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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
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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
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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
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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
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CL.605 Flight Crew Operating Manual
PSP 605.6
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