Airworthiness Directive 80-13-51
one-timeAirworthiness Directives; ferried in accordance with FAR Sections 21.197 and 21.199 to a place where replacement can be made, if CF-6-50C or CF- 6-50C1 engi
Which aircraft AD 80-13-51 applies to
If CF6-50C or CF6-50C1 engines are installed, ferry per FAR 21.197/21.199 to a location for replacement with serviceable CF6-50C2 engines; within 20 hours time in service after the effective date, incorporate Airbus Industrie A300B4-103 AFM Revision 6, dated May 28, 1980, or an FAA-approved equivalent.
Whether AD 80-13-51 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.