AD 95-04-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | T-34C | Airworthiness Directives; Beech Aircraft Corporation Models 34C, T-34C, and T-34C-1 Airplanes |
Unsafe Condition
Failure of the wing attachment nut assembly due to stress corrosion, which could cause the wing to separate from the fuselage.
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Required Actions
Replace all eight steel wing attach bolts and hardware with Inconel bolts and hardware in accordance with Beech Service Bulletin No. 2487. Special flight permits may be issued to operate the airplane to a location where the AD requirements can be accomplished.
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Compliance Time
Within whichever of the following occurs later: four years after airplane manufacture; four years after installing a new wing attachment assembly; or within the next 30 calendar days after the effective date of this AD.
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Affected Aircraft
Beech Aircraft Corporation Models 34C (serial numbers GP-1 through GP-50), T-34C (GL-2 through GL-353), and T-34C-1 (GM-1 through GM-71 and GM-78 through GM-98).
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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