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off.
Check IGNITION A/B advisory
message out.
(16) Airspeed .......................................................... Establish best glide speed.
Airplane Weight Target Airspeed Rate of Descent (Flaps 0°)
20,865 KG (46,000 LB) 211 KIAS 1835 fpm
13,607 KG (30,000 LB) 173 KIAS 1600 fpm
NOTE
1. Target glide speed provides a range of approximately
2.5 NM for each 1,000 feet altitude.
2. Refer to Flight Planning and Cruise Control Manual,
Chapter 6: Special Operational Data – Descent with
Two Engines Inoperative, for detailed descent
(time/distance) performance data.
(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
03−03−10
REV 76, Jul 17/09
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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
03−03−11
REV 76, Jul 17/09
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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
03−03−12
REV 76, Jul 17/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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 −
　
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