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Commercial Airplanes 747 Requirements Bulletin ALERT Number: 747-57A2367 RB Original Issue: November 15, 2019 Revision 1: March 20, 2023 ATA System: 5752 2751 SUBJECT: WINGS - Flaps - Trailing Edge - Inboard Foreflap Assembly Change and Inspection 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 © 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Unpublished Work.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 RBRevision 1: March 20, 2023 1 of 289
3.0
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RBRevision 1: March 20, 2023 2 of 289 REQUIREMENTS BULLETIN 747-57A2367
ALERTALERT
BLANK PAGE
Table of Contents
Revision Transmittal Sheet7
1. EFFECTIVITY9
A. Airplanes9
B. Spares Affected14
2. CONCURRENT REQUIREMENTS14
3. COMPLIANCE14
4. APPROVAL24
5. ACCOMPLISHMENT INSTRUCTIONS25
A. General Information25
B. Work Instructions27
FIGURE 1: LEFT SIDE - INBOARD FOREFLAP - INBOARD LINK ASSEMBLY - REMOVAL100
FIGURE 2: LEFT SIDE - INBOARD FOREFLAP - INBOARD LINK ASSEMBLY - INSTALLATION . . 102 FIGURE 3: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY WITH EXISTING DOUBLER INSTALLED - REMOVAL [Group 1; Group 2, Configuration 1-2; Group 3, Configuration
1-2; Group 4-8]105
FIGURE 4: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY WITH EXISTING
DOUBLER INSTALLED - INSTALLATION [Group 1]108
FIGURE 5: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY WITH EXISTING DOUBLER INSTALLED - INSTALLATION [Group 2, Configuration 1-2; Group 3, Configuration
1-2; Group 4-6]111
FIGURE 6: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY WITH EXISTING
DOUBLER INSTALLED - INSTALLATION [Group 7-8]115
FIGURE 7: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY WITHOUT EXISTING
DOUBLER - REMOVAL [Group 2, Configuration 3-4; Group 3, Configuration 3-4]119
FIGURE 8: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY WITHOUT EXISTING DOUBLER - INSTALLATION [Group 2, Configuration 3-4; Group 3, Configuration 3-4] . 122 FIGURE 9: LEFT SIDE - INBOARD FOREFLAP CARRIAGE ATTACHMENT - CENTER TOGGLE ROLLER
- REMOVAL129
FIGURE 10: LEFT SIDE - INBOARD FOREFLAP CARRIAGE ATTACHMENT - CENTER TOGGLE ROLLER
- INSTALLATION132
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]135
FIGURE 12: LEFT SIDE - INBOARD TRAILING EDGE FLAP - OUTBOARD TRACK NUMBER 3 - STOP - INSTALLATION [Group 1-2, Configuration 2; Group 2, Configuration 4; Group 3, Configuration
2, 4; Group 4-5, Configuration 2]138
FIGURE 13: LEFT SIDE - INBOARD TRAILING EDGE FLAP - OUTBOARD TRACK 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]141
FIGURE 14: LEFT SIDE - INBOARD TRAILING EDGE FLAP - OUTBOARD TRACK 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]144
FIGURE 15: LEFT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRACK NUMBER 4 - STOP - REMOVAL [Group 1-2, Configuration 1; Group 2, Configuration 3; Group 4, Configuration 1;
Group 6-7]147
FIGURE 16: LEFT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRACK NUMBER 4 - STOP - INSTALLATION [Group 1-2, Configuration 2; Group 2, Configuration 4; Group 4, Configuration
2]150
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RBRevision 1: March 20, 2023 3 of 289 REQUIREMENTS BULLETIN 747-57A2367
ALERTALERT
FIGURE 17: LEFT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRACK NUMBER 4 - STOP -
INSTALLATION [Group 3, Configuration 2, 4; Group 5, Configuration 2]153
FIGURE 18: LEFT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRACK NUMBER 4 - STOP - INSTALLATION [Group 1-2, Configuration 1; Group 2, Configuration 3; Group 4, Configuration
1; Group 6-7]156
FIGURE 19: LEFT SIDE - INBOARD FOREFLAP - STOP LUG ATTACHMENT BOLTS - REMOVAL . 159 FIGURE 20: LEFT SIDE - INBOARD FOREFLAP - STOP LUG ATTACHMENT BOLTS - INSTALLATION
.162
FIGURE 21: LEFT SIDE - INBOARD FOREFLAP FLAP TRACK - ROLLERS - REMOVAL165
FIGURE 22: LEFT SIDE - INBOARD FOREFLAP FLAP TRACK - ROLLERS - INSTALLATION169
FIGURE 23: LEFT SIDE - INBOARD FOREFLAP ASSEMBLY - DETAILED INSPECTIONS173
FIGURE 24: LEFT SIDE - INBOARD FOREFLAP AND MIDFLAP ASSEMBLY - DETAILED INSPECTIONS
.177
FIGURE 25: LEFT SIDE - INBOARD FOREFLAP AND MIDFLAP ASSEMBLY - DETAILED INSPECTIONS
.180
