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Airworthiness directives › 2023-05-08

AD 2023-05-08 Airworthiness Directives; Airbus Canada Limited Partnership (Type Certificate Previously Held by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.) Airplanes

Superseded. This directive was replaced by AD 2024-22-01. Work to the current one.
2023-05-12
2023-04-07
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Airframe
2024-22-01

Models named: BD-500-1A10, BD-500-1A11. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Airbus Canada Limited Partnership airplanes, certificated in any category, as identified in paragraphs (c)(1) and (2) of this AD. (1) Model BD-500-1A10 airplanes, serial numbers 50001 and subsequent with an original airworthiness certificate or original export certificate of airworthiness issued on or before February 3, 2022. (2) Model BD-500-1A11 airplanes, serial numbers 55001 and subsequent with an original airworthiness certificate or original export certificate of airworthiness issued on or before February 3, 2022.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

This paragraph restates the requirements of paragraph (g) of AD 2021-04-05, with a new terminating action. For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or before June 18, 2020: Within 90 days after March 30, 2021 (the effective date of AD 2021-04-05), revise the existing maintenance or inspection program, as applicable, to incorporate the information specified in Airbus Canada Limited Partnership A220 Airworthiness Limitations, BD500-3AB48-11400-02, Issue 011.00, dated June 18, 2020. The initial compliance time for doing the tasks is at the time specified in Airbus Canada Limited Partnership A220 Airworthiness Limitations, BD500-3AB48-11400-02, Issue 011.00, dated June 18, 2020, or within 90 days after March 30, 2021, whichever occurs later. Accomplishing the revision of the existing maintenance or inspection program required by paragraph (i) of this AD terminates the requirements of this paragraph for Sections 01, “Airworthiness limitations—Introduction;” 02, “Certification maintenance requirements—General;” 04, “ALI structural inspections—General;” 05, “Life limited parts (systems)—General;” 06, “Life limited parts (structures)—General;” 07, “Fuel system limitations—General;” 08, “Critical design configuration control limitations—General;” 09, “Power plant limitations—General;” 10, “Structural repair limitations—General;” and 11, “Limit of validity—General;” of Airbus Canada Limited Partnership A220 Airworthiness Limitations, BD500-3AB48-11400-02, Issue 011.00, dated June 18, 2020, only.

Unsafe condition

This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. The FAA is issuing this AD to address reduced structural integrity of the airplane or reduced controllability of the airplane.

Affected ADs

This AD replaces AD 2021-04-05, Amendment 39-21426 (86 FR 10799, February 23, 2021) (AD 2021-04-05).

Read the original on the Federal Register →

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1