Airworthiness Directive 93-25-02

one-time
AD 93-25-02 · 1993-01-01 · airframe

Airworthiness 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

MakesSundstrand
Part-conditional734187, 734378, 734380, 734382.

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:

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 93-25-02 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.