000 flight cycles.

Replace the carriage with

a new or documented

carriage. (a)

Airplanes with a documented carriage having

under 40,000 total flight

cycles. (a)

(a) A documented carriage is a carriage where the service life, in flight cycles, is known. A documented

carriage must have less than 40,000 total flight cycles on it to be considered serviceable. An undocumented

carriage is a carriage where the service life, in flight cycles, is unknown.

The inspections given in Service Bulletin 737-57A1277 still apply.

F. Approval

This service bulletin was examined by the Federal Aviation Administration (FAA). The changes specified

in this service bulletin comply with the applicable regulations and are FAA approved, as well as European

Aviation Safety Agency (EASA)/Joint Aviation Authorities (JAA) approved for all EASA/JAA approved

airplanes listed in the service bulletin effectivity. This service bulletin and its approval were based on

the airplane in its original Boeing delivery configuration or as modified by other approved Boeing

changes.

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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT
The Manager of the FAA Seattle Aircraft Certification Office (ACO) approves the accomplishment of

the applicable inspections, investigative and corrective actions with the corresponding compliance

times specified in Service Bulletin 737-57A1218 Revision 6 as an AMOC to the accomplishment of the

applicable inspections, investigative and corrective actions with the corresponding compliance times

specified in Service Bulletin 737-57A1218 Revision 5 required by paragraphs (i), (k), (l), (o), (p), (q),

(r), and (s) of AD 2010-15-08 . When this service bulletin specifies contacting Boeing for repair instruction,

the repair instructions must be approved by the FAA in accordance with paragraph (t) of the AD. All

provisions of AD 2010-15-08 that are not specifically referenced in this paragraph remain fully applicable

and must be complied with.

If an airplane has a non-Boeing modification or repair that affects a component or system also affected

by this service bulletin, the operator is responsible for obtaining appropriate regulatory agency approval

before incorporating this service bulletin.

G. Manpower

The data below shows an estimate of the man-hours necessary to do this change for each airplane.

This estimate is for direct labor only, done by an experienced crew. Adjust the estimate with operator

man-hour data if necessary. The estimate does not include lost time. These are some examples of lost

time:

— Time to adjust to the workplace

— Time to schedule the work

— Time to examine the work

— Time to cure the materials

— Time to make the parts

— Time to find the tools.

Elapsed Time

(Hours)

Number of Man-Hours

Persons

Task

Open Access 6 30 5

Examine 2 2 1

Repair 2 32 16

Apply serial number 1 0.25 0.25

Close Access 6 42 7

Test 3 3 1

TOTAL FOR EACH AIRPLANE 109.25 30.25

H. Weight and Balance Changes

None.

I. Electrical Load Data

Not changed.

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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT
J. References

1. Existing Data:

a. Engineering Change Memo PRR 35005-260RS and PRR 35014.

b. Service Related Problem (SRP) 737-57-0147.

c. 737 Maintenance Manual (AMM) Subjects 27-51-34, 27-51-44, 27-51-72 and 27-51-81.

d. Overhaul Manual (OHM) 57-53-35 (737-100/-200/-200C airplanes).

e. Component Maintenance Manual (CMM) 57-53-36 (737-300/-400/-500 airplanes).

f. Boeing Standard Overhaul Practices Manual (SOPM) 20-50-10 and 20-30-02, 20-20-01.

g. Boeing Standard Wiring Practices Manual SWPM 20-10-11, SWPM 20-10-12, SWPM 20-10-19.

h. Boeing Service Bulletin 737-57A1256: WINGS - Trailing Edge Flaps - Outboard Flap Carriage

Spindle Inspection and Repair.

i. Boeing Service Bulletin 737-57A1277: WINGS - Trailing Edge Flaps - Outboard Flap Carriage

Spindle - Inspection for Cracking.

j. Federal Aviation Administration (FAA) Airworthiness Directive AD 2010-15-08.

k. Boeing Service Letter 737-SL-51-042.

2. Data supplied with this Service Bulletin:

None.

3. Installation Drawings Used in the Preparation of this Service Bulletin:

Drawing Number Title

65C16930 Trailing Edge Flap Installation and Rigging Procedures

65C27409 Carriage Sub Assy - Outboard Flap

65C34483 Flap Instl - Outboard, Wing T.E. (top kit)

65C34946 Mid/Aft Flap Assy - Outboard Flap

65-46437 Flap Assembly, Outboard Flap

65-46481 Carriage Assy, Outboard Flap, Wing

65-47821 Carriage Assy - Outboard Flap

65-67159 Carriage Assy - Outboard Flap

65-79949 Carriage Assy Outbd Flap Wing (rework drawing)

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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT
K. Publications Affected

1. Publications:

Publication Chapter-Section

737 Corrosion Prevention Manual 57-00 and 57-50

Component Maintenance Manual 57-53-36

Overhaul Manual 57-53-35

2. Damage Tolerance Based Structural Inspections:

Boeing has evaluated the repairs and/or changes in this service bulletin for effects on Fatigue

Critical Structure (FCS) and for changes to Damage Tolerance Inspections (DTI) required in the

Maintenance Program. This service bulletin affects FCS but no new DTIs are necessary.

L. Interchangeability and Intermixability of Parts

Accomplishment of this service bulletin does not affect interchangeability or intermixability of parts.

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ALERT ALERT
2. MATERIAL INFORMATION

A. Material - Price and Availability

The operator can supply the parts and materials shown in Paragraph 2.C., Parts Necessary For Each

Airplane and Paragraph 2.D., Parts Necessary to Change Spares. As an alternative, operators can

purchase the parts from Boeing Spares. This service bulletin does not show the Boeing price and

supply data.

B. Industry Support Information

Boeing warranty remedies are not available for the inspection and repair procedures given in this

service bulletin.

C. Parts Necessary For Each Airplane

1. Kits/Parts:

None.

2. Parts and Materials Supplied by the Operator:

None.

3. Parts Modified and Reidentified:

None.

4. Parts Removed and Not Replaced:

None.

D. Parts Necessary to Change Spares

Refer to the AMM, OHM and CMM Manuals for bearing replacement.

E. Special Tooling - Price and Availability

None.

F. Special Tooling Necessary to do this Service Bulletin

No special tools or equipment are necessary to do the change in this service bulletin. Also, maintenance

and overhaul tools in manuals shown in Paragraph 1.J., References, can be necessary. Examine

operator tool supply to make sure all necessary tools are available.

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ALERT ALERT
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BOEING SERVICE BULLETIN 737-57A1218

ALERT ALERT

BLANK PAGE
3. ACCOMPLISHMENT INSTRUCTIONS

A. GENERAL INFORMATION

CAUTION: KEEP THE WORK AREA, WIRES AND ELECTRICAL BUNDLES CLEAN OF METAL

PARTICLES OR CONTAMINATION WHEN YOU USE TOOLS. UNWANTED MATERIAL,

METAL PARTICLES OR CONTAMINATION CAUGHT IN WIRE BUNDLES CAN CAUSE

DAMAGE TO THE BUNDLES. DAMAGED WIRE BUNDLES CAN CAUSE SPARKS OR

OTHER ELECTRICAL DAMAGE.

NOTE: 1. The instructions identified in Paragraph 3.B., Work Instructions and the Figure(s)

give the recommended sequence of steps. The sequence of steps to do this service

bulletin can be changed.

2. Manual titles are referred to by acronyms. Refer to Paragraph 1.J., References, for

definition of the acronyms.

3. Obey all of the warnings and cautions given in the specified manual sections.

4. Unless shown differently, these dimensions and tolerances are used:

– Linear dimensions are in inches

– Tolerance on linear dimensions, other than rivet and bolt edge margins, is plus

or minus 0.03 inch

– Tolerance on rivet and bolt edge margin is plus or minus 0.05 inch

– Angular tolerance is plus or minus 2 degrees

– Hole dimensions for standard solid rivets and fasteners are in Structural Repair

Manual (SRM) Chapter 51

– Torque limits to tighten nuts and bolts are in SRM Chapter 51

5. Use the approved fastener and process material substitutions in accordance with

SRM Chapter 51. Alternate fasteners are listed in SRM Chapter 51 and Boeing

Drawing 65-88700.

6. Refer to the SWPM 20-10-11 and SWPM 20-10-12 for the wire installation procedures,

and SWPM 20-10-19 for the wire separation requirements, as accepted procedures.

7. If the length of any fastener specified in this service bulletin does not meet installation

standards given in SRM Chapter 51, then a fastener of the same specification, or

an approved substitute, with a length which meets the installation standards given

in SRM Chapter 51 may be used. In addition, washers may be installed for fastener

grip length in accordance with SRM Chapter 51.

