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System No. 2 and No. 3 Failure 05−13−10
System No. 1 and No. 3 Failure 05−13−12
ABNORMAL PROCEDURES
Table of Contents
05−00−5
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
Page
ICE AND RAIN PROTECTION
Ice and Rain Protection 05−14−1
Ice Dispersal Procedure 05−14−1
Ice Detected 05−14−2
One Ice Detector Failed 05−14−3
Both Ice Detectors Failed 05−14−5
Wing Anti-Ice Sensor Failure 05−14−6
Cowl Anti-Ice Failure 05−14−7
Wing Leading Edge Temperature and Pressure Low 05−14−8
Insufficient Heat for Wing Anti-Icing 05−14−9
Probe Heater Failures 05−14−10
Windshield/Window Heat Failure 05−14−11
Windshield Outer Face Ply Failure 05−14−11
INSTRUMENTS SYSTEM
Instruments System 05−15−1
Primary Flight Display Failure 05−15−1
Display Control Panel Failure 05−15−1
EFIS Comparator Failure 05−15−1
EFIS Comparator Monitor Failures 05−15−1
Air Data Computer Failure 05−15−3
Radio Altimeter Failure 05−15−4
Inertial Reference System Failure 05−15−5
LANDING GEAR, WHEEL AND BRAKE SYSTEM
Landing Gear, Wheel and Brake System 05−16−1
Inboard Anti-Skid Failure 05−16−1
Outboard Anti-Skid Failure 05−16−2
Anti-Skid (Inboard and Outboard) Failure 05−16−2
Inboard/Outboard Brake Pressure Low 05−16−3
Parking Brake Shut-Off Valve Failure 05−16−3
Main Landing Gear Overheat Detector Failure 05−16−4
Nose Wheel Steering System Failure 05−16−4
Weight-on-Wheels Input Fault 05−16−5
Weight-on-Wheels Output Fault 05−16−6
ABNORMAL PROCEDURES
Table of Contents
05−00−6
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
Page
LANDING GEAR, WHEEL AND BRAKE SYSTEM
Proximity Sensing System Failure (Total System Shutdown) 05−16−8
Landing Gear Manual Extension 05−16−10
MISCELLANEOUS SYSTEMS
Miscellaneous Systems 05−17−1
Emergency Lighting System Selected Off 05−17−1
Crew Oxygen Low Pressure 05−17−1
Passenger Oxygen Deployed and Activated 05−17−1
Radio Tuning Unit Failure 05−17−2
Dual HF Transmission Failure 05−17−2
Flight Management System Tuning Failure 05−17−2
Flight Management System CDU/FMC Failure 05−17−3
AURAL/VISUAL WARNING SYSTEM
Aural/Visual Warning System 05−18−1
EICAS Primary Display Failure 05−18−1
EICAS Secondary Display Failure 05−18−1
EICAS Control Panel Failure 05−18−1
Data Concentrator Unit Failure 05−18−2
Data Concentrator Unit Aural Failure 05−18−2
EICAS Comparator Inoperative 05−18−2
TCAS System Failure 05−18−2
TCAS Resolution Advisory Failure 05−18−3
TCAS Traffic Advisory Failure 05−18−3
TCAS Traffic Display Failure 05−18−3
ABNORMAL PROCEDURES
Table of Contents
05−00−7
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
Page
ABNORMAL PROCEDURES
Table of Contents
05−00−8
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. GENERAL
The abnormal operating procedures included in this chapter contain items peculiar to the CL 600,
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.
　
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