Commercial

Airplane

Group

767

Service Bulletin

ALERT

Number: 767-78A0081 Revision Transmittal Sheet

Date: July 24, 1997

Revision 2: April 19, 2001

ATA System: 7830

SUBJECT: EXHAUST (CF6-80C2 Engines) - Thrust Reverser - Thrust Reverser Control System - Center

Drive Unit (CDU) Cone Brake Integrity Test

This revision includes all pages of the service bulletin.

COMPLIANCE INFORMATION RELATED TO THIS REVISION

Federal Aviation Administration (FAA) Airworthiness Directive (AD) 2000-09-04, Amendment 39-11712, is

related to this service bulletin.

More work is necessary on airplanes changed as shown in the Revision 1 of this service bulletin.

Airplanes were added to Group 2 of the service bulletin effectivity.

REASON FOR REVISION

This revision adds the inspection interval of the Electro-Mechanical brake and CDU cone brake for airplanes

equipped with thrust reversers that have been modified in accordance with Boeing Service Bulletin

767-78-0063 or after the equivalent modification (Production Revision Record B11481-90) incorporating in

production. Revise the service bulletin effectivity to add Group 2 airplanes which is included all 767-200,

-300 and -300F airplanes (including future 767-200, -300 and -300F airplanes) with CF6-80C2 engines from

production control line 475. Also, the Industry Support Information statement has been changed.

Paragraph 1.A., Effectivity, shows changes of airplane operators. Each operator should examine the

Effectivity paragraph for changes.

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

Initial Release: July 24, 1997

Revision 1: October 9, 1997

Revision 2: April 19, 2001

767-78A0081

Revision Transmittal Page 1 of 1

Commercial

Airplane

Group

767

Service Bulletin

ALERT

Number: 767-78A0081 Summary Date: July 24, 1997

Revision 2: April 19, 2001

ATA System: 7830

SUBJECT: EXHAUST (CF6-80C2 Engines) - Thrust Reverser - Thrust Reverser Control System - Center

Drive Unit (CDU) Cone Brake Integrity Test

CONCURRENT REQUIREMENTS

None

BACKGROUND

This inspection will make sure that the center drive

unit (CDU) cone brake and the Thrust Reverser

Actuation System (TRAS) brake have the holding

torque required to prevent any uncommanded thrust

reverser sleeve movement.

The CDU cone brake and the TRAS brake are

primary safety devices required to prevent

inadvertent thrust reverser sleeve movement. To

meet the system reliability requirements, periodic

torque checks are required to ensure the integrity of

these locking devices. A failure of either of these

locks is not detected during normal operation. The

torque check intervals have been determined

through industry-wide accepted probability and

reliability methods.

The TRAS lock is a solenoid activated disk brake

this is connected to the upper angle gearbox by a

flexible drive shaft. The brake is released when 28

VDC is applied from the control circuit and is locked

at all other times. Low torque can be the result of a

brake or flexible shaft failure.

The CDU cone brake is a spring load, unidirectional

device that prevent rotation of the air motor in the

deploy direction. The cone brake always allows the

air motor to rotate in the stow direction. The brake

is disengaged when the directional control valve

actuator piston is commanded to the deploy position

from the control circuit.

Boeing Service Related Problem (SRP)

767-SRP-78-0036 is related to this service bulletin.

ACTION

For Group 1 airplanes that have not incorporated

Boeing Service Bulletin 767-78-0063, on each thrust

reverser half, do a functional test on the CDU cone

brake to verify the holding torque.

For Group 1 airplanes that have incorporated

Boeing Service Bulletin 767-78-0063 and Group 2

airplanes, on each thrust reverser half, do a

functional test of the Electro-Mechanical brake and

CDU cone brake to verify the holding torque.

EFFECTIVITY

All 767-200, -300 and -300F airplanes powered by

CF6-80C2 engines.

COMPLIANCE

Boeing recommends the operators do this service

bulletin within 650 flight hours after receipt of this

service bulletin.

