Commercial 

Airplanes 767

Service Bulletin

Number: 767-28-0105

Original Issue: January 12, 2012

Revision 1: February 06, 2013

ATA System: 2811

SUBJECT: FUEL - Fuel Tanks - Access Door Inspection/Replacement

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

CFR 300-774). An export license may be required before it is used for development, production or use by foreign

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

laws.

ECCN: 9E991

BOEING PROPRIETARY, CONFIDENTIAL AND/OR TRADE SECRET

Copyright © 2012 Boeing.

Unpublished Work. All Rights Reserved.

Treatment of this document and its content is governed by contract with Boeing. Rights to use this document

are licensed on a per aircraft basis and such rights may not be transferable. For more information, contact The

Boeing Company.

Boeing, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, 787, DreamlinerTM,

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 Boeing

liveries are all trademarks owned by The Boeing Company; and no trademark license is granted in connection

with this document unless provided in writing by Boeing. BOEING is a trademark of Boeing Management

Company.

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4.0
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BOEING SERVICE BULLETIN 767-28-0105

BLANK PAGE
Table of Contents

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

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

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

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

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

2. Spares Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17

B. Concurrent Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17

C. Reason . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17

D. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18

E. Compliance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18

F. Approval . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

G. Manpower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

H. Weight and Balance Changes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

I. Electrical Load Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

J. References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

1. Existing Data: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

2. Data Supplied with this Service Bulletin: . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

3. Installation Drawings Used in the Preparation of this Service Bulletin: . . . . . . . . . . . 21

K. Publications Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

L. Interchangeability and Intermixability of Parts . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

M. Software Accomplishment Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

2. MATERIAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

A. Material - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

B. Industry Support Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

C. Parts Necessary for Each Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

1. Kits/Parts: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

2. Parts and Materials Supplied by the Operator: . . . . . . . . . . . . . . . . . . . . . . . . 23

3. Parts Modified and Reidentified: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

4. Parts Removed and Not Replaced: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

D. Parts Necessary to Change Spares . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

E. Special Tooling - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

F. Special Tooling Necessary to do this Service Bulletin . . . . . . . . . . . . . . . . . . . . . . . 23

3. ACCOMPLISHMENT INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25

A. GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25

B. WORK INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25

FIGURE 1: ACCESS DOOR INSPECTION - LEFT WING . . . . . . . . . . . . . . . . . . . . . . . . 27

FIGURE 2: ACCESS DOOR INSPECTION - RIGHT WING . . . . . . . . . . . . . . . . . . . . . . . 29

APPENDIX A: PROCEDURE FOR ACCESS DOOR INSPECTION . . . . . . . . . . . . . . . . . . . . . 31

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BOEING SERVICE BULLETIN 767-28-0105

BLANK PAGE
Commercial 

Airplanes 767

Service Bulletin

Revision Transmittal Sheet Number: 767-28-0105

Original Issue: January 12, 2012

Revision 1: February 06, 2013

ATA System: 2811

SUBJECT: FUEL - Fuel Tanks - Access Door Inspection/Replacement

This revision includes all pages of the service bulletin.

COMPLIANCE INFORMATION RELATED TO THIS REVISION

Airplanes VR268-VR284, VS924-VS928, VS941, VS951-VS954, VS961-VS969, VS971-VS977, VS981-VS982,

VT001-VT006, VT544-VT545, VT551-VT552 were added to Group 2 of this service bulletin effectivity.

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

REASON FOR REVISION

This revision is sent to tell operators that the service bulletin effectivity was revised to add new airplanes to

Group 2 of this service bulletin effectivity. Group 2 was added to the service bulletin Effectivity to include all the

767 airplanes delivered prior to the release of the Maintenance Planning Data (MPD) update containing

Airworthiness Limitation (AWL) 57-AWL-01, which makes sure that Impact Resistant Access Doors are installed

at the correct locations. Also, one stencil location dimension on the alternate configuration in Figure 1 and Figure

2 was corrected, and a footnote was added to allow for more flexibility for the stencil and marker locations. The

General Visual Inspection Procedure in Appendix A, Option 1, has been updated to show that impact resistant

access doors have flat ends. A compliance table was added to Paragraph 1.E., Compliance. In addition, the

last step in the Work Instructions was corrected.