FIGURE 26: RIGHT SIDE - INBOARD FOREFLAP - INBOARD LINK ASSEMBLY - REMOVAL183
FIGURE 27: RIGHT SIDE - INBOARD FOREFLAP - INBOARD LINK ASSEMBLY - INSTALLATION . 185 FIGURE 28: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY WITH EXISTING DOUBLER INSTALLED - REMOVAL [Group 1; Group 2, Configuration 1-2; Group 3, Configuration
1-2; Group 4-8]188
FIGURE 29: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY WITH EXISTING
DOUBLER INSTALLED - INSTALLATION [Group 1]191
FIGURE 30: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY WITH EXISTING DOUBLER INSTALLED - INSTALLATION [Group 2, Configuration 1-2; Group 3, Configuration
1-2; Group 4-6]194
FIGURE 31: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY WITH EXISTING
DOUBLER INSTALLED - INSTALLATION [Group 7-8]198
FIGURE 32: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY WITHOUT EXISTING
DOUBLER - REMOVAL [Group 2, Configuration 3-4; Group 3, Configuration 3-4]202
FIGURE 33: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY WITHOUT EXISTING DOUBLER - INSTALLATION [Group 2, Configuration 3-4; Group 3, Configuration 3-4] . 205 FIGURE 34: RIGHT SIDE - INBOARD FOREFLAP CARRIAGE ATTACHMENT - CENTER TOGGLE ROLLER
- REMOVAL212
FIGURE 35: RIGHT SIDE - INBOARD FOREFLAP CARRIAGE ATTACHMENT - CENTER TOGGLE ROLLER
- INSTALLATION215
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]218
FIGURE 37: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - OUTBOARD TRACK NUMBER 6 - STOP
- INSTALLATION [Group 1-2, Configuration 2; Group 2, Configuration 4; Group 3, Configuration
2, 4; Group 4-5, Configuration 2]221
FIGURE 38: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - OUTBOARD TRACK 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]224
FIGURE 39: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - OUTBOARD TRACK 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]227
FIGURE 40: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRACK NUMBER 5 - STOP - REMOVAL [Group 1-2, Configuration 1; Group 2, Configuration 3; Group 4, Configuration 1;
Group 6-7]230
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RBRevision 1: March 20, 2023 4 of 289 REQUIREMENTS BULLETIN 747-57A2367
ALERTALERT
FIGURE 41: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - OUTBOARD TRACK NUMBER 5 - STOP
- INSTALLATION [Group 1-2, Configuration 2; Group 2, Configuration 4; Group 4, Configuration
2]233
FIGURE 42: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRACK NUMBER 5 - STOP -
INSTALLATION [Group 3, Configuration 2, 4; Group 5, Configuration 2]236
FIGURE 43: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRACK NUMBER 5 - STOP - INSTALLATION [Group 1-2, Configuration 1; Group 2, Configuration 3; Group 4, Configuration
1; Group 6-7]239
FIGURE 44: RIGHT SIDE - INBOARD FOREFLAP - STOP LUG ATTACHMENT BOLTS - REMOVAL. 242 FIGURE 45: RIGHT SIDE - INBOARD FOREFLAP - STOP LUG ATTACHMENT BOLTS - INSTALLATION
.245
FIGURE 46: RIGHT SIDE - INBOARD FOREFLAP FLAP TRACK - ROLLERS - REMOVAL248
FIGURE 47: RIGHT SIDE - INBOARD FOREFLAP FLAP TRACK - ROLLERS - INSTALLATION . . . 252 FIGURE 48: LEFT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRACK NUMBER 4 - STOP -
REMOVAL [Group 3, Configuration 1, 3; Group 5, Configuration 1; Group 8]256
FIGURE 49: LEFT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRACK NUMBER 4 - STOP -
INSTALLATION [Group 3, Configuration 1, 3; Group 5, Configuration 1; Group 8]259
FIGURE 50: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRACK NUMBER 5 - TRACK - STOP - REMOVAL [Group 3, Configuration 1, 3; Group 5, Configuration 1; Group 8] . . 262 FIGURE 51: RIGHT SIDE - INBOARD TRAILING EDGE FLAP - INBOARD TRACK NUMBER 5 - STOP -
INSTALLATION [Group 3, Configuration 1, 3; Group 5, Configuration 1; Group 8]265
FIGURE 52: RIGHT SIDE - INBOARD FOREFLAP ASSEMBLY - DETAILED INSPECTIONS268
FIGURE 53: RIGHT SIDE - INBOARD FOREFLAP AND MIDFLAP ASSEMBLY - DETAILED INSPECTIONS
.272
FIGURE 54: RIGHT SIDE - INBOARD FOREFLAP AND MIDFLAP ASSEMBLY - DETAILED INSPECTIONS
.275
FIGURE 55: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY - LUBRICATION. 278 FIGURE 56: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY - LUBRICATION
.281
FIGURE 57: LEFT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY - GENERAL VISUAL
