TextPartly OCR
Some pages are OCR from a scan. OCR can misread letters and numbers.
Query with SQL
duckdb -csv -c "SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '1e159cdeb32b338dfd3c77f2cb47d80dab301f5595e9cb37b415ef1eacf5f5b2' ORDER BY p.page"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '1e159cdeb32b338dfd3c77f2cb47d80dab301f5595e9cb37b415ef1eacf5f5b2' ORDER BY p.page
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
Commercial Airplanes 747 Requirements Bulletin ALERT Number: 747-57A2367 RB Original Issue: November 15, 2019 ATA System: 5752 2751 SUBJECT: WINGS - Flaps - Trailing Edge - Inboard Foreflap Assembly Change and Inspection 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.
9E991ECCN:
Copyright © 2019 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Unpublished Work.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: November 15, 2019 747-57A2367 RB 1 of 288
5.0
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RB 2 of 288 REQUIREMENTS BULLETIN 747-57A2367
ALERTALERT
BLANK PAGE
Table of Contents
1 . E F F E C T I V I T Y7
A. Airplanes7
B . S p a r e s A f f e c t e d ........................................... 1 2
2. CONCURRENT REQUIREMENTS .................................... 1 2 3 . C O M P L I A N C E ............................................... 1 2
4. APPROVAL ................................................ 2 1
5. ACCOMPLISHMENT INSTRUCTIONS .................................. 2 3 A. General Information ......................................... 2 3 B. Work Instructions ........................................... 2 5 FIGURE 1: LEFT SIDE - INBOARD FOREFLAP - INBOARD LINK ASSEMBLY - R E M O V A L .... 1 0 3 FIGURE 2: LEFT SIDE - INBOARD FOREFLAP - INBOARD LINK ASSEMBLY - INSTALLATION . . 105 FIGURE 3: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMB LY WITH EXISTING DOUBLER INSTALLED - REMOVAL [Group 1; Group 2, Configuration 1-2; Group 3, Configuration 1-2; Group 4-8] ........................................ 1 0 8 FIGURE 4: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMB LY WITH EXISTING
D O U B L E R I N S T A L L E D - I N S T A L L A T I O N [ G r o u p 1 ]111
FIGURE 5: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMB LY WITH EXISTING DOUBLER INSTALLED - INSTALLATION [Group 2, Configuration 1-2; Group 3, Configuration 1-2; Group 4-6] ........................................ 1 1 4 FIGURE 6: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMB LY WITH EXISTING DOUBLER INSTALLED - INSTALLATION [Group 7-8] ................... 1 1 7 FIGURE 7: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMB LY WITHOUT EXISTING DOUBLER - REMOVAL [Group 2, Configuration 3-4; Group 3, Configu ration 3-4] .... 1 2 0 FIGURE 8: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMB LY WITHOUT EXISTING DOUBLER - INSTALLATION [Group 2, Configuration 3-4; Group 3, Co nfiguration 3-4] . 123 FIGURE 9: LEFT SIDE - INBOARD FOREFLAP CARRIAGE ATTACHMENT - CEN TER TOGGLE ROLLER
- R E M O V A L .......................................... 1 3 0 FIGURE 10: LEFT SIDE - INBOARD FOREFLAP CARRIAGE ATTACHMENT - CENTER TOGGLE ROLLER
- INSTALLATION ....................................... 1 3 3 FIGURE 11: LEFT SIDE - INBOARD TRAILING EDGE FLAP TRACKS NUMBER 3 AND 4 - STOP - REMOVAL [Group 1-2, Configuration 2; Group 2, Configuration 4; Group 3, Configuration 2, 4; Group 4-5, Configuration 2] ........................................ 1 3 6 FIGURE 12: LEFT SIDE - INBOARD TRAILING EDGE FLAP - OUTBOARD TRA CK NUMBER 3 - STOP - INSTALLATION [Group 1-2, Configuration 2; Group 2, Configuration 4; Group 3, Configuration 2, 4; Group 4-5, Configuration 2] ............................... 1 3 9 FIGURE 13: LEFT SIDE - INBOARD TRAILING EDGE FLAP - OUTBOARD TRA CK NUMBER 3 - STOP - REMOVAL [Group 1-2, Configuration 1; Group 2, Configuration 3; Group 3, Configuration 1, 3;
