Airworthiness Directives; Honeywell International Inc. (formerly AlliedSignal Inc. and Garrett Turbine Engine Company) TPE331-8, -10N, and -12B Turboprop Engines
airworthiness · Rule · Final rule; request for comments. · Published 2001-10-19 · Effective 2001-11-19 · 66 FR 53083
Document
Document number
01-26323
Federal Register citation
66 FR 53083
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Honeywell International Inc. (formerly AlliedSignal Inc. and Garrett Turbine
Publication date
2001-10-19
Effective date
2001-11-19
FAA docket
Docket No. 2000-NE-39-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to Honeywell International Inc. (formerly AlliedSignal Inc. and Garrett Turbine Engine Company) TPE331-8, -10N, and -12B turboprop engines with certain electronic engine controls (EEC's) installed. This AD requires revising the Emergency and Normal Procedures section of the applicable Airplane Flight Manual (AFM) until the existing EEC's are replaced. This amendment is prompted by a report of an engine experiencing an uncommanded full power increase during an approach while both engine power levers were at the flight idle gate. The actions specified in this AD are intended to minimize exposure to flight and ground operations that could lead to the loss of control of the airplane due to asymmetric thrust and an uncommanded torque increase.