Is AD 2009-13-02 a recurring Airworthiness Directive?

No — AD 2009-13-02 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2009-13-02 apply to?

AD 2009-13-02 applies to Fokker — models F.28. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2009-13-02

one-time

Official AD 2009-13-02 · FR doc E9-14676 · 2009-06-29 · airframe

Airworthiness Directives; Fokker Model F.28 Mark 0100 Airplanes

What this AD requires

The FAA is superseding an existing airworthiness directive (AD), which applies to certain Fokker Model F.28 Mark 0100 airplanes. That AD currently requires revisions to the airplane flight manual (AFM) to include procedures to prohibit use of reverse engine thrust power settings between idle and emergency maximum and to prohibit stabilized engine operation in a certain engine speed range on the ground. This new AD continues to require revising the AFM to include certain procedures. This AD also requires removing the normal maximum (second) detent for the reverse-thrust control. In addition, this AD requires revising the AFM to prohibit use of reverse thrust in flight and to limit operation of Max Reverse thrust. This AD results from issuance of mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. We are issuing this AD to prevent inadvertent operation in the prohibited stabilized engine speed range on the ground, which could result in uncontained engine fan blade failure due to high cycle fatigue cracking.

Which aircraft AD 2009-13-02 applies to

MakesFokker

ModelsF.28

serial/model applicability read from the AD body — confirm the exact serial/model from the records

Whether AD 2009-13-02 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 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 2009-13-02 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.