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APU Generator Overload 05−09−4
Battery Bus Failure 05−09−4
DC BUS 1 Failure 05−09−5
DC BUS 2 Failure 05−09−5
DC Essential Bus Failure 05−09−5
AC Generator 1 Failure 05−09−6
AC Generator 2 Failure 05−09−7
AC Generator Overload 05−09−7
Main Battery Failure 05−09−8
DC Emergency Bus Failure 05−09−8
FIRE PROTECTION
Fire Protection 05−10−1
APU Fire Detector Loop Failure 05−10−1
Engine Fire Detector Loop Failure 05−10−1
Jetpipe Overheat Detector Failure 05−10−1
APU Firex Bottle Discharged 05−10−1
Engine Firex Bottle Discharged 05−10−1
FLIGHT CONTROLS
Flight Controls 05−11−1
Lightning Strike 05−11−1
Stall Protection System Failure 05−11−2
ABNORMAL PROCEDURES
Table of Contents
05−00−3
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
Page
FLIGHT CONTROLS
Stall Protection System Altitude Compensation Failure 05−11−2
Flight Spoilers Deployed During Flight 05−11−3
Flight Spoilers Lever Jam 05−11−3
Flight Spoilers Failure to Deploy 05−11−3
Flight Spoiler Asymmetric Extension 05−11−3
Flight Spoiler Asymmetric Retraction 05−11−4
Flight Spoilers Failure 05−11−4
Flaps Failure 05−11−5
Ground Spoilers Failure 05−11−8
Ground Spoilers Unsafe 05−11−8
Ground Spoilers Deployed During Flight 05−11−10
Mach Trim Failure 05−11−10
Stabilizer Trim Failure 05−11−11
Stabilizer Trim Malfunction 05−11−14
Aileron PCU Malfunction 05−11−15
Elevator System Malfunction 05−11−16
FUEL
Fuel 05−12−1
Fuel Imbalance 05−12−1
Engine Shut-Off Valve Failed Closed 05−12−3
Engine Shut-Off Valve Failed to Close After Engine Shutdown Due to Fire 05−12−3
Fuel Filter Impending Bypass 05−12−3
Low Fuel Pressure 05−12−4
Bulk Fuel Temperature is Less than –37°C 05−12−5
Fuel Temperature Less than 5°C 05−12−6
Fuel Boost Pump Failure 05−12−6
Motive Flow Failure 05−12−7
Scavenge Ejector Failure 05−12−8
Primary Tail Tank Pump Failure (Manual Mode) 05−12−9
Secondary Tail Tank Pump Failure (Manual Mode) 05−12−10
Tail Tank to Aux Tank Automatic Transfer Failure 05−12−11
Tail Tank Transfer is Inhibited 05−12−12
Excessive Fuel Load – Aux Tank 05−12−13
ABNORMAL PROCEDURES
Table of Contents
05−00−4
REV 77, Oct 20/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
Page
FUEL
Excessive Fuel Load – Tail Tank 05−12−14
Tail Dump SOV Failed (SOV not in commanded position) 05−12−16
Tail Transfer SOV Failed Closed 05−12−16
Tail Transfer SOV Failed Open 05−12−18
Tail Transfer SOV Failed in Middle Position 05−12−19
L/R TO AUX Crossflow Valve Open 05−12−20
L/R TO AUX Crossflow Valve Fails to Close 05−12−20
Auxiliary Tank Contents Increasing (abnormally) During L/R TO AUX
Crossflow 05−12−21
Dump Valve Open for More than 5 Minutes 05−12−21
Loss of Auxiliary Tank Fuel Quantity Indication 05−12−22
Loss of Wing Tank Fuel Quantity Indication 05−12−23
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
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 1(124)
