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Display of Altitude Pressure and STD Baro Setting
Figure 11−10−33
Standby Attitude Indicator
The standby attitude indicator has an electrically-operated vertical gyroscope. The gyroscope is
mechanically connected to the sphere to show attitude information. To cage or uncage the
instrument, the PULL TO CAGE knob is pulled and turned. When the instrument is uncaged, the
cage knob is turned to adjust the pitch reference.
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−45
REV 73, May 14/08
CL−604 Operating Manual
PSP 604−6
STANDBY INSTRUMENTS (CONT'D)
Standby Attitude indicator
Figure 11−10−34
Standby Compass
The standby magnetic compass is a self-contained dry unit, which uses eddy current damping to
prevent overshooting. The standby compass is installed below the overhead panel.
Standby Compass
Figure 11−10−35
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−46
REV 73, May 14/08
CL−604 Operating Manual
PSP 604−6
AIRCRAFT CLOCKS
The digital clocks are located on the side panels of the pilot and copilot. The clocks can display local
time, flight time and elapsed time. Starting with A/C 5331, the clocks have been changed to add a
GMT time display.
Clock Prior to A/C 5331
Figure 11−10−36
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−47
REV 73, May 14/08
CL−604 Operating Manual
PSP 604−6
AIRCRAFT CLOCKS (CONT'D)
Clock A/C 5331 and Later
Figure 11−10−37
EICAS MESSAGES
MESSAGE MEANING
EFIS COMP MON Indicates mismatch detected between on-side and cross-side data.
EFIS COMP INOP EFIS comparator has failed.
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−48
REV 73, May 14/08
CL−604 Operating Manual
PSP 604−6
POWER SUPPLY AND CIRCUIT BREAKER SUMMARY
SYSTEM SUB-SYSTEM CB NAME BUS BAR
CB
PANEL
CB LOCATION NOTES
Standby
Instruments
Standby Instruments STBY HORIZ
DC BATT 1
Q11
Air Data Computer ADC 2 STBY P6
Pilot’s Flight Data
Primary Flight
Display
EFIS 1 PFD
DC ESS 4
C1
Multi-Function
Display
EFIS 1 MFD C2
Control Panel EFIS 1 CONT PNL C3
Air Data Computer ADC 1 C6
Airplane Clock CLOCK 1
DC BUS 2 2
K7
Copilot’s Flight
Data
Primary Flight
Display
EFIS 2 PFD L1
Multi-Function
Display
EFIS 2 MFD L2
Control Panel EFIS 2 CONT PNL L3
Air Data Computer ADC 2 K6
Airplane Clock CLOCK 2 DC ESS 4 C7
FLIGHT INSTRUMENTS
Summary
Vol. 2 11−20−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
FLIGHT INSTRUMENTS
Summary
Vol. 2 11−20−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
THIS PAGE INTENTIONALLY LEFT BLANK
DESCRIPTION
General 12−10−1
Fuel Tank System 12−10−1
Description 12−10−1
Components and Operation 12−10−1
Fuel Distribution 12−10−5
Description 12−10−5
Components and Operation 12−10−5
Fuel Transfer 12−10−10
Description 12−10−10
Components and Operation 12−10−11
Refueling/Defueling System 12−10−17
Description 12−10−17
Components and Operation 12−10−19
Controls and Indicators 12−10−26
FUEL Control Panel 12−10−26
Fuel Quantity Indicators 12−10−27
Bulk Fuel Temperature Indication 12−10−27
Engine Fuel Temperature Indications 12−10−27
Fuel Flow Indications 12−10−27
EICAS Messages 12−10−31
SUMMARY
Power Supply and Circuit Breaker Summary 12−20−1
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 12−10−1 Fuel Tank System 12−10−1
Figure 12−10−2 Water Drains Arrangement 12−10−3
Figure 12−10−3 Fuel Vent System (Manual Vent Relief Valves) 12−10−4
Figure 12−10−4 Tail Tank Relief Valve 12−10−4
Figure 12−10−5 Boost Pump Switch/Lights 12−10−5
Figure 12−10−6 Main Ejector and Ejector Operation 12−10−7
FUEL SYSTEM
Table of Contents
Vol. 2 12−00−1
REV 74, Nov 07/08
CHAPTER 12 - FUEL SYSTEM
12−00−1
CL−604 Operating Manual
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庞巴迪挑战者604操作手册 Operating Manual 4(28)
