Is AD 75-24-11 a recurring Airworthiness Directive?

No — AD 75-24-11 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 75-24-11 apply to?

AD 75-24-11 applies to Beech — models A45, T-34A, D45, T-34B, 45. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 75-24-11

one-time

AD 75-24-11 · 1975-01-01 · airframe

Airworthiness Directives; BEECH Models A45 (Military T-34A, B-45) and D45 (Military T-34B) Airplanes

Which aircraft AD 75-24-11 applies to

MakesBeech

ModelsA45, T-34A, D45, T-34B, 45

Part-conditional — 45-524504, 45-524505, 45-524697, 45-524028.

To prevent failure of the P/N 45-524504 and 45-524505 rudder-aileron bungee interconnect cable assembly and the P/N 45-524697 or P/N 45-524028 bellcrank assembly; Model A45 = Military T-34A; Model D45 = Military T-34B; effective November 28, 1975.

Whether AD 75-24-11 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 75-24-11 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.