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Airworthiness Directive 2007-26-08

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Official AD 2007-26-08 · FR doc E9-26126 · 2009-10-30 · airframe

Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes

What this AD requires

We are rescinding an existing airworthiness directive (AD) for the products listed above. The existing AD resulted from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Which aircraft AD 2007-26-08 applies to

MakesAsi AviationReims Aviation S.A.
ModelsF406
Part-conditional — 9910154-4.

Applies to all serial numbers, but only airplanes equipped with landing gear emergency blowdown bottle P/N 9910154-4.

Whether AD 2007-26-08 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 2007-26-08 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.