Airworthiness Directive 47-30-08

one-time
AD 47-30-08 · 1947-01-01 · airframe

Airworthiness Directives; bottom lip of lugs. (Aeronca Service Memorandum M-76 dated May 15, 1947, covers this same subject.) FOOTER: Gores, William 65-CA (

Which aircraft AD 47-30-08 applies to

MakesAeronca
Models65-CA, 65-LA, S-65-CA

Army designation L-3F for model 65-CA (per Aeronca Service Memorandum M-76 dated May 15, 1947); type certificate later associated with William Gores

Whether AD 47-30-08 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 47-30-08 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.