EASA AD CF-2024-19
Flight Controls — Pitch-up on Landing When Using Thrust Reversers in Partial Flap Configurations
Canadian Airworthiness Directive CF-2024-19 addresses a pitch-up issue on landing when using thrust reversers in partial flap configurations for Bombardier Inc. aircraft models CL-600-1A11, CL-600-2A12, and CL-600-2B16. The directive mandates revisions to the Aircraft Flight Manual (AFM) procedures to mitigate the risk of tail strikes during landing. This AD applies to specific serial number ranges of these Challenger series aircraft.