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Airworthiness Directive 50-06-02

one-time
AD 50-06-02 · 1950-01-01 · airframe

Airworthiness Directives; -01. FOOTER: Boeing Airplane Company, Wichita Division 75 (Army PT-13) A75 (Army PT-13A, -13B, -13C) A75J1 (Army PT-18) A75L3 A75L

Which aircraft AD 50-06-02 applies to

MakesBoeing Airplane Company, Wichita Division
Models75, A75, A75J1, A75L3, A75L300, A75N1, B75, B75N1, D75N1, E75, E75N1, IB75A

Model designations per manufacturer index: 75 (Army PT-13), A75 (Army PT-13A/-13B/-13C), A75J1 (Army PT-18), A75L3, A75L300, A75N1 (Army PT-17/-17A, Navy N2S-1/-4), B75 (Navy N2S-5), B75N1 (Navy N2S-3), D75N1 (Army PT-27), E75 (Army PT-13D, Navy N2S-5), E75N1 (Army PT-13D, Navy N2S-5), IB75A.

Whether AD 50-06-02 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 50-06-02 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.