Landing Gear And Brakes - BOMBARDIER Challenger 601-3A CL-600-2B16 Pilot Training Manual

INTRODUCTION
The Canadair Challenger CL-600-2B16, model CL-601-3A/R landing gear is electrically
controlled, hydraulically actuated, and is partially enclosed by mechanically or hy-
draulically actuated doors. Gear position and warning are provided by indicator lights
and a warning horn.
Hydraulically actuated nosewheel steering is provided for ground taxiing and directional
control during takeoff and landing.
Brake assemblies are mounted in each main gear wheel. They are powered by hydraulic
pressure through an antiskid system.
GENERAL
Each inward-retracting main landing gear uses
hydraulic actuators to release the uplocks, to
extend and retract the landing gear, and to
disengage the downlocks. There is also an ac-
tuator to assist downlocking during emergency
extension.

LANDING GEAR AND BRAKES

FOR TRAINING PURPOSES ONLY
FlightSafety Canada
CL-600-2B16 PILOT TRAINING MANUAL
CHAPTER 14
The forward-retracting nose landing gear also
uses hydraulic actuators to release the up-
locks, to extend and retract the nose gear, to
disengage the downlocks, and to operate the
forward nose gear doors. All landing gear up-
locks can be released from the cockpit for
emergency extension.
Lt é e
Lt d .
CL 601-3A/R 14-1