# Airworthiness Directives; Bombardier Model CL-44 Series Airplanes
> **Rule** · Final rule. · Published 1997-12-09 · Effective 1998-01-13 · 62 FR 64680
## Document
- **Document number:** 97-32112
- **Category:** airworthiness
- **Manufacturer:** Bombardier Model CL-44 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 62 FR 64680
- **Publication date:** 1997-12-09
- **Effective date:** 1998-01-13
- **FAA docket:** Docket No. 97-NM-37-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Bombardier Model CL-44 series airplanes, that requires revising the Airplane Flight Manual (AFM) to modify the limitation that prohibits positioning the 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 ground propeller 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.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1997/12/09/97-32112/airworthiness-directives-bombardier-model-cl-44-series-airplanes)
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