Airworthiness Directive 47-43-03

one-time
AD 47-43-03 · 1947-01-01 · appliance

Airworthiness Directives; -03-00A, change 1, dated May 15, 1947; and Edo Service Bulletin No. 3 dated August 30, 1947, cover this same subject.) FOOTER: Ces

Which aircraft AD 47-43-03 applies to

MakesCessna Aircraft CompanyTextron Aviation Inc
Models120, 140

Seat belt buckle removal/replacement; footer identifies Cessna 120/140 (current TC holder Textron Aviation Inc); also references Edo Service Bulletin/Drawing 88-03-00A for float-related hardware (applicability read from the AD teaser — confirm exact model/serial from the records.)

Whether AD 47-43-03 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 47-43-03 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.