8. A Detailed Inspection is defined as: An intensive examination of a specific item,

installation, or assembly to detect damage, failure, or irregularity. Available lighting

is normally supplemented with a direct source of good lighting at an intensity deemed

appropriate. Inspection aids such as mirrors, magnifying lenses, etc. may be

necessary. Surface cleaning and elaborate procedures may be required.

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ALERT ALERT
9. These work instructions refer to procedures included in other Boeing documents.

When the words "refer to" are used and the operator has an accepted alternative

procedure, the accepted alternative procedure can be used. When the words "in

accordance with" are included in the instruction, the procedure in the Boeing document

must be used.

10. Boeing Service Letter 737-SL-51-042, Damage Reporting and Repair Plan/Design

Guidelines, is an acceptable procedure to request information from Boeing for

additional structural repair instructions. The Service Letter describes what information

must be provided to Boeing before a structural repair can be provided.

11. Refer to Appendix B for manufacturing date and serial number for 65C27409-25

(Table B.1) and 65C27409-27 (Table B.2) carriages manufactured between October

1, 1995 and November 7, 2004..

12. The instructions in Paragraph 3.B., Work Instructions and the figures can include

operation of tools or test equipment. Boeing Engineering Tool Drawings, the Illustrated

Tool and Equipment Manual, and the Special Tool and Ground Handling Drawing

Index contain data on versions of the tools or test equipment that you can use. It is

permitted to use replaced tools. It is not permitted to use superseded tools.

13. If it is necessary to remove more parts for access, you can remove those parts. If

you can get access without removing identified parts, it is not necessary to remove

all of the identified parts. Jacking and shoring limitations must be observed.

14. Where the work instructions include installation of a kept part, a new or serviceable

part with the same part number can be installed as an alternative to the kept part.

The removed part can be discarded if a new or serviceable part is installed.

15. This service bulletin includes functional test procedures for the systems changed by

this service bulletin. More functional tests can possibly be necessary in accordance

with standard maintenance practices because of interruption to other airplane systems.

16. Some Boeing parts are supplied in a temporary configuration. Those parts are

identified with a 'U', 'W', or 'Y' in place of the '-' (dash) in the part number. It is

permitted to install parts identified with a 'U', 'W', or 'Y' as an alternative to the '-'

(dash) part number. Boeing Drawing 005W0900 contains more data.

B. WORK INSTRUCTIONS

Part 1 - Outboard Flap Carriage Spindle Inspection and Repair

1. Remove the outboard trailing edge flaps. Refer to 737-100/200 AMM 27-51-72 or 737-300/400/500

AMM 27-51-34.

2. Remove the midflap carriages from the outboard midflap. Refer to 737-100/200 AMM 27-51-81 or

737-300/400/500 AMM 27-51-44.

3. Remove the CRES sleeve, if present, from the carriage spindle and discard.

4. Remove all finishes, coatings and plating from the spindle, in accordance with Figure 1.

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ALERT ALERT
5. Perform a Detailed Inspection of the entire Carriage Spindle for corrosion and pitting and perform

magnetic particle inspection for cracks in accordance with Figure 1.

6. Do an inspection of the Carriage Spindle in accordance with Figure 2 to make sure the spindle is

not smaller than the minimum allowable diameter. If the carriage does not meet these requirements

it must be removed from service and discarded.

7. Overhaul the Carriage Spindle and repair damage in accordance with OHM 57-53-35

(737-100/200/200C airplanes) or CMM 57-53-36 (737-300/400/500 airplanes).

8. Restore the spindle at the location of the removed sleeve in accordance with OHM 57-53-35

(737-100/200/200C airplanes) or CMM 57-53-36 (737-300/400/500 airplanes).

9. Assemble the carriage in accordance with OHM 57-53-35 (737-100/200/200C airplanes) or CMM

57-53-36 (737-300/400/500 airplanes).

10. Install the midflap carriages in the outboard midflap. Refer to 737-100/200 AMM 27-51-81 or

737-300/400/500 AMM 27-51-44.

11. Install the outboard trailing edge flaps. Refer to 737-100/200 AMM 27-51-72 or 737-300/400/500

AMM 27-51-34.

12. Put the airplane back in serviceable condition.

Part 2 - Outboard Flap Carriage Addition of Serial Number and Tracking of Flight Cycles to

Determine Serviceable Life

1. Track each carriage with a serial number that is added by this service bulletin or was added by

manufacturing and replace the carriage when it reaches it's life limit in accordance with Paragraph

1.E., Compliance.

2. Examine records to see if the number of flight cycles have been recorded for any installed outboard

flap carriage (carriage sub assembly). Refer to Appendix B for the 2 locations of the original serial

number and part number applied during manufacturing, or in accordance with Figures 3 or 4 for

the location of the new serial numbers.

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a. If the recorded past part usage information is available for the carriage, use the data to establish

the number of flight cycles for the carriage when starting the tracking program.

b. If the carriage flight cycles are not available, but records indicate that the carriage has not

been removed from the airplane, use the airplane flight cycles to start the tracking program.

c. If carriage flight cycles are not available and records indicate that the carriage may have come

from one or more older airplanes in the same maintenance program, then use the airplane

flight cycles from the oldest airplane in the maintenance program to start the tracking program.

d. If carriage flight cycles are not available and the flight cycles of the oldest airplane in the

maintenance program are unavailable, or if the carriage has ever been out of your maintenance

program, or was obtained as a previously used spare, consider the carriage to be

undocumented (in accordance with paragraph 1.E., Compliance).

e. Appendix B contains the "Date of Manufacture" for 65C27409-25 and -27 carriages

(manufactured from October 1995 to November 2004) to help determine the service history

of an applicable carriage if required. Records of older carriages are no longer available at

Boeing.

3. If a carriage has exceeded the life limit, follow the instructions in accordance with paragraph 1.E.,

Compliance to determine when it must be replaced.

4. Add a temporary serial number, if required, as follows:

NOTE: This temporary serial number can be used until access is available for applying the

permanent serial number to the carriage. The original manufacturing serial number location

is not easily accessed and it may no longer be readable due to prior overhauls.

a. Supply power to hydraulic system A. Refer to 737-100/200 AMM 27-51-0 or 737-300/400/500

AMM 27-51-00.

b. Extend the outboard main flaps. Refer to 737-100/200 AMM 27-51-00 or 737-300/400/500

AMM 27-51-00.

c. Remove power from hydraulic system A. Refer to 737-100/200 AMM 27-51-0 or

737-300/400/500 AMM 27-51-00.

d. Apply temporary serial number in accordance with Figure 3.

e. Supply power to hydraulic system A. Refer to 737-100/200 AMM 27-51-0 or 737-300/400/500

AMM 27-51-00.

f. Retract the outboard main flaps. Refer to 737-100/200 AMM 27-51-00 or 737-300/400/500

AMM 27-51-00.

g. Remove power from hydraulic system A. Refer to 737-100/200 AMM 27-51-0 or

737-300/400/500 AMM 27-51-00.

h. Put the airplane back to a serviceable condition.

5. Add a permanent serial number, if required, as follows:

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a. Remove the outboard flap track center fairings. Refer to 737-100/200 AMM 27-51-121 page

401 or 737-300/400/500 AMM 27-51-52 page 401.

b. Add a permanent serial number in accordance with Figure 4. Use the same serial number

used for the temporary serial number, if a temporary serial number was applied.

NOTE: The original manufacturing serial number location is not easily accessed and it may

no longer be readable due to prior overhauls.

c. Install the outboard flap track center fairings. Refer to 737-100/200 AMM 27-51-121 page 401

or 737-300/400/500 AMM 27-51-52 page 401.

d. Put the airplane back to a serviceable condition.

NOTE: This permanent serial number should be added the next time the outboard flap track

center fairings are removed.

NOTE: The serial number should be added in addition to the serial number that was added in

production. The serial number that was added in production is located in accordance with

Figure 3.

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ALERT ALERT
FIGURE 1: CARRIAGE SPINDLE INSPECTION AND REPAIR

(SHEET 1 OF 3)

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The step numbers shown below agree with the numbers shown in the circle symbols in the figure.

FIGURE 1: CARRIAGE SPINDLE INSPECTION AND REPAIR

(SHEET 2 OF 3)

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STEP TASK NAME PROCEDURE NOTES

1 Remove Trailing Edge Flap AMM 27-51-72 or

AMM 27-51-34

2 Remove Midflap Carriage AMM 27-51-81 or

AMM 27-51-44

3 Remove Cress Sleeve (a)

Note: When overhauling the spindle, all finishes, coatings and plating must be removed from

the spindle.

