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Commercial Airplanes 747 Requirements Bulletin ALERT Number: 747-31A2544 RB Original Issue: March 31, 2020 ATA System: 3161 SUBJECT: INDICATING/RECORDING SYSTEMS - Integrated Display System - Integrated Display System 805 Software Installation 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 © 2020 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Unpublished Work.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: March 31, 2020 747-31A2544 RB 1 of 10
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Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: March 31, 2020 747-31A2544 RB 2 of 10 REQUIREMENTS BULLETIN 747-31A2544
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Table of Contents
1. EFFECTIVITY5
A. Airplanes5
B. Spares Affected6
2. CONCURRENT REQUIREMENTS6
3. COMPLIANCE6
4. APPROVAL7
5. ACCOMPLISHMENT INSTRUCTIONS9
A. General Information9
B. Work Instructions10
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: March 31, 2020 747-31A2544 RB 3 of 10 REQUIREMENTS BULLETIN 747-31A2544
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Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: March 31, 2020 747-31A2544 RB 4 of 10 REQUIREMENTS BULLETIN 747-31A2544
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Commercial Airplanes 747 Requirements Bulletin ALERT Number: 747-31A2544 RB Original Issue: March 31, 2020 ATA System: 3161 SUBJECT: INDICATING/RECORDING SYSTEMS - Integrated Display System - Integrated Display System 805 Software Installation
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 747-8, 747-8F Airplane(s), line number(s) 1420-1557 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.
DESCRIPTIONCONFIGURATIONGROUP 747-8, 747-8F airplanes delivered with Integrated Display System (IDS)-801, IDS-802, or IDS-803 software installed.
-1 747-8, 747-8F airplanes delivered with IDS-804 software installed.-2 Airplane Models:
747-8, 747-8F GroupVariable Number 1RC001 - RC009 2RC021 1RC022 - RC039 2RC040 GroupVariable Number 2RC051 - RC060 1RC066 - RC069 2RC070 - RC072 2RC076 - RC077 GroupVariable Number 1RC501 - RC512 2RC513 - RC514 1RC521 - RC528 2RC531 - RC540 Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: March 31, 2020 747-31A2544 RB 5 of 10
GroupVariable Number 1RC541 1RC546 - RC549 2RC550 1RC551 - RC564 2RC565 - RC566 GroupVariable Number 1RC571 - RC582 1RC601 - RC605 2RC606 - RC609 1RC641 - RC642 2RC643 - RC644 GroupVariable Number 2RC651 - RC652 2RC661 1RC671 - RC672 2RC673 - RC674 2RC681 - RC684 B. Spares Affected None.
2. CONCURRENT REQUIREMENTS Group 1:
The service bulletin(s) listed below must be done before or at the same time as this service bulletin:
DescriptionService BulletinCompany INDICATING/RECORDING SYSTEMS - Integrated Display System - Integrated Display System 804 Software Change.
747-31-2497 Original IssueBoeing Group 2:
None.
3. COMPLIANCE The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to Requirements Bulletin 747-31A2544 RB. The Airworthiness Directive will make the compliance tasks and times given in Requirements Bulletin 747-31A2544 RB mandatory.
Accomplish the required action(s), based on the applicable condition(s) in Table(s) 1, in accordance with Accomplishment Instructions.
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: March 31, 2020 747-31A2544 RB 6 of 10 REQUIREMENTS BULLETIN 747-31A2544
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Table 1: Integrated Display System Software Installation Repeat Interval Compliance TimeActionCondition -Within 12 months after the original issue date of Requirements Bulletin 747-31A2544 RB.
ACTION 1: Do all applicable ACCOM- PLISHMENT INSTRUCTIONS actions identified in the service bulletin specified in CONCURRENT REQUIREMENTS.
All airplanes.
ACTION 2: Install the Interface Units (EIU) Software part number COL3F- 0034-E805 or later approved software part number.
AND Do the software configuration check to make sure that the EIU Software part number COL3F-0034-E805 or later approved software part number is installed.
If EIU Software part number COL3F- 0034-E805 or later approved software part number is not installed, do the corrective action until the EIU software part number is installed.
ACTION 3: Install the Liquid Crystal Display (LCD) Software part number 3177-COL-DL8-05 or later approved software part number.
AND Do the software configuration check to make sure LCD Software part number 3177-COL-DL8-05 or later approved software part number is installed. If LCD Software part number 3177-COL-DL8- 05 or later approved software part number is not installed, do the corrective action until the LCD software part number is installed.
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: March 31, 2020 747-31A2544 RB 7 of 10 REQUIREMENTS BULLETIN 747-31A2544
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Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: March 31, 2020 747-31A2544 RB 8 of 10 REQUIREMENTS BULLETIN 747-31A2544
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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. 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.
5. 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.
Original Issue: March 31, 2020 747-31A2544 RB 9 of 10 REQUIREMENTS BULLETIN 747-31A2544
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B. WORK INSTRUCTIONS Actions Required for Compliance
1. Requirements:
Table 1: Integrated Display System Software Installation Refer to the listed procedures in SB 747-31A2544 Original Issue or later approved revisions as an accepted procedure.
Method of ComplianceActionCondition --ACTION 1: Do all applicable ACCOM- PLISHMENT INSTRUCTIONS actions identified in the service bulletin specified in CONCURRENT RE- QUIREMENTS.
All airplanes.
PART 1: Access-ACTION 2: Install the EIU Software part number COL3F-0034-E805 or later approved software part number.
PART 2: EIU OPS Software Installation.AND Do the software configuration check to make sure that the EIU Software part number COL3F-0034-E805 or later approved software part number is installed. If EIU Software part number COL3F-0034-E805 or later approved software part number is not installed, do the corrective action until the EIU software part number is installed.
PART 3: IDU OPS Software Installation.
-ACTION 3: Install the LCD Software part number 3177-COL-DL8-05 or later approved software part number.
AND Do the software configuration check to make sure LCD Software part number 3177-COL-DL8-05 or later approved software part number is installed. If LCD Software part number 3177-COL-DL8-05 or later approved software part number is not installed, do the corrective action until the LCD software part number is installed.
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: March 31, 2020 747-31A2544 RB 10 of 10 REQUIREMENTS BULLETIN 747-31A2544