Airworthiness Directive

AD 2006-14-08 71 FR 40389 Active

Federal Aviation Administration · 14 CFR part 39

FR document
06-6179
Amendment
39-14679
Published
2006-07-17
Effective
2006-08-21
Models covered
1
Last live check
2026-10-01
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AD

2006-14-08

FR doc 06-6179 · 71 FR 40389

AD 2006-14-08Published 2006-07-17Effective 2006-08-21

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 you to verify that the current flight idle blade angles are set at 12 degrees.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for some Mitsubishi Heavy Industries (MHI) MU-2B series airplanes. This AD requires you to verify that the current flight idle blade angles are set at 12 degrees. If not already set at that angle, set the flight idle blade angles to 12 degrees. This AD results from a recent safety evaluation that used a data-driven approach to analyze the design, operation, and maintenance of the MU-2B series airplanes in order to determine their safety and define what steps, if any, are necessary for their safe operation. Part of that evaluation was the identification of unsafe conditions that exist or could develop on the affected type design airplanes. We are issuing this AD to prevent incorrect flight idle blade angle settings. This unsafe condition, if not corrected, could lead to an asymmetric thrust situation in certain flight conditions, which could result in airplane controllability problems.

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  2. AD 2016-08-19 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes 2016-05-02
  3. AD 2015-01-02 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes 2015-01-22
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  5. AD 2007-17-09 Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airpl... 2007-08-21

All Mitsubishi MU-2 directives

Applies to 1 model in our index