Airworthiness Directive

AD 2013-02-13 78 FR 7642 Active

Federal Aviation Administration · 14 CFR part 39

Requires inspections of the stabilator control system and replacement of parts as necessary.

FR document
2013-02075
Amendment
39-17334
Published
2013-02-04
Effective
2013-03-11
Models covered
4

Last live check: 2026-08-19

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AD

2013-02-13

FR doc 2013-02075 · 78 FR 7642

AD 2013-02-13Published 2013-02-04Effective 2013-03-11

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 inspections of the stabilator control system and replacement of parts as necessary.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (type certificate previously held by The New Piper Aircraft Inc.) PA-28, PA-32, PA-34, and PA-44 airplanes. This AD was prompted by reports of control cable assembly failures that may lead to failure of the horizontal stabilator control system and could result in loss of pitch control. This AD requires inspections of the stabilator control system and replacement of parts as necessary. 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

Applies to 4 models in our index