EASA AD CF-2022-45
Auto Flight System — Airplane Flight Manual Limitations and Procedures — Velocity Decay during Low Level Altitudes Capture (V) ALTS CAP or (V) ALTV CAP modes in One Engine Inoperative Conditions
Airworthiness Directive CF-2022-45 is issued by Transport Canada and addresses the Auto Flight System limitations and procedures related to velocity decay during low level altitude capture modes (V ALTS CAP or V ALTV CAP) in one engine inoperative conditions. This directive applies specifically to Bombardier Inc. CL-600-2B16 aircraft, serial numbers 5301 through 5665, 5701 through 5988, and 6050 through 6160. It mandates updates to the Airplane Flight Manual (AFM) to ensure safe operation during engine failure scenarios in these flight modes.
Airworthiness DirectiveFlight OpsSafety MgmtBombardier CL-600 (Challenger)Bombardier CL-600-2B16