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• Full free movement.
• Corresponding surface
displacement on flight
controls page.
• Ensure that no hydraulic
messages come on.
NORMAL PROCEDURES
Engine Starting
Vol. 1 04−05−20
REV 77, Oct 20/09
▼
CL−604 Operating Manual
PSP 604−6
1. ENGINE STARTING (CONT'D)
H. After Engine Start Check (Cont’d)
(14) Elevators ...........................................................Operate over full travel range.
Check the following:
• Free full movement.
• Corresponding surface
displacement on flight
control page.
• Ensure that no hydraulic
messages come on.
• ELEVATOR SPLIT caution
message out.
(15) Ground spoilers check.............................................Test 1
(a) GND SPOILERS switch................................ Select to DISARM.
Verify that both ground spoiler
panels are retracted.
NOTE
If on the ground and both engines are above 70% N1, with the GND
SPOILERS switch not armed the GND SPOILERS NOT ARMED caution
message will come on.
(b) GND SPOILERS switch................................ Select to ARM.
Verify that both ground spoiler
panels deploy to maximum
travel.
(c) GND SPOILERS switch................................ Select to AUTO.
Verify that ground spoiler
panels are retracted.
(16) Flight spoilers check................................................Test 1
(a) FLIGHT SPOILER lever ............................... Select to MAX.
Verify that flight spoiler panels
deploy.
NOTE
When flight spoilers are fully deployed (on the ground with the throttles
at IDLE), ground spoilers will deploy if selected to AUTO.
(b) FLIGHT SPOILER lever ............................... Select to RETRACT.
Verify that flight spoiler panels
retract.
(17) NOSE STEER switch ...........................................Select to ARMED.
Check STEERING INOP
caution message out.
NORMAL PROCEDURES
Engine Starting
Vol. 1 04−05−21
REV 77, Oct 20/09
▼
CL−604 Operating Manual
PSP 604−6
1. ENGINE STARTING (CONT'D)
H. After Engine Start Check (Cont’d)
(18) APR......................................................................Check
(a) ENGINE CONTROL, ENG
SPEED switches...........................................Check both selected to ON.
(b) ENGINE CONTROL, right APR
switch............................................................ Select to TEST 1 and TEST 2 in turn.
Check the following:
• APR TEST 1 OK advisory
message on.
• APR TEST 2 OK advisory
message on.
NOTE
APR TEST 1 and 2 OK advisory messages go out after 10 seconds.
If 2 DCUs are installed:
(c) ENGINE CONTROL, left APR
switch............................................................ Select to ARM.
If 3 DCUs are installed:
(d) ENGINE CONTROL, left APR
switch............................................................ Select to TEST 3.
Check the following:
• APR TEST 3 OK advisory
message on.
• Select left switch to ARM.
NOTE
AT 79% N1 during take-off, the APR ARM advisory message should
come on.
CAUTION
If an APR INOP caution message is displayed, select the ENGINE
CONTROL, APR switch to OFF and use APR-off performance. Refer to
Chapter 5; ABNORMAL PROCEDURES – APR Failure.
(19) ADG AUTO DEPLOY CONTROL
switch ...................................................................Select to UNIT. Check that TEST
light comes on for two (2)
seconds, then goes out.
NORMAL PROCEDURES
Engine Starting
Vol. 1 04−05−22
REV 77, Oct 20/09
CL−604 Operating Manual
PSP 604−6
1. TAXIING AND TAKE-OFF
A. Taxi Check
CAUTION
Always make sure that the steering is within the nominal operating
range of ±55° before re-cycling the arming switch.
NOTE
At airports where runway structural repair or debris is known to exist,
use thrust reversers with extreme caution to preclude the possibility of
foreign object damage (FOD) from occurring.
(1) Brakes ..................................................................Check
(a) Airplane ............................................................Roll forward and apply brakes.
Check that no anti-skid or
brake messages come on.
If conditions exist that could result in water saturated brakes:
(b) Brakes .......................................................... Warm Perform the following number
of firm brake applications from
　
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