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C. 14TH Stage, Left/Right Bleed Duct Failure
Indication: L (R) 14TH DUCT warning message and “BLEED AIR DUCT” aural on.
Affected engine:
(1) BLEED AIR, 14TH STAGE L (R)
switch/light .......................................................Press out to close bleed air valve on
affected engine.
Check L (R) 14TH STAGE
CLOSED light on.
NOTE
1. Avoid icing conditions.
2. Cowl anti-icing will not be available on the affected engine.
3. The thrust reverser is inoperative on the affected engine.
Wing anti-ice required:
Yes
(2) BLEED AIR, 14TH STAGE
ISOL switch/light........................................Press in to open 14th-stage bleed air
isolation valve.
Check 14TH ISOL OPEN light
on.
No
Warning message persists:
Yes
(2) Affected thrust lever..................................... Retard to eliminate warning.
L (R) 14TH DUCT warning message still persists:
Yes
(3) 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
Bleed Air Leaks
03−08−3
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
EMERGENCY PROCEDURES
Bleed Air Leaks
03−08−4
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. DITCHING AND FORCED LANDING
TO ENSURE A SAFE WATER LANDING: TO ENSURE A SAFE FORCED LANDING:
• Approach speed................................ VREF • Approach speed................................ VREF
• Descent rate
(if thrust available)..............200 – 300 fpm
• Descent rate
(if thrust available)..............200 – 300 fpm
• Landing gear............................. Retracted • Landing gear.......................... As required
• Flaps setting............................45 degrees • Flaps setting............................45 degrees
• IF FLAPS 45 IS NOT POSSIBLE, USE THE MOST EXTENDED FLAP SETTING
AVAILABLE.
• FINAL APPROACH SPEED:
• FLAPS 0: VREF +30 KTS
• FLAPS 20: VREF +14 KTS
• FLAPS 30: VREF +7 KTS
A. Ditching or Forced Landing Imminent
This procedure is intended for use if an immediate airplane ditching is required.
PRELIMINARY
(1) AIR-CONDITIONING, L and R
PACK switch/lights ..........................................Press out to ensure minimum
differential pressure within
airplane.
(2) CABIN PRESSURIZATION,
EMER DEPRESS switch/light ...........................Press in to drive outflow valves open.
Check EMER DEPRESS
caution message on.
JUST BEFORE CONTACT
(1) Thrust levers.................................................SHUT OFF
(2) APU, LH and RH ENG FIRE
PUSH switch/lights (3).......................................Press in 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.
(3) Water (or terrain) ............................................... Contact with minimum forward speed,
but not less than stick shaker
speed, and at minimum sink
rate.
EMERGENCY PROCEDURES
Ditching and Forced Landing
03−09−1
REV 66, Feb 01/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. DITCHING AND FORCED LANDING (CONT'D)
A. Ditching or Forced Landing Imminent (Cont’d)
AFTER CONTACT
When the airplane has stopped:
(1) BOTTLE ARMED – PUSH TO
DISCH switch/lights (3) .....................................Press in to discharge.
Check ENG BOTTLE 1 and 2
LO and APU BOTTLE LO
caution messages on.
(2) Door and overwing exit.......................................... Open
(3) Passenger evacuation......................................... Initiate
(4) BATT MASTER switch .........................................Select to OFF, to prevent CVR
erasure.
(5) Airplane ........................................................... Abandon with survival equipment.
END
EMERGENCY PROCEDURES
Ditching and Forced Landing
03−09−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. DITCHING AND FORCED LANDING (CONT'D)
B. Planned Ditching
This procedure is intended for use where sufficient time is available.
　
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