Is AD 2012-22-05 a recurring Airworthiness Directive?

No — AD 2012-22-05 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2012-22-05 apply to?

AD 2012-22-05 applies to Fokker Services B.V. — models F.28 Mark 0070, F.28 Mark 0100, F.28. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2012-22-05

one-time

Official AD 2012-22-05 · FR doc 2012-26781 · 2012-11-15 · airframe

Airworthiness Directives; Fokker Services B.V. Airplanes

What this AD requires

We are superseding an existing airworthiness directive (AD) for certain Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes. That AD currently requires performing a detailed visual inspection for cracks of the pistons on the main landing gear (MLG), and replacing the affected pistons if necessary. This new AD also requires modifying the MLG by installing a piston containing a certain part number, and revising the airplane maintenance program. This AD was prompted by a new modification developed to safeguard the integrity of the MLG assembly and improve surface protection of the affected area of the MLG piston. We are issuing this AD to prevent MLG failure, possibly resulting in loss of control of the airplane during the landing roll- out.

Which aircraft AD 2012-22-05 applies to

MakesFokker Services B.V.

ModelsF.28 Mark 0070, F.28 Mark 0100, F.28

Part-conditional — 41050-7, 41050-8, 41050-9, 41050-10, 41050-11, 41050-12, 41050-13, 41050-14.

Applies to all serial numbers of F.28 Mark 0070 and 0100 airplanes equipped with Goodrich (formerly Menasco, Colt Industries) main landing gear (MLG) units bearing one of the listed part numbers.

Whether AD 2012-22-05 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 2012-22-05 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.