Commercial 

Airplanes 747

Service Bulletin

ALERT

Number: 747-53A2605

Original Issue: October 08, 2009

Revision 1: May 27, 2010

ATA System: 5312

SUBJECT: FUSELAGE - Center Section - Tension Ties and Frames - Modification and Inspection

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

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ECCN: 9E991

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Copyright © 2009 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Unpublished Work - All Rights Reserved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

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7.0
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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 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

B. Concurrent Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

C. Reason . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

D. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

E. Compliance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

F. Approval . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

G. Manpower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24

H. Weight and Balance Changes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32

I. Electrical Load Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32

J. References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32

1. Existing Data: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32

2. Data supplied with this Service Bulletin: . . . . . . . . . . . . . . . . . . . . . . . . . . . 32

3. Installation Drawings Used in the Preparation of this Service Bulletin: . . . . . . . . . . . 36

K. Publications Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 36

L. Interchangeability and Intermixability of Parts . . . . . . . . . . . . . . . . . . . . . . . . . . . 36

2. MATERIAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37

A. Material - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37

B. Industry Support Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38

C. Parts Necessary For Each Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38

1. Kits/Parts: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38

2. Parts and Materials Supplied by the Operator: . . . . . . . . . . . . . . . . . . . . . . . 145

3. Parts Modified and Reidentified: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 145

4. Parts Removed and Not Replaced: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 145

D. Parts Necessary to Change Spares . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 145

E. Special Tooling - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 145

F. Special Tooling Necessary to do this Service Bulletin . . . . . . . . . . . . . . . . . . . . . . 146

3. ACCOMPLISHMENT INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 147

A. GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 147

B. WORK INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 148

APPENDIX A: TENSION TIE DISCONNECTION METHODS . . . . . . . . . . . . . . . . . . . . . . . 157

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BLANK PAGE
Commercial 

Airplanes 747

Service Bulletin

ALERT

Revision Transmittal Sheet Number: 747-53A2605

Original Issue: October 08, 2009

Revision 1: May 27, 2010

ATA System: 5312

SUBJECT: FUSELAGE - Center Section - Tension Ties and Frames - Modification and Inspection

This revision includes all pages of the service bulletin.

COMPLIANCE INFORMATION RELATED TO THIS REVISION

No more work is necessary on airplanes changed in accordance with the original issue of this service bulletin.

More airplanes were added to the service bulletin effectivity. Airplanes RR561 and RR566 were added to Group

8.

REASON FOR REVISION

This revision is sent to add more airplanes to the service bulletin effectivity and add Appendix A to give information

on methods for disconnecting tension ties.

These sections were changed:

1. In Paragraph 1.A., Effectivity, added airplanes RR561 and RR566 to Group 8.

2. In Paragraph 1.C., Reason, and Paragraph 1.D., Description, added revision information.

3. In Paragraph 1.J.2, Data Supplied with this Service Bulletin, updated drawing list. Drawing number,

142U0101#DL Revision B, is sent with this revision of the service bulletin.

4. In Paragraph 2.A., Material - Price and Availability, updated pricing of the kits.

5. Appendix A was added to give information on methods for disconnecting tension ties.

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.

REVISION HISTORY

Original Issue: October 08, 2009

Revision 1: May 27, 2010

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BLANK PAGE
Commercial 

Airplanes 747

Service Bulletin

ALERT

Summary Number: 747-53A2605

Original Issue: October 08, 2009

Revision 1: May 27, 2010

ATA System: 5312

SUBJECT: FUSELAGE - Center Section - Tension Ties and Frames - Modification and Inspection

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 gives instructions for modification of upper deck tension ties and adjacent frame structure

on non stretched upper deck (Non-SUD) airplanes. The tension ties have been determined to be structure that

is susceptible to Widespread Fatigue Damage (WFD). WFD can cause tension ties to become severed or

disconnected from the frames. Severed or disconnected Tension Ties and/or Frames at multiple locations could

result in rapid in-flight decompression.

For more information about WFD, refer to Boeing Service Letter 747-SL-53-088B.

Service Bulletin 747-53A2502 recommends initial and repeat inspection of Non-SUD airplane tension ties from

body station (STA) 760 to STA 940. Service Bulletin 747-53-2502 was issued to address multiple reports of

cracks found in tension ties and adjacent frame structure. Accomplishment of the modification in this service

bulletin terminates the repeat inspection requirement of Service Bulletin 747-53-2502.

Federal Aviation Administration (FAA) Airworthiness Directives 2004-07-22 R1 and 2006-01-07 are related to

this service bulletin.

Boeing Service Related Problem (SRP) 747-SRP-53-0200 is related to this service bulletin.

ACTION (PRR 85901-68RS)

Get access to the Frame to Tension Tie joints at STA 720 through STA 940 or STA 840 through STA 940

depending on the group. At each station, disconnect and remove a section of the tension tie between the frame

and approximate Buttock Line (BL) 36. For each frame, remove a specified section of the frame above and

below the tension tie attach point. After the existing frame and tension tie structure has been removed and

discarded, install new frame and tension tie structure. Do the modification on both sides of the airplane.

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After modification, do initial and repeat inspections of the unmodified areas of the tension ties at the compliance

time specified in paragraph 1.E., Compliance. Also, if the airplane will be operated past the post-modification

inspection compliance time specified in paragraph 1.E., then contact Boeing for post-modification inspection

instructions and do initial and repeat inspections of the modified tension tie and frame structure.

EFFECTIVITY

747-100, 747-100B, 747-200B, 747-200C, 747-200F, 747-400F, and 747SR airplanes. Refer to paragraph 1.A.,

Effectivity, for the list of affected airplanes.

COMPLIANCE

The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to this service

bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service bulletin

mandatory.

Federal Aviation Administration (FAA) Airworthiness Directives 2004-07-22 R1 and 2006-01-07 are related to

this service bulletin.

Refer to paragraph 1.E, Compliance.

INDUSTRY SUPPORT INFORMATION

Boeing warranty remedies are not available for the modification and inspections given in this service bulletin.

MANPOWER

Refer to paragraph 1.G., Manpower.

MATERIAL INFORMATION

Boeing Supplied Kits/Parts.

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

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BLANK PAGE
Commercial 

Airplanes 747

Service Bulletin

ALERT

Number: 747-53A2605

Original Issue: October 08, 2009

Revision 1: May 27, 2010

ATA System: 5312

SUBJECT: FUSELAGE - Center Section - Tension Ties and Frames - Modification and Inspection

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

This service bulletin is for the airplanes shown below. Refer to PRR 85901-68RS for data about

this change.

Refer to Service Bulletin Index Document D6-30300 Part 3 for Airplane Variable Number, Line

Number, and Serial Number data.

NOTE: This service bulletin is for the airplanes identified below.

GROUP CONFIGURATION DESCRIPTION

747-100/-200B airplanes. Contains 142U0102-233 Tension Tie Mod.

Kit.

1 -

2 - 747-100 airplanes. Contains 142U0102-233 Tension Tie Mod. Kit.

3 - 747-100/-200B airplanes.

4 - 747-100/-100B/-200B and 747SR airplanes.

5 - 747-200B and 747SR airplanes.

6 - 747-100/-100B/-200B and 747SR airplanes.

7 - 747-200B and 747SR airplanes.

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GROUP CONFIGURATION DESCRIPTION

8 - 747-200F Freighter airplanes.

9 - 747-200C airplanes.

10 - 747-400F Freighter airplanes.

11 - 747-100 airplanes. Contains 142U0102-233 Tension Tie Mod. Kit.

12 - 747-100 airplanes.

13 - 747-100 airplanes. Contains 142U0102-232 Tension Tie Mod. Kit.

14 - 747-100 airplanes. Contains 142U0102-232 Tension Tie Mod. Kit.

15 - 747-100 airplanes. Contains 142U0102-232 Tension Tie Mod. Kit.

Airplane Models:

747-100, 747-100B, 747-200B, 747-200C, 747-200F, 747-400F, 747SR

Variable Number Group

RA001 - RA025 13

RA026 11

RA027 - RA028 1

RA029 11

RA030 - RA032 1

RA033 11

RA034 1

RA101 - RA103 15

RA104 - RA110 14

RA111 - RA112 11

RA113 - RA115 2

RA161 - RA162 11

RA163 12

RA164 3

RA201 - RA203 14

RA216 1

RA217 3

RA245 1

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Variable Number Group

RA246 4

RA251 - RA254 13

RA255 1

RA256 - RA266 3

RA301 - RA303 13

RA304 - RA306 1

RA307 - RA313 3

RA314 - RA317 4

RA318 6

RA351 - RA355 13

RA356 - RA360 1

RA369 - RA371 1

RA372 - RA373 3

RA401 - RA403 14

RA404 - RA412 2

RA413 3

RA414 - RA418 4

RA501 - RA502 1

RA521 - RA523 13

RA524 12

RA525 - RA528 3

RA532 - RA534 1

RA535 - RA543 3

RA544 - RA548 4

RA551 - RA552 13

RA559 - RA560 1

RA561 3

RA581 - RA582 1

RA585 3

RA601 - RA602 1

RA631 1

RA632 11

RA633 1

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Variable Number Group

RA634 - RA635 12

RA651 - RA652 1

RA671 - RA674 1

RA675 - RA677 3

RA701 1

RA702 3

RA721 - RA722 1

RA723 - RA724 3

RA725 - RA731 4

RA741 - RA743 1

RA744 - RA745 3

RA749 - RA750 4

RA761 - RA762 1

RA781 1

RA782 - RA784 4

RA901 - RA902 15

RA903 - RA904 14

RA905 - RA909 2

RA910 - RA916 11

RB001 - RB016 4

RB041 15

RB042 14

RB043 15

RB044 2

RB071 - RB075 3

RB101 - RB102 1

RB411 - RB413 6

RB421 4

RB601 - RB603 4

RB604 - RB605 5

RB606 4

RB607 5

RB681 - RB695 6

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Variable Number Group

RB696 7

RB697 6

RB711 6

RB721 - RB723 4

RB741 - RB748 4

RD001 - RD004 4

RD021 - RD022 4

RD041 5

RD042 4

RD043 - RD044 5

RD045 - RD054 4

RD055 5

RD056 - RD059 4

RD071 - RD072 4

RD081 4

RD082 - RD083 7

RD091 - RD092 6

RD101 - RD104 4

RD121 4

RD122 - RD127 6

RD131 - RD141 6

RD142 7

RD143 6

RD144 7

RD166 - RD167 6

RD171 - RD172 4

RD181 - RD183 6

RD201 - RD204 6

RD221 - RD224 6

RD225 7

RD226 6

RD227 7

RD231 - RD232 6

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Variable Number Group

RD233 - RD235 7

RD241 - RD243 6

RD251 - RD262 4

RD271 - RD272 6

RD291 - RD292 6

RD301 - RD302 7

RD311 6

RD351 - RD357 6

RD358 7

RD361 - RD366 7

RD411 - RD412 7

RD413 - RD414 6

RD421 - RD426 6

RD431 - RD435 4

RD441 - RD442 7

RD451 - RD456 6

RD461 7

RD471 - RD475 6

RD513 - RD519 6

RD531 - RD533 6

RD551 5

RD561 6

RD571 4

RD581 - RD583 7

RD591 - RD593 6

RD621 4

RD622 - RD623 5

RD641 - RD643 7

RD644 - RD645 6

RD646 7

RD647 - RD649 6

RD651 - RD659 6

RD661 6

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Variable Number Group

RD671 4

RD681 - RD682 6

RD691 7

RD692 6

RD701 - RD702 6

RD741 - RD742 6

RD751 6

RD752 7

RD753 - RD755 6

RD761 6

RD771 - RD775 6

RD781 - RD783 6

RD791 - RD792 6

RE001 6

RJ131 - RJ133 9

RJ151 - RJ152 9

RJ301 - RJ303 9

RJ321 - RJ322 9

RJ331 - RJ333 9

RL401 - RL403 10

RL411 - RL436 10

RL451 - RL456 10

RL461 - RL462 10

RL471 - RL481 10

RL491 - RL492 10

RL501 - RL502 10

RL511 - RL516 10

RL521 - RL522 10

RL531 - RL534 10

RL551 10

RL561 - RL568 10

RL571 - RL572 10

RL576 - RL577 10

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Variable Number Group

RL579 10

RL581 - RL586 10

RL651 - RL655 10

RL671 - RL675 10

RL681 - RL684 10

RL751 - RL752 10

RM851 - RM859 10

RM861 - RM863 10

RM871 - RM899 10

RM901 - RM906 10

RM911 10

RR001 - RR005 8

RR021 - RR025 8

RR031 8

RR201 - RR206 8

RR221 - RR226 8

RR261 - RR267 8

RR301 - RR310 8

RR331 - RR332 8

RR336 8

RR341 - RR345 8

RR361 - RR362 8

RR421 - RR422 8

RR431 - RR432 8

RR441 - RR442 8

RR451 8

RR501 - RR504 8

RR521 - RR522 8

RR526 8

RR531 8

RR551 - RR556 8

RR561 8

RR566 8

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Variable Number Group

RR701 10

RR721 - RR724 10

RR746 - RR748 10

RR851 - RR856 10

RR861 - RR862 10

RR951 - RR952 10

2. Spares Affected

None.

B. Concurrent Requirements

None.

C. Reason

This service bulletin gives instructions for modification of upper deck tension ties and adjacent frame

structure on non stretched upper deck (Non-SUD) airplanes. The tension ties have been determined

to be structure that is susceptible to Widespread Fatigue Damage (WFD). WFD can cause tension ties

to become severed or disconnected from the frames. Severed or disconnected Tension Ties and/or

Frames at multiple locations could result in rapid in-flight decompression.

For more information about WFD, refer to Boeing Service Letter 747-SL-53-088B.

Service Bulletin 747-53-2502 recommends initial and repeat inspection of Non-SUD airplane tension

ties from body station (STA) 760 to STA 940. Service Bulletin 747-53-2502 was issued to address

multiple reports of cracks found in tension ties and adjacent frame structure. Accomplishment of the

modification in this service bulletin terminates the repeat inspection requirement of Service Bulletin

747-53-2502.

Federal Aviation Administration (FAA) Airworthiness Directives 2004-07-22 R1 and 2006-01-07 are

related to this service bulletin.

Revision 1 is sent to add more airplanes to the service bulletin effectivity and add Appendix A to give

information on methods for disconnecting tension ties.

Boeing Service Related Problem (SRP) 747-SRP-53-0200 is related to this service bulletin.

D. Description

Get access to the Frame to Tension Tie joints at STA 720 through STA 940 or STA 840 through STA

940 depending on the group. At each station, disconnect and remove a section of the tension tie

between the frame and approximate Buttock Line (BL) 36. For each frame, remove a specified section

of the frame above and below the tension tie attach point. After the existing frame and tension tie

structure has been removed and discarded, install new frame and tension tie structure. Do the

modification on both sides of the airplane.

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BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
After modification, do initial and repeat inspections of the unmodified areas of the tension ties at the

compliance time specified in paragraph 1.E., Compliance. Also, if the airplane will be operated past

the post-modification inspection compliance time specified in paragraph 1.E., then contact Boeing for

post-modification inspection instructions and do initial and repeat inspections of the modified tension

tie and frame structure.

Revision 1 - No more work is necessary on airplanes changed in accordance with the original issue of

this service bulletin.

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

Group 1, 3:

Affected Maintenance Zones

Model Zone

747-100, 747-200B 233, 234, 243, 244

Group 2, 11-15:

Affected Maintenance Zones

Model Zone

747-100 233, 234, 243, 244

Group 4, 6:

Affected Maintenance Zones

Model Zone

747-100, 747-100B, 747-200B, 233, 234, 243, 244

747SR

Group 5, 7:

Affected Maintenance Zones

Model Zone

747-200B, 747SR 233, 234, 243, 244

Group 8:

Affected Maintenance Zones

Model Zone

747-200F 233, 234, 243, 244

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BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 9:

Affected Maintenance Zones

Model Zone

747-200C 233, 234, 243, 244

Group 10:

Affected Maintenance Zones

Model Zone

747-400F 233, 234, 243, 244

E. Compliance

The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to

this service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this

service bulletin mandatory.

Federal Aviation Administration (FAA) Airworthiness Directives 2004-07-22 R1 and 2006-01-07 are

related to this service bulletin.

Table 1: Tension Tie and Frame - Modification and Inspection

Repeat Interval

(Not to Exceed)

Compliance Time (Whichever

Occurs Later)

Condition Action

Within 3,000 -

flight cycles after the original

issue date of

this service bulletin.

Before 30,000

total flight cycles.

Do the tension tie and

frame structure modification in accordance with

the Accomplishment Instructions, paragraph

3.B., Part 1.

All airplanes.

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Table 1: Tension Tie and Frame - Modification and Inspection

Repeat Interval

(Not to Exceed)

Compliance Time (Whichever

Occurs Later)

Condition Action

Before 6,000 flight cycles after -

modification in accordance with

the Accomplishment Instructions,

paragraph 3.B., Part 1.

Do a detailed inspection

of the unmodified areas

of the tension ties for

cracks, in accordance

with the Accomplishment

Instructions, paragraph

3.B., Part 2.

Modification has been done

in accordance with the Accomplishment Instructions,

paragraph 3.B., Part 1 of

this service bulletin. (a)

Before 20,000 flight cycles after -

modification in accordance with

the Accomplishment Instructions,

paragraph 3.B., Part 1.

Do an inspection of the

modified areas of the

tension tie and frame

structure in accordance

with the Accomplishment

Instructions, paragraph

3.B., Part 3. Contact

Boeing for post-modification inspection instructions.

Repeat the detailed in- - 6,000 flight cycles.

spection of the unmodified areas of the tension

ties for cracks, in accordance with the Accomplishment Instructions,

paragraph 3.B., Part 2.

No crack found during inspection in accordance

with the Accomplishment

Instructions, paragraph

3.B., Part 2.

Contact Boeing for repair Before further flight. -

instructions, and do the

repair.

Any crack found during inspection in accordance

with the Accomplishment

Instructions, paragraph

3.B., Part 2. (a) Repeat the detailed in- - 6,000 flight cycles.

spection of the unmodified areas of the tension

ties for cracks, in accordance with the Accomplishment Instructions,

paragraph 3.B., Part 2.

Contact Boeing for

repeat interval.

Repeat the inspection of -

the modified areas of the

tension tie and frame

structure in accordance

with the Accomplishment

Instructions, paragraph

3.B., Part 3. Contact

Boeing for post-modification inspection instructions.

No discrepancy found during post-modification inspection in accordance

with the Accomplishment

Instructions, paragraph

3.B., Part 3.

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ALERT ALERT
Table 1: Tension Tie and Frame - Modification and Inspection

Repeat Interval

(Not to Exceed)

Compliance Time (Whichever

Occurs Later)

Condition Action

Contact Boeing for repair Before further flight. -

instructions, and do the

repair.

Any discrepancy found

during post-modification inspection in accordance

with the Accomplishment

Instructions, paragraph

3.B., Part 3. (a)

Contact Boeing for

repeat interval.

Repeat the inspection of -

the modified areas of the

tension tie and frame

structure in accordance

with the Accomplishment

Instructions, paragraph

3.B., Part 3. Contact

Boeing for post-modification inspection instructions.

(a) Do all of the actions specified for this condition.

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.

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.

This service bulletin has been approved by the FAA. In addition, the Manager of the Seattle Aircraft

Certification Office (ACO) approves the accomplishment of the modification, post modification inspection

and corrective action with the corresponding compliance times specified in Table 1, under paragraph

1.E.,"Compliance," of Service Bulletin 747-53A2605, Revision 1, as an alternative method of compliance

(AMOC) to the inspections and corrective action required by paragraphs (h), (i), and (j) of AD 2004-07-22

R1, for the inspection of Structural Significant Item (SSI) F-19A of the Supplemental Structural Inspection

Document (SSID) D6-35022, Revision G. This AMOC only applies to the areas inspected by this service

bulletin. When this service bulletin specifies contacting Boeing for repair instructions, the repair

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

of AD 2004-07-22 R1 that are not specifically referenced in this paragraph remain fully applicable and

must be complied with.

In addition, the Manager of the Seattle ACO approves the accomplishment of the modification,

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

specified in Table 1, under paragraph 1.E., "Compliance," of Service Bulletin 747-53A2605 Revision

1 as an AMOC to the inspections, corrective and related investigative actions with the corresponding

compliance times specified under paragraph 1.E., "Compliance," of Service Bulletin 747-53-2502, dated

April 21, 2005, required by paragraph (f) of AD 2006-01-07. When this service bulletin specifies

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contacting Boeing for repair instructions, the repair instructions must be approved by the FAA in

accordance with paragraph (g) of the AD. All provisions of AD 2006-01-07 that are not specifically

referenced in this paragraph, including but not limited to repeat inspections in accordance with paragraph

(f) until the modification in accordance with Service Bulletin 747-53A2605 Revision 1 is installed, remain

fully applicable and must be complied with.

In addition, the Manager of the Seattle ACO approves the accomplishment of the modification,

inspections and repair with the corresponding compliance times specified in Table 1, under paragraph

1.E., "Compliance," of Service Bulletin 747-53A2605 Revision 1 as an AMOC to the inspections, repair

and modification with the corresponding compliance times required by paragraphs A. and B. of AD

84-19-01. When this service bulletin specifies contacting Boeing for repair instructions, the repair

instructions must be approved by the FAA in accordance with paragraph C. of the AD. All provisions

of AD 84-19-01 that are not specifically referenced in this paragraph, including but not limited to repeat

inspections in accordance with paragraphs A. and B. until the modification in accordance with Service

Bulletin 747-53A2605 Revision 1 is installed, remain fully applicable and must be complied with.

In addition, the Manager of the Seattle ACO approves the accomplishment of the modification,

inspections and repair with the corresponding compliance times specified in Table 1, under paragraph

1.E., "Compliance," of Service Bulletin 747-53A2605 Revision 1 as an AMOC to the inspections, repair

and modification with the corresponding compliance times required by paragraphs (a) and (b) of AD

94-13-06. When this service bulletin specifies contacting Boeing for repair instructions, the repair

instructions must he approved by the FAA in accordance with paragraph (c) of the AD. All provisions

of AD 94-13-06 that are not specifically referenced in this paragraph, including but not limited to repeat

inspections in accordance with paragraphs (a) and (b) until the modification in accordance with Service

Bulletin 747-53A2605 Revision 1 is installed, remain fully applicable and must be complied with.

G. Manpower

The table below shows an estimate of the task hours necessary to do the modification for each airplane.

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

task 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 inspect the work

— Time to cure the materials

— Time to make the parts

— Time to find the tools.

