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Aircraft Maintenance Manual

BOMBARDIER CHALLENGER 350 · Maintenance Manual

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Overview

The Bombardier Challenger 350 Maintenance Manual provides detailed technical information necessary for the maintenance, operation, and repair of the BD-100-1A10 aircraft model. It includes guidelines, procedures, and specifications relevant to the aircraft's systems and components.

  • Publication No. CH 350 AMM.
  • Model: BD-100-1A10 (CH-350 and CH 3500).
  • A/C Effectivity: 20501-21399.
  • Document is proprietary and confidential to Bombardier.
  • Technical assistance hotline available for North America and international.
  • Document includes a record of revisions.
  • Effective pages are listed with revision dates.
  • Maintenance procedures are outlined in detail.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.

Document

Source

Copy found at regulations.gov. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
·
Maintenance Manual
Year
·
2023
File size
·
564 KB
Copy found at
·
regulations.gov
Language
·
en
About this document
What is the Aircraft Maintenance Manual?

The Aircraft Maintenance Manual is a maintenance manual for the BOMBARDIER CHALLENGER 350, dated 2023.

What year was the Aircraft Maintenance Manual published?

The Aircraft Maintenance Manual — the BOMBARDIER CHALLENGER 350 maintenance manual on file — is dated 2023.

How rare is it?
1,280BOMBARDIER CHALLENGER 350 registered worldwide · 1,248 active

Common. More common than 97% of the aircraft models we track.

Documentation completeness
3/7

Most owners only have the POH. Here's the essential set for the BOMBARDIER CHALLENGER 350.

More BOMBARDIER CHALLENGER 350manuals & documents

In this document

Introduction

The manual serves as a comprehensive guide for maintaining the Challenger 350 aircraft, detailing necessary procedures and technical data.

Record of Revisions

This section lists all revisions made to the manual, including issue dates and the dates they were incorporated.

Effective Pages

A list of effective pages is provided, indicating which pages are current and applicable for maintenance.

Technical Assistance

Contact information for Bombardier's customer services hotline is provided for technical assistance and in-flight emergencies.

Proprietary Information

The document emphasizes that all information is proprietary to Bombardier and cannot be reproduced without authorization.

Maintenance Procedures

Detailed maintenance procedures for various aircraft systems are included, ensuring proper operation and safety.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Full document text

Aircraft Maintenance Manual Publication No. CH 350 AMM P A R T T W O MODEL BD-100-1A10 (CH-350 and CH 3500) A/C EFFECTIVITY 20501-21399 Bombardier Aerospace P. O. Box 6087, Station Centre-ville Montreal, Quebec, Canada H3C 3G9 https://my.businessaircraft.bombardier.com For more information regarding Technical Publications please contact: To ease the ordering process, please refer to Publication No. on cover page. It is understood that this documentation, comprising technical data and other information in any media shall not be reproduced or disclosed in whole or in part without Bombardier's written authorization, is proprietary and confidential to Bombardier and that all rights to patent, copyright, trademark, trade secret and other intellectual property rights therein belong to Bombardier. Such documentation, technical data and other information shall not be modified, translated, reverse assembled, reverse engineered or de-compiled and shall be used solely to maintain, operate or repair the aircraft. Copyright © 2023 by Bombardier Inc. All rights reserved. Printed in Canada Customer Services Hotline (Technical Assistance & In−flight Emergencies) North America: 1−866−JET−1247 (1−866−538−1247) International: +1−514−855−2999 Email: ac.yul@aero.bombardier.com User Comments (Technical Publications) North America: 1−866−JET−1247 (1−866−538−1247) International: +1−514−855−2999 Ordering & Distribution (Technical Publications) North America: 1−866−JET−1247 (1−866−538−1247) International: +1−514−855−2999 Bombardier Customer Services Business Aircraft Email: bbad.pubs.dist@aero.bombardier.com Email: bbad.user.comments@aero.bombardier.com Basic May 26/2014 May 26/2014 Bombardier 1 Aug 12/2014 Aug 12/2014 Bombardier 2 Oct 31/2014 Oct 31/2014 Bombardier 3 Feb 05/2015 Feb 05/2015 Bombardier 4 Mar 31/2015 Mar 31/2015 Bombardier 5 Jun 30/2015 Jun 30/2015 Bombardier 6 Sep 28/2015 Sep 28/2015 Bombardier 7 Dec 22/2015 Dec 22/2015 Bombardier 8 Mar 31/2016 Mar 31/2016 Bombardier 9 Jun 22/2016 Jun 22/2016 Bombardier 10 Sep 20/2016 Sep 20/2016 Bombardier 11 Dec 15/2016 Dec 15/2016 Bombardier 12 Mar 09/2017 Mar 09/2017 Bombardier 13 Jul 03/2017 Jul 03/2017 Bombardier 14 Sep 20/2017 Sep 20/2017 Bombardier 15 Dec 18/2017 Dec 18/2017 Bombardier 16 Mar 15/2018 Mar 15/2018 Bombardier 17 Jun 12/2018 Jun 12/2018 Bombardier 18 Sep 07/2018 Sep 07/2018 Bombardier 19 Dec 03/2018 Dec 03/2018 Bombardier 20 Apr 08/2019 Apr 08/2019 Bombardier 21 Jul 08/2019 Jul 08/2019 Bombardier BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II RECORD OF REVISIONS A signature in the "INSERTED BY" column shows that the publication holder has incorporated the revision. REVISION NO. ISSUE DATE DATE INSERTED INSERTED BY 22 Oct 01/2019 Oct 01/2019 Bombardier 23 Jan 15/2020 Jan 15/2020 Bombardier 24 Apr 01/2020 Apr 01/2020 Bombardier 25 Jul 01/2020 Jul 01/2020 Bombardier 26 Sep 25/2020 Sep 25/2020 Bombardier 27 Dec 22/2020 Dec 22/2020 Bombardier 28 Apr 01/2021 Apr 01/2021 Bombardier 29 Jun 28/2021 Jun 28/2021 Bombardier 30 Sep 22/2021 Sep 22/2021 Bombardier 31 Dec 17/2021 Dec 17/2021 Bombardier 32 Mar 29/2022 Mar 29/2022 Bombardier 33 Jun 14/2022 Jun 14/2022 Bombardier 34 Sep 27/2022 Sep 27/2022 Bombardier 35 Nov 09/2022 Nov 09/2022 Bombardier 36 May 11/2023 May 11/2023 Bombardier 37 Aug 09/2023 Aug 09/2023 Bombardier 38 Nov 09/2023 Nov 09/2023 Bombardier BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II RECORD OF REVISIONS A signature in the "INSERTED BY" column shows that the publication holder has incorporated the revision. REVISION NO. ISSUE DATE DATE INSERTED INSERTED BY 24 − Effective Pages 1 Nov 09/2023 20231109 2 Sep 25/2020 20200925 3 May 11/2023 20230511 4 Aug 09/2023 20230809 5 Jun 14/2022 20220614 6 Jun 28/2021 20210628 7 Jun 28/2021 20210628 8 May 11/2023 20230511 9 Jun 14/2022 20220614 10 Jun 14/2022 20220614 11 Mar 29/2022 20220329 24 − Effective Temporary Revisions 1 Nov 09/2023 20231109 24 − Contents 1 May 26/2014 20140526 2 May 26/2014 20140526 3 Apr 01/2020 20200401 4 Apr 01/2020 20200401 5 Apr 01/2020 20200401 6 Jun 14/2022 20220614 7 Apr 01/2020 20200401 8 Apr 01/2020 20200401 9 Jul 01/2020 20200701 10 Apr 01/2020 20200401 11 Apr 01/2020 20200401 12 Apr 01/2020 20200401 13 Apr 01/2020 20200401 14 Apr 01/2020 20200401 15 Apr 01/2020 20200401 16 Apr 01/2020 20200401 24−00−00 ALL 201 Apr 01/2020 20200401 202 Apr 01/2020 20200401 203 Apr 01/2020 20200401 204 Sep 28/2015 20150928 205 Sep 25/2020 20200925 206 Sep 25/2020 20200925 207 Sep 25/2020 20200925 208 Sep 25/2020 20200925 24−00−00 ALL 501 Mar 15/2018 20180315 502 Mar 15/2018 20180315 24−31−00 ALL 101 May 26/2014 20140526 102 May 26/2014 20140526 103 May 26/2014 20140526 104 May 26/2014 20140526 24−31−00 ALL 201 Mar 09/2017 20170309 202 Mar 09/2017 20170309 203 Mar 09/2017 20170309 204 May 26/2014 20140526 205 May 26/2014 20140526 206 May 26/2014 20140526 207 May 26/2014 20140526 208 May 26/2014 20140526 209 May 26/2014 20140526 210 May 26/2014 20140526 211 Mar 15/2018 20180315 212 Mar 15/2018 20180315 213 May 26/2014 20140526 214 May 26/2014 20140526 215 May 26/2014 20140526 216 May 26/2014 20140526 217 May 26/2014 20140526 218 May 26/2014 20140526 219 May 26/2014 20140526 220 May 26/2014 20140526 24−31−01 ALL 401 Mar 09/2017 20170309 402 Jun 14/2022 20220614 403 Jul 01/2020 20200701 404 Jul 01/2020 20200701 24−31−01 ALL 501 Jul 03/2017 20170703 502 May 26/2014 20140526 503 Jun 30/2015 20150630 504 May 26/2014 20140526 505 May 26/2014 20140526 506 Dec 18/2017 20171218 507 Dec 18/2017 20171218 508 Dec 18/2017 20171218 509 May 26/2014 20140526 510 May 26/2014 20140526 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II CHAPTER 24 − ELECTRICAL POWER LIST OF EFFECTIVE PAGES 24 − EFFECTIVE PAGES Page 1