4 Remove Finish SOPM 20-30-02 (a)

Coating SOPM 20-30-02 (a)

Plating SOPM 20-30-02 (a)

Look for corrosion, pitting

and cracks along the entire

length of the spindle.

5 Inspect Carriage Spindle Detailed Inspection

Inspect for cracks refer to

SOPM 20-20-01. If cracks

are found discard the carriage.

Magnetic Particle Inspection

If damage is beyond the repair limits, the carriage must

be discarded.

OHM 57-53-35 or

CMM 57-53-36

Overhaul / Carriage Spindle

Repair

6

(a) If applicable.

FIGURE 1: CARRIAGE SPINDLE INSPECTION AND REPAIR

(SHEET 3 OF 3)

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ALERT ALERT
The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY

numbers shown below are the number of parts necessary for each carriage.

FIGURE 2: MINIMUM ALLOWABLE SPINDLE DIAMETER

(SHEET 1 OF 2)

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STEP TASK NAME IDENTIFICATION QTY MORE DATA

1 Measure Spindle Diameter "A" - 1 (a)

2 Measure Spindle Diameter "B" - 1 (a)

3 Measure Spindle Diameter "C" - 1 (a)

(a) Measure and record the spindle diameter "A" or "B" or "C". There can be the option of two possible carriages

installed on the airplane as shown.

If spindle diameter before plating/coating is less than detailed in the following list, remove carriage from service.

Airplane Model Effective Part Number Inboard/Outboard Minimum Allowable Diameter

"A" "B" "C"

Inboard and Out- 1.6810 1.6668 0.8371

board

737-100/200 65-47821-6/-8/-10/-12/-16

Inboard and Out- 1.6810 1.6590 0.8371

board

737-100/200 65-47821-20/-22/-24/-26/-28

Inboard and Out- 1.8792 1.8792 0.8898

board

737-100/200HGW 65-67159-1/-5/-7

Inboard and Out- 1.8792 1.8730 0.8898

board

737-100/200HGW 65-67159-9

737-300/400/500 65C27409-5/-9/-13/-17 Outboard 1.7858 1.7199 0.9046

737-300/400/500 65C27409-6/-10/-18/-21/-23 Inboard 1.8800 1.8151 0.8939

737-300/400/500 65C27409-25 Outboard 1.8111 1.7174 0.9046

737-300/400/500 65C27409-27 Inboard 1.9409 1.8151 0.8827

FIGURE 2: MINIMUM ALLOWABLE SPINDLE DIAMETER

(SHEET 2 OF 2)

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ALERT ALERT
The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY

numbers shown below are the number of parts necessary for each airplane.

FIGURE 3: APPLICATION OF CARRIAGE TEMPORARY SERIAL NUMBERS

(SHEET 1 OF 2)

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ALERT ALERT
STEP TASK NAME IDENTIFICATION QTY MORE DATA

1 Mark Outboard Flap Carriage - 4 (a)

2 Track Serial Number - - (b)

(a) Mark serial numbers on all carriages in order to start tracking of the component. To get carriages

with unique serial numbers, use your company three letter code or company name and a numerical

sequence number as the serial number (example: XYZ001). The serial number must be different on

each carriage. Mark within the area shown approximately in the illustration.

Note: Use a rubber stamp to apply the temporary serial number within the approximate area shown

in the illustration. Refer to SOPM 20-50-10 or apply with ink or paint as per an equivalent procedure.

Do not use any of the methods detailed for the application of carriage permanent serial numbers

given in Figure 4.

(b) Reference Appendix B for the two locations of the original serial numbers and part numbers applied

during manufacturing.

FIGURE 3: APPLICATION OF CARRIAGE TEMPORARY SERIAL NUMBERS

(SHEET 2 OF 2)

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ALERT ALERT
The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY

numbers shown below are the number of parts necessary for each airplane.

FIGURE 4: APPLICATION OF CARRIAGE PERMANENT SERIAL NUMBERS

(SHEET 1 OF 2)

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ALERT ALERT
STEP TASK NAME IDENTIFICATION QTY MORE DATA

1 Mark Outboard Flap Carriage - 4 (a) (b)

2 Track Serial Number - - (c)

(a) Mark serial numbers on all carriages in order to start tracking of the component. To get carriages

with unique serial numbers, use your company three letter code or company name and a numerical

sequence number as the serial number (example: XYZ001). The serial number must be different on

each carriage. Mark within the approximate area shown in the illustration.

Note: Use one of the options below, or an equivalent procedure, to mark a serial number on a carriage.

The maximum height of each character is to be 0.25 inches. It must be possible to read the serial

number after all finishes are applied. Refer to SOPM 20-50-10.

1) Deep electro-chemical etch (0.006 to 0.009 inch deep).

2) Electric vibrating pencil (maximum 0.015 inch deep).

3) Spherical nose cutter (maximum 0.015 inch deep).

4) Dot Peen Marking.

(b) This is where Boeing rubber stamped the part number, serial number and date of manufacture.

(c) Reference Appendix B for the two locations of the original serial numbers and part numbers applied

during manufacturing.

FIGURE 4: APPLICATION OF CARRIAGE PERMANENT SERIAL NUMBERS

(SHEET 2 OF 2)

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ALERT ALERT
The Existing Parts Accountability table has been removed. All carriages are subject to the requirements of

paragraph 1.E., Compliance. See Table 1 in paragraph 1.D., Description, for a list of carriage and carriage

assembly part numbers.

Appendix A: EXISTING PARTS ACCOUNTABILITY

(SHEET 1 OF 1)

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ALERT ALERT
This appendix contains information on 65C27409-25 (Table B.1) and 65C27409-27 (Table B.2) carriages

manufactured between October 1, 1995 and November 7, 2004. Records of older carriages are no longer

available at Boeing. The illustration below shows the location of this information on the carriage. The date of

manufacture is the date of the final assembly acceptance.

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 1 OF 22)

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ALERT ALERT
Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 2 OF 22)

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ALERT ALERT
TABLE B.1: 65C27409-25

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

1279 3/1/1996 1759 5/5/1996 1928 1/10/1996

1280 3/1/1996 1760 5/5/1996 1929 1/10/1996

1281 3/1/1996 1761 5/5/1996 1931 1/10/1996

1282 3/1/1996 1766 5/10/1996 1932 1/10/1996

1362 3/1/1996 1767 5/10/1996 1933 10/1/1995

1364 3/1/1996 1768 5/10/1996 1934 10/1/1995

1371 3/1/1996 1769 5/10/1996 1935 10/1/1995

1374 3/1/1996 1777 8/22/1996 1936 10/1/1995

1570 3/18/1996 1782 5/30/1996 1944 3/18/1996

1573 3/18/1996 1783 5/30/1996 1948 2/19/1996

1577 7/1/1996 1784 5/30/1996 1953 2/19/1996

1593 3/12/1996 1785 5/30/1996 1958 2/19/1996

1595 3/12/1996 1827 4/17/1996 1961 4/17/1996

1597 6/4/1996 1828 4/17/1996 1965 6/20/1996

1605 3/12/1996 1829 4/17/1996 1970 6/20/1996

1627 3/5/1996 1831 5/16/1996 1973 6/20/1996

1629 5/16/1996 1832 5/16/1996 1977 7/16/1996

1632 3/5/1996 1833 5/16/1996 1981 5/3/1996

1634 3/5/1996 1834 5/20/1996 1982 8/21/1996

1645 3/11/1996 1835 5/20/1996 1983 9/2/1996

1646 3/11/1996 1836 5/20/1996 1984 5/3/1996

1647 3/11/1996 1837 5/20/1996 1985 9/10/1996

1648 3/11/1996 1898 1/24/1996 1986 5/3/1996

1710 6/26/1996 1899 2/20/1996 1987 6/20/1996

1711 6/26/1996 1900 2/20/1996 1988 9/10/1996

1712 6/26/1996 1901 3/13/1996 1989 8/21/1996

1713 6/26/1996 1902 2/20/1996 1990 8/22/1996

1714 6/26/1996 1903 2/20/1996 1991 8/22/1996

1715 6/26/1996 1904 1/24/1996 1992 8/21/1996

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 3 OF 22)

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ALERT ALERT
TABLE B.1: 65C27409-25

