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Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airplanes

airworthiness · Rule · Final rule. · Published 1997-12-03 · Effective 1998-01-21 · 62 FR 63830

Document

Document number
97-31675
Federal Register citation
62 FR 63830
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Mitsubishi Heavy Industries MU-2B Series
Publication date
1997-12-03
Effective date
1998-01-21
FAA docket
Docket No. 97-CE-22-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Mitsubishi Heavy Industry (Mitsubishi) MU-2B series airplanes. This AD requires amending the Limitations Section of the airplane flight manual (AFM) to prohibit the positioning of the power levers below the flight idle stop while the airplane is in flight. This AFM amendment will include a statement of consequences if the limitation is not followed. This AD results from numerous incidents and five documented accidents involving airplanes equipped with turboprop engines where the propeller beta was improperly utilized during flight. The actions specified by this AD are intended to prevent loss of airplane control or engine overspeed with consequent loss of engine power caused by the power levers being positioned below the flight idle stop while the airplane is in flight.

Source

Authoritative
Federal Register document
Machine
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