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Nov 09/2023 Ch−Se−Su Effectivity Page Date Ch−Se−Su Effectivity Page Date EFFECTIVITY: ALL 24−31−01 ALL 511 May 26/2014 20140526 512 Mar 15/2018 20180315 513 Mar 15/2018 20180315 514 Mar 15/2018 20180315 515 Mar 15/2018 20180315 516 Mar 15/2018 20180315 517 Mar 15/2018 20180315 518 Mar 15/2018 20180315 519 Mar 15/2018 20180315 520 Mar 15/2018 20180315 521 Mar 15/2018 20180315 522 Mar 15/2018 20180315 523 May 26/2014 20140526 524 May 26/2014 20140526 525 May 26/2014 20140526 526 May 26/2014 20140526 527 May 26/2014 20140526 528 May 26/2014 20140526 24−31−05 ALL 301 May 26/2014 20140526 24−31−05 ALL 401 May 26/2014 20140526 402 Jun 12/2018 20180612 403 May 26/2014 20140526 404 Sep 07/2018 20180907 405 Sep 25/2020 20200925 406 Sep 25/2020 20200925 407 Sep 25/2020 20200925 408 Sep 25/2020 20200925 409 Sep 25/2020 20200925 24−31−05 ALL 501 Sep 07/2018 20180907 502 Sep 07/2018 20180907 503 Sep 07/2018 20180907 504 Sep 20/2017 20170920 505 Mar 15/2018 20180315 506 Mar 15/2018 20180315 507 Sep 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Page Date Ch−Se−Su Effectivity Page Date EFFECTIVITY: ALL 24−61−73 ALL 401 Dec 18/2017 20171218 402 Dec 18/2017 20171218 403 May 26/2014 20140526 404 May 26/2014 20140526 405 Sep 25/2020 20200925 406 Oct 31/2014 20141031 407 Sep 25/2020 20200925 24−61−77 ALL 401 Mar 15/2018 20180315 402 Mar 15/2018 20180315 403 May 26/2014 20140526 404 May 26/2014 20140526 405 Mar 15/2018 20180315 406 Mar 15/2018 20180315 407 Mar 15/2018 20180315 24−61−79 ALL 401 Mar 15/2018 20180315 402 Mar 15/2018 20180315 403 May 26/2014 20140526 404 Sep 25/2020 20200925 405 Mar 31/2015 20150331 406 Sep 25/2020 20200925 24−61−81 ALL 401 Mar 15/2018 20180315 402 May 26/2014 20140526 403 May 26/2014 20140526 404 May 26/2014 20140526 405 Apr 08/2019 20190408 406 Apr 08/2019 20190408 407 Apr 08/2019 20190408 24−61−82 ALL 401 Mar 15/2018 20180315 402 Mar 15/2018 20180315 403 May 26/2014 20140526 404 May 26/2014 20140526 405 Jul 01/2020 20200701 406 Jul 01/2020 20200701 407 Jul 01/2020 20200701 24−62−00 ALL 101 May 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Sep 07/2018 20180907 403 May 26/2014 20140526 404 Sep 07/2018 20180907 405 Sep 07/2018 20180907 24−62−04 ALL 401 Mar 15/2018 20180315 402 May 26/2014 20140526 403 May 26/2014 20140526 404 May 26/2014 20140526 405 Mar 15/2018 20180315 406 Mar 15/2018 20180315 24−62−05 ALL 401 Apr 08/2019 20190408 402 Apr 08/2019 20190408 403 Apr 08/2019 20190408 404 May 26/2014 20140526 405 Mar 09/2017 20170309 406 Dec 03/2018 20181203 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − EFFECTIVE PAGES Page 7 Jun 28/2021 Ch−Se−Su Effectivity Page Date Ch−Se−Su Effectivity Page Date EFFECTIVITY: ALL 24−62−05 ALL 407 Mar 09/2017 20170309 408 Jul 01/2020 20200701 409 Sep 25/2020 20200925 410 Sep 25/2020 20200925 411 Sep 25/2020 20200925 412 Sep 25/2020 20200925 24−63−00 ALL 101 May 26/2014 20140526 102 May 26/2014 20140526 24−63−01 ALL 401 Jun 12/2018 20180612 402 May 26/2014 20140526 403 May 26/2014 20140526 404 Jun 12/2018 20180612 405 Jun 12/2018 20180612 406 Jun 12/2018 20180612 407 Jun 12/2018 20180612 408 May 26/2014 20140526 409 Jun 12/2018 20180612 410 May 26/2014 20140526 411 May 26/2014 20140526 24−63−01 ALL 501 May 26/2014 20140526 502 May 26/2014 20140526 503 Sep 20/2017 20170920 504 Sep 20/2017 20170920 505 Dec 15/2016 20161215 506 Dec 15/2016 20161215 507 May 26/2014 20140526 508 Dec 15/2016 20161215 509 Jun 14/2022 20220614 510 May 11/2023 20230511 511 Jun 14/2022 20220614 512 Jul 01/2020 20200701 513 Jul 01/2020 20200701 514 Jul 01/2020 20200701 515 Jul 01/2020 20200701 516 Jul 01/2020 20200701 517 May 26/2014 20140526 518 May 26/2014 20140526 519 Jul 03/2017 20170703 520 May 26/2014 20140526 521 Mar 15/2018 20180315 522 Mar 15/2018 20180315 523 Mar 15/2018 20180315 524 Mar 15/2018 20180315 525 Mar 15/2018 20180315 526 May 26/2014 20140526 527 May 26/2014 20140526 24−63−01 ALL 528 May 26/2014 20140526 529 May 26/2014 20140526 530 May 26/2014 20140526 531 May 26/2014 20140526 532 May 26/2014 20140526 533 May 26/2014 20140526 534 May 26/2014 20140526 535 May 26/2014 20140526 536 May 26/2014 20140526 537 Jul 01/2020 20200701 538 Jun 14/2022 20220614 539 Dec 03/2018 20181203 540 Dec 03/2018 20181203 541 Jul 01/2020 20200701 542 Jun 14/2022 20220614 543 Jun 14/2022 20220614 544 Jun 14/2022 20220614 24−63−03 ALL 401 May 26/2014 20140526 402 May 26/2014 20140526 403 Mar 31/2015 20150331 404 May 26/2014 20140526 24−63−05 ALL 401 Sep 25/2020 20200925 402 Sep 25/2020 20200925 403 May 26/2014 20140526 404 Sep 07/2018 20180907 405 Mar 31/2015 20150331 406 May 26/2014 20140526 407 Sep 07/2018 20180907 408 Sep 07/2018 20180907 409 Mar 09/2017 20170309 410 Sep 07/2018 20180907 411 Sep 07/2018 20180907 24−63−05 ALL 501 May 26/2014 20140526 502 May 26/2014 20140526 503 Dec 15/2016 20161215 504 Dec 15/2016 20161215 505 May 26/2014 20140526 506 May 26/2014 20140526 507 May 26/2014 20140526 508 May 26/2014 20140526 509 Sep 25/2020 20200925 510 May 11/2023 20230511 511 May 11/2023 20230511 512 Jan 15/2020 20200115 513 Sep 22/2021 20210922 514 Jan 15/2020 20200115 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − EFFECTIVE PAGES Page 8 May 11/2023 Ch−Se−Su Effectivity Page Date Ch−Se−Su Effectivity Page Date EFFECTIVITY: ALL 24−63−05 ALL 515 Jan 15/2020 20200115 516 Jan 15/2020 20200115 517 Jan 15/2020 20200115 518 Jan 15/2020 20200115 519 Jan 15/2020 20200115 520 Sep 25/2020 20200925 521 Jan 15/2020 20200115 522 Jan 15/2020 20200115 523 Jan 15/2020 20200115 524 Jan 15/2020 20200115 525 Jan 15/2020 20200115 526 Jan 15/2020 20200115 527 Jan 15/2020 20200115 528 Jan 15/2020 20200115 529 Jan 15/2020 20200115 530 Jan 15/2020 20200115 531 Jan 15/2020 20200115 532 Jan 15/2020 20200115 533 Jan 15/2020 20200115 534 Jan 15/2020 20200115 535 Jan 15/2020 20200115 536 Jan 15/2020 20200115 537 Jan 15/2020 20200115 538 Jan 15/2020 20200115 539 Jan 15/2020 20200115 540 Jan 15/2020 20200115 541 Jan 15/2020 20200115 542 Jul 01/2020 20200701 543 Dec 22/2020 20201222 544 May 26/2014 20140526 545 May 