Airworthiness Directive 62-25-02
one-timeAD 62-25-02 · 1962-01-01 · airframe
Airworthiness Directives; 300 hours' time in service. \n\n\t(c) Inspect, using dye penetrant, or magnetic particle, or FAA approved equivalent, for cracks i
Which aircraft AD 62-25-02 applies to
Makes300 Hours' Time In Service \N\N\T Inspect Using Dye Penetrant Or Magnetic Particle Or Faa Approved Equivalent For Cracks In 0 125-Inch Radii At Edges Of Torque November 28 1962) Unknown 62-25-02 Ad Final Rules 62-25-02 Douglas Amdt 510 Part 507 Federal Register November 28 1962 Applies To All
ModelsDC-6, DC-7
Applies to all models of the make above.
Whether AD 62-25-02 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 compliance — The specific action taken (inspected, replaced, modified) and to what revision.
Date — When the work was done.
Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.
Signature & certificate — The A&P/IA who returned it to service, with certificate number.
Is AD 62-25-02 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.