### Commercial **Airplane Group**  

# 767 Service Bulletin **Number: 767-27-0202** Date: June 25, 2007 Revision 1: February 21, 2008 ATA System: 2731 **SUBJECT:** FLIGHT CONTROLS - Elevator - Repetitive Mis-Rig Check Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15 CFR 730-774). An export license may be required before it is used for development, production or use by foreign persons from specific countries. The controller of this data has the individual responsibility to abide by all export laws. 9E991 ECCN: 

## BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET Copyright © 2007 The Boeing Company Unpublished Work - All Rights Reserved Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter.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, MD-10, MD-11, MD-80, MD-88, MD-90, and the Boeing livery are all trademarks owned by The Boeing Company; and no trademark license is granted in connection with this document unless provided in writing by Boeing.

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 1 of 24 2.0BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 2 of 24 **BOEING SERVICE BULLETIN 767-27-0202**

BLANK PAGE**Table of Contents** Revision Transmittal Sheet ............................................ 5 Summary ..................................................... 7 1. PLANNING INFORMATION......................................... 9 A. Effectivity................................................ 9 1. Airplanes............................................. 9 2. Spares Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15 B. Concurrent Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15 C. Reason . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16 D. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16 E. Compliance. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17 F. Approval . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17 G. Manpower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18 H. Weight and Balance Changes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18 I. Electrical Load Data. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18 J. References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18 1. Existing Data:. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18 2. Data supplied with this Service Bulletin: . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 3. Installation Drawings Used in the Preparation of this Service Bulletin:. . . . . . . . . . . 19 K. Publications Affected. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 L. Interchangeability and Intermixability of Parts . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 2. MATERIAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 A. Material - Price and Availability. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 B. Industry Support Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 C. Parts Necessary For Each Airplane. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 1. Kits/Parts:. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 2. Parts and Materials Supplied by the Operator:. . . . . . . . . . . . . . . . . . . . . . . . 21 3. Parts Modified and Reidentified:. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 4. Parts Removed and Not Replaced: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 D. Parts Necessary to Change Spares. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 E. Special Tooling - Price and Availability. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 F. Special Tooling Necessary to do this Service Bulletin. . . . . . . . . . . . . . . . . . . . . . . 21 3. ACCOMPLISHMENT INSTRUCTIONS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23 A. GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23 B. WORK INSTRUCTIONS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 3 of 24 **BOEING SERVICE BULLETIN 767-27-0202**BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 4 of 24 **BOEING SERVICE BULLETIN 767-27-0202**

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### Commercial **Airplane Group**  

# 767 Service Bulletin **Revision Transmittal Sheet Number: 767-27-0202**  Date: June 25, 2007 Revision 1: February 21, 2008 ATA System: 2731 **SUBJECT:** FLIGHT CONTROLS - Elevator - Repetitive Mis-Rig Check This revision includes all pages of the service bulletin. **COMPLIANCE INFORMATION RELATED TO THIS REVISION** No more work is necessary on airplanes changed as shown in the original issue of this service bulletin. **REASON FOR REVISION** This revision is sent to clarify Paragraph 1.E., Compliance. 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** June 25, 2007 Original Issue: February 21, 2008 Revision 1:

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 5 of 24BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 6 of 24 **BOEING SERVICE BULLETIN 767-27-0202**

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### Commercial **Airplane Group**  