Task Number of Persons Task Hours Elapsed Hours

Access 4 24.00 6.00

Restoration 4 30.00 7.50

TOTAL FOR EACH AIRPLANE 54.00 13.50

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Group 1-5, 8-9, 11-15:

Shear Panel Removal/Installation

Task Number of Persons Task Hours Elapsed Hours

Remove 2 10.00 5.00

Install 2 10.00 5.00

TOTAL FOR EACH AIRPLANE 20.00 10.00

Group 6-7:

Shear Panel Removal/Installation

Task Number of Persons Task Hours Elapsed Hours

Remove 2 10.00 5.00

Install 2 10.00 5.00

TOTAL FOR EACH AIRPLANE 20.00 10.00

Group 10:

Shear Panel Removal/Installation

Task Number of Persons Task Hours Elapsed Hours

Remove 2 10.00 5.00

Install 2 10.00 5.00

TOTAL FOR EACH AIRPLANE 20.00 10.00

Group 10:

STA 720 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 7.00 3.50

Install 2 7.00 3.50

TOTAL FOR EACH AIRPLANE 14.00 7.00

Group 10:

STA 740 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 7.00 3.50

Install 2 7.00 3.50

TOTAL FOR EACH AIRPLANE 14.00 7.00

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Group 1, 13:

STA 760 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 7.50 3.75

Install 2 7.50 3.75

TOTAL FOR EACH AIRPLANE 15.00 7.50

Group 2-3, 14:

STA 760 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 6.50 3.25

Install 2 6.50 3.25

TOTAL FOR EACH AIRPLANE 13.00 6.50

Group 10:

STA 760 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 6.00 3.00

Install 2 6.00 3.00

TOTAL FOR EACH AIRPLANE 12.00 6.00

Group 1-2, 8, 11, 13-15:

STA 780 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 7.00 3.50

Install 2 7.00 3.50

TOTAL FOR EACH AIRPLANE 14.00 7.00

Group 3, 12:

STA 780 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 6.50 3.25

Install 2 6.50 3.25

TOTAL FOR EACH AIRPLANE 13.00 6.50

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Group 10:

STA 780 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 5.00 2.50

Install 2 5.00 2.50

TOTAL FOR EACH AIRPLANE 10.00 5.00

Group 1-5, 8-9, 11-15:

STA 800 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 6.50 3.25

Install 2 6.50 3.25

TOTAL FOR EACH AIRPLANE 13.00 6.50

Group 10:

STA 800 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 5.00 2.50

Install 2 5.00 2.50

TOTAL FOR EACH AIRPLANE 10.00 5.00

Group 1-5, 9, 11-15:

STA 820 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 26.00 13.00

Install 2 26.00 13.00

TOTAL FOR EACH AIRPLANE 52.00 26.00

Group 8, 10:

STA 820 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 27.50 13.75

Install 2 27.50 13.75

TOTAL FOR EACH AIRPLANE 55.00 27.50

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Group 1-5, 9-15:

STA 840 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 24.00 12.00

Install 2 24.00 12.00

TOTAL FOR EACH AIRPLANE 48.00 24.00

Group 6-7:

STA 840 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 23.50 11.75

Install 2 23.50 11.75

TOTAL FOR EACH AIRPLANE 47.00 23.50

Group 8:

STA 840 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 26.00 13.00

Install 2 26.00 13.00

TOTAL FOR EACH AIRPLANE 52.00 26.00

Group 1-5, 8, 11-15:

STA 860 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 27.50 13.75

Install 2 27.50 13.75

TOTAL FOR EACH AIRPLANE 55.00 27.50

Group 6-7:

STA 860 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 26.00 13.00

Install 2 26.00 13.00

TOTAL FOR EACH AIRPLANE 52.00 26.00

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Group 9:

STA 860 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 27.00 13.50

Install 2 27.00 13.50

TOTAL FOR EACH AIRPLANE 54.00 27.00

Group 10:

STA 860 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 25.50 12.75

Install 2 25.50 12.75

TOTAL FOR EACH AIRPLANE 51.00 25.50

Group 1-9, 11-15:

STA 880 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 28.00 14.00

Install 2 28.00 14.00

TOTAL FOR EACH AIRPLANE 56.00 28.00

Group 10:

STA 880 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 25.00 12.50

Install 2 25.00 12.50

TOTAL FOR EACH AIRPLANE 50.00 25.00

Group 1-4, 6, 11-15:

STA 900 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 26.00 13.00

Install 2 26.00 13.00

TOTAL FOR EACH AIRPLANE 52.00 26.00

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Group 5, 7:

STA 900 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 24.50 12.25

Install 2 24.50 12.25

TOTAL FOR EACH AIRPLANE 49.00 24.50

Group 8:

STA 900 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 25.50 12.75

Install 2 25.50 12.75

TOTAL FOR EACH AIRPLANE 51.00 25.50

Group 9-10:

STA 900 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 24.00 12.00

Install 2 24.00 12.00

TOTAL FOR EACH AIRPLANE 48.00 24.00

STA 920 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 25.00 12.50

Install 2 25.00 12.50

TOTAL FOR EACH AIRPLANE 50.00 25.00

Group 1-2, 11:

STA 940 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 28.50 14.25

Install 2 28.50 14.25

TOTAL FOR EACH AIRPLANE 57.00 28.50

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Group 3-4, 6, 12:

STA 940 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 29.00 14.50

Install 2 29.00 14.50

TOTAL FOR EACH AIRPLANE 58.00 29.00

Group 5, 7, 9:

STA 940 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 32.00 16.00

Install 2 32.00 16.00

TOTAL FOR EACH AIRPLANE 64.00 32.00

Group 8:

STA 940 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 28.00 14.00

Install 2 28.00 14.00

TOTAL FOR EACH AIRPLANE 56.00 28.00

Group 10:

STA 940 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 32.50 16.25

Install 2 32.50 16.25

TOTAL FOR EACH AIRPLANE 65.00 32.50

Group 13-15:

STA 940 Left ,Right Side, and Center Modification

Task Number of Persons Task Hours Elapsed Hours

Remove 2 26.00 13.00

Install 2 26.00 13.00

TOTAL FOR EACH AIRPLANE 52.00 26.00

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H. Weight and Balance Changes

Weight and Balance Changes data will be included in a future revision of this service bulletin.

I. Electrical Load Data

Not changed.

J. References

1. Existing Data:

a. 747-100/200/300 Aircraft Maintenance Manual (AMM) 24-22-00, 25-21-04, 25-22-01, and

25-25-01.

b. 747-400 Aircraft Maintenance Manual (AMM) 24-22-00, 25-21-04, 25-22-01, and 25-25-01.

c. 747-100/200/300 Structural Repair Manual (SRM) 51-10-01, 51-30-09, and 53-11-21.

d. 747-400F Structural Repair Manual (SRM) 51-10-02, 51-40-09, 53-20-07.

e. 747 Non-Destructive Testing (NDT) Manual, Part 6, Chapter 51-00-00, Figure 1, 11, or 16.

f. Federal Aviation Administration (FAA) Airworthiness Directives 2004-07-22 R1 and 2006-01-07.

g. Boeing Service Related Problem (SRP) 747-53-0200.

h. Boeing Service Letter 747-SL-53-088B.

i. Standard Overhaul Practices Manual (SOPM) 20-41-01 and 20-41-05.

j. Engineering Change Memo PRR-85901-68RS.

2. Data supplied with this Service Bulletin:

a. Drawings:

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Drawing No Title Sheet DCN/REV ADCN

TOP KIT - FRAME AND TENSION TIE 1 - -

MODIFICATION, STA 720 - STA 940

142U0100

10 - -

11 - -

12 - -

13 - -

14 - -

2 - -

3 - -

4 - -

5 - -

6 - -

7 - -

9 - -

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Drawing No Title Sheet DCN/REV ADCN

KIT - FRAME MODIFICATION, STA 820 - 1 - -

STA 940

142U0101

10 - -

11 - -

12 - -

13 - -

14 - -

15 - -

16 - -

17 - -

18 - -

19 - -

2 - -

20 - -

21 - -

22 - -

23 - -

24 - -

3 - -

4 - -

5 - -

6 - -

7 - -

8 - -

9 - -

KIT - FRAME MODIFICATION, STA 820 - PSDL B -

STA 940

142U0101#DL

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Drawing No Title Sheet DCN/REV ADCN

KIT - TENSION TIE MODIFICATION, STA 1 - -

720 - STA 940

142U0102

10 A -

11 A -

12 A -

13 A -

14 A -

15 A -

16 A -

17 A -

18 A -

19 A -

2 A -

20 A -

21 A -

22 A -

23 A -

24 A -

25 A -

26 A -

27 A -

28 A -

29 A -

3 A -

30 A -

31 A -

32 A -

33 - -

34 - -

35 - -

4 A -

5 A -

6 A -

7 A -

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Drawing No Title Sheet DCN/REV ADCN

8 - A

9 A -

KIT - TENSION TIE MODIFICATION, STA PSDL - -

720 - STA 940

142U0102#DL

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

None.

K. Publications Affected

1. Publications

Publication Chapter-Section

747-100/200/300 Structural Repair Manual 53-11

747-400F Structural Repair Manual 53-20

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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2. MATERIAL INFORMATION

A. Material - Price and Availability

Boeing can supply the kits shown in Paragraph 2.C., Parts Necessary For Each Airplane, as shown

below. If there is a limit to the quantity (QTY) of available kits, a supply sequence is given by Spares.

More kits become available as shown in the Reorder Lead Time (ROLT). ROLT is calculated from the

date Boeing gets the purchase order.

Unit Price thru December 31, 2011ROLT

(Weeks)

Kit Number Name Date QTY

TOP KIT - TENSION TIE AND 8/26/09 1 57 $635,004.00

FRAME MODIFICATION

142U0100-1001

TOP KIT - TENSION TIE AND (a) - 57 634,277.00

FRAME MODIFICATION

142U0100-1002

TOP KIT - TENSION TIE AND 8/28/09 1 57 655,323.00

FRAME MODIFICATION

142U0100-1003

TOP KIT - TENSION TIE AND 8/31/09 1 57 623,027.00

FRAME MODIFICATION

142U0100-1004

TOP KIT - TENSION TIE AND 9/03/09 1 57 623,719.00

FRAME MODIFICATION

142U0100-1005

TOP KIT - TENSION TIE AND 9/04/09 1 57 535,131.00

FRAME MODIFICATION

142U0100-1006

TOP KIT - TENSION TIE AND 9/08/09 1 57 535,823.00

FRAME MODIFICATION

142U0100-1007

TOP KIT - TENSION TIE AND 9/10/09 1 57 645,067.00

FRAME MODIFICATION

142U0100-1008

TOP KIT - TENSION TIE AND (a) - 57 623,537.00

FRAME MODIFICATION

142U0100-1009

TOP KIT - TENSION TIE AND (a) - 57 658,423.00

FRAME MODIFICATION

142U0100-1010

TOP KIT - TENSION TIE AND 9/11/09 1 57 618,575.00

FRAME MODIFICATION

142U0100-1011

TOP KIT - TENSION TIE AND (a) - 57 639,219.00

FRAME MODIFICATION

142U0100-1012

TOP KIT - TENSION TIE AND (a) - 57 18,657.00

FRAME MODIFICATION

142U0100-2001

TOP KIT - TENSION TIE AND (a) - 57 21,288.00

FRAME MODIFICATION

142U0100-2002

(a) Contact Boeing Spares for price and availability.

NOTE: Due to the limited number of kits available and the long ROLT, Boeing recommends that

operators submit purchase orders 18 months in advance of performing the modification.

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The kits are subject to the terms and conditions of the Boeing standard purchase order acknowledgment.

After the Unit Price date, new price and ROLT data is applicable. Prices are in United States dollars.

Terms: Net 30 days.

Reference this service bulletin and submit your purchase order by one of the methods that

follow:

1. Order on-line via ATA Spec 2000 or Boeing Part Page

2. Fax to (206) 662-7145

3. Spares Customer Support - MC 36-65 Boeing Spares Department P.O. Box 3707 Seattle,

Washington 98124-2207 USA

B. Industry Support Information

Boeing warranty remedies are not available for the inspection or modification procedures given in this

service bulletin.

C. Parts Necessary For Each Airplane

1. Kits/Parts:

NOTE: The top kits shown in the table that follows and the items shown in Paragraph 2.C.2.,

Parts and Materials Supplied by the Operator, are necessary for each airplane.

To get the kits/parts shown below, refer to Paragraph 2.A., Material - Price and Availability.

Group(s) Top Kit

1 142U0100-1001 and 142U0100-2002

2 142U0100-1002 and 142U0100-2002

3 142U0100-1003

4 142U0100-1004

5 142U0100-1005

6 142U0100-1006

7 142U0100-1007

8 142U0100-1008

9 142U0100-1009

10 142U0100-1010

11 142U0100-1011 and 142U0100-2002

12 142U0100-1012

13 142U0100-1001 and 142U0100-2001

14 142U0100-1002 and 142U0100-2001

15 142U0100-1011 and 142U0100-2001

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

38 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1, 13:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1001

KIT - FRAME MODIFICATION, STA 820142U0101-101 1

KIT - FRAME MODIFICATION, STA 840142U0101-104 1

KIT - FRAME MODIFICATION, STA 860142U0101-107 1

KIT - FRAME MODIFICATION, STA 880142U0101-111 1

KIT - FRAME MODIFICATION, STA 900142U0101-113 1

KIT - FRAME MODIFICATION, STA 920142U0101-117 1

KIT - FRAME MODIFICATION, STA 940142U0101-121 1

KIT - TENSION TIE MODIFICATION, STA 760142U0102-203 1

KIT - TENSION TIE MODIFICATION, STA 780142U0102-207 1

KIT - TENSION TIE MODIFICATION, STA 800142U0102-210 1

KIT - TENSION TIE MODIFICATION, STA 820142U0102-212 1

KIT - TENSION TIE MODIFICATION, STA 840142U0102-214 1

KIT - TENSION TIE MODIFICATION, STA 860142U0102-217 1

KIT - TENSION TIE MODIFICATION, STA 880142U0102-220 1

KIT - TENSION TIE MODIFICATION, STA 900142U0102-222 1

KIT - TENSION TIE MODIFICATION, STA 920142U0102-225 1

KIT - SHEAR PANEL INSTL

- TENSION TIE MODIFICATION

142U0102-301 1

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

39 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 2, 14:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1002

KIT - FRAME MODIFICATION, STA 820142U0101-101 1

KIT - FRAME MODIFICATION, STA 840142U0101-104 1

KIT - FRAME MODIFICATION, STA 860142U0101-107 1

KIT - FRAME MODIFICATION, STA 880142U0101-111 1

KIT - FRAME MODIFICATION, STA 900142U0101-113 1

KIT - FRAME MODIFICATION, STA 920142U0101-117 1

KIT - FRAME MODIFICATION, STA 940142U0101-121 1

KIT - TENSION TIE MODIFICATION, STA 760142U0102-204 1

KIT - TENSION TIE MODIFICATION, STA 780142U0102-207 1

KIT - TENSION TIE MODIFICATION, STA 800142U0102-210 1

KIT - TENSION TIE MODIFICATION, STA 820142U0102-212 1

KIT - TENSION TIE MODIFICATION, STA 840142U0102-214 1

KIT - TENSION TIE MODIFICATION, STA 860142U0102-217 1

KIT - TENSION TIE MODIFICATION, STA 880142U0102-220 1

KIT - TENSION TIE MODIFICATION, STA 900142U0102-222 1

KIT - TENSION TIE MODIFICATION, STA 920142U0102-225 1

KIT - SHEAR PANEL INSTL

- TENSION TIE MODIFICATION

142U0102-301 1

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

40 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 3:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1003

KIT - FRAME MODIFICATION, STA 820142U0101-101 1

KIT - FRAME MODIFICATION, STA 840142U0101-104 1

KIT - FRAME MODIFICATION, STA 860142U0101-107 1

KIT - FRAME MODIFICATION, STA 880142U0101-111 1

KIT - FRAME MODIFICATION, STA 900142U0101-113 1

KIT - FRAME MODIFICATION, STA 920142U0101-117 1

KIT - FRAME MODIFICATION, STA 940142U0101-121 1

KIT - TENSION TIE MODIFICATION, STA 760142U0102-205 1

KIT - TENSION TIE MODIFICATION, STA 780142U0102-208 1

KIT - TENSION TIE MODIFICATION, STA 800142U0102-210 1

KIT - TENSION TIE MODIFICATION, STA 820142U0102-212 1

KIT - TENSION TIE MODIFICATION, STA 840142U0102-214 1

KIT - TENSION TIE MODIFICATION, STA 860142U0102-217 1

KIT - TENSION TIE MODIFICATION, STA 880142U0102-220 1

KIT - TENSION TIE MODIFICATION, STA 900142U0102-222 1

KIT - TENSION TIE MODIFICATION, STA 920142U0102-225 1

KIT - TENSION TIE MODIFICATION, STA 940142U0102-229 1

KIT - SHEAR PANEL INSTL

- TENSION TIE MODIFICATION

142U0102-301 1

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

41 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 4:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1004

KIT - FRAME MODIFICATION, STA 820142U0101-101 1

KIT - FRAME MODIFICATION, STA 840142U0101-104 1

KIT - FRAME MODIFICATION, STA 860142U0101-107 1

KIT - FRAME MODIFICATION, STA 880142U0101-111 1

KIT - FRAME MODIFICATION, STA 900142U0101-113 1

KIT - FRAME MODIFICATION, STA 920142U0101-117 1

KIT - FRAME MODIFICATION, STA 940142U0101-121 1

KIT - TENSION TIE MODIFICATION, STA 800142U0102-210 1

KIT - TENSION TIE MODIFICATION, STA 820142U0102-212 1

KIT - TENSION TIE MODIFICATION, STA 840142U0102-214 1

KIT - TENSION TIE MODIFICATION, STA 860142U0102-217 1

KIT - TENSION TIE MODIFICATION, STA 880142U0102-220 1

KIT - TENSION TIE MODIFICATION, STA 900142U0102-222 1

KIT - TENSION TIE MODIFICATION, STA 920142U0102-225 1

KIT - TENSION TIE MODIFICATION, STA 940142U0102-229 1

KIT - SHEAR PANEL INSTL

- TENSION TIE MODIFICATION

142U0102-301 1

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

42 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 5:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1005

KIT - FRAME MODIFICATION, STA 820142U0101-101 1

KIT - FRAME MODIFICATION, STA 840142U0101-104 1

KIT - FRAME MODIFICATION, STA 860142U0101-107 1

KIT - FRAME MODIFICATION, STA 880142U0101-111 1

KIT - FRAME MODIFICATION, STA 900142U0101-125 1

KIT - FRAME MODIFICATION, STA 920142U0101-126 1

KIT - FRAME MODIFICATION, STA 940142U0101-127 1

KIT - TENSION TIE MODIFICATION, STA 800142U0102-210 1

KIT - TENSION TIE MODIFICATION, STA 820142U0102-212 1

KIT - TENSION TIE MODIFICATION, STA 840142U0102-214 1

KIT - TENSION TIE MODIFICATION, STA 860142U0102-217 1

KIT - TENSION TIE MODIFICATION, STA 880142U0102-220 1

KIT - TENSION TIE MODIFICATION, STA 900142U0102-223 1

KIT - TENSION TIE MODIFICATION, STA 920142U0102-226 1

KIT - TENSION TIE MODIFICATION, STA 940142U0102-230 1

KIT - SHEAR PANEL INSTL

- TENSION TIE MODIFICATION

142U0102-301 1

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

43 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 6:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1006

KIT - FRAME MODIFICATION, STA 840142U0101-104 1

KIT - FRAME MODIFICATION, STA 860142U0101-107 1

KIT - FRAME MODIFICATION, STA 880142U0101-111 1

KIT - FRAME MODIFICATION, STA 900142U0101-113 1

KIT - FRAME MODIFICATION, STA 920142U0101-117 1

KIT - FRAME MODIFICATION, STA 940142U0101-121 1

KIT - TENSION TIE MODIFICATION, STA 840142U0102-215 1

KIT - TENSION TIE MODIFICATION, STA 860142U0102-218 1

KIT - TENSION TIE MODIFICATION, STA 880142U0102-220 1

KIT - TENSION TIE MODIFICATION, STA 900142U0102-222 1

KIT - TENSION TIE MODIFICATION, STA 920142U0102-225 1

KIT - TENSION TIE MODIFICATION, STA 940142U0102-229 1

KIT - SHEAR PANEL INSTL

- TENSION TIE MODIFICATION

142U0102-302 1

Group 7:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1007

KIT - FRAME MODIFICATION, STA 840142U0101-104 1

KIT - FRAME MODIFICATION, STA 860142U0101-107 1

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

44 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 7:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1007

KIT - FRAME MODIFICATION, STA 880142U0101-111 1

KIT - FRAME MODIFICATION, STA 900142U0101-125 1

KIT - FRAME MODIFICATION, STA 920142U0101-126 1

KIT - FRAME MODIFICATION, STA 940142U0101-127 1

KIT - TENSION TIE MODIFICATION, STA 840142U0102-215 1

KIT - TENSION TIE MODIFICATION, STA 860142U0102-218 1

KIT - TENSION TIE MODIFICATION, STA 880142U0102-220 1

KIT - TENSION TIE MODIFICATION, STA 900142U0102-223 1

KIT - TENSION TIE MODIFICATION, STA 920142U0102-226 1

KIT - TENSION TIE MODIFICATION, STA 940142U0102-230 1

KIT - SHEAR PANEL INSTL

- TENSION TIE MODIFICATION

142U0102-302 1

Group 8:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1008

KIT - FRAME MODIFICATION, STA 820142U0101-102 1

KIT - FRAME MODIFICATION, STA 840142U0101-105 1

KIT - FRAME MODIFICATION, STA 860142U0101-108 1

KIT - FRAME MODIFICATION, STA 880142U0101-111 1

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

45 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 8:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1008

KIT - FRAME MODIFICATION, STA 900142U0101-114 1

KIT - FRAME MODIFICATION, STA 920142U0101-117 1

KIT - FRAME MODIFICATION, STA 940142U0101-121 1

KIT - TENSION TIE MODIFICATION, STA 780142U0102-207 1

KIT - TENSION TIE MODIFICATION, STA 800142U0102-210 1

KIT - TENSION TIE MODIFICATION, STA 820142U0102-212 1

KIT - TENSION TIE MODIFICATION, STA 840142U0102-214 1

KIT - TENSION TIE MODIFICATION, STA 860142U0102-217 1

KIT - TENSION TIE MODIFICATION, STA 880142U0102-220 1

KIT - TENSION TIE MODIFICATION, STA 900142U0102-222 1

KIT - TENSION TIE MODIFICATION, STA 920142U0102-225 1

KIT - TENSION TIE MODIFICATION, STA 940142U0102-228 1

KIT - SHEAR PANEL INSTL

- TENSION TIE MODIFICATION

142U0102-301 1

Group 9:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1009

KIT - FRAME MODIFICATION, STA 820142U0101-101 1

KIT - FRAME MODIFICATION, STA 840142U0101-104 1

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

46 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 9:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1009

KIT - FRAME MODIFICATION, STA 860142U0101-109 1

KIT - FRAME MODIFICATION, STA 880142U0101-111 1

KIT - FRAME MODIFICATION, STA 900142U0101-115 1

KIT - FRAME MODIFICATION, STA 920142U0101-119 1

KIT - FRAME MODIFICATION, STA 940142U0101-123 1

KIT - TENSION TIE MODIFICATION, STA 800142U0102-210 1

KIT - TENSION TIE MODIFICATION, STA 820142U0102-212 1

KIT - TENSION TIE MODIFICATION, STA 840142U0102-214 1

KIT - TENSION TIE MODIFICATION, STA 860142U0102-217 1

KIT - TENSION TIE MODIFICATION, STA 880142U0102-220 1

KIT - TENSION TIE MODIFICATION, STA 900142U0102-223 1

KIT - TENSION TIE MODIFICATION, STA 920142U0102-226 1

KIT - TENSION TIE MODIFICATION, STA 940142U0102-230 1

KIT - SHEAR PANEL INSTL

- TENSION TIE MODIFICATION

142U0102-301 1

Group 10:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1010

KIT - FRAME MODIFICATION, STA 820142U0101-103 1

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

47 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1010

KIT - FRAME MODIFICATION, STA 840142U0101-106 1

KIT - FRAME MODIFICATION, STA 860142U0101-110 1

KIT - FRAME MODIFICATION, STA 880142U0101-112 1

KIT - FRAME MODIFICATION, STA 900142U0101-116 1

KIT - FRAME MODIFICATION, STA 920142U0101-120 1

KIT - FRAME MODIFICATION, STA 940142U0101-124 1

KIT - TENSION TIE MODIFICATION, STA 720142U0102-201 1

KIT - TENSION TIE MODIFICATION, STA 740142U0102-202 1

KIT - TENSION TIE MODIFICATION, STA 760142U0102-206 1

KIT - TENSION TIE MODIFICATION, STA 780142U0102-209 1

KIT - TENSION TIE MODIFICATION, STA 800142U0102-211 1

KIT - TENSION TIE MODIFICATION, STA 820142U0102-213 1

KIT - TENSION TIE MODIFICATION, STA 840142U0102-216 1

KIT - TENSION TIE MODIFICATION, STA 860142U0102-219 1

KIT - TENSION TIE MODIFICATION, STA 880142U0102-221 1

KIT - TENSION TIE MODIFICATION, STA 900142U0102-224 1

KIT - TENSION TIE MODIFICATION, STA 920142U0102-227 1

KIT - TENSION TIE MODIFICATION, STA 940142U0102-231 1

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

48 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1010

KIT - SHEAR PANEL INSTL - TENSION TIE MODIFICATION142U0102-303 1

Group 11, 15:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1011

KIT - FRAME MODIFICATION, STA 820142U0101-101 1

KIT - FRAME MODIFICATION, STA 840142U0101-104 1

KIT - FRAME MODIFICATION, STA 860142U0101-107 1

KIT - FRAME MODIFICATION, STA 880142U0101-111 1

KIT - FRAME MODIFICATION, STA 900142U0101-113 1

KIT - FRAME MODIFICATION, STA 920142U0101-117 1

KIT - FRAME MODIFICATION, STA 940142U0101-121 1

KIT - TENSION TIE MODIFICATION, STA 780142U0102-207 1

KIT - TENSION TIE MODIFICATION, STA 800142U0102-210 1

KIT - TENSION TIE MODIFICATION, STA 820142U0102-212 1

KIT - TENSION TIE MODIFICATION, STA 840142U0102-214 1

KIT - TENSION TIE MODIFICATION, STA 860142U0102-217 1

KIT - TENSION TIE MODIFICATION, STA 880142U0102-220 1

KIT - TENSION TIE MODIFICATION, STA 900142U0102-222 1

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

49 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 11, 15:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1011

KIT - TENSION TIE MODIFICATION, STA 920142U0102-225 1

KIT - SHEAR PANEL INSTL - TENSION TIE MODIFICATION142U0102-301 1

Group 12:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1012

KIT - FRAME MODIFICATION, STA 820142U0101-101 1

KIT - FRAME MODIFICATION, STA 840142U0101-104 1

KIT - FRAME MODIFICATION, STA 860142U0101-107 1

KIT - FRAME MODIFICATION, STA 880142U0101-111 1

KIT - FRAME MODIFICATION, STA 900142U0101-113 1

KIT - FRAME MODIFICATION, STA 920142U0101-117 1

KIT - FRAME MODIFICATION, STA 940142U0101-121 1

KIT - TENSION TIE MODIFICATION, STA 780142U0102-208 1

KIT - TENSION TIE MODIFICATION, STA 800142U0102-210 1

KIT - TENSION TIE MODIFICATION, STA 820142U0102-212 1

KIT - TENSION TIE MODIFICATION, STA 840142U0102-214 1

KIT - TENSION TIE MODIFICATION, STA 860142U0102-217 1

KIT - TENSION TIE MODIFICATION, STA 880142U0102-220 1

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

50 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 12:

Kit 142U0100

New Part Number QTY Name Existing Part Number Notes

-1012

KIT - TENSION TIE MODIFICATION, STA 900142U0102-222 1

KIT - TENSION TIE MODIFICATION, STA 920142U0102-225 1

KIT - TENSION TIE MODIFICATION, STA 940142U0102-229 1

KIT - SHEAR PANEL INSTL - TENSION TIE MODIFICATION142U0102-301 1

Group 13-15:

Kit 142U0100

Existing Part Notes

Number

New Part Number QTY Name

-2001

KIT - TENSION TIE MODIFICATION,

STA 940

142U0102-232 1

Group 1-2, 11:

Kit 142U0100

Existing Part Notes

Number

New Part Number QTY Name

-2002

KIT - TENSION TIE MODIFICATION, STA 940142U0102-233 1

Group 1-5, 9, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-101

142U0106-11 2 STRAP

142U0106-19 2 STRAP

142U0106-21 2 STRAP

142U0107-23 1 FRAME SEGMENT

142U0107-24 1 FRAME SEGMENT

142U0107-27 1 TRIPLER

142U0107-28 1 TRIPLER

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

51 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-5, 9, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-101

142U0107-29 1 DOUBLER

142U0107-30 1 DOUBLER

142U0107-55 2 STIFFENER

142U0108-11 2 STRINGER CLIP TEE

142U0108-12 2 STRINGER CLIP TEE

142U0108-47 1 SHEAR TIE TEE, S-11 TO S-12

142U0108-48 1 SHEAR TIE TEE, S-11 TO S-12

142U0108-49 2 SHEAR TIE TEE, S-10A TO S-11

142U0108-50 2 SHEAR TIE TEE, S-10 TO S-10A

142U0108-51 2 SHEAR TIE TEE, S-9 TO S-10

142U0108-53 2 SHEAR TIE, S-8 TO S-9

142U0108-54 2 CHORD SPLICE - UPPER

142U0108-55 1 CHORD SEGMENT

142U0108-56 1 CHORD SEGMENT

142U0108-115 2 CHORD SPLICE - LOWER

142U0108-117 1 STIFFENER

142U0108-118 1 STIFFENER

142U0108-119 2 STIFFENER

144U0064-6 2 STRINGER CLIP TEE

144U0064-7 2 STRINGER CLIP TEE

144U0064-8 8 STRINGER CLIP TEE

144U0064-9 8 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D018B0F0 2 BRACKET, ANGLE

BACB30NW6K5Y 88 BOLT, 100 DEG HEX DR

BACB30NW6K6X 26 BOLT, 100 DEG HEX DR

BACB30NX6K3 139 BOLT, PROTRUDING HD

BACB30NX6K3X 4 BOLT, PROTRUDING HD

BACB30NX6K3Y 48 BOLT, PROTRUDING HD

BACB30NX6K4 238 BOLT, PROTRUDING HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

52 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-5, 9, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-101

BACB30NX6K4X 31 BOLT, PROTRUDING HD

BACB30NX6K4Y 27 BOLT, PROTRUDING HD

BACB30NX6K5 201 BOLT

BACB30NX6K5X 2 BOLT, PROTRUDING HD

BACB30NX6K5Y 12 BOLT, PROTRUDING HD

BACB30NX6K6 40 BOLT

BACB30NX6K7 46 HI-LOK

BACB30NX6K7X 18 BOLT, PROTRUDING HD

BACB30NX6K8 112 BOLT, PROTRUDING HD

BACB30NX6K8X 13 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACC30AC6 83 COLLAR

BACC30BH6 840 COLLAR

BACC30M6 26 COLLAR

BACC30R6 88 COLLAR

BACF3H05JF008HN 4 RADIUS FILLER

BACF3T01B10-40 8 FILLER, TAPERED

BACN10TL3A12 2 NUT STANDOFF

BACR15BB12AD8C 2 RIVET, UNIVERSAL HD

BACR15BB4AD5C 4 RIVETS

BACR15BB4AD6C 4 RIVET

BACR15BB6AD4C 26 RIVET, UNIVERSAL HD

BACR15BB8AD6C 2 RIVET, UNIVERSAL HD

BACR15GF6D5 26 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R008B035F 4 SHIM, LAMINATED

BACS40R008B038F 4 SHIM, LAMINATED

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

53 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 8:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-102

142U0106-23 2 STRAP

142U0106-25 2 STRAP

142U0106-27 2 STRAP

142U0107-23 1 FRAME SEGMENT

142U0107-24 1 FRAME SEGMENT

142U0107-25 1 DOUBLER

142U0107-26 1 DOUBLER

142U0107-27 1 TRIPLER

142U0107-28 1 TRIPLER

142U0107-55 2 STIFFENER

142U0108-11 4 STRINGER CLIP TEE

142U0108-12 4 STRINGER CLIP TEE

142U0108-47 1 SHEAR TIE TEE, S-11 TO S-12

142U0108-48 1 SHEAR TIE TEE, S-11 TO S-12

142U0108-49 2 SHEAR TIE TEE, S-10A TO S-11

142U0108-50 2 SHEAR TIE TEE, S-10 TO S-10A

142U0108-51 2 SHEAR TIE TEE, S-9 TO S-10

142U0108-53 2 SHEAR TIE, S-8 TO S-9

142U0108-54 2 CHORD SPLICE - UPPER

142U0108-55 1 CHORD SEGMENT

142U0108-56 1 CHORD SEGMENT

142U0108-115 2 CHORD SPLICE - LOWER

142U0108-117 1 STIFFENER

142U0108-118 1 STIFFENER

142U0108-119 2 STIFFENER

144U0064-6 2 STRINGER CLIP TEE

144U0064-7 2 STRINGER CLIP TEE

144U0064-8 8 STRINGER CLIP TEE

144U0064-9 8 STRINGER CLIP TEE

BACB2D016B0F0 2 BRACKET, ANGLE

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

54 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 8:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-102

BACB30NW6K5Y 88 BOLT, 100 DEG HEX DR

BACB30NX6K3 113 BOLT, PROTRUDING HD

BACB30NX6K3X 29 BOLT, PROTRUDING HD

BACB30NX6K3Y 136 BOLT, PROTRUDING HD

BACB30NX6K4 222 BOLT, PROTRUDING HD

BACB30NX6K4X 20 BOLT, PROTRUDING HD

BACB30NX6K4Y 86 BOLT, PROTRUDING HD

BACB30NX6K5 196 BOLT

BACB30NX6K5X 6 BOLT, PROTRUDING HD

BACB30NX6K5Y 22 BOLT, PROTRUDING HD

BACB30NX6K6 40 BOLT

BACB30NX6K6Y 6 BOLT, PROTRUDING HD

BACB30NX6K7 42 HI-LOK

BACB30NX6K7X 24 BOLT, PROTRUDING HD

BACB30NX6K7Y 4 BOLT, PROTRUDING HD

BACB30NX6K8 103 BOLT, PROTRUDING HD

BACB30NX6K8X 6 BOLT, PROTRUDING HD

BACB30NX6K8Y 6 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACC30AC6 262 COLLAR

BACC30BH6 775 COLLAR

BACC30M6 26 COLLAR

BACC30R6 88 COLLAR

BACF3H05JF008HN 2 RADIUS FILLER

BACF3T01B10-40 8 FILLER, TAPERED

BACN10TL3A6 2 SPACER PLATE NUT

BACR15BB12AD8C 2 RIVET, UNIVERSAL HD

BACR15BB4AD5C 4 RIVETS

BACR15BB6AD4C 26 RIVET, UNIVERSAL HD

BACR15BB8AD6C 2 RIVET, UNIVERSAL HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

55 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 8:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-102

BACR15GF6D5 26 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R008B035F 4 SHIM, LAMINATED

BACS40R008B038F 4 SHIM, LAMINATED

Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-103

142U0106-3 2 STRAP

142U0106-27 2 STRAP

142U0106-41 2 STRAP

142U0107-23 1 FRAME SEGMENT

142U0107-24 1 FRAME SEGMENT

142U0107-25 1 DOUBLER

142U0107-26 1 DOUBLER

142U0107-27 1 TRIPLER

142U0107-28 1 TRIPLER

142U0107-55 4 STIFFENER

142U0108-11 4 STRINGER CLIP TEE

142U0108-12 4 STRINGER CLIP TEE

142U0108-47 1 SHEAR TIE TEE, S-11 TO S-12

142U0108-48 1 SHEAR TIE TEE, S-11 TO S-12

142U0108-49 2 SHEAR TIE TEE, S-10A TO S-11

142U0108-50 2 SHEAR TIE TEE, S-10 TO S-10A

142U0108-51 2 SHEAR TIE TEE, S-9 TO S-10

142U0108-52 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-54 2 CHORD SPLICE - UPPER

142U0108-77 1 CHORD SEGMENT

142U0108-78 1 CHORD SEGMENT

142U0108-115 2 CHORD SPLICE - LOWER

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

56 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-103

144U0064-6 10 STRINGER CLIP TEE

144U0064-7 10 STRINGER CLIP TEE

BACB30NW6K6X 26 BOLT, 100 DEG HEX DR

BACB30NW6K6Y 106 BOLT, 100 DEG HEX DR

BACB30NX6K3 189 BOLT, PROTRUDING HD

BACB30NX6K3X 29 BOLT, PROTRUDING HD

BACB30NX6K3Y 29 BOLT, PROTRUDING HD

BACB30NX6K4 209 BOLT, PROTRUDING HD

BACB30NX6K4X 53 BOLT, PROTRUDING HD

BACB30NX6K4Y 62 BOLT, PROTRUDING HD

BACB30NX6K5 196 BOLT

BACB30NX6K5X 20 BOLT, PROTRUDING HD

BACB30NX6K5Y 2 BOLT, PROTRUDING HD

BACB30NX6K6 53 BOLT

BACB30NX6K6Y 6 BOLT, PROTRUDING HD

BACB30NX6K7 42 HI-LOK

BACB30NX6K7X 26 BOLT, PROTRUDING HD

BACB30NX6K8 110 BOLT, PROTRUDING HD

BACB30NX6K8X 13 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACC30AC6 100 COLLAR

BACC30BH6 941 COLLAR

BACC30M6 26 COLLAR

BACC30R6 106 COLLAR

BACF3T01B10-40 8 FILLER, TAPERED

BACR15BB12AD8C 2 RIVET, UNIVERSAL HD

BACR15BB6AD4C 31 RIVET, UNIVERSAL HD

BACR15BB8AD6C 2 RIVET, UNIVERSAL HD

BACR15GF6D5 31 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

57 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-103

BACS40R008B035F 4 SHIM, LAMINATED

BACS40R008B038F 4 SHIM, LAMINATED

Group 1-7, 9, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-104

142U0106-15 2 STRAP

142U0106-29 2 STRAP

142U0106-31 2 STRAP

142U0107-39 4 STIFFENER

142U0107-41 1 FRAME SEGMENT

142U0107-42 1 FRAME SEGMENT

142U0107-43 1 DOUBLER

142U0107-44 1 DOUBLER

142U0107-45 1 TRIPLER

142U0107-46 1 TRIPLER

142U0108-11 2 STRINGER CLIP TEE

142U0108-12 2 STRINGER CLIP TEE

142U0108-79 2 SHEAR TIE, S-8 TO S-9

142U0108-81 2 SHEAR TIE TEE, S-9 TO S-10

SHEAR TIE TEE, S-10 TO S10A / S-10A TO S-11

142U0108-83 4

142U0108-85 1 SHEAR TIE TEE, S-11 TO S-12

142U0108-86 1 SHEAR TIE TEE, S-11 TO S-12

142U0108-87 2 CHORD SPLICE - UPPER

142U0108-89 2 CHORD SPLICE - LOWER

142U0108-91 1 CHORD SEGMENT

142U0108-92 1 CHORD SEGMENT

144U0064-8 10 STRINGER CLIP TEE

144U0064-9 10 STRINGER CLIP TEE

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

58 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-7, 9, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-104

69B41412-3 2 INSULATOR

BACB2D018B0F0 2 BRACKET, ANGLE

BACB30NW6K5Y 88 BOLT, 100 DEG HEX DR

BACB30NW6K6X 27 BOLT, 100 DEG HEX DR

BACB30NW6K7Y 2 BOLT, 100 DEG HEX DR

BACB30NX6K3 110 BOLT, PROTRUDING HD

BACB30NX6K3X 4 BOLT, PROTRUDING HD

BACB30NX6K3Y 29 BOLT, PROTRUDING HD

BACB30NX6K4 216 BOLT, PROTRUDING HD

BACB30NX6K4X 18 BOLT, PROTRUDING HD

BACB30NX6K4Y 20 BOLT, PROTRUDING HD

BACB30NX6K5 190 BOLT

BACB30NX6K5X 2 BOLT, PROTRUDING HD

BACB30NX6K5Y 11 BOLT, PROTRUDING HD

BACB30NX6K6 40 BOLT

BACB30NX6K6X 4 BOLT, PROTRUDING HD

BACB30NX6K7 47 HI-LOK

BACB30NX6K7X 14 BOLT, PROTRUDING HD

BACB30NX6K8 104 BOLT, PROTRUDING HD

BACB30NX6K8X 6 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACC30AC6 60 COLLAR

BACC30BH6 748 COLLAR

BACC30M6 27 COLLAR

BACC30R6 90 COLLAR

BACF3T01B10-40 8 FILLER, TAPERED

BACN10TL3A12 2 NUT STANDOFF

BACR15BB4AD5C 4 RIVETS

BACR15BB4AD6C 4 RIVET

BACR15BB6AD4C 27 RIVET, UNIVERSAL HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

59 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-7, 9, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-104

BACR15GF6D5 27 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R007B034F 4 SHIM,LAMINATED

BACS40R008B038F 4 SHIM, LAMINATED

Group 8:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-105

142U0106-17 2 STRAP

142U0106-29 2 STRAP

142U0106-31 2 STRAP

142U0107-39 4 STIFFENER

142U0107-41 1 FRAME SEGMENT

142U0107-42 1 FRAME SEGMENT

142U0107-45 1 TRIPLER

142U0107-46 1 TRIPLER

142U0107-47 1 DOUBLER

142U0107-48 1 DOUBLER

142U0108-11 4 STRINGER CLIP TEE

142U0108-12 4 STRINGER CLIP TEE

142U0108-79 2 SHEAR TIE, S-8 TO S-9

142U0108-81 2 SHEAR TIE TEE, S-9 TO S-10

SHEAR TIE TEE, S-10 TO S-10A

/ S-10A TO S-11

142U0108-83 4

142U0108-85 1 SHEAR TIE TEE, S-11 TO S-12

142U0108-86 1 SHEAR TIE TEE, S-11 TO S-12

142U0108-87 2 CHORD SPLICE - UPPER

142U0108-89 2 CHORD SPLICE - LOWER

142U0108-91 1 CHORD SEGMENT

142U0108-92 1 CHORD SEGMENT

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

60 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 8:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-105

144U0064-8 10 STRINGER CLIP TEE

144U0064-9 10 STRINGER CLIP TEE

BACB2D017B0G0 2 BRACKET, ANGLE

BACB30NW6K5Y 88 BOLT, 100 DEG HEX DR

BACB30NW6K6X 27 BOLT, 100 DEG HEX DR

BACB30NX6K3 154 BOLT, PROTRUDING HD

BACB30NX6K3X 4 BOLT, PROTRUDING HD

BACB30NX6K3Y 60 BOLT, PROTRUDING HD

BACB30NX6K4 214 BOLT, PROTRUDING HD

BACB30NX6K4X 29 BOLT, PROTRUDING HD

BACB30NX6K4Y 62 BOLT, PROTRUDING HD

BACB30NX6K5 190 BOLT

BACB30NX6K5X 8 BOLT, PROTRUDING HD

BACB30NX6K5Y 11 BOLT, PROTRUDING HD

BACB30NX6K6 36 BOLT

BACB30NX6K6X 4 BOLT, PROTRUDING HD

BACB30NX6K7 47 HI-LOK

BACB30NX6K7X 16 BOLT, PROTRUDING HD

BACB30NX6K8 106 BOLT, PROTRUDING HD

BACB30NX6K8X 6 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACB30YP6K7 2 BOLT, 100 DEG HEX DR

BACC30AC6 132 COLLAR

BACC30BH6 805 COLLAR

BACC30M6 27 COLLAR

BACC30R6 88 COLLAR

BACF3T01B10-40 8 FILLER, TAPERED

BACN10TL3A6 2 SPACER PLATE NUT

BACR15BB4AD5C 4 RIVETS

BACR15BB6AD4C 27 RIVET, UNIVERSAL HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

61 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 8:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-105

BACR15GF6D5 27 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R007B034F 4 SHIM,LAMINATED

BACS40R007B038F 4 SHIM, LAMINATED

Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-106

142U0106-17 2 STRAP

142U0106-29 2 STRAP

142U0106-31 2 STRAP

142U0107-39 4 STIFFENER

142U0107-41 1 FRAME SEGMENT

142U0107-42 1 FRAME SEGMENT

142U0107-43 1 DOUBLER

142U0107-44 1 DOUBLER

142U0107-45 1 TRIPLER

142U0107-46 1 TRIPLER

142U0108-11 2 STRINGER CLIP TEE

142U0108-12 2 STRINGER CLIP TEE

142U0108-81 2 SHEAR TIE TEE, S-9 TO S-10

SHEAR TIE TEE, S-10 TO S-10A

/ S-10A TO S-11

142U0108-83 4

142U0108-85 1 SHEAR TIE TEE, S-11 TO S-12

142U0108-86 1 SHEAR TIE TEE, S-11 TO S-12

142U0108-87 2 CHORD SPLICE - UPPER

142U0108-89 2 CHORD SPLICE - LOWER

142U0108-91 1 CHORD SEGMENT

142U0108-92 1 CHORD SEGMENT

142U0108-93 2 SHEAR TIE TEE, S-8 TO S-9

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

62 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-106

144U0064-8 10 STRINGER CLIP TEE

144U0064-9 10 STRINGER CLIP TEE

BACB2C024E0E0 1 BRACKET, ANGLE

BACB30NW6K5Y 106 BOLT, 100 DEG HEX DR

BACB30NW6K6X 27 BOLT, 100 DEG HEX DR

BACB30NX6K3 105 BOLT, PROTRUDING HD

BACB30NX6K3X 18 BOLT, PROTRUDING HD

BACB30NX6K3Y 33 BOLT, PROTRUDING HD

BACB30NX6K4 202 BOLT, PROTRUDING HD

BACB30NX6K4X 18 BOLT, PROTRUDING HD

BACB30NX6K4Y 31 BOLT, PROTRUDING HD

BACB30NX6K5 193 BOLT

BACB30NX6K5X 4 BOLT, PROTRUDING HD

BACB30NX6K5Y 11 BOLT, PROTRUDING HD

BACB30NX6K6 36 BOLT

BACB30NX6K6X 4 BOLT, PROTRUDING HD

BACB30NX6K7 58 HI-LOK

BACB30NX6K7X 16 BOLT, PROTRUDING HD

BACB30NX6K8 104 BOLT, PROTRUDING HD

BACB30NX6K8X 6 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACC30AC6 75 COLLAR

BACC30BH6 765 COLLAR

BACC30M6 27 COLLAR

BACC30R6 105 COLLAR

BACF3T01B10-40 8 FILLER, TAPERED

BACR15BB6AD4C 27 RIVET, UNIVERSAL HD

BACR15GF6D5 27 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R007B034F 4 SHIM,LAMINATED

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

63 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-106

BACS40R007B038F 4 SHIM, LAMINATED

BACS53B1ES1 2 ELECTRICAL GROUND STUD

Group 1-7, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-107

142U0106-5 2 DOUBLER

142U0106-6 2 STRAP

142U0106-7 2 STRAP

142U0106-8 2 STRAP

142U0106-59 2 FILLER

142U0107-13 1 FRAME SEGMENT

142U0107-14 1 FRAME SEGMENT

142U0107-15 1 DOUBLER

142U0107-16 1 DOUBLER

142U0107-17 1 DOUBLER

142U0107-18 1 DOUBLER

142U0108-13 1 SHEAR TIE, S-7 TO S-8

142U0108-14 1 SHEAR TIE, S-7 TO S-8

142U0108-15 1 SHEAR TIE, S-11 TO S-12

142U0108-16 1 SHEAR TIE, S-11 TO S-12

142U0108-35 4 ANGLE

142U0108-36 4 ANGLE

142U0108-37 2 CHORD SPLICE - UPPER

142U0108-38 2 CHORD SPLICE - LOWER

142U0108-39 1 CHORD SEGMENT

142U0108-40 1 CHORD SEGMENT

142U0108-41 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-42 2 SHEAR TIE TEE, S-9 TO S-10

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

64 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-7, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-107

SHEAR TIE TEE, S-10 TO S-10A

/ S-10A TO S-11

142U0108-43 4

144U0064-6 14 STRINGER CLIP TEE

144U0064-7 14 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D018B0F0 2 BRACKET, ANGLE

BACB30NW6K5Y 117 BOLT, 100 DEG HEX DR

BACB30NW6K6X 14 BOLT, 100 DEG HEX DR

BACB30NX6K10X 2 BOLT, PROTRUDING HD

BACB30NX6K2X 2 BOLT, PROTRUDING HD

BACB30NX6K3 91 BOLT, PROTRUDING HD

BACB30NX6K3X 14 BOLT, PROTRUDING HD

BACB30NX6K3Y 31 BOLT, PROTRUDING HD

BACB30NX6K4 20 BOLT, PROTRUDING HD

BACB30NX6K4X 6 BOLT, PROTRUDING HD

BACB30NX6K5 379 BOLT

BACB30NX6K5X 11 BOLT, PROTRUDING HD

BACB30NX6K5Y 6 BOLT, PROTRUDING HD

BACB30NX6K6 97 BOLT

BACB30NX6K6X 8 BOLT, PROTRUDING HD

BACB30NX6K6Y 2 BOLT, PROTRUDING HD

BACB30NX6K7 31 HI-LOK

BACB30NX6K7X 8 BOLT, PROTRUDING HD

BACB30NX6K8 181 BOLT, PROTRUDING HD

BACB30NX6K8X 29 BOLT, PROTRUDING HD

BACB30NX6K9 14 BOLT

BACB30NX8K3X 6 BOLT, PROTRUDING HD

BACB30NX8K5X 2 BOLT, PROTRUDING HD

BACB30NX8K6X 2 BOLT, PROTRUDING HD

BACB30NX8K8X 4 BOLT, PROTRUDING HD

BACC30AC6 36 COLLAR

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

65 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-7, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-107

BACC30BH6 893 COLLAR

BACC30BH8 14 COLLAR

BACC30M6 131 COLLAR

BACF3T01B10-40 8 FILLER, TAPERED

BACN10TL3A12 2 NUT STANDOFF

BACR15BB4AD5C 4 RIVETS

BACR15BB4AD6C 4 RIVET

BACR15BB6AD4C 31 RIVET, UNIVERSAL HD

BACR15GF6D5 31 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R008A043F 4 SHIM, LAMINATED

BACS40R008B038F 4 SHIM, LAMINATED

Group 8:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-108

142U0106-5 2 DOUBLER

142U0106-6 2 STRAP

142U0106-7 2 STRAP

142U0106-8 2 STRAP

142U0106-60 2 FILLER

142U0107-13 1 FRAME SEGMENT

142U0107-14 1 FRAME SEGMENT

142U0107-15 1 DOUBLER

142U0107-16 1 DOUBLER

142U0107-17 1 DOUBLER

142U0107-18 1 DOUBLER

142U0108-13 1 SHEAR TIE, S-7 TO S-8

142U0108-14 1 SHEAR TIE, S-7 TO S-8

142U0108-15 1 SHEAR TIE, S-11 TO S-12

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

66 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 8:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-108

142U0108-16 1 SHEAR TIE, S-11 TO S-12

142U0108-35 4 ANGLE

142U0108-36 4 ANGLE

142U0108-37 2 CHORD SPLICE - UPPER

142U0108-38 2 CHORD SPLICE - LOWER

142U0108-39 1 CHORD SEGMENT

142U0108-40 1 CHORD SEGMENT

142U0108-41 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-42 2 SHEAR TIE TEE, S-9 TO S-10

SHEAR TIE TEE, S-10 TO S-10A

/ S-10A TO S-11

142U0108-43 4

144U0064-6 14 STRINGER CLIP TEE

144U0064-7 14 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D018B0F0 2 BRACKET, ANGLE

BACB30NW6K5Y 104 BOLT, 100 DEG HEX DR

BACB30NW6K6X 14 BOLT, 100 DEG HEX DR

BACB30NX6K3 102 BOLT, PROTRUDING HD

BACB30NX6K3X 11 BOLT, PROTRUDING HD

BACB30NX6K3Y 31 BOLT, PROTRUDING HD

BACB30NX6K4 22 BOLT, PROTRUDING HD

BACB30NX6K4X 8 BOLT, PROTRUDING HD

BACB30NX6K5 384 BOLT

BACB30NX6K5X 20 BOLT, PROTRUDING HD

BACB30NX6K6 97 BOLT

BACB30NX6K6X 6 BOLT, PROTRUDING HD

BACB30NX6K7 29 HI-LOK

BACB30NX6K7X 8 BOLT, PROTRUDING HD

BACB30NX6K8 179 BOLT, PROTRUDING HD

BACB30NX6K8X 29 BOLT, PROTRUDING HD

BACB30NX6K9 14 BOLT

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

67 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 8:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-108

