Airworthiness Directive 47-43-04

one-time
AD 47-43-04 · 1947-01-01 · airframe

Airworthiness Directives; the installation of Cessna P/N 0411303 or its equivalent. Cracked parts should be replaced with Cessna P/N 0310168 made of 0.080-i

Which aircraft AD 47-43-04 applies to

MakesCessna

Installation of Cessna P/N 0411303 or equivalent; cracked parts replaced with Cessna P/N 0310168 (0.080-in material)

Whether AD 47-43-04 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 47-43-04 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.