26/2014 20140526 546 May 26/2014 20140526 547 Jul 01/2020 20200701 548 Jul 01/2020 20200701 549 Jul 01/2020 20200701 550 Jul 01/2020 20200701 24−63−07 ALL 401 May 26/2014 20140526 402 May 26/2014 20140526 403 Mar 31/2015 20150331 404 May 26/2014 20140526 24−63−09 ALL 401 Sep 07/2018 20180907 402 May 26/2014 20140526 403 May 26/2014 20140526 404 Jun 12/2018 20180612 405 Jun 12/2018 20180612 406 Jul 01/2020 20200701 407 Jul 01/2020 20200701 24−63−09 ALL 408 May 26/2014 20140526 409 Jun 12/2018 20180612 410 May 26/2014 20140526 411 May 26/2014 20140526 24−63−09 ALL 501 May 26/2014 20140526 502 May 26/2014 20140526 503 Sep 20/2017 20170920 504 Sep 20/2017 20170920 505 May 26/2014 20140526 506 May 26/2014 20140526 507 Mar 29/2022 20220329 508 Dec 03/2018 20181203 509 May 26/2014 20140526 510 Jun 14/2022 20220614 511 Jun 14/2022 20220614 512 Jun 14/2022 20220614 513 Jun 14/2022 20220614 514 Jun 14/2022 20220614 515 May 26/2014 20140526 516 Feb 05/2015 20150205 517 May 26/2014 20140526 518 May 26/2014 20140526 519 May 26/2014 20140526 520 May 26/2014 20140526 521 Mar 31/2015 20150331 522 Feb 05/2015 20150205 523 Feb 05/2015 20150205 524 May 26/2014 20140526 525 May 26/2014 20140526 526 May 26/2014 20140526 527 Jul 03/2017 20170703 528 May 26/2014 20140526 529 Feb 05/2015 20150205 530 Mar 29/2022 20220329 531 Feb 05/2015 20150205 532 Jun 14/2022 20220614 533 Jun 14/2022 20220614 534 Jun 28/2021 20210628 535 May 26/2014 20140526 536 Jun 14/2022 20220614 537 Jun 14/2022 20220614 538 Jun 14/2022 20220614 539 May 26/2014 20140526 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − EFFECTIVE PAGES Page 9 Jun 14/2022 Ch−Se−Su Effectivity Page Date Ch−Se−Su Effectivity Page Date EFFECTIVITY: ALL 24−63−11 ALL 401 May 26/2014 20140526 402 May 26/2014 20140526 403 Mar 31/2015 20150331 404 May 26/2014 20140526 24−63−13 ALL 401 Jun 12/2018 20180612 402 May 26/2014 20140526 403 Jun 14/2022 20220614 404 Jun 12/2018 20180612 405 Jun 12/2018 20180612 406 Jun 12/2018 20180612 407 Jun 12/2018 20180612 408 Jun 14/2022 20220614 409 Jun 12/2018 20180612 410 May 26/2014 20140526 411 May 26/2014 20140526 24−63−13 ALL 501 May 26/2014 20140526 502 May 26/2014 20140526 503 May 26/2014 20140526 504 May 26/2014 20140526 505 May 26/2014 20140526 506 Dec 03/2018 20181203 507 May 26/2014 20140526 508 Jun 14/2022 20220614 509 Jun 14/2022 20220614 510 Jun 14/2022 20220614 511 Jun 14/2022 20220614 512 Jun 14/2022 20220614 513 Jun 14/2022 20220614 514 Jun 14/2022 20220614 515 Jun 14/2022 20220614 516 Jun 14/2022 20220614 517 Jun 14/2022 20220614 518 Jun 14/2022 20220614 519 Jun 14/2022 20220614 520 Jun 14/2022 20220614 521 Jun 14/2022 20220614 522 Jun 14/2022 20220614 523 Jun 14/2022 20220614 524 Jun 14/2022 20220614 525 Jun 14/2022 20220614 526 Jun 14/2022 20220614 527 Jun 14/2022 20220614 528 Jun 14/2022 20220614 529 Jun 14/2022 20220614 530 Jun 14/2022 20220614 531 Jun 14/2022 20220614 532 Jun 14/2022 20220614 24−63−13 ALL 533 Jun 14/2022 20220614 534 Jun 28/2021 20210628 535 May 26/2014 20140526 536 Jun 14/2022 20220614 537 Jun 14/2022 20220614 538 Jun 14/2022 20220614 539 May 26/2014 20140526 24−63−15 ALL 401 May 26/2014 20140526 402 Jun 14/2022 20220614 403 Mar 31/2015 20150331 404 May 26/2014 20140526 24−64−00 ALL 101 May 26/2014 20140526 102 May 26/2014 20140526 24−64−01 ALL 401 Mar 15/2018 20180315 402 Mar 15/2018 20180315 403 May 26/2014 20140526 404 Dec 03/2018 20181203 405 Jul 01/2020 20200701 406 Jul 01/2020 20200701 24−64−01 ALL 501 May 26/2014 20140526 502 May 26/2014 20140526 503 May 26/2014 20140526 504 May 26/2014 20140526 505 May 26/2014 20140526 506 May 26/2014 20140526 24−64−03 ALL 401 Mar 15/2018 20180315 402 May 26/2014 20140526 403 Dec 03/2018 20181203 404 Dec 03/2018 20181203 24−64−04 ALL 401 Mar 15/2018 20180315 402 Mar 15/2018 20180315 403 Mar 15/2018 20180315 404 Mar 15/2018 20180315 24−64−05 ALL 401 Mar 15/2018 20180315 402 May 26/2014 20140526 403 May 26/2014 20140526 404 Mar 15/2018 20180315 405 Mar 15/2018 20180315 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − EFFECTIVE PAGES Page 10 Jun 14/2022 Ch−Se−Su Effectivity Page Date Ch−Se−Su Effectivity Page Date EFFECTIVITY: ALL 24−64−09 ALL 401 Mar 15/2018 20180315 402 May 26/2014 20140526 403 May 26/2014 20140526 404 Mar 15/2018 20180315 405 Mar 15/2018 20180315 24−64−13 ALL 401 Mar 15/2018 20180315 402 May 26/2014 20140526 403 Mar 15/2018 20180315 404 Mar 15/2018 20180315 24−64−17 ALL 401 Mar 15/2018 20180315 402 May 26/2014 20140526 403 May 26/2014 20140526 404 Mar 15/2018 20180315 405 Mar 15/2018 20180315 24−65−00 ALL 401 Sep 25/2020 20200925 402 Sep 25/2020 20200925 403 Mar 31/2015 20150331 404 Jul 08/2019 20190708 405 Jul 08/2019 20190708 406 Jul 08/2019 20190708 407 Sep 25/2020 20200925 408 Sep 25/2020 20200925 409 Jan 15/2020 20200115 410 Jan 15/2020 20200115 411 Jan 15/2020 20200115 24−65−00 ALL 501 Sep 25/2020 20200925 502 Mar 29/2022 20220329 503 Sep 25/2020 20200925 504 Sep 25/2020 20200925 505 Sep 25/2020 20200925 506 Jan 15/2020 20200115 24−65−01 ALL 201 Sep 25/2020 20200925 202 Sep 25/2020 20200925 203 Sep 25/2020 20200925 204 Sep 25/2020 20200925 205 Sep 25/2020 20200925 206 Jul 08/2019 20190708 207 Jul 08/2019 20190708 208 Jul 08/2019 20190708 209 Jul 08/2019 20190708 210 Jul 08/2019 20190708 211 Jul 08/2019 20190708 24−65−01 ALL 401 May 26/2014 20140526 402 May 26/2014 20140526 403 May 26/2014 20140526 404 May 26/2014 20140526 405 May 26/2014 20140526 406 Dec 03/2018 20181203 407 Dec 03/2018 20181203 408 Jul 01/2020 20200701 24−65−03 ALL 201 Jun 12/2018 20180612 202 Jun 12/2018 20180612 203 Jun 12/2018 20180612 204 Jun 12/2018 20180612 205 Jun 12/2018 20180612 206 Jun 12/2018 20180612 207 Jun 12/2018 20180612 208 Jun 12/2018 20180612 209 Jun 12/2018 20180612 24−65−05 ALL 201 Dec 18/2017 20171218 202 Mar 29/2022 20220329 203 Mar 29/2022 20220329 204 Mar 29/2022 20220329 205 Mar 29/2022 20220329 206 Mar 29/2022 20220329 207 Mar 29/2022 20220329 208 Mar 29/2022 20220329 209 Mar 29/2022 20220329 210 Mar 29/2022 20220329 211 Mar 29/2022 20220329 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − EFFECTIVE