2020-26-14
FR doc 2020-28855 · 85 FR 85506AD 2020-26-14Published 2020-12-29Effective 2021-02-02
Requires modification and repetitive inspections of the PPC lever linkage.
Supersedes an earlier directive that is not in our index. See the official text.
Full official abstract
The FAA is superseding Airworthiness Directive (AD) 75-16-20, which applied to all Mitsubishi Heavy Industries, Ltd., Model MU-2B, MU-2B-10, MU-2B-15, MU-2B-20, MU-2B-25, MU-2B-26, MU-2B-30, MU-2B-35, and MU-2B-36 airplanes. AD 75-16-20 required repetitive inspections of the propeller pitch control (PPC) lever for security and proper rigging. This AD requires modification and repetitive inspections of the PPC lever linkage. The FAA is issuing this AD to address the unsafe condition on these products.
More directives for Mitsubishi MU-2
- AD 2016-08-19 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes Effective 2016-06-06
- AD 2015-01-02 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes Effective 2015-02-26
- AD 2010-10-17 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Various Mode... Effective 2010-07-22
- AD 2007-17-09 Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airpl... Effective 2007-09-25
- AD 2006-17-05 Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airpl... Effective 2006-09-22