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

1716 6/26/1996 1905 1/24/1996 1993 8/22/1996

1717 6/26/1996 1914 1/24/1996 1994 8/22/1996

1750 4/15/1996 1915 1/24/1996 1995 8/25/1996

1752 4/15/1996 1917 2/6/1996 1996 8/25/1996

1754 4/15/1996 1919 2/6/1996 1997 8/21/1996

1756 4/15/1996 1920 1/24/1996 1998 9/7/1998

1758 5/5/1996 1921 1/24/1996 1999 8/21/1996

2000 8/25/1996 2086 10/26/1996 2381 5/15/1997

2003 8/22/1996 2087 10/26/1996 2382 5/15/1997

2006 8/7/1996 2088 10/26/1996 2383 5/15/1997

2007 8/22/1996 2130 11/13/1996 2384 6/12/1997

2008 8/22/1996 2133 11/13/1996 2385 6/12/1997

2009 8/7/1996 2134 11/13/1996 2386 6/12/1997

2010 8/7/1996 2135 11/13/1996 2387 6/12/1997

2011 8/7/1996 2136 11/26/1996 2397 6/12/1997

2016 9/30/1996 2137 12/3/1996 2398 6/12/1997

2017 9/30/1996 2139 11/26/1996 2400 6/12/1997

2018 9/30/1996 2140 11/13/1996 2401 6/12/1997

2019 9/30/1996 2142 11/13/1996 2402 6/12/1997

2021 8/22/1996 2143 11/13/1996 2403 8/20/1997

2022 10/23/1996 2145 11/13/1996 2404 6/12/1997

2024 10/31/1996 2146 11/24/1996 2405 5/30/1997

2025 10/23/1996 2150 11/24/1996 2406 5/30/1997

2038 11/12/1996 2151 11/24/1996 2407 5/30/1997

2039 10/23/1996 2152 11/24/1996 2408 5/30/1997

2041 10/23/1996 2154 12/3/1996 2431 5/30/1997

2045 10/23/1996 2155 11/2/1996 2433 5/30/1997

2053 10/23/1996 2156 11/2/1996 2435 5/30/1997

2054 10/23/1996 2157 11/2/1996 2436 5/30/1997

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 4 OF 22)

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ALERT ALERT
TABLE B.1: 65C27409-25

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

2060 10/23/1996 2159 11/2/1996 2446 6/12/1997

2061 10/23/1996 2167 12/3/1996 2448 6/12/1997

2068 6/27/1996 2172 11/26/1996 2450 6/12/1997

2069 6/27/1996 2175 12/3/1996 2452 6/12/1997

2070 6/27/1996 2177 11/26/1996 2465 6/27/1997

2071 6/27/1996 2181 11/20/1996 2524 6/12/1997

2075 10/23/1996 2185 11/20/1996 2542 7/27/1997

2077 10/23/1996 2188 11/20/1996 2554 8/8/1997

2078 10/23/1996 2190 11/20/1996 2555 6/27/1997

2079 10/23/1996 2219 12/18/1996 2556 6/27/1997

2080 10/23/1996 2220 12/18/1996 2561 8/4/1997

2082 8/19/1996 2221 12/18/1996 2562 8/4/1997

2083 8/19/1996 2225 12/18/1996 2563 8/4/1997

2084 8/19/1996 2300 8/8/1997 2564 8/20/1997

2085 10/26/1996 2380 5/15/1997 2573 9/24/1997

2574 11/1/1997 2631 7/15/1997 2716 8/25/1997

2575 11/1/1997 2632 7/15/1997 2717 8/25/1997

2576 11/1/1997 2641 8/4/1997 2718 10/8/1997

2581 7/4/1997 2642 8/4/1997 2723 9/8/1997

2582 7/1/1997 2643 8/4/1997 2724 9/8/1997

2583 7/4/1997 2644 8/4/1997 2725 9/8/1997

2584 7/1/1997 2648 7/15/1997 2726 9/8/1997

2585 7/4/1997 2650 7/15/1997 2727 12/2/1997

2586 6/27/1997 2651 7/15/1997 2728 12/2/1997

2587 7/4/1997 2652 7/15/1997 2729 9/28/1997

2588 7/1/1997 2661 9/5/1997 2730 12/2/1997

2593 7/1/1997 2662 9/5/1997 2736 9/28/1997

2594 7/1/1997 2663 9/5/1997 2738 9/28/1997

2595 7/1/1997 2664 9/5/1997 2740 9/28/1997

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 5 OF 22)

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ALERT ALERT
TABLE B.1: 65C27409-25

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

2596 7/1/1997 2666 8/20/1997 2742 9/28/1997

2597 7/1/1997 2667 8/20/1997 2743 11/11/1997

2598 7/1/1997 2668 8/20/1997 2745 11/11/1997

2599 7/1/1997 2673 9/15/1997 2746 11/11/1997

2600 7/1/1997 2674 9/15/1997 2747 11/11/1997

2605 7/8/1997 2675 9/15/1997 2756 10/9/1997

2606 7/8/1997 2676 9/15/1997 2760 10/9/1997

2607 7/8/1997 2682 8/5/1997 2762 11/7/2004

2608 7/8/1997 2683 8/5/1997 2763 10/9/1997

2609 7/29/1997 2684 8/5/1997 2766 10/9/1997

2610 7/29/1997 2685 8/5/1997 2767 11/7/2004

2611 7/29/1997 2686 9/4/1997 2768 11/7/2004

2612 7/29/1997 2687 9/4/1997 2769 11/7/2004

2621 8/7/1997 2689 9/4/1997 2776 11/11/1997

2622 8/7/1997 2690 9/4/1997 2777 11/11/1997

2623 8/7/1997 2699 8/20/1997 2778 11/11/1997

2624 8/7/1997 2701 8/20/1997 2780 11/11/1997

2625 7/15/1997 2702 8/20/1997 2786 11/25/1997

2626 7/15/1997 2707 8/20/1997 2787 11/25/1997

2627 7/15/1997 2708 8/20/1997 2788 11/25/1997

2628 7/15/1997 2709 8/20/1997 2789 11/25/1997

2629 7/15/1997 2710 8/20/1997 2793 11/24/1997

2630 7/15/1997 2715 8/25/1997 2794 12/10/1997

2795 12/10/1997 2880 12/18/1997 2970 2/25/1998

2796 12/10/1997 2882 1/20/1998 2971 3/2/1998

2797 12/10/1997 2894 11/20/1997 2972 3/2/1998

2798 10/10/1997 2915 1/20/1998 2973 3/2/1998

2799 10/10/1997 2916 1/20/1998 2974 3/2/1998

2800 10/10/1997 2917 1/20/1998 2975 3/1/1998

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 6 OF 22)

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ALERT ALERT
TABLE B.1: 65C27409-25

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

2801 10/10/1997 2918 1/20/1998 2976 3/1/1998

2812 2/12/1998 2923 1/3/1998 2977 3/1/1998

2813 2/12/1998 2924 1/3/1998 2978 3/1/1998

2814 2/12/1998 2925 1/7/1998 2995 6/26/1998

2815 3/1/1998 2926 1/3/1998 3002 7/28/1998

2820 2/10/1998 2931 1/9/1998 3003 7/28/1998

2821 2/10/1998 2932 1/9/1998 3004 7/28/1998

2822 2/10/1998 2933 1/9/1998 3005 7/28/1998

2823 2/10/1998 2934 1/9/1998 3024 9/14/1998

2827 6/11/1998 2935 1/8/1998 3025 9/14/1998

2828 2/16/1998 2936 1/8/1998 3026 9/14/1998

2829 2/16/1998 2938 1/8/1998 3027 9/14/1998

2830 2/16/1998 2939 1/8/1998 3028 9/2/1998

2831 2/16/1998 2940 1/23/1998 3029 9/2/1998

2832 1/27/1998 2942 1/23/1998 3030 9/2/1998

2833 1/27/1998 2943 1/23/1998 3031 9/2/1998

2834 1/27/1998 2944 1/23/1998 3044 9/5/1998

2835 1/27/1998 2947 2/1/1998 3045 9/5/1998

2852 2/24/1998 2954 1/8/1998 3046 9/5/1998

2853 2/24/1998 2955 1/8/1998 3047 9/5/1998

2854 2/24/1998 2956 1/8/1998 3052 8/26/1998

2855 2/24/1998 2958 1/20/1998 3053 9/2/1998

2865 1/29/1998 2960 1/20/1998 3054 8/26/1998

2866 1/29/1998 2961 2/25/1998 3055 9/2/1998

2867 1/29/1998 2962 1/20/1998 3056 8/26/1998

2868 1/29/1998 2964 1/20/1998 3057 9/2/1998

2869 1/25/1999 2965 2/25/1998 3059 9/2/1998

2875 1/4/1998 2966 1/20/1998 3062 3/28/1998

2876 1/5/1998 2967 1/20/1998 3063 3/28/1998

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 7 OF 22)