Group 4-5, Configuration 1; Group 6-8] ........................... 1 4 2 FIGURE 14: LEFT SIDE - INBOARD TRAILING EDGE FLAP - OUTBOARD TRA CK NUMBER 3 - STOP - INSTALLATION [Group 1-2, Configuration 1; Group 2, Configuration 3; Group 3, Configuration 1, 3; Group 4-5, Configuration 1; Group 6-8] ........................ 1 4 5 FIGURE 15: LEFT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRAC K NUMBER 4 - STOP - REMOVAL [Group 1-2, Configuration 1; Group 2, Configuration 3; Group 4, Configuration 1;
Group 6-7] ........................................... 1 4 8 FIGURE 16: LEFT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRAC K NUMBER 4 - STOP - INSTALLATION [Group 1-2, Configuration 2; Group 2, Configuration 4; Group 4, Configuration 2 ] ................................................ 1 5 1 Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RB 3 of 288 REQUIREMENTS BULLETIN 747-57A2367
ALERTALERT
FIGURE 17: LEFT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRAC K NUMBER 4 - STOP - INSTALLATION [Group 3, Configuration 2, 4; Group 5, Configurati o n 2 ] ......... 1 5 4 FIGURE 18: LEFT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRAC K NUMBER 4 - STOP - INSTALLATION [Group 1-2, Configuration 1; Group 2, Configuration 3; Group 4, Configuration 1; Group 6-7] ......................................... 1 5 7 FIGURE 19: LEFT SIDE - INBOARD FOREFLAP - STOP LUG ATTACHMENT BO LTS - REMOVAL . 160 FIGURE 20: LEFT SIDE - INBOARD FOREFLAP - STOP LUG ATTACHMENT BO LTS - INSTALLATION ................................................. 1 6 3 FIGURE 21: LEFT SIDE - INBOARD FOREFLAP FLAP TRACK - ROLLERS - R E M O V A L ...... 1 6 6 FIGURE 22: LEFT SIDE - INBOARD FOREFLAP FLAP TRACK - ROLLERS - I NSTALLATION .... 1 7 0 FIGURE 23: LEFT SIDE - INBOARD FOREFLAP ASSEMBLY - DETAILED INSP ECTIONS ...... 1 7 4 FIGURE 24: LEFT SIDE - INBOARD FOREFLAP AND MIDFLAP ASSEMBLY - D ETAILED INSPECTIONS ................................................. 1 7 8 FIGURE 25: LEFT SIDE - INBOARD FOREFLAP AND MIDFLAP ASSEMBLY - D ETAILED INSPECTIONS ................................................. 1 8 1 FIGURE 26: RIGHT SIDE - INBOARD FOREFLAP - INBOARD LINK ASSEMBLY - R E M O V A L .... 1 8 4 FIGURE 27: RIGHT SIDE - INBOARD FOREFLAP - INBOARD LINK ASSEMBLY - INSTALLATION . 186 FIGURE 28: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSE MBLY WITH EXISTING DOUBLER INSTALLED - REMOVAL [Group 1; Group 2, Configuration 1-2; Group 3, Configuration 1-2; Group 4-8] ........................................ 1 8 9 FIGURE 29: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSE MBLY WITH EXISTING DOUBLER INSTALLED - INSTALLATION [Group 1] .................... 1 9 2 FIGURE 30: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSE MBLY WITH EXISTING DOUBLER INSTALLED - INSTALLATION [Group 2, Configuration 1-2; Group 3, Configuration 1-2; Group 4-6] ........................................ 1 9 5 FIGURE 31: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSE MBLY WITH EXISTING DOUBLER INSTALLED - INSTALLATION [Group 7-8] ................... 1 9 8 FIGURE 32: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY WITHOUT EXISTING DOUBLER - REMOVAL [Group 2, Configuration 3-4; Group 3, Configu ration 3-4] .... 2 0 1 FIGURE 33: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY WITHOUT EXISTING DOUBLER - INSTALLATION [Group 2, Configuration 3-4; Group 3, Co nfiguration 3-4] . 204 FIGURE 34: RIGHT SIDE - INBOARD FOREFLAP CARRIAGE ATTACHMENT - CENTER TOGGLE ROLLER
- R E M O V A L .......................................... 2 1 1 FIGURE 35: RIGHT SIDE - INBOARD FOREFLAP CARRIAGE ATTACHMENT - CENTER TOGGLE ROLLER
- INSTALLATION ....................................... 2 1 4 FIGURE 36: RIGHT SIDE - INBOARD TRAILING EDGE FLAP TRACKS NUMBER 5 AND 6 - STOP - REMOVAL [Group 1-2, Configuration 2; Group 2, Configuration 4; Group 3, Configuration 2, 4;
