Airworthiness Directive

AD 97-11-08 62 FR 27943 Active

Federal Aviation Administration · 14 CFR part 39

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…

FR document
97-13465
Amendment
39-10037
Published
1997-05-22
Effective
1997-06-06
Models covered
1

Last live check: 2026-08-19

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AD

97-11-08

FR doc 97-13465 · 62 FR 27943

AD 97-11-08Published 1997-05-22Effective 1997-06-06

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 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.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Bombardier Model CL-415 series airplanes. This action 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 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