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ALERT ALERT
TABLE B.1: 65C27409-25

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

2877 1/3/1998 2968 1/20/1998 3064 3/28/1998

2878 1/3/1998 2969 2/25/1998 3065 3/28/1998

3087 4/13/1998 3183 6/23/1998 B3251 3/16/1999

3089 4/13/1998 3184 6/23/1998 B3252 3/21/1999

3090 4/13/1998 3185 6/13/1998 B3268 6/3/1999

3091 4/13/1998 3190 6/26/1998 B3269 6/2/1999

3104 3/16/1998 3191 6/26/1998 B3270 6/2/1999

3105 3/16/1998 3192 6/26/1998 B3271 6/14/1999

3106 3/16/1998 B2740 2/10/2004 B3273 4/22/1999

3107 3/16/1998 B2896 9/11/2004 B3274 5/12/1999

3108 4/21/2004 B3194 10/21/1998 B3277 5/12/1999

3109 4/21/2004 B3195 10/21/1998 B3281 3/29/1999

3110 4/21/2004 B3196 11/30/1998 B3288 2/26/1999

3116 6/9/1998 B3197 10/21/1998 B3299 6/14/1999

3117 4/15/1998 B3198 11/12/1998 B3300 6/14/1999

3118 4/15/1998 B3199 11/12/1998 B3305 6/16/1999

3119 6/16/1998 B3200 11/12/1998 B3306 6/16/1999

3124 7/9/1998 B3201 11/12/1998 B3307 6/14/1999

3125 7/15/1998 B3206 2/26/1999 B3313 4/22/1999

3126 7/9/1998 B3209 2/26/1999 B3314 5/12/1999

3127 7/15/1998 B3210 2/23/1999 B3315 5/12/1999

3136 8/3/1998 B3211 2/3/1999 B3417 12/21/2000

3137 7/9/1998 B3212 2/23/1999 B3418 12/19/2000

3138 8/23/1998 B3213 2/3/1999 B3419 12/21/2000

3139 7/9/1998 B3214 1/20/1999 B3447 5/8/2001

3144 5/11/1998 B3215 2/3/1999 B3449 4/30/2001

3145 5/11/1998 B3216 1/20/1999 B3450 5/8/2001

3146 5/11/1998 B3218 2/3/1999 B3453 4/16/2001

3147 5/11/1998 B3227 11/5/1998 B3456 4/5/2002

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 8 OF 22)

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ALERT ALERT
TABLE B.1: 65C27409-25

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

3148 8/12/1998 B3228 11/5/1998 B3458 4/16/2001

3156 4/21/1998 B3230 11/5/1998 B3459 5/5/2001

3157 4/21/1998 B3231 11/5/1998 B3461 12/19/2000

3158 4/21/1998 B3232 1/20/1999 B3465 8/24/2001

3159 4/21/1998 B3236 2/10/1999 B3466 10/25/2001

3178 5/11/1998 B3238 1/20/1999 B3469 8/21/2001

3179 7/9/1998 B3240 1/25/1999 B3471 8/18/2001

3180 5/11/1998 B3241 4/22/1999 B3472 7/12/2001

3181 5/11/1998 B3247 3/29/1999 B3477 10/25/2001

3182 6/23/1998 B3250 3/16/1999 B3479 11/27/2001

B3482 11/15/2003 B3557 4/11/2003 B3627 2/25/2004

B3483 11/15/2001 B3560 5/20/2003 B3635 11/12/2003

B3485 11/6/2001 B3561 5/20/2003 B3636 1/23/2004

B3489 10/1/2002 B3563 4/23/2003 B3637 11/11/2003

B3490 10/1/2002 B3565 1/29/2003 B3638 11/21/2003

B3491 10/30/2002 B3566 10/10/2003 B3644 10/16/2003

B3492 10/28/2002 B3567 5/20/2003 B3645 10/16/2003

B3496 1/10/2003 B3569 11/2/2003 B3646 10/6/2003

B3497 11/27/2001 B3570 11/12/2003 B3647 10/14/2003

B3498 11/27/2001 B3571 11/12/2003 B3654 1/23/2004

B3504 2/7/2002 B3573 11/12/2003 B3655 1/28/2004

B3505 4/1/2002 B3574 11/12/2003 B3656 4/2/2004

B3507 21/6/2002 B3579 10/13/2003 B3657 1/21/2004

B3508 4/2/2002 B3581 10/13/2003 B3662 1/16/2004

B3509 5/30/2002 B3582 10/3/2003 B3663 1/6/2004

B3510 5/30/2002 B3583 10/4/2003 B3664 1/16/2004

B3511 4/27/2002 B3584 10/3/2003 B3665 1/23/2004

B3512 7/26/2002 B3590 1/6/2004 B3666 11/23/2003

B3513 4/27/2002 B3591 1/6/2004 B3667 1/23/2004

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 9 OF 22)

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ALERT ALERT
TABLE B.1: 65C27409-25

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

B3516 1/30/2003 B3592 1/6/2004 B3668 1/23/2004

B3521 10/11/2003 B3593 1/6/2004 B3669 1/23/2004

B3523 6/11/2003 B3598 11/26/2003 B3670 12/20/2003

B3525 6/11/2003 B3599 11/26/2003 B3672 11/22/2003

B3528 6/30/2003 B3600 1/16/2004 B3674 1/31/2004

B3529 6/30/2003 B3601 12/11/2003 B3675 1/16/2004

B3530 8/25/2003 B3602 1/6/2004 B3696 5/15/2004

B3534 5/1/2003 B3603 1/23/2004 B3697 3/6/2004

B3536 4/5/2003 B3604 1/6/2004 B3698 3/10/2004

B3537 4/5/2003 B3605 1/23/2004 B3699 3/17/2004

B3539 4/12/2003 B3610 1/6/2004 B3700 2/27/2004

B3541 7/2/2003 B3611 1/6/2004 B3701 2/27/2004

B3542 7/2/2003 B3612 1/6/2004 B3703 4/13/2004

B3543 6/4/2003 B3613 1/16/2004 B3704 2/25/2004

B3544 7/2/2003 B3619 11/19/2003 B3705 4/5/2004

B3550 7/2/2003 B3621 11/19/2003 B3706 2/1/2004

B3552 6/30/2003 B3623 11/19/2003 B3707 2/10/2004

B3555 7/8/2003 B3626 11/19/2003 B3708 2/20/2004

B3709 3/18/2004 B3812 3/17/2004 B3863 8/14/2004

B3710 2/15/2004 B3813 3/29/2004 B3864 6/6/2004

B3711 2/15/2004 B3817 5/24/2004 B3865 5/13/2004

B3712 3/18/2004 B3818 6/21/2004 B3866 6/6/2004

B3737 2/29/2004 B3819 3/29/2004 B3867 5/13/2004

B3738 2/25/2004 B3820 5/12/2004 B3868 5/12/2004

B3739 2/15/2004 B3821 4/28/2004 B3869 4/30/2004

B3741 2/27/2004 B3822 3/17/2004 B3880 6/21/2004

B3742 2/6/2004 B3823 3/10/2004 B3881 6/22/2004

B3743 2/6/2004 B3824 3/29/2004 B3889 10/6/2004

B3744 2/27/2004 B3825 5/13/2004 B3890 10/5/2004

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 10 OF 22)

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Original Issue: July 22, 1993

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ALERT ALERT
TABLE B.1: 65C27409-25

