# Airworthiness Directives; Fokker Model F27 Mark 100, 200, 300, 400, 500, 600, and 700 Series Airplanes, and Model F27 Mark 050 Series Airplanes
> **Rule** · Final rule. · Published 1998-07-07 · Effective 1998-08-11 · 63 FR 36551
## Document
- **Document number:** 98-17948
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 63 FR 36551
- **Publication date:** 1998-07-07
- **Effective date:** 1998-08-11
- **FAA docket:** Docket No. 97-NM-139-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Fokker Model F27 Mark 100, 200, 300, 400, 500, 600, and 700 series airplanes, and Model F27 Mark 050 series airplanes, that requires revising the Airplane Flight Manual 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 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/1998/07/07/98-17948/airworthiness-directives-fokker-model-f27-mark-100-200-300-400-500-600-and-700-series-airplanes-and)
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