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ABNORMAL PROCEDURES – FLIGHT CONTROLS – Flaps
Failure, for factors to be applied to approach speed and landing
distance.
2. Higher than normal engine vibration of a fluctuating nature may be
experienced in icing conditions. If the FAN VIB gauge indicates
greater than 2.7 mils, refer to Chapter 5; ABNORMAL
PROCEDURES – POWER PLANT.
3. During single engine operation in icing conditions with wing anti-ice
system on, open bleed air isolation valve to prevent asymmetric
anti-icing. N2 RPM in excess of 78% may be required to provide
sufficient bleed air to prevent L and R WING A/ICE caution
messages.
4. Use of cowl and wing anti-ice systems affects engine and airplane
performance. Refer to Chapter 6; PERFORMANCE, for applicable
factors.
5. If the airplane flies out of icing conditions and the ice detector
system senses no ice present, the ICE message will go out (after
60 seconds).
I. Before Landing
(1) ANTI-ICE, WING switch and L
and R COWL switches .........................................Check status. See NOTE 4 above.
J. After Landing
If no icing, precipitation or other conditions that could cause fogging or misting exist:
(1) ANTI-ICE, WSHLD/WIND L and R
switches................................................................Select as required.
NORMAL PROCEDURES
Ice and Rain Protection
04−14−7
REV 77, Oct 20/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
NORMAL PROCEDURES
Ice and Rain Protection
04−14−8
REV 77, Oct 20/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. LANDING GEAR, WHEELS AND BRAKES
A. Main Landing Gear Bay Overheat Detection – First Flight of the Day
Check the MLG overheat detection system as follows:
(1) MLG BAY OVHT TEST, OVHT
switch ...................................................................Select to OVHT and hold.
Check the following:
• MLG BAY OVHT warning
message on.
• “GEAR BAY OVERHEAT”
aural message on.
Release switch and check that
aural and warning messages
go out.
(2) MLG BAY OVHT TEST, FAIL
switch ...................................................................Select to FAIL and hold.
Check MLG OVHT FAIL
caution message on.
Release switch and check that
caution message goes out.
B. Brakes and Anti-Skid System – Before Each Flight
Check the wheel brake and anti-skid systems as follows:
(1) PARKING BRAKE ................................................Select to off.
Check PARKING BRAKE ON
advisory message out.
(2) ANTI-SKID, ARMED switch..................................Select to ARMED.
(3) ANTI-SKID, TEST switch .....................................Select to TEST momentarily, and
check A/SKID IN TEST
advisory message on.
After approximately
6 seconds, check A/SKID IN
TEST advisory message out.
NOTE
Anti-skid system is inoperative if the A/SKID IN TEST advisory
message does not come on during test.
Anti-skid system is inoperative if A/SKID INBD or A/SKID OUTBD
caution messages come on during test.
(4) PARKING BRAKE ................................................Select to on.
Check PARKING BRAKE ON
advisory message on.
NORMAL PROCEDURES
Landing Gear, Wheels and Brakes
04−15−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. LANDING GEAR, WHEELS AND BRAKES (CONT'D)
C. Brakes and Anti-Skid System – Before Landing
Check the wheel brake and anti-skid systems as follows:
(1) LDG GEAR lever ..................................................Select to DN, and check for proper
indication.
(2) ANTI-SKID, ARMED switch..................................Check selected to ARMED.
(3) ANTI-SKID, TEST switch .....................................Select to TEST momentarily, and
check A/SKID IN TEST
advisory message on.
After approximately 3
seconds, check A/SKID IN
TEST advisory message out.
NOTE
Anti-skid system is inoperative if the A/SKID IN TEST advisory
message does not come on during test.
Anti-skid system is inoperative if A/SKID INBD or A/SKID OUTBD
caution messages come on during test.
(4) NOSE STEER switch ...........................................Check selected to ARMED.
NOTE
When the nose wheel steering system is armed in flight, the tiller
should be centered.
NORMAL PROCEDURES
Landing Gear, Wheels and Brakes
04−15−2
REV 66, Feb 01/07
　
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