PAGES Page 11 Mar 29/2022 Ch−Se−Su Effectivity Page Date Ch−Se−Su Effectivity Page Date EFFECTIVITY: ALL ELECTRICAL POWER 24−00−00 Maintenance Practices ALL TASK 24−00−00−910−801 Electrical/Electronic Safety Precautions 201 TASK 24−00−00−910−802 Electrostatic−Discharge Safety Precautions 204 TASK 24−00−00−861−801 Connect Electrical Power to the Aircraft 205 TASK 24−00−00−861−802 Remove the Electrical Power from the Aircraft 207 Adjustment/Test ALL TASK 24−00−00−710−801 Operational Check (Cycling) of Thermal Circuit Breakers 501 PRIMARY DC−POWER SYSTEM 24−31−00 Component Location ALL TASK 24−31−00−992−801 Component Location 101 Maintenance Practices ALL TASK 24−31−00−861−801 Energize the Primary DC−Power Supply 201 TASK 24−31−00−861−802 Removal of the Power for the Primary DC−Power Supply 207 TASK 24−31−00−861−803 Energize the Auxiliary DC−Power Supply 210 TASK 24−31−00−861−804 Removal of the Power for the Auxiliary DC−Power Supply 218 ELECTRICAL CONTROL PANEL 24−31−01 Removal/Installation ALL TASK 24−31−01−000−801 Removal of the Electrical Control Panel 401 TASK 24−31−01−400−801 Installation of the Electrical Control Panel 403 Adjustment/Test ALL TASK 24−31−01−710−801 Operational Test of the ELECTRICAL Control Panel 501 TASK 24−31−01−710−802 Operational Test of the ELECTRICAL Control Panel (For Return to Service) 506 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II CHAPTER 24 − ELECTRICAL POWER TABLE OF CONTENTS 24 − CONTENTS Page 1 May 26/2014 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL MAIN GENERATOR 24−31−05 Servicing ALL TASK 24−31−05−610−801 Restoration (Overhaul) of the Main Generator 301 Removal/Installation ALL TASK 24−31−05−000−801 Removal of the Main Generator 401 TASK 24−31−05−400−801 Installation of the Main Generator 405 Adjustment/Test ALL TASK 24−31−05−710−801 Operational Test of the Main Generator 501 APU GENERATOR 24−31−09 Servicing ALL TASK 24−31−09−610−801 Restoration (Overhaul) of the Auxiliary Power Unit (APU) Generator 301 Removal/Installation ALL TASK 24−31−09−000−801 Removal of the APU Generator 401 TASK 24−31−09−400−801 Installation of the APU Generator 406 Adjustment/Test ALL TASK 24−31−09−710−801 Operational Test of the APU Generator 501 GENERATOR CONTROL UNIT (GCU) − PRIMARY 24−31−13 Removal/Installation ALL TASK 24−31−13−000−801 Removal of the Generator Control Unit (GCU) − Primary 401 TASK 24−31−13−400−801 Installation of the Generator Control Unit (GCU) − primary 405 AUXILIARY GENERATOR CONTROL−UNIT 24−31−17 Removal/Installation ALL TASK 24−31−17−000−801 Removal of the Auxiliary Generator Control−Unit 401 TASK 24−31−17−400−801 Installation of the Auxiliary Generator Control−Unit 404 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − CONTENTS Page 2 May 26/2014 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL GENERATOR POWER MODULE 24−31−21 Removal/Installation ALL TASK 24−31−21−000−801 Removal of the Generator Power Module 401 TASK 24−31−21−400−801 Installation of the Generator Power Module 405 AUXILIARY GENERATOR POWER−MODULE 24−31−25 Removal/Installation ALL TASK 24−31−25−000−801 Removal of the Auxiliary Generator Power−Module 401 TASK 24−31−25−400−801 Installation of the Auxiliary Generator Power−Module 404 BATTERY SYSTEM 24−32−00 Component Location ALL TASK 24−32−00−992−801 Component Location 101 Maintenance Practices ALL TASK 24−32−00−040−801 Disconnect the Batteries 201 TASK 24−32−00−440−801 Connect the Batteries 204 BATTERY 24−32−01 Servicing ALL TASK 24−32−01−610−801 Restoration (Bench Check) of the Batteries 301 Removal/Installation ALL TASK 24−32−01−000−801 Removal of the Battery 401 TASK 24−32−01−400−801 Installation of the Battery 403 Adjustment/Test ALL TASK 24−32−01−710−801 Operational Test of the Batteries 501 TASK 24−32−01−720−801 Functional Test of the Batteries 504 BATTERY HARNESS ASSEMBLY 24−32−03 Removal/Installation ALL TASK 24−32−03−000−801 Removal of the Battery Cables 401 TASK 24−32−03−400−801 Installation of the Battery Cables 407 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − CONTENTS Page 3 Apr 01/2020 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL STANDBY INSTRUMENT BATTERY 24−32−05 Servicing ALL TASK 24−32−05−610−801 Restoration of the Integrated Standby−Instrument (ISI) Battery, Part No. 100−2410−02 301 Removal/Installation ALL TASK 24−32−05−000−801 Removal of the Standby Instrument Battery 401 TASK 24−32−05−400−801 Installation of the Standby Instrument Battery 404 Adjustment/Test ALL TASK 24−32−05−710−801 Operational Test of the Integrated − Standby Instrument (ISI) Battery Capacity 501 TASK 24−32−05−710−802 Operational Test of the Built − In Test (BIT) for the Integrated Standby − Instrument (ISI) Battery 507 STANDBY INSTRUMENT BATTERY TRAY 24−32−07 Removal/Installation ALL TASK 24−32−07−000−801 Removal of the Standby-Instrument Battery Tray 401 TASK 24−32−07−400−801 Installation of the Standby-Instrument Battery Tray 403 EMERGENCY DC−POWER SYSTEM 24−33−00 Adjustment/Test Post SB 350−24−001 TASK 24−33−00−710−801 Operational Test of the HMDG System 501 HYDRAULIC−MOTOR DRIVEN GENERATOR (HMDG) 24−33−01 Removal/Installation ALL TASK 24−33−01−000−801 Removal of the Hydraulic−Motor Driven Generator (HMDG) 401 TASK 24−33−01−400−801 Installation of the Hydraulic−Motor Driven Generator (HMDG) 406 TASK 24−33−01−040−801 Deactivation of the Hydraulic−Motor Driven Generator (HMDG) 411 TASK 24−33−01−440−801 Activation of the Hydraulic−Motor Driven Generator (HMDG) 415 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − CONTENTS Page 4 Apr 01/2020 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL ECOLOGY BOTTLE 24−33−05 Removal/Installation ALL TASK 24−33−05−000−801 Removal of the Ecology Bottle 401 TASK 24−33−05−400−801 Installation of the Ecology Bottle 404 GENERATOR CONTROL UNIT (GCU) − EMERGENCY 24−33−09 Removal/Installation ALL TASK 24−33−09−000−801 Removal of the Generator Control Unit (GCU)−Emergency 401 TASK 24−33−09−400−801 Installation of the Generator Control Unit (GCU)−Emergency 404 POWER CENTER 24−33−13 Removal/Installation ALL TASK 24−33−13−000−801 Removal of the