Airworthiness Directive 46-36-01

one-time
AD 46-36-01 · 1946-01-01 · airframe

Airworthiness Directives; 75C; Piper AE-1, HE-1; J3C-65, J3C-65S; J4, J4A, J4A-S; J4E; J5A, J5A-80, J5C; Silvaire (Luscombe) 8, 8A, 8B, 8C, 8D, 8E; Stinson

Which aircraft AD 46-36-01 applies to

MakesPiperSilvaire (Luscombe)StinsonSuperior (Culver)TaylorcraftUniversal (Taylorcraft)
ModelsAE-1, HE-1, J3C-65, J3C-65S, J4, J4A, J4A-S, J4E, J5A, J5A-80, J5C, 8, 8A, 8B, 8C, 8D, 8E, HW-75, 10, LCA, DC-65, DCO-65, BC

Applicability lists many small manufacturer/model combinations (1940s-era light aircraft); condition and corrective-action text not present in captured excerpt (cut off mid-list at 'Universal (Taylorcraft) BC').

Whether AD 46-36-01 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 46-36-01 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.