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FAA orders · airworthiness directive · historical

2023-11-08: Pneumatic, Air

FAA order 2023-11-08 is an airworthiness directive in force since July 18, 2023. The FAA's subject line: Pneumatic, Air. It names Airbus A330: about 153 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Airbus SAS
Models
A330-841, A330-941
On this site
Airbus A330 153 registered

Dates and paperwork

In force since
July 18, 2023
Published
June 13, 2023 (signed June 2, 2023)
Docket
FAA-2023-0156
Replaces
2022-19-05
Replaced by
2025-04-05
Status
Historical
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is superseding Airworthiness Directive (AD) 2022-19- 05, which applied to all Airbus SAS Model A330-841 and -941 airplanes. AD 2022-19-05 required maintenance actions, including a high pressure valve (HPV) seal integrity test, repetitive replacement of the HPV clips, revision of the existing airplane flight manual (AFM), and implementation of updates to the FAA-approved operator's minimum equipment list (MEL). This AD was prompted by additional instructions and maintenance procedures developed to address failures of the HPV. This AD continues to require certain actions in AD 2022-19-05 and provides additional criteria for the installation of HPV and HPV clips, 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.

The order itself the regulatory text, as published

Show the full text (6,440 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: a. Removing Airworthiness Directive 2022-19-05, Amendment 39-22174 (87 FR 54870, dated September 8, 2022); and b. Adding the following new AD: 2023-11-08 Airbus SAS: Amendment 39-22454; Docket No. FAA-2023-0156; Project Identifier MCAI-2022-01511-T. (a) Effective Date This airworthiness directive (AD) is effective July 18, 2023. (b) Affected ADs This AD replaces AD 2022-19-05, Amendment 39-22174 (87 FR 54870, September 8, 2022) (AD 2022-19-05). (c) Applicability This AD applies to all Airbus SAS Model A330-841 and -941 airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code: 36, Pneumatic; 75, Air. (e) Unsafe Condition This AD was prompted by reports of leaking bleed system high pressure valves (HPVs), likely due to HPV clip failure and sealing ring damage, and by the development of additional instructions and maintenance procedures to address HPV failures. The FAA is issuing this AD to address a leaking HPV, which may expose the pressure regulating valve (PRV), which is installed downstream from the HPV, to high pressure, possibly damaging the PRV itself and preventing its closure. The unsafe condition, if not addressed, could result in high pressure and temperatures in the duct downstream from the PRV, with possible duct burst, damage to several systems, and consequent loss of control of the airplane. (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, European Union Aviation Safety Agency (EASA) AD 2022-0227, dated November 24, 2022 (EASA AD 2022-0227). (h) Exceptions to EASA AD 2022-0227 (1) Where EASA AD 2022-0227 refers to "05 September 2022 [the effective date of EASA AD 2022-0181]," this AD requires using September 15, 2022 (the effective date of AD 2022-19-05). (2) Where EASA AD 2022-0227 refers to its effective date, this AD requires using the effective date of this AD. (3) Where paragraphs (1) and (4) of EASA AD 2022-0227 specify to inform all flightcrews of airplane flight manual (AFM) revisions and dispatch limitations, and thereafter to operate the airplane accordingly, this AD does not require those actions, as those actions are already required by existing FAA regulations (see 14 CFR 91.9, 91.505, and 121.137). (4) This AD does not adopt the reporting requirements of paragraph (17) of EASA AD 2022-0227. (5) This AD does not adopt the "Remarks" section of EASA AD 2022-0227. (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) of this AD. Information may be emailed to: [email protected]. (i) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office. (ii) AMOCs approved previously for AD 2022-19-05 are approved as AMOCs for the corresponding provisions of EASA AD 2022-0227 that are required by paragraph (g) of this AD. (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 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 paragraph(s) (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 Vladimir Ulyanov, Aviation Safety Engineer, FAA, International Validation Branch, 2200 South 216th Street, Des Moines, WA 98198; telephone 206-231-3229; email [email protected]. (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) European Union Aviation Safety Agency (EASA) AD 2022-0227, dated November 24, 2022. (ii) [Reserved] (3) For EASA AD 2022-0227, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email: [email protected]; website: easa.europa.eu. You may find this EASA AD on the EASA website: ad.easa.europa.eu. (4) You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th Street, Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. (5) You may view this material that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, email [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html. Issued on June 2, 2023. Michael Linegang, Acting Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2023-12441 Filed 6-12-23; 8:45 am]BILLING CODE 4910-13-P

Related safety bulletins advice on the same designs, not orders

2017-07-19NM-17-20 · Equipment/Furnishings
2009-06-01NM-09-33 · Flight Control Primary Computer (FCPC)
2008-12-11NM-09-03 · Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations
2008-09-03NM-08-43 · Cabin Equipment/Furnishings - Seats
2008-07-02NM-08-31 · Equipment/Furnishings: Non-Textile Floors

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 3, 2026. Connections as data: /graph/directive/2023-11-08.json · aircraft systems.