Airworthiness Directive

AD 2015-01-02 80 FR 3164 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2015-00007
Amendment
39-18063
Published
2015-01-22
Effective
2015-02-26
Models covered
1
Last live check
2026-10-01
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AD

2015-01-02

FR doc 2015-00007 · 80 FR 3164

AD 2015-01-02Published 2015-01-22Effective 2015-02-26

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 certain Mitsubishi Heavy Industries, Ltd. Models MU-2B-30, MU-2B-35, MU-2B-36, MU-2B-36A, and MU-2B-60 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 stress corrosion cracking in the flanges of the airframe at stations 4610 and 5605. We are issuing this AD to require actions to address the unsafe condition on these products.

More directives for Mitsubishi MU-2

  1. AD 2020-26-14 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes 2020-12-29
  2. AD 2016-08-19 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes 2016-05-02
  3. AD 2010-10-17 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Various Mode... 2010-06-17
  4. AD 2007-17-09 Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airpl... 2007-08-21
  5. AD 2006-17-05 Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airpl... 2006-08-18

All Mitsubishi MU-2 directives

Applies to 1 model in our index