Is AD 95-04-10 a recurring Airworthiness Directive?

No — AD 95-04-10 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 95-04-10 apply to?

AD 95-04-10 applies to Beech — models 34C, T-34C, T-34C-1, T-34. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 95-04-10

one-time

Official AD 95-04-10 · FR doc 95-4367 · 1995-03-07 · airframe

Airworthiness Directives; Beech Aircraft Corporation Models 34C, T-34C, and T-34C-1 Airplanes

What this AD requires

This amendment adopts a new airworthiness directive (AD) that applies to certain Beech Aircraft Corporation (Beech) Models 34C, T- 34C, and T-34C-1 airplanes. This action requires replacing the eight wing attachment steel bolts and hardware with Inconel bolts and hardware. A report of the right lower aft wing attachment nut assembly separating in two pieces on a Model T-34C-1 airplane prompted this action. The actions specified by this AD are intended to prevent the wing from separating from the fuselage because of failure of this assembly.

Which aircraft AD 95-04-10 applies to

MakesBeech

Models34C, T-34C, T-34C-1, T-34

Serial-conditional — narrows to serials GP-1–GP-50, GL-2–GL-353, GM-1–GM-71, GM-78–GM-98.

Applies only to airplanes with steel wing attachment assembly bolts and hardware.

Whether AD 95-04-10 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 95-04-10 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 →Read the full directive (Federal Register)

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.