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Airworthiness Directive

AD 2017-14-04 82 FR 31892 Active

Federal Aviation Administration · 14 CFR part 39

Prompted by several inquiries asking for clarification of the AD's applicability and compliance requirements.

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FR document
2017-14375
Amendment
39-18948
Published
2017-07-11
Effective
2017-08-15
Models covered
2

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2017-14-04 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2017-14-04

FR doc 2017-14375 · 82 FR 31892

AD 2017-14-04Published 2017-07-11Effective 2017-08-15

Supersedes 95-26-13

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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.

Prompted by several inquiries asking for clarification of the AD's applicability and compliance requirements.

Full official abstract

We are superseding Airworthiness Directive (AD) 95-26-13 for certain Piper Aircraft, Inc. Models PA-28-140, PA-28-150, PA-28-151, PA-28-161, PA-28-160, PA-28-180, PA-28-181, PA-28-235, PA-28-236, PA- 28R-180, PA-28R-200, PA-28R-201, PA-28S-160, PA-28S-180, PA-32-260, PA- 32-300, PA-32-301, PA-32-301T, PA-32R-300, PA-32R-301 (SP), PA-32R-301 (HP), PA-32R-301T, PA-32RT-300, PA-32RT-300T, and PA-32S-300 airplanes equipped with oil cooler hose assemblies that do not meet certain technical standard order (TSO) requirements. AD 95-26-13 required inspections, replacement, and adjustment of the oil cooler hose assemblies, as well as providing for a terminating action. This AD retains all of the requirements of AD 95-26-13 and adds language to clarify those requirements. This AD was prompted by several inquiries asking for clarification of the AD's applicability and compliance requirements. We are issuing this AD to correct the unsafe condition on these products.

More directives for Piper PA-28

  1. AD 2024-10-04 Airworthiness Directives; Piper Aircraft, Inc. Airplanes Effective 2024-06-06
  2. AD 2020-26-16 Airworthiness Directives; Piper Aircraft, Inc. Airplanes Effective 2021-02-16
  3. AD 2020-24-05 Airworthiness Directives; Piper Aircraft, Inc. Airplanes Effective 2020-12-28
  4. AD 2018-07-03 Airworthiness Directives; Piper Aircraft, Inc. Effective 2018-04-20
  5. AD 2018-02-05 Airworthiness Directives; Piper Aircraft, Inc. Effective 2018-02-07

All Piper PA-28 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 2 models in our index