Airworthiness Directive 65-21-05
one-timeAirworthiness Directives; Region, before further flight, except that the airplane may be flown in accordance with FAR 21.197 to a base where the repair can
Which aircraft AD 65-21-05 applies to
Lockheed Drawing 841307 (structural crack repair) — Applicability read from the AD teaser — confirm exact model/serial from the records.
Whether AD 65-21-05 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.