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Commercial Airplanes 767 Requirements Bulletin
SPECIAL ATTENTION Number: 767-25-0589 RB Original Issue: February 25, 2022 ATA System: 2510 1131 SUBJECT: EQUIPMENT/FURNISHINGS - Flight Compartment - First Observer Seat Positions Marker Installation EXPORT CONTROLLED - This technology or software is subject to the U.S. Export Administration Regulations (EAR), (15 C.F.R. Parts 730-774). No authorization from the U.S. Department of Commerce is required for export, re-export, in-country transfer, or access EXCEPT to country group E:1 or E:2 countries/persons per Supp.1 to Part 740 of the EAR.
9E991ECCN:
Copyright © 2022 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Unpublished Work.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, Dreamliner, BBJ, DC-8, DC-9, DC-10, KC-10, KC-46, KDC-10, MD-10, MD-11, MD-80, MD-88, MD-90, P-8, 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.
Original Issue: February 25, 2022 767-25-0589 RB 1 of 13
2.0
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 25, 2022 767-25-0589 RB 2 of 13 REQUIREMENTS BULLETIN 767-25-0589
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Table of Contents
1. EFFECTIVITY5
A. Airplanes5
B. Spares Affected6
2. CONCURRENT REQUIREMENTS6
3. COMPLIANCE6
4. APPROVAL6
5. ACCOMPLISHMENT INSTRUCTIONS7
A. General Information7
B. Work Instructions8
FIGURE 1: FLIGHT DECK - MARKERS FOR FIRST OBSERVER SEAT INSTALLATION10
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 25, 2022 767-25-0589 RB 3 of 13 REQUIREMENTS BULLETIN 767-25-0589
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 25, 2022 767-25-0589 RB 4 of 13 REQUIREMENTS BULLETIN 767-25-0589
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Commercial Airplanes 767 Requirements Bulletin
SPECIAL ATTENTION Number: 767-25-0589 RB Original Issue: February 25, 2022 ATA System: 2510 1131 SUBJECT: EQUIPMENT/FURNISHINGS - Flight Compartment - First Observer Seat Positions Marker Installation BOEING RECOMMENDS THAT EACH OPERATOR EXAMINE THIS DOCUMENT IMMEDIATELY. THIS IS AN ENHANCED REQUIRED FOR COMPLIANCE DOCUMENT. THE BOEING PROCESSES USED TO CREATE
THE SERVICE BULLETIN (SB) AND THE REQUIREMENTS BULLETIN (RB) ENSURE THAT THE INFORMATION BETWEEN "RC START" AND "RC END" IN THE SB ARE IDENTICAL TO THE INFORMATION IN THE SAME SECTIONS (COMPLIANCE, WORK INSTRUCTIONS…) OF THE RB WHICH THE SB REFERS TO AS THE RELATED DOCUMENT.
1. Effectivity A. Airplanes This bulletin is applicable to 767-300F Airplane(s), line number(s) 580, 590, 594, 598, 600, 616, 622, 624, 626, 628, 630, 632, 634, 636, 638, 640, 660, 666, 670, 672, 674, 678, 682, 712, 724, 726, 728, 730, 732, 756, 760, 764, 778, 806, 846, 848, 854, 858, 860, 885, 934, 936-937, 939, 947-948, 956, 959-960, 979, 983, 986, 988-989, 991-992, 1002-1003, 1005-1006, 1008, 1020, 1022, 1024-1026, 1028, 1035, 1044, 1046, 1048, 1051, 1053, 1056-1059, 1061, 1063-1064, 1070-1090, 1093-1097, 1099, 1101, 1103, 1105-1106, 1108, 1110, 1112, 1115, 1118, 1121, 1123, 1125, 1127, 1130, 1133, 1136, 1138, 1140-1142, 1144, 1146, 1148, 1150, 1152-1153, 1155, 1157, 1159, 1161, 1163, 1165, 1167, 1169, 1171, 1173, 1175, 1177, 1179-1180, 1182-1183, 1185-1187, 1189-1191, 1193-1195, 1197-1199, 1201, 1203-1204, 1206 in 2 Group(s). Where the effectivity is presented with hyphens between line numbers, the airplane applicability means "through" and "inclusive", e.g. line numbers 1-9 means line numbers 1 through 9 inclusive.