Group 4-5, Configuration 2] .................................. 2 1 7 FIGURE 37: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - OUTBOARD TR ACK NUMBER 6 - STOP
- INSTALLATION [Group 1-2, Configuration 2; Group 2, Configuration 4; Group 3, Configuration 2, 4; Group 4-5, Configuration 2] ............................... 2 2 0 FIGURE 38: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - OUTBOARD TR ACK NUMBER 6 - STOP
- REMOVAL [Group 1-2, Configuration 1; Group 2, Configuration 3; Group 3, Configuration 1, 3; Group 4-5, Configuration 1; Group 6-8] .......................... 2 2 3 FIGURE 39: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - OUTBOARD TR ACK NUMBER 6 - STOP
- INSTALLATION [Group 1-2, Configuration 1; Group 2, Configuration 3; Group 3, Configuration 1, 3; Group 4-5, Configuration 1; Group 6-8] ........................ 2 2 6 FIGURE 40: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRA CK NUMBER 5 - STOP - REMOVAL [Group 1-2, Configuration 1; Group 2, Configuration 3; Group 4, Configuration 1;
Group 6-7] ........................................... 2 2 9 Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RB 4 of 288 REQUIREMENTS BULLETIN 747-57A2367
ALERTALERT
FIGURE 41: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - OUTBOARD TR ACK NUMBER 5 - STOP
- INSTALLATION [Group 1-2, Configuration 2; Group 2, Configuration 4; Group 4, Configuration 2 ] ................................................ 2 3 2 FIGURE 42: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRA CK NUMBER 5 - STOP - INSTALLATION [Group 3, Configuration 2, 4; Group 5, Configurati o n 2 ] ......... 2 3 5 FIGURE 43: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRA CK NUMBER 5 - STOP - INSTALLATION [Group 1-2, Configuration 1; Group 2, Configuration 3; Group 4, Configuration 1; Group 6-7] ......................................... 2 3 8 FIGURE 44: RIGHT SIDE - INBOARD FOREFLAP - STOP LUG ATTACHMENT B OLTS - REMOVAL . 241 FIGURE 45: RIGHT SIDE - INBOARD FOREFLAP - STOP LUG ATTACHMENT B OLTS - INSTALLATION ................................................. 2 4 4 FIGURE 46: RIGHT SIDE - INBOARD FOREFLAP FLAP TRACK - ROLLERS - R E M O V A L ...... 2 4 7 FIGURE 47: RIGHT SIDE - INBOARD FOREFLAP FLAP TRACK - ROLLERS - INSTALLATION . . . 251 FIGURE 48: LEFT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRAC K NUMBER 4 - STOP - REMOVAL [Group 3, Configuration 1, 3; Group 5, Configuration 1; G r o u p 8 ] ....... 2 5 5 FIGURE 49: LEFT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRAC K NUMBER 4 - STOP - INSTALLATION [Group 3, Configuration 1, 3; Group 5, Configurati o n 1 ; G r o u p 8 ] .... 2 5 8 FIGURE 50: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRA CK NUMBER 5 - TRACK - STOP - REMOVAL [Group 3, Configuration 1, 3; Group 5, Configura tion 1; Group 8] . . 261 FIGURE 51: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRA CK NUMBER 5 - STOP - INSTALLATION [Group 3, Configuration 1, 3; Group 5, Configurati o n 1 ; G r o u p 8 ] .... 2 6 4 FIGURE 52: RIGHT SIDE - INBOARD FOREFLAP ASSEMBLY - DETAILED INS P E C T I O N S ..... 2 6 7 FIGURE 53: RIGHT SIDE - INBOARD FOREFLAP AND MIDFLAP ASSEMBLY - DETAILED INSPECTIONS ................................................. 2 7 1 FIGURE 54: RIGHT SIDE - INBOARD FOREFLAP AND MIDFLAP ASSEMBLY - DETAILED INSPECTIONS ................................................. 2 7 4 FIGURE 55: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY - LUBRICATION . 277 FIGURE 56: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSE MBLY - LUBRICATION ................................................. 2 8 0 FIGURE 57: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEM BLY - GENERAL VISUAL INSPECTION ......................................... 2 8 3 FIGURE 58: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY - GENERAL VISUAL INSPECTION ......................................... 2 8 6 Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RB 5 of 288 REQUIREMENTS BULLETIN 747-57A2367
