Airworthiness Directive 54-24-02
one-timeAirworthiness 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
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:
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.