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warnings.
Check GPWS FAIL status
message on.
(6) AUDIO WARNING switches............................DISABLE to silence DCU aural alerts.
Check DCU 1 and 2 AURAL
INOP status messages on.
If installed, check DCU 3
AURAL INOP status message
on.
EMERGENCY PROCEDURES
Landing Gear, Wheel and Brake System
03−15−5
REV 66, Feb 01/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
D. Landing Gear Up/Unsafe Landing Procedure (Cont’d)
(7) Shoulder harness ...........................................Tightened and locked.
APPROACH
(1) AIR-CONDITIONING, L and R
PACK switch/lights ..........................................Press out to shutdown both packs.
Check L and R PACK OFF
lights on.
(2) CABIN PRESSURIZATION,
PRESS CONT switch/light ................................Press in to select manual mode.
Check PRESS CONT
MANUAL light on.
(3) CABIN PRESSURIZATION, MAN
ALT selector .......................................... Select and hold to UP.
When depressurized:
(4) BLEED AIR, L and R 10TH
STAGE BLEED switch/lights ...........................Press out to close both SOVs.
Check L and R 10TH STAGE
CLOSED lights on.
(5) FLAPS ..................................................................Select to 45°.
(6) EMER LTS switch ................................................Select to ON.
Check EMER LTS ON status
message on.
(7) Brace for impact ....................................................Order over the PA system,
“BRACE–BRACE–BRACE”.
BEFORE IMPACT
(1) Airplane attitude ............................................... Maintain a nose high attitude.
(2) Ground/landing field .......................................... Contact with minimum forward speed,
but not less than stick shaker
speed, and at a minimum sink
rate.
AFTER LANDING
(1) Thrust levers.................................................SHUT OFF
EMERGENCY PROCEDURES
Landing Gear, Wheel and Brake System
03−15−6
REV 66, Feb 01/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
D. Landing Gear Up/Unsafe Landing Procedure (Cont’d)
Landing gear has collapsed or failed to extend:
Yes
(2) APU, LH and RH ENG FIRE
PUSH switch/lights (3)...............................Press in Check all three BOTTLE
ARMED PUSH TO DISCH
lights on.
Check the following advisory
messages on:
• L and R ENG SOV CLSD,
• APU SOV CLSD, and
• HYD SOV 1 and 2 CLSD.
No
Any gear extended:
Yes
(2) HYDRAULIC pump switches
3A and 3B.....................................................Select to ON, until landing gear is
secured with locking pins.
No
(2) Passenger Evacuation procedure ............... As required Refer to EMERGENCY
EVACUATION – Passenger
Evacuation in this chapter.
END
EMERGENCY PROCEDURES
Landing Gear, Wheel and Brake System
03−15−7
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
E. Main Landing Gear Bay Overheat Warning
Indication: MLG BAY OVHT warning message and “GEAR BAY OVERHEAT” aural
on.
(1) Airspeed ............................................................ Reduce to 197 KIAS.
(2) LDG GEAR lever ..................................................Select to DN.
MLG BAY OVHT warning message persists:
Yes
(3) LDG GEAR lever ....................................Leave DN
(4) Airspeed ..........................................Do not exceed
250 KIAS
(5) Land at the nearest suitable airport.
− END −
No
(3) Flight................................................................ Continue with gear down, for minimum
of 5 minutes.
(4) LDG GEAR lever ..................................................Select to UP.
END
EMERGENCY PROCEDURES
Landing Gear, Wheel and Brake System
03−15−8
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
F. Nose Door Fails Open
Indication: NOSE DOOR OPEN warning message and “NOSE DOOR” aural on.
(1) Airspeed ............................................................ Reduce to prevent structural damage
to nose gear doors, as follows:
• Flaps 0° – 181 KIAS.
　
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