Airworthiness Directive · Amendment 39-22589 · Time limits/maintenance checks
Dassault Aviation Airplanes
Superseded. A later AD replaced this one: AD 2026-09-10. Comply with the one in force.
This AD applies to Dassault Aviation airplanes specified in paragraphs (c)(1) and (2) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2023-0060, dated March 16, 2023 (EASA AD 2023-0060).
(1) Model FAN JET FALCON airplanes.
(2) Model FAN JET FALCON SERIES C, D, E, F, and G airplanes.
The FAA is superseding Airworthiness Directive (AD) 2020-23- 10, which applied to certain Dassault Aviation Model FAN JET FALCON and FAN JET FALCON SERIES C, D, E, F, and G airplanes. AD 2020-23-10 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. This AD continues to require the actions in AD 2020-23-10 and requires revising the existing maintenance or inspection program, as applicable, to incorporate additional 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.
This paragraph restates the requirements of paragraph (i) of AD 2020-23-10, with a new terminating action. Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA AD 2019-0141, dated June 17, 2019 (EASA AD 2019-0141). Accomplishing the revision of the existing maintenance or inspection program required by paragraph (j) of this AD terminates the requirements of this paragraph.
This paragraph restates the exceptions specified in paragraph (j) of AD 2020-23-10, with no changes.
(1) The requirements specified in paragraphs (1), (2), (4), and (5) of EASA AD 2019-0141 do not apply to this AD.
(2) Paragraph (3) of EASA AD 2019-0141 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, tasks and associated thresholds and intervals” specified in paragraph (3) of EASA AD 2019-0141 within 90 days after December 23, 2020 (the effective date of AD 2020-23-10).
(3) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2019-0141 is at the applicable “associated thresholds” specified in paragraph (3) of EASA AD 2019-0141, or within 90 days after December 23, 2020 (the effective date of AD 2020-23-10), whichever occurs later.
(4) The “Remarks” section of EASA AD 2019-0141 does not apply to this AD.
This paragraph restates the requirements of paragraph (k) of AD 2020-23-10, with a new exception. Except as required by paragraph (j) of this AD, after the maintenance or inspection program has been revised as required by paragraph (g) of this AD, no alternative actions (e.g., inspections) or intervals are allowed except as specified in the provisions of the “Ref. Publications” section of EASA AD 2019-0141.
Except as specified in paragraph (k) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA AD 2023-0060. Accomplishing the revision of the existing maintenance or inspection program required by this paragraph terminates the requirements of paragraph (g) of this AD.
(1) This AD does not adopt the requirements specified in paragraphs (1) and (2) of EASA AD 2023-0060.
(2) Paragraph (3) of EASA AD 2023-0060 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, within 90 days after the effective date of this AD.
(3) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2023-0060 is at the applicable “limitations” and “associated thresholds” as incorporated by the requirements of paragraph (3) of EASA AD 2023-0060, or within 90 days after the effective date of this AD, whichever occurs later.
(4) This AD does not adopt the provisions specified in paragraphs (4) and (5) of EASA AD 2023-0060.
(5) This AD does not adopt the “Remarks” section of EASA AD 2023-0060.
After the existing maintenance or inspection program has been revised as required by paragraph (j) 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 2023-0060.
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 (n) of this AD. Information may be emailed to: 9-AVS-AIR-730-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, International Validation Branch, FAA; or EASA; or Dassault Aviation's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature.
For more information about this AD, contact Tom Rodriguez, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone: 206-231-3226; email: tom.rodriguez@faa.gov.
