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Airworthiness Directives; Bombardier Model CL-415 Series Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 1997-05-22 · Effective 1997-06-06 · 62 FR 27943

Document

Document number
97-13465
Federal Register citation
62 FR 27943
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Bombardier Model CL-415 Series
Publication date
1997-05-22
Effective date
1997-06-06
FAA docket
Docket No. 97-NM-31-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Bombardier Model CL-415 series airplanes. This action requires revising the Airplane Flight Manual (AFM) to modify the limitation that prohibits positioning the power levers below the flight idle stop during flight, and to provide a statement of the consequences of positioning the power levers below the flight idle stop during flight. This amendment is prompted by incidents and accidents involving airplanes equipped with turboprop engines in which the propeller ground beta range was used improperly during flight. The actions specified in this AD are intended to prevent loss of airplane controllability, or engine overspeed and 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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