These sections were changed:

1. Summary: Added Summary Evaluation Table.

2. Paragraph 1.A., Effectivity: Added VR268-VR284, VS924-VS928, VS941, VS951-VS954, VS961-VS969,

VS971-VS977, VS981-VS982, VT001-VT006, VT544-VT545, VT551-VT552.

3. Paragraph 1.A., Effectivity: Created Group 2 for the new airplanes that were added.

4. Paragraph 1.E., Compliance: Added a compliance table.

5. Paragraph 2.B., Industry Support Information: Added a warranty statement for Group 2 airplanes.

6. Paragraph 3.B., Work Instructions, Step 10: Corrected instruction.

7. Figures 1 and 2: Corrected illustration.

8. Figures 1 and 2: Added a footnote to step table.

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9. Appendix A: Corrected illustration to show rounded edges on impact resistant access door.

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

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Commercial 

Airplanes 767

Service Bulletin

Summary Number: 767-28-0105

Original Issue: January 12, 2012

Revision 1: February 06, 2013

ATA System: 2811

SUBJECT: FUEL - Fuel Tanks - Access Door Inspection/Replacement

CONCURRENT REQUIREMENTS

Refer to Paragraph 1.B., Concurrent Requirements.

BACKGROUND

This service bulletin provides instructions to inspect the Wing Fuel Tank Access Doors to make sure that Impact

Resistant Access Doors are installed in the correct locations and stencils and index markers are applied. Fire

can result from damage to a standard access door if it is located where an Impact Resistant Access Door is

required.

An operator identified a standard access door located where an Impact Resistant Access Door is required. In

addition, the operator examined its spares stock and found that some Impact Resistant Access Doors were

without stencils. These findings have raised a concern about the possibility of more standard access doors being

installed at locations where Impact Resistant Access Doors are required. Impact Resistant Access Doors minimize

risk of penetration from engine debris or objects thrown by airplane tires. By accomplishing the inspection in

this service bulletin, operators can make sure that stencils and index markers are applied and Impact Resistant

Access Doors are installed at the correct locations, providing increased resistance to Wing Fuel Tank penetration.

Boeing Service Related Problem (SRP) 767-SRP-57-0225 is related to this service bulletin.

This table is provided to operators for planning purposes only. Refer to the applicable sections for more

information.

Planning Data Affected Reference

Spares Affected No Paragraph 1.A.2., Spares Affected

Paragraph 1.E., Compliance and Paragraph

1.F., Approval

AD Related Yes

Weight and Balance Change No Paragraph 1.H., Weight and Balance Changes

Electrical Load Changed No Paragraph 1.I., Electrical Load Data

Publications Affected No Paragraph 1.K., Publications Affected

Airplane Flight Operations Affected (Flight Crew No Paragraph 1.K., Publications Affected

Operations Manual and/or FAA Approved Airplane Flight Manual)

Kits/Parts Required No Paragraph 2.C.1., Kits/Parts

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Planning Data Affected Reference

Paragraph 2.C.2., Parts and Materials Supplied

by the Operator

Operator Supplied Parts/Material Yes

Paragraph 2.F., Special Tooling Necessary to

do this Service Bulletin

Special Tooling Required No

ACTION

Identify the Wing Fuel Tank Access Doors. Do a General Visual Inspection or an ultrasonic Non-Destructive

Test (NDT) to make sure that Impact Resistant Access Doors are installed in the correct locations. If a standard

access door is identified in a location where an Impact Resistant Access Door is required, replace the door with

an Impact Resistant Access Door. Do a General Visual Inspection to make sure that stencils and index markers

are applied. If a stencil and/or index marker is missing, apply new stencil and/or index marker.

EFFECTIVITY

767-200/-300/-300F/-400ER Airplanes.

Refer to Paragraph 1.A.1, Effectivity.

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.

Refer to Paragraph 1.E., Compliance.

INDUSTRY SUPPORT INFORMATION

Refer to Paragraph 2.B., Industry Support Information.

MANPOWER

Refer to Paragraph 1.G., Manpower.

