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时间:2010-09-27 07:46来源:蓝天飞行翻译 作者:admin
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Loss of Tail Tank Fuel Quantity Indication 05−12−24
Loss of Totalizer Fuel Quantity Indication 05−12−24
Fuel Leak Procedure 05−12−25
HYDRAULIC POWER
Hydraulic Power 05−13−1
System No. 1 Failure 05−13−1
System No. 2 Failure 05−13−2
System No. 3 Failure 05−13−3
System No. 1 High Temperature 05−13−4
System No. 2 High Temperature 05−13−5
System No. 3 High Temperature 05−13−6
Engine-Driven Pump Failure 05−13−6
Electric Pump 1B Failure 05−13−7
Electric Pump 2B Failure 05−13−7
Electric Pump 3A Failure 05−13−7
Electric Pump 3B Failure 05−13−8
Hydraulic Shut-Off Valve Failure After Engine Shutdown Due to Fire 05−13−8
System No. 1 and No. 2 Failure 05−13−9
System No. 2 and No. 3 Failure 05−13−10
ABNORMAL PROCEDURES
Table of Contents
Vol. 1 05−00−5
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
Page
HYDRAULIC POWER
System No. 1 and No. 3 Failure 05−13−12
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
ABNORMAL PROCEDURES
Table of Contents
Vol. 1 05−00−6
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
Page
LANDING GEAR, WHEEL AND BRAKE SYSTEM
Weight-on-Wheels Input Fault 05−16−5
Weight-on-Wheels Output Fault 05−16−6
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
Vol. 1 05−00−7
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
Page
ABNORMAL PROCEDURES
Table of Contents
Vol. 1 05−00−8
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
THIS PAGE INTENTIONALLY LEFT BLANK
1. GENERAL
The abnormal operating procedures included in this chapter contain items peculiar to the CL 600,
 
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