For Group 1 airplanes that have not incorporated

Boeing Service Bulletin 767-78-0063, Boeing

recommends the operators repeat CDU cone brake

test every 650 flight hours.

For Group 1 airplanes on which Boeing Service

Bulletin 767-78-0063 has been incorporated and on

Group 2 airplanes, Boeing recommends the

operators repeat the Electro-Mechanical brake and

CDU cone brake tests every 1,000 flight hours.

Federal Aviation Administration (FAA) Airworthiness

Directive (AD) 2000-09-04, Amendment 39-11712,

is related to this service bulletin.

767-78A0081

Summary Page 1 of 2
ALERT BOEING SERVICE BULLETIN 767-78A0081 ALERT

INDUSTRY SUPPORT INFORMATION

Boeing warranty remedies are not available for the

inspection given in this service bulletin.

MANPOWER

Total Man-hours - 6 for each airplane

Elapsed Time - 3 Hours

MATERIAL INFORMATION

None

ELECTRO-MECHANICAL BRAKE

DO A FUNCTIONAL TEST ON THE

FOR EACH THRUST REVERSER HALF:

DO A FUNCTIONAL TEST ON THE

FOR EACH THRUST REVERSER HALF:

CENTER DRIVE UNIT (CDU) CONE BRAKE

RIGHT SIDE OPPOSITE

LEFT SIDE SHOWN,

S13036

July 24, 1997 767-78A0081

Revision 2: April 19, 2001 Summary Page 2 of 2
Commercial

Airplane

Group

767

Service Bulletin

ALERT

Number: 767-78A0081

Date: July 24, 1997

Revision 2: April 19, 2001

ATA System: 7830

SUBJECT: EXHAUST (CF6-80C2 Engines) - Thrust Reverser - Thrust Reverser Control System - Center

Drive Unit (CDU) Cone Brake Integrity Test

1. PLANNING INFORMATION

A. Effectivity

NOTE:* THIS EFFECTIVITY INCLUDES ALL FUTURE 767-200, -300 AND -300F AIRPLANES

WITH CF6-80C2 ENGINES FROM PRODUCTION LINE NUMBER 475, EVEN IF THEY

ARE NOT LISTED IN THIS SECTION.

1. Airplanes

Refer to Service Bulletin Index Document D624T001, Part 3 for Airplane Variable Number, Line

Number, and Serial Number data.

Airplane Models:

767-200 767-300 767-300F

IDENTIFICATION BY CUSTOMER, CUSTOMER CODE, GROUP AND VARIABLE NUMBER

AEROFLOT (ARO)

2 VS321-VS324

AIR ALGERIE (ALG)

1 VK131-VK133

AIR CANADA (ACN)

1 VN052 VN054 VN057 VN731

2 VS546-VS548

AIR DO (HIA)

2 VS176

AIR EUROPA (ARE)

2 VS291-VS292

AIR EUROPE ITALY (EIY)

1 VN811-VN812

AIR FRANCE (AFA)

2 VN634-VN635

July 24, 1997 767-78A0081

Revision 2: April 19, 2001 Page 1 of 14
ALERT BOEING SERVICE BULLETIN 767-78A0081 ALERT

AIR MADAGASCAR (MAD)

2 VS316

AIR MAURITIUS (MAU)

1 VF001-VF002

AIR NEW ZEALAND (ANZ)

1 VN651-VN652

2 VN653-VN658 VS112-VS113

AIR PACIFIC (APC)

2 VN676

AIR SEYCHELLES (ASY)

1 VF051

2 VL941 VS526

AIR 2000 (ATZ)

2 VN921-VN922 VS216-VS217

AIRTOURS INT'L AIRWAYS (GUE)

2 VN951-VN953

ALITALIA (ALI)

2 VL701-VL702 VN422-VN427 VS366-VS367 VS401

ALL NIPPON AIRWAYS (ANA)

1 VK081-VK102 VN191-VN195

2 VK103-VK113 VN196-VN198 VR401

AMERICAN AIRLINES (AAL)

1 VN001-VN028

2 VN029-VN041 VS196-VS203

AMIRI FLIGHT (ABD)

2 VS391

ANSETT AUSTRALIA (ANS)

2 VL755

ASIANA AIRLINES (AAR)

1 VK141-VK142 VN753

2 VK143-VK148 VL703 VR426 VS231 VW851

BOEING (TBC)

2 VY999

BRITANNIA AIRWAYS (BRI)

1 VB331-VB332

2 VL911-VL913 VS051-VS056

BRITANNIA AIRWAYS AB (TNS)

2 VL914

CANADIAN AIRLINES (CDI)

1 VN051 VN053 VN058-VN062 VN751-VN752 VN813

2 VN732 VS381-VS382

July 24, 1997 767-78A0081

Revision 2: April 19, 2001 2
ALERT BOEING SERVICE BULLETIN 767-78A0081 ALERT

CHINA UNITED AIRLINES (CUL)

2 VS274

CITY BIRD (CBD)

2 VN436 VS177

CONTINENTAL AIRLINES (CAL)

2 VR051-VR058

DELTA AIR LINES (DAL)

1 VN301-VN306

2 VL753 VS073-VS078 VS266-VS273 VS466-VS471

EUROFLY (EUY)

2 VS392

EVA AIR (EVA)

1 VN471-VN472 VN791-VN792

2 VB441-VB444

GULF AIR (GUL)

1 VL004-VL006 VN307-VN308

2 VN309-VN310 VN313-VN314

H.M.S.F. AND AMEDEO CORP. (BWN)

2 VF180

IBERIA AIRLINES (IBE)

2 VN546-VN547

ITOCHU CORPORATION (CIT)

2 VF181-VF184

JAPAN AIRLINES (JAL)

2 VK012-VK016 VK181 VK186 VR441 VR461

K.B.A. FOUNDATION (KBA)

2 VN312

KALAIR USA CORP (KLA)

2 VN311

KENYA AIRWAYS (KEN)

2 VS331

KLM - ROYAL DUTCH AIRLINES (KLM)

2 VL891-VL900 VS136-VS137

LANCHILE AIRLINES (LAN)

1 VN063-VN064

2 VN968-VN970 VR251 VR256-VR257 VS131-VS133

LAPA ARGENTINA (LAZ)

2 VS111

LOT POLISH AIRLINES (LOT)

1 VF041-VF042 VN291

2 VN292-VN293

July 24, 1997 767-78A0081

Revision 2: April 19, 2001 3
ALERT BOEING SERVICE BULLETIN 767-78A0081 ALERT

MALEV HUNGARIAN AIRLINES (HGA)

1 VL003

2 VF171-VF172

MID EAST JET (SKL)

2 VF251

QANTAS (QAN)

1 VN081-VN093

2 VN094-VN099 VS186-VS187 VS486

ROYAL BRUNEI AIRLINES (RBA)

2 VN637-VN638

SKYMARK AIRLINES (SKM)

2 VS261-VS262

SOBELAIR (SBL)

2 VN421 VN636

TRANSBRASIL (TBL)

1 VL001-VL002

UPS (UPS)

2 VR201-VR209 VW701-VW721

US AIRWAYS (USA)

1 VE141-VE151

2 VE152

VARIG AIRLINES (VAR)

1 VE121-VE126 VN055-VN056 VN231-VN234

VIETNAM AIRLINES (VIE)

