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Automatic deploymentofthe ADGis inhibited, ontheground, whentheparkingbrake isset.
The ADGsystemcircuits canbe checkedthrough aLAMP/UNITtest switch ontheADG controlpanel. Whenthe switchis setto LAMP, agroundis suppliedto checkthatthe green TESTlightilluminates. The UNITtesthas two modes, Pre-
takeoffand Inflight:
W Pre-
takeoff, When the test switchis setto UNITthe ADGsystemcircuits are checked andthe TESTlightwillilluminate within 1second and remainONfor2seconds.
W Inflight, When the test switchis setto UNITthe ADGsystemcircuits are checked andthe TESTlightwillilluminate after 5 secondsand remain ONfor2 seconds.
Flight Crew Operating Manual MASTER
CSP A-
013
ELECTRICAL Vol. 1 07-
20-
13
AC Electrical System REV 56, Jan 31/03
TEST Light (green)
LAMP/UNIT Switch
Comes on after successful
Usedto test auto-
deploysystem.
completion of auto-
deploy
Test can onlybe accomplished with
system test.
ADG Manual Deploy Handle
Usedto manually deploy theADG.
Air Driven Generator (ADG)Figure 07---20---7
Center Pedestal
PWR TXFR OVERRIDE
UsedtotransferAC essentialbus power source from theADG bus back to the mainACbus.
Flight Crew Operating Manual MASTER
CSP A-
013
ELECTRICAL AC Electrical System Vol. 1 07-
20-
14
REV 56, Jan 31/03
F. System Circuit Breakers
SYSTEM SUB-
SYST EM CB NAME BUS BAR CB PANEL CB LOCATION NOTES
ACAC El i lEle
c
t
r
ic
a
l Power GeneratorsGenerators IDG 1 DISC DC BATTERYDC BATTERY BUSBUS 1 P9
IDG 2 DISC P10
G tGenerator C lCo
n
t
r
o
l GCU1 Q10
GCU2 Q11
GCU3 Q12
ADG D lDeploy ADG AUTO APU BATTERYAPU BATTERY DIRECT BUS 55 B10
ADG MAