Airworthiness Directive · Amendment 39-21279 · Time limits/maintenance checks
Airbus SAS Airplanes
Superseded. A later AD replaced this one: AD 2022-09-03. Comply with the one in force.
This AD applies to Airbus SAS Model A350-941 and -1041 airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before June 7, 2019.
The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A350-941 and -1041 airplanes. This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. This AD requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations, 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 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 2020-0091, dated April 22, 2020 (“EASA AD 2020-0091”).
(1) The requirements specified in paragraph (1) of EASA AD 2020-0091 do not apply to this AD.
(2) Paragraph (2) of EASA AD 2020-0091 specifies revising “the approved AMP” within 12 months after its effective date, but this AD requires revising the existing maintenance or inspection program, as applicable, to incorporate the “limitations” specified in paragraph (2) of EASA 2020-0091 within 90 days after the effective date of this AD.
(3) The initial compliance time for complying with the limitations specified in paragraph (2) of EASA AD 2020-0091 is at the applicable “limitations” specified in paragraph (2) of EASA AD 2020-0091, or within 90 days after the effective date of this AD, whichever occurs later.
(4) The provisions specified in paragraphs (3) and (4) of EASA AD 2020-0091 do not apply to this AD.
(5) The “Remarks” section of EASA AD 2020-0091 does not apply to this AD.
After the existing maintenance or inspection program has been revised as required by paragraph (g) of this AD, no alternative actions (e.g., inspections) and intervals are allowed unless they are approved as specified in the provisions of the “Ref. Publications” section of EASA AD 2020-0091.
The aircraft, engines and makers this AD names, by the model designations in its text. A model listed here may still be outside the AD's serial ranges.
Aircraft
