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2024-10-03: Flight Controls

FAA order 2024-10-03 is an airworthiness directive in force since June 28, 2024. The FAA's subject line: Flight Controls. 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: flight controls.

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
June 28, 2024
Published
May 24, 2024 (signed May 8, 2024)
Docket
FAA-2023-1997
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 all Airbus Canada Limited Partnership Model BD-500-1A10 and BD-500-1A11 airplanes. This AD was prompted by the determination that reliance on design assurance level (DAL) D software for flight-critical fly-by-wire (FBW) rigging functions may result in undetected inaccurate positioning of the primary flight control surfaces. This AD requires the use of specific issues of the aircraft maintenance publication (AMP) for electrical rigging procedures, and an electrical rigging confirmation check of primary flight control surfaces for certain airplanes, 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 (5,303 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: 2024-10-03 Airbus Canada Limited Partnership (Type Certificate Previously Held by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.): Amendment 39-22748; Docket No. FAA-2023-1997; Project Identifier MCAI-2023-00383-T. (a) Effective Date This airworthiness directive (AD) is effective June 28, 2024. (b) Affected ADs None. (c) Applicability This AD applies to all Airbus Canada Limited Partnership Model BD-500-1A10 and BD-500-1A11 airplanes, certified in any category. (d) Subject Air Transport Association (ATA) of America Code 27, Flight Controls. (e) Unsafe Condition It is possible that the surface travel checks were not done after the electrical rigging of the ailerons, the elevators, and the rudder. If this occurs, it is possible that the ailerons, the elevators, and the rudder will not be able to reach their maximum travel or return to their neutral position. The FAA is issuing this AD to ensure accurate rigging of the aircraft primary flight control surfaces by adding physical travel and centering checks of primary flight control surfaces. The unsafe condition, if not addressed, could result in undetected inaccurate positioning of the primary flight control surfaces, which in combination with an additional failure or extreme maneuvers, can lead to runway excursion or structure ultimate load exceedance. (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-2023-15, dated March 2, 2023 (Transport Canada AD CF-2023-15). (h) Exceptions to Transport Canada AD CF-2023-15 (1) Where Transport Canada AD CF-2023-15 refers to its effective date, this AD requires using the effective date of this AD. (2) Where Transport Canada AD CF-2023-15 refers to hours air time, this AD requires replacing those words with flight hours. (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 International Validation Branch, send it to the attention of the person identified in paragraph (j)(1) 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 Airbus Canada Limited Partnership's Transport Canada Design Approval Organization (DAO). If approved by the DAO, the approval must include the DAO-authorized signature. (j) Additional Information (1) For more information about this AD, contact William Reisenauer, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: 516-228-7300; email: [email protected]. (2) For Airbus Canada Limited Partnership service information identified in this AD that is not incorporated by reference, contact Airbus Canada Limited Partnership, 13100 Henri-Fabre Boulevard, Mirabel, Québec J7N 3C6, Canada; telephone 450-476-7676; email [email protected]; website a220world.airbus.com. (k) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise. (i) Transport Canada AD CF-2023-15 dated March 2, 2023. (ii) [Reserved] (3) For Transport Canada AD CF-2023-15, contact Transport Canada, Transport Canada National Aircraft Certification, 159 Cleopatra Drive, Nepean, Ontario K1A 0N5, Canada; telephone 888-663-3639; email [email protected]; website 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/ibr-locations.html, or email [email protected]. Issued on May 8, 2024. James D. Foltz, Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2024-11410 Filed 5-23-24; 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/2024-10-03.json · aircraft systems.