2 VL751-VL752 VL754

IDENTIFICATION BY VARIABLE NUMBER

GROUP 1

VB331-VB332 VE121-VE126 VE141-VE151 VF001-VF002 VF041-VF042 VF051

VK081-VK102 VK131-VK133 VK141-VK142 VL001-VL006 VN001-VN028

VN051-VN064 VN081-VN093 VN191-VN195 VN231-VN234 VN291 VN301-VN308

VN471-VN472 VN651-VN652 VN731 VN751-VN753 VN791-VN792 VN811-VN813

GROUP 2 *

VB441-VB444 VE152 VF171_VF172 VF180-VF184 VF251 VK012-VK016

VK103-VK113 VK143-VK148 VK181 VK186 VL701-VL703 VL751-VL755

VL891-VL900 VL911-VL914 VL941 VN029-VN041 VN094-VN099 VN196-VN198

VN292-VN293 VN309-VN314 VN421-VN427 VN436 VN546-VN547 VN634-VN638

VN653-VN658 VN676 VN732 VN921-VN922 VN951-VN953 VN968-VN970

VR051-VR058 VR201-VR209 VR251 VR256-VR257 VR401 VR426

VR441 VR461 VS051-VS056 VS073-VS078 VS111-VS113 VS131-VS133

VS136-VS137 VS176-VS177 VS186-VS187 VS196-VS203 VS216-VS217 VS231

VS261-VS262 VS266-VS274 VS291-VS292 VS316 VS321-VS324 VS331

VS366-VS367 VS381-VS382 VS391-VS392 VS401 VS466-VS471 VS486

VS526 VS546-VS548 VW701-VW721 VW851 VY999

July 24, 1997 767-78A0081

Revision 2: April 19, 2001 4
ALERT BOEING SERVICE BULLETIN 767-78A0081 ALERT

2. Spares

None

July 24, 1997 767-78A0081

Revision 2: April 19, 2001 5
ALERT BOEING SERVICE BULLETIN 767-78A0081 ALERT

B. Concurrent Requirements

None

C. Reason

This inspection will make sure that the center drive unit (CDU) cone brake and the Thrust Reverser

Actuation System (TRAS) brake have the holding torque required to prevent any uncommanded

thrust reverser sleeve movement.

The CDU cone brake and the TRAS brake are primary safety devices required to prevent inadvertent

thrust reverser sleeve movement. To meet the system reliability requirements, periodic torque

checks are required to ensure the integrity of these locking devices. A failure of either of these locks

is not detected during normal operation. The torque check intervals have been determined through

industry-wide accepted probability and reliability methods.

The TRAS lock is a solenoid activated disk brake this is connected to the upper angle gearbox by a

flexible drive shaft. The brake is released when 28 VDC is applied from the control circuit and is

locked at all other times. Low torque can be the result of a brake or flexible shaft failure.

The CDU cone brake is a spring load, unidirectional device that prevent rotation of the air motor in the

deploy direction. The cone brake always allows the air motor to rotate in the stow direction. The

brake is disengaged when the directional control valve actuator piston is commanded to the deploy

position from the control circuit.

Boeing Service Related Problem (SRP) 767-SRP-78-0036 is related to this service bulletin.

Revision 1 is sent to change the inspection interval for the CDU cone brake test from 600 to 650 flight

hours to coincide with operators maintenance schedule.

Revision 2 adds the inspection interval of the Electro-Mechanical brake and CDU cone brake for

airplanes equipped with thrust reversers that have been modified in accordance with Boeing Service

Bulletin 767-78-0063 or after the equivalent modification (Production Revision Record B11481-90)

incorporating in production. Revise the service bulletin effectivity to add Group 2 airplanes which is

included all 767-200, -300 and -300F airplanes (including future 767-200, -300 and -300F airplanes)

with CF6-80C2 engines from production control line 475. Also, the Industry Support Information

statement has been changed.

D. Description

For Group 1 airplanes that have not incorporated Boeing Service Bulletin 767-78-0063, on each

thrust reverser half, do a functional test on the CDU cone brake to verify the holding torque.

For Group 1 airplanes that have incorporated Boeing Service Bulletin 767-78-0063 and Group 2

airplanes, on each thrust reverser half, do a functional test of the Electro-Mechanical brake and CDU

cone brake to verify the holding torque.

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

service bulletin.

Revision 2 - More work is necessary on airplanes changed as shown in the Revision 1 of this service

bulletin.

