Airworthiness Directive

AD 2010-15-10 75 FR 43809 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to inspect the control wheel shaft on both the pilot and copilot sides and, if necessary, replace the control wheel shaft.

FR document
2010-18012
Amendment
39-16376
Published
2010-07-27
Effective
2010-08-31
Models covered
4

Last live check: 2026-08-19

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AD

2010-15-10

FR doc 2010-18012 · 75 FR 43809

AD 2010-15-10Published 2010-07-27Effective 2010-08-31

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 you to inspect the control wheel shaft on both the pilot and copilot sides and, if necessary, replace the control wheel shaft.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (Piper) PA-28, PA-32, PA-34, and PA-44 series airplanes. This AD requires you to inspect the control wheel shaft on both the pilot and copilot sides and, if necessary, replace the control wheel shaft. This AD results from two field reports of incorrectly assembled control wheel shafts. We are issuing this AD to detect and correct any incorrectly assembled control wheel shafts. This condition, if left uncorrected, could lead to separation of the control wheel shaft, resulting in loss of pitch and roll control.

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  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
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All Piper PA-28 directives

Applies to 4 models in our index