Is AD 2012-01-05 a recurring Airworthiness Directive?

Yes — AD 2012-01-05 requires a repetitive inspection every 16 months. Next-due depends on the aircraft's time in service.

Airworthiness Directive 2012-01-05

Q: Which aircraft does AD 2012-01-05 apply to?

AD 2012-01-05 applies to Airbus — models A300 B2-1C, A300 B2K-3C, A300 B2-203, A300 B4-2C, A300 B4-103, A300 B4-203, A300 B4-601, A300 B4-603. Serial/part conditions may narrow it to specific aircraft.

recurring

Official AD 2012-01-05 · FR doc 2012-9189 · 2012-05-08 · airframe

Airworthiness Directives; Airbus Airplanes

What this AD requires

We are superseding an existing airworthiness directive (AD) for certain Airbus Model A300 B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 airplanes; and Model A300 B4-601, B4-603, B4-620, B4-622, B4- 605R, B4-622R, and F4-605R airplanes. That AD currently requires repetitive inspections for cracking in Gear Rib 5 of the main landing gear (MLG) attachment fittings at the lower flange, and repair if necessary; and provides an optional spot-facing modification around certain fastener holes, which would terminate certain repetitive inspections. This new AD mandates the optional spot-facing modification. This AD was prompted by new cases of cracks discovered during scheduled maintenance checks. We are issuing this AD to prevent cracking of the Gear Rib 5 right-hand and left-hand attachment fitting at the lower flanges of the MLG, which could result in failed bolts penetrating through the rear spar and into a fuel tank, consequent fuel loss, and reduced structural integrity of the airplane.

Repetitive inspection. Re-inspect every 16 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 2012-01-05 applies to

MakesAirbus

ModelsA300 B2-1C, A300 B2K-3C, A300 B2-203, A300 B4-2C, A300 B4-103, A300 B4-203, A300 B4-601, A300 B4-603, A300 B4-620, A300 B4-622, A300 B4-605R, A300 B4-622R, A300 F4-605R, A300

Excludes airplanes on which Airbus Modification 11912 or 11932 has been installed.

Whether AD 2012-01-05 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 2012-01-05 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.