BACC30AC6 31 COLLAR

BACC30BH6 902 COLLAR

BACC30M6 117 COLLAR

BACF3T01B10-40 8 FILLER, TAPERED

BACN10TL3A12 2 NUT STANDOFF

BACR15BB4AD5C 4 RIVETS

BACR15BB4AD6C 4 RIVET

BACR15BB6AD4C 31 RIVET, UNIVERSAL HD

BACR15GF6D5 31 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R008A043F 4 SHIM, LAMINATED

BACS40R008B038F 4 SHIM, LAMINATED

Group 9:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-109

142U0106-5 2 DOUBLER

142U0106-6 2 STRAP

142U0106-7 2 STRAP

142U0106-8 2 STRAP

142U0107-13 1 FRAME SEGMENT

142U0107-14 1 FRAME SEGMENT

142U0107-15 1 DOUBLER

142U0107-16 1 DOUBLER

142U0107-17 1 DOUBLER

142U0107-18 1 DOUBLER

142U0108-13 1 SHEAR TIE, S-7 TO S-8

142U0108-14 1 SHEAR TIE, S-7 TO S-8

142U0108-15 1 SHEAR TIE, S-11 TO S-12

142U0108-16 1 SHEAR TIE, S-11 TO S-12

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

68 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 9:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-109

142U0108-35 4 ANGLE

142U0108-36 4 ANGLE

142U0108-37 2 CHORD SPLICE - UPPER

142U0108-38 2 CHORD SPLICE - LOWER

142U0108-39 1 CHORD SEGMENT

142U0108-40 1 CHORD SEGMENT

142U0108-41 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-42 2 SHEAR TIE TEE, S-9 TO S-10

SHEAR TIE TEE, S-10 TO S-10A

/ S-10A TO S-11

142U0108-43 4

144U0064-6 14 STRINGER CLIP TEE

144U0064-7 14 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D018B0F0 2 BRACKET, ANGLE

BACB30NW6K5Y 104 BOLT, 100 DEG HEX DR

BACB30NW6K6X 14 BOLT, 100 DEG HEX DR

BACB30NX6K10X 2 BOLT, PROTRUDING HD

BACB30NX6K3 73 BOLT, PROTRUDING HD

BACB30NX6K3X 6 BOLT, PROTRUDING HD

BACB30NX6K3Y 31 BOLT, PROTRUDING HD

BACB30NX6K4 18 BOLT, PROTRUDING HD

BACB30NX6K4X 8 BOLT, PROTRUDING HD

BACB30NX6K5 368 BOLT

BACB30NX6K5X 22 BOLT, PROTRUDING HD

BACB30NX6K5Y 6 BOLT, PROTRUDING HD

BACB30NX6K6 97 BOLT

BACB30NX6K6X 8 BOLT, PROTRUDING HD

BACB30NX6K6Y 2 BOLT, PROTRUDING HD

BACB30NX6K7 31 HI-LOK

BACB30NX6K7X 8 BOLT, PROTRUDING HD

BACB30NX6K8 179 BOLT, PROTRUDING HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

69 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 9:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-109

BACB30NX6K8X 29 BOLT, PROTRUDING HD

BACB30NX6K9 14 BOLT

BACB30NX8K5X 2 BOLT, PROTRUDING HD

BACB30NX8K6X 2 BOLT, PROTRUDING HD

BACB30NX8K8X 4 BOLT, PROTRUDING HD

BACC30AC6 40 COLLAR

BACC30BH6 863 COLLAR

BACC30BH8 8 COLLAR

BACC30M6 117 COLLAR

BACF3T01B10-40 8 FILLER, TAPERED

BACN10TL3A12 2 NUT STANDOFF

BACR15BB4AD5C 4 RIVETS

BACR15BB4AD6C 4 RIVET

BACR15BB6AD4C 31 RIVET, UNIVERSAL HD

BACR15GF6D5 31 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R008A043F 4 SHIM, LAMINATED

BACS40R008B038F 4 SHIM, LAMINATED

Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-110

142U0106-5 2 DOUBLER

142U0106-6 2 STRAP

142U0106-7 2 STRAP

142U0106-8 2 STRAP

142U0106-60 2 FILLER

142U0107-13 1 FRAME SEGMENT

142U0107-14 1 FRAME SEGMENT

142U0107-15 1 DOUBLER

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

70 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-110

142U0107-16 1 DOUBLER

142U0107-17 1 DOUBLER

142U0107-18 1 DOUBLER

142U0108-13 1 SHEAR TIE, S-7 TO S-8

142U0108-14 1 SHEAR TIE, S-7 TO S-8

142U0108-15 1 SHEAR TIE, S-11 TO S-12

142U0108-16 1 SHEAR TIE, S-11 TO S-12

142U0108-35 4 ANGLE

142U0108-36 4 ANGLE

142U0108-37 2 CHORD SPLICE - UPPER

142U0108-38 2 CHORD SPLICE - LOWER

142U0108-39 1 CHORD SEGMENT

142U0108-40 1 CHORD SEGMENT

142U0108-41 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-42 2 SHEAR TIE TEE, S-9 TO S-10

SHEAR TIE TEE, S-10 TO S-10A

/ S-10A TO S-11

142U0108-43 4

144U0064-6 14 STRINGER CLIP TEE

144U0064-7 14 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D018B0F0 2 BRACKET, ANGLE

BACB30NW6K5Y 104 BOLT, 100 DEG HEX DR

BACB30NW6K6X 14 BOLT, 100 DEG HEX DR

BACB30NX6K10X 2 BOLT, PROTRUDING HD

BACB30NX6K3 102 BOLT, PROTRUDING HD

BACB30NX6K3X 11 BOLT, PROTRUDING HD

BACB30NX6K3Y 31 BOLT, PROTRUDING HD

BACB30NX6K4 22 BOLT, PROTRUDING HD

BACB30NX6K4X 8 BOLT, PROTRUDING HD

BACB30NX6K5 381 BOLT

BACB30NX6K5X 20 BOLT, PROTRUDING HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

71 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-110

BACB30NX6K6 95 BOLT

BACB30NX6K6X 8 BOLT, PROTRUDING HD

BACB30NX6K7 29 HI-LOK

BACB30NX6K7X 8 BOLT, PROTRUDING HD

BACB30NX6K8 176 BOLT, PROTRUDING HD

BACB30NX6K8X 29 BOLT, PROTRUDING HD

BACB30NX6K9 6 BOLT

BACC30AC6 31 COLLAR

BACC30BH6 905 COLLAR

BACC30M6 117 COLLAR

BACF3T01B10-40 8 FILLER, TAPERED

BACN10TL3A12 2 NUT STANDOFF

BACR15BB4AD5C 4 RIVETS

BACR15BB4AD6C 4 RIVET

BACR15BB6AD4C 31 RIVET, UNIVERSAL HD

BACR15GF6D5 31 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R008A043F 4 SHIM, LAMINATED

BACS40R008B038F 4 SHIM, LAMINATED

Group 1-9, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-111

142U0106-1 2 SPLICE PLATE

142U0106-3 2 STRAP

142U0106-43 2 STRAP

142U0106-45 2 STRAP

142U0107-1 1 FRAME SEGMENT

142U0107-2 1 FRAME SEGMENT

142U0107-3 1 DOUBLER

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

72 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-9, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-111

142U0107-4 1 DOUBLER

142U0107-5 1 TRIPLER

142U0107-6 1 TRIPLER

142U0107-59 4 STIFFENER

142U0108-1 1 CHORD SEGMENT

142U0108-2 1 CHORD SEGMENT

142U0108-3 2 CHORD SPLICE - UPPER

142U0108-4 2 SHEAR TIE, S-7 TO S-8

142U0108-5 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-6 2 SHEAR TIE TEE, S-9 TO S-10

142U0108-7 2 SHEAR TIE TEE, S-10 TO S-10A

142U0108-8 2 SHEAR TIE TEE, S-10A TO S-11

142U0108-9 1 SHEAR TIE, S-11 TO S-12

142U0108-10 1 SHEAR TIE, S-11 TO S-12

142U0108-11 1 STRINGER CLIP TEE

142U0108-12 1 STRINGER CLIP TEE

144U0064-6 11 STRINGER CLIP TEE

144U0064-7 11 STRINGER CLIP TEE

144U0064-25 1 STRINGER CLIP TEE

144U0064-26 1 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D015B0F0 2 BRACKET, ANGLE

BACB2D018B0F0 2 BRACKET, ANGLE

BACB30NW6K5Y 84 BOLT, 100 DEG HEX DR

BACB30NW6K6X 15 BOLT, 100 DEG HEX DR

BACB30NX6K3 110 BOLT, PROTRUDING HD

BACB30NX6K3X 13 BOLT, PROTRUDING HD

BACB30NX6K3Y 59 BOLT, PROTRUDING HD

BACB30NX6K4 271 BOLT, PROTRUDING HD

BACB30NX6K4X 20 BOLT, PROTRUDING HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

73 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-9, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-111

BACB30NX6K4Y 59 BOLT, PROTRUDING HD

BACB30NX6K5 167 BOLT

BACB30NX6K5X 33 BOLT, PROTRUDING HD

BACB30NX6K5Y 22 BOLT, PROTRUDING HD

BACB30NX6K6 44 BOLT

BACB30NX6K6X 26 BOLT, PROTRUDING HD

BACB30NX6K7 51 HI-LOK

BACB30NX6K7X 22 BOLT, PROTRUDING HD

BACB30NX6K8 112 BOLT, PROTRUDING HD

BACB30NX6K8X 4 BOLT, PROTRUDING HD

BACB30NX6K8Y 6 BOLT, PROTRUDING HD

BACB30NX8K5X 6 BOLT, PROTRUDING HD

BACB30NX8K7 2 BOLT, HEX DRIVE

BACB30NX8K7X 4 BOLT, PROTRUDING HD

BACC30AC6 147 COLLAR

BACC30BH6 873 COLLAR

BACC30BH8 13 COLLAR

BACC30M6 15 COLLAR

BACC30R6 84 COLLAR

BACF3T01B10-40 12 FILLER, TAPERED

BACF3T01E07-10 4 TAPERED FILLER

BACN10TL3A12 2 NUT STANDOFF

BACN10TL3A6 2 SPACER PLATE NUT

BACR15BB4AD5C 8 RIVETS

BACR15BB4AD6C 8 RIVET

BACR15BB6AD4C 27 RIVET, UNIVERSAL HD

BACR15GF6D5 27 RIVET

BACS40R005C005F 10 SHIM,LAMINATED

BACS40R008B037F 4 SHIM - LAMINATED

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

74 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-112

142U0106-1 2 SPLICE PLATE

142U0106-9 2 STRAP

142U0106-45 2 STRAP

142U0106-47 2 STRAP

142U0107-1 1 FRAME SEGMENT

142U0107-2 1 FRAME SEGMENT

142U0107-3 1 DOUBLER

142U0107-4 1 DOUBLER

142U0107-5 1 TRIPLER

142U0107-6 1 TRIPLER

142U0107-59 4 STIFFENER

142U0108-1 1 CHORD SEGMENT

142U0108-2 1 CHORD SEGMENT

142U0108-3 2 CHORD SPLICE - UPPER

142U0108-4 2 SHEAR TIE, S-7 TO S-8

142U0108-5 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-6 2 SHEAR TIE TEE, S-9 TO S-10

142U0108-7 2 SHEAR TIE TEE, S-10 TO S-10A

142U0108-8 2 SHEAR TIE TEE, S-10A TO S-11

142U0108-9 1 SHEAR TIE, S-11 TO S-12

142U0108-10 1 SHEAR TIE, S-11 TO S-12

144U0064-6 10 STRINGER CLIP TEE

144U0064-7 10 STRINGER CLIP TEE

144U0064-8 2 STRINGER CLIP TEE

144U0064-9 2 STRINGER CLIP TEE

BACB2D019C0D0 1 BRACKET, ANGLE

BACB30NW6K5Y 84 BOLT, 100 DEG HEX DR

BACB30NW6K6X 15 BOLT, 100 DEG HEX DR

BACB30NX6K3 64 BOLT, PROTRUDING HD

BACB30NX6K3X 33 BOLT, PROTRUDING HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

75 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-112

BACB30NX6K3Y 40 BOLT, PROTRUDING HD

BACB30NX6K4 255 BOLT, PROTRUDING HD

BACB30NX6K4X 26 BOLT, PROTRUDING HD

BACB30NX6K4Y 37 BOLT, PROTRUDING HD

BACB30NX6K5 165 BOLT

BACB30NX6K5X 29 BOLT, PROTRUDING HD

BACB30NX6K5Y 22 BOLT, PROTRUDING HD

BACB30NX6K6 24 BOLT

BACB30NX6K6X 20 BOLT, PROTRUDING HD

BACB30NX6K7 59 HI-LOK

BACB30NX6K7X 22 BOLT, PROTRUDING HD

BACB30NX6K8 112 BOLT, PROTRUDING HD

BACB30NX6K8X 11 BOLT, PROTRUDING HD

BACC30AC6 99 COLLAR

BACC30BH6 820 COLLAR

BACC30M6 15 COLLAR

BACC30R6 84 COLLAR

BACF3T01B10-40 12 FILLER, TAPERED

BACF3T01E07-10 4 TAPERED FILLER

BACN10TL3A10 1 NUT PLATE

BACR15BB4AD5C 2 RIVETS

BACR15BB6AD4C 27 RIVET, UNIVERSAL HD

BACR15GF6D5 27 RIVET

BACS40R005C005F 10 SHIM,LAMINATED

BACS40R008B037F 4 SHIM - LAMINATED

Group 1-4, 6, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-113

142U0106-33 2 STRAP

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

76 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-4, 6, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-113

142U0106-35 2 STRAP

142U0106-37 2 STRAP

142U0107-49 1 FRAME SEGMENT

142U0107-50 1 FRAME SEGMENT

142U0107-51 1 DOUBLER

142U0107-52 1 DOUBLER

142U0107-53 1 TRIPLER

142U0107-54 1 TRIPLER

142U0108-95 1 CHORD SEGMENT

142U0108-96 1 CHORD SEGMENT

142U0108-97 2 CHORD SPLICE - UPPER

142U0108-99 2 CHORD SPLICE - LOWER

142U0108-101 1 SHEAR TIE, S-7 TO S-8

142U0108-102 1 SHEAR TIE, S-7 TO S-8

142U0108-105 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-107 2 SHEAR TIE TEE, S-9 TO S-10

142U0108-109 2 SHEAR TIE TEE, S-10 TO S-11

142U0108-113 1 SHEAR TIE, S-11 TO S-12

142U0108-114 1 SHEAR TIE, S-11 TO S-12

144U0064-8 10 STRINGER CLIP TEE

144U0064-9 10 STRINGER CLIP TEE

144U0064-25 2 STRINGER CLIP TEE

144U0064-26 2 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D019B0F0 2 BRACKET, ANGLE

BACB30NW6K5Y 106 BOLT, 100 DEG HEX DR

BACB30NW6K8X 29 BOLT, 100 DEG HEX DR

BACB30NX6K3 89 BOLT, PROTRUDING HD

BACB30NX6K3X 6 BOLT, PROTRUDING HD

BACB30NX6K3Y 29 BOLT, PROTRUDING HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

77 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-4, 6, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-113

BACB30NX6K4 291 BOLT, PROTRUDING HD

BACB30NX6K4X 8 BOLT, PROTRUDING HD

BACB30NX6K4Y 29 BOLT, PROTRUDING HD

BACB30NX6K5 236 BOLT

BACB30NX6K5X 2 BOLT, PROTRUDING HD

BACB30NX6K5Y 14 BOLT, PROTRUDING HD

BACB30NX6K6Y 2 BOLT, PROTRUDING HD

BACB30NX6K7 49 HI-LOK

BACB30NX6K7X 11 BOLT, PROTRUDING HD

BACB30NX6K7Y 6 BOLT, PROTRUDING HD

BACB30NX6K8 130 BOLT, PROTRUDING HD

BACB30NX6K8Y 8 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACC30AC6 89 COLLAR

BACC30BH6 824 COLLAR

BACC30M6 135 COLLAR

BACN10TL3A12 2 NUT STANDOFF

BACR15BB4AD5C 4 RIVETS

BACR15BB4AD6C 4 RIVET

BACR15BB6AD4C 27 RIVET, UNIVERSAL HD

BACR15GF6D5 27 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R007B036F 4 SHIM, LAMINATED

BACS40R007B045F 4 SHIM, LAMINATED

BACS40R010B061F 2 SHIM, LAMINATED

Group 8:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-114

142U0106-33 2 STRAP

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

78 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 8:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-114

142U0106-35 2 STRAP

142U0106-37 2 STRAP

142U0107-49 1 FRAME SEGMENT

142U0107-50 1 FRAME SEGMENT

142U0107-51 1 DOUBLER

142U0107-52 1 DOUBLER

142U0107-53 1 TRIPLER

142U0107-54 1 TRIPLER

142U0108-95 1 CHORD SEGMENT

142U0108-96 1 CHORD SEGMENT

142U0108-97 2 CHORD SPLICE - UPPER

142U0108-99 2 CHORD SPLICE - LOWER

142U0108-101 1 SHEAR TIE, S-7 TO S-8

142U0108-102 1 SHEAR TIE, S-7 TO S-8

142U0108-105 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-107 2 SHEAR TIE TEE, S-9 TO S-10

142U0108-109 2 SHEAR TIE TEE, S-10 TO S-11

142U0108-113 1 SHEAR TIE, S-11 TO S-12

142U0108-114 1 SHEAR TIE, S-11 TO S-12

144U0064-8 10 STRINGER CLIP TEE

144U0064-9 10 STRINGER CLIP TEE

144U0064-25 2 STRINGER CLIP TEE

144U0064-26 2 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D019B0F0 2 BRACKET, ANGLE

BACB30NW6K5Y 108 BOLT, 100 DEG HEX DR

BACB30NW6K8X 16 BOLT, 100 DEG HEX DR

BACB30NX6K3 89 BOLT, PROTRUDING HD

BACB30NX6K3X 6 BOLT, PROTRUDING HD

BACB30NX6K3Y 29 BOLT, PROTRUDING HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

79 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 8:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-114

BACB30NX6K4 291 BOLT, PROTRUDING HD

BACB30NX6K4X 8 BOLT, PROTRUDING HD

BACB30NX6K4Y 29 BOLT, PROTRUDING HD

BACB30NX6K5 236 BOLT

BACB30NX6K5X 2 BOLT, PROTRUDING HD

BACB30NX6K5Y 14 BOLT, PROTRUDING HD

BACB30NX6K6Y 2 BOLT, PROTRUDING HD

BACB30NX6K7 49 HI-LOK

BACB30NX6K7X 11 BOLT, PROTRUDING HD

BACB30NX6K7Y 4 BOLT, PROTRUDING HD

BACB30NX6K8 108 BOLT, PROTRUDING HD

BACB30NX6K8Y 8 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACC30AC6 86 COLLAR

BACC30BH6 802 COLLAR

BACC30M6 124 COLLAR

BACN10TL3A12 2 NUT STANDOFF

BACR15BB4AD5C 4 RIVETS

BACR15BB4AD6C 4 RIVET

BACR15BB6AD4C 27 RIVET, UNIVERSAL HD

BACR15GF6D5 27 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R007B036F 4 SHIM, LAMINATED

BACS40R007B045F 4 SHIM, LAMINATED

Group 9:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-115

142U0106-33 2 STRAP

142U0106-35 2 STRAP

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

80 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 9:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-115

142U0106-37 2 STRAP

142U0107-49 1 FRAME SEGMENT

142U0107-50 1 FRAME SEGMENT

142U0107-51 1 DOUBLER

142U0107-52 1 DOUBLER

142U0107-53 1 TRIPLER

142U0107-54 1 TRIPLER

142U0108-95 1 CHORD SEGMENT

142U0108-96 1 CHORD SEGMENT

142U0108-97 2 CHORD SPLICE - UPPER

142U0108-99 2 CHORD SPLICE - LOWER

142U0108-103 1 SHEAR TIE TEE, S-7 TO S-8

142U0108-104 1 SHEAR TIE TEE, S-7 TO S-8

142U0108-105 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-107 2 SHEAR TIE TEE, S-9 TO S-10

142U0108-111 2 SHEAR TIE, S-10 TO S-11

142U0108-113 1 SHEAR TIE, S-11 TO S-12

142U0108-114 1 SHEAR TIE, S-11 TO S-12

144U0064-8 10 STRINGER CLIP TEE

144U0064-9 10 STRINGER CLIP TEE

144U0064-25 2 STRINGER CLIP TEE

144U0064-26 2 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D019B0F0 2 BRACKET, ANGLE

BACB30NW6K5Y 124 BOLT, 100 DEG HEX DR

BACB30NX6K3 86 BOLT, PROTRUDING HD

BACB30NX6K3X 4 BOLT, PROTRUDING HD

BACB30NX6K3Y 31 BOLT, PROTRUDING HD

BACB30NX6K4 284 BOLT, PROTRUDING HD

BACB30NX6K4X 8 BOLT, PROTRUDING HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

81 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 9:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-115

BACB30NX6K4Y 27 BOLT, PROTRUDING HD

BACB30NX6K5 231 BOLT

BACB30NX6K5X 2 BOLT, PROTRUDING HD

BACB30NX6K5Y 20 BOLT, PROTRUDING HD

BACB30NX6K6Y 2 BOLT, PROTRUDING HD

BACB30NX6K7 40 HI-LOK

BACB30NX6K7X 11 BOLT, PROTRUDING HD

BACB30NX6K7Y 10 BOLT, PROTRUDING HD

BACB30NX6K8 124 BOLT, PROTRUDING HD

BACB30NX6K8Y 15 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACB30YP6K7 2 BOLT, 100 DEG HEX DR

BACC30AC6 104 COLLAR

BACC30BH6 794 COLLAR

BACC30BL6 2 COLLAR

BACC30M6 124 COLLAR

BACN10TL3A12 2 NUT STANDOFF

BACR15BB4AD5C 4 RIVETS

BACR15BB4AD6C 4 RIVET

BACR15BB6AD4C 27 RIVET, UNIVERSAL HD

BACR15GF6D5 27 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R007B036F 4 SHIM, LAMINATED

BACS40R007B045F 4 SHIM, LAMINATED

Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-116

142U0106-33 2 STRAP

142U0106-35 2 STRAP

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

82 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-116

142U0106-37 2 STRAP

142U0107-49 1 FRAME SEGMENT

142U0107-50 1 FRAME SEGMENT

142U0107-51 1 DOUBLER

142U0107-52 1 DOUBLER

142U0107-53 1 TRIPLER

142U0107-54 1 TRIPLER

142U0108-95 1 CHORD SEGMENT

142U0108-96 1 CHORD SEGMENT

142U0108-97 2 CHORD SPLICE - UPPER

142U0108-99 2 CHORD SPLICE - LOWER

142U0108-101 1 SHEAR TIE, S-7 TO S-8

142U0108-102 1 SHEAR TIE, S-7 TO S-8

142U0108-105 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-107 2 SHEAR TIE TEE, S-9 TO S-10

142U0108-109 2 SHEAR TIE TEE, S-10 TO S-11

142U0108-113 1 SHEAR TIE, S-11 TO S-12

142U0108-114 1 SHEAR TIE, S-11 TO S-12

144U0064-8 10 STRINGER CLIP TEE

144U0064-9 10 STRINGER CLIP TEE

144U0064-25 2 STRINGER CLIP TEE

144U0064-26 2 STRINGER CLIP TEE

BACB2C028E0E0 1 BRACKET

BACB2D019B0G0 2 BRACKET, ANGLE

BACB30NW6K5Y 108 BOLT, 100 DEG HEX DR

BACB30NW6K8X 16 BOLT, 100 DEG HEX DR

BACB30NX6K3 89 BOLT, PROTRUDING HD

BACB30NX6K3X 6 BOLT, PROTRUDING HD

BACB30NX6K3Y 29 BOLT, PROTRUDING HD

BACB30NX6K4 300 BOLT, PROTRUDING HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

83 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-116

BACB30NX6K4X 4 BOLT, PROTRUDING HD

BACB30NX6K4Y 25 BOLT, PROTRUDING HD

BACB30NX6K5 238 BOLT

BACB30NX6K5X 2 BOLT, PROTRUDING HD

BACB30NX6K5Y 14 BOLT, PROTRUDING HD

BACB30NX6K6Y 2 BOLT, PROTRUDING HD

BACB30NX6K7 44 HI-LOK

BACB30NX6K7X 11 BOLT, PROTRUDING HD

BACB30NX6K7Y 4 BOLT, PROTRUDING HD

BACB30NX6K8 128 BOLT, PROTRUDING HD

BACB30NX6K8Y 8 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACB30YP6K7 2 BOLT, 100 DEG HEX DR

BACC30AC6 82 COLLAR

BACC30BH6 824 COLLAR

BACC30BL6 2 COLLAR

BACC30M6 124 COLLAR

BACN10TL3A8 2 NUT, SPACER PLATE

BACR15BB4AD6C 4 RIVET

BACR15BB6AD4C 27 RIVET, UNIVERSAL HD

BACR15GF6D5 27 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R007B036F 4 SHIM, LAMINATED

