Airworthiness Directive

AD 2014-23-03 79 FR 67340 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2014-26706
Amendment
39-18019
Published
2014-11-13
Effective
2014-12-18
Models covered
1
Last live check
2026-09-30
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AD

2014-23-03

FR doc 2014-26706 · 79 FR 67340

AD 2014-23-03Published 2014-11-13Effective 2014-12-18

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 the use of new service information and expands the scope of the inspections of the turbocharger exhaust system.

Full official abstract

We are superseding Airworthiness Directive (AD) 76-06-09 for certain Piper Aircraft, Inc. Model PA-31P airplanes. AD 76-06-09 required repetitive inspection of certain exhaust system parts with replacement of parts mating with the turbocharger, as necessary, and allowed installation of a certain tailpipe v-band coupling as terminating action. This new AD requires the use of new service information and expands the scope of the inspections of the turbocharger exhaust system. This AD was prompted by reports of exhaust system failures, new service information, and the tailpipe v-band coupling used for terminating action is obsolete. We are issuing this AD to correct the unsafe condition on these products.

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