BOMBARDIER Challenger 601-3A CL-600-2B16 Pilot Training Manual page 484

If AP is engaged at the moment of failure de-
tection, the active channel disengages fol-
lowing a fault detection, and the standby
channel automatically takes over the correct
automatic control functions. Once the pilot
has acknowledged the reversion, he can clear
the caution message by pressing the RESET
pushbutton on the advisory display.
Automatic sensor reversion occurs whenever
invalid data from one sensor is detected; the
invalid condition is annunciated by a caution
MIC
16-72 CL 601-3A/R
CL-600-2B16 PILOT TRAINING MANUAL
MANUAL PITCH
TRIM SWITCH
AUTOPILOT/STICK PUSHER
DISCONNECT SWITCH
FRONT VIEW
AUTOPILOT TOUCH CONTROL
STEERING (TCS) SWITCH
REAR VIEW
Figure 16-64. Control Wheel Switches
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
message on the advisory display. The autopi-
lot then automatically selects the remaining-
s i d e s e n s o r d a t a f o r f l i g h t g u i d a n c e
computations. Once the pilot has acknowl-
edged the reversion, he can clear the caution
message by pressing the RESET pushbutton
on the advisory display.
Autopilot Disconnects
The autopilot disconnects when the following
conditions exist (Figure 16-64):
L t é e
L t d .