Is AD 2019-15-08 a recurring Airworthiness Directive?

Yes — AD 2019-15-08 requires a repetitive inspection. Next-due depends on the aircraft's time in service.

Which aircraft does AD 2019-15-08 apply to?

AD 2019-15-08 applies to Airbus Sas — models A300 C4-605R Variant F, A300. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2019-15-08

recurring

Official AD 2019-15-08 · FR doc 2019-17503 · 2019-08-15 · airframe

Airworthiness Directives; Airbus SAS Airplanes

What this AD requires

The FAA is superseding Airworthiness Directive (AD) 2002-07- 05, which applied to all Airbus Model A300 B2, A300 B4, A300 B4-600, and A300 B4-600R series airplanes, and Model A300 F4-605R airplanes. AD 2002-07-05 required repetitive inspections for cracking of certain fittings, corrective action if necessary, and, for certain airplanes, a modification. This AD requires repetitive inspections for cracking of certain fittings, corrective actions if necessary, and, for certain airplanes, a modification; as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. This AD was prompted by a determination that, for certain airplanes, the existing inspection compliance times were not sufficient to address the unsafe condition and needed to be reduced. The FAA is issuing this AD to address the unsafe condition on these products.

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

Which aircraft AD 2019-15-08 applies to

MakesAirbus Sas

ModelsA300 C4-605R Variant F, A300

Source excerpt is fragmentary (preamble/background text, not the full applicability paragraph). It indicates this AD (a revision related to AD 2002-07-05) added Model A300 C4-605R Variant F airplanes to the applicability, since those airplanes were not on the U.S. type certificate data sheet when AD 2002-07-05 was issued. Full applicability list not captured in the available text; see EASA AD 2019-0011R1.

Whether AD 2019-15-08 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 compliance — The specific action taken (inspected, replaced, modified) and to what revision.

Date — When the work was done.

Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.

Signature & certificate — The A&P/IA who returned it to service, with certificate number.

Is AD 2019-15-08 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.