Airworthiness Directive 64-21-06 R2

one-time
AD 64-21-06 R2 · 1964-01-01 · airframe

Airworthiness Directives; September 10, 1964. Amendment 39-2156 was effective April 9, 1975. This Amendment 39-3827 is effective July 7, 1980. FOOTER: Colum

Which aircraft AD 64-21-06 R2 applies to

Models107-II, 107

Original directive effective September 10, 1964; Amendment 39-2156 effective April 9, 1975; this Amendment 39-3827 (Revision 2) effective July 7, 1980.

Whether AD 64-21-06 R2 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 64-21-06 R2 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.

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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.