Airworthiness Directive 92-07-05

one-time
AD 92-07-05 · 1992-01-01 · airframe

Airworthiness Directives; Beech Models 65-90, 65-A90, 65-A90-1, 65-A90-2, 65-A90-3, 65-A90-4, B90, C90, C90A, E90, H90, 99, 99A, A99A, B99, C99, 100, A100,

Which aircraft AD 92-07-05 applies to

MakesBeech
Models65-90, 65-A90, 65-A90-1, 65-A90-2, 65-A90-3, 65-A90-4, B90, C90, C90A, E90, H90, 99, 99A, A99A, B99, C99, 100, A100, B100, 90

Inspection and possible modification required per Beech Service Bulletin No. 2365, Revision 1, dated December 1991; submitted through Wichita Aircraft Certification Office.

Whether AD 92-07-05 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 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 92-07-05 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.

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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.