Airworthiness Directives; de Havilland Inc. Models DHC-6-1, DHC- 6-100, DHC-6-200, and DHC-6-300 Airplanes
airworthiness · Rule · Final rule. · Published 1999-08-31 · 64 FR 47374
Document
Document number
99-22535
Federal Register citation
64 FR 47374
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1999-08-31
FAA docket
Docket No. 97-CE-10-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that applies to all de Havilland Inc. Models DHC-6-1, DHC-6-100, DHC-6-200, and DHC-6-300 airplanes. This AD requires amending the Limitations Section of the airplane flight manual (AFM) to prohibit the positioning of the power levers aft of the flight idle stop while the airplane is in flight. The AFM amendment includes a statement of consequences if the limitation is not followed. This AD is a result of numerous incidents and five documented accidents involving airplanes equipped with turboprop engines where the propeller beta was improperly utilized during flight. None of the incidents or accidents involved de Havilland Inc. Models DHC-6-1, DHC-6-100, DHC-6- 200, and DHC-6-300 airplanes. 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 aft of the flight idle stop while the airplane is in flight.