Airworthiness Directives; Fairchild Model F-27 Series Airplanes
airworthiness · Rule · Final rule. · Published 1997-11-13 · Effective 1997-12-18 · 62 FR 60775
Document
Document number
97-29824
Federal Register citation
62 FR 60775
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Fairchild Model F-27 Series
Publication date
1997-11-13
Effective date
1997-12-18
FAA docket
Docket No. 97-NM-35-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to all Fairchild Model F-27 series airplanes, that requires revising the Airplane Flight Manual (AFM) to prohibit positioning 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 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.