Airworthiness Directive 82-14-02
one-timeAirworthiness Directives; on the effective date of this AD shall be inspected before 6,000 cycles. d. Disks with more than 5,500 cycles on the effective dat
Which aircraft AD 82-14-02 applies to
Third-stage [turbine] disk fluorescent-penetrant/visual inspection based on accumulated cycles: disks with more than 5,500 cycles on the effective date must be inspected within 500 cycles; disks approaching 6,000 cycles must be inspected before reaching 6,000 cycles. Cracked disks addressed per following (truncated) text.
Whether AD 82-14-02 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.