Airworthiness Directive

AD 2013-22-13 78 FR 67011 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2013-25953
Amendment
39-17645
Published
2013-11-08
Effective
2013-11-29
Models covered
1
Last live check
2026-09-30
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AD

2013-22-13

FR doc 2013-25953 · 78 FR 67011

AD 2013-22-13Published 2013-11-08Effective 2013-11-29

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 actions to address the unsafe condition on these products.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain PILATUS Aircraft Ltd. Model PC-7 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as chafing on the wiring harness attached to the engine mounting frame on the right-hand side of the engine compartment, which could cause a short circuit and could result in a fire in the engine compartment. We are issuing this AD to require actions to address the unsafe condition on these products.

More directives for Pilatus PC-7

  1. AD 2020-26-19 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2021-02-22
  2. AD 2021-04-06 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2021-02-12
  3. AD 2019-05-15 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2019-04-03
  4. AD 2018-04-10 Airworthiness Directives; Pilatus Aircraft Limited Airplanes 2018-03-08
  5. AD 2016-17-07 Airworthiness Directives; PILATUS Aircraft Ltd. Airplanes 2016-08-26

All Pilatus PC-7 directives

Applies to 1 model in our index