BACS40R007B045F 4 SHIM, LAMINATED

BACS53B1ES1 1 ELECTRICAL GROUND STUD

Group 1-4, 6, 8, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-117

142U0106-12 2 STRAP

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

84 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-4, 6, 8, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-117

142U0106-51 2 STRAP

142U0106-53 2 STRAP

142U0107-7 1 TRIPLER

142U0107-8 1 TRIPLER

142U0107-9 1 FRAME SEGMENT

142U0107-10 1 FRAME SEGMENT

142U0107-11 1 DOUBLER

142U0107-12 1 DOUBLER

142U0108-21 1 CHORD SEGMENT

142U0108-22 1 CHORD SEGMENT

142U0108-23 2 CHORD SPLICE - UPPER

142U0108-25 2 SHEAR TIE TEE, S-7 TO S-8

142U0108-27 1 SHEAR TIE, S-11 TO S-12

142U0108-28 1 SHEAR TIE, S-11 TO S-12

142U0108-33 2 SHEAR TIE, S-10 TO S-11

142U0108-45 2 CHORD SPLICE - LOWER

142U0108-57 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-121 2 SHEAR TIE TEE, S-9 TO S-10

144U0064-6 12 STRINGER CLIP TEE

144U0064-7 12 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D018A0C0 2 BRACKET, ANGLE

BACB2D018B0F0 2 BRACKET, ANGLE

BACB30NW6K5Y 124 BOLT, 100 DEG HEX DR

BACB30NW6K6Y 16 BOLT, 100 DEG HEX DR

BACB30NX6K3 91 BOLT, PROTRUDING HD

BACB30NX6K3X 6 BOLT, PROTRUDING HD

BACB30NX6K3Y 29 BOLT, PROTRUDING HD

BACB30NX6K4 266 BOLT, PROTRUDING HD

BACB30NX6K4X 17 BOLT, PROTRUDING HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

85 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-4, 6, 8, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-117

BACB30NX6K4Y 18 BOLT, PROTRUDING HD

BACB30NX6K5 261 BOLT

BACB30NX6K5X 4 BOLT, PROTRUDING HD

BACB30NX6K5Y 11 BOLT, PROTRUDING HD

BACB30NX6K7 47 HI-LOK

BACB30NX6K7X 22 BOLT, PROTRUDING HD

BACB30NX6K8 117 BOLT, PROTRUDING HD

BACB30NX6K8X 6 BOLT, PROTRUDING HD

BACB30NX6K8Y 6 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACC30AC6 64 COLLAR

BACC30BH6 838 COLLAR

BACC30M6 140 COLLAR

BACN10TL3A12 2 NUT STANDOFF

BACN10TL3A6 2 SPACER PLATE NUT

BACR15BB4AD5C 4 RIVETS

BACR15BB6AD4C 27 RIVET, UNIVERSAL HD

BACR15GF6D5 27 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R008B036F 2 SHIM - LAMINATED

BACS40R008B037F 2 SHIM - LAMINATED

BACS40R008B044F 4 SHIM - LAMINATED

Group 9:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-119

142U0106-12 2 STRAP

142U0106-51 2 STRAP

142U0106-53 2 STRAP

142U0107-7 1 TRIPLER

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

86 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 9:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-119

142U0107-8 1 TRIPLER

142U0107-9 1 FRAME SEGMENT

142U0107-10 1 FRAME SEGMENT

142U0107-11 1 DOUBLER

142U0107-12 1 DOUBLER

142U0108-21 1 CHORD SEGMENT

142U0108-22 1 CHORD SEGMENT

142U0108-23 2 CHORD SPLICE - UPPER

142U0108-27 1 SHEAR TIE, S-11 TO S-12

142U0108-28 1 SHEAR TIE, S-11 TO S-12

142U0108-29 2 SHEAR TIE, S-7 TO S-8

142U0108-31 2 SHEAR TIE TEE, S-10 TO S-11

142U0108-45 2 CHORD SPLICE - LOWER

142U0108-57 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-121 2 SHEAR TIE TEE, S-9 TO S-10

144U0064-6 12 STRINGER CLIP TEE

144U0064-7 12 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D018B0F0 2 BRACKET, ANGLE

BACB30NW6K5Y 141 BOLT, 100 DEG HEX DR

BACB30NW6K6Y 16 BOLT, 100 DEG HEX DR

BACB30NX6K3 91 BOLT, PROTRUDING HD

BACB30NX6K3X 6 BOLT, PROTRUDING HD

BACB30NX6K3Y 29 BOLT, PROTRUDING HD

BACB30NX6K4 266 BOLT, PROTRUDING HD

BACB30NX6K4X 17 BOLT, PROTRUDING HD

BACB30NX6K4Y 18 BOLT, PROTRUDING HD

BACB30NX6K5 258 BOLT

BACB30NX6K5X 4 BOLT, PROTRUDING HD

BACB30NX6K5Y 11 BOLT, PROTRUDING HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

87 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 9:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-119

BACB30NX6K7 47 HI-LOK

BACB30NX6K7X 22 BOLT, PROTRUDING HD

BACB30NX6K8 124 BOLT, PROTRUDING HD

BACB30NX6K8X 6 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACC30AC6 58 COLLAR

BACC30BH6 842 COLLAR

BACC30M6 157 COLLAR

BACN10TL3A12 2 NUT STANDOFF

BACR15BB4AD5C 4 RIVETS

BACR15BB6AD4C 27 RIVET, UNIVERSAL HD

BACR15GF6D5 27 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R008B036F 2 SHIM - LAMINATED

BACS40R008B037F 2 SHIM - LAMINATED

BACS40R008B044F 4 SHIM - LAMINATED

Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-120

142U0106-12 2 STRAP

142U0106-51 2 STRAP

142U0106-53 2 STRAP

142U0107-7 1 TRIPLER

142U0107-8 1 TRIPLER

142U0107-9 1 FRAME SEGMENT

142U0107-10 1 FRAME SEGMENT

142U0107-11 1 DOUBLER

142U0107-12 1 DOUBLER

142U0108-21 1 CHORD SEGMENT

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

88 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-120

142U0108-22 1 CHORD SEGMENT

142U0108-23 2 CHORD SPLICE - UPPER

142U0108-25 2 SHEAR TIE TEE, S-7 TO S-8

142U0108-27 1 SHEAR TIE, S-11 TO S-12

142U0108-28 1 SHEAR TIE, S-11 TO S-12

142U0108-31 2 SHEAR TIE TEE, S-10 TO S-11

142U0108-45 2 CHORD SPLICE - LOWER

142U0108-57 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-121 2 SHEAR TIE TEE, S-9 TO S-10

144U0064-6 12 STRINGER CLIP TEE

144U0064-7 12 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D018B0E0 1 BRACKET, ANGLE

BACB2D018B0F0 2 BRACKET, ANGLE

BACB30NW6K5Y 141 BOLT, 100 DEG HEX DR

BACB30NW6K6Y 16 BOLT, 100 DEG HEX DR

BACB30NX6K3 91 BOLT, PROTRUDING HD

BACB30NX6K3X 11 BOLT, PROTRUDING HD

BACB30NX6K3Y 25 BOLT, PROTRUDING HD

BACB30NX6K4 275 BOLT, PROTRUDING HD

BACB30NX6K4X 17 BOLT, PROTRUDING HD

BACB30NX6K4Y 18 BOLT, PROTRUDING HD

BACB30NX6K5 263 BOLT

BACB30NX6K5X 4 BOLT, PROTRUDING HD

BACB30NX6K5Y 11 BOLT, PROTRUDING HD

BACB30NX6K7 47 HI-LOK

BACB30NX6K7X 22 BOLT, PROTRUDING HD

BACB30NX6K8 115 BOLT, PROTRUDING HD

BACB30NX6K8X 6 BOLT, PROTRUDING HD

BACB30NX6K8Y 6 BOLT, PROTRUDING HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

89 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-120

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACC30AC6 60 COLLAR

BACC30BH6 852 COLLAR

BACC30M6 157 COLLAR

BACN10TL3A12 2 NUT STANDOFF

BACN10TL3A8 1 NUT, SPACER PLATE

BACR15BB4AD5C 6 RIVETS

BACR15BB6AD4C 27 RIVET, UNIVERSAL HD

BACR15GF6D5 27 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R008B036F 2 SHIM - LAMINATED

BACS40R008B037F 2 SHIM - LAMINATED

BACS40R008B044F 4 SHIM - LAMINATED

Group 1-4, 6, 8, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-121

142U0106-10 2 STRAP

142U0106-55 2 STRAP

142U0106-57 2 STRAP

142U0107-33 1 FRAME SEGMENT

142U0107-34 1 FRAME SEGMENT

142U0107-35 1 DOUBLER

142U0107-36 1 DOUBLER

142U0107-37 1 TRIPLER

142U0107-38 1 TRIPLER

142U0108-59 1 CHORD SEGMENT

142U0108-60 1 CHORD SEGMENT

142U0108-61 2 CHORD SPLICE - LOWER

142U0108-63 2 CHORD SPLICE - UPPER

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

90 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-4, 6, 8, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-121

142U0108-65 1 SHEAR TIE, S-11 TO S-12

142U0108-66 1 SHEAR TIE, S-11 TO S-12

142U0108-67 2 SHEAR TIE, S-10 TO S-11

142U0108-69 2 SHEAR TIE TEE, S-7 TO S-8

142U0108-71 2 SHEAR TIE TEE, S-6 TO S-7

142U0108-75 2 SHEAR TIE TEE, S-9 TO S-10

142U0108-123 2 SHEAR TIE TEE, S-8 TO S-9

144U0064-6 14 STRINGER CLIP TEE

144U0064-7 14 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D018B0F0 2 BRACKET, ANGLE

BACB2D019A0C0 2 BRACKET, ANGLE

BACB30NW6K3Y 6 BOLT, 100 DEG HEX DR

BACB30NW6K6Y 141 BOLT, 100 DEG HEX DR

BACB30NW6K7Y 16 BOLT, 100 DEG HEX DR

BACB30NX6K3 84 BOLT, PROTRUDING HD

BACB30NX6K3X 14 BOLT, PROTRUDING HD

BACB30NX6K3Y 29 BOLT, PROTRUDING HD

BACB30NX6K4 167 BOLT, PROTRUDING HD

BACB30NX6K4X 15 BOLT, PROTRUDING HD

BACB30NX6K4Y 14 BOLT, PROTRUDING HD

BACB30NX6K5 168 BOLT

BACB30NX6K5X 2 BOLT, PROTRUDING HD

BACB30NX6K5Y 14 BOLT, PROTRUDING HD

BACB30NX6K6X 16 BOLT, PROTRUDING HD

BACB30NX6K6Y 4 BOLT, PROTRUDING HD

BACB30NX6K7 34 HI-LOK

BACB30NX6K7X 11 BOLT, PROTRUDING HD

BACB30NX6K7Y 2 BOLT, PROTRUDING HD

BACB30NX6K8 138 BOLT, PROTRUDING HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

91 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-4, 6, 8, 11-15:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-121

BACB30NX6K8X 6 BOLT, PROTRUDING HD

BACB30NX6K8Y 6 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACB30YP6K8 18 BOLT, 100 DEG HEX DR

BACC30AC6 589 COLLAR

BACC30BH6 31 COLLAR

BACC30BL6 18 COLLAR

BACC30M6 169 COLLAR

BACN10TL3A12 2 NUT STANDOFF

BACN10TL3A6 2 SPACER PLATE NUT

BACR15BB4AD5C 4 RIVETS

BACR15BB6AD4C 31 RIVET, UNIVERSAL HD

BACR15GF6D5 31 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R008B035F 2 SHIM, LAMINATED

BACS40R008B036F 6 SHIM - LAMINATED

Group 9:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-123

FILLER BETWEEN CLIPS OF

CREASE

142U0103-154 2

142U0104-5 1 BEAM

142U0104-6 1 BEAM

142U0104-7 1 CLIP

142U0104-8 1 CLIP

142U0106-10 2 STRAP

142U0106-55 2 STRAP

142U0106-57 2 STRAP

142U0107-33 1 FRAME SEGMENT

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

92 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 9:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-123

142U0107-34 1 FRAME SEGMENT

142U0107-35 1 DOUBLER

142U0107-36 1 DOUBLER

142U0107-37 1 TRIPLER

142U0107-38 1 TRIPLER

142U0108-59 1 CHORD SEGMENT

142U0108-60 1 CHORD SEGMENT

142U0108-61 2 CHORD SPLICE - LOWER

142U0108-63 2 CHORD SPLICE - UPPER

142U0108-65 1 SHEAR TIE, S-11 TO S-12

142U0108-66 1 SHEAR TIE, S-11 TO S-12

142U0108-67 2 SHEAR TIE, S-10 TO S-11

142U0108-69 2 SHEAR TIE TEE, S-7 TO S-8

142U0108-73 2 SHEAR TIE, S-6 TO S-7

142U0108-75 2 SHEAR TIE TEE, S-9 TO S-10

142U0108-123 2 SHEAR TIE TEE, S-8 TO S-9

144U0064-6 14 STRINGER CLIP TEE

144U0064-7 14 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D018B0F0 2 BRACKET, ANGLE

BACB30NW6K5 4 BOLT, HILOK

BACB30NW6K6Y 137 BOLT, 100 DEG HEX DR

BACB30NW6K7Y 16 BOLT, 100 DEG HEX DR

BACB30NX6K20 2 BOLT, PROTRUDING HD

BACB30NX6K2Y 48 BOLT, HEX DRIVE

BACB30NX6K3 101 BOLT, PROTRUDING HD

BACB30NX6K3X 14 BOLT, PROTRUDING HD

BACB30NX6K3Y 126 BOLT, PROTRUDING HD

BACB30NX6K4 310 BOLT, PROTRUDING HD

BACB30NX6K4X 15 BOLT, PROTRUDING HD

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Original Issue: October 08, 2009

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BOEING SERVICE BULLETIN 747-53A2605

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Group 9:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-123

BACB30NX6K4Y 12 BOLT, PROTRUDING HD

BACB30NX6K5 310 BOLT

BACB30NX6K5X 4 BOLT, PROTRUDING HD

BACB30NX6K5Y 20 BOLT, PROTRUDING HD

BACB30NX6K6 8 BOLT

BACB30NX6K6X 14 BOLT, PROTRUDING HD

BACB30NX6K7 43 HI-LOK

BACB30NX6K7X 13 BOLT, PROTRUDING HD

BACB30NX6K7Y 4 BOLT, PROTRUDING HD

BACB30NX6K8 142 BOLT, PROTRUDING HD

BACB30NX6K8X 6 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACC30AC6 210 COLLAR

BACC30BH6 975 COLLAR

BACC30M6 168 COLLAR

BACN10TL3A12 2 NUT STANDOFF

BACR15BB4AD5C 4 RIVETS

BACR15BB6AD4C 31 RIVET, UNIVERSAL HD

BACR15GF6D5 31 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R008B035F 2 SHIM, LAMINATED

BACS40R008B036F 6 SHIM - LAMINATED

Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-124

FILLER BETWEEN CLIPS OF

CREASE

142U0103-154 2

142U0104-5 1 BEAM

142U0104-6 1 BEAM

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

94 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-124

142U0104-7 1 CLIP

142U0104-8 1 CLIP

142U0106-10 2 STRAP

142U0106-55 2 STRAP

142U0106-57 2 STRAP

142U0107-33 1 FRAME SEGMENT

142U0107-34 1 FRAME SEGMENT

142U0107-35 1 DOUBLER

142U0107-36 1 DOUBLER

142U0107-37 1 TRIPLER

142U0107-38 1 TRIPLER

142U0108-59 1 CHORD SEGMENT

142U0108-60 1 CHORD SEGMENT

142U0108-61 2 CHORD SPLICE - LOWER

142U0108-63 2 CHORD SPLICE - UPPER

142U0108-65 1 SHEAR TIE, S-11 TO S-12

142U0108-66 1 SHEAR TIE, S-11 TO S-12

142U0108-67 2 SHEAR TIE, S-10 TO S-11

142U0108-69 2 SHEAR TIE TEE, S-7 TO S-8

142U0108-71 2 SHEAR TIE TEE, S-6 TO S-7

SHEAR TIE TEE, S-9 TO S10142U0108-75 2

142U0108-123 2 SHEAR TIE TEE, S-8 TO S-9

144U0064-6 14 STRINGER CLIP TEE

144U0064-7 14 STRINGER CLIP TEE

255U0281U5 1 CLIP

69B41412-3 2 INSULATOR

BACB2D018B0F0 2 BRACKET, ANGLE

BACB2D020E0H0 1 BRACKET, ANGLE

BACB30NW6K5 6 BOLT, HILOK

BACB30NW6K6Y 159 BOLT, 100 DEG HEX DR

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

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95 of 158

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ALERT ALERT
Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-124

BACB30NW6K7Y 16 BOLT, 100 DEG HEX DR

BACB30NX6K20 2 BOLT, PROTRUDING HD

BACB30NX6K2Y 48 BOLT, HEX DRIVE

BACB30NX6K3 99 BOLT, PROTRUDING HD

BACB30NX6K3X 14 BOLT, PROTRUDING HD

BACB30NX6K3Y 128 BOLT, PROTRUDING HD

BACB30NX6K4 315 BOLT, PROTRUDING HD

BACB30NX6K4X 17 BOLT, PROTRUDING HD

BACB30NX6K4Y 14 BOLT, PROTRUDING HD

BACB30NX6K5 329 BOLT

BACB30NX6K5X 6 BOLT, PROTRUDING HD

BACB30NX6K5Y 22 BOLT, PROTRUDING HD

BACB30NX6K6 8 BOLT

BACB30NX6K6X 14 BOLT, PROTRUDING HD

BACB30NX6K7 43 HI-LOK

BACB30NX6K7X 16 BOLT, PROTRUDING HD

BACB30NX6K7Y 16 BOLT, PROTRUDING HD

BACB30NX6K8 142 BOLT, PROTRUDING HD

BACB30NX6K8X 6 BOLT, PROTRUDING HD

BACB30NX6K8Y 8 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACC30AC6 237 COLLAR

BACC30BH6 998 COLLAR

BACC30M6 191 COLLAR

BACF3F008L008NN 1 FILLER

BACF3F008V008NN 1 FILLER

BACF3H07RF009HN 1 FILLER, RADIUSED EDGE

BACN10TL3A12 2 NUT STANDOFF

BACN10TL3A4 1 NUT, SPACER PLATE

BACR15BB4AD4C 2 RIVET, UNIVERSAL HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

96 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-124

BACR15BB4AD5C 4 RIVETS

BACR15BB6AD4C 31 RIVET, UNIVERSAL HD

BACR15GF6D5 31 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R008B035F 2 SHIM, LAMINATED

BACS40R008B036F 6 SHIM - LAMINATED

Group 5, 7:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-125

142U0106-33 2 STRAP

142U0106-35 2 STRAP

142U0106-37 2 STRAP

142U0107-49 1 FRAME SEGMENT

142U0107-50 1 FRAME SEGMENT

142U0107-51 1 DOUBLER

142U0107-52 1 DOUBLER

142U0107-53 1 TRIPLER

142U0107-54 1 TRIPLER

142U0108-95 1 CHORD SEGMENT

142U0108-96 1 CHORD SEGMENT

142U0108-97 2 CHORD SPLICE - UPPER

142U0108-99 2 CHORD SPLICE - LOWER

142U0108-103 1 SHEAR TIE TEE, S-7 TO S-8

142U0108-104 1 SHEAR TIE TEE, S-7 TO S-8

142U0108-105 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-107 2 SHEAR TIE TEE, S-9 TO S-10

142U0108-111 2 SHEAR TIE, S-10 TO S-11

142U0108-113 1 SHEAR TIE, S-11 TO S-12

142U0108-114 1 SHEAR TIE, S-11 TO S-12

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

97 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 5, 7:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-125

144U0064-8 10 STRINGER CLIP TEE

144U0064-9 10 STRINGER CLIP TEE

144U0064-25 2 STRINGER CLIP TEE

144U0064-26 2 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D019B0F0 2 BRACKET, ANGLE

BACB30NW6K5Y 124 BOLT, 100 DEG HEX DR

BACB30NX6K3 95 BOLT, PROTRUDING HD

BACB30NX6K3X 4 BOLT, PROTRUDING HD

BACB30NX6K3Y 38 BOLT, PROTRUDING HD

BACB30NX6K4 284 BOLT, PROTRUDING HD

BACB30NX6K4X 8 BOLT, PROTRUDING HD

BACB30NX6K4Y 29 BOLT, PROTRUDING HD

BACB30NX6K5 231 BOLT

BACB30NX6K5X 2 BOLT, PROTRUDING HD

BACB30NX6K5Y 20 BOLT, PROTRUDING HD

BACB30NX6K6Y 2 BOLT, PROTRUDING HD

BACB30NX6K7 40 HI-LOK

BACB30NX6K7X 11 BOLT, PROTRUDING HD

BACB30NX6K7Y 12 BOLT, PROTRUDING HD

BACB30NX6K8 126 BOLT, PROTRUDING HD

BACB30NX6K8Y 15 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACB30YP6K7 2 BOLT, 100 DEG HEX DR

BACC30AC6 115 COLLAR

BACC30BH6 805 COLLAR

BACC30BL6 2 COLLAR

BACC30M6 126 COLLAR

BACN10TL3A12 2 NUT STANDOFF

BACR15BB4AD5C 4 RIVETS

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

98 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 5, 7:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-125

BACR15BB4AD6C 4 RIVET

BACR15BB6AD4C 31 RIVET, UNIVERSAL HD

BACR15GF6D5 31 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R007B036F 4 SHIM, LAMINATED

BACS40R007B045F 4 SHIM, LAMINATED

Group 5, 7:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-126

142U0106-12 2 STRAP

142U0106-51 2 STRAP

142U0106-53 2 STRAP

142U0107-7 1 TRIPLER

142U0107-8 1 TRIPLER

142U0107-9 1 FRAME SEGMENT

142U0107-10 1 FRAME SEGMENT

142U0107-11 1 DOUBLER

142U0107-12 1 DOUBLER

142U0108-21 1 CHORD SEGMENT

142U0108-22 1 CHORD SEGMENT

142U0108-23 2 CHORD SPLICE - UPPER

142U0108-25 2 SHEAR TIE TEE, S-7 TO S-8

142U0108-27 1 SHEAR TIE, S-11 TO S-12

142U0108-28 1 SHEAR TIE, S-11 TO S-12

142U0108-31 2 SHEAR TIE TEE, S-10 TO S-11

142U0108-45 2 CHORD SPLICE - LOWER

142U0108-57 2 SHEAR TIE TEE, S-8 TO S-9

142U0108-121 2 SHEAR TIE TEE, S-9 TO S-10

144U0064-6 12 STRINGER CLIP TEE

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

99 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 5, 7:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-126

144U0064-7 12 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D018B0F0 2 BRACKET, ANGLE

BACB30NW6K5Y 141 BOLT, 100 DEG HEX DR

BACB30NW6K6Y 16 BOLT, 100 DEG HEX DR

BACB30NX6K3 91 BOLT, PROTRUDING HD

BACB30NX6K3X 6 BOLT, PROTRUDING HD

BACB30NX6K3Y 29 BOLT, PROTRUDING HD

BACB30NX6K4 266 BOLT, PROTRUDING HD

BACB30NX6K4X 17 BOLT, PROTRUDING HD

BACB30NX6K4Y 18 BOLT, PROTRUDING HD

BACB30NX6K5 258 BOLT

BACB30NX6K5X 4 BOLT, PROTRUDING HD

BACB30NX6K5Y 11 BOLT, PROTRUDING HD

BACB30NX6K7 47 HI-LOK

BACB30NX6K7X 22 BOLT, PROTRUDING HD

BACB30NX6K8 124 BOLT, PROTRUDING HD

BACB30NX6K8X 6 BOLT, PROTRUDING HD

BACB30NX6K8Y 6 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACC30AC6 64 COLLAR

BACC30BH6 842 COLLAR

BACC30M6 157 COLLAR

BACN10TL3A12 2 NUT STANDOFF

BACR15BB4AD5C 4 RIVETS

BACR15BB6AD4C 27 RIVET, UNIVERSAL HD

BACR15GF6D5 27 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R008B036F 2 SHIM - LAMINATED

BACS40R008B037F 2 SHIM - LAMINATED

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

100 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 5, 7:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-126

BACS40R008B044F 4 SHIM - LAMINATED

Group 5, 7:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-127

FILLER BETWEEN CLIPS OF

CREASE

142U0103-154 2

142U0104-5 1 BEAM

142U0104-6 1 BEAM

142U0104-7 1 CLIP

142U0104-8 1 CLIP

142U0106-10 2 STRAP

142U0106-55 2 STRAP

142U0106-57 2 STRAP

142U0107-33 1 FRAME SEGMENT

142U0107-34 1 FRAME SEGMENT

142U0107-35 1 DOUBLER

142U0107-36 1 DOUBLER

142U0107-37 1 TRIPLER

142U0107-38 1 TRIPLER

142U0108-59 1 CHORD SEGMENT

142U0108-60 1 CHORD SEGMENT

142U0108-61 2 CHORD SPLICE - LOWER

142U0108-63 2 CHORD SPLICE - UPPER

142U0108-65 1 SHEAR TIE, S-11 TO S-12

142U0108-66 1 SHEAR TIE, S-11 TO S-12

142U0108-67 2 SHEAR TIE, S-10 TO S-11

142U0108-69 2 SHEAR TIE TEE, S-7 TO S-8

142U0108-71 2 SHEAR TIE TEE, S-6 TO S-7

142U0108-75 2 SHEAR TIE TEE, S-9 TO S-10

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

101 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 5, 7:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-127

