Airworthiness Directive 54-24-02

one-time
AD 54-24-02 · 1954-01-01 · airframe

Airworthiness Directives; stains alone as an indication of a crack is not sufficient due to the presence of sealant on the inside of the tank surface. 2. Re

Which aircraft AD 54-24-02 applies to

Models1049C, 1049E, 1049D, 1049

Reinforce main beam web between wing stations 551 (fuel tank area); fuel-stain inspection alone is insufficient to detect a crack due to sealant; repeat inspection at approximately 125-hour intervals until area is reinforced.

Whether AD 54-24-02 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 54-24-02 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.