An evaluation form is attached to this service bulletin. Please use this form to tell us what you think

of the quality of this service bulletin.

July 24, 1997 767-78A0081

Revision 2: April 19, 2001 6
ALERT BOEING SERVICE BULLETIN 767-78A0081 ALERT

E. Compliance

Boeing recommends the operators do this service bulletin within 650 flight hours after receipt of this

service bulletin.

For Group 1 airplanes that have not incorporated Boeing Service Bulletin 767-78-0063, Boeing

recommends the operators repeat CDU cone brake test every 650 flight hours.

For Group 1 airplanes on which Boeing Service Bulletin 767-78-0063 has been incorporated and on

Group 2 airplanes, Boeing recommends the operators repeat the Electro-Mechanical brake and CDU

cone brake tests every 1,000 flight hours.

Federal Aviation Administration (FAA) Airworthiness Directive (AD) 2000-09-04, Amendment

39-11712, is related to this service bulletin.

F. Approval

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

specified in this service bulletin comply with the applicable Federal Aviation Regulations (FAR) and

are FAA approved. This service bulletin and the FAA approval were based on the airplane in its

original Boeing delivery configuration or as modified by other FAA 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 FAA Seattle

Aircraft Certification Office approves the inspection and tests defined in this service bulletin as an

alternative method of compliance to the requirements of paragraphs (d)(2), (f) and (g) of AD

2000-09-04. All provisions of AD 2000-09-04 that are not specifically referenced in the above

sentence remain fully applicable and must be complied with.

G. Manpower

Approximately 6 man-hours and 2 persons are necessary to do this test for each airplane.

Time does not include CDU replacement.

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

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

lost time:

- Time to adjust to the workplace

- Time to schedule the work

- Time to examine the work

- Time to cure the materials

- Time to make the parts

- Time to find the tools.

H. Weight and Balance Changes

None

I. Electrical Load Data

Not changed

July 24, 1997 767-78A0081

Revision 2: April 19, 2001 7
ALERT BOEING SERVICE BULLETIN 767-78A0081 ALERT

J. References

1. Existing Data:

a. Service Related Problem (SRP) 767-SRP-78-0036

b. 767 Maintenance Manual (AMM) Subject 71-11-04, 78-31-21

c. Boeing Service Bulletin 767-78-0047, "Thrust Reverser (CF6-80C2 Engines) - Thrust Reverser

Control System - Operational Test"

d. Boeing Service Bulletin 767-78-0063, "Exhaust (GE CF6-80C2 Engines) - Thrust Reverser -

Lock Installation"

2. Data supplied with this service bulletin:

None

3. Installation Drawings:

None

K. Publications Changed

None

L. Interchangeability and Intermixability of Parts

Refer to Paragraph 2.E., Existing Parts Accountability, for interchangeability and intermixability

information.

July 24, 1997 767-78A0081

Revision 2: April 19, 2001 8
ALERT BOEING SERVICE BULLETIN 767-78A0081 ALERT

2. MATERIAL INFORMATION

A. Material - Price and Availability

None

B. Industry Support Information

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

C. Parts Necessary For Each Airplane

Parts and Materials Supplied by the Operator:

NOTE: Part quantity dependent on test result.

Quantity Part Number Name

4 126784-() Center Drive Unit (a)

(a) Replace this part when the holding torque is less than 15 pound inches.

D. Parts Necessary to Change Spares

None

E. Existing Parts Accountability

None

F. Special Tooling - Price and Availability

None

G. 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.

July 24, 1997 767-78A0081

Revision 2: April 19, 2001 9
ALERT BOEING SERVICE BULLETIN 767-78A0081 ALERT

3. ACCOMPLISHMENT INSTRUCTIONS

GENERAL NOTES

1. The lettered paragraphs contain the test to be accomplished at the specifies interval.

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

3. For Group 1 airplanes that have not incorporated Boeing Service Bulletin 767-78-0063, repeat

CDU cone brake test every 650 flight hours.