142U0108-123 2 SHEAR TIE TEE, S-8 TO S-9

144U0064-6 14 STRINGER CLIP TEE

144U0064-7 14 STRINGER CLIP TEE

69B41412-3 2 INSULATOR

BACB2D018B0F0 2 BRACKET, ANGLE

BACB30NW6K5 4 BOLT, HILOK

BACB30NW6K6Y 137 BOLT, 100 DEG HEX DR

BACB30NW6K7Y 16 BOLT, 100 DEG HEX DR

BACB30NX6K20 2 BOLT, PROTRUDING HD

BACB30NX6K2Y 48 BOLT, HEX DRIVE

BACB30NX6K3 101 BOLT, PROTRUDING HD

BACB30NX6K3X 14 BOLT, PROTRUDING HD

BACB30NX6K3Y 126 BOLT, PROTRUDING HD

BACB30NX6K4 310 BOLT, PROTRUDING HD

BACB30NX6K4X 15 BOLT, PROTRUDING HD

BACB30NX6K4Y 12 BOLT, PROTRUDING HD

BACB30NX6K5 310 BOLT

BACB30NX6K5X 4 BOLT, PROTRUDING HD

BACB30NX6K5Y 20 BOLT, PROTRUDING HD

BACB30NX6K6 8 BOLT

BACB30NX6K6X 14 BOLT, PROTRUDING HD

BACB30NX6K7 43 HI-LOK

BACB30NX6K7X 13 BOLT, PROTRUDING HD

BACB30NX6K7Y 4 BOLT, PROTRUDING HD

BACB30NX6K8 142 BOLT, PROTRUDING HD

BACB30NX6K8X 6 BOLT, PROTRUDING HD

BACB30NX6K9X 2 BOLT, PROTRUDING HD

BACC30AC6 210 COLLAR

BACC30BH6 975 COLLAR

BACC30M6 168 COLLAR

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

102 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 5, 7:

Kit 142U0101

Existing Part Notes

Number

New Part Number QTY Name

-127

BACN10TL3A12 2 NUT STANDOFF

BACR15BB4AD5C 4 RIVETS

BACR15BB6AD4C 31 RIVET, UNIVERSAL HD

BACR15GF6D5 31 RIVET

BACS40R005C005F 4 SHIM,LAMINATED

BACS40R008B035F 2 SHIM, LAMINATED

BACS40R008B036F 6 SHIM - LAMINATED

Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-201

142U0103-1 1 ALUMINUM STRAP LEFT

142U0103-2 1 ALUMINUM STRAP RIGHT

142U0103-3 2 STEEL STRAP

142U0103-4 2 STEEL STRAP

142U0103-5 2 STEEL STRAP

142U0104-1 4 TENSION TIE SPLICE

142U0105-1 1 STRINGER CLIP LEFT

142U0105-2 1 STRINGER CLIP RIGHT

142U0105-4 4 TENSION TIE SEGMENT

BACB30NX6K3 2 BOLT, PROTRUDING HD

BACB30NX6K3X 2 BOLT, PROTRUDING HD

BACB30NX8K3 203 HI-LOK

BACB30NX8K4 71 HI-LOK

BACB30NX8K5 49 HI LOK

BACB30NX8K6 14 BOLT

BACB30NX8K7 27 BOLT, HEX DRIVE

BACB30US4K11 8 BOLT, 12 PT HEAD

BACB30US4K9 13 BOLT, 12 PT HEAD

BACC30BH6 4 COLLAR

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

103 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-201

BACC30BH8 361 COLLAR

BACN10HR4CD 22 NUT

BACR15BB6AD4C 2 RIVET, UNIVERSAL HD

BACR15GF6D5 2 RIVET

BACS40R011B053F 4 SHIM, LAMINATED

BACS40R011B054F 4 SHIM, LAMINATED

BACW10BP4CD 22 WASHER

BACW10BP4DP 22 WASHER

Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-202

142U0103-6 2 STEEL STRAP

142U0103-7 1 ALUMINUM STRAP LEFT

142U0103-8 1 ALUMINUM STRAP RIGHT

142U0103-9 2 STEEL STRAP

142U0103-10 2 STEEL STRAP

142U0104-1 4 TENSION TIE SPLICE

142U0105-4 4 TENSION TIE SEGMENT

BACB30NX8K3 163 HI-LOK

BACB30NX8K4 71 HI-LOK

BACB30NX8K5 53 HI LOK

BACB30NX8K6 14 BOLT

BACB30NX8K7 27 BOLT, HEX DRIVE

BACB30US4K10 4 BOLT, 12 PT HEAD

BACB30US4K11 14 BOLT, 12 PT HEAD

BACB30US4K9 4 BOLT, 12 PT HEAD

BACC30BH8 328 COLLAR

BACN10HR4CD 22 NUT

BACS40R011B052F 2 SHIM, LAMINATED

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

104 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-202

BACS40R011B059F 2 SHIM, LAMINATED

BACS40R011B062F 2 SHIM, LAMINATED

BACS40R011B064F 2 SHIM, LAMINATED

BACW10BP4CD 22 WASHER

BACW10BP4DP 22 WASHER

Group 1, 13:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-203

142U0103-11 1 ALUMINUM STRAP LEFT

142U0103-12 1 ALUMINUM STRAP RIGHT

142U0103-13 2 STEEL STRAP

142U0103-14 2 STEEL STRAP

142U0103-15 2 STEEL STRAP

142U0103-16 2 FILLER

142U0103-17 2 DOUBLER

142U0103-18 2 DOUBLER SPLICE

142U0103-19 2 FILLER

142U0104-3 4 TENSION TIE SPLICE

142U0104-24 1 ANGLE

142U0104-25 1 ANGLE

142U0105-5 4 TENSION TIE SEGMENT

BACB30NW6K5X 2 BOLT, 100 DEG HEX DR

BACB30NX6K4Y 14 BOLT, PROTRUDING HD

BACB30NX6K5X 8 BOLT, PROTRUDING HD

BACB30NX6K7X 18 BOLT, PROTRUDING HD

BACB30NX6K8X 2 BOLT, PROTRUDING HD

BACB30NX8K3 185 HI-LOK

BACB30NX8K4 58 HI-LOK

BACB30NX8K5 36 HI LOK

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

105 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1, 13:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-203

BACB30NX8K6 40 BOLT

BACB30NX8K7 27 BOLT, HEX DRIVE

BACB30US4K10 6 BOLT, 12 PT HEAD

BACB30US5K11 4 BOLT, 12 PT HEAD

BACB30US5K12 8 BOLT, 12 PT HEAD

BACC30AC6 14 COLLAR

BACC30BH6 29 COLLAR

BACC30BH8 346 COLLAR

BACC30M6 2 COLLAR

BACF3F009J051NG 2 FILLER, FLAT

BACN10HR4CD 6 NUT

BACN10HR5CD 14 NUT

BACS40R008B051F 8 SHIM, LAMINATED

BACW10BP4CD 6 WASHER

BACW10BP4DP 6 WASHER

BACW10BP5CD 14 CSK WASHER

BACW10BP5DP 14 WASHER

Group 2, 14:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-204

142U0103-18 2 DOUBLER SPLICE

142U0103-21 1 ALUMINUM STRAP LEFT

142U0103-22 1 ALUMINUM STRAP RIGHT

142U0103-23 2 STEEL STRAP

142U0103-24 2 STEEL STRAP

142U0103-25 2 STEEL STRAP

142U0103-26 2 DOUBLER

142U0103-27 2 FILLER

142U0104-3 4 TENSION TIE SPLICE

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

106 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 2, 14:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-204

142U0105-5 4 TENSION TIE SEGMENT

BACB30NX8K3 168 HI-LOK

BACB30NX8K4 62 HI-LOK

BACB30NX8K5 36 HI LOK

BACB30NX8K6 40 BOLT

BACB30NX8K7 31 BOLT, HEX DRIVE

BACB30US4K9 4 BOLT, 12 PT HEAD

BACB30US5K10 4 BOLT, 12 PT HEAD

BACB30US5K11 8 BOLT, 12 PT HEAD

BACC30BH8 332 COLLAR

BACN10HR4CD 4 NUT

BACN10HR5CD 13 NUT

BACS40R008B052F 8 SHIM,LAMINATED

BACW10BP4CD 4 WASHER

BACW10BP4DP 4 WASHER

BACW10BP5CD 13 CSK WASHER

BACW10BP5DP 13 WASHER

Group 3:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-205

142U0103-18 2 DOUBLER SPLICE

142U0103-28 2 FILLER

142U0103-29 1 ALUMINUM STRAP LEFT

142U0103-30 1 ALUMINUM STRAP RIGHT

142U0103-31 2 STEEL STRAP

142U0103-32 2 STEEL STRAP

142U0103-33 2 STEEL STRAP

142U0103-34 2 DOUBLER

142U0104-3 4 TENSION TIE SPLICE

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

107 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 3:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-205

142U0105-5 4 TENSION TIE SEGMENT

BACB30NX8K3 172 HI-LOK

BACB30NX8K4 62 HI-LOK

BACB30NX8K5 36 HI LOK

BACB30NX8K6 40 BOLT

BACB30NX8K7 31 BOLT, HEX DRIVE

BACB30US4K9 4 BOLT, 12 PT HEAD

BACB30US5K10 4 BOLT, 12 PT HEAD

BACB30US5K11 8 BOLT, 12 PT HEAD

BACC30BH8 337 COLLAR

BACN10HR4CD 4 NUT

BACN10HR5CD 13 NUT

BACS40R008B051F 8 SHIM, LAMINATED

BACW10BP4CD 4 WASHER

BACW10BP4DP 4 WASHER

BACW10BP5CD 13 CSK WASHER

BACW10BP5DP 13 WASHER

Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-206

142U0103-35 1 ALUMINUM STRAP LEFT

142U0103-36 1 ALUMINUM STRAP RIGHT

142U0103-37 2 STEEL STRAP

142U0103-38 2 STEEL STRAP

142U0103-39 2 STEEL STRAP

142U0104-1 4 TENSION TIE SPLICE

142U0105-4 4 TENSION TIE SEGMENT

BACB30NX8K3 150 HI-LOK

BACB30NX8K4 62 HI-LOK

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

108 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-206

BACB30NX8K5 47 HI LOK

BACB30NX8K6 14 BOLT

BACB30NX8K7 33 BOLT, HEX DRIVE

BACB30US4K7 4 BOLT, 12 PT HEAD

BACB30US4K8 2 BOLT, 12 PT HEAD

BACB30US4K9 14 BOLT, 12 PT HEAD

BACC30BH8 306 COLLAR

BACN10HR4CD 20 NUT

BACS40R011B052F 2 SHIM, LAMINATED

BACS40R011B055F 2 SHIM, LAMINATED

BACS40R011B057F 4 SHIM LAMINATED

BACW10BP4CD 20 WASHER

BACW10BP4DP 20 WASHER

Group 1-2, 8, 11, 13-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-207

142U0103-18 2 DOUBLER SPLICE

142U0103-40 2 FILLER

142U0103-41 1 ALUMINUM STRAP LEFT

142U0103-42 1 ALUMINUM STRAP RIGHT

142U0103-43 2 STEEL STRAP

142U0103-44 2 STEEL STRAP

142U0103-45 2 STEEL STRAP

142U0103-46 2 DOUBLER

142U0103-47 2 FILLER

142U0103-48 2 FILLER

142U0104-3 4 TENSION TIE SPLICE

142U0104-26 1 CHORD

142U0104-27 1 CHORD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

109 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-2, 8, 11, 13-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-207

142U0105-5 4 TENSION TIE SEGMENT

BACB30NX6K5X 11 BOLT, PROTRUDING HD

BACB30NX6K6X 2 BOLT, PROTRUDING HD

BACB30NX6K7X 22 BOLT, PROTRUDING HD

BACB30NX8K3 172 HI-LOK

BACB30NX8K4 58 HI-LOK

BACB30NX8K5 36 HI LOK

BACB30NX8K6 40 BOLT

BACB30NX8K7 27 BOLT, HEX DRIVE

BACB30US4K10 4 BOLT, 12 PT HEAD

BACB30US4K11 4 BOLT, 12 PT HEAD

BACB30US4K12 8 BOLT, 12 PT HEAD

BACB30US4K15 4 BOLT, 12 PT HEAD

BACC30BH6 35 COLLAR

BACC30BH8 333 COLLAR

BACF3H10XP010HN 4 FILLER, RECTANGULAR

BACN10HR4CD 22 NUT

BACS40R008B051F 8 SHIM, LAMINATED

BACW10BP4CD 22 WASHER

BACW10BP4DP 22 WASHER

Group 3, 12:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-208

142U0103-18 2 DOUBLER SPLICE

142U0103-49 1 ALUMINUM STRAP LEFT

142U0103-50 1 ALUMINUM STRAP RIGHT

142U0103-51 2 STEEL STRAP

142U0103-52 2 STEEL STRAP

142U0103-53 2 STEEL STRAP

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

110 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 3, 12:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-208

142U0103-54 2 FILLER

142U0103-55 2 DOUBLER

142U0104-3 4 TENSION TIE SPLICE

142U0105-5 4 TENSION TIE SEGMENT

BACB30NX8K3 172 HI-LOK

BACB30NX8K4 58 HI-LOK

BACB30NX8K5 36 HI LOK

BACB30NX8K6 40 BOLT

BACB30NX8K7 27 BOLT, HEX DRIVE

BACB30US4K10 4 BOLT, 12 PT HEAD

BACB30US4K11 8 BOLT, 12 PT HEAD

BACB30US4K14 4 BOLT, 12 PT HEAD

BACB30US4K9 4 BOLT, 12 PT HEAD

BACC30BH8 333 COLLAR

BACF3H10XP010HN 4 FILLER, RECTANGULAR

BACN10HR4CD 22 NUT

BACS40R008B051F 8 SHIM, LAMINATED

BACW10BP4CD 22 WASHER

BACW10BP4DP 22 WASHER

Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-209

142U0103-56 2 STEEL STRAP

142U0103-57 1 ALUMINUM STRAP LEFT

142U0103-58 1 ALUMINUM STRAP RIGHT

142U0103-59 2 STEEL STRAP

142U0103-60 2 STEEL STRAP

142U0104-3 4 TENSION TIE SPLICE

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

111 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-209

TENSION TIE STOCK SEGMENT144U0064-66 4

BACB30NX8K3 108 HI-LOK

BACB30NX8K4 56 HI-LOK

BACB30NX8K5 49 HI LOK

BACB30NX8K6 16 BOLT

BACB30NX8K7 27 BOLT, HEX DRIVE

BACB30US3K8Y 2 BOLT

BACB30US4K10 11 BOLT, 12 PT HEAD

BACB30US4K14 2 BOLT, 12 PT HEAD

BACB30US4K9 4 BOLT, 12 PT HEAD

BACC30BH8 253 COLLAR

BACF3H10XK010HN 2 FILLER, RECTANGULAR

BACN10HR3CD 2 SELF-LOCKING NUT

BACN10HR4CD 17 NUT

BACS40R008B051F 2 SHIM, LAMINATED

BACS40R008B055F 6 SHIM, LAMINATED

BACW10BP32CD 2 WASHER, PLAIN

BACW10BP32DP 2 WASHER

BACW10BP4CD 17 WASHER

BACW10BP4DP 17 WASHER

Group 1-5, 8-9, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-210

142U0103-61 1 ALUMINUM STRAP LEFT

142U0103-62 1 ALUMINUM STRAP RIGHT

142U0103-63 2 STEEL STRAP

142U0103-64 2 STEEL STRAP

142U0103-65 2 STEEL STRAP

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

112 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-5, 8-9, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-210

142U0103-66 2 FILLER

142U0104-3 4 TENSION TIE SPLICE

TENSION TIE STOCK

SEGMENT

144U0064-66 4

BACB30NX8K3 185 HI-LOK

BACB30NX8K4 58 HI-LOK

BACB30NX8K5 44 HI LOK

BACB30NX8K6 14 BOLT

BACB30NX8K7 29 BOLT, HEX DRIVE

BACB30US3K10Y 4 BOLT

BACB30US3K8Y 11 BOLT

BACB30US3K9Y 6 BOLT

BACC30BH8 328 COLLAR

BACN10HR3CD 21 SELF-LOCKING NUT

BACS40R008B052F 4 SHIM,LAMINATED

BACS40R008B053F 4 SHIM, LAMINATED

BACS40R018A031F 2 SHIM LAMINATED

BACS40R018A051F 2 SHIM, LAMINATED

BACW10BP32CD 21 WASHER, PLAIN

BACW10BP32DP 21 WASHER

Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-211

142U0103-67 1 ALUMINUM STRAP LEFT

142U0103-68 1 ALUMINUM STRAP RIGHT

142U0103-69 2 STEEL STRAP

142U0103-70 2 STEEL STRAP

142U0103-71 2 STEEL STRAP

142U0104-3 4 TENSION TIE SPLICE

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

113 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-211

TENSION TIE STOCK SEGMENT144U0064-66 4

BACB30NX8K3 104 HI-LOK

BACB30NX8K4 51 HI-LOK

BACB30NX8K5 44 HI LOK

BACB30NX8K6 18 BOLT

BACB30NX8K7 27 BOLT, HEX DRIVE

BACB30US4K7 4 BOLT, 12 PT HEAD

BACB30US4K8 4 BOLT, 12 PT HEAD

BACB30US4K9 14 BOLT, 12 PT HEAD

BACC30BH8 244 COLLAR

BACN10HR4CD 22 NUT

BACS40R008B054F 2 SHIM, LAMINATED

BACS40R008B058F 2 SHIM, LAMINATED

BACS40R008B059F 2 SHIM, LAMINATED

BACS40R008B064F 2 SHIM, LAMINATED

BACW10BP4CD 22 WASHER

BACW10BP4DP 22 WASHER

Group 1-5, 8-9, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-212

142U0103-72 2 FILLER

142U0103-73 1 ALUMINUM STRAP LEFT

142U0103-74 1 ALUMINUM STRAP RIGHT

142U0103-75 2 STEEL STRAP

142U0103-76 2 STEEL STRAP

142U0103-77 2 STEEL STRAP

142U0104-3 4 TENSION TIE SPLICE

142U0105-5 4 TENSION TIE SEGMENT

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

114 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-5, 8-9, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-212

BACB30NX8K3 117 HI-LOK

BACB30NX8K4 66 HI-LOK

BACB30NX8K5 49 HI LOK

BACB30NX8K6 14 BOLT

BACB30NX8K7 27 BOLT, HEX DRIVE

BACB30US4K10 2 BOLT, 12 PT HEAD

BACB30US4K11 2 BOLT, 12 PT HEAD

BACB30US4K12 8 BOLT, 12 PT HEAD

BACB30US4K13 4 BOLT, 12 PT HEAD

BACC30BH8 271 COLLAR

BACN10HR4CD 16 NUT

BACS40R008B052F 2 SHIM,LAMINATED

BACS40R008B053F 4 SHIM, LAMINATED

BACS40R008B054F 2 SHIM, LAMINATED

BACW10BP4CD 16 WASHER

BACW10BP4DP 16 WASHER

Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-213

142U0103-78 2 FILLER

142U0103-79 1 ALUMINUM STRAP LEFT

142U0103-80 1 ALUMINUM STRAP RIGHT

142U0103-81 2 STEEL STRAP

142U0103-82 2 STEEL STRAP

142U0103-83 2 STEEL STRAP

142U0104-3 4 TENSION TIE SPLICE

TENSION TIE STOCK SEGMENT144U0064-66 4

BACB30NX8K3 128 HI-LOK

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

115 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-213

BACB30NX8K4 51 HI-LOK

BACB30NX8K5 49 HI LOK

BACB30NX8K6 16 BOLT

BACB30NX8K7 27 BOLT, HEX DRIVE

BACB30US4K10 4 BOLT, 12 PT HEAD

BACB30US4K11 4 BOLT, 12 PT HEAD

BACB30US4K12 14 BOLT, 12 PT HEAD

BACC30BH8 271 COLLAR

BACN10HR4CD 22 NUT

BACS40R008B051F 6 SHIM, LAMINATED

BACS40R008B052F 2 SHIM,LAMINATED

BACW10BP4CD 22 WASHER

BACW10BP4DP 22 WASHER

Group 1-5, 8-9, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-214

142U0103-84 2 FILLER

142U0103-85 1 ALUMINUM STRAP LEFT

142U0103-86 1 ALUMINUM STRAP RIGHT

142U0103-87 2 STEEL STRAP

142U0103-88 2 STEEL STRAP

142U0103-89 2 STEEL STRAP

142U0104-3 4 TENSION TIE SPLICE

TENSION TIE STOCK

SEGMENT

144U0064-66 4

BACB30NX6K3 4 BOLT, PROTRUDING HD

BACB30NX8K3 112 HI-LOK

BACB30NX8K4 66 HI-LOK

BACB30NX8K5 49 HI LOK

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

116 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-5, 8-9, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-214

BACB30NX8K6 14 BOLT

BACB30NX8K7 27 BOLT, HEX DRIVE

BACB30US3K15 2 BOLT

BACB30US4K10 4 BOLT, 12 PT HEAD

BACB30US4K11 4 BOLT, 12 PT HEAD

BACB30US4K12 8 BOLT, 12 PT HEAD

BACC30BH6 4 COLLAR

BACC30BH8 266 COLLAR

BACN10HR3CD 2 SELF-LOCKING NUT

BACN10HR4CD 17 NUT

BACS40R008B050F . SHIM, LAMINATED

BACS40R008B051F 4 SHIM, LAMINATED

BACS40R008B052F 4 SHIM,LAMINATED

BACW10BP3CD 2 WASHER

BACW10BP3DP 2 WASHER

BACW10BP4CD 17 WASHER

BACW10BP4DP 17 WASHER

Group 6-7:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-215

142U0103-84 2 FILLER

142U0103-85 1 ALUMINUM STRAP LEFT

142U0103-86 1 ALUMINUM STRAP RIGHT

142U0103-87 2 STEEL STRAP

142U0103-88 2 STEEL STRAP

142U0103-89 2 STEEL STRAP

142U0104-3 4 TENSION TIE SPLICE

TENSION TIE STOCK SEGMENT144U0064-66 4

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

117 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 6-7:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-215

BACB30NX8K3 112 HI-LOK

BACB30NX8K4 66 HI-LOK

BACB30NX8K5 49 HI LOK

BACB30NX8K6 14 BOLT

BACB30NX8K7 27 BOLT, HEX DRIVE

BACB30US3K15 2 BOLT

BACB30US4K10 4 BOLT, 12 PT HEAD

BACB30US4K11 4 BOLT, 12 PT HEAD

BACB30US4K12 8 BOLT, 12 PT HEAD

BACC30BH8 266 COLLAR

BACN10HR3CD 2 SELF-LOCKING NUT

BACN10HR4CD 17 NUT

BACS40R008B050F 2 SHIM, LAMINATED

BACS40R008B051F 2 SHIM, LAMINATED

BACS40R008B053F 4 SHIM, LAMINATED

BACW10BP3CD 2 WASHER

BACW10BP3DP 2 WASHER

BACW10BP4CD 17 WASHER

BACW10BP4DP 17 WASHER

Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-216

142U0103-84 2 FILLER

142U0103-90 2 STEEL STRAP

142U0103-91 1 ALUMINUM STRAP LEFT

142U0103-92 1 ALUMINUM STRAP RIGHT

142U0103-93 2 STEEL STRAP

142U0103-94 2 STEEL STRAP

142U0104-3 4 TENSION TIE SPLICE

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

118 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-216

TENSION TIE STOCK SEGMENT144U0064-66 4

BACB30NX8K3 128 HI-LOK

BACB30NX8K4 47 HI-LOK

BACB30NX8K5 44 HI LOK

BACB30NX8K6 16 BOLT

BACB30NX8K7 29 BOLT, HEX DRIVE

BACB30US4K10 4 BOLT, 12 PT HEAD

BACB30US4K11 4 BOLT, 12 PT HEAD

BACB30US4K12 14 BOLT, 12 PT HEAD

BACC30BH8 264 COLLAR

BACN10HR4CD 22 NUT

BACS40R008B053F 6 SHIM, LAMINATED

BACS40R008B054F 2 SHIM, LAMINATED

BACW10BP4CD 22 WASHER

BACW10BP4DP 22 WASHER

Group 1-5, 8-9, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-217

142U0103-95 1 ALUMINUM STRAP LEFT

142U0103-96 1 ALUMINUM STRAP RIGHT

142U0103-97 2 STEEL STRAP

142U0103-98 2 STEEL STRAP

142U0103-99 2 STEEL STRAP

142U0103-100 2 FILLER

142U0104-3 4 TENSION TIE SPLICE

TENSION TIE STOCK

SEGMENT

144U0064-66 4

BACB30NX6K2 28 BOLT, PROTRUDING HD

BACB30NX6K3 3 BOLT, PROTRUDING HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

119 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-5, 8-9, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-217

