Airworthiness Directive 2024-16-02

recurring
Official AD 2024-16-02 · FR doc 2024-20835 · 2024-09-16 · airframe

Airworthiness Directives; Airbus SAS Airplanes

What this AD requires

The FAA is superseding Airworthiness Directive (AD) 2018-01- 07, AD 2018-19-33, AD 2019-21-01, AD 2021-26-20, AD 2022-13-09, AD 2022-14-06, AD 2023-09-05, and AD 2023-26-06, which applied to all Airbus SAS Model A300 B4-600, B4-600R, and F4-600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called Model A300-600 series airplanes); and AD 2020-23-11, which applied to all Airbus SAS Model A300 and A300-600 series airplanes. AD 2018-01-07, AD 2018-19-33, AD 2019-21-01, AD 2021-26-20, AD 2022-13-09, AD 2022-14-06, AD 2023-09-05, and AD 2023-26-06 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. AD 2020-23-11 required repetitive inspections for discrepancies of certain areas in and around the fuselage and repair if necessary. This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. This AD continues to require certain actions specified in the superseded ADs, and requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations; as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, which is incorporated by reference. This AD also removes the Model A300 series airplanes from the applicability. The FAA is issuing this AD to address the unsafe condition on these products.

Repetitive inspection. Re-inspect every 12 months. The next-due date/hours depend on this aircraft’s time in service — a records report computes it from the logbooks.

Which aircraft AD 2024-16-02 applies to

MakesAirbus
ModelsA300 B4-601, A300 B4-603, A300 B4-620, A300 B4-622, A300 B4-605R, A300 B4-622R, A300 C4-605R Variant F, A300 F4-605R, A300 F4-622R, A300

Whether AD 2024-16-02 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2024-16-02 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.