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FAN COM 3
LIGHTNING
DET
CFO0106002_004
3 3 3 3
3 3 3 3 3 3 15
3
3
5 25 5
7.5 3 5 5 5 3 7.5 5
10 10 3 3
LBATT
SEC BUS
20
NORM
OFF
L GEN
COMM
R AUDIO
PWR 2
3
3
OXYGEN
3 3
NAV
ELT/
AUTO DEP
THERAPTC
RAM AIR/
OFV PWR2
L FOOT
WARM PWR CTRL
REV 2
AIRPLANE GENERAL
May 06/2005 Flight Crew Operating Manual Volume 2
REV 2 CSP 100-6 01-04-11
CIRCUIT BREAKER PANELS (Cont)
CB 4 LEFT SIDE EQUIPMENT RACK CIRCUIT BREAKER PANEL (TYPICAL)
A
C
B
D
E
F
CFO0106002_003
9 8 7 6 5 4 3 2 1
TR OUTBD
WHL SPD
ENG RUN
CH B
SYNC/
IGN B
ENG
START B
ENGINE
NORM
ELEC
R ENG
SOV
XFER
QTY 2 VALVE
FUEL
R FORCE
SENSOR
PEDAL
TRIM AUTO FLT ADJ
MSTR DISC
FLIGHT CONTROL
LIGHTS CABIN
BUS
CTRL
PWR
1
PWR
2
INDICATING/RECORDING
3 3 3 3
3 3 5 3 3 3 3
3
5
5 3 10 10 50 50
NORM
20
HYD GEN
R BATT APU GEN R GEN
SEC BUS
3 7.5
PWR/
TEST HTR
3 0.5
ENVIRONMENTAL
CTRL PWR
R SIDE WINDOW
ANTI ICE
5 25 5 3 5 5
NOSE GEAR WING
STROBE
R CKPT
NAV LOGO LDG TAXI CABIN /CBP
NAV
7.5 5 10 10 5 5 3
PRI
SEC
3rd AUDIO SATCOM OXYGEN
/IND
LAV SMK MAN DEP
DET
DRN
MAST HTR
RAM AIR/
OFV PWR1
R FOOT
WARM
R PFD
HTR
R MFD
HTR
PAX
ADDRESS
COMPASS
LIGHT
COMM
15 3
FLT
PHONE
L AUDIO
PWR2
OFF OFF
V 2
AIRPLANE GENERAL
Volume 2 Flight Crew Operating Manual May 06/2005
01-04-12 CSP 100-6 REV 2
CIRCUIT BREAKER PANELS (Cont)
CB 5 LEFT DC POWER CENTER CIRCUIT BREAKER PANEL (TYPICAL)
CB 6 RIGHT DC POWER CENTER CIRCUIT BREAKER PANEL (TYPICAL)
2 8 7 6 5 43
A
C
B
2 1
HF 1
PWR
L ATS/
A HYD SOL
PRI STAB
L LDG MOTOR
L DCPC
ESS BUS
L SPC
BAT BUS
R DCPC
ESS BUS
LIGHTS FCTL FIREX ENGINE AVNX
ELECTRICAL
EXT BAG/
AFT BAY
5 5 25 5 3 3
25 5 7.5
CFO0106002_002
FAN
PWR 1
AVNX
35
PWR 2
GROUND SERVICE
PWR 1
25 25
ELECT
5
EDC
PWR
HF 2
PWR
R ATS/
HYD SOL B
SEC STAB
MOTOR R LDG
L DCPC
ESS BUS
R SPC
BATT BUS CTRL VALVES
R DCPC
ESS BUS
AVIONICS ENGINE FIREX FCTL LIGHTS
ELECTRICAL REFUEL DEFUEL
1 2 3 4 5 6 8
A
C
B
1 2
3 5 5 5 25 5
5 7.5 25 3 3
CFO0106002_001
7
SATCOM
CTRL
PWR 1 PWR 2
ENVIRONMENT
15 15
BAG COMP HTR
FAN
PWR 2
AVNX
35
V 2
AIRPLANE GENERAL
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 01-04-13
CONTROL WHEEL
The pilot and copilot control wheels contain the following switches:
- Autopilot synchronization switch
- Checklist line advance switch
- Transponder identification switch
- Microphone key switch
- Master disconnect switch
- Pitch and roll trim switch
AUTOPILOT SYNCHRONIZATION SWITCH
The autopilot synchronization switch enables the pilot to maneuver the airplane without disconnecting the autopilot.
CHECKLIST LINE ADVANCE SWITCH
The checklist line advance switch enables the pilot to advance the electronic checklist on the MFD.
TRANSPONDER IDENTIFICATION SWITCH
The transponder switch activates the transponder IDENT function.
MICROPHONE SWITCH
The microphone switch activates the selected radio transmitter when pulled outboard and the interphone when pushed inboard.
MASTER DISCONNECT SWITCH
The master disconnect switch disengages the autopilot, and deactivates the pitch trim and stall pusher. The stall pusher is
not deactivated on JAA approved aircraft. When released, the pitch trim system and pusher are immediately reactivated but
the autopilot remains disengaged.
PITCH/ROLL TRIM SWITCH
The pitch and roll trim switch enables the pilot/copilot to control the trim from each control wheel.
CFO0101002_009
MASTER
DISCONNECT
SWITCH
TRIM SWITCH
DOUBLE ACTING
PITCH/ROLL AND
TRIM ARMING
AUTOPILOT
SYNCHRONIZATION
SWITCH
CHECKLIST LINE
ADVANCE SWITCH
　
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本文鏈接地址：Bombardier 300 airplane general(6)