# 767 Service Bulletin **Summary Number: 767-27-0202**  Date: June 25, 2007 Revision 1: February 21, 2008 ATA System: 2731 **SUBJECT:** FLIGHT CONTROLS - Elevator - Repetitive Mis-Rig Check **CONCURRENT REQUIREMENTS** Refer to Paragraph 1.B., Concurrent Requirements. **BACKGROUND** This service bulletin gives instructions to do repetitive checks of the elevator Power Control Actuator (PCA) rigging to determine if there is a mis-rig condition. As an alternative to Boeing Alert Service Bulletin 767-27A0168, the incorporation of Boeing Service Bulletin 767-27-0186 to replace or rework the elevator PCA bellcranks combined with the repetitive check of the elevator PCA input rod assemblies recommended in Boeing Service Bulletin 767-27-0200 and the repetitive check of the elevator PCA rigging recommended in this service bulletin will prevent continued operation with yielded or failed shear rivets in a bellcrank assembly for the elevator PCA and will also allow for longer inspection intervals. Operators are currently required by the Federal Aviation Administration (FAA) Airworthiness Directive (AD) 2001-04-09 to do the 400 flight-hour repetitive check recommended in Boeing Alert Service Bulletin 767-27A0168. One operator reported the left elevator drooping during a preflight check. Examination of the elevator control system found sheared rivets in the left-inboard and center PCA bellcrank assemblies. The elevator single hydraulic system check required by a Certification Maintenance Requirement (CMR) may not detect yielded or failed shear rivets in the bellcrank assemblies for the elevator PCA. As a result, the FAA issued AD 2000-17-05 to mandate the accomplishment of the actions specified in Boeing Alert Service Bulletin 767-27A0166, dated August 17, 2000. Since the issuance of AD 2000-17-05, the FAA has received reports that several 767-200, 767-300, and 767-300F airplanes failed the one-time functional check of the shear rivets required by the AD. As a result, the FAA issued AD 2001-04-09 to mandate the accomplishment of the actions specified in Boeing Alert Service Bulletin 767-27A0168, dated November 21, 2000. A detailed review found that the override device incorporated into the elevator PCA input rod assembly of the PCA provides protection against malfunctions and non-normal PCA operation. This design review also found that the shear rivets are not needed.The completion of Boeing Service Bulletin 767-27-0186 to replace or rework elevator PCA bellcranks combined with the repetitive check of the elevator PCA input rod assemblies recommended in Boeing Service Bulletin 767-27-0200 and the repetitive check of the elevator PCA rigging recommended in this service bulletin is an alternative to the 400 flight-hour repetitive check recommended in Boeing Alert Service Bulletin 767-27A0168. Boeing Service Related Problem (SRP) 767-SRP-27-0128 is related to this service bulletin.

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 7 of 24**ACTION (PRR B12901-35S)** Do a check of the elevator power control actuator (PCA) rigging. **EFFECTIVITY** 767-200, -300, and -300F Airplanes. Refer to Paragraph 1.A.1 Airplanes, for the list of affected airplanes. **COMPLIANCE** Federal Aviation Administration (FAA) Airworthiness Directive 2001-04-09 is related to this service bulletin. The FAA will possibly release a new Airworthiness Directive related to this service bulletin. The new Airworthiness Directive will make the compliance tasks and times given in this service bulletin mandatory. See Service Bulletin Paragraph 1.E. for compliance information. **INDUSTRY SUPPORT INFORMATION** Boeing warranty remedies are not available for the inspection, and/or repair procedures given in this service bulletin. **MANPOWER Elapsed Hours**  **Total Task Hours** 1.0 2.0
**MATERIAL INFORMATION** None.

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 8 of 24 **BOEING SERVICE BULLETIN 767-27-0202**

### Commercial **Airplane Group**  

# 767 Service Bulletin **Number: 767-27-0202** Date: June 25, 2007 Revision 1: February 21, 2008 ATA System: 2731 **SUBJECT:** FLIGHT CONTROLS - Elevator - Repetitive Mis-Rig Check **1. PLANNING INFORMATION A. Effectivity**  1. Airplanes Refer to Service Bulletin Index Document D624T001 Part 3 for Airplane Variable Number, Line Number, and Serial Number data. This service bulletin is for the airplanes shown below. Refer to PRR B12901-35S for data about this change. **NO TE:**  This service bulletin is for the airplanes identified below. The effectivity list shown below is complete for airplanes through line number 967. Airplanes after line number 967 are also affected by this service bulletin.These airplanes will be added to the service bulletin's MyBoeingFleet.com (MBF) "get effectivity" result when they are added to the MBF Fleet Profile Page. **NO TE:**  This Service Bulletin is for the airplanes identified below. The Effectivity list shown below is complete for airplanes through line number 967. Airplanes after line number 967 are also affected by this service bulletin, and are in Group(s): 1,2
**DESCRIPTION CONFIGURATION**  **GROUP** 767-200, -300 and -300F airplanes line numbers 1-901 require incorporation of SB 767-27-0186. - 1

