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Airworthiness Directive 93-02-05

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AD 93-02-05 · 1993-01-01 · airframe

Airworthiness Directives; -24 Comanche, PA-30 and PA-39 Twin Comanche, PA-28 Arrow, and PA-23 Aztec; Beech 60 Duke and 23 Musketeer; Mooney M20; and Cessna

Which aircraft AD 93-02-05 applies to

MakesPiperBeechMooneyCessna
ModelsPA-24 Comanche, PA-30 Twin Comanche, PA-39 Twin Comanche, PA-28 Arrow, PA-23 Aztec, Beech 60 Duke, Beech 23 Musketeer, Mooney M20, Cessna 177 Cardinal, PA-24, PA-30, PA-39, PA-28, PA-23, 60, 23, M20, 177

Excerpt lists these airframes as installation platforms for an affected engine; text explicitly notes only engine variants with an 'I' in the model designation prefix (fuel-injected) incorporate the affected fuel system — engine make/model itself not captured in this excerpt, so applicability must be confirmed per-aircraft (applicability read from the AD teaser — confirm exact model/serial from the records.)

Whether AD 93-02-05 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 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 93-02-05 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.