Airworthiness Directive

AD 97-07-03 62 FR 14794 Active

Federal Aviation Administration · 14 CFR part 39

FR document
97-7680
Amendment
39-9976
Published
1997-03-28
Effective
1997-05-15
Models covered
1
Last live check
2026-10-03
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AD

97-07-03

FR doc 97-7680 · 62 FR 14794

AD 97-07-03Published 1997-03-28Effective 1997-05-15

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 inspecting the nose wheel flange for cracks.

Full official abstract

This amendment supersedes Airworthiness Directive (AD) 81-11- 04 that applies to The New Piper Aircraft, Inc. (Piper) Models PA31, PA31-300, PA31-325, and PA31-350 airplanes that have Cleveland nose wheel assembly part number (P/N) 40-76B installed. AD 81-11-04 currently requires inspecting the nose wheel flange for cracks. The repetitive inspections terminate by replacing the nose wheel assembly with Cleveland P/N 40-140, which is an improved design. This action is prompted by the lack of designation of Piper Model PA31P in the Applicability section of AD 81-11-04, and the subsequent failure of a nose wheel assembly on a Piper Model PA31P airplane during taxiing operations. The actions specified by this AD are intended to prevent the failure of the nose wheel, which if not corrected, could result in loss of control of the airplane during taxiing, take-off, or landing operations.

More directives for Piper PA-31 Navajo/Cheyenne

  1. AD 2017-10-20 Airworthiness Directives; Piper Aircraft, Inc. Airplanes 2017-05-25
  2. AD 2017-02-06 Airworthiness Directives; Piper Aircraft, Inc. Airplanes 2017-02-07
  3. AD 2016-08-18 Airworthiness Directives; Piper Aircraft, Inc. Airplanes 2016-05-02
  4. AD 2016-05-01 Airworthiness Directives; Piper Aircraft, Inc. Airplanes 2016-03-11
  5. AD 2015-24-05 Airworthiness Directives; Piper Aircraft, Inc. Airplanes 2015-12-08

All Piper PA-31 Navajo/Cheyenne directives

Applies to 1 model in our index