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

B3746 2/6/2004 B3826 3/18/2004 B3891 10/9/2004

B3753 4/12/2004 B3827 9/11/2004 B3892 9/15/2004

B3754 3/10/2004 B3828 3/18/2004 B3893 10/6/2004

B3755 3/17/2004 B3829 4/8/2004 B3894 9/11/2004

B3756 2/29/2004 B3830 4/2/2004 B3895 10/6/2004

B3758 2/27/2004 B3831 5/12/2004 B3898 8/14/2004

B3759 2/25/2004 B3832 5/15/2004 B3899 10/18/2004

B3760 2/25/2004 B3833 6/6/2004 B3900 9/9/2004

B3771 6/6/2004 B3834 5/3/2004 B3902 10/6/2004

B3774 5/24/2004 B3835 5/15/2004 B3903 10/6/2004

B3778 4/2/2004 B3840 3/29/2004 B3904 10/6/2004

B3779 5/27/2004 B3841 5/12/2004 B3906 7/25/2004

B3792 3/10/2004 B3842 6/14/2004 B3907 8/20/2004

B3793 3/10/2004 B3843 5/13/2004 B3908 8/29/2004

B3795 3/17/2004 B3844 5/13/2004 B3909 8/20/2004

B3796 3/20/2004 B3845 4/2/2004 B3911 6/14/2004

B3797 5/13/2004 B3846 5/24/2004 B3916 8/21/2004

B3798 3/20/2004 B3853 5/15/2004 B3920 8/15/2004

B3800 3/16/2004 B3855 3/18/2004 B3932 8/5/2004

B3802 6/10/2004 B3856 5/15/2004 B3935 6/26/2004

B3803 5/24/2004 B3857 6/21/2004 B3937 6/26/2004

B3804 4/2/2004 B3858 5/13/2004 B3944 10/6/2004

B3805 4/28/2004 B3859 5/15/2004 B3954 10/3/2004

B3806 5/17/2004 B3860 5/15/2004 B4004 6/21/2004

B3808 5/27/2004 B3861 4/2/2004 B4005 6/21/2004

B3811 8/14/2004 B3862 6/14/2004 B4006 6/22/2004

B4008 6/21/2004 B4057 10/6/2004 P7092 8/16/1996

B4020 6/21/2004 B4058 8/14/2004 P7097 7/27/1996

B4021 6/26/2004 B4059 8/21/2004 P7112 6/13/1996

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 11 OF 22)

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: July 22, 1993

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ALERT ALERT
TABLE B.1: 65C27409-25

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

B4023 8/5/2004 B4077 10/18/2004 P7116 6/20/1996

B4024 8/22/2004 B4078 10/6/2004 P7117 6/24/1996

B4025 8/20/2004 B4079 10/9/2004 P7118 6/20/1996

B4026 10/6/2004 B4080 10/6/2004 P7119 10/16/1996

B4027 6/14/2004 B4081 10/17/2004 P7144 7/27/1996

B4028 8/14/2004 B4082 10/18/2004 P7146 6/20/1996

B4029 6/26/2004 B4083 10/9/2004 P7155 8/16/1996

B4030 8/27/2004 B4084 10/18/2004 P7157 8/14/1996

B4032 8/21/2004 B4085 8/27/2004 P7160 7/17/1996

B4033 8/29/2004 B4086 8/21/2004 P7175 10/29/1996

B4034 7/25/2004 B4096 10/18/2004 P7184 10/16/1996

B4035 6/21/2004 B4097 10/18/2004 P7185 10/16/1996

B4040 10/6/2004 B4099 10/18/2004 P7234 8/16/1996

B4041 10/6/2004 P6990 6/13/1996 P7242 6/20/1996

B4042 10/18/2004 P7020 6/24/1996 P7245 10/16/1996

B4043 10/6/2004 P7025 10/29/1996 P7247 10/16/1996

B4046 10/6/2004 P7026 10/16/1996 P7248 8/14/1996

B4047 10/9/2004 P7027 10/16/1996 P7249 10/16/1996

B4052 8/20/2004 P7032 6/24/1996 P7251 8/22/1996

B4053 9/11/2004 P7033 10/29/1996 P7253 7/27/1996

B4054 8/27/2004 P7037 8/16/1996 P7273 8/14/1996

B4055 8/27/2004 P7085 10/29/1996 P7305 7/27/1996

B4056 8/27/2004 P7089 10/21/1996

TABLE B.2: 65C27409-27

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

1283 4/2/1996 1718 7/1/1996 1789 5/21/1996

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 12 OF 22)

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Copyright © Unpublished Work - See page 1 for details.

Original Issue: July 22, 1993

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ALERT ALERT
TABLE B.2: 65C27409-27

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

1284 4/9/1996 1719 7/1/1996 1795 9/26/1996

1285 4/2/1996 1720 9/26/1996 1823 4/30/1996

1286 4/2/1996 1721 5/26/1996 1824 4/30/1996

1297 3/15/1996 1722 6/28/1996 1825 4/30/1996

1306 1/10/1996 1723 6/28/1996 1826 4/30/1996

1307 1/10/1996 1724 6/28/1996 1892 3/18/1996

1308 1/10/1996 1725 6/28/1996 1894 3/18/1996

1309 1/10/1996 1742 3/28/1996 1895 3/18/1996

1352 2/19/1996 1743 4/28/1997 1897 3/18/1996

1353 2/19/1996 1744 3/28/1996 1906 4/18/1996

1354 2/19/1996 1745 4/28/1997 1907 5/19/1996

1360 2/19/1996 1746 3/28/1996 1908 4/18/1996

1385 3/15/1996 1747 4/28/1997 1909 4/18/1996

1386 3/15/1996 1748 3/28/1996 1922 1/10/1996

1392 3/15/1996 1749 4/28/1997 1923 1/10/1996

1628 9/26/1996 1751 3/24/1996 1924 1/24/1996

1630 9/26/1996 1753 5/26/1996 1925 1/10/1996

1633 9/26/1996 1755 5/26/1996 1926 1/24/1996

1649 4/2/1996 1757 3/24/1996 1927 1/10/2006

1650 4/2/1996 1763 5/3/1996 1939 1/24/1996

1651 4/2/1996 1764 5/3/1996 1940 2/24/1996

1652 4/2/1996 1765 5/3/1996 1942 1/24/1996

1661 1/23/1996 1770 6/6/1996 1959 7/17/1996

1662 1/23/1996 1771 6/6/1996 1960 7/17/1996

1665 2/29/1996 1772 6/6/1996 1962 7/17/1996

1666 2/29/1996 1773 6/6/1996 1963 7/17/1996

1667 2/29/1996 1774 9/7/1996 1964 7/19/1996

1668 2/28/1996 1775 9/7/1996 1966 7/19/1996

1669 10/4/1995 1776 9/7/1996 1967 7/19/1996

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 13 OF 22)

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: July 22, 1993

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ALERT ALERT
TABLE B.2: 65C27409-27

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

1670 2/19/1996 1777 8/22/1996 1968 7/19/1996

1671 10/4/1995 1778 8/14/1996 1969 6/28/1996

1672 10/4/1995 1779 8/14/1996 1971 6/28/1996

1673 1/10/1996 1780 8/14/1996 1972 6/28/1996

1674 1/10/1996 1781 8/14/1996 1974 6/28/1996

1675 1/10/1996 1787 5/21/1996 1975 6/6/1996

1676 1/10/1996 1788 5/21/1996 1979 6/6/1996

1980 6/6/1996 2061 10/23/1996 2153 11/14/1996

2001 7/19/1996 2062 7/1/1996 2158 11/14/1996

2002 7/19/1996 2063 7/1/1996 2160 11/25/1996

2003 8/22/1996 2064 10/21/1996 2161 11/14/1996

2004 7/19/1996 2065 7/1/1996 2162 11/25/1996

2005 7/19/1996 2066 10/21/1996 2163 11/14/1996

2006 8/7/1996 2067 10/21/1996 2164 11/25/1996

2007 8/22/1996 2072 10/21/1996 2165 11/25/1996

2008 8/22/1996 2073 11/14/1996 2173 11/26/1996

2009 8/7/1996 2075 10/23/1996 2176 11/26/1996

2010 8/7/1996 2077 10/23/1996 2178 11/26/1996

2011 8/7/1996 2078 10/23/1996 2204 12/17/1996

2012 8/7/1996 2079 10/23/1996 2207 12/17/1996

2013 8/7/1996 2080 10/23/1996 2210 12/17/1996

2014 8/7/1996 2081 9/30/1996 2232 12/18/1996

2015 8/7/1996 2082 8/19/1996 2233 12/18/1996

2021 8/22/1996 2083 8/19/1996 2236 12/18/1996

2023 12/17/1996 2084 8/19/1996 2238 12/18/1996

2030 12/17/1996 2114 10/11/1996 2388 5/21/1997

2042 12/17/1996 2115 10/11/1996 2390 5/21/1997

2043 12/17/1996 2116 10/11/1996 2392 5/21/1997

2044 7/8/1996 2117 10/11/1996 2394 5/21/1997

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 14 OF 22)

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: July 22, 1993

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ALERT ALERT
TABLE B.2: 65C27409-27