767-200, -300 and -300F airplanes line numbers 902 and on do not require SB 767-27-0186. Intent of SB 767-27-0186 was done in production for these airplanes. - 2

Airplane Models: 767-200, 767-300, 767-300F **Group Variable Number**  1 VA001 - VA012

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 9 of 24**Group Variable Number**  1 VA014 - VA020 1 VA301 - VA315 1 VA501 - VA523 1 VA525 1 VA527 - VA530 1 VA701 - VA719 1 VA801 1 VA803 - VA804 1 VA806 - VA810 1 VB001 - VB002 1 VB051 1 VB053 - VB055 1 VB101 - VB123 1 VB125 1 VB201 - VB202 1 VB281 - VB284 1 VB301 - VB302 1 VB321 1 VB323 1 VB325 - VB332 1 VB371 - VB373 1 VB441 - VB444 1 VE001 - VE002 1 VE021 - VE023 1 VE041 1 VE061 1 VE063 - VE064 1 VE066 - VE069 1 VE083 - VE086 1 VE101 - VE104 1 VE116 - VE118 1 VE121 - VE126 1 VE141 - VE149

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 10 of 24 **BOEING SERVICE BULLETIN 767-27-0202 Group**  **Variable Number** 1 VE151 - 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 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

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 11 of 24 **BOEING SERVICE BULLETIN 767-27-0202 Group**  **Variable Number** 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 1 VN221 - VN225 1 VN231 - VN234 1 VN242 - VN243 1 VN251 - VN276 1 VN291 - VN293 1 VN301 - VN314 1 VN371 - VN372 1 VN376 1 VN381 - VN388 1 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

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 12 of 24 **BOEING SERVICE BULLETIN 767-27-0202 Group**  **Variable Number** 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 VR051 - VR060 1 VR081 2 VR084 2 VR086 - VR089 2 VR106 - VR109 1 VR201 - VR211 1 VR251 1 VR256 - VR260 1 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

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 13 of 24 **BOEING SERVICE BULLETIN 767-27-0202 Group**  **Variable Number** 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 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 - VS703 2 VS704 - VS718 1 VS721 - VS728 2 VS729 - VS734 1 VS751 - VS753 2 VS754 - VS759

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 14 of 24 **BOEING SERVICE BULLETIN 767-27-0202 Group**  **Variable Number** 1 VS821 - VS824 2 VS825 1 VS841 - VS843 2 VS844 2 VS861 2 VS881 - VS883 2 VS891 2 VS896 2 VS901 - VS908 2 VS911 - VS912 2 VS916 1 VT501 2 VT511 - VT513 2 VT521 - VT523 2 VT531 - VT533 1 VW701 - VW721 1 VW851 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: **Group 1: Description**  **Service Bulletin Company**  Elevator Power Control Actuator Bellcrank replacement 767-27-0186 Original Issue Boeing

