Airworthiness Directive

AD 2020-11-06 85 FR 31361 Active

Federal Aviation Administration · 14 CFR part 39

Requires actions to address the unsafe condition on these products.

FR document
2020-11204
Amendment
39-21131
Published
2020-05-26
Effective
2020-06-30
Models covered
1

Last live check: 2026-08-19

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AD

2020-11-06

FR doc 2020-11204 · 85 FR 31361

AD 2020-11-06Published 2020-05-26Effective 2020-06-30

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

The FAA is adopting a new airworthiness directive (AD) for Pilatus Aircraft Ltd. Model PC-6, PC-6/350, PC-6/350-H1, PC-6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/ B2-H4, PC-6/C-H2, PC-6/C1-H2, PC-6-H1, and PC-6-H2 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 flap actuator taper pins that were not swaged during the manufacturing process. The FAA is issuing this AD to require actions to address the unsafe condition on these products.

More directives for Pilatus PC-6 Porter

  1. AD 2021-24-22 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Effective 2022-01-25
  2. AD 2021-11-08 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Effective 2021-07-12
  3. AD 2020-16-02 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Effective 2020-09-09
  4. AD 2019-10-07 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Effective 2019-07-10
  5. AD 2017-04-03 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Effective 2017-04-07

All Pilatus PC-6 Porter directives

Applies to 1 model in our index