飞行翻译_公务机_公务航空_Business Jet_Business Aviation

PNEUMATIC SUPPLY (CONT'D) Bleed Air Indication
APU bleed air indication is displayed on the EICAS page below the CABIN information section.

APU Pneumatic Supply
Figure 05.10.11

CONTROLS AND INDICATORS
The APU panel provides the control for the APU operation, and the EICAS page provides a visual display of APU indications. The APU fault panel supplements the EICAS for specific APU faults.
The APU panel has two switch/lights:
.
PWR FUEL; Activates the ECU, which commands fuel valves and pump operation.

.
START/STOP; Commands APU start and shutdown modes of operation.

 AUXILIARY POWER UNIT Description  Vol. 2  05.10.22 
Oct 05/06 

APU monitoring is provided by RPM and EGT digital readout on the EICAS page. The APU indications are activated when the PWR FUEL switch/light is pressed in, and are removed 60 seconds after selecting the PWR FUEL switch/light out.

APU Panel and EICAS Indications
Figure 05.10.12

 AUXILIARY POWER UNIT Description  Vol. 2  05.10.23 
Oct 05/06 

EICAS and Synoptic Page Color Coding
Figure 05.10.13

 AUXILIARY POWER UNIT Description  Vol. 2  05.10.24 
Oct 05/06 

CL.605 Flight Crew Operating Manual
PSP 605.6

 AUXILIARY POWER UNIT Summary  Vol. 2  05.20.1 
Oct 05/06 

CB

SYSTEM
SUB-SYSTEM CB NAME BUS BAR CB LOCATION NOTES
PANEL
Auxiliary Power
APU Electronic APU ECU PRIM DC BATT 5 A4
Unit Control Unit B9
APU Fault DC BATT
APU FAULT ANN 1 L2
Annunciation APU Start L3 Fuel APU FUEL PUMP DC BATT 2 P4 Control APU CONTROL
DC BATT 1 L1

CL.605 Flight Crew Operating Manual
PSP 605.6

 AUXILIARY POWER UNIT Summary  Vol. 2  05.20.2 
Oct 05/06 

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CL.605 Flight Crew Operating Manual
PSP 605.6