AD 94-26372
Published 1994-10-25 · 2 models · 22 US-registered tails affected · Federal Register
Airworthiness Directives; Beech Aircraft Corporation Models 34C, T-34C, and T-34C-1 Airplanes Federal Register ↗
Abstract
This document proposes to adopt a new airworthiness directive (AD) that would apply to certain Beech Aircraft Corporation (Beech) Models 34C, T-34C, and T-34C-1 airplanes. The proposed action would require 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 the proposed action. The actions specified by the proposed AD are intended to prevent the wing from separating from the fuselage because of failure of this assembly.
Applicability · by US fleet size
- BEECH T-34C-1 TCDS A26CE 14 tails
- BEECH T-34C TCDS A26CE 8 tails
Compliance instructions
Required actions, compliance times, parts/serial numbers and methods of compliance are in the Federal Register publication — not paraphrased here. Read AD on Federal Register ↗