Airworthiness Directive 80-01-05 R1
one-timeAirworthiness Directives; PACIFIC SCIENTIFIC COMPANY KIN-TECH DIVISION Restraint Systems Rotary Buckles manufactured through 1970
Which aircraft AD 80-01-05 R1 applies to
Restraint system rotary buckles manufactured through 1970; compliance required within 240 days from January 31, 1980; determine if the rotary buckle assembly contains a black body plate assembly as identified in Figure I of the AD.
Whether AD 80-01-05 R1 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.