Airworthiness Directive

AD 2020-16-02 85 FR 47295

Federal Aviation Administration · 14 CFR part 39

FR document
2020-16989
Amendment
39-21186
Published
2020-08-05
Models covered
1
Last live check
2026-08-17
AD

2020-16-02

FR doc 2020-16989 · 85 FR 47295

AD 2020-16-02Published 2020-08-05Effective 2020-09-09

Corrects: The MCAI describes the unsafe condition as rudder shaft assemblies with incorrect rivet configurations.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for Pilatus Aircraft Ltd. Models 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 rudder shaft assemblies with incorrect rivet configurations. The FAA is issuing this AD to address the unsafe condition on these products.

Applies to 1 model in our index