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

2046 10/10/1996 2119 9/26/1996 2409 6/23/1997

2047 7/16/1996 2120 9/26/1996 2410 6/23/1997

2048 10/10/1996 2121 9/26/1996 2411 6/23/1997

2049 10/10/1996 2122 11/27/1996 2412 6/23/1997

2050 10/10/1996 2123 11/27/1996 2421 5/21/1997

2051 7/8/1996 2128 11/27/1996 2423 5/21/1997

2052 7/8/1996 2129 11/27/1996 2425 5/21/1997

2053 10/23/1996 2131 11/24/1996 2427 5/21/1997

2054 10/23/1996 2132 11/20/1996 2429 6/6/1997

2055 7/8/1996 2138 11/24/1996 2430 6/5/1997

2056 7/8/1996 2141 11/20/1996 2432 6/6/1997

2057 7/8/1996 2144 10/31/1996 2434 6/6/1997

2058 7/8/1996 2147 10/31/1996 2437 6/6/1997

2059 7/1/1996 2148 10/31/1996 2438 6/6/1997

2060 10/23/1996 2149 10/31/1996 2439 6/6/1997

2440 9/21/1997 2570 11/11/1997 2659 8/19/1997

2441 6/5/1997 2571 11/11/1997 2660 8/19/1997

2442 6/5/1997 2572 12/18/1997 2669 9/4/1997

2443 6/5/1997 2577 9/11/1997 2670 9/4/1997

2444 6/5/1997 2578 9/11/1997 2671 9/4/1997

2445 6/23/1997 2579 9/11/1997 2672 9/4/1997

2447 6/23/1997 2580 9/11/1997 2678 8/15/1997

2449 6/23/1997 2589 6/28/1997 2679 8/15/1997

2451 6/23/1997 2590 6/28/1997 2680 8/15/1997

2453 7/9/1997 2591 6/28/1997 2681 8/15/1997

2454 6/24/1997 2592 6/28/1997 2691 8/29/1997

2455 7/9/1997 2613 7/9/1997 2692 10/8/1997

2456 6/24/1997 2614 7/9/1997 2693 8/29/1997

2457 7/9/1997 2615 7/9/1997 2694 8/29/1997

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 15 OF 22)

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: July 22, 1993

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ALERT ALERT
TABLE B.2: 65C27409-27

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

2458 6/24/1997 2616 7/9/1997 2695 8/15/1997

2459 7/9/1997 2617 7/17/1997 2696 8/15/1997

2460 6/24/1997 2618 7/17/1997 2697 8/15/1997

2461 6/25/1997 2619 7/17/1997 2698 8/15/1997

2462 6/25/1997 2620 7/17/1997 2703 8/15/1997

2463 6/25/1997 2633 7/25/1997 2704 8/15/1997

2464 6/25/1997 2634 7/25/1997 2706 8/15/1997

2479 5/15/1997 2635 7/25/1997 2711 8/29/1997

2484 5/15/1997 2636 7/25/1997 2712 8/29/1997

2498 12/18/1997 2637 7/26/1997 2713 8/29/1997

2511 6/6/1997 2638 9/8/1997 2719 9/17/1997

2515 6/6/1997 2639 7/26/1997 2720 10/23/1997

2543 6/6/1997 2640 9/8/1997 2721 10/23/1997

2549 6/6/1997 2645 7/23/1997 2722 10/23/1997

2550 6/25/1997 2646 7/23/1997 2731 9/17/1997

2551 6/25/1997 2647 7/23/1997 2732 9/17/1997

2552 6/25/1997 2649 7/23/1997 2733 9/17/1997

2553 6/25/1997 2653 10/8/1997 2734 9/17/1997

2557 7/21/1997 2654 9/21/1997 2735 10/6/1997

2558 7/21/1997 2655 9/21/1997 2737 10/6/1997

2559 7/21/1997 2656 9/21/1997 2739 10/6/1997

2560 7/21/1997 2657 8/19/1997 2741 10/6/1997

2569 12/18/1997 2658 8/19/1997 2744 9/11/1997

2748 10/23/1997 2842 2/25/1998 2904 1/7/1998

2749 10/23/1997 2843 2/25/1998 2905 1/7/1998

2750 10/23/1997 2845 2/12/1998 2906 1/7/1998

2751 9/11/1997 2846 2/12/1998 2907 12/18/1997

2753 9/11/1997 2847 2/12/1998 2908 12/18/1997

2754 10/23/1997 2848 2/12/1998 2909 1/3/1998

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 16 OF 22)

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: July 22, 1993

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ALERT ALERT
TABLE B.2: 65C27409-27

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

2755 10/9/1997 2849 2/20/1998 2910 12/18/1997

2757 10/9/1997 2850 2/20/1998 2911 1/15/1998

2758 9/11/1997 2851 2/20/1998 2912 1/15/1998

2761 10/9/1997 2856 2/20/1998 2913 1/15/1998

2765 10/9/1997 2857 1/22/1998 2914 1/15/1998

2771 11/1/1997 2858 1/22/1998 2919 12/22/1997

2773 11/24/1997 2861 2/18/1998 2920 12/22/1997

2774 11/1/1997 2862 2/18/1998 2921 12/22/1997

2775 11/1/1997 2863 2/18/1998 2922 12/22/1997

2802 1/7/1998 2864 2/18/1998 2927 1/12/1998

2803 1/7/1998 2869 1/22/1998 2928 1/12/1998

2804 1/7/1998 2870 12/11/1997 2929 1/12/1998

2805 2/12/1998 2871 12/19/1997 2930 1/12/1998

2806 3/18/1998 2872 2/1/1998 2937 2/24/1998

2808 2/12/1998 2879 12/19/1997 2946 2/24/1998

2810 6/7/1998 2881 12/19/1997 2947 2/1/1998

2811 2/12/1998 2883 12/11/1997 2948 2/1/1998

2816 2/2/1998 2884 3/6/1998 2949 2/1/1998

2817 2/2/1998 2885 12/11/1997 2950 1/12/1998

2818 2/2/1998 2886 12/11/1997 2951 1/12/1998

2819 2/2/1998 2887 12/9/1997 2952 1/12/1998

2832 1/27/1998 2888 12/9/1997 2953 1/12/1998

2833 1/27/1998 2889 12/9/1997 2959 2/24/1998

2834 1/27/1998 2890 12/9/1997 2987 2/24/1998

2835 1/27/1998 2891 11/25/1997 2988 2/24/1998

2836 1/23/1998 2892 11/25/1997 2989 2/24/1998

2837 1/23/1998 2893 11/25/1997 2990 2/24/1998

2838 1/23/1998 2895 11/26/1997 2991 3/6/1998

2839 6/7/1998 2896 11/26/1997 2992 3/6/1998

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 17 OF 22)

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TABLE B.2: 65C27409-27

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

2840 1/23/1998 2902 2/24/1998 2993 3/6/1998

2841 2/25/1998 2903 1/7/1998 2997 7/1/1998

2998 7/1/1998 3102 3/23/1998 B3221 1/18/1999

2999 7/1/1998 3103 3/23/1998 B3222 1/18/1999

3000 7/1/1998 3120 4/15/1998 B3224 3/12/1999

3006 8/4/1998 3121 4/15/1998 B3233 4/26/1999

3008 8/4/1998 3122 4/15/1998 B3234 3/9/1999

3009 8/4/1998 3123 4/15/1998 B3235 2/20/1999

3010 8/21/1998 3128 7/2/1998 B3237 3/9/1999

3016 9/29/1998 3130 7/2/1998 B3239 2/20/1999

3017 9/11/1998 3131 7/2/1998 B3244 4/28/1999

3018 9/11/1998 3132 8/21/1998 B3245 4/20/1999

3019 9/29/1998 3133 8/23/1998 B3246 4/28/1999

3020 10/28/1998 3134 7/28/1998 B3248 3/18/1999

3021 10/28/1998 3135 7/28/1998 B3249 3/18/1999

3022 10/28/1998 3140 9/7/1998 B3254 4/5/1999

3023 11/30/1998 3141 7/10/1998 B3256 7/1/1999

3032 8/28/1998 3152 5/28/1998 B3257 7/1/1999

3033 8/28/1998 3153 5/28/1998 B3258 7/1/1999

3034 8/28/1998 3154 5/28/1998 B3265 6/17/1999

3035 8/28/1998 3155 5/28/1998 B3267 7/12/1999

3036 8/23/1998 3166 4/21/1998 B3268 6/3/1999

3040 8/3/1998 3167 4/21/1998 B3269 6/2/1999

3041 8/3/1998 3168 4/21/1998 B3270 6/2/1999

3042 8/3/1998 3169 4/21/1998 B3271 6/14/1999

3043 8/3/1998 3170 11/17/1998 B3272 4/20/1999

3048 9/7/1998 3171 11/17/1998 B3275 4/27/1999

3049 9/7/1998 3172 6/6/1998 B3276 4/28/1999

3050 8/29/1998 3172 11/17/1998 B3278 4/27/1999

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 18 OF 22)

