Airworthiness Directive 82-14-02

one-time
AD 82-14-02 · 1982-01-01 · turbine engine

Airworthiness 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

MakesPratt & Whitney
ModelsJT3D-1, JT3D-1-MC6, JT3D-1-MC7, JT3D-1A, JT3D-1A-MC6, JT3D-1A-MC7, JT3D-3, JT3D-3B, JT3D-3C, JT3D-5A, JT3D-7, JT3D-7A, JT3D

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:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 82-14-02 complied with on your aircraft?

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.