Airworthiness Directives; Bombardier Model CL-215T Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 1997-05-28 · Effective 1997-06-12 · 62 FR 28796
Document
Document number
97-13846
Federal Register citation
62 FR 28796
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Bombardier Model CL-215T Series
Publication date
1997-05-28
Effective date
1997-06-12
FAA docket
Docket No. 97-NM-33-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to all Bombardier Model CL-215T series airplanes. This action requires revising the Airplane Flight Manual (AFM) to modify the limitation that prohibits the positioning of the power levers below the flight idle stop during flight, and to add 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.