Power Center 401 TASK 24−33−13−400−801 Installation of the Power Center 404 EXTERNAL DC POWER 24−41−00 Component Location ALL TASK 24−41−00−992−801 Component Location 101 Maintenance Practices ALL TASK 24−41−00−861−801 Connect and Energize External DC Power 201 TASK 24−41−00−861−802 Remove External DC Power 206 EXTERNAL−POWER CONTROL PANEL 24−41−05 Removal/Installation ALL TASK 24−41−05−000−801 Removal of the External−Power Control Panel 401 TASK 24−41−05−400−801 Installation of the External−Power Control Panel 404 Adjustment/Test ALL TASK 24−41−05−710−801 Operational Test of the External−Power Control Panel 501 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − CONTENTS Page 5 Apr 01/2020 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL DC POWER CENTER (DCPC) SYSTEM 24−61−00 Component Location ALL TASK 24−61−00−992−801 Component Location 101 DC POWER CENTER (DCPC) 24−61−01 Servicing ALL TASK 24−61−01−160−801 Restoration (Cleaning) of the Left DC Power Center (DCPC) 301 Removal/Installation ALL TASK 24−61−01−000−801 Removal of the DC Power Center (DCPC) 401 TASK 24−61−01−400−801 Installation of the DC Power Center (DCPC) 407 Adjustment/Test ALL TASK 24−61−01−720−801 Functional Test of the DC Power Center (DCPC) 501 BATTERY CONTACTOR 24−61−05 Removal/Installation ALL TASK 24−61−05−000−801 Removal of the Battery Contactor 401 TASK 24−61−05−400−801 Installation of the Battery Contactor 405 Adjustment/Test ALL TASK 24−61−05−710−801 Operational Test of the Battery Contactor 501 GENERATOR LINE CONTACTOR 24−61−09 Removal/Installation ALL TASK 24−61−09−000−801 Removal of the Generator Line Contactor 401 TASK 24−61−09−400−801 Installation of the Generator Line Contactor 405 AUXILIARY POWER CONTACTOR 24−61−13 Removal/Installation ALL TASK 24−61−13−000−801 Removal of the Auxiliary Power Contactor 401 TASK 24−61−13−400−801 Installation of the Auxiliary Power Contactor 405 Adjustment/Test ALL TASK 24−61−13−710−801 Operational Test of the Auxiliary Power Contactor 501 TASK 24−61−13−710−802 Operational Test of the Auxiliary Power Contactor (For Return to Service) 515 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − CONTENTS Page 6 Jun 14/2022 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL EXTERNAL DC CONTACTOR 24−61−17 Removal/Installation ALL TASK 24−61−17−000−801 Removal of the External DC Contactor 401 TASK 24−61−17−400−801 Installation of the External DC Contactor 404 Adjustment/Test ALL TASK 24−61−17−710−801 Operational Test of the External DC Contactor 501 GROUND SERVICE CONTACTOR (GSC) 24−61−19 Removal/Installation ALL TASK 24−61−19−000−801 Removal of the Ground Service Contactor (GSC) 401 TASK 24−61−19−400−801 Installation of the Ground Service Contactor (GSC) 404 AUXILIARY CONTACTOR 24−61−21 Removal/Installation ALL TASK 24−61−21−000−801 Removal of the Auxiliary Contactor 401 TASK 24−61−21−400−801 Installation of the Auxiliary Contactor 405 Adjustment/Test ALL TASK 24−61−21−710−801 Operational Test of the Auxiliary Contactor 501 ESSENTIAL CONTACTOR 24−61−25 Removal/Installation ALL TASK 24−61−25−000−801 Removal of the Essential Contactor 401 TASK 24−61−25−400−801 Installation of the Essential Contactor 405 Adjustment/Test ALL TASK 24−61−25−710−801 Operational Test of the Electrical System Emergency Mode 501 BUS TIE CONTACTOR 24−61−29 Removal/Installation ALL TASK 24−61−29−000−801 Removal of the Bus Tie Contactor 401 TASK 24−61−29−400−801 Installation of the Bus Tie Contactor 405 Adjustment/Test ALL TASK 24−61−29−710−801 Operational Test of the Bus Tie Contactor 501 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − CONTENTS Page 7 Apr 01/2020 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL HYDRAULIC PUMP CONTACTOR 24−61−33 Removal/Installation ALL TASK 24−61−33−000−801 Removal of the Hydraulic Pump Contactor 401 TASK 24−61−33−400−801 Installation of the Hydraulic Pump Contactor 405 GENERATOR SENSOR 24−61−41 Removal/Installation ALL TASK 24−61−41−000−801 Removal of the Generator Sensor 401 TASK 24−61−41−400−801 Installation of the Generator Sensor 405 Adjustment/Test ALL TASK 24−61−41−710−801 Operational Test of the Generator Sensor 501 BATTERY SENSOR 24−61−45 Removal/Installation ALL TASK 24−61−45−000−801 Removal of the Battery Sensor 401 TASK 24−61−45−400−801 Installation of the Battery Sensor 407 HYDRAULIC−PUMP MONITORING CURRENT SENSOR 24−61−47 Removal/Installation ALL TASK 24−61−47−000−801 Removal of the Hydraulic−Pump Monitoring Current Sensor 401 TASK 24−61−47−400−801 Installation of the Hydraulic−Pump Monitoring Current Sensor 405 Adjustment/Test ALL TASK 24−61−47−710−801 Operational Test of the Hydraulic−Pump Monitoring Current Sensor 501 CURRENT THERMAL SENSOR 24−61−51 Removal/Installation ALL TASK 24−61−51−000−801 Removal of the Current Thermal Sensor 401 TASK 24−61−51−400−801 Installation of the Current Thermal Sensor 405 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − CONTENTS Page 8 Apr 01/2020 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL REMOTE−CONTROL CIRCUIT BREAKER (RCCB) CONTACTORS 24−61−61 Removal/Installation ALL TASK 24−61−61−000−801 Removal of the Remote−Control Circuit Breaker (RCCB) Contactors 401 TASK 24−61−61−400−801 Installation of the Remote−Control Circuit Breaker (RCCB) Contactors 406 AUXILIARY HYDRAULIC−PUMP CONTACTOR 24−61−69 Removal/Installation ALL TASK 24−61−69−000−801 Removal of the Auxiliary Hydraulic−Pump Contactor 401 TASK 24−61−69−400−801 Installation of the Auxiliary Hydraulic−Pump Contactor 404 DC POWER−CENTER PRIMARY−LOGIC 24−61−73 Removal/Installation ALL TASK 24−61−73−000−801 Removal of the DC Power−Center Primary−Logic 401 TASK 24−61−73−400−801 Installation of the DC Power−Center Primary−Logic 405 DC POWER−CENTER PROTECTION 24−61−77 Removal/Installation ALL TASK 24−61−77−000−801 Removal of the DC Power−Center Protection 401 TASK 24−61−77−400−801 Installation of the DC Power−Center Protection 405 DC POWER−CENTER FUSES 24−61−79 Removal/Installation ALL TASK 24−61−79−000−801 Removal of the DC Power−Center Fuses 401 TASK 24−61−79−400−801 Installation of the DC Power−Center Fuses 404 DC