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2024-24-08: Equipment/Furnishings

FAA order 2024-24-08 is an airworthiness directive in force since January 13, 2025. The FAA's subject line: Equipment/Furnishings. It names Airbus Canada Ltd Ptnrsp BD-500, Airbus BD-500: about 218 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: cabin, seats and restraints.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Airbus Canada Limited Partnership
Models
BD-500-1A10, BD-500-1A11
On this site
Airbus Canada Ltd Ptnrsp BD-500 31 registered
Airbus BD-500 187 registered

Dates and paperwork

In force since
January 13, 2025
Published
December 9, 2024 (signed November 22, 2024)
Docket
FAA-2024-0468
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is adopting a new airworthiness directive (AD) for certain Airbus Canada Limited Partnership Model BD-500-1A10 and BD-500- 1A11 airplanes. This AD was prompted by multiple occurrences of pilot and co-pilot seats locking in a fore-aft position due to the seat fore- aft adjustment mechanism disconnecting, caused by a broken cotter pin in the seat base egress linkage. This AD requires modifying the pilot and co-pilot seats by replacing the hardware of the seat base egress linkage, as specified in a Transport Canada AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (6,222 characters)
1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. 2. The FAA amends § 39.13 by adding the following new airworthiness directive: 2024-24-08 Airbus Canada Limited Partnership (Type Certificate Previously Held by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.): Amendment 39-22898; Docket No. FAA-2024-0468; Project Identifier MCAI-2023-00762-T. (a) Effective Date This airworthiness directive (AD) is effective January 13, 2025. (b) Affected ADs None. (c) Applicability This AD applies to Airbus Canada Limited Partnership (Type Certificate previously held by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.) Model BD-500-1A10 and BD-500-1A11 airplanes, certificated in any category, as identified in Transport Canada AD CF-2023-40, dated June 13, 2023 (Transport Canada AD CF-2023-40). (d) Subject Air Transport Association (ATA) of America Code 25, Equipment/Furnishings. (e) Unsafe Condition This AD was prompted by multiple occurrences of pilot and co-pilot seats locking in a fore-aft position due to the seat fore-aft adjustment mechanism disconnecting. The FAA is issuing this AD to address the disconnection of the seat fore-aft adjustment mechanism caused by a broken cotter pin in the seat base egress linkage. The unsafe condition, if not addressed, could result in a significant increase in crew workload for continued safe flight and landing. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Requirements Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, Transport Canada AD CF-2023-40. (h) Exceptions to Transport Canada AD CF-2023-40 (1) Where Transport Canada AD CF-2023-40 refers to its effective date, this AD requires using the effective date of this AD. (2) Where Transport Canada AD CF-2023-40 refers to "hours air time," this AD requires using flight hours. (3) Where the service information referenced in Transport Canada AD CF-2023-40 specifies to "Do Goodrich Interiors Service Bulletin 1430-25-003," this AD requires replacing that text with "Do Goodrich Interiors Service Bulletin 1430-25-003, Revision C, dated November 22, 2022." (4) Where the service information specified in Transport Canada AD CF-2023-40 specifies removal and installation steps in accordance with both Airbus Canada Limited Partnership Service Bulletin BD500-251006 and Goodrich Interiors Service Bulletin 1430-25-003, this AD does not require the removal/installation steps in Goodrich Interiors Service Bulletin 1430-25-003. (i) Additional AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Validation Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or responsible Flight Standards Office, as appropriate. If sending information directly to the manager of the International Validation Branch, mail it to the address identified in paragraph (j) of this AD. Information may be emailed to [email protected]. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office. (2) Contacting the Manufacturer: For any requirement in this AD to obtain instructions from a manufacturer, the instructions must be accomplished using a method approved by the Manager, International Validation Branch, FAA; or Transport Canada; or Transport Canada Design Approval Organization (DAO). If approved by the DAO, the approval must include the DAO-authorized signature. (3) Required for Compliance (RC): Except as required by paragraph (i)(2) of this AD, if any service information contains procedures or tests that are identified as RC, those procedures and tests must be done to comply with this AD; any procedures or tests that are not identified as RC are recommended. Those procedures and tests that are not identified as RC may be deviated from using accepted methods in accordance with the operator's maintenance or inspection program without obtaining approval of an AMOC, provided the procedures and tests identified as RC can be done and the airplane can be put back in an airworthy condition. Any substitutions or changes to procedures or tests identified as RC require approval of an AMOC. (j) Additional Information For more information about this AD, contact Fatin Saumik, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone 516-228-7300; email [email protected]. (k) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the material listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this material as applicable to do the actions required by this AD, unless this AD specifies otherwise. (i) Transport Canada AD CF-2023-40, dated June 13, 2023. (ii) [Reserved] (3) For Transport Canada AD CF-2023-40 identified in this AD, contact Transport Canada, Transport Canada National Aircraft Certification, 159 Cleopatra Drive, Nepean, Ontario K1A 0N5, Canada; telephone 888-663-3639; email [email protected]. You may find this Transport Canada AD on the Transport Canada website at tc.canada.ca/en/aviation. (4) You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. (5) You may view this material at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, visit www.archives.gov/federal-register/cfr/[email protected]. Issued on November 22, 2024. Peter A. White, Deputy Director, Integrated Certificate Management Division, Aircraft Certification Service. [FR Doc. 2024-28785 Filed 12-6-24; 8:45 am]BILLING CODE 4910-13-P

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Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 6, 2026. Connections as data: /graph/directive/2024-24-08.json · aircraft systems.