Airworthiness Directive 65-26-02

one-time
AD 65-26-02 · 1965-01-01 · airframe

Airworthiness Directives; runaway aileron or stabilizer trim due to shorting of wires, accomplish the following: (a) Remove two side screws holding control

Which aircraft AD 65-26-02 applies to

MakesLear Jet Corporation
Part-conditional2315153-015, 2315155-025, 2315155-024.

applicability read from the AD teaser — confirm exact model/serial from the records

Whether AD 65-26-02 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 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 65-26-02 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.

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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.