Airworthiness Directive 2008-10-13
one-timeAirworthiness Directives; EADS SOCATA Model TBM 700 Airplanes
What this AD requires
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the 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 2008-10-13 applies to
Concerns rupture of the alternator and vapour cycle cooling system pulley drive assembly. AD retains requirements of AD 2008-0063-E (superseded) and introduces a terminating action replacing the pulley drive assembly with an improved-design assembly (EADS SOCATA modification MOD 70-0231-21).
Whether AD 2008-10-13 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:
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.