For Group 1 airplanes on which Boeing Service Bulletin 767-78-0063 has been incorporated and

on Group 2 airplanes, repeat the Electro-Mechanical brake and CDU cone brake tests every 1,000

flight hours.

4. Refer to Compliance Paragraph for recommendation and repeat inspection requirements.

WORK INSTRUCTIONS

A. Do the functional test on both thrust reverser for the Electro-Mechanical brakes of both engines as

follows:

1. Open the engine fan cowl panels as shown in 767 Maintenance Manual Subject 71-11-04 or

your own equivalent procedure.

2. Do a check of the running torque of the thrust reverser system:

a. Manually extend the thrust reverser six inches and measure the running torque. Make sure

the torque is less than 10 pound-inches.

3. Do a check of the electro-mechanical brake holding torque:

a. Make sure the thrust reverser translating cowl is extended at least one inch.

b. Make sure the CDU lock handle is released.

c. Pull down on the manual release handle on the electro-mechanical brake until the handle

fully engages the retaining clip.

NOTE: This will lock the electro-mechanical brake.

d. With the manual drive lockout cover removed from the CDU, install a 1/4-inch extension tool

and dial -type torque wrench into the drive pad.

NOTE: You will need a 24-inch extension to provide adequate clearance for the torque

wrench.

e. Apply 90 pound-inches of torque to the system.

1) The electro-mechanical brake system is working correctly if the torque is reached before

you turn the wrench 450 degrees (1-1/4 turns).

2) If the flexshaft turns more than 450 degrees (1-1/4 turns) before you reach the specified

torque, you must replace the long flexshaft between the CDU and the upper angle

gearbox.

July 24, 1997 767-78A0081

Revision 2: April 19, 2001 10
ALERT BOEING SERVICE BULLETIN 767-78A0081 ALERT

3) If you do not get 90 pound-inches of torque, inspect the short flexshaft between the

upper angle gearbox and the electro-mechanical brake. If the flexshaft is twisted, broken

or otherwise damaged, replace the flexshaft and repead (e). If you still do not get 90

pound-inches of torque, you must replace the electro-mechanical brake.

f. Release the torque by turning the wrench in the position direction until you read zero

pound-inches.

1) If the wrench does not turn to within 30 degrees of initial starting point, you must replace

the long flexshaft between the CDU and upper angle gearbox.

4. Fully retract the thrust reverser.

5. Repeat this procedure on other reverser half and on the remaining engines.

6. End the Electro-Mechanical brake check.

B. For Group 1 airplanes on which Boeing Service Bulletin 767-78-0063 has been incorporated and

on Group 2 airplanes, repeat the Electro-Mechanical brake test at 1,000 flight hours intervals

C. Do the functional test on both thrust reverser for the Center Drive Unit (CDU) cone brakes of both

engines as follows:

1. Pull up on the manual release handle to unlock the electro-mechanical brake (if so equipped).

2. Pull the manual brake release lever on the CDU to release the cone brake. Refer to Figure 1

for location.

NOTE: This will release the pre-load tension that may occur during a stow cycle.

3. Return the manual brake release lever to the locked position to engage the cone brake. Refer

to Figure 1 for location.

4. Remove the two bolts that hold the lockout plate to the CDU and remove the lockout plate.

Refer to Figure 1 for location.

5. Install a 1/4-inch drive and a dial-type torque wrench into the CDU drive pad.

WARNING: Do not use more than 100 pound-inches of torque when carrying out this check.

Excessive torque will damage the CDU.

6. Turn the torque wrench to try to manually extend the translating cowl until you get at least 15

pound-inches of torque.

NOTE: The cone brake prevents movement in the extend direction only. If you try to measure

the torque in the retract direction, you will get a false reading.

7. If the sleeve translates to deploy with a torque less than 15 pound inches you must replace the

CDU. Refer to 767 Maintenance Manual Subject 78-31-21.