POWER−CENTER RELAYS 24−61−81 Removal/Installation ALL TASK 24−61−81−000−801 Removal of the DC Power−Center Relays 401 TASK 24−61−81−400−801 Installation of the DC Power−Center Relays 405 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − CONTENTS Page 9 Jul 01/2020 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL DCPC BATTERY DIODE 24−61−82 Removal/Installation ALL TASK 24−61−82−000−801 Removal of the DCPC Battery−Diode Printed−Circuit−Board (PCB) 401 TASK 24−61−82−400−801 Installation of the DCPC Battery−Diode Printed−Circuit−Board (PCB) 405 SECONDARY POWER CENTER (SPC) SYSTEM 24−62−00 Component Location ALL TASK 24−62−00−992−801 Component Location 101 SECONDARY POWER CENTER (SPC) 24−62−01 Removal/Installation ALL TASK 24−62−01−000−801 Removal of the Secondary Power Center (SPC) 401 TASK 24−62−01−400−801 Installation of the Secondary Power Center (SPC) 405 Adjustment/Test ALL TASK 24−62−01−710−801 Operational Test of the Secondary Power Center (SPC) 501 SECONDARY POWER CENTER (SPC) FUSES 24−62−03 Removal/Installation ALL TASK 24−62−03−000−801 Removal of the Secondary Power Center (SPC) Fuses 401 TASK 24−62−03−400−801 Installation of the Secondary Power Center (SPC) Fuses 404 SECONDARY POWER CENTER (SPC) RELAYS 24−62−04 Removal/Installation ALL TASK 24−62−04−000−801 Removal of the Secondary Power Center (SPC) Relays 401 TASK 24−62−04−400−801 Installation of the Secondary Power Center (SPC) Relays 405 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − CONTENTS Page 10 Apr 01/2020 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL REMOTE−CONTROL CIRCUIT BREAKER (RCCB) 24−62−05 Removal/Installation ALL TASK 24−62−05−000−801 Removal of the Remote−Control Circuit Breaker (RCCB) Contactor and RCCB Thermal Current Sensor 401 TASK 24−62−05−400−801 Installation of the Remote−Control Circuit Breaker (RCCB) Contactor and RCCB Thermal Current Sensor 408 COMPONENT LOCATION 24−63−00 Component Location ALL TASK 24−63−00−992−802 Junction Boxes−Component Location 101 JUNCTION BOX JB1 24−63−01 Removal/Installation ALL TASK 24−63−01−000−802 Removal of the Junction Box JB1 401 TASK 24−63−01−400−802 Installation of the Junction Box JB1 404 TASK 24−63−01−000−803 Removal of the Junction Box JB1 Circuit−Cards 406 TASK 24−63−01−400−803 Installation of the Junction Box JB1 Circuit−Cards 409 Adjustment/Test ALL TASK 24−63−01−710−805 Operational Test of Junction Box JB1 Card 1 501 TASK 24−63−01−710−806 Operational Test of Junction Box JB1 Card 2 503 TASK 24−63−01−710−807 Operational Test of Junction Box JB1 Card 3 505 TASK 24−63−01−710−808 Operational Test of Junction Box JB1 Card 4 507 TASK 24−63−01−710−809 Operational Test of Junction Box JB1 Card 5 508 TASK 24−63−01−720−801 Functional Test of Junction Box JB1 509 JUNCTION BOX JB1 TRAY 24−63−03 Removal/Installation ALL TASK 24−63−03−000−801 Removal of the Junction Box JB1 Tray 401 TASK 24−63−03−400−801 Installation of the Junction Box JB1 Tray 403 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − CONTENTS Page 11 Apr 01/2020 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL JUNCTION BOX JB2 24−63−05 Removal/Installation ALL TASK 24−63−05−000−802 Removal of the Junction Box JB2 Circuit−Cards 401 TASK 24−63−05−400−802 Installation of the Junction Box JB2 Circuit−Cards 404 TASK 24−63−05−000−803 Removal of the Junction Box JB2 407 TASK 24−63−05−400−803 Installation of the Junction Box JB2 410 Adjustment/Test ALL TASK 24−63−05−710−826 Operational Test of Junction Box JB2 Card 1 501 TASK 24−63−05−710−827 Operational Test of Junction Box JB2 Card 2 503 TASK 24−63−05−710−828 Operational Test of Junction Box JB2 Card 3 505 TASK 24−63−05−710−829 Operational Test of Junction Box JB2 Card 4 506 TASK 24−63−05−710−830 Operational Test of Junction Box JB2 Card 5 508 TASK 24−63−05−720−801 Functional Test of the Junction Box JB2 509 JUNCTION BOX JB2 TRAY 24−63−07 Removal/Installation ALL TASK 24−63−07−000−801 Removal of the Junction Box JB2 Tray 401 TASK 24−63−07−400−801 Installation of the Junction Box JB2 Tray 403 JUNCTION BOX JB3 24−63−09 Removal/Installation ALL TASK 24−63−09−000−802 Removal of the Junction Box JB3 401 TASK 24−63−09−400−802 Installation of the Junction Box JB3 404 TASK 24−63−09−000−803 Removal of the Junction Box JB3 Circuit−Cards 406 TASK 24−63−09−400−803 Installation of the Junction Box JB3 Circuit−Cards 409 Adjustment/Test ALL TASK 24−63−09−710−801 Operational Test of Junction Box JB3 Card 1 501 TASK 24−63−09−710−802 Operational Test of Junction Box JB3 Card 2 503 TASK 24−63−09−710−803 Operational Test of Junction Box JB3 Card 3 505 TASK 24−63−09−710−804 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − CONTENTS Page 12 Apr 01/2020 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL Operational Test of Junction Box JB3 Card 4 507 TASK 24−63−09−710−805 Operational Test of Junction Box JB3 Card 5 508 TASK 24−63−09−720−801 Functional Test of Junction Box JB3 510 JUNCTION BOX JB3 TRAY 24−63−11 Removal/Installation ALL TASK 24−63−11−000−801 Removal of the Junction Box JB3 Tray 401 TASK 24−63−11−400−801 Installation of the Junction Box JB3 Tray 403 JUNCTION BOX JB4 24−63−13 Removal/Installation ALL TASK 24−63−13−000−802 Removal of the Junction Box JB4 401 TASK 24−63−13−400−802 Installation of the Junction Box JB4 404 TASK 24−63−13−000−803 Removal of the Junction Box JB4 Circuit−Cards 406 TASK 24−63−13−400−803 Installation of the Junction Box JB4 Circuit−Cards 409 Adjustment/Test ALL TASK 24−63−13−710−801 Operational Test of Junction Box JB4 Card 1 501 TASK 24−63−13−710−802 Operational Test of Junction Box JB4 Card 2 503 TASK 24−63−13−710−803 Operational Test of Junction Box JB4 Card 3 504 TASK 24−63−13−710−804 Operational Test of Junction Box JB4 Card 4 505 TASK 24−63−13−710−805 Operational Test of Junction Box JB4 Card 5 506 TASK 24−63−13−720−801 Functional Test of Junction Box JB4 508 JUNCTION BOX JB4 TRAY 24−63−15 Removal/Installation ALL TASK 24−63−15−000−801 Removal of the Junction Box JB4 Tray 401 TASK 24−63−15−400−801 Installation of the Junction Box JB4 Tray 403 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − CONTENTS