MATERIAL INFORMATION

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

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BOEING SERVICE BULLETIN 767-28-0105

BLANK PAGE
Commercial 

Airplanes 767

Service Bulletin

Number: 767-28-0105

Original Issue: January 12, 2012

Revision 1: February 06, 2013

ATA System: 2811

SUBJECT: FUEL - Fuel Tanks - Access Door Inspection/Replacement

1. PLANNING INFORMATION

A. Effectivity

1. Airplanes

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

Number, and Serial Number data.

This service bulletin is for the airplanes shown below.

GROUP CONFIGURATION DESCRIPTION

1 - 767-200/300/300F/400ER Airplanes, line numbers 1-717 and 719-984

2 - 767-300/300F Airplanes, line numbers 985-1039

Airplane Models:

767-200, 767-300, 767-300F, 767-400ER

Variable Number Group

VA001 - VA020 1

VA301 - VA315 1

VA501 - VA530 1

VA701 - VA719 1

VA801 - VA810 1

VB001 - VB002 1

VB051 - VB055 1

VB101 - VB125 1

VB201 - VB202 1

VB251 - VB253 1

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Variable Number Group

VB281 - VB284 1

VB301 - VB302 1

VB321 - VB332 1

VB371 - VB373 1

VB401 1

VB441 - VB444 1

VE001 - VE003 1

VE021 - VE023 1

VE041 - VE043 1

VE061 - VE069 1

VE083 - VE086 1

VE101 - VE104 1

VE116 - VE118 1

VE121 - VE126 1

VE141 - VE152 1

VE171 - VE172 1

VF001 - VF002 1

VF041 - VF042 1

VF051 1

VF061 - VF062 1

VF071 - VF072 1

VF091 - VF093 1

VF101 - VF102 1

VF161 - VF162 1

VF171 - VF172 1

VF180 - VF184 1

VF251 1

VK001 - VK016 1

VK021 - VK022 1

VK031 - VK056 1

VK081 - VK113 1

VK131 - VK133 1

VK141 - VK148 1

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BOEING SERVICE BULLETIN 767-28-0105
Variable Number Group

VK161 - VK164 1

VK171 1

VK181 1

VK186 1

VL001 - VL006 1

VL011 1

VL701 - VL703 1

VL751 - VL755 1

VL806 - VL807 1

VL871 - VL873 1

VL891 - VL900 1

VL911 - VL914 1

VL931 - VL932 1

VL941 1

VN001 - VN041 1

VN051 - VN064 1

VN081 - VN099 1

VN111 - VN127 1

VN130 - VN137 1

VN151 - VN158 1

VN163 - VN168 1

VN171 - VN174 1

VN191 - VN198 1

VN211 - VN212 1

VN221 - VN225 1

VN231 - VN234 1

VN241 - VN243 1

VN251 - VN276 1

VN291 - VN293 1

VN301 - VN314 1

VN371 - VN372 1

VN376 1

VN381 - VN388 1

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BOEING SERVICE BULLETIN 767-28-0105
Variable Number Group

VN421 - VN427 1

VN436 1

VN471 - VN472 1

VN491 - VN513 1

VN531 - VN532 1

VN536 - VN537 1

VN541 - VN542 1

VN546 - VN547 1

VN551 1

VN556 - VN557 1

VN561 - VN562 1

VN631 - VN638 1

VN651 - VN658 1

VN671 - VN672 1

VN676 1

VN681 - VN691 1

VN731 - VN732 1

VN751 - VN753 1

VN791 - VN792 1

VN811 - VN813 1

VN921 - VN922 1

VN931 - VN936 1

VN951 - VN953 1

VN966 - VN972 1

VQ001 - VQ021 1

VQ071 - VQ086 1

VQ111 1

VR051 - VR060 1

VR081 1

VR084 1

VR086 - VR089 1

VR106 - VR109 1

VR201 - VR211 1

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BOEING SERVICE BULLETIN 767-28-0105
Variable Number Group

