Airworthiness Directive · Amendment 39-22965 · Fire protection
Airbus SAS Airplanes
This AD applies to Airbus SAS Model A330-201, -202, -203, -223, -223F, -243, -243F, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0119, dated June 27, 2024 (EASA AD 2024-0119).
The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A330-200, A330-200 Freighter, and A330-300 series airplanes. This AD was prompted by a report of contamination of the advanced pneumatic detector pressure switch of engine pylon fire detectors. This AD requires require replacement of the affected parts and prohibits installation of affected parts, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
Except as specified in paragraphs (h) and (i) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA AD 2024-0119.
(1) Where EASA AD 2024-0119 refers to its effective date, this AD requires using the effective date of this AD.
(2) Where paragraph (1) of the EASA AD 2024-0119 states to “replace each affected part with a serviceable part in accordance with the instructions of the SB” this AD requires replacing that text with “replace each affected part with a serviceable part in accordance with the applicable tasks for removal and installation of the affected parts as specified in the accomplishment instructions of the SB.”
(3) Where EASA AD 2024-0119 defines a serviceable part as “Engine pylon fire detector, eligible for installation in accordance with Airbus instructions, which is not an affected part” for this AD replace that text with “Engine pylon fire detector, eligible for installation that is not an affected part.”
(4) This AD does not adopt the “Remarks” section of EASA AD 2024-0119.
Although the material referenced in EASA AD 2024-0119 specifies to send affected pylon fire detectors to Kidde Technologies Inc., this AD does not include that requirement.
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, AIR-520, Continued Operational Safety 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 AIR-520, Continued Operational Safety Branch, send it to the attention of the person identified in paragraph (k) of this AD and email to: AMOC@faa.gov. 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, AIR-520, Continued Operational Safety Branch, FAA; or EASA; or Airbus SAS's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature.
(3) Required for Compliance (RC): Except as required by paragraphs (i) and (j)(2) of this AD, if any material 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.
For more information about this AD, contact Vladimir Ulyanov, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 206-231-3229; email vladimir.ulyanov@faa.gov.
