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

airworthiness · Rule · Final rule. · Published 1995-03-07 · Effective 1995-04-07 · 60 FR 12406

Document

Document number
95-4367
Federal Register citation
60 FR 12406
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Beech
Publication date
1995-03-07
Effective date
1995-04-07
FAA docket
Docket No. 94-CE-07-AD

Abstract

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.

Source

Authoritative
Federal Register document
Machine
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