Airworthiness Directive

AD 95-04-10 60 FR 12406 Active

Federal Aviation Administration · 14 CFR part 39

FR document
95-4367
Amendment
39-9162
Published
1995-03-07
Effective
1995-04-07
Models covered
1
Last live check
2026-09-30
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AD

95-04-10

FR doc 95-4367 · 60 FR 12406

AD 95-04-10Published 1995-03-07Effective 1995-04-07

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires replacing the eight wing attachment steel bolts and hardware with Inconel bolts and hardware.

Full official 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.

More directives for Beechcraft T-34 Mentor

  1. AD 2007-08-08 Airworthiness Directives; Raytheon Aircraft Company (The Beech Aircraft ... 2007-04-20
  2. AD 2007-06-01 Airworthiness Directives; Raytheon Aircraft Company Beech Models 45 (YT-... 2007-03-12
  3. AD 2004-25-51 Airworthiness Directives; Raytheon Aircraft Company Beech Models 45 (YT-... 2004-12-20
  4. AD 2001-13-18 R1 Airworthiness Directives; Raytheon Aircraft Corporation Beech Models 45 ... 2004-03-01
  5. AD 2001-23-10 Airworthiness Directives; Raytheon Aircraft Company 33, T-34, 35, 36, 55... 2001-11-21

All Beechcraft T-34 Mentor directives

Applies to 1 model in our index