BACB30NX6K5 4 BOLT

BACB30NX8K2 82 BOLT, PROTRUDING HD

BACB30NX8K3 83 HI-LOK

BACB30NX8K4 58 HI-LOK

BACB30NX8K5 18 HI LOK

BACB30NX8K6 14 BOLT

BACB30NX8K7 29 BOLT, HEX DRIVE

BACB30US4K11 4 BOLT, 12 PT HEAD

BACB30US4K12 4 BOLT, 12 PT HEAD

BACB30US4K13 14 BOLT, 12 PT HEAD

BACC30BH6 38 COLLAR

BACC30BH8 279 COLLAR

BACN10HR4CD 22 NUT

BACS40R008B052F 4 SHIM,LAMINATED

BACS40R008B053F 4 SHIM, LAMINATED

BACS40R008B054F 1 SHIM, LAMINATED

BACS40R018A031F 2 SHIM LAMINATED

BACS40R018A053F 2 SHIM, LAMINATED

BACW10BP4CD 22 WASHER

BACW10BP4DP 22 WASHER

Group 6-7:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-218

142U0103-95 1 ALUMINUM STRAP LEFT

142U0103-96 1 ALUMINUM STRAP RIGHT

142U0103-97 2 STEEL STRAP

142U0103-98 2 STEEL STRAP

142U0103-99 2 STEEL STRAP

142U0103-100 2 FILLER

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

120 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 6-7:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-218

142U0105-6 4 TENSION TIE SEGMENT

144U0063-32 4 TENSION TIE SPLICE

BACB30NX8K2 83 BOLT, PROTRUDING HD

BACB30NX8K3 51 HI-LOK

BACB30NX8K4 53 HI-LOK

BACB30NX8K5 18 HI LOK

BACB30NX8K6 14 BOLT

BACB30NX8K7 29 BOLT, HEX DRIVE

BACB30US4K11 4 BOLT, 12 PT HEAD

BACB30US4K12 4 BOLT, 12 PT HEAD

BACB30US4K13 14 BOLT, 12 PT HEAD

BACC30BH8 248 COLLAR

BACN10HR4CD 22 NUT

BACS40R008B052F 4 SHIM,LAMINATED

BACS40R008B053F 4 SHIM, LAMINATED

BACW10BP4CD 22 WASHER

BACW10BP4DP 22 WASHER

Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-219

142U0103-100 2 FILLER

142U0103-101 1 ALUMINUM STRAP LEFT

142U0103-102 1 ALUMINUM STRAP RIGHT

142U0103-103 2 STEEL STRAP

142U0103-104 2 STEEL STRAP

142U0103-105 2 STEEL STRAP

142U0104-1 4 TENSION TIE SPLICE

142U0105-4 4 TENSION TIE SEGMENT

BACB30NX8K3 124 HI-LOK

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

121 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-219

BACB30NX8K4 44 HI-LOK

BACB30NX8K5 42 HI LOK

BACB30NX8K6 14 BOLT

BACB30NX8K7 31 BOLT, HEX DRIVE

BACB30US3K16 2 BOLT

BACB30US4K11 4 BOLT, 12 PT HEAD

BACB30US4K12 4 BOLT, 12 PT HEAD

BACB30US4K13 11 BOLT, 12 PT HEAD

BACC30BH8 255 COLLAR

BACN10HR4CD 19 NUT

BACS40R011B051F 2 SHIM, LAMINATED

BACS40R011B055F 2 SHIM, LAMINATED

BACS40R011B057F 4 SHIM LAMINATED

BACW10BP3CD 2 WASHER

BACW10BP3DP 2 WASHER

BACW10BP4CD 19 WASHER

BACW10BP4DP 19 WASHER

Group 1-9, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-220

142U0103-106 2 FILLER

142U0103-107 1 ALUMINUM STRAP LEFT

142U0103-108 1 ALUMINUM STRAP RIGHT

142U0103-109 2 STEEL STRAP

142U0103-110 2 STEEL STRAP

142U0103-111 2 STEEL STRAP

142U0104-3 4 TENSION TIE SPLICE

142U0105-7 2 FITTING

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

122 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-9, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-220

TENSION TIE STOCK SEGMENT144U0064-66 4

BACB30NX6K2 8 BOLT, PROTRUDING HD

BACB30NX8K2 93 BOLT, PROTRUDING HD

BACB30NX8K3 84 HI-LOK

BACB30NX8K4 59 HI-LOK

BACB30NX8K5 8 HI LOK

BACB30NX8K6 8 BOLT

BACB30NX8K7 29 BOLT, HEX DRIVE

BACB30NX8K8 8 BOLT

BACB30US3K12 2 BOLT, 12 PT HEAD

BACB30US4K10 2 BOLT, 12 PT HEAD

BACB30US4K11 2 BOLT, 12 PT HEAD

BACB30US4K12 14 BOLT, 12 PT HEAD

BACC30BH6 8 COLLAR

BACC30BH8 290 COLLAR

BACF3H06LC007HN 4 FILLER, RECTANGULAR

BACN10HR3CD 2 SELF-LOCKING NUT

BACN10HR4CD 18 NUT

BACS40R008B008F 2 SHIM,LAMINATED

BACS40R008B052F 4 SHIM,LAMINATED

BACS40R008B053F 4 SHIM, LAMINATED

BACS40R018A031F 2 SHIM LAMINATED

BACW10BP3CD 2 WASHER

BACW10BP3DP 2 WASHER

BACW10BP4CD 18 WASHER

BACW10BP4DP 18 WASHER

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

123 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-221

142U0103-106 2 FILLER

142U0103-112 2 STEEL STRAP

142U0103-113 1 ALUMINUM STRAP LEFT

142U0103-114 1 ALUMINUM STRAP RIGHT

142U0103-115 2 STEEL STRAP

142U0103-116 2 STEEL STRAP

142U0104-1 4 TENSION TIE SPLICE

142U0105-4 4 TENSION TIE SEGMENT

BACB30NX8K3 119 HI-LOK

BACB30NX8K4 42 HI-LOK

BACB30NX8K5 44 HI LOK

BACB30NX8K6 16 BOLT

BACB30NX8K7 29 BOLT, HEX DRIVE

BACB30US3K15 6 BOLT

BACB30US4K10 4 BOLT, 12 PT HEAD

BACB30US4K11 2 BOLT, 12 PT HEAD

BACB30US4K12 6 BOLT, 12 PT HEAD

BACC30BH8 250 COLLAR

BACN10HR3CD 6 SELF-LOCKING NUT

BACN10HR4CD 14 NUT

BACS40R011B053F 8 SHIM, LAMINATED

BACW10BP3CD 6 WASHER

BACW10BP3DP 6 WASHER

BACW10BP4CD 14 WASHER

BACW10BP4DP 14 WASHER

Group 1-4, 6, 8, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-222

142U0103-117 1 ALUMINUM STRAP LEFT

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

124 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-4, 6, 8, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-222

142U0103-118 1 ALUMINUM STRAP RIGHT

142U0103-119 2 STEEL STRAP

142U0103-120 2 STEEL STRAP

142U0103-121 2 STEEL STRAP

142U0103-122 2 FILLER

142U0104-3 4 TENSION TIE SPLICE

142U0105-7 2 FITTING

TENSION TIE STOCK SEGMENT144U0064-66 4

BACB30NX6K2 25 BOLT, PROTRUDING HD

BACB30NX8K2 8 BOLT, PROTRUDING HD

BACB30NX8K3 137 HI-LOK

BACB30NX8K4 57 HI-LOK

BACB30NX8K5 44 HI LOK

BACB30NX8K6 14 BOLT

BACB30NX8K7 37 BOLT, HEX DRIVE

BACB30US4K11 4 BOLT, 12 PT HEAD

BACB30US4K12 4 BOLT, 12 PT HEAD

BACB30US4K13 14 BOLT, 12 PT HEAD

BACC30BH6 25 COLLAR

BACC30BH8 297 COLLAR

BACF3H06LC007HN 4 FILLER, RECTANGULAR

BACN10HR4CD 22 NUT

BACS40R008B008F 2 SHIM,LAMINATED

BACS40R008B051F 8 SHIM, LAMINATED

BACW10BP4CD 22 WASHER

BACW10BP4DP 22 WASHER

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

125 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 5, 7, 9:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-223

142U0103-122 2 FILLER

142U0103-123 1 ALUMINUM STRAP LEFT

142U0103-124 1 ALUMINUM STRAP RIGHT

142U0103-125 2 STEEL STRAP

142U0103-126 2 STEEL STRAP

142U0103-127 2 STEEL STRAP

142U0104-3 4 TENSION TIE SPLICE

TENSION TIE STOCK SEGMENT144U0064-66 4

BACB30NX6K2 18 BOLT, PROTRUDING HD

BACB30NX8K2 8 BOLT, PROTRUDING HD

BACB30NX8K3 115 HI-LOK

BACB30NX8K4 49 HI-LOK

BACB30NX8K5 36 HI LOK

BACB30NX8K6 4 BOLT

BACB30NX8K7 29 BOLT, HEX DRIVE

BACB30US3K16 2 BOLT

BACB30US4K11 4 BOLT, 12 PT HEAD

BACB30US4K12 4 BOLT, 12 PT HEAD

BACB30US4K13 8 BOLT, 12 PT HEAD

BACC30BH6 18 COLLAR

BACC30BH8 241 COLLAR

BACN10HR3CD 2 SELF-LOCKING NUT

BACN10HR4CD 18 NUT

BACS40R008B051F 4 SHIM, LAMINATED

BACS40R008B052F 4 SHIM,LAMINATED

BACW10BP3CD 2 WASHER

BACW10BP3DP 2 WASHER

BACW10BP4CD 18 WASHER

BACW10BP4DP 18 WASHER

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

126 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-224

142U0103-122 2 FILLER

142U0103-128 2 STEEL STRAP

142U0103-129 1 ALUMINUM STRAP LEFT

142U0103-130 1 ALUMINUM STRAP RIGHT

142U0103-131 2 STEEL STRAP

142U0103-132 2 STEEL STRAP

142U0104-1 4 TENSION TIE SPLICE

142U0105-4 4 TENSION TIE SEGMENT

BACB30NX8K3 124 HI-LOK

BACB30NX8K4 42 HI-LOK

BACB30NX8K5 40 HI LOK

BACB30NX8K6 11 BOLT

BACB30NX8K7 29 BOLT, HEX DRIVE

BACB30US3K14 2 BOLT, 12 PT HEAD

BACB30US3K15 2 BOLT

BACB30US4K11 2 BOLT, 12 PT HEAD

BACB30US4K12 2 BOLT, 12 PT HEAD

BACB30US4K13 11 BOLT, 12 PT HEAD

BACC30BH8 246 COLLAR

BACN10HR3CD 4 SELF-LOCKING NUT

BACN10HR4CD 16 NUT

BACS40R011B052F 2 SHIM, LAMINATED

BACS40R011B053F 4 SHIM, LAMINATED

BACS40R011B054F 2 SHIM, LAMINATED

BACW10BP3CD 4 WASHER

BACW10BP3DP 4 WASHER

BACW10BP4CD 16 WASHER

BACW10BP4DP 16 WASHER

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

127 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-4, 6, 8, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-225

142U0103-133 1 ALUMINUM STRAP LEFT

142U0103-134 1 ALUMINUM STRAP RIGHT

142U0103-135 2 STEEL STRAP

142U0103-136 2 STEEL STRAP

142U0103-137 2 STEEL STRAP

142U0103-138 2 FILLER

142U0104-3 4 TENSION TIE SPLICE

TENSION TIE STOCK SEGMENT144U0064-66 4

BACB30NX6K3 3 BOLT, PROTRUDING HD

BACB30NX6K4 15 BOLT, PROTRUDING HD

BACB30NX6K5 2 BOLT

BACB30NX6K7 4 HI-LOK

BACB30NX8K2 4 BOLT, PROTRUDING HD

BACB30NX8K3 137 HI-LOK

BACB30NX8K4 44 HI-LOK

BACB30NX8K5 42 HI LOK

BACB30NX8K6 4 BOLT

BACB30NX8K7 33 BOLT, HEX DRIVE

BACB30US3K10 6 BOLT, 12 PT HEAD

BACB30US4K11 4 BOLT, 12 PT HEAD

BACB30US4K12 13 BOLT, 12 PT HEAD

BACC30BH6 24 COLLAR

BACC30BH8 264 COLLAR

BACN10HR3CD 6 SELF-LOCKING NUT

BACN10HR4CD 17 NUT

BACS40R008B050F 2 SHIM, LAMINATED

BACS40R008B051F 4 SHIM, LAMINATED

BACS40R008B052F 4 SHIM,LAMINATED

BACW10BP3CD 6 WASHER

BACW10BP3DP 6 WASHER

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

128 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-4, 6, 8, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-225

BACW10BP4CD 17 WASHER

BACW10BP4DP 17 WASHER

Group 5, 7, 9:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-226

142U0103-138 2 FILLER

142U0103-139 1 ALUMINUM STRAP LEFT

142U0103-140 1 ALUMINUM STRAP RIGHT

142U0103-141 2 STEEL STRAP

142U0103-142 2 STEEL STRAP

142U0103-143 2 STEEL STRAP

142U0104-3 4 TENSION TIE SPLICE

TENSION TIE STOCK

SEGMENT

144U0064-66 4

BACB30NX6K3 2 BOLT, PROTRUDING HD

BACB30NX6K4 14 BOLT, PROTRUDING HD

BACB30NX8K3 134 HI-LOK

BACB30NX8K4 49 HI-LOK

BACB30NX8K5 44 HI LOK

BACB30NX8K6 8 BOLT

BACB30NX8K7 29 BOLT, HEX DRIVE

BACB30US3K10 6 BOLT, 12 PT HEAD

BACB30US4K11 4 BOLT, 12 PT HEAD

BACB30US4K12 14 BOLT, 12 PT HEAD

BACC30BH6 16 COLLAR

BACC30BH8 262 COLLAR

BACN10HR3CD 6 SELF-LOCKING NUT

BACN10HR4CD 17 NUT

BACS40R008B046F 2 SHIM, LAMINATED

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

129 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 5, 7, 9:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-226

BACS40R008B047F 2 SHIM, LAMINATED

BACS40R008B049F 2 SHIM - LAMINATED

BACS40R008B053F 2 SHIM, LAMINATED

BACW10BP3CD 6 WASHER

BACW10BP3DP 6 WASHER

BACW10BP4CD 17 WASHER

BACW10BP4DP 17 WASHER

Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-227

142U0103-138 2 FILLER

142U0103-144 2 STEEL STRAP

142U0103-145 1 ALUMINUM STRAP LEFT

142U0103-146 1 ALUMINUM STRAP RIGHT

142U0103-147 2 STEEL STRAP

142U0103-148 2 STEEL STRAP

142U0104-1 4 TENSION TIE SPLICE

142U0105-4 4 TENSION TIE SEGMENT

BACB30NX8K3 124 HI-LOK

BACB30NX8K4 38 HI-LOK

BACB30NX8K5 36 HI LOK

BACB30NX8K6 6 BOLT

BACB30NX8K7 29 BOLT, HEX DRIVE

BACB30US3K10 4 BOLT, 12 PT HEAD

BACB30US3K13 2 BOLT

BACB30US4K11 4 BOLT, 12 PT HEAD

BACB30US4K12 14 BOLT, 12 PT HEAD

BACC30BH8 233 COLLAR

BACN10HR3CD 6 SELF-LOCKING NUT

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

130 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-227

BACN10HR4CD 17 NUT

BACS40R011B054F 6 SHIM, LAMINATED

BACS40R011B055F 2 SHIM, LAMINATED

BACW10BP3CD 6 WASHER

BACW10BP3DP 6 WASHER

BACW10BP4CD 17 WASHER

BACW10BP4DP 17 WASHER

Group 8:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-228

142U0103-149 1 ALUMINUM STRAP LEFT

142U0103-150 1 ALUMINUM STRAP RIGHT

142U0103-151 2 STEEL STRAP

142U0103-152 2 STEEL STRAP

142U0103-153 2 STEEL STRAP

FILLER BETWEEN CLIPS

OF CREASE

142U0103-154 2

FILLER BETWEEN TT

AND FRAME

142U0103-155 2

142U0104-3 4 TENSION TIE SPLICE

142U0104-5 1 BEAM

142U0104-6 1 BEAM

142U0104-7 1 CLIP

142U0104-8 1 CLIP

142U0104-11 1 CHANNEL SEGMENT

142U0104-12 1 CHANNEL SEGMENT

144U0063-123 2 SPLICE CHANNEL

TENSION TIE STOCK

SEGMENT

144U0064-66 4

BACB30NW6K5 6 BOLT, HILOK

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

131 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 8:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-228

BACB30NX6K20X 2 BOLT, PROTRUDING HD

BACB30NX6K2Y 49 BOLT, HEX DRIVE

BACB30NX6K3 6 BOLT, PROTRUDING HD

BACB30NX6K3X 8 BOLT, PROTRUDING HD

BACB30NX6K3Y 95 BOLT, PROTRUDING HD

BACB30NX6K4 49 BOLT, PROTRUDING HD

BACB30NX6K5 24 BOLT

BACB30NX6K5Y 8 BOLT, PROTRUDING HD

BACB30NX6K6 4 BOLT

BACB30NX6K7 6 HI-LOK

BACB30NX8K2 86 BOLT, PROTRUDING HD

BACB30NX8K3 93 HI-LOK

BACB30NX8K4 66 HI-LOK

BACB30NX8K5 36 HI LOK

BACB30NX8K6 4 BOLT

BACB30NX8K7 29 BOLT, HEX DRIVE

BACB30US3K10 2 BOLT, 12 PT HEAD

BACB30US3K11 4 BOLT, 12 PT HEAD

BACB30US3K13 2 BOLT

BACB30US4K12 14 BOLT, 12 PT HEAD

BACB30US4K13 2 BOLT, 12 PT HEAD

BACC30AC6 174 COLLAR

BACC30BH6 91 COLLAR

BACC30BH8 314 COLLAR

BACC30M6 18 COLLAR

BACN10HR3CD 8 SELF-LOCKING NUT

BACN10HR4CD 16 NUT

BACS40R008B052F 2 SHIM,LAMINATED

BACS40R008B053F 2 SHIM, LAMINATED

BACS40R008B054F 2 SHIM, LAMINATED

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

132 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 8:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-228

BACS40R008B055F 2 SHIM, LAMINATED

BACW10BP3CD 8 WASHER

BACW10BP3DP 8 WASHER

BACW10BP4CD 16 WASHER

BACW10BP4DP 16 WASHER

Group 3-4, 6, 12:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-229

FILLER BETWEEN CLIPS

OF CREASE

142U0103-154 2

FILLER BETWEEN TT AND

FRAME

142U0103-155 2

142U0103-156 2 STEEL STRAP

142U0103-157 1 ALUMINUM STRAP LEFT

142U0103-158 1 ALUMINUM STRAP RIGHT

142U0103-159 2 STEEL STRAP

142U0103-160 2 STEEL STRAP

142U0104-3 4 TENSION TIE SPLICE

142U0104-13 1 CHANNEL SEGMENT

142U0104-14 1 CHANNEL SEGMENT

142U0104-15 1 BEAM

142U0104-16 1 BEAM

142U0104-17 1 CLIP

142U0104-18 1 CLIP

142U0105-3 2 BRACKET

144U0063-123 2 SPLICE CHANNEL

TENSION TIE STOCK SEGMENT144U0064-66 4

BACB30NW6K5 6 BOLT, HILOK

BACB30NW6K7 2 BOLT

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

133 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 3-4, 6, 12:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-229

BACB30NW6K8 2 HI-LOK

BACB30NX6K20X 2 BOLT, PROTRUDING HD

BACB30NX6K2Y 58 BOLT, HEX DRIVE

BACB30NX6K3 16 BOLT, PROTRUDING HD

BACB30NX6K3X 8 BOLT, PROTRUDING HD

BACB30NX6K3Y 95 BOLT, PROTRUDING HD

BACB30NX6K4 42 BOLT, PROTRUDING HD

BACB30NX6K5 20 BOLT

BACB30NX6K5Y 31 BOLT, PROTRUDING HD

BACB30NX6K6 6 BOLT

BACB30NX8K2 62 BOLT, PROTRUDING HD

BACB30NX8K3 93 HI-LOK

BACB30NX8K4 80 HI-LOK

BACB30NX8K5 36 HI LOK

BACB30NX8K6 11 BOLT

BACB30NX8K7 29 BOLT, HEX DRIVE

BACB30US3K10 6 BOLT, 12 PT HEAD

BACB30US3K14 2 BOLT, 12 PT HEAD

BACB30US3K15 2 BOLT

BACB30US4K11 4 BOLT, 12 PT HEAD

BACB30US4K12 6 BOLT, 12 PT HEAD

BACB30US4K13 2 BOLT, 12 PT HEAD

BACC30AC6 183 COLLAR

BACC30BH6 84 COLLAR

BACC30BH8 311 COLLAR

BACC30BL6 6 COLLAR

BACC30M6 22 COLLAR

BACN10HR3CD 11 SELF-LOCKING NUT

BACN10HR4CD 13 NUT

BACS40R008B051F 2 SHIM, LAMINATED

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

134 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 3-4, 6, 12:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-229

BACS40R008B053F 4 SHIM, LAMINATED

BACS40R008B054F 2 SHIM, LAMINATED

BACW10BP3CD 11 WASHER

BACW10BP3DP 11 WASHER

BACW10BP4CD 13 WASHER

BACW10BP4DP 13 WASHER

BACW10P168L 22 WASHER, PLAIN

BACW10P4L 8 WASHER, PLAIN

Group 5, 7, 9:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-230

142U0103-161 1 ALUMINUM STRAP LEFT

142U0103-162 1 ALUMINUM STRAP RIGHT

142U0103-163 2 STEEL STRAP

142U0103-164 2 STEEL STRAP

142U0103-165 2 STEEL STRAP

FILLER BETWEEN TT AND

FRAME

142U0103-166 2

142U0104-3 4 TENSION TIE SPLICE

142U0104-19 1 CHANNEL SEGMENT

142U0104-20 1 CHANNEL SEGMENT

142U0105-3 2 BRACKET

142U0105-4 . TENSION TIE SEGMENT

144U0063-123 2 SPLICE CHANNEL

TENSION TIE STOCK SEGMENT144U0064-66 4

BACB30NX6K2Y 8 BOLT, HEX DRIVE

BACB30NX6K3 8 BOLT, PROTRUDING HD

BACB30NX6K5Y 22 BOLT, PROTRUDING HD

BACB30NX8K2 77 BOLT, PROTRUDING HD

BOEING PROPRIETARY -

Copyright © Unpublished Work - See page 1 for details.

Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

135 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 5, 7, 9:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-230

BACB30NX8K3 97 HI-LOK

BACB30NX8K4 75 HI-LOK

BACB30NX8K5 36 HI LOK

BACB30NX8K6 14 BOLT

BACB30NX8K7 38 BOLT, HEX DRIVE

BACB30US3K10 6 BOLT, 12 PT HEAD

BACB30US4K11 11 BOLT, 12 PT HEAD

BACB30US4K12 6 BOLT, 12 PT HEAD

BACC30AC6 30 COLLAR

BACC30BH6 8 COLLAR

BACC30BH8 337 COLLAR

BACN10HR3CD 6 SELF-LOCKING NUT

BACN10HR4CD 18 NUT

BACR15BA5B4C 8 RIVET, 100 DEG

BACS40R008B052F 2 SHIM,LAMINATED

BACS40R008B054F 2 SHIM, LAMINATED

BACS40R008B056F 4 SHIM, LAMINATED

BACW10BP3CD 6 WASHER

BACW10BP3DP 6 WASHER

BACW10BP4CD 18 WASHER

BACW10BP4DP 18 WASHER

BACW10P168L 22 WASHER, PLAIN

BACW10P4L 8 WASHER, PLAIN

Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-231

FILLER BETWEEN TT AND

FRAME

142U0103-166 2

142U0103-167 1 ALUMINUM STRAP LEFT

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136 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-231

142U0103-168 1 ALUMINUM STRAP RIGHT

142U0103-169 2 STEEL STRAP

142U0103-170 2 STEEL STRAP

142U0103-171 2 STEEL STRAP

142U0104-1 4 TENSION TIE SPLICE

142U0104-21 1 CHANNEL SEGMENT

142U0104-22 1 CHANNEL SEGMENT

142U0104-23 2 SPLICE CHANNEL

142U0105-4 4 TENSION TIE SEGMENT

BACB30NX8K2 86 BOLT, PROTRUDING HD

BACB30NX8K3 110 HI-LOK

BACB30NX8K4 82 HI-LOK

BACB30NX8K5 36 HI LOK

BACB30NX8K6 6 BOLT

BACB30NX8K7 29 BOLT, HEX DRIVE

BACB30US3K10 6 BOLT, 12 PT HEAD

BACB30US4K11 6 BOLT, 12 PT HEAD

BACB30US4K12 11 BOLT, 12 PT HEAD

BACC30BH8 349 COLLAR

BACN10HR3CD 6 SELF-LOCKING NUT

BACN10HR4CD 17 NUT

BACS40R011B053F 6 SHIM, LAMINATED

BACS40R011B055F 2 SHIM, LAMINATED

BACW10BP3CD 6 WASHER

BACW10BP3DP 6 WASHER

BACW10BP4CD 17 WASHER

BACW10BP4DP 17 WASHER

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Copyright © Unpublished Work - See page 1 for details.

