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(17) Descent and approach ............................................Plan
NOTE
Recommended approach is a descending 360° turn starting at
5,000 feet above the landing area.
EMERGENCY PROCEDURES
Power Plant
Vol. 1 03−03−10
REV 76, Jul 17/09
▼
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
C. Double Engine Failure (Cont’d)
APU GEN available:
Yes
(18) ADG, PWR TXFR
OVERRIDE switch.........................................Press to override.
No
The following significant systems are not available when on emergency power only:
• Yaw damper 2 and AFCS 2
• Flaps, ground spoilers
• Stabilizer trim channel 1
• Mach trim, aileron and rudder trim
• Hydraulic pumps 1B, 2B & 3A
• DME, FMS 2, GPS
On airplanes 5301 to 5386 not incorporating SB 604−24−002:
• FMS 1
• Copilot’s PFD, MFD, navigation & communication systems
• R Pack
• Right probe heaters, AOA vane heater and ice detector
• Nose wheel steering system, anti-skid system
• Both windshield heaters, right window heater
• Copilot’s instrument lights, NAV lights, and L & R landing lights
• SPS altitude compensation
At 10,000 feet MSL or lowest safe altitude:
(18) AIR-CONDITIONING,
RAM-AIR switch/light.........................................Press in to open ram air valve.
Check RAM AIR OPEN light
on.
(19) GPWS/FLAP OVRD switch
(if installed) ...........................................................Select to OVRD (to mute flap aural
warning).
(20) Approach start point ........................................ Establish at 5,000 feet AGL over landing
area.
(21) Turn (20° to 30° bank angle) .................................. Start over landing area.
(22) Target airspeed ................................................ Maintain
(23) Downwind leg .................................................. Establish at 2,500 feet AGL abeam
landing area and 180° from
final approach heading.
EMERGENCY PROCEDURES
Power Plant
Vol. 1 03−03−11
REV 76, Jul 17/09
▼
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
C. Double Engine Failure (Cont’d)
(24) FLAPS (if available)..............................................Select to 20° for landing.
(25) LDG GEAR lever .......................................................DN prior to turning final.
(26) Final approach................................................. Establish at 1,500 feet AGL.
(27) Final approach speed...........................VREF (Flaps 45°)
+ ΔVREF for applicable flap setting.
(28) Actual landing distance .................................... Increase as applicable by factor given
below:
Flaps Setting
(Degrees)
Δ VREF
(KTS)
ALD Factor
APU generator available Emergency power only
0 30 1.80 (80%) 3.60 (260%)
20 14 1.55 (55%) 3.20 (220%)
When time and conditions permit:
(29) Ditching and Forced Landing
procedures ......................................................... Review Refer to DITCHING AND
FORCED LANDING
procedures in this chapter.
END
EMERGENCY PROCEDURES
Power Plant
Vol. 1 03−03−12
REV 76, Jul 17/09
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
D. Jet Pipe Overheat
Indication: L (R) JETPIPE OVHT warning message and “JETPIPE OVERHEAT” aural
on.
(1) Affected thrust lever .........................Confirm and retard slowly until warning message
goes out.
L (R) JETPIPE OVHT message persists:
Yes
(2) In-Flight Engine
Failure/Shutdown................................. Accomplish Refer to Chapter 5;
ABNORMAL PROCEDURES
– POWER PLANT – In-Flight
Engine Failure/Shutdown.
− END −
No
(2) No further action required.
END
EMERGENCY PROCEDURES
Power Plant
Vol. 1 03−03−13
REV 76, Jul 17/09
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
E. Engine Oil Pressure Low
Indication: L (R) ENG OIL PRESS warning message, “ENGINE OIL” aural on,
or left or right engine oil pressure is below 25 psi.
(1) Affected thrust lever .......................... Confirm and IDLE
(2) Affected engine oil pressure.................................Check
L (R) ENG OIL PRESS warning message is on:
Yes
Affected engine oil pressure is below 25 psi:
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庞巴迪挑战者604操作手册 Operating Manual 1(40)