ALERTALERT
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RB 6 of 288 REQUIREMENTS BULLETIN 747-57A2367
ALERTALERT
BLANK PAGE
Commercial Airplanes 747 Requirements Bulletin ALERT Number: 747-57A2367 RB Original Issue: November 15, 2019 ATA System: 5752 2751 SUBJECT: WINGS - Flaps - Trailing Edge - Inboard Foreflap Assembly Change and Inspection
THIS DOCUMENT IS SENT TO THE OPERATORS OF RECORD OF THE AIRPLANES SHOWN IN PARAGRAPH 1.A., EFFECTIVITY. IF AN AIRPLANE HAS BEEN LEASED OR SOLD, SEND THIS DOCUMENT TO THE NEW OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS DOCUMENT TO THE NEW OWNER. 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 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR Airplane(s), line number(s) 1-264, 266-267, 269, 271-272, 274, 276-277, 279, 281, 283, 285, 287, 289, 291-292, 294-297, 299-300, 302-303, 305, 308-324, 326-328, 330, 332-366, 368-370, 372, 374-404, 406-412, 414, 416-432, 434-438, 440, 442-444, 446, 448-454, 456-466, 468-472, 474-500, 502-504, 506, 508-528, 530-533, 535-536, 538-559, 561-563, 565-566, 568-668, 670-675, 677-1419 in 8 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.
DESCRIPTIONCONFIGURATIONGROUP 747-100/-200B/-200C/-200F/-747SR Airplanes.-1 Airplanes that have replaced stop and attachment bolts in accordance with 747-57-2218.
1 Airplanes that have not replaced stop and attachment bolts in accordance with 747-57-2218.
2 Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RB 7 of 288
DESCRIPTIONCONFIGURATIONGROUP 747-100/-200B/-200C/-200F Airplanes.-2 Airplanes that have completed terminating action in 747-57-2218, and have installed a doubler under the inboard flap sequence carriage attachment fitting in accordance with 747-57-2302.
1 Airplanes that have not completed terminating action in 747-57-2218, and have installed a doubler under the inboard flap sequence carriage attachment fitting in accordance with 747-57-2302.
2 Airplanes that have completed terminating action in 747-57-2218, and have not installed a doubler under the inboard flap sequence carriage attachment fitting in accordance with 747-57-2302.
3 Airplanes that have not completed terminating action in 747-57-2218, and have not installed a doubler under the inboard flap sequence carriage attachment fitting in accordance with 747-57-2302.
4 747SR Airplanes.-3 Airplanes that have completed terminating action in 747-57-2218, and have installed a doubler under the inboard flap sequence carriage attachment fitting in accordance with 747-57-2302.
1 Airplanes that have not completed terminating action in 747-57-2218, and have installed a doubler under the inboard flap sequence carriage attachment fitting in accordance with 747-57-2302.
2 Airplanes that have completed terminating action in 747-57-2218, and have not installed a doubler under the inboard flap sequence carriage attachment fitting in accordance with 747-57-2302.
3 Airplanes that have not completed terminating action in 747-57-2218, and have not installed a doubler under the inboard flap sequence carriage attachment fitting in accordance with 747-57-2302.
4 747-100/-100B/-200B/-200C/-200F Airplanes.-4 Airplanes that have completed terminating action in 747-57-2218.1 Airplanes that have not completed terminating action in 747-57-2218.2 747-100B/-747SR Airplanes.-5 Airplanes that have completed terminating action in 747-57-2218.1 Airplanes that have not completed terminating action in 747-57-2218.2 Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RB 8 of 288 REQUIREMENTS BULLETIN 747-57A2367
ALERTALERT
DESCRIPTIONCONFIGURATIONGROUP 747-100B/-100B SUD/-200B/-200C/-200F/-300/-400/-400D/-400F/-747SR Airplanes.
