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

 PNEUMATIC SYSTEM Description  Vol. 2  18.10.9 
Oct 05/06 

Bleed Air Leak Detection System Capabilities
Figure 18.10.5

 PNEUMATIC SYSTEM Description  Vol. 2  18.10.10 
Oct 05/06 

The controls (switch/lights) and the test functions for the pneumatic system are located on the BLEED AIR panel.
The systems advisory, caution and warning messages are displayed on the EICAS page. The 10th-stage bleed air pressure readouts are displayed on the EICAS SUMMARY page (see Figure 18.10.7).
BLEED AIR Panel

BLEED AIR Panel
Figure 18.10.6

 PNEUMATIC SYSTEM Description  Vol. 2  18.10.11 
Oct 05/06 

EICAS SUMMARY Page . Bleed Pressure Readouts Figure 18.10.7

EICAS MESSAGES

AURAL WARNING
MEANING (IF ANY)
Bleed air leak in the respective 10th-stage ducting. “BLEED AIR DUCT” Bleed air leak in the respective 14th-stage ducting. “BLEED AIR DUCT”
Bleed air leak in the fuselage or wing anti-ice ducting. “ANTI-ICE DUCT”
APU load control valve has failed in the open position with APU LCV interlock
activated.
Bleed air leak detection systems passed self-test.

The respective 10th-stage duct overheat loop circuit has passed self-test.

 PNEUMATIC SYSTEM Description  Vol. 2  18.10.12 
Oct 05/06 

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CL.605 Flight Crew Operating Manual
PSP 605.6

 PNEUMATIC SYSTEM Summary  Vol. 2  18.20.1 
Oct 05/06 

CL.605 Flight Crew Operating Manual
PSP 605.6

 PNEUMATIC SYSTEM Summary  Vol. 2  18.20.2 
Oct 05/06 

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CL.605 Flight Crew Operating Manual
PSP 605.6