Airworthiness Directive

AD 2020-24-05 85 FR 74598 Active

Federal Aviation Administration · 14 CFR part 39

Requires inspecting the left and right main wing spars for corrosion, and, if corrosion is found, taking all necessary corrective actions.

FR document
2020-25690
Amendment
39-21335
Published
2020-11-23
Effective
2020-12-28
Models covered
2

Last live check: 2026-08-19

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AD

2020-24-05

FR doc 2020-25690 · 85 FR 74598

AD 2020-24-05Published 2020-11-23Effective 2020-12-28

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 inspecting the left and right main wing spars for corrosion, and, if corrosion is found, taking all necessary corrective actions.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (Piper) Models PA-28-140, PA-28-150, PA- 28-160, PA-28-180, PA-28-235, PA-32-260, and PA-32-300 airplanes. This AD was prompted by reports of corrosion found in an area of the main wing spar not easily accessible for inspection. This AD requires inspecting the left and right main wing spars for corrosion, and, if corrosion is found, taking all necessary corrective actions. The FAA is issuing this AD to address 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 2018-07-03 Airworthiness Directives; Piper Aircraft, Inc. Effective 2018-04-20
  4. AD 2018-02-05 Airworthiness Directives; Piper Aircraft, Inc. Effective 2018-02-07
  5. AD 2017-14-04 Airworthiness Directives; Piper Aircraft, Inc. Airplanes Effective 2017-08-15

All Piper PA-28 directives

Applies to 2 models in our index