The Variable Numbers and Group Information for the applicable airplanes is given below.
DESCRIPTIONCONFIGURATIONGROUP 767-300F Airplanes that do not have an Emergency Locator Transmitter (ELT) on the aft side of the P61 panel in the flight compartment.
-1 767-300F Airplanes that have an ELT on the aft side of the P61 panel in the flight compartment.
-2 Airplane Models:
767-300F Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 25, 2022 767-25-0589 RB 5 of 13
GroupVariable Number 1VR201 - VR211 1VR251 1VR256 - VR259 2VR260 GroupVariable Number 1VR266 - VR298 2VT501 1VT511 - VT513 2VT521 - VT523 GroupVariable Number 1VT531 - VT533 1VT556 - VT638 1VW701 - VW721 1VW851 B. Spares Affected None.
2. CONCURRENT REQUIREMENTS None.
3. COMPLIANCE The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to Requirements Bulletin 767-25-0589 RB. The Airworthiness Directive will make the compliance tasks and times given in Requirements Bulletin 767-25-0589 RB mandatory.
When more than one OPTION is given for a CONDITION, do only one of the OPTION numbers. When more than one ACTION is given for a CONDITION or an OPTION, do all of the ACTION numbers for thatCONDITION or OPTION Table 1: FLIGHT DECK - FIRST OBSERVER SEAT MARKERS INSTALLATION Repeat Interval (Not to Exceed) Boeing Recommended Compliance Time ActionCondition -Within 12 months after the Original Issue date of Requirements Bulletin 767-25-0589 RB.
ACTION 1: Install marker, part number BAC27TFDE714, in the flight deck.
All Airplanes ACTION 2: Install marker, part number BAC27TFDE715, in the flight deck (2 locations).
4. APPROVAL This Requirements Bulletin was examined by the Federal Aviation Administration (FAA). The changes specified in this document comply with the applicable regulations and are FAA approved, as well as European Union Aviation Safety Agency (EASA)/Joint Aviation Authorities (JAA) approved for all EASA/JAA approved airplanes listed in this Requirements Bulletin effectivity. This document and its approval were based on the airplane in its original Boeing delivery configuration or as modified by other Boeing changes.
If an airplane has a non-Boeing modification or repair that affects a component or system also affected by this Requirements Bulletin, the operator is responsible for obtaining appropriate regulatory agency approval before incorporating this Requirements Bulletin.
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 25, 2022 767-25-0589 RB 6 of 13 REQUIREMENTS BULLETIN 767-25-0589
5. ACCOMPLISHMENT INSTRUCTIONS A. GENERAL INFORMATION NOTE: 1. This is an Enhanced Required for Compliance document. There will be a separate Service Bulletin (SB) and a separate Requirements Bulletin (RB). If an RB is mandated by an Airworthiness Directive (AD), then all applicable requirements specified in the RB must be done. For the related SB, some locations are marked RC Start and RC End to identify the requirements that are restated from the RB. For the related SB, the areas between RC Start and RC End, including sub-steps and any figures identified between RC Start and RC End, must be done to comply with the AD.
Therefore, an Alternative Method of Compliance (AMOC) is required for any deviations to steps between RC Start and RC End, including substeps and identified figures.
For the related SB, the steps not between RC Start and RC End may be deviated from using accepted methods in accordance with the operator's maintenance or inspection program without obtaining approval of an AMOC; this is provided that the steps between RC Start and RC End, including sub-steps and identified figures, can still be done as specified, and the airplane can be put back in an airworthy condition.
Figures not required for compliance are omitted from the RB.
