Airworthiness Directive

AD 2015-14-10 80 FR 42018 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2015-17200
Amendment
39-18208
Published
2015-07-16
Effective
2015-08-20
Models covered
1
Last live check
2026-10-01
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AD

2015-14-10

FR doc 2015-17200 · 80 FR 42018

AD 2015-14-10Published 2015-07-16Effective 2015-08-20

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 PILATUS AIRCRAFT LTD. Model PC-12/47 and PC-12/47E airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as the aileron trim tab disconnecting above 10,000 feet altitude. We are issuing this AD to require actions to address the unsafe condition on these products.

More directives for Pilatus PC-12

  1. AD 2026-15-12 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2026-08-28
  2. AD 2026-15-07 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2026-07-30
  3. AD 2026-12-01 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2026-06-09
  4. AD 2024-08-07 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2024-04-29
  5. AD 2023-12-17 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2023-07-03

All Pilatus PC-12 directives

Applies to 1 model in our index