# Airworthiness Directives; Beech Aircraft Corporation Models 34C, T-34C, and T-34C-1 Airplanes
> **Rule** · Final rule. · Published 1995-03-07 · Effective 1995-04-07 · 60 FR 12406
## Document
- **Document number:** 95-4367
- **Category:** airworthiness
- **Manufacturer:** Beech
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 60 FR 12406
- **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
- [Federal Register document](https://www.federalregister.gov/documents/1995/03/07/95-4367/airworthiness-directives-beech-aircraft-corporation-models-34c-t-34c-and-t-34c-1-airplanes)
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