2. This is an Enhanced Required for Compliance document. The Boeing processes used to create the Service Bulletin (SB) and the Requirements Bulletin (RB) ensure that the information between "RC Start" and "RC End" in the SB are identical to the information in the same sections (Compliance, Work Instructions...) of the RB which the SB refers to as the related document.
3. The compliance times for the actions in WORK INSTRUCTIONS are in Compliance.
4. Unless shown differently, these dimensions and tolerances are used:
– Linear dimensions are in inches – Tolerance on linear dimensions, other than rivet and bolt edge margins, is plus or minus 0.03 inch – Tolerance on rivet and bolt edge margin is plus or minus 0.05 inch – Angular tolerance is plus or minus 2 degrees – Hole dimensions for standard solid rivets and fasteners are in Structural Repair Manual (SRM) Chapter 51 – Torque Values:
— Non-standard torque values for maintenance tasks are included in the applicable installation step.
5. When more than one OPTION is given for a CONDITION, do only one of the OPTION numbers. When more than one ACTION is given for a CONDITION or an OPTION, do all of the ACTION numbers for thatCONDITION or OPTION.
6. 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.
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
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7. If it is necessary to remove more parts for access, you can remove those parts. If you can get access without removing identified parts, it is not necessary to remove all of the identified parts. Jacking and shoring limitations must be observed.
B. WORK INSTRUCTIONS Actions Required for Compliance
1. Requirements Group 1:
TABLE 1: FLIGHT DECK - FIRST OBSERVER SEAT MARKERS INSTALLATION Refer to the listed procedures in SB 767-25-0589 Original Issue or later approved revisions as an accepted procedure Method of ComplianceActionCondition PART 1 - OPEN ACCESS--All Airplanes -FIGURE 1ACTION 1: Install marker, part number BAC27TFDE714, in the flight deck.
ACTION 2: Install marker, part number BAC27TFDE715, in the flight deck (2 locations).
PART 4 - CLOSE AC- CESS -- Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 25, 2022 767-25-0589 RB 8 of 13 REQUIREMENTS BULLETIN 767-25-0589
Group 2:
TABLE 2: FLIGHT DECK - FIRST OBSERVER SEAT MARKERS INSTALLATION Refer to the listed procedures in SB 767-25-0589 Original Issue or later approved revisions as an accepted procedure Method of ComplianceActionCondition PART 1 - OPEN ACCESS--All Airplanes PART 2 - SPACING-- -FIGURE 1ACTION 1: Install marker, part number BAC27TFDE714, in the flight deck.
ACTION 2: Install marker, part number BAC27TFDE715, in the flight deck (2 locations).
PART 3 - ELT MARKER
INSTALLATION -- PART 4 - CLOSE AC- CESS -- Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
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REQUIREMENTS BULLETIN 767-25-0589 FWD
FLIGHT COMPARTMENT (TYPICAL)
CLOSURE
ASSEMBLY
0.75 STA 0.25 190
0.75
0.25 FWD 2976092 FIGURE 1: FLIGHT DECK - MARKERS FOR FIRST OBSERVER SEAT INSTALLATION (SHEET 1 OF 4) Original Issue: February 25, 2022 Export Controlled ECCN: 9E991 767-25-0589 RB Copyright © Unpublished Work - See page 1 for details. 10 of 13
FIGURE 1: FLIGHT DECK - MARKERS FOR FIRST OBSERVER SEAT INSTALLATION (SHEET 2 OF 4) Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
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REQUIREMENTS BULLETIN 767-25-0589
LIFE JACKETS -
STOWAGE
TYPICAL STA 245
CENTERLINE
- OF MARKERS
• MARKERS
SIDEWALL LINING A-A ND 2976878 FIGURE 1: FLIGHT DECK - MARKERS FOR FIRST OBSERVER SEAT INSTALLATION (SHEET 3 OF 4) Original Issue: February 25, 2022 767-25-0589 RB Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details. 12 of 13