VR251 1

VR256 - VR260 1

VR266 - VR267 1

VR268 - VR284 2

VR401 1

VR421 - VR423 1

VR426 1

VR441 1

VR461 1

VR471 - VR472 1

VS051 - VS056 1

VS061 1

VS066 - VS070 1

VS073 - VS078 1

VS091 - VS104 1

VS111 - VS113 1

VS131 - VS133 1

VS136 - VS137 1

VS176 - VS177 1

VS186 - VS187 1

VS196 - VS203 1

VS206 - VS208 1

VS211 1

VS216 - VS217 1

VS231 1

VS246 - VS248 1

VS261 - VS263 1

VS266 - VS274 1

VS291 - VS293 1

VS301 - VS303 1

VS306 - VS311 1

VS316 1

VS321 - VS324 1

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BOEING SERVICE BULLETIN 767-28-0105
Variable Number Group

VS331 - VS333 1

VS336 - VS337 1

VS366 - VS367 1

VS381 - VS382 1

VS391 - VS392 1

VS401 1

VS426 - VS428 1

VS466 - VS472 1

VS486 1

VS496 - VS497 1

VS506 - VS507 1

VS526 1

VS546 - VS549 1

VS701 - VS736 1

VS751 - VS759 1

VS821 - VS825 1

VS841 - VS844 1

VS861 1

VS881 - VS883 1

VS891 1

VS896 1

VS901 - VS912 1

VS916 1

VS921 - VS923 1

VS924 - VS928 2

VS931 - VS933 1

VS941 2

VS951 - VS954 2

VS961 - VS969 2

VS971 - VS977 2

VS981 - VS982 2

VT001 - VT006 2

VT501 1

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BOEING SERVICE BULLETIN 767-28-0105
Variable Number Group

VT511 - VT513 1

VT521 - VT523 1

VT531 - VT533 1

VT541 - VT543 1

VT544 - VT545 2

VT551 - VT552 2

VW701 - VW721 1

VW851 1

2. Spares Affected

None.

B. Concurrent Requirements

The service bulletin listed below must be done before or at the same time as this service bulletin:

Company Service Bulletin Description

Boeing 767-28A0019 Original Issue Fuel - Storage - Tank Access Door Replacement

C. Reason

This service bulletin provides instructions to inspect the Wing Fuel Tank Access Doors to make sure

that Impact Resistant Access Doors are installed in the correct locations and stencils and index markers

are applied. Fire can result from damage to a standard access door if it is located where an Impact

Resistant Access Door is required.

An operator identified a standard access door located where an Impact Resistant Access Door is

required. In addition, the operator examined its spares stock and found that some Impact Resistant

Access Doors were without stencils. These findings have raised a concern about the possibility of more

standard access doors being installed at locations where Impact Resistant Access Doors are required.

Impact Resistant Access Doors minimize risk of penetration from engine debris or objects thrown by

airplane tires. By accomplishing the inspection in this service bulletin, operators can make sure that

stencils and index markers are applied and Impact Resistant Access Doors are installed at the correct

locations, providing increased resistance to Wing Fuel Tank penetration.

Boeing Service Related Problem (SRP) 767-SRP-57-0225 is related to this service bulletin.

Revision 1 is sent to tell operators that the service bulletin effectivity was revised to add new airplanes

to Group 2 of this service bulletin effectivity. Group 2 was added to the service bulletin Effectivity to

include all the 767 airplanes delivered prior to the release of the Maintenance Planning Data (MPD)

update containing Airworthiness Limitation (AWL) 57-AWL-01, which makes sure that Impact Resistant

Access Doors are installed at the correct locations. Also, one stencil location dimension on the alternate

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BOEING SERVICE BULLETIN 767-28-0105
configuration in Figure 1 and Figure 2 was corrected, and a footnote was added to allow for more

flexibility for the stencil and marker locations. The General Visual Inspection Procedure in Appendix

A, Option 1, has been updated to show that impact resistant access doors have flat ends. A compliance

table was added to to Paragraph 1.E., Compliance. In addition, the last step in the Work Instructions

was corrected.

D. Description

Identify the Wing Fuel Tank Access Doors. Do a General Visual Inspection or an ultrasonic

Non-Destructive Test (NDT) to make sure that Impact Resistant Access Doors are installed in the

correct locations. If a standard access door is identified in a location where an Impact Resistant Access

Door is required, replace the door with an Impact Resistant Access Door. Do a General Visual Inspection

to make sure that stencils and index markers are applied. If a stencil and/or index marker is missing,

apply new stencil and/or index marker.

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:

Affected Maintenance Zones

Model Zone

767-200, 767-300, 767-300F, 531, 532, 631, 632

767-400ER

Group 2:

Affected Maintenance Zones

Model Zone

767-300, 767-300F 531, 532, 631, 632

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.

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BOEING SERVICE BULLETIN 767-28-0105
Table 1: Compliance Time for Impact Resistant Access Doors and Stencils and Index Markers

Inspection/Replacement

Repeat Interval

(Not to Exceed)

Condition Action Compliance Time

Within 72 months -

after the original issue date of this

service bulletin

Do a General Visual Inspection or an ultrasonic

Non-Destructive Test

(NDT) of the left and right

auxiliary fuel tank access

doors, and the left and

right main fuel tank access doors to make sure

that Impact Resistant Access Doors are installed

in the correct locations, in

accordance with Accomplishment Instructions,

Step 1 and Step 5.

All airplanes

Before further -

flight.

Replace each standard

access door with an Impact Resistance access

door, in accordance with

Accomplishment Instructions, Step 2 and Step 6,

as applicable.

One or more standard access doors are found (i.e.,

impact resistant doors are

not found).

Within 72 months -

after the original issue date of this

service bulletin

Do a General Visual Inspection of the left and

right auxiliary fuel tank

access doors, and the left

and right main fuel tank

access doors to make

sure that stencils and index markers are applied,

in accordance with Accomplishment Instructions, Step 3 and Step 7.

All airplanes

Before further -

flight.

Apply stencil in accordance with Accomplishment Instructions, Step 4

and Step 8, as applicable.

Any stencil is missing.

Before further -

flight.

Apply index marker in accordance with Accomplishment Instructions,

Step 4 and Step 8, as

applicable.

Any index marker is missing.

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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.

G. Manpower

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

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

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

— Time to adjust to the workplace

— Time to schedule the work

— Time to examine the work

— Time to cure the materials

— Time to make the parts

— Time to find the tools.

OPTION 1: MAN-HOURS FOR GENERAL VISUAL INSPECTION PROCEDURE

Task Number of Persons Task Hours Elapsed Hours More Data

Figure 1 1 3.25 3.25 (a)

Figure 2 1 3.25 3.25 (a)

TOTAL FOR EACH AIRPLANE 6.50 6.50 (a)

(a) Does not include time to defuel/refuel.

OPTION 2: MAN-HOURS FOR ULTRASONIC NON-DESTRUCTIVE TEST (NDT) INSPECTION PROCEDURE

Task Number of Persons Task Hours Elapsed Hours More Data

Figure 1 1 2.25 2.25 (a)

Figure 2 1 2.25 2.25 (a)

TOTAL FOR EACH AIRPLANE 4.50 2.50 (a)

(a) Does not include time to defuel/refuel.

H. Weight and Balance Changes

None

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I. Electrical Load Data

Not applicable

J. References

1. Existing Data:

a. Boeing Service Related Problem (SRP) 767-SRP-57-0225

b. Boeing Service Bulletin 767-28A0019

c. Standard Overhaul Practices Manual (SOPM) 20-50-10

d. 767 Aircraft Maintenance Manual (AMM) 28-11-01, 28-11-02, 28-26-00

e. 767 Illustrated Parts Catalog (IPC) 28-11-01

f. 767 Non-Destructive Testing (NDT) Manual 767 NDT Part 4, 51-00-10

2. Data Supplied with this Service Bulletin:

None.

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

Engineering Drawing Nomenclature

112T6007 Access Door Instl - Fuel Tank, Wing

110T3301 Marking Instl - Exterior, Wing

K. Publications Affected

1. Publications:

None.

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 does not affect FCS, therefore DTIs are not necessary.

L. Interchangeability and Intermixability of Parts

Refer to Paragraph 2.C., Parts Necessary For Each Airplane, for interchangeability and intermixability

information.

M. Software Accomplishment Summary

Not affected.

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BLANK PAGE
2. MATERIAL INFORMATION

A. Material - Price and Availability

Refer to Paragraph 2.C., Parts Necessary For Each Airplane.

