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When connected, external DC ground power automatically supplies the APU BATT DIR BUS
through the external DC contactor, and the BATT BUS when the BATT MASTER switch is
selected ON. The DC EXTERNAL POWER white IN USE light, on the ELECTRICAL POWER
panel, illuminates whenever DC external power is connected.
External DC ground power is identified on the DC electrical synoptic page by the symbol EXT
DC. This symbol appears only if DC external power is connected to the aircraft.
ELECTRICAL
Description
Vol. 2 07−10−26
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
DC ELECTRICAL POWER SYSTEM (CONT'D)
External DC Power Connected
Figure 07−10−22
Circuit Breakers
Description
Electrical power distribution is accomplished through five circuit breaker panels. Four circuit
breaker panels are installed in the flight deck, and the fifth panel is in the aft equipment bay.
They are identified as follows:
• Circuit breaker panel 1 (CBP−1);
• Circuit breaker panel 2 (CBP−2);
• Circuit breaker panel 3 (CBP−3);
• Circuit breaker panel 4 (CBP−4); and
• Circuit breaker panel 5 (CBP−5).
ELECTRICAL
Description
Vol. 2 07−10−27
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
DC ELECTRICAL POWER SYSTEM (CONT'D)
Electrical equipment protection is provided by conventional thermal circuit breakers. When a
circuit breaker is tripped, a white collar is exposed. Depending on airplane completion
specification, circuit breakers may also be located in other parts of the airplane. Should a circuit
breaker trip while the airplane is in flight, the circuit breaker should be allowed to cool for as long
as possible before resetting.
NOTE
Do not attempt more than one reset of a circuit breaker.
ELECTRICAL
Description
Vol. 2 07−10−28
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
DC ELECTRICAL POWER SYSTEM (CONT'D)
Circuit Breaker Panels (CBPs)
Figure 07−10−23
ELECTRICAL
Description
Vol. 2 07−10−29
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
DC ELECTRICAL POWER SYSTEM (CONT'D)
Circuit Breaker Grid System
A circuit breaker can be located, when called for in a procedure, by using the grid reference on
the circuit breaker panel.
For example, the “VOLTS & FREQ IND” circuit breaker location is identified as (3A13), and
therefore found on panel CBP−3, row A, column 13.
Circuit Breaker Grid System
Figure 07−10−24
CONTROLS AND INDICATORS
The overhead ELECTRICAL POWER panel and the air-driven generator (ADG) panel provide the
system controls. The AC ELECTRICAL and DC ELECTRICAL synoptic pages provide a pictorial
representation of system status. The EICAS pages provide system caution and advisory messages
respectively. Circuit breaker panel (CBP) diagrams are also located in this section.
ELECTRICAL
Description
Vol. 2 07−10−30
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
CONTROLS AND INDICATORS (CONT'D)
AC Electrical Power
ELECTRICAL POWER Panel
Figure 07−10−25
ELECTRICAL
Description
Vol. 2 07−10−31
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
CONTROLS AND INDICATORS (CONT'D)
Air-Driven Generator (ADG)
Air-Driven Generator (ADG)
Figure 07−10−26
ELECTRICAL
Description
Vol. 2 07−10−32
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
CONTROLS AND INDICATORS (CONT'D)
DC Electrical Power
ELECTRICAL POWER Panel
Figure 07−10−27
Circuit Breaker Panels
ELECTRICAL
Description
Vol. 2 07−10−33
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ELECTRICAL
Description
Vol. 2 07−10−34
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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CONTROLS AND INDICATORS (CONT'D)
Circuit Breaker Panel 1
Figure 07−10−28
ELECTRICAL
Description
Vol. 2 07−10−35
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ELECTRICAL
Description
Vol. 2 07−10−36
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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庞巴迪挑战者605机组操作手册 CL605-ELECTRICAL(8)
