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EMERGENCY PROCEDURES
Table of Contents
Vol. 1 03−00−4
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
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1. GENERAL
Procedures given in this chapter of the Operating Manual are concerned with foreseeable but
unusual situations in which immediate and precise crew action, as indicated by the items within
the “boxed” area at the beginning of each procedure, will substantially reduce the risk of disaster.
In addition to the failure indications referenced in the following procedures, the master warning
system and appropriate switch/lights operate where applicable.
The emergency procedures contained within this chapter have been developed and
recommended by Bombardier and approved by Transport Canada for use in the operation of the
CL–604 Challenger airplane. These procedures are provided as guidance and should not be
construed as prohibiting the development of equivalent Transport Canada-approved procedures.
2. LANDING DISTANCE FACTORS
Landing distance factors are provided herein with and without the use of thrust reversers. No
operation should be predicated on the use of thrust reversers.
EMERGENCY PROCEDURES
Introduction
Vol. 1 03−01−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
EMERGENCY PROCEDURES
Introduction
Vol. 1 03−01−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
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1. REJECTED TAKE-OFF
A. Rejected Take-Off Before Achieving V1
Rejection of the take-off must be initiated no later than V1.
Simultaneously:
(1) Take-off ....................................................... Discontinue immediately.
(2) Thrust levers...........................................................IDLE
(3) Wheel brakes ........................................................Apply maximum braking, until a
safe stop on runway is
assured.
(4) FLIGHT SPOILER lever .......................................Select to MAX.
(5) Thrust reverser(s)
[operating engine(s)] .............................................Apply maximum; consistent with
directional control.
Take-off was rejected due to an engine fire or severe damage:
Yes
(6) Engine Fire/Severe Engine
Damage (On Ground)
procedure ............................................ Accomplish Refer to POWER PLANT –
Engine Fire/Severe Engine
Damage (On Ground)
procedure in this chapter.
− END −
No
Take-off was rejected due to engine failure:
(6) Thrust lever of failed engine .........................SHUT OFF
Evacuation is required:
Yes
(7) Passenger Evacuation
procedure ............................................ Accomplish Refer to EMERGENCY
EVACUATION – Passenger
Evacuation procedure in this
chapter.
− END −
No
(7) Passengers ......................................................... Advise to remain in their seats.
After a rejected take-off, procedures associated with cooling of wheels, brakes and tires must
be observed (Refer to Chapter 6; PERFORMANCE – TURN−AROUND TIME – Cooling of
Wheels, Brakes and Tires, in the Airplane Flight Manual).
END
EMERGENCY PROCEDURES
Rejected Take-Off
Vol. 1 03−02−1
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
EMERGENCY PROCEDURES
Rejected Take-Off
Vol. 1 03−02−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
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1. POWER PLANT
NOTE
In the event of a lightning strike, simultaneous fire/overheat
indications could occur. Abnormal values of secondary symptoms
may be used to determine if an actual fire exists.
A. Engine Fire/Severe Engine Damage (In Flight)
Indication: L (R) ENG FIRE PUSH light on, L (R) ENGINE FIRE warning message and
fire bell on.
At a safe altitude, affected engine:
(1) Thrust lever ....................................... Confirm and IDLE
(2) Thrust lever ................................................ Confirm and
SHUT OFF
(3) ENG FIRE PUSH switch/light............................Press in Check the following:
• BOTTLE ARMED PUSH
TO DISCH lights on,
• L (R) ENG SOV CLSD
advisory message on and
• HYD SOV 1 (2) CLSD
advisory message on.
(4) FUEL, L (R) BOOST PUMP
switch/light .......................................................Press out to disarm affected boost
pump.
Check L (R) FUEL PUMP
　
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