Airworthiness Directive 47-43-03
one-timeAirworthiness 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
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:
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.