**Group 2:** None.The changes given in Boeing Service Bulletin 767-27-0186 were made on these airplanes before delivery.

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 15 of 24 **BOEING SERVICE BULLETIN 767-27-0202 C. Reason**  This service bulletin gives instructions to do repetitive checks of the elevator Power Control Actuator (PCA) rigging to determine if there is a mis-rig condition. As an alternative to Boeing Alert Service Bulletin 767-27A0168, the incorporation of Boeing Service Bulletin 767-27-0186 to replace or rework the elevator PCA bellcranks combined with the repetitive check of the elevator PCA input rod assemblies recommended in Boeing Service Bulletin 767-27-0200 and the repetitive check of the elevator PCA rigging recommended in this service bulletin will prevent continued operation with yielded or failed shear rivets in a bellcrank assembly for the elevator PCA and will also allow for longer inspection intervals. Operators are currently required by the Federal Aviation Administration (FAA) Airworthiness Directive (AD) 2001-04-09 to do the 400 flight-hour repetitive check recommended in Boeing Alert Service Bulletin 767-27A0168. One operator reported the left elevator drooping during a preflight check. Examination of the elevator control system found sheared rivets in the left-inboard and center PCA bellcrank assemblies. The elevator single hydraulic system check required by a Certification Maintenance Requirement (CMR) may not detect yielded or failed shear rivets in the bellcrank assemblies for the elevator PCA. As a result, the FAA issued AD 2000-17-05 to mandate the accomplishment of the actions specified in Boeing Alert Service Bulletin 767-27A0166, dated August 17, 2000. Since the issuance of AD 2000-17-05, the FAA has received reports that several 767-200, 767-300, and 767-300F airplanes failed the one-time functional check of the shear rivets required by the AD. As a result, the FAA issued AD 2001-04-09 to mandate the accomplishment of the actions specified in Boeing Alert Service Bulletin 767-27A0168, dated November 21, 2000. A detailed review found that the override device incorporated into the elevator PCA input rod assembly of the PCA provides protection against malfunctions and non-normal PCA operation.This design review also found that the shear rivets are not needed.The completion of Boeing Service Bulletin 767-27-0186 to replace or rework elevator PCA bellcranks combined with the repetitive check of the elevator PCA input rod assemblies recommended in Boeing Service Bulletin 767-27-0200 and the repetitive check of the elevator PCA rigging recommended in this service bulletin is an alternative to the 400 flight-hour repetitive check recommended in Boeing Alert Service Bulletin 767-27A0168. Boeing Service Related Problem (SRP) 767-SRP-27-0128 is related to this service bulletin. Revision 1 is sent to clarify Paragraph 1.E., Compliance. **D. Description** Do a check of the elevator power control actuator (PCA) rigging. Revision 1 - No more work is necessary on airplanes changed as shown in the original issue of this service bulletin.
**Affected Maintenance Zones Zone**  **Model** 336, 337, 346, 347 767-200, 767-300, 767-300F

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 16 of 24 **BOEING SERVICE BULLETIN 767-27-0202 E. Compliance**  **Group 1:** Boeing recommends this check be done within 6,000 flight hours after completion of Boeing Service Bulletin 767-27-0186.Thereafter, Boeing recommends that this check be done within every 6,000 flight hours. **Group 2:** Boeing recommends this check be done at the latest of the following times: **Group 2:** 1. Within 6,000 flight hours after completion of the previous mis-rig check in the original release of this service bulletin, or 2. Within 6,000 flight hours after the bellcrank repetitive check identified in Service Bulletin 767-27A0168, or 3. Within 6,000 flight hours after the date of issuance of the original standard certificate of airworthiness or the original export certificate of airworthiness. **Group 2:** Thereafter, Boeing recommends that this check be repeated at intervals not to exceed 6,000 flight hours. Federal Aviation Administration (FAA) Airworthiness Directive 2001-04-09 is related to this service bulletin. The FAA will possibly release a new Airworthiness Directive related to this service bulletin. The new Airworthiness Directive will make the compliance tasks and times given in this service bulletin mandatory. **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 FAA Seattle Aircraft Certification Office approves the action (i.e. inspection or modification) defined in this service bulletin combined with the actions defined in Boeing Service Bulletins 767-27-0186 and 767-27-0200 as an alternative method of compliance to the requirements of paragraph (a) of AD 2001-04-09. All provisions of AD 2001-04-09 that are not specifically referenced in the above statement remain fully applicable and must be complied with.

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 17 of 24 **BOEING SERVICE BULLETIN 767-27-0202 G. Manpower**  The table below shows an estimate of the task-hours necessary to do the mis-rig check 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 examine the work — Time to find the tools. **Group 1-2: Elapsed Hours**  **Task-Hours Number of**  **Persons Task**  **Work Package Number**  0.5 1.0 2 Check for Mis-Rig 1 0.5 1.0 TOTAL FOR WORK PACKAGE 1
0.5 1.0 2 Check for Mis-Rig 2 0.5 1.0 TOTAL FOR WORK PACKAGE 2
1.0 2.0 TOTAL FOR EACH AIRPLANE **H. Weight and Balance Changes** None. **I. Electrical Load Data** Not changed. **J. References** 1. Existing Data: a. Engineering Change Memo PRR B12901-35S b. 767 Aircraft Maintenance Manual (AMM) 27-31-00 c. 767 Maintenance Planning Data (MPD) 1Appendix G d. Service Related Problem (SRP) 767-SRP-27-0128 e. Boeing Service Bulletin 767-27A0166 f. Boeing Service Bulletin 767-27A0168 g. Boeing Service Bulletin 767-27-0186