-6 747-400 Airplanes.-7 747-400/-400F Airplanes.-8 Airplane Models:
747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR GroupVariable Number 1RA001 - RA034 1RA101 - RA115 1RA161 - RA164 1RA201 - RA203 1RA216 - RA217 1RA245 - RA246 1RA251 - RA262 2RA263 - RA264 4RA265 - RA266 1RA301 - RA315 2RA316 - RA317 4RA318 1RA351 - RA360 1RA369 - RA373 1RA401 - RA418 1RA501 - RA502 1RA521 - RA527 4RA528 1RA532 - RA540 2RA541 - RA542 4RA543 - RA548 1RA551 - RA552 GroupVariable Number 1RA559 - RA561 1RA581 - RA582 1RA585 1RA601 - RA602 1RA631 - RA635 1RA651 - RA652 1RA671 - RA677 1RA701 - RA702 1RA721 - RA724 4RA725 - RA731 1RA741 - RA744 2RA745 2RA749 4RA750 1RA761 - RA762 1RA781 - RA783 4RA784 1RA901 - RA916 1RB001 - RB006 2RB007 - RB009 4RB010 - RB012 1RB013 - RB014 GroupVariable Number 2RB015 4RB016 1RB041 - RB044 1RB071 - RB075 1RB101 - RB102 6RB411 - RB413 6RB421 1RB601 3RB602 - RB606 5RB607 5RB681 - RB696 6RB697 4RB711 5RB721 - RB722 6RB723 4RB741 - RB748 1RD001 - RD002 2RD003 4RD004 1RD021 - RD022 1RD041 - RD042 2RD043 Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RB 9 of 288 REQUIREMENTS BULLETIN 747-57A2367
ALERTALERT
GroupVariable Number 4RD044 - RD059 1RD071 - RD072 4RD081 - RD083 4RD091 - RD092 1RD101 - RD102 2RD103 - RD104 4RD121 - RD127 4RD131 - RD144 6RD166 - RD167 4RD171 - RD172 4RD181 - RD183 4RD201 - RD204 4RD221 - RD224 6RD225 - RD227 6RD231 - RD235 4RD241 - RD243 4RD251 - RD257 6RD258 - RD262 4RD271 - RD272 6RD291 - RD292 6RD301 - RD302 6RD311 4RD351 - RD356 6RD357 - RD358 4RD361 - RD365 6RD366 4RD381 - RD383 4RD411 - RD414 4RD421 - RD426 4RD431 - RD435 4RD441 - RD442 4RD451 - RD454 6RD455 - RD456 GroupVariable Number 4RD461 4RD471 - RD475 4RD513 - RD519 4RD531 - RD533 4RD551 4RD561 4RD571 4RD581 - RD583 4RD591 - RD593 4RD601 - RD607 4RD621 - RD623 4RD641 - RD649 4RD651 - RD658 6RD659 4RD661 4RD671 4RD681 - RD682 4RD691 - RD692 4RD701 - RD702 4RD721 - RD722 4RD741 - RD742 4RD751 - RD753 6RD754 - RD755 4RD761 6RD771 - RD775 6RD781 - RD783 6RD791 - RD792 4RE001 8RF001 - RF006 1RJ131 - RJ132 2RJ133 4RJ151 - RJ152 4RJ301 - RJ303 GroupVariable Number 6RJ322 4RJ331 - RJ333 8RL401 - RL403 8RL411 - RL436 8RL451 - RL456 8RL461 - RL462 8RL471 - RL481 8RL491 - RL492 8RL501 - RL502 8RL511 - RL516 8RL521 - RL522 8RL531 - RL534 8RL551 8RL561 - RL568 8RL571 - RL572 8RL576 - RL577 8RL579 8RL581 - RL586 8RL651 - RL655 8RL671 - RL675 8RL681 - RL684 8RL751 - RL752 7RM001 - RM007 7RM010 - RM013 7RM021 - RM024 7RM026 - RM030 7RM036 - RM045 7RM051 - RM053 7RM071 7RM081 - RM084 7RM091 7RM096 - RM097 7RM116 - RM117 Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RB 10 of 288 REQUIREMENTS BULLETIN 747-57A2367
ALERTALERT
