Airworthiness Directive 77-08-05
one-timeAirworthiness Directives; method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region. C) Ces
Which aircraft AD 77-08-05 applies to
Compliance per Cessna Service Letter ME77-8, dated March 28, 1977; alternative methods of compliance require approval by FAA Chief, Engineering and Manufacturing Branch, Central Region.
Whether AD 77-08-05 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:
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.