EASA Regulations for Mitsubishi Heavy Industries CL-600-2E25

EASA AD CF-2022-37

Auto Flight System — Airplane Flight Manual (AFM) Limitations and Abnormal Procedures — Velocity Decay during Low Level ALT CAP in One Engine Inoperative Conditions

Airworthiness Directive CF-2022-37 is a Canadian regulatory document addressing the Auto Flight System limitations and abnormal procedures related to velocity decay during low-level altitude capture in one engine inoperative conditions. It applies to Mitsubishi Heavy Industries RJ Aviation ULC models CL-600-2B19, CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 aircraft. The directive mandates updates to the Airplane Flight Manual (AFM) to enhance safety during engine failure scenarios in climb phases.