Airworthiness Directive · Amendment 39-21863 · Time limits/maintenance checks
Saab AB, Support and Services (Formerly Known as Saab AB, Saab Aeronautics) Airplanes
Superseded. A later AD replaced this one: AD 2024-15-12. Comply with the one in force.
This AD applies to all Saab AB, Support and Services Model SAAB 2000 airplanes, certificated in any category.
The FAA is superseding Airworthiness Directive (AD) 2020-07- 17, which applied to all Saab AB, Support and Services Model SAAB 2000 airplanes. AD 2020-07-17 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. Since the FAA issued AD 2020-07- 17, it has determined that new or more restrictive airworthiness limitations are necessary. This AD retains the requirements of AD 2020- 07-17 and 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. The FAA is issuing this AD to address the unsafe condition on these products.
This paragraph restates the requirements of paragraph (g) of AD 2020-07-17, with no changes. 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 2019-0263, dated October 22, 2019 (EASA AD 2019-0263). Accomplishing the maintenance or inspection program revision required by paragraph (j) of this AD terminates the requirements of this paragraph.
This paragraph restates the requirements of paragraph (h) of AD 2020-07-17, with revised exceptions.
(1) The requirements specified in paragraphs (1) and (2) of EASA AD 2019-0263 do not apply to this AD.
(2) Paragraph (3) of EASA AD 2019-0263 specifies revising “the approved AMP [aircraft maintenance program]” 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 2019-0263 within 90 days after May 26, 2020 (the effective date of AD 2020-07-17).
(3) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2019-0263 is at the applicable “associated thresholds” specified in paragraph (3) of EASA AD 2019-0263, or within 90 days after May 26, 2020 (the effective date of AD 2020-07-17), whichever occurs later.
(4) The provisions specified in paragraphs (4) and (5) of EASA AD 2019-0263 do not apply to this AD.
(5) The “Remarks” section of EASA AD 2019-0263 does not apply to this AD.
This paragraph restates the requirements of paragraph (i) of AD 2020-07-17, 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), intervals, and CDCCLs are allowed unless they are approved as specified in the provisions of the “Ref. Publications” section of EASA AD 2019-0263.
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 2021-0132, dated May 25, 2021 (EASA AD 2021-0132). Accomplishing the maintenance or inspection program revision required by this paragraph terminates the requirements of paragraph (g) of this AD.
(1) The requirements specified in paragraphs (1) and (2) of EASA AD 2021-0132 do not apply to this AD.
(2) Paragraph (3) of EASA AD 2021-0132 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 2021-0132 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 2021-0132 is at the applicable “associated thresholds” specified in paragraph (3) of EASA AD 2021-0132, or within 90 days after the effective date of this AD, whichever occurs later.
(4) The provisions specified in paragraphs (4) and (5) of EASA AD 2021-0132 do not apply to this AD.
(5) The “Remarks” section of EASA AD 2021-0132 does not apply to this AD.
After the maintenance or inspection program has been revised as required by paragraph (j) of this AD, no alternative actions (e.g., inspections), intervals, and CDCCLs are allowed unless they are approved as specified in the provisions of the “Ref. Publications” section of EASA AD 2021-0132.
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, Large Aircraft Section, 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 Large Aircraft Section, 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, Large Aircraft Section, International Validation Branch, FAA; or EASA; or Saab AB, Support and Services' (Formerly Known as Saab AB, Saab Aeronautics) EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature.
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
