Airworthiness Directive

AD 2016-07-21 81 FR 21261 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2016-07580
Amendment
39-18466
Published
2016-04-11
Effective
2016-04-26
Models covered
1
Last live check
2026-10-02
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AD

2016-07-21

FR doc 2016-07580 · 81 FR 21261

AD 2016-07-21Published 2016-04-11Effective 2016-04-26

Supersedes 2015-20-13

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 reports that additional airplanes have been found with the same cracks.

Full official abstract

We are superseding Airworthiness Directive (AD) 2015-20-13 for certain Piper Aircraft, Inc. Models PA-28-161, PA-28-181, and PA-28R- 201 airplanes. AD 2015-20-13 required inspecting the right wing rib at wing station 140.09 for cracks and taking necessary corrective action. This AD retains the actions for AD 2015-20-13 and adds airplanes to the applicability. This AD was prompted by reports that additional airplanes have been found with the same cracks. 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 2024-05-22
  2. AD 2020-26-16 Airworthiness Directives; Piper Aircraft, Inc. Airplanes 2021-01-15
  3. AD 2020-24-05 Airworthiness Directives; Piper Aircraft, Inc. Airplanes 2020-11-23
  4. AD 2018-07-03 Airworthiness Directives; Piper Aircraft, Inc. 2018-04-05
  5. AD 2018-02-05 Airworthiness Directives; Piper Aircraft, Inc. 2018-01-23

All Piper PA-28 directives

Applies to 1 model in our index