Bombardier Challenger 600 manuals

This document is the operating manual for the Bombardier Challenger 600, specifically focusing on the hydraulic systems and landing gear operations. It details the components, controls, and emergency procedures related to the hydraulic systems that power flight controls, landing gear, and brakes.

• The aircraft has three independent hydraulic systems: No. 1, No. 2, and No. 3.
• Hydraulic power is essential for flight controls, landing gear, nose wheel steering, and brakes.
• Each hydraulic system can be powered by engine-driven or electric pumps.
• The landing gear can be operated normally or manually in case of hydraulic failure.
• Overheat detection is provided for the main landing gear bay.
• Nose wheel steering is hydraulically operated and requires the N/W STEER switch to be armed.
• The hydraulic systems maintain a nominal pressure of 3000 psi.
• Emergency procedures are in place for hydraulic system failures.