Airworthiness Directive

AD 97-11-09 62 FR 28796 Active

Federal Aviation Administration · 14 CFR part 39

FR document
97-13846
Amendment
39-10038
Published
1997-05-28
Effective
1997-06-12
Models covered
1
Last live check
2026-10-01
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AD

97-11-09

FR doc 97-13846 · 62 FR 28796

AD 97-11-09Published 1997-05-28Effective 1997-06-12

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires revising the Airplane Flight Manual (AFM) to modify the limitation that prohibits the positioning of the power levers below the flight idle stop during flight, and to add a statement of the consequences of positioning…

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Bombardier Model CL-215T series airplanes. This action requires revising the Airplane Flight Manual (AFM) to modify the limitation that prohibits the positioning of the power levers below the flight idle stop during flight, and to add 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 propeller ground beta range was used improperly during flight. The actions specified in 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.

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All Canadair CL-215 / CL-415 directives

Applies to 1 model in our index