INSPECTION284
FIGURE 58: RIGHT SIDE - INBOARD FOREFLAP - OUTBOARD FITTING ASSEMBLY - GENERAL VISUAL
INSPECTION287
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RBRevision 1: March 20, 2023 5 of 289 REQUIREMENTS BULLETIN 747-57A2367
ALERTALERT
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RBRevision 1: March 20, 2023 6 of 289 REQUIREMENTS BULLETIN 747-57A2367
ALERTALERT
BLANK PAGE
Commercial Airplanes 747 Requirements Bulletin ALERT Revision Transmittal SheetNumber: 747-57A2367 RBOriginal Issue: November 15, 2019 Revision 1: March 20, 2023 ATA System: 5752 2751 SUBJECT: WINGS - Flaps - Trailing Edge - Inboard Foreflap Assembly Change and Inspection This revision includes all pages of the requirements bulletin.
COMPLIANCE INFORMATION RELATED TO THIS REVISION Federal Aviation Administration (FAA) Airworthiness Directive AD 2021-02-15 is related to this Requirements Bulletin.
The Federal Aviation Administration (FAA) will possibly release an additional Airworthiness Directive related to this Requirements Bulletin. The Airworthiness Directive will make the compliance tasks and times given in this Requirements Bulletin mandatory.
Effects of this Revision on airplanes on which the Original Issue of Requirements Bulletin 747-57A2367 RB was previously done:
None.
NOTE: Compliance time changes for the required actions have been made. Operators are encouraged to review COMPLIANCE for impact to bulletin accomplishment schedule.
REASON FOR REVISION This revision is sent to separate the sequencing of part replacements in order to provide operators with flexibility in the replacement of parts to satisfy the compliance requirements. Also to change inspection compliance time from whichever occurs later to whichever occurs first. Also to change inspection criteria wording from 'or' to 'and'. In addition Federal Aviation Administration (FAA) Airworthiness Directive AD 2021-02-15 has been added.
-Compliance, added statement, changed statement, added three new tables, changed Tables 1, 2, 3, 4, 5, 6, and 7, compliance times and updated table numbers. Removed footnote for Table 1, 2, and 3.
-General Information, updated table numbers that define a serviceable inboard foreflap assembly.
-Work Instructions, added three new tables, removed footnote for Table 2, changed Tables 4, 5, 6, and 7, and updated table numbers.
-FIGURE 3, 4, 5, 6, 10, 28, 29, 30, 31, 35, 36, updated step table.
-FIGURE 8, 33, updated step table and fastener code table.
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RBRevision 1: March 20, 2023 7 of 289
-FIGURE 21, 46, changed sheets 2 and 3, and updated step table.
-FIGURE 22, 47, changed sheet 3 and updated step table.
REVISION HISTORY Service BulletinService BulletinRequirement BulletinRequirement Bulletin 747-57A2367747-57A2367747-57A2367 RB747-57A2367 RB Issue DateIssue Date November 15, 2019Original Issue:November 15, 2019Original Issue:
March 20, 2023Revision 1:March 20, 2023Revision 1:
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 15, 2019 747-57A2367 RBRevision 1: March 20, 2023 8 of 289 REQUIREMENTS BULLETIN 747-57A2367
ALERTALERT
Commercial Airplanes 747 Requirements Bulletin ALERT Number: 747-57A2367 RB Original Issue: November 15, 2019 Revision 1: March 20, 2023 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 RBRevision 1: March 20, 2023 9 of 289
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 747-57A2302.
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 747-57A2302.
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 747-57A2302.
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 747-57A2302.
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 747-57A2302.
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 747-57A2302.
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 747-57A2302.
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 747-57A2302.
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 RBRevision 1: March 20, 2023 10 of 289 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 RBRevision 1: March 20, 2023 11 of 289 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 RBRevision 1: March 20, 2023 12 of 289 REQUIREMENTS BULLETIN 747-57A2367