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L ENG SOV CLSD Fuel shutoff valve is closed after activation of the respective ENG FIRE PUSH
R ENG SOV CLSD switch/light.
IGNITION A ’A’ igniters are activated, ’B’ igniters off.
IGNITION A/B Both ’A’ and B’ igniters are activated.
IGNITION B ’B’ igniters are activated, ’A’ igniters off.
L REV ARMED
The respective thrust reverser is armed.
R REV ARMED
DCU 1 APR FAIL
The respective DCU has failed its APR test.
DCU 2 APR FAIL
L ENG ECU FAIL
The respective engine ECU failed to respond to an APR test.
R ENG ECU FAIL
POWER PLANT
Description
Vol. 2 19−10−31
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
POWER PLANT
Description
Vol. 2 19−10−32
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
THIS PAGE INTENTIONALLY LEFT BLANK
POWER SUPPLY AND CIRCUIT BREAKER SUMMARY
SYSTEM SUB−SYSTEM CB NAME BUS BAR
CB
PANEL
CB LOCATION NOTES
Power Plant Ignition System ENG IGN A AC ESS 3 C7
ENG IGN A DC BATT 1 L7
ENG IGN B DC BATT 1 L8
ENG IGN B BATT BUS 5 A1
Starter System ENG START L DC BATT 1 L10
ENG START R DC BATT 1 L9
Oil Pressure
Indications
L OIL PRESS
TRANS
DC BATT 1 L6
R OIL PRESS
TRANS
DC ESS 4 B6
OIL BYPASS IND DC APU
BATT
DIRECT
5 B3
ENG OIL POWER DC APU
BATT
DIRECT
5 B4
Vibration Monitor ENG VIB MON AC BUS 1 1 C7
Thrust Reversers THRUST REV
AUTO STOW 1
DC ESS 4 A4
THRUST REV
AUTO STOW 2
DC ESS 4 A5
THRUST REV 1 DC ESS 4 A6
THRUST REV 2 DC ESS 4 A7
Automatic
Performance
Reserve
APR
DC BATT 5 A2
POWER PLANT
Summary
Vol. 2 19−20−1
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
POWER PLANT
Summary
Vol. 2 19−20−2
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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