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Commercial Airplanes 737 Requirements Bulletin ALERT Number: 737-22A1322 RB Original Issue: November 21, 2018 ATA System: 2211 SUBJECT: AUTO FLIGHT - Digital Flight Control System - Flight Control Computer Software Change 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 © 2018 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Unpublished Work.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 21, 2018 737-22A1322 RB 1 of 8
4.0
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 21, 2018 737-22A1322 RB 2 of 8 REQUIREMENTS BULLETIN 737-22A1322
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Table of Contents
1. EFFECTIVITY5
A. Airplanes5
B. Spares Affected5
2. CONCURRENT REQUIREMENTS5
3. COMPLIANCE5
4. APPROVAL6
5. ACCOMPLISHMENT INSTRUCTIONS7
A. General Information7
B. Work Instructions8
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 21, 2018 737-22A1322 RB 3 of 8 REQUIREMENTS BULLETIN 737-22A1322
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Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 21, 2018 737-22A1322 RB 4 of 8 REQUIREMENTS BULLETIN 737-22A1322
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Commercial Airplanes 737 Requirements Bulletin ALERT Number: 737-22A1322 RB Original Issue: November 21, 2018 ATA System: 2211 SUBJECT: AUTO FLIGHT - Digital Flight Control System - Flight Control Computer Software Change
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 737-600, 737-700, 737-700C, 737-800, 737-900 and 737-900ER Airplanes, line numbers 1270, 1272, 1278 through 7153 in 1 Group.
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 737-22A1322 RB. The Airworthiness Directive will make the compliance tasks and times given in Requirements Bulletin 737-22A1322 RB mandatory.
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 21, 2018 737-22A1322 RB 5 of 8
Accomplish the required action(s), based on the applicable condition(s) in Table(s) 1, in accordance with Accomplishment Instructions.
Table 1: Flight Control Computer Software Installation and Test Repeat Interval (Not to Exceed) Compliance TimeActionCondition -Within 12 months after the original issue date of Requirements Bulletin 737-22A1322 RB.
Install new Flight Control Computer (FCC) Operational Program Software (OPS) on FCC A and FCC B.
All airplanes.
-Do a software installation test.
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 Aviation Safety Agency (EASA)/Joint Aviation Authorities (JAA) approved for all EASA/JAA approved airplanes listed in the service 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: November 21, 2018 737-22A1322 RB 6 of 8 REQUIREMENTS BULLETIN 737-22A1322
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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. 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.
5. Later approved software is only software that is approved by Boeing as a replacement for the software specified in this bulletin and approved as part of the type design by the Federal Aviation Administration (FAA) after issuance of this bulletin Original Issue date.
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 21, 2018 737-22A1322 RB 7 of 8 REQUIREMENTS BULLETIN 737-22A1322
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B. WORK INSTRUCTIONS Actions Required for Compliance:
1. Requirements.
Table 1: Flight Control Computer Software Installation and Test Refer to the listed procedures in SB 737-22A1322 Original Issue or later approved revisions as an accepted procedure:
Method of ComplianceActionCondition PART 1: Flight Control Computer Software Installation and Test.
Install FCC OPS, software version P11.1, part number 2270-COL-AC2-22 or later approved software part number on FCC A and FCC B.
Install new Flight Control Computer (FCC) Operational Program Software (OPS) on FCC A and FCC B.
All airplanes.
Do a software installation test and make sure that software part number 2270-COL-AC2-22 or later approved software part number is installed on FCC A and FCC B. If software part number 2270-COL- AC2-22 or later approved software part number is not shown as installed on FCC A and FCC B, do corrective action(s) until the software part number is installed on FCC A and FCC B.
Do a software installation test.
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 21, 2018 737-22A1322 RB 8 of 8 REQUIREMENTS BULLETIN 737-22A1322