BOMBARDIER Challenger 601-3A CL-600-2B16 Pilot Training Manual page 407

1. Aileron and elevator flutter is prevented by:
A. Hydraulic dampers
B. The associated PCU's
C. Artificial feel units
D. None of the above
2. If one set of aileron control linkage
jams and the ROLL DISCONNECT han-
dle is pulled:
A. The pilot can actuate both ailerons.
B. The copilot can actuate both ailerons.
C. The pilot can actuate the left aileron;
t h e c o p i l o t c a n a c t u a t e t h e r i g h t
aileron.
D. The aileron opposite the jammed
linkage can be actuated by the pilot
on that side.
3. The primary flight control surfaces are
protected from gust damage by:
A. The flutter dampers
B. A mechanical control lock in the
cockpit
C. A damping effect within the PCU's
D. An absolute liquid lock in the PCU's
4. If one PCU control valve jams:
A. The surface cannot be actuated.
B. The surface is actuated by the re-
maining PCU.
C. The surface will actuate at half speed.
D. Surface travel is reduced.
CL-600-2B16 PILOT TRAINING MANUAL
QUESTIONS
5.
6.
7.
8.
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
Travel of the primary flight controls is
limited by:
A. PCU travel only
B. Mechanical stops only
C. Mechanical stops and PCU travel
D. Airspeed and mechanical stops
Stabilizer trim is achieved by:
A. An electric actuator that positions the
elevator PCU's
B. Varying the angle of incidence of the
horizontal stabilizer with a hydraulic
actuator
C. Varying the angle of incidence of
the horizontal stabilizer with elec-
tric motors
D. Electric motors that position the ele-
vators
The two electric motors in the flap PDU:
A. Are powered by separate buses
B. Are powered by a single bus
C. Continue to operate when in an over-
heated condition
D. Must be operating simultaneously to
actuate the flaps
If both pointers of the SPS TEST indica-
tor move into the STALL sector:
A. A warning tone sounds (warbler).
B. The red STALL PUSH lights flash.
C. The stick pusher activates.
D. All the above
L t ée
L t d .
CL 601-3A/R 15-17