Airworthiness Directive 65-21-05

one-time
AD 65-21-05 · 1965-01-01 · airframe

Airworthiness 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

Part-conditional841309-102.

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:

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 65-21-05 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.