Page 13 Apr 01/2020 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL AUXILIARY DC POWER CENTER (AUX DCPC) SYSTEM 24−64−00 Component Location ALL TASK 24−64−00−992−801 Component Location 101 AUXILIARY DC POWER CENTER (AUX DCPC) 24−64−01 Removal/Installation ALL TASK 24−64−01−000−801 Removal of the Auxiliary DC Power Center (Aux DCPC) 401 TASK 24−64−01−400−801 Installation of the Auxiliary DC Power Center (Aux DCPC) 404 Adjustment/Test ALL TASK 24−64−01−710−801 Operational Test of the Auxiliary DC Power Center (Aux DCPC) 501 AUXILIARY DC POWER CENTER (AUX DCPC) FUSES 24−64−03 Removal/Installation ALL TASK 24−64−03−000−801 Removal of the Auxiliary DC Power Center (Aux DCPC) Fuses 401 TASK 24−64−03−400−801 Installation of the Auxiliary DC Power Center (Aux DCPC) Fuses 403 AUXILIARY DC POWER CENTER (AUX DCPC) RELAYS 24−64−04 Removal/Installation ALL TASK 24−64−04−000−801 Removal of the Auxiliary DC Power Center (AUX DCPC) Relays 401 TASK 24−64−04−400−801 Installation of the Auxiliary DC Power Center (AUX DCPC) Relays 404 AUXILIARY DC POWER CONTACTOR 24−64−05 Removal/Installation ALL TASK 24−64−05−000−801 Removal of the Auxiliary DC Power Contactor 401 TASK 24−64−05−400−801 Installation of the Auxiliary DC Power Contactor 404 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − CONTENTS Page 14 Apr 01/2020 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL AUXILIARY POWER START CONTACTOR 24−64−09 Removal/Installation ALL TASK 24−64−09−000−801 Removal of the Auxiliary Power Start Contactor 401 TASK 24−64−09−400−801 Installation of the Auxiliary Power Start Contactor 404 AUXILIARY POWER CENTER PRIMARY−LOGIC 24−64−13 Removal/Installation ALL TASK 24−64−13−000−801 Removal of the Auxiliary Power Center Primary−Logic 401 TASK 24−64−13−400−801 Installation of the Auxiliary Power Center Primary−Logic 403 AUXILIARY POWER UNIT SENSOR 24−64−17 Removal/Installation ALL TASK 24−64−17−000−801 Removal of the Auxiliary Power Unit Sensor 401 TASK 24−64−17−400−801 Installation of the Auxiliary Power Unit Sensor 404 DC CIRCUIT BREAKERS 24−65−00 Removal/Installation ALL TASK 24−65−00−960−801 Replacement of DC Circuit Breakers 401 Adjustment/Test ALL TASK 24−65−00−710−801 Operational Test of the DC Circuit Breakers 501 CIRCUIT BREAKER PANELS (LCBP/RCBP) 24−65−01 Maintenance Practices ALL TASK 24−65−01−010−801 Open the Left Circuit−Breaker−Panel (LCBP) 201 TASK 24−65−01−410−801 Close the Left Circuit−Breaker−Panel (LCBP) 204 TASK 24−65−01−010−802 Open the Right Circuit−Breaker−Panel (RCBP) 206 TASK 24−65−01−410−802 Close the Right Circuit−Breaker−Panel (RCBP) 210 Removal/Installation ALL TASK 24−65−01−000−801 Removal of the Cockpit Circuit−Breaker Panel (CCBP) 401 TASK 24−65−01−400−801 Installation of the Cockpit Circuit−Breaker Panel (CCBP) 406 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − CONTENTS Page 15 Apr 01/2020 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL SECONDARY−POWER−CENTER (SPC) CIRCUIT−BREAKER−PANELS 24−65−03 Maintenance Practices ALL TASK 24−65−03−010−801 Open the Left Secondary−Power−Center (LSPC) Circuit−Breaker−Panel 201 TASK 24−65−03−410−801 Close the Left Secondary−Power−Center (LSPC) Circuit−Breaker−Panel 204 TASK 24−65−03−010−802 Open the Right Secondary−Power−Center (RSPC) Circuit−Breaker−Panel 206 TASK 24−65−03−410−802 Close the Right Secondary−Power−Center (RSPC) Circuit−Breaker−Panel 208 DC POWER CENTER (DCPC) CIRCUIT−BREAKER−PANELS 24−65−05 Maintenance Practices ALL TASK 24−65−05−010−801 Open the Left DC Power Center (LDCPC) Circuit−Breaker−Panel 201 TASK 24−65−05−410−801 Close the Left DC Power Center (LDCPC) Circuit−Breaker−Panel 205 TASK 24−65−05−010−802 Open the Right DC Power Center (RDCPC) Circuit−Breaker−Panel 207 TASK 24−65−05−410−802 Close the Right DC Power Center (RDCPC) Circuit−Breaker−Panel 210 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II 24 − CONTENTS Page 16 Apr 01/2020 Subject Ch−Se−Su Effectivity Page EFFECTIVITY: ALL DC POWER CENTER (DCPC) - REMOVAL/INSTALLATION TASK 24−61−01−000−801 1. Removal of the DC Power Center (DCPC) A. Reference Information REFERENCE DESIGNATION TASK 24−00−00−910−801 Electrical/Electronic Safety Precautions TASK 24−00−00−910−802 Electrostatic−Discharge Safety Precautions TASK 24−32−00−040−801 Disconnect the Batteries TASK 52−41−00−010−801 Open the Aft Equipment−Compartment Door (182GL) B. Setup (1) Obey all the electrical/electronic safety precautions (TASK 24−00−00−910−801). (2) Obey all the electrostatic−discharge safety precautions (TASK 24−00−00−910−802). (3) Open the aft equipment compartment door (182GL) (TASK 52−41−00−010−801). (4) Disconnect the batteries (TASK 24−32−00−040−801). C. Procedure Refer to Figure 401. CAUTION: MAKE SURE THE DCPC THAT YOU REMOVED IS CORRECTLY PUT IN THE SHIPPING CONTAINER. USE THE SHIPPING CONTAINER AGAIN WITH ALL PROTECTIVE MATERIAL SUPPLIED WITH THE NEW DCPC. IF YOU DO NOT DO THIS, DAMAGE TO THE DCPC CAN OCCUR DURING SHIPMENT. (1) Remove the right dc power center A36 (19). (2) To remove the left dc power center (LDCPC) A35 (1), do the below steps. (3) Loosen the captive screws (37). BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II EFFECTIVITY: ALL 24−61−01 Page 401 Sep 22/2021 (4) Remove the four cover plates (38). NOTE: Do not use any air−powered tools when you remove the nuts (7), (10) and/or (14). If you use air−powered tools when you remove the nuts (7), (10) and/or (14), you can cause damage to the stud threads. (5) Remove the nuts (7), (10), and (14). (6) Remove the spring−washers (6), (9), and (13). (7) Remove the flat washers (5), (8), and (12). (8) Identify, remove, and tag all of the terminal lugs (11). (9) Disconnect the electrical connectors A35P5 (4), A35P4 (15), A35P3 (18), A35P2 (17), and A35P1 (16), from the LDCPC A35 (1). (10) Put protective covers on the connectors A35P5 (4), A35P4 (15), A35P3 (18), A35P2 (17), A35P1 (16) and the receptacles. (11) Hold the LDCPC A35 (1), and remove the screws (2), the washers (3) and the backplate (41) from the LDCPC A35 (1). (12) Remove the LDCPC A35 (1). (13) To remove