Airworthiness Directive

AD 2001-21-02 66 FR 53083

Federal Aviation Administration · 14 CFR part 39

FR document
01-26323
Amendment
39-12472
Published
2001-10-19
Models covered
1
Last live check
2026-08-17
AD

2001-21-02

FR doc 01-26323 · 66 FR 53083

AD 2001-21-02Published 2001-10-19Effective 2001-11-19

Requires revising the Emergency and Normal Procedures section of the applicable Airplane Flight Manual (AFM) until the existing EEC's are replaced.

Full official 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.

Applies to 1 model in our index