Airworthiness Directive 93-22-05
one-timeAD 93-22-05 · 1993-01-01 · airframe
Airworthiness Directives; 7FC, 7JC, 7ECA, 11BC, S11BC, 11CC, S11CC, and 402; Anderson Greenwood Model 14; Cessna Model 120, 140, 140A, 150, 150A-M, and A150
Which aircraft AD 93-22-05 applies to
Makes7Fc 7Jc 7Eca 11Bc S11Bc 11Cc S11Cc And 402 Anderson Greenwood
Models14, 120, 140, 140A, 150, 150A-M, 8E, 8F, B85C, PA-18, PA-19
Whether AD 93-22-05 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 93-22-05 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.
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.