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TABLE B.2: 65C27409-27

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

3051 9/7/1998 3173 11/17/1998 B3279 4/20/1999

3060 3/18/1998 3174 5/6/1998 B3280 3/26/1999

3061 3/18/1998 3175 6/6/1998 B3282 3/16/1999

3066 3/21/1998 3176 5/6/1998 B3284 4/13/1999

3067 3/21/1998 3187 5/20/1998 B3289 3/26/1999

3068 6/7/1998 3193 11/30/1998 B3291 4/28/1999

3069 3/21/1998 B3207 4/5/1999 B3304 6/19/1999

3076 6/7/1998 B3208 3/16/1999 B3305 6/16/1999

3100 6/7/1998 B3219 1/18/1999 B3306 6/16/1999

3101 6/7/1998 B3220 1/18/1999 B3307 6/14/1999

B3312 7/28/1999 B3531 10/17/2003 B3617 12/16/2003

B3316 4/26/1999 B3532 4/5/2003 B3618 1/6/2004

B3385 10/12/2003 B3533 4/8/2003 B3620 10/14/2003

B3412 12/18/2000 B3535 4/8/2003 B3622 10/29/2003

B3413 12/18/2000 B3540 7/8/2003 B3625 10/29/2003

B3414 12/18/2000 B3545 5/20/2003 B3628 3/12/2004

B3415 11/21/2000 B3547 6/11/2003 B3629 11/12/2003

B3416 12/18/2000 B3548 9/17/2003 B3631 10/17/2003

B3445 4/20/2001 B3549 7/16/2003 B3632 12/16/2003

B3446 6/20/2001 B3551 7/16/2003 B3633 10/17/2003

B3448 6/19/2001 B3553 6/24/2003 B3639 10/13/2003

B3451 4/20/2001 B3554 9/4/2003 B3640 10/18/2003

B3455 4/20/2001 B3556 5/20/2003 B3641 10/9/2003

B3467 8/19/2001 B3558 6/11/2003 B3643 10/27/2003

B3470 8/19/2001 B3559 5/1/2003 B3658 1/17/2004

B3473 1/12/2002 B3562 7/8/2003 B3659 1/31/2004

B3475 11/7/2001 B3575 11/2/2003 B3660 1/31/2004

B3476 10/30/2001 B3576 12/21/2003 B3661 1/29/2004

B3480 11/7/2001 B3577 11/2/2003 B3676 1/31/2004

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 19 OF 22)

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TABLE B.2: 65C27409-27

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

B3481 1/12/2002 B3578 10/9/2003 B3677 1/16/2004

B3484 11/6/2001 B3580 10/9/2003 B3679 1/16/2004

B3486 11/28/2001 B3585 10/17/2003 B3680 1/6/2004

B3487 1/12/2002 B3586 12/16/2003 B3681 2/7/2004

B3488 9/20/2001 B3587 2/29/2004 B3682 1/23/2004

B3493 1/13/2003 B3588 1/14/2004 B3684 6/22/2004

B3495 1/10/2003 B3589 12/19/2003 B3686 1/23/2004

B3499 4/1/2002 B3594 10/29/2003 B3687 1/16/2004

B3500 1/12/2002 B3595 12/23/2003 B3690 1/31/2004

B3502 3/13/2002 B3596 1/16/2004 B3692 1/23/2004

B3503 4/2/2002 B3597 1/28/2004 B3713 4/2/2004

B3517 1/31/2003 B3606 1/29/2004 B3714 2/29/2004

B3518 1/31/2003 B3607 1/16/2004 B3715 2/25/2004

B3519 1/31/2003 B3608 1/29/2004 B3716 2/25/2004

B3522 6/18/2003 B3609 12/16/2003 B3717 2/25/2004

B3524 8/21/2003 B3614 1/6/2004 B3718 2/25/2004

B3526 7/16/2003 B3615 12/17/2003 B3719 2/8/2004

B3527 7/16/2003 B3616 12/16/2003 B3720 2/25/2004

B3721 2/20/2004 B3776 4/28/2004 B3877 7/25/2004

B3722 1/31/2004 B3777 4/28/2004 B3878 6/26/2004

B3723 1/31/2004 B3780 3/29/2004 B3879 4/28/2004

B3724 1/17/2004 B3781 3/29/2004 B3882 7/24/2004

B3725 3/29/2004 B3782 5/20/2004 B3883 7/24/2004

B3726 5/3/2004 B3783 3/2/2004 B3884 6/11/2004

B3727 1/17/2004 B3784 2/29/2004 B3885 6/2/2004

B3728 2/27/2004 B3785 2/29/2004 B3886 6/21/2004

B3729 4/2/2004 B3786 3/26/2004 B3887 6/11/2004

B3730 3/29/2004 B3787 5/20/2004 B3888 6/21/2004

B3731 4/2/2004 B3788 5/20/2004 B3901 9/14/2004

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 20 OF 22)

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TABLE B.2: 65C27409-27

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

B3732 9/11/2004 B3789 2/29/2004 B3905 9/14/2004

B3733 4/28/2004 B3790 6/22/2004 B3910 8/21/2004

B3734 8/3/2004 B3799 7/24/2004 B3912 6/23/2004

B3735 3/29/2004 B3807 9/7/2004 B3913 8/21/2004

B3736 3/10/2004 B3809 4/28/2004 B3914 7/30/2004

B3745 2/29/2004 B3810 8/21/2004 B3915 8/14/2004

B3746 1/19/2004 B3814 3/29/2004 B3917 9/11/2004

B3747 2/19/2004 B3815 6/8/2004 B3918 7/31/2004

B3748 3/10/2004 B3816 4/30/2004 B3919 8/27/2004

B3749 2/19/2004 B3836 6/11/2004 B3921 8/5/2004

B3750 2/25/2004 B3837 5/7/2004 B3922 7/31/2004

B3751 2/29/2004 B3838 4/28/2004 B3923 8/14/2004

B3752 2/20/2004 B3839 6/22/2004 B3924 8/14/2004

B3761 5/20/2004 B3847 6/11/2004 B3925 9/11/2004

B3762 4/13/2004 B3848 6/10/2004 B3926 10/9/2004

B3763 3/29/2004 B3849 6/10/2004 B3927 9/14/2004

B3764 4/28/2004 B3850 6/2/2004 B3928 7/31/2004

B3765 3/29/2004 B3851 5/15/2004 B3929 9/14/2004

B3766 5/3/2004 B3852 4/30/2004 B3930 6/22/2004

B3767 3/29/2004 B3870 4/28/2004 B3931 6/21/2004

B3768 4/28/2004 B3871 6/30/2004 B3933 7/25/2004

B3769 4/28/2004 B3872 4/28/2004 B3934 6/2/2004

B3770 6/10/2004 B3873 5/3/2004 B3936 9/7/2004

B3772 5/25/2004 B3874 4/30/2004 B3938 10/9/2004

B3773 7/30/2004 B3875 6/26/2004 B3939 9/22/2004

B3775 8/21/2004 B3876 5/20/2004 B3941 10/12/2004

B3942 10/12/2004 B4013 9/14/2004 B4091 9/7/2004

B3945 10/12/2004 B4015 8/29/2004 B4092 9/7/2004

B3946 10/12/2004 B4016 9/11/2004 B4093 10/12/2004

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 21 OF 22)

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TABLE B.2: 65C27409-27

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

Date of ManufactureSerial

Number

B3962 10/12/2004 B4017 9/15/2004 B4094 10/12/2004

B3969 10/12/2004 B4019 8/14/2004 B4098 10/12/2004

B3994 8/28/2004 B4031 6/22/2004 B4100 10/12/2004

B3995 9/22/2004 B4036 8/27/2004 B4128 11/3/2004

B3996 10/9/2004 B4037 9/13/2004

B3997 10/9/2004 B4038 9/11/2004

B3998 9/13/2004 B4039 9/11/2004

B3999 10/9/2004 B4044 9/11/2004

B4000 9/22/2004 B4045 10/9/2004

B4001 9/13/2004 B4048 9/11/2004

B4002 7/30/2004 B4049 9/15/2004

B4003 5/27/2004 B4050 9/11/2004

B4007 6/21/2004 B4051 9/13/2004

B4009 7/25/2004 B4087 8/21/2004

B4010 9/14/2004 B4088 9/11/2004

B4011 9/14/2004 B4089 8/29/2004

B4012 9/11/2004 B4090 8/27/2004

Appendix B: CARRIAGE MANUFACTURED DATES

(SHEET 22 OF 22)

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