Is AD 77-13-08 a recurring Airworthiness Directive?

No — AD 77-13-08 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 77-13-08 apply to?

AD 77-13-08 applies to Beech — models 58P, 58PA, 58TC, 58TCA, 58. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 77-13-08

one-time

AD 77-13-08 · 1977-01-01 · airframe

Airworthiness Directives; BEECH Models 58P and 58PA, 58TC and 58TCA Airplanes

Which aircraft AD 77-13-08 applies to

MakesBeech

Models58P, 58PA, 58TC, 58TCA, 58

Serial-conditional — narrows to serials TJ-2–TJ-99, TK-1–TK-54.

Certificated in all categories. To assure structural integrity of the right and left truss tube assemblies in both engine nacelles; applies to 58P/58PA (S/Ns TJ-2 thru TJ-99) and 58TC/58TCA (S/Ns TK-1 thru TK-54) airplanes that do not have Beech Kit (source text truncated).

Whether AD 77-13-08 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 77-13-08 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 →

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.