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Airworthiness Directive 75-24-13

one-time
AD 75-24-13 · 1975-01-01 · propeller

Airworthiness Directives; Great Lakes Region. The manufacturer's specifications and procedures identified in this Directive are incorporated herein and made

Which aircraft AD 75-24-13 applies to

MakesMccauley
ModelsD2AF34C52/80GF-0, D2AF34C52A/80GF-0

Reinforce main beam web between wing stations as described; inspection for fuel stains alone is insufficient to rule out a crack.

Whether AD 75-24-13 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 75-24-13 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.