Airworthiness Directive 47-20-06

one-time
AD 47-20-06 · 1947-01-01 · airframe

Airworthiness Directives; and -6) to the front face of the aileron beam and lower surface of the lower aileron skin, respectively, following the procedure o

Which aircraft AD 47-20-06 applies to

MakesUnivair Aircraft Corporation
Models415-C, 415-CD, 415-D, 415

Requires attaching a reinforcement (rivets/doublers; part designation truncated, ending '...and -6') to the front face of the aileron beam and the lower surface of the lower aileron skin; corresponds to Ercoupe Service Dept. Bulletin No. 20, dated February 17, 1947 (blind rivet, Type A, referenced).

Whether AD 47-20-06 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 47-20-06 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.