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137 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 13-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-232

142U0103-149 1 ALUMINUM STRAP LEFT

142U0103-150 1 ALUMINUM STRAP RIGHT

142U0103-151 2 STEEL STRAP

142U0103-152 2 STEEL STRAP

FILLER BETWEEN CLIPS OF

CREASE

142U0103-154 2

FILLER BETWEEN TT AND

FRAME

142U0103-155 2

142U0103-172 2 STEEL STRAP

142U0104-3 4 TENSION TIE SPLICE

142U0104-9 1 CLIP

142U0104-10 1 CLIP

142U0104-11 1 CHANNEL SEGMENT

142U0104-12 1 CHANNEL SEGMENT

142U0105-3 2 BRACKET

144U0063-123 2 SPLICE CHANNEL

TENSION TIE STOCK SEGMENT144U0064-66 4

BACB30NW6K5 2 BOLT, HILOK

BACB30NX6K3 11 BOLT, PROTRUDING HD

BACB30NX6K3Y 4 BOLT, PROTRUDING HD

BACB30NX6K4 51 BOLT, PROTRUDING HD

BACB30NX6K5 18 BOLT

BACB30NX6K5Y 22 BOLT, PROTRUDING HD

BACB30NX6K6 2 BOLT

BACB30NX6K7 6 HI-LOK

BACB30NX8K2 53 BOLT, PROTRUDING HD

BACB30NX8K3 93 HI-LOK

BACB30NX8K4 75 HI-LOK

BACB30NX8K5 36 HI LOK

BACB30NX8K6 6 BOLT

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138 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 13-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-232

BACB30NX8K7 29 BOLT, HEX DRIVE

BACB30US3K10 2 BOLT, 12 PT HEAD

BACB30US3K11 4 BOLT, 12 PT HEAD

BACB30US3K13 2 BOLT

BACB30US4K11 2 BOLT, 12 PT HEAD

BACB30US4K12 14 BOLT, 12 PT HEAD

BACB30VT6K5 16 BOLT

BACC30AC6 26 COLLAR

BACC30BH6 88 COLLAR

BACC30BH8 292 COLLAR

BACC30BL6 16 COLLAR

BACC30M6 2 COLLAR

BACN10HR3CD 8 SELF-LOCKING NUT

BACN10HR4CD 16 NUT

BACS40R008B052F 2 SHIM,LAMINATED

BACS40R008B053F 2 SHIM, LAMINATED

BACS40R008B054F 2 SHIM, LAMINATED

BACS40R008B055F 2 SHIM, LAMINATED

BACW10BP3CD 8 WASHER

BACW10BP3DP 8 WASHER

BACW10BP4CD 16 WASHER

BACW10BP4DP 16 WASHER

BACW10P168L 22 WASHER, PLAIN

BACW10P4L 8 WASHER, PLAIN

Group 1-2, 11:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-233

142U0103-149 1 ALUMINUM STRAP LEFT

142U0103-150 1 ALUMINUM STRAP RIGHT

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139 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-2, 11:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-233

142U0103-151 2 STEEL STRAP

142U0103-152 2 STEEL STRAP

142U0103-153 2 STEEL STRAP

FILLER BETWEEN CLIPS OF

CREASE

142U0103-154 2

FILLER BETWEEN TT AND

FRAME

142U0103-155 2

142U0104-3 4 TENSION TIE SPLICE

142U0104-5 1 BEAM

142U0104-6 1 BEAM

142U0104-7 1 CLIP

142U0104-8 1 CLIP

142U0104-11 1 CHANNEL SEGMENT

142U0104-12 1 CHANNEL SEGMENT

142U0105-3 2 BRACKET

144U0063-123 2 SPLICE CHANNEL

TENSION TIE STOCK SEGMENT144U0064-66 4

BACB30NW6K5 6 BOLT, HILOK

BACB30NX6K20X 2 BOLT, PROTRUDING HD

BACB30NX6K2Y 49 BOLT, HEX DRIVE

BACB30NX6K3 16 BOLT, PROTRUDING HD

BACB30NX6K3X 8 BOLT, PROTRUDING HD

BACB30NX6K3Y 95 BOLT, PROTRUDING HD

BACB30NX6K4 49 BOLT, PROTRUDING HD

BACB30NX6K5 24 BOLT

BACB30NX6K5Y 31 BOLT, PROTRUDING HD

BACB30NX6K6 4 BOLT

BACB30NX6K7 6 HI-LOK

BACB30NX8K2 53 BOLT, PROTRUDING HD

BACB30NX8K3 93 HI-LOK

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Original Issue: October 08, 2009

Revision 1: May 27, 2010 747-53A2605

140 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-2, 11:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-233

BACB30NX8K4 75 HI-LOK

BACB30NX8K5 36 HI LOK

BACB30NX8K6 6 BOLT

BACB30NX8K7 29 BOLT, HEX DRIVE

BACB30US3K10 2 BOLT, 12 PT HEAD

BACB30US3K11 4 BOLT, 12 PT HEAD

BACB30US3K13 2 BOLT

BACB30US4K12 14 BOLT, 12 PT HEAD

BACB30US4K13 2 BOLT, 12 PT HEAD

BACC30AC6 174 COLLAR

BACC30BH6 98 COLLAR

BACC30BH8 290 COLLAR

BACC30M6 18 COLLAR

BACN10HR3CD 8 SELF-LOCKING NUT

BACN10HR4CD 16 NUT

BACS40R008B052F 2 SHIM,LAMINATED

BACS40R008B053F 2 SHIM, LAMINATED

BACS40R008B054F 2 SHIM, LAMINATED

BACS40R008B055F 2 SHIM, LAMINATED

BACW10BP3CD 8 WASHER

BACW10BP3DP 8 WASHER

BACW10BP4CD 16 WASHER

BACW10BP4DP 16 WASHER

BACW10P168L 22 WASHER, PLAIN

BACW10P4L 8 WASHER, PLAIN

Group 1-5, 8-9, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-301

142U0104-40 2 ANGLE

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141 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 1-5, 8-9, 11-15:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-301

142U0104-41 1 SHEAR PANEL

142U0104-42 1 SHEAR PANEL

142U0104-43 1 PANEL TIE

142U0104-44 1 PANEL TIE

142U0104-45 1 CHANNEL

142U0104-46 1 CHANNEL

142U0104-47 1 CLIP

142U0104-48 1 CLIP

BACB30NX6K2 258 BOLT, PROTRUDING HD

BACB30NX6K3 8 BOLT, PROTRUDING HD

BACB30NX6K5 6 BOLT

BACB30NX6K6 2 BOLT

BACB30NX6K9 6 BOLT

BACB30NX8K2 20 BOLT, PROTRUDING HD

BACB30NX8K3 49 HI-LOK

BACB30NX8K4 4 HI-LOK

BACC30BH6 280 COLLAR

BACC30BH8 75 COLLAR

BACF3F008L015NN 2 FLAT FILLER

Group 6-7:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-302

142U0104-28 2 ANGLE

142U0104-29 1 SHEAR WEB

142U0104-30 1 SHEAR WEB

142U0104-31 1 PANEL TIE

142U0104-32 1 PANEL TIE

142U0104-33 1 CHANNEL

142U0104-34 1 CHANNEL

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142 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 6-7:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-302

142U0104-35 1 ANGLE

142U0104-36 1 ANGLE

142U0104-37 2 ANGLE

142U0104-38 2 ANGLE

142U0104-39 2 ANGLE

BACB30NX6K12 8 BOLT, PROTRUDING HD

BACB30NX6K2 249 BOLT, PROTRUDING HD

BACB30NX6K3 60 BOLT, PROTRUDING HD

BACB30NX6K4 6 BOLT, PROTRUDING HD

BACB30NX6K5 10 BOLT

BACB30NX6K6 4 BOLT

BACB30NX8K2 14 BOLT, PROTRUDING HD

BACB30NX8K3 44 HI-LOK

BACB30NX8K4 2 HI-LOK

BACB30NX8K6 2 BOLT

BACB30NX8K7 2 BOLT, HEX DRIVE

BACC30BH6 339 COLLAR

BACC30BH8 66 COLLAR

BACF3F010L028NN 2 FILLER

BACF3H38RP010HN 2 FILLER, RECTANGULAR

BACF3T01E10-08 2 FILLER,TAPERED

BACF3T01F86-08 2 FILLER, TAPERED

BACF3T02C88-08 2 FILLER, TAPERED

BACF3T02E10-09 4 FILLER, TAPERED

BACF3T05E88-08 2 FILLER, TAPERED

BACF3T10M78-08 2 FILLER, TAPERED

BACF3T14M24-08 2 FILLER, TAPERED

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Original Issue: October 08, 2009

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143 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
Group 10:

Kit 142U0102

Existing Part Notes

Number

New Part Number QTY Name

-303

140U0072U1 1 CHANNEL-DETAIL

140U0072U2 1 CHANNEL-DETAIL

142U1023U142 2 STIFFENER

142U1023U153 1 SHEAR PLATE

142U1023U154 1 SHEAR PLATE

142U1023U155 1 GUSSET

142U1023U156 1 GUSSET

142U1023U157 1 GUSSET

142U1023U158 1 GUSSET

142U1023U159 1 SHEAR PANEL

142U1023U160 1 SHEAR PANEL

142U1023U161 1 CHANNEL

142U1023U162 1 CHANNEL

142U1023U165 2 GUSSET

142U1023U166 2 GUSSET

BACB30NX6K2 169 BOLT, PROTRUDING HD

BACB30NX6K2Y 35 BOLT, HEX DRIVE

BACB30NX6K3 37 BOLT, PROTRUDING HD

BACB30NX6K3X 13 BOLT, PROTRUDING HD

BACB30NX6K4 4 BOLT, PROTRUDING HD

BACB30NX6K4X 18 BOLT, PROTRUDING HD

BACB30NX8K2 19 BOLT, PROTRUDING HD

BACB30NX8K3 46 HI-LOK

BACB30NX8K4 2 HI-LOK

BACB30NX8K5 4 HI LOK

BACC30AC6 35 COLLAR

BACC30BH6 241 COLLAR

BACC30BH8 71 COLLAR

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144 of 158

BOEING SERVICE BULLETIN 747-53A2605

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

Part Number / Speci- QTY Name Notes

fication

as re- Chemical Conversion Coating (a) (b)

quired

Alodine

as re- Primer (b)

quired

BMS 10-11, Type I

as re- Corrosion Inhibiting Compound (b)

quired

BMS 3-23, Type II

as re- Sealant (b)

quired

BMS 5-95

as re- Cadmium Plating - Brush (b)

quired

BAC5849

as re- Raw Material - Filler (c)

quired

7075-T6 Clad Sheet

(QQ-A-250/13)

Optional to 7075-T6 Clad

Sheet

as re- Raw Material - Filler

quired

2024-T3 Clad Sheet

(QQ-A-250/5)

(a) Refer to SOPM 20-43-03 for material alternatives.

(b) See the Qualified Products List at the end of the Boeing Material Specification (BMS) for supplier data.

(c) During installation of new frame parts, it may be necessary to install radius fillers at some fastener locations. If necessary, fabricate radius fillers from 7075-T6 Clad sheet per QQ-A-250/13

or 2024-T3 Clad sheet per QQ-A-250/5. See instructions in Frame installation drawings for

details.

3. Parts Modified and Reidentified:

None.

4. Parts Removed and Not Replaced:

None.

D. Parts Necessary to Change Spares

None.

E. Special Tooling - Price and Availability

The 747 Structural Repair Manual Subject 747-100/200/300 SRM 51-30-09, 747-400 SRM 51-40-09,

or 747-400F SRM 51-40-09 gives data about cold working tools and sleeves necessary to do the work

given in this service bulletin. These tools are available from industry sources.

Engineering, service, and a kit of cold working tools made for this change are available from Fatigue

Technology, Inc. or West Coast Industries, Inc.

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145 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
— Refer To:

FTI Kit Number: FTI-747-53A2605-1 Fatigue Technology, Inc. P.O. Box C-88388 Seattle, WA

98188 USA Phone Number (206) 246-2010 Fax (206) 244-9886

— Refer To:

WCI Kit Number: WCI-747-53A-2605 West Coast Industries, Inc. 14900 Whitman Avenue North

Seattle, WA 98133-6532 USA Phone Number (206) 365-7513 Fax (206) 365-7483

F. Special Tooling Necessary to do this Service Bulletin

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

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

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

Cold working tools are necessary to do the change given in this service bulletin. To get the cold working

tools, refer to Paragraph 2.E, Special Tooling - Price and Availability.

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146 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
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 give the recommended

sequence of steps. The sequence of steps to do this service bulletin can be changed.

Operators may perform the modification steps in a different sequence as long as the

tension ties are disconnected using an allowable method. Refer to Appendix A.

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 are in 747 SRM, Chapter 51

— Torque limits to tighten nuts and bolts are in 747 SRM, Chapter 51.

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

747 SRM, Chapter 51 and Boeing Drawing 012W6100. Alternate fasteners are also

listed in 747 SRM, Chapter 51 and Boeing Drawing 012W6100.

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

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.

7. 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.

8. These work instructions refer to procedures included on 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.

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147 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
9. If any of the existing frames or tension ties already have a repair installed which

prevents the modification given in this service bulletin, contact Boeing for instructions

before you accomplish the modification at the affected frame station.

10. Do not remove fasteners from all Tension Tie to Frame joints at the same time. Refer

to Appendix A for allowable methods to disconnect the Tension Ties.

11. Refer to SOPM 20-41-01 for explanations of Boeing finish codes.

B. WORK INSTRUCTIONS

Access

1. Remove electrical power and ground the airplane. Refer to 747-100/200/300 AMM 24-22-00 or

747-400 AMM 24-22-00 as accepted procedures.

2. Get access to the tension ties and frames as follows:

a. Remove/keep seats as necessary between STA 720 and STA 940. Refer to 747-100/200/300

AMM 25-25-01 or 747-400 AMM 25-25-01 as accepted procedures.

b. Remove/keep main deck ceiling panels as necessary between STA 720 and STA 940. Refer

to 747-100/200/300 AMM 25-22-01 or 747-400 AMM 25-22-01 as accepted procedures.

c. Remove/keep insulation as necessary between STA 720 and STA 940. Refer to

747-100/200/300 AMM 25-21-04 or 747-400 AMM 25-21-04 as accepted procedures.

Part 1: Modification

1. Remove existing shear panels as follows:

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BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
a. Group 1-5, 8-9, 11-15:

Remove left and right side shear panels between STA 820 and 840 in accordance with Drawing

142U0102-301, Sheet 33.

b. Group 6-7:

Remove left and right side shear panels between STA 840 and 860 in accordance with Drawing

142U0102-302, Sheet 34.

c. Group 10:

Remove left and right side shear panels between STA 780 and 800 in accordance with Drawing

142U0102-303, Sheet 35.

2. Group 10:

Modify existing left and right side tension tie structure at STA 720 in accordance with Drawing

142U0102-201, Sheet 2. Remove small cracks and fatigue damage material from the existing

holes in the unmodified center section of the tension tie channels in accordance with the

"zero-timing" procedure of 747-400F SRM 51-10-02.

3. Group 10:

Modify existing left and right side tension tie structure at STA 740 in accordance with Drawing

142U0102-202, Sheet 3. Remove small cracks and fatigue damage material from the existing

holes in the unmodified center section of the tension tie channels in accordance with the

"zero-timing" procedure of 747-400F SRM 51-10-02.

4. Group 1-3, 10, 13-14:

Modify existing left and right side tension tie structure at STA 760 as follows:

a. Group 1, 13:

Modify left and right side tension tie structure in accordance with Drawing 142U0102-203,

Sheet 4. Remove small cracks and fatigue damage material from the existing holes in the

unmodified center section of the tension tie channels in accordance with the "zero-timing"

procedure of 747-100/200/300 SRM 51-10-01.

b. Group 2, 14:

Modify left and right side tension tie structure in accordance with Drawing 142U0102-204,

Sheet 5. Remove small cracks and fatigue damage material from the existing holes in the

unmodified center section of the tension tie channels in accordance with the "zero-timing"

procedure of 747-100/200/300 SRM 51-10-01.

c. Group 3:

Modify left and right side tension tie structure in accordance with Drawing 142U0102-205,

Sheet 6. Remove small cracks and fatigue damage material from the existing holes in the

unmodified center section of the tension tie channels in accordance with the "zero-timing"

procedure of 747-100/200/300 SRM 51-10-01.

d. Group 10:

Modify left and right side tension tie structure in accordance with Drawing 142U0102-206,

Sheet 7. Remove small cracks and fatigue damage material from the existing holes in the

unmodified center section of the tension tie channels in accordance with the "zero-timing"

procedure of 747-400F SRM 51-10-02.

5. Group 1-3, 8, 10-15:

Modify existing left and right side tension tie structure at STA 780 as follows:

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149 of 158

BOEING SERVICE BULLETIN 747-53A2605

ALERT ALERT
a. Group 1-2, 8, 11, 13-15:

Modify left and right side tension tie structure in accordance with Drawing 142U0102-207,

Sheet 8. Remove small cracks and fatigue damage material from the existing holes in the

unmodified center section of the tension tie channels in accordance with the "zero-timing"

procedure of 747-100/200/300 SRM 51-10-01.

b. Group 3, 12:

Modify left and right side tension tie structure in accordance with Drawing 142U0102-208,

Sheet 9. Remove small cracks and fatigue damage material from the existing holes in the

unmodified center section of the tension tie channels in accordance with the "zero-timing"

procedure of 747-100/200/300 SRM 51-10-01.

c. Group 10:

Modify left and right side tension tie structure in accordance with Drawing 142U0102-209,

Sheet 10. Remove small cracks and fatigue damage material from the existing holes in the

unmodified center section of the tension tie channels in accordance with the "zero-timing"

procedure of 747-400F SRM 51-10-02.

6. Group 1-5, 8-15:

Modify existing left and right side tension tie structure at STA 800 as follows:

a. Group 1-5, 8-9, 11-15:

Modify left and right side tension tie structure in accordance with Drawing 142U0102-210,

Sheet 11. Remove small cracks and fatigue damage material from the existing holes in the

unmodified center section of the tension tie channels in accordance with the "zero-timing"

procedure of 747-100/200/300 SRM 51-10-01.

b. Group 10:

Modify left and right side tension tie structure in accordance with Drawing 142U0102-211,

Sheet 12. Remove small cracks and fatigue damage material from the existing holes in the

unmodified center section of the tension tie channels in accordance with the "zero-timing"

procedure of 747-400F SRM 51-10-02.

7. Group 1-5, 8-15:

Modify existing left and right side tension tie and frame structure at STA 820 as follows:

a. Group 1-5, 9, 11-15:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-212, Sheet 13 and 142U0101-101, Sheet 2. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

b. Group 8:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-212, Sheet 13 and 142U0101-102, Sheet 3. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

c. Group 10:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-213, Sheet 14 and 142U0101-103, Sheet 4. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-400F SRM 51-10-02.

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8. Modify existing left and right side tension tie and frame structure at STA 840 as follows:

a. Group 1-5, 9, 11-15:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-214, Sheet 15 and 142U0101-104, Sheet 5. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

b. Group 6-7:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-215, Sheet 16 and 142U0101-104, Sheet 5. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

c. Group 8:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-214, Sheet 15 and 142U0101-105, Sheet 6. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

d. Group 10:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-216, Sheet 17 and 142U0101-106, Sheet 7. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-400F SRM 51-10-02.

9. Modify existing left and right side tension tie and frame structure at STA 860 as follows:

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a. Group 1-5, 11-15:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-217, Sheet 18 and 142U0101-107, Sheet 8. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

b. Group 6-7:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-218, Sheet 19 and 142U0101-107, Sheet 8. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

c. Group 8:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-217,Sheet 18 and 142U0101-108, Sheet 9. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

d. Group 9:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-217, Sheet 18 and 142U0101-109, Sheet 10. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

e. Group 10:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-219, Sheet 20 and 142U0101-110, Sheet 11. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-400F SRM 51-10-02.

10. Modify existing left and right side tension tie and frame structure at STA 880 as follows:

a. Group 1-9, 11-15:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-220, Sheet 21 and 142U0101-111, Sheet 12. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

b. Group 10:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-221, Sheet 22 and 142U0101-112, Sheet 13. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-400F SRM 51-10-02.

11. Modify existing left and right side tension tie and frame structure at STA 900 as follows:

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a. Group 1-4, 6, 11-15:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-222, Sheet 23 and 142U0101-113, Sheet 14. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

b. Group 5, 7:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-223, Sheet 24 and 142U0101-125, Sheet 18. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

c. Group 8:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-222, Sheet 23 and 142U0101-114, Sheet 15. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

d. Group 9:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-223, Sheet 24 and 142U0101-115, Sheet 16. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

e. Group 10:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-224, Sheet 25 and 142U0101-116, Sheet 17. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-400F SRM 51-10-02.

12. Modify existing left and right side tension tie and frame structure at STA 920 as follows:

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a. Group 1-4, 6, 8, 11-15:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-225, Sheet 26 and 142U0101-117, Sheet 19. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

b. Group 5, 7:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-226, Sheet 27 and 142U0101-126, Sheet 20. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

c. Group 9:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-226, Sheet 27 and 142U0101-119, Sheet 20. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

d. Group 10:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-227, Sheet 28 and 142U0101-120, Sheet 21. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-400F SRM 51-10-02.

13. Modify existing left and right side tension tie and frame structure at STA 940 as follows:

a. Group 1-2, 11:

Modify left and right side tension tie and frame structure in accordance with Drawings ,

142U0102-233, Sheet 29 and 142U0101-121,Sheet 22. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

b. Group 3-4, 6, 12:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-229, Sheet 30 and 142U0101-121, Sheet22. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

c. Group 5, 7:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-230, Sheet 31 and 142U0101-127, Sheet 23. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

d. Group 8:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-228, Sheet 29 and 142U0101-121, Sheet 22. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

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e. Group 9:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-230, Sheet 31 and 142U0101-123, Sheet 23. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

f. Group 10:

Modify left and right side tension tie and frame structure in accordance with Drawings

142U0102-231, Sheet 32 and 142U0101-124, Sheet 24. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-400F SRM 51-10-02.

g. Group 13-15:

Modify left and right side tension tie and frame structure in accordance with Drawings ,

142U0102-232, Sheet 29 and 142U0101-121,Sheet 22. Remove small cracks and fatigue

damage material from the existing holes in the unmodified center section of the tension tie

channels in accordance with the "zero-timing" procedure of 747-100/200/300 SRM 51-10-01.

14. Install new shear panels as follows:

a. Group 1-5, 8-9, 11-15:

Install left and right side shear panels between STA 820 and 840 in accordance with Drawing

142U0102-301, Sheet 33.

b. Group 6-7:

Install left and right side shear panels between STA 840 and 860 in accordance with Drawing

142U0102-302, Sheet 34.

c. Group 10:

Install left and right side shear panels between STA 780 and 800 in accordance with Drawing

142U0102-303, Sheet 35.

PART 2: INSPECTION OF THE UNMODIFIED AREAS OF THE TENSION TIES

1. At all body stations where modification was previously done in accordance with this service bulletin,

do a detailed inspection of the remaining unmodified area of the tension tie for cracks. The

unmodified area of the tension tie at all body stations will be from approximately LBL 36 to RBL

36. Do the inspection on both sides of the tension tie (FWD and AFT) so that both tension tie

channels are inspected.

2. If no crack is found, repeat the detailed inspection of the unmodified areas of the tension ties for

cracks, at the time specified in paragraph 1.E., Compliance.

3. If any crack is found, contact Boeing for repair instructions and do the repair. Repeat the detailed

inspection of the unmodified areas of the tension ties for cracks, at the time specified in paragraph

1.E., Compliance.

PART 3: POST-MODIFICATION INSPECTION

1. Do initial and repeat inspections of the modified areas of the tension tie and frame structure.

Contact Boeing for inspection instructions.

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RESTORATION

1. Apply BMS 3-23, Type II, Corrosion Inhibiting Compound to the modified areas. Refer to SOPM

20-41-05 as an accepted procedure.

2. Install/kept insulation as necessary between STA 720 and STA 940. Refer to 747-100/200/300

AMM 25-21-04 or 747-400 AMM 25-21-04 as an accepted procedure.

3. Install/kept main deck ceiling panels as necessary between STA 720 and STA 940. Refer to

747-100/200/300 AMM 25-22-01 or 747-400 AMM 25-22-01 as an accepted procedure.

4. Install/kept seats as necessary between STA 720 and STA 940. Refer to 747-100/200/300 AMM

25-25-01 or 747-400 AMM 25-25-01 as an accepted procedure.

5. Supply electrical power to the airplane. Refer to 747-100/200/300 AMM 24-22-00 or 747-400 AMM

24-22-00 as an accepted procedure.

6. Return the airplane to a serviceable condition.

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APPENDIX A: TENSION TIE DISCONNECTION METHODS

(SHEET 1 OF 2)

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METHOD TASK NOTES

With the airplane on its gear, disconnect every other Tension Tie from -

the Frame at both ends, as shown in the view for Method 1.

1

With the airplane on its gear, remove all but four fasteners at each end -

of each Tension Tie. Do the necessary Work Instructions specified in this

service bulletin, and re-install fasteners. Remove the remaining four fasteners at each end of each Tension Tie and do the necessary Work Instructions at those locations.

2

not

shown

APPENDIX A: TENSION TIE DISCONNECTION METHODS

(SHEET 2 OF 2)

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