Airworthiness Directives; Bombardier Model CL-44 Series Airplanes
airworthiness · Rule · Final rule. · Published 1997-12-09 · Effective 1998-01-13 · 62 FR 64680
Document
Document number
97-32112
Federal Register citation
62 FR 64680
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Bombardier Model CL-44 Series
Publication date
1997-12-09
Effective date
1998-01-13
FAA docket
Docket No. 97-NM-37-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to all Bombardier Model CL-44 series airplanes, that 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 ground propeller beta range was used improperly during flight. The actions specified by 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.