GroupVariable Number 7RM126 - RM132 7RM136 - RM147 7RM156 - RM157 8RM158 7RM166 - RM177 7RM191 - RM192 7RM231 - RM233 7RM241 - RM246 7RM261 - RM264 7RM316 - RM318 7RM331 - RM333 7RM341 7RM351 - RM355 7RM366 - RM367 7RM401 - RM403 7RM426 7RM431 7RM441 - RM443 7RM445 7RM801 - RM803 7RM811 - RM813 8RM851 - RM859 8RM861 - RM863 8RM871 - RM899 8RM901 - RM906 8RM911 4RR001 - RR005 4RR021 - RR023 6RR024 - RR025 4RR031 1RR201 4RR202 - RR203 6RR204 - RR206 GroupVariable Number 2RR221 4RR222 - RR226 2RR261 4RR262 - RR264 6RR265 - RR267 2RR301 4RR302 - RR306 6RR307 - RR310 4RR331 - RR332 4RR336 4RR341 - RR345 4RR361 - RR362 4RR421 - RR422 6RR431 - RR432 6RR441 - RR442 6RR451 4RR501 - RR504 4RR521 6RR522 6RR526 4RR531 6RR551 - RR556 4RR561 6RR566 6RR701 6RR721 - RR722 8RR723 - RR724 6RR746 - RR748 6RR851 - RR856 6RR861 8RR862 6RR951 - RR952 6RS001 - RS002 GroupVariable Number 6RS201 6RS211 - RS212 6RS221 - RS222 6RS231 - RS241 6RS251 - RS259 6RS263 6RS265 - RS268 6RS271 - RS276 6RS291 - RS292 6RS301 - RS306 6RS311 - RS320 6RS331 - RS333 6RS341 - RS342 6RS699 6RS701 - RS703 6RS711 - RS713 6RS721 - RS722 6RS731 - RS732 6RS741 - RS743 6RS751 - RS752 6RS761 - RS762 6RS771 6RS781 - RS782 6RS786 6RT001 - RT013 7RT014 6RT021 - RT022 6RT031 - RT034 7RT035 6RT041 - RT047 6RT061 6RT071 - RT075 6RT101 - RT103 Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RB 11 of 288 REQUIREMENTS BULLETIN 747-57A2367
ALERTALERT
GroupVariable Number 6RT121 6RT131 - RT136 7RT137 6RT151 - RT152 6RT161 - RT168 6RT401 - RT412 6RT431 - RT446 7RT447 6RT451 - RT469 6RT471 - RT499 6RT501 - RT535 6RT551 - RT568 6RT571 - RT591 6RT601 - RT627 7RT628 - RT630 6RT631 - RT637 7RT638 - RT640 GroupVariable Number 6RT641 - RT657 6RT671 - RT673 6RT681 - RT682 6RT691 - RT699 6RT701 - RT704 6RT711 - RT717 6RT741 - RT755 7RT756 - RT757 6RT776 - RT777 6RT781 - RT784 6RT801 - RT802 7RT803 6RT811 - RT814 6RT831 - RT837 6RT861 - RT864 6RT876 - RT880 6RT931 - RT932 GroupVariable Number 6RT945 - RT949 6RT951 - RT954 7RT955 6RT966 - RT967 6RU001 - RU006 6RU016 7RU017 6RU031 - RU032 6RU051 - RU052 6RU059 - RU062 6RU081 - RU083 6RU101 7RU102 6RU121 - RU129 7RU130 - RU132 6RU801 - RU809 6RU831 - RU841 B. Spares Affected None.
2. CONCURRENT REQUIREMENTS None.
3. COMPLIANCE The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to this Requirements Bulletin 747-57A2367 RB. The Airworthiness Directive will make the compliance tasks and times given in this Requirements Bulletin 747-57A2367 RB mandatory.
Accomplish the required actions, based on the applicable conditions in Tables 1 to 4 , in accordance with Paragraph 3. Accomplishment Instructions.
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 that CONDITION or OPTION.
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RB 12 of 288 REQUIREMENTS BULLETIN 747-57A2367