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(a) STAB TRIM, CH 1 and MACH
TRIM switch/lights ..................................... Press in Check STAB CH 2 INOP status
message on.
Check for independent CH 1
operation from both stabilizer
trim switches in both
directions.
(b) Copilot’s STAB TRIM DISC
switch.............................................................Press Check the following:
• STAB TRIM caution
message on.
• MACH TRIM caution
message on.
• Stabilizer trim is inoperative.
(c) STAB TRIM, CH 2 and MACH
TRIM switch/lights ..................................... Press in Check STAB CH 1 INOP status
message on.
Check for independent CH 2
operation from both stabilizer
trim switches in both
directions.
(d) Pilot’s STAB TRIM DISC switch ....................Press Check the following:
• STAB TRIM caution
message on.
• MACH TRIM caution
message on.
• Stabilizer trim is inoperative.
NORMAL PROCEDURES
Airplane Preparation
Vol. 1 04−04−33
REV 68, Apr 16/07
▼
CL−604 Operating Manual
PSP 604−6
1. AIRPLANE PREPARATION (CONT'D)
E. Systems Check (Cont’d)
(e) STAB TRIM CH 1 and CH 2
switch/lights ............................................... Press in to engage CH 1 and CH 2.
Check the following:
• STAB CH 1 and CH 2 INOP
status messages out.
• STAB TRIM caution
message out.
(f) MACH TRIM switch/light............................ Press in to engage Mach trim.
Check MACH TRIM caution
message out.
(g) Aileron and rudder trims ...............................Check for free movement in both
directions.
Set at neutral for take-off.
(h) Stabilizer trim switch..................................... Select to NOSE UP or NOSE DN and
hold until trim clacker is
audible.
(11) YD 1 and YD 2 switch/lights ..............................Press in to engage. Check that the
YAW DAMPER caution
message is out.
LOWER PEDESTAL
(1) AFCS SEL ................................................... As required
(2) ATC SEL ..............................................................Select to STBY.
(3) INHIBIT PUSH switch/lights .................................Check pressed out.
(4) Reversionary selectors............................................. Set to NORM.
(5) IRS selectors ............................................................ Set to NAV. Verify IRS ALIGNING
DO NOT TAXI message out.
(6) IRS reversionary selectors (If
installed) ...................................................... As required
(7) FMS 3 selector (If installed)......................... As required
(8) LANDING GEAR MANUAL
RELEASE handle ...............................................Stowed
(9) ADG handle........................................................Stowed
(10) ADG AUTO DEPLOY CONTROL
switch ...................................................................Select to LAMP. Check that TEST
light illuminates.
NORMAL PROCEDURES
Airplane Preparation
Vol. 1 04−04−34
REV 75, Feb 17/09
CL−604 Operating Manual
PSP 604−6
1. ENGINE STARTING
A. Before Start Check
(1) Gravity crossflow ..................................................Check
(a) FUEL, GRAVITY XFLOW
switch/light ................................................. Press in to open gravity crossflow
valve.
Check GRAVITY XFLOW
OPEN light on.
(b) FUEL, GRAVITY XFLOW
switch/light ...............................................Press out to close gravity crossflow
valve.
Check GRAVITY XFLOW
OPEN light out.
CAUTION
Do not leave the fuel system in manual or gravity crossflow while the
airplane is on the ground. Uneven ground surface may create fuel
imbalance.
(2) Windshield/window heat..........................................Test
(a) ANTI-ICE, WSHLD/WIND
L and R switches .......................................... Select to HI.
(b) ANTI-ICE, WSHLD/WIND,
TEST switch ..................................................Press and hold. Check the following:
• L and R WSHLD HEAT OK
advisory messages on.
• L and R WINDOW HEAT OK
advisory messages on.
(c) ANTI-ICE, WSHLD/WIND
L and R switches .......................................... Select as required.
(3) Wing overheat detection system .............................Test
(a) ANTI-ICE, TEST switch ................................ Select to WING. Check the following:
• WING OVHT warning
message on.
• “WING OVERHEAT” aural
on.
• WING L HEAT and R HEAT
　
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