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STAGE, L and R
switch/lights .....................................Press out to close shutoff valves.
Check L and R 14TH STAGE
CLOSED lights on.
If ice accumulation persists:
(9) Repeat steps (5) through (8), as required.
WARNING
Even small accumulations of ice on the wing leading
edge can change the stall speed, stall characteristics,
or the warning margins provided by the stall protection
system.
Impossible to remove ice from the wing leading edge:
Yes
Assure adequate stall margin:
(10) Maneuvering speed ........... Not less than
200 KIAS
Prior to landing:
(11) GPWS/FLAP OVRD
switch (if installed) ........................ Select to OVRD, to mute the flap
aural warning.
(12) FLAPS .......................................... Select to 20° for landing.
(13) Approach speed............VREF (Flaps 45°)
+ 27 KIAS
(14) Actual landing distance............. Increase as applicable by factor given
below:
WITHOUT THRUST
REVERSERS WITH THRUST REVERSERS
1.80 (80%) 1.70 (70%)
EMERGENCY PROCEDURES
Ice and Rain Protection
03−14−4
REV 66, Feb 01/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. ICE AND RAIN PROTECTION (CONT'D)
B. Fuselage/Wing Anti-Ice Duct Failure (Cont’d)
At 50 feet AGL:
(15) Thrust levers ...................................IDLE and do not prolong the flare.
− END −
No
(4) No further action required.
END
EMERGENCY PROCEDURES
Ice and Rain Protection
03−14−5
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
EMERGENCY PROCEDURES
Ice and Rain Protection
03−14−6
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM
A. Gear UP Disagree
Indication: GEAR DISAGREE warning message and “GEAR DISAGREE” aural on.
AND/OR
One or more landing gear (box) symbols (nose, left or right main gear)
display red hash marks (not safe), with LDG GEAR lever selected UP.
(1) Airspeed ............................................................ Reduce to not more than:
• Flaps 0° – 181 KIAS.
• Flaps 20° – 197 KIAS.
• Flaps 30° – 197 KIAS.
• Flaps 45° – 189 KIAS.
(2) HYDRAULIC pump switches 2B
and 3B ..................................................................Select to ON.
(3) LANDING GEAR MANUAL
RELEASE handle ..................................................PULL to full extension.
NOTE
The NOSE DOOR OPEN warning message may be displayed when
manual gear extension is accomplished.
(4) LDG GEAR lever ..................................................Select to DN.
(5) Landing gear indication ........................................Check for three DN indications.
Gear disagree persists:
Yes
(6) Gear DN Disagree procedure.............. Accomplish Refer to Gear DN Disagree in
this section.
− END −
No
CAUTION
Do not stow LANDING GEAR MANUAL RELEASE handle until
gear locking pins are installed.
Nose wheel steering may not be available upon landing.
(6) No further action required.
END
EMERGENCY PROCEDURES
Landing Gear, Wheel and Brake System
03−15−1
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
B. Gear DN Disagree
Indication: GEAR DISAGREE warning message and “GEAR DISAGREE” aural on.
AND/OR
One or more landing gear (box) symbols (nose, left or right main gear)
display red hash marks (not safe), with LDG GEAR lever selected DN.
(1) Airspeed ............................................................ Reduce to not more than:
• Flaps 0° – 181 KIAS.
• Flaps 20° – 197 KIAS.
• Flaps 30° – 197 KIAS.
• Flaps 45° – 189 KIAS.
(2) HYDRAULIC pump switches 2B
and 3B ..................................................................Select to ON.
(3) LANDING GEAR MANUAL
RELEASE handle ..................................................PULL to full extension.
NOTE
The NOSE DOOR OPEN warning message may be displayed when
manual gear extension is accomplished.
(4) Landing gear indication ........................................Check for three DN indications.
Gear disagree persists:
Yes
(5) HYDRAULIC pump switches
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 1(83)