the right dc power center (RDCPC) A36 (19), do the below steps. (14) Loosen the captive screws (39). (15) Remove the four cover plates (40). NOTE: Do not use any air−powered tools when you remove the nuts (24), (25) and/or (28). If you use air−powered tools when you remove the nuts (24), (25) and/or (28), you can cause damage to the stud threads. (16) Remove the nuts (24), (25), and (28). (17) Remove the spring−washers (23), (26), and (29). (18) Remove the flat washers (22), (27), and (30). (19) Identify, remove, and tag all of the terminal lugs (31). (20) Disconnect the electrical connectors A36P5 (32), A36P4 (33), A36P1 (34), A36P2 (35), and A36P3 (36) from the right dc power center A36 (19). (21) Put protective covers on the connectors A36P5 (32), A36P4 (33), A36P1 (34), A36P2 (35), A36P3 (36), and the receptacles. (22) Hold the RDCPC A36 (19) and remove the screws (21), the washers (20) and the backplate (41) from the RDCPC A36 (19). BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II EFFECTIVITY: ALL 24−61−01 Page 402 Sep 22/2021 A C FS669.76 BMM2461014_001 B A 4 1 14 11 12 13 6 7 8 9 10 2 3 38 37 38 37 5 41 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II DC Power Center (DCPC) − Removal/Installation Figure 401 (Sheet 1 of 4) EFFECTIVITY: ALL 24−61−01 Page 403 May 26/2014 BMM2461014_002 5 6 7 8 9 10 12 13 14 18 17 16 15 37 38 37 38 41 B BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II DC Power Center (DCPC) − Removal/Installation Figure 401 (Sheet 2 of 4) EFFECTIVITY: ALL 24−61−01 Page 404 May 26/2014 BMM2461014_003 D 19 21 22 23 24 25 26 27 28 29 30 32 20 31 40 39 39 41 C BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II DC Power Center (DCPC) − Removal/Installation Figure 401 (Sheet 3 of 4) EFFECTIVITY: ALL 24−61−01 Page 405 May 26/2014 BMM2461014_004 22 23 24 25 26 27 40 39 39 40 36 35 34 33 41 D BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II DC Power Center (DCPC) − Removal/Installation Figure 401 (Sheet 4 of 4) EFFECTIVITY: ALL 24−61−01 Page 406 May 26/2014 TASK 24−61−01−400−801 2. Installation of the DC Power Center (DCPC) A. Reference Information REFERENCE DESIGNATION TASK 24−32−00−440−801 Connect the Batteries TASK 24−61−01−720−801 Functional Test of the DC Power Center (DCPC) TASK 52−41−00−410−801 Close the Aft Equipment−Compartment Door (182GL) SPM−MM 20−21−00−910−801 Torquing of Threaded Fasteners SPM−MM 51−80−00−760−801 Electrical Bonding Test B. Tools and Equipment REFERENCE DESIGNATION Commercially Available Wrench, Torque 2.21 lbf in (0.25 Nm) Commercially Available Wrench, Torque 20 to 25 lbf in (2.26 to 2.82 Nm) Commercially Available Wrench, Torque 33.80 to 41.58 lbf in (3.82 to 4.70 Nm) Commercially Available Wrench, Torque 60.69 to 80.69 lbf in (6.86 to 9.12 Nm) Commercially Available Wrench, Torque 98.47 to 134.49 lbf in (11.13 to 15.20 Nm) NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. C. Parts REFERENCE NAME OF PART QUANTITY IPC SEQUENCE NO. 1 Power Center, Left DC 1 24−61−01−01−005 2 Screw 6 24−61−01−01−070 3 Washer 6 24−61−01−01−075 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II EFFECTIVITY: ALL 24−61−01 Page 407 Jun 12/2018 5 Washer, Flat 4 24−61−01−01−025 6 Washer, Spring 4 24−61−01−01−023 7 Nut 4 24−61−01−01−022 8 Washer, Flat 3 24−61−01−01−055 9 Washer, Spring 3 24−61−01−01−050 10 Nut 3 24−61−01−01−045 12 Washer, Flat 7 24−61−01−01−040 13 Washer, Spring 7 24−61−01−01−035 14 Nut 7 24−61−01−01−030 19 Power Center, Right DC 1 24−61−01−02−005 20 Washer 6 24−61−01−02−075 21 Screw 6 24−61−01−02−070 22 Washer, Flat 4 24−61−01−02−025 23 Washer, Spring 4 24−61−01−02−020 24 Nut 4 24−61−01−02−022 25 Nut 6 24−61−01−02−030 26 Washer, Spring 6 24−61−01−02−035 27 Washer, Flat 6 24−61−01−02−040 28 Nut 2 24−61−01−02−045 29 Washer, Spring 2 24−61−01−02−050 30 Washer, Flat 2 24−61−01−02−055 38 Plate, Cover 4 24−61−01−01−146 39 Screws, Captive 16 24−61−01−01−137 40 Plate, Cover 4 24−61−01−01−136 41 Backplate 2 24−61−01−01−065 24−61−01−02−065 BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II EFFECTIVITY: ALL 24−61−01 Page 408 Jun 12/2018 D. Setup (1) Make sure that the aircraft is in the same configuration as in the removal task. E. Procedure Refer to Figure 401. (1) To install the left dc power center (LDCPC) A35 (1), do the below steps. NOTE: Make sure that the mating surfaces are clean with no corrosion, paint, grease, or preservation fluids. (2) Put the backplate (41) and the LDCPC A35 (1) in position. NOTE: Make sure that the formed−in beads of the backplate are installed facing towards the mounting structure. (3) Install the screws (2) and the washers (3). (4) Torque the screws (2) from 20 to 25 lbf in (2.26 to 2.82 Nm) (SPM−MM 20−21−00−910−801). (5) Remove the protective covers A35P5 (4), A35P4 (15), A35P3 (18), A35P2 (17), and A35P1 (16) from the connectors and the receptacles. CAUTION: DO NOT USE TOO MUCH FORCE WHEN YOU CONNECT THE ELECTRICAL CONNECTORS. IF THE ELECTRICAL CONNECTORS DO NOT ENGAGE EASILY, EXAMINE THE CONNECTORS AND PINS FOR DAMAGE. DAMAGED CONNECTORS CAN CAUSE EQUIPMENT AND/OR SYSTEMS TO OPERATE INCORRECTLY. (6) Connect the electrical connectors A35P5 (4), A35P4 (15), A35P3 (18), A35P2 (17), and A35P1 (16) to the LDCPC A35 (1). NOTE: Make sure that all cable lugs, terminal posts and hardware are free of oxidation/corrosion. Clean all cable lugs, terminal posts and hardware as necessary, refer to best shop practices. If you do not clean the cable lugs, terminal posts and hardware, the cable conductivity will decrease and cause generator failure intermittently, when the generator operates during heavy current load outputs. (7) Install all of the terminal lugs (11) on the LDCPC A35 (1). (8) Install the flat−washers (5), (8), and (12). (9) Install the spring−washers (6), (9), and (13). NOTE: Do not use any air−powered tools when you install the nuts (7), (10) and/or (14). If you use air−powered tools when you install the nuts (7), (10) and/or (14), you can cause damage to the stud threads. BD−100 AIRCRAFT MAINTENANCE MANUAL − PART II EFFECTIVITY: ALL 24−61−01 Page 409 Jul 01/2020