Airworthiness Directive

AD 2020-26-14 85 FR 85506 Active

Federal Aviation Administration · 14 CFR part 39

Requires modification and repetitive inspections of the PPC lever linkage.

FR document
2020-28855
Amendment
39-21369
Published
2020-12-29
Effective
2021-02-02
Models covered
1

Last live check: 2026-08-19

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AD

2020-26-14

FR doc 2020-28855 · 85 FR 85506

AD 2020-26-14Published 2020-12-29Effective 2021-02-02

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 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

  1. AD 2016-08-19 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes Effective 2016-06-06
  2. AD 2015-01-02 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes Effective 2015-02-26
  3. AD 2010-10-17 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Various Mode... Effective 2010-07-22
  4. AD 2007-17-09 Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airpl... Effective 2007-09-25
  5. AD 2006-17-05 Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airpl... Effective 2006-09-22

All Mitsubishi MU-2 directives

Applies to 1 model in our index