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 18 of 24 **BOEING SERVICE BULLETIN 767-27-0202**h. Boeing Service Bulletin 767-27-0200 i. FAA Airworthiness Directive 2000-17-05 j. FAA Airworthiness Directive 2001-04-09 2. Data supplied with this Service Bulletin: None. 3. Installation Drawings Used in the Preparation of this Service Bulletin: None. **K. Publications Affected** None. **L. Interchangeability and Intermixability of Parts** Accomplishment of this service bulletin does not affect interchangeability or intermixability of parts.

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 19 of 24 **BOEING SERVICE BULLETIN 767-27-0202**BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 20 of 24 **BOEING SERVICE BULLETIN 767-27-0202**

BLANK PAGE**2. MATERIAL INFORMATION A. Material - Price and Availability**  None. **B. Industry Support Information** Boeing warranty remedies are not available for the inspection, and/or repair procedures given in this service bulletin. **C. Parts Necessary For Each Airplane** 1. Kits/Parts: None. 2. Parts and Materials Supplied by the Operator: None. 3. Parts Modified and Reidentified: None. 4. Parts Removed and Not Replaced: None. **D. Parts Necessary to Change Spares** 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.

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 21 of 24 **BOEING SERVICE BULLETIN 767-27-0202**BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 22 of 24 **BOEING SERVICE BULLETIN 767-27-0202**

BLANK PAGE**3. ACCOMPLISHMENT INSTRUCTIONS A. GENERAL INFORMATION**  **W**

**ARNING:** KEEP PERSONS AND EQUIPMENT AWAY FROM ALL CONTROL SURFACES WHEN HYDRAULIC POWER IS SUPPLIED. AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS, SPOILERS AND STABILIZER ARE FULLY POWERED SURFACES. INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR WHEN HYDRAULIC POWER IS SUPPLIED. **CA UTION:**  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. **NO TE:**  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. The work instructions are divided into work packages.Task-Hours and Elapsed-Hours for each package are given in Paragraph 1.G., Manpower.You can do each work package independently or at the same time.The work instructions for the left and right elevators are the same and both work packages need to be completed before the plane is returned to service. 4. 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 "as given in" are included in the instruction, the procedure in the Boeing document must be used. **B. WORK INSTRUCTIONS W** **ORK P A** **CKA GE 1 - LEFT ELEV**  **A**

**T OR MIS-RIG CHECK**  1. Do a check of the elevator Power Control Actuator (PCA) rigging. Refer to "Functional Test - Elevator PCA Mis-Rig" in 767 AMM 27-31-00 as an accepted procedure. a. If a mis-rig condition is found, do the following steps:

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 23 of 24 **BOEING SERVICE BULLETIN 767-27-0202**(1) Adjust the PCA Input Rod Assemblies. Refer to 767 AMM 27-31-00 as an accepted procedure. (2) Do the Structural Inspection MPD Items 5510-335-01I and 5510-345-01I. Refer to 767 MPD 1 Appendix G as an accepted procedure. 2. Put the airplane back to a serviceable condition. **W ORK P**  **A CKA** **GE 2 - RIGHT ELEV A** 

**T OR MIS-RIG CHECK**  1. Do a check of the elevator PCA rigging. Refer to "Functional Test - Elevator PCA Mis-Rig" in 767 AMM 27-31-00 as an accepted procedure. a. If a mis-rig condition is found, do the following steps: (1) Adjust the PCA Input Rod Assemblies. Refer to 767 AMM 27-31-00 as an accepted procedure. (2) Do the Structural Inspection MPD Items 5510-335-01I and 5510-345-01I. Refer to 767 MPD 1 Appendix G as an accepted procedure. 2. Put the airplane back to a serviceable condition.

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. June 25, 2007 767-27-0202 Revision 1: February 21, 2008 24 of 24 **BOEING SERVICE BULLETIN 767-27-0202**