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model 2B16, variant CL-604 Challenger airplane. These checks address foreseeable situations,
usually involving a failure condition, in which the use of the normal or alternate systems can be
expected to maintain an acceptable level of airworthiness.
In addition to the failure indications referenced in the following abnormal procedures, the master
caution system operates where applicable.
Unless otherwise specified in these abnormal procedures, the landing configuration of the
airplane will be landing gear down and flaps 45.
These procedures have been developed and recommended by Bombardier and approved by
Transport Canada for use in the operation of the CL-604 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.
ABNORMAL PROCEDURES
Introduction
Vol. 1 05−01−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
ABNORMAL PROCEDURES
Introduction
Vol. 1 05−01−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
THIS PAGE INTENTIONALLY LEFT BLANK
1. POWER PLANT
A. Reverser Unsafe to Arm
Indication: L (R) REV UNSAFE caution message.
CAUTION
Do not arm affected thrust reverser during flight.
(1) Affected THRUST REVERSER
ARM switch .............................................................OFF L (R) REV ARMED advisory
message out.
CAUTION
Use remaining thrust reverser carefully upon landing.
END
B. In-Flight Engine Failure/Shutdown
Accomplish an engine shutdown only when flight conditions permit.
Shut down the engine if any of the following malfunction symptoms/indications occur:
• Excessive or uncontrollable power changes, or
• Indications outside the engine operating limitations, or
• Unsuccessful restart attempts after an unexplained flameout, or
• Any other condition that indicates advisability of engine shutdown.
(1) Affected engine, thrust lever.............. Confirm and IDLE
(2) Affected engine, thrust lever............ Confirm and SHUT
OFF
(3) FUEL, TAIL TANK TRANSFER,
MANUAL OVRD switch/light ...........................Press out if MANUAL light on, and if
rotor burst is suspected.
Anti-ice system is on:
Yes
(4) BLEED AIR, 14TH STAGE
ISOL switch/light........................................Press in to open 14th stage isolation
valve.
Check ISOL OPEN light on.
(5) ANTI-ICE, COWL L (R)
switch/light ...............................................Press out to select applicable cowl
anti-ice off.
No
ABNORMAL PROCEDURES
Power Plant
Vol. 1 05−02−1
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
B. In-Flight Engine Failure/Shutdown (Cont’d)
HYD 1 (2) HI TEMP caution message is out:
Yes
(4) HYDRAULIC pump switch............................Select applicable pump to ON.
• If left engine shut down,
turn 1B ON. Check that HYD
1 LO PRESS caution
message out.
• If right engine shut down,
turn 2B ON. Check that HYD
2 LO PRESS caution
message out.
No
(4) AIR-CONDITIONING,
L (R) PACK switch/light ...................................Press out to shutdown affected pack.
Check L (R) PACK OFF light
on.
(5) BLEED AIR, 10TH STAGE
L (R) switch/light ..............................................Press out to close affected shut-off
valve.
Check L (R) CLOSED light on.
NOTE
Use only one air-conditioning pack during single engine
operations, when the operating engine is the only 10th-stage
bleed source.
(6) AC POWER, GEN 1 (2) switch.............................Select affected generator to OFF.
Check GEN 1 (2) OFF caution
message on.
(7) APU (if available).................................................... Start when at or below 20,000 feet.
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006 or
604–49–009:
(7) APU (if available).................................................... Start when at or below 15,000 feet.
ABNORMAL PROCEDURES
Power Plant
Vol. 1 05−02−2
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
B. In-Flight Engine Failure/Shutdown (Cont’d)
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006 or
　
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