Airworthiness Directive 92-12-05
one-timeAD 92-12-05 · 1992-01-01 · reciprocating engine
Airworthiness Directives; AIRWORTHINESS DIRECTIVES FINAL RULES: 92-12-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 91-ANE-48
Which aircraft AD 92-12-05 applies to
MakesAirworthiness Directives Final Rules 92-12-05 Citation This Information Is Not Available Page Number Docket Number 91-Ane-48 Amendment 39-8265 Ad Number 92-12-05 Subject Heading Textron Lycoming
ModelsO-320, IO-320, LIO-320, AIO-320, AEIO-320, O-340, O-360, LO-360, HO-360, VO-360, IVO-360, IO-360, AIO-360, HIO-360, LHIO-360, LIO-360, AEIO-360, TO-360, LTO-360, TIO-360, O-480, GSO-480, IGSO-480, IGO-480, GO-480, O-540, O-540-J, O-540-L, IO-540-W, VO-540, IO-540
Whether AD 92-12-05 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 92-12-05 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.