Airworthiness Directive

AD 96-24-13 61 FR 60016 Active

Federal Aviation Administration · 14 CFR part 39

FR document
96-29986
Amendment
39-9837
Published
1996-11-26
Effective
1997-01-17
Models covered
1
Last live check
2026-10-03
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AD

96-24-13

FR doc 96-29986 · 61 FR 60016

AD 96-24-13Published 1996-11-26Effective 1997-01-17

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 modifying the landing gear selector cable forward attachment pin assembly by installing a safety lock wire on certain The New Piper Aircraft Inc.

Full official abstract

This document supersedes AD 75-26-18, which currently requires modifying the landing gear selector cable forward attachment pin assembly by installing a safety lock wire on certain The New Piper Aircraft Inc., (Piper) PA-31, PA-31P, and PA-31T series airplanes. The action will require the same action as AD 75-26-18. An incorrect designation of Piper Model PA-31 airplanes as Piper Model PA-31-310 airplanes in AD 75-26-18 prompted the proposed AD action. The actions specified by this AD are intended to prevent the landing gear selector cable forward attachment pin assembly from becoming separated from the powerpack control arm, which, if not corrected, could cause loss of landing gear retraction or extension.

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