Airworthiness Directive 80-14-07

one-time
AD 80-14-07 · 1980-01-01 · reciprocating engine

Airworthiness Directives; HEADING: AVCO LYCOMING Model O-320-H, O-360-E, LO-360-E Series Engines ACTION: SUMMARY: DATES: Effective July 7, 1980. ADDRESSES:

Which aircraft AD 80-14-07 applies to

MakesLycomingTextron LycomingAvco Lycoming
ModelsO-320-H, O-360-E, LO-360-E, O-320, O-360, LO-360

Lycoming O-320-H, O-360-E, LO-360-E series specifically (does NOT apply to other O-320/O-360 dash-suffixes) — applicability read from the AD title (pre-1994 directive, no full text on file) — confirm the exact engine model, serial, and compliance status from the records

Whether AD 80-14-07 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 80-14-07 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.