Airworthiness Directive 79-01-01

one-time
AD 79-01-01 · 1979-01-01 · airframe

Airworthiness Directives; -hours. This amendment becomes effective January 8, 1979. FOOTER: Textron Aviation Inc. 100 200 35-B33 35-C33 35-C33A 56TC 58 58A

Which aircraft AD 79-01-01 applies to

MakesTextron AviationBeechcraft
Models100, 200, 35-B33, 35-C33, 35-C33A, 56TC, 58, 58A, 58P, 58PA, 58TC, 58TCA, 65-B80, 70, 95-A55, 95-B55, 95-B55A, 95-C55, 95-C55A, 99, 99A, A100, A36, A99A, B100, B90, B99, C90, D55, D55A, E55, E55A, E90, F33A, F33C, G33, V35B, 33, 55, 95, 36, 90

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

Whether AD 79-01-01 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 79-01-01 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 →

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.