Airworthiness Directive 64-26-02
one-timeAD 64-26-02 · 1964-01-01 · reciprocating engine
Airworthiness Directives; GENERAL ELECTRIC Models CT58-100-1, -100-2, -110-1, CT58-140-1; Military T58-GE-1, T58-GE-5 Engines ACTION: SUMMARY: DATES: Effect
Which aircraft AD 64-26-02 applies to
MakesGeneral Electric
ModelsCT58-100-1, CT58-140-1, T58-GE-1, T58-GE-5
Serial-conditional — narrows to serials 295001–295018, 285001–285016.
Whether AD 64-26-02 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 64-26-02 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.