Airworthiness Directive 92-06-08

one-time
AD 92-06-08 · 1992-01-01 · airframe

Airworthiness Directives; 8401, Washington, DC. (e) This amendment (39-8188) becomes effective on April 17, 1992. FOOTER: SOCATA - Groupe Aerospatiale GA-7

Which aircraft AD 92-06-08 applies to

MakesSocata
ModelsGA-7

Amendment 39-8188, effective April 17, 1992. Captured text is administrative boilerplate only; substantive condition/corrective-action text not present in excerpt.

Whether AD 92-06-08 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 complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 92-06-08 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.

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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.