B. Industry Support Information

Group 1:

Boeing warranty remedies are available for 767 airplanes in warranty as of June 19, 2008. For inspection

man-hour reimbursement for airplanes in warranty as of that date, send a warranty claim to Boeing

Warranty & Product Assurance Contracts. If the condition described in this service bulletin is found

during the initial inspection for airplanes in warranty as of that date and additional man-hours or parts

are required, send a warranty claim to Boeing Warranty & Product Assurance Contracts. Warranty

remedies are not available for continued inspections as described in this Service Bulletin as these

actions are considered routine maintenance.

Group 2:

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

service bulletin.

C. Parts Necessary for Each Airplane

1. Kits/Parts:

None

2. Parts and Materials Supplied by the Operator:

Refer to Illustrated Parts Catalog (IPC) 767 IPC 28-11-01.

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

None

F. Special Tooling Necessary to do this Service Bulletin

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

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BLANK PAGE
3. ACCOMPLISHMENT INSTRUCTIONS

A. GENERAL INFORMATION

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

PARTICLES OR CONTAMINATION WHEN YOU USE TOOLS. UNWANTED MATERIAL,

METAL PARTICLES OR CONTAMINATION CAUGHT IN WIRE BUNDLES CAN CAUSE

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

OTHER ELECTRICAL DAMAGE.

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

definition of the acronyms.

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

3. 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

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

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

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

SRM Chapter 51 may be used.

5. A General Visual Inspection is defined as: A visual examination of an interior or

exterior area, installation or assembly to detect obvious damage, failure or irregularity.

This level of inspection is made from within touching distance unless otherwise

specified. A mirror may be necessary to enhance visual access to all exposed surfaces

in the inspection area. This level of inspection is made under normally available

lighting conditions such as daylight, hangar lighting, flashlight or drop-light and may

require removal or opening of access panels or doors. Stands, ladders or platforms

may be required to gain proximity to the area being checked.

6. A Non-Destructive Test (NDT) is an inspection/testing procedure used to determine

the condition of a material in such a manner as to not damage or destroy the material

under investigation. The material is examined for flaws or conditions that could be

detrimental to the integrity of the structure.

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

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

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

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

must be used.

B. WORK INSTRUCTIONS

1. Do a General Visual Inspection (GVI) or an ultrasonic Non-Destructive Test (NDT) of the left

auxiliary fuel tank and left main fuel tank access doors to make sure that Impact Resistant Access

Doors are installed in the correct locations, in accordance with FIGURE 1.

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2. If one or more standard access doors are found, replace each standard access door with an Impact

Resistance access door. Refer to 767 AMM 28-11-01 as an accepted procedure to replace main

tank access doors. Refer to 767 AMM 28-11-02 as an accepted procedure to replace auxiliary

tank access doors.

3. Do a General Visual Inspection of the left auxiliary fuel tank and left main fuel tank access doors

to make sure that stencils and index markers are applied in accordance with FIGURE 1.

4. If a stencil and/or index marker is missing, apply stencil and/or index marker in accordance with

FIGURE 1.

5. Do a GVI or an ultrasonic NDT of the right auxiliary fuel tank and right main fuel tank access doors

to make sure that Impact Resistant Access Doors are installed in the correct locations, in accordance

with FIGURE 2.

6. If one or more standard access doors are found, replace each standard access door with an Impact

Resistance access door. Refer to 767 AMM 28-11-01 as an accepted procedure to replace main

tank access doors. Refer to 767 AMM 28-11-02 as an accepted procedure to replace auxiliary

tank access doors.

7. Do a General Visual Inspection of the right auxiliary fuel tank and right main fuel tank access doors

to make sure that stencils and index markers are applied in accordance with FIGURE 2.

8. If a stencil and/or index marker is missing, apply stencil and/or index marker in accordance with

FIGURE 2.

9. If one or more access doors were replaced and a leak check has not been done, refuel the

applicable fuel tank and check for leaks. Repair if necessary. Refer to 767 AMM 28-11-01 as an

accepted procedure to replace main tank access doors. Refer to 767 AMM 28-11-02 as an accepted

procedure to replace auxiliary tank access doors.

10. Put the airplane back to a serviceable condition.

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

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

FIGURE 1: ACCESS DOOR INSPECTION - LEFT WING

(SHEET 1 OF 2)

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STEP TASK NAME PART NUMBER QTY NOTE

1 Inspect Access Door - 5 (a)

Stencil and Index - - (b) (c)

Marker

2 Inspect

3 Inspect Stencil - - (b) (c)

4 Inspect Index Marker - - (b) (c)

(a) In accordance with APPENDIX A.

(b) If a stencil and/or index marker is missing, apply stencil and/or index marker with BMS 10-60, Polyurethane

Gloss Enamel, matching color to existing stencil and/or index marker. Refer to SOPM 20-50-10 as an

accepted procedure.

(c) Stencil and/or Index Marker location may be adjusted, as required, to avoid application over fastener

heads.

FIGURE 1: ACCESS DOOR INSPECTION - LEFT WING

(SHEET 2 OF 2)

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

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

FIGURE 2: ACCESS DOOR INSPECTION - RIGHT WING

(SHEET 1 OF 2)

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STEP TASK NAME PART NUMBER QTY NOTE

1 Inspect Access Door - 5 (a)

Stencil and Index - - (b) (c)

Marker

2 Inspect

3 Inspect Stencil - - (b) (c)

4 Inspect Index Marker - - (b) (c)

(a) In accordance with APPENDIX A.

(b) If a stencil and/or index marker is missing, apply stencil and/or index marker with BMS 10-60, Polyurethane

Gloss Enamel, matching color to existing stencil and/or index marker. Refer to SOPM 20-50-10 as an

accepted procedure.

(c) Stencil and/or Index Marker location may be adjusted, as required, to avoid application over fastener

heads.

FIGURE 2: ACCESS DOOR INSPECTION - RIGHT WING

(SHEET 2 OF 2)

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Use one of these two procedures to inspect each of the specified access doors.

OPTION 1: GENERAL VISUAL INSPECTION PROCEDURE

1. Defuel the applicable fuel tank. Refer to 767 AMM 28-26-00 as an accepted procedure.

2. Remove the access door. Refer to 767 AMM 28-11-01 as an accepted procedure to remove main tank

access doors. Refer to 767 AMM 28-11-02 as an accepted procedure to remove auxiliary tank and

main fuel tank access doors.

3. Do a General Visual Inspection of the internal surface of the access door. If the door ends are flat and

the inner surface is smooth, then the door is an impact resistant access door (Figure A1). If the internal

surface of the access door has protruding cast aluminum integral ribs and the door ends are rounded,

then the door is a standard access door (Figure A1).

APPENDIX A: PROCEDURE FOR ACCESS DOOR INSPECTION

(SHEET 1 OF 4)

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Figure A1

APPENDIX A: PROCEDURE FOR ACCESS DOOR INSPECTION

(SHEET 2 OF 4)

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OPTION 2: ULTRASONIC NON-DESTRUCTIVE TEST (NDT) INSPECTION PROCEDURE

1. General:

a. This procedure is permitted with or without fuel in the tanks.

b. Refer to Non-Destructive Test (NDT) Standard Practices Manual 767 NDT Part 4, 51-00-10,

Procedure 1 or 2, as an accepted procedure.

2. Equipment:

a. Digital thickness gage: Kramer Branson CL300, or equivalent.

b. Aluminum step wedge standard with a range that includes 0.08 to 0.50 inch.

c. A 0.25 inch, 15mhz delay tip or equivalent transducer.

d. Couplant: A low viscosity oil or UT couplant which will not damage the airplane structure.

3. Preparation: Clean fuel tank access door external skin.

4. Calibration: Calibrate the gage between 0.08 and 0.50 inch.

5. Inspection:

a. Along the center line of the long axis, slowly scan the fuel tank access door from one end to the

other end (Figure A2).

b. If a rib is detected and the rib thickness is greater than 0.50 inch, then the door is a standard

access door.

c. If the access door has a thickness between 0.08 and 0.10 inch and no ribs are detected, then the

access door is an impact resistant access door.

APPENDIX A: PROCEDURE FOR ACCESS DOOR INSPECTION

(SHEET 3 OF 4)

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Figure A2

APPENDIX A: PROCEDURE FOR ACCESS DOOR INSPECTION

(SHEET 4 OF 4)

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