Airworthiness Directive 93-25-02
one-timeAirworthiness Directives; specified in paragraphs (a)(1), (a)(2), (a)(3), and (a)(4) of this AD: (1) Locate and inspect the flap primary-drive torque tubes
Which aircraft AD 93-25-02 applies to
Gated by flap primary-drive torque tube P/N and S/N per AD Table 1 (e.g. P/N 734187 S/N 125-171, P/N 734378 S/N 129-150, P/N 734380 S/N 127-166); applicability read from the AD teaser — confirm exact model/serial from the records
Whether AD 93-25-02 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.