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(1) Thrust reverse levers................................... Lift and pull back.
When interlocks release (REV icons inside N1 gauges are green):
(2) Thrust reverse levers....................................... Pull back to required reverse thrust
setting.
When speed falls to 60 KIAS:
(3) Thrust reverse levers............................................Select to not more than 60% N1
reverse thrust or STOW.
Check REV icons (on EICAS)
go out when thrust reversers
are stowed.
CAUTION
An engine must not be shutdown until the affected thrust reverser is
confirmed stowed:
• The thrust reverse levers are at the stowed position,
• The REV icon in the N1 gauge goes out, and
• The REV UNLOCKED caution message is not displayed.
NOTE
1. Reverse thrust idle is 25 to 30% N1 .
2. Thrust reverse (piggy-back) levers must be pushed fully down in
order to do the following;
• Achieve thrust reverser stow, and
• Ensure that the main thrust lever mechanical lock is
disengaged.
NORMAL PROCEDURES
Power Plant
04−02−12
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. POWER PLANT (CONT'D)
P. Engine Shutdown
Prior to shutdown, operate the engines at IDLE for a minimum of two (2) minutes, to dissipate
heat and stabilize internal operating temperatures.
Prior to engine shutdown:
(1) Engines ............................................................Operate at IDLE for a minimum of two
(2) minutes.
NOTE
Taxi time at 70% N2 or below may be included in the 2-minute
cool down period.
(2) FUEL, L and R BOOST PUMP
switch/lights .....................................................Press out to disarm/shutdown both fuel
pumps.
Check the following:
• L and R BOOST PUMP ON
lights out.
• L and R BOOST PUMP
INOP lights on.
• L and R FUEL PUMP ON
advisory messages out.
• L and R FUEL PUMP
caution messages on.
• L and R FUEL LO PRESS
caution messages on.
After the two minute cool-down period:
CAUTION
Confirm that the thrust reversers have stowed.
(3) Thrust levers............................................................. Set to SHUT OFF.
(4) Engine instruments...............................................Check that both engines have
shutdown.
Check that N2, fuel flow and
ITT are decreasing.
NOTE
1. ITT should not exceed 350°C.
2. Due to an engine control system anomaly, an APR CMD SET
caution message may be displayed upon engine shutdown. When
this occurs, the message should be disregarded.
NORMAL PROCEDURES
Power Plant
04−02−13
REV 66, Feb 01/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. POWER PLANT (CONT'D)
P. Engine Shutdown (Cont’d)
If required:
(5) ANTI-ICE, COWL, L and R
switch/lights .....................................................Press out to select cowl anti-ice off.
Check the following:
• COWL A/ICE ON advisory
message out.
• Drop in ITT.
(6) ANTI-ICE, WING switch .......................................Select to OFF.
Check the following:
• N2 gauges indicate wing
anti-ice off.
• WING A/ICE ON advisory
message out.
NORMAL PROCEDURES
Power Plant
04−02−14
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FLIGHT COMPARTMENT AND CABIN
NOTE
1. The cabin pressurization system MAN ALT selector is a three
(3) position switch. The switch is spring loaded to mid
position/center.
2. On the first flight of the day, ensure that the L (R) PACK OFF
lights are on before the packs are selected on.
3. The cabin pressurization system must not be operated to
–1,500 feet when the system is in manual mode.
4. If above 40,000 feet, one air-conditioning unit or cowl anti-ice
must be selected on for each engine.
5. To prevent avionics overheat, ground operation of
electrical/avionics equipment is limited to 30 minutes at ambient
temperatures above 40°C (104°F), unless at least one
air-conditioning pack is selected on, and the passenger door is
closed.
A. Bleed Leak Detection Test – First Flight of the Day
Prior to selecting any bleeds, check 10th-stage and 14th-stage bleed leak detection
systems as follows:
(1) BLEED AIR, DUCT MON switch .............................. Set to TEST. Check that:
• L and R DUCT FAIL lights
(10th and 14th) are on.
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 1(94)