8. Reinstall the lockout plate.

9. Fully retract the thrust reverser.

10. Pull down on the manual release handle on the electro-mechanical brake until the handle fully

engages the retaining clip (if so equipped).

NOTE: This will lock the electro-mechanical brake.

July 24, 1997 767-78A0081

Revision 2: April 19, 2001 11
ALERT BOEING SERVICE BULLETIN 767-78A0081 ALERT

11. Repeat this procedure on other reverser half and on the remaining engines.

12. Close the engine fan cowl panels as shown in 767 Maintenance Manual Subject 71-11-04 or

your own equivalent procedure.

13. End the CDU cone brake check.

D. For Group 1 airplanes that have not incorporated Boeing Service Bulletin 767-78-0063, repeat

CDU cone brake test every 650 flight hours.

E. For Group 1 airplanes on which Boeing Service Bulletin 767-78-0063 has been incorporated and

on Group 2 airplanes, repeat CDU cone brake tests every 1,000 flight hours.

July 24, 1997 767-78A0081

Revision 2: April 19, 2001 12
ALERT BOEING SERVICE BULLETIN 767-78A0081 ALERT

FIGURE TABLE OF CONTENTS

Title Page

FIGURE 1. ELECTRO-MECHANICAL BRAKE, CDU MANUAL BRAKE RELEASE

LEVER, LOCKOUT PLATE AND DRIVE PAD LOCATIONS . . . . . . . . . . . . . 14

July 24, 1997 767-78A0081

Revision 2: April 19, 2001 13
ALERT BOEING SERVICE BULLETIN 767-78A0081 ALERT

UPPER ANGLE GEARBOX

ELECTRO-MECHANICAL BRAKE

(LEFT SIDE SHOWN,

RIGHT SIDE TURNED 180 DEGREES)

CENTER

(CDU)

DRIVE UNIT

DRIVE PAD

PLATE AND

LOCKOUT

BRAKE RELEASE

CDU MANUAL

LEVER

CENTER DRIVE UNIT

S13037

FIGURE 1. ELECTRO-MECHANICAL BRAKE, CDU MANUAL BRAKE RELEASE LEVER, LOCKOUT

PLATE AND DRIVE PAD LOCATIONS

July 24, 1997 SHEET 1 OF 1 767-78A0081

Revision 2: April 19, 2001 14
Commercial

Airplane

Group

767

Service Bulletin

Number: 767-78A0081 Evaluation Form

Date: July 24, 1997

Revision 2: April 19, 2001

ATA System: 7830

Prepared By: Phuoc Tran

SUBJECT: EXHAUST (CF6-80C2 Engines) - Thrust Reverser - Thrust Reverser Control System - Center

Drive Unit (CDU) Cone Brake Integrity Test

Use this evaluation form to tell us what you think of the quality of this service bulletin. We will use the data

that you give us to improve the quality of our service bulletins.

NOTE: Please do not use this evaluation form to tell us to make changes to your manuals. To make these

changes, please use a Publication Change Request (PCR) form.

Please give us this data:

(If necessary, please use the other side. Thank you for the time you used to give us your comments.)

OPERATOR: TODAY'S DATE:

PREPARED BY: TITLE:

ORGANIZATION: TELEX CODE:

TELEPHONE NUMBER: BASE:

Please rate the quality of this service bulletin: (good) 4321 (poor)

Please rate the quality of the illustrations: (good) 4321 (poor)

Will you do the change given by this service bulletin? Yes No If not, please explain:

Is this service bulletin easy to understand? Yes No If not, please explain:

Is this service bulletin easy to use? Yes No If not, please explain:

Are the Planning Information, Material Information, and

Accomplishment Instructions accurate? Yes No If not, please explain:

Is the Manpower estimate accurate? Yes No If not, please explain:

Give the completed evaluation form to your Boeing Field Service Representative or send the evaluation form

directly to this address:

Manager

Service Bulletin Engineering

Boeing Commercial Airplane Group

P.O. Box 3707, Mail Stop 2H-37

Seattle, WA 98124-2207