Airworthiness Directive 66-14-04
one-timeAirworthiness Directives; REGULATORY TEXT: 66-14-04 PRATT & WHITNEY: Amdt. 39-247 Part 39 Federal Register June 8, 1966. Applies to Pratt & Whitney Aircraft
Which aircraft AD 66-14-04 applies to
Applies to Pratt & Whitney Aircraft Wasp Jr. and R-985 Series Engines. Replace cam reduction drive gear assembly P/N 3965 with cam reduction drive gear P/N 331098 at next engine overhaul, per Pratt & Whitney Aircraft Service Bulletin No. 1671, Supplement No. 1, Revision A. Amendment 39-247, Federal Register June 8, 1966.
Whether AD 66-14-04 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:
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.