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Fuel Flow Indications
Fuel flow indications are displayed for each engine immediately below the N2 arcs on the EICAS page. The normally green fuel flow indication will turn amber and display dashed lines if fuel flow exceeds 5,000 pph (2,273 kg/h), or if the input value is invalid. Fuel flow can also be viewed through FMS page selection.
FUEL SYSTEM Description Vol. 2 12.10.27
Oct 05/06
EICAS Fuel Information Display
Figure 12.10.19
Interior Optional Fuel/Defuel Panel
Figure 12.10.20
FUEL SYSTEM Description Vol. 2 12.10.28
Oct 05/06
Exterior FUEL/DEFUEL Panel
Figure 12.10.21
FUEL SYSTEM Description Vol. 2 12.10.29
Oct 05/06
EICAS Page . Fuel Readout
Figure 12.10.22
FUEL SYSTEM Description Vol. 2 12.10.30
Oct 05/06
CL.605 Flight Crew Operating Manual
PSP 605.6
FUEL SYSTEM Description Vol. 2 12.10.31
Oct 05/06
MESSAGE MEANING
With either primary and/or secondary tail tank transfer pump pressures output at an acceptable high level, the tail tank transfer SOV is not fully open.
With either primary and/or secondary tail tank transfer pump pressures low, the tail tank transfer SOV is not fully closed.
After APU fire push is activated, the fuel shutoff and negative-’G’ shutoff valves are closed.
L engine fuel SOV closed after activation of respective fire push switch/light.
R engine fuel SOV closed after activation of respective fire push switch/light.
L fuel pump on, with sufficient outlet fuel pressure.
R fuel pump on, with sufficient outlet fuel pressure.
Respective channel in the fuel system computer has failed.
Both fuel system computer (FSC) channels have degraded accuracy signal, or one FSC channel has degraded accuracy while the other channel has a data word label invalid.
Inertial reference system (IRS) is not valid for both channels of the FSCU with airplane weight off wheels.
Low fuel pressure at respective main ejectors, with respective engine running.
Primary tail xfer pump failed in auto mode. Secondary tail xfer pump failed in auto mode. Tail refuel SOV open with DC BUS 1 powered.
FUEL SYSTEM Description Vol. 2 12.10.32
Oct 05/06
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CL.605 Flight Crew Operating Manual
PSP 605.6
FUEL SYSTEM Summary Vol. 2 12.20.1
Oct 05/06
CL.605 Flight Crew Operating Manual
PSP 605.6
FUEL SYSTEM Summary Vol. 2 12.20.2
Oct 05/06
CL.605 Flight Crew Operating Manual
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本文链接地址：庞巴迪挑战者605公务机机组操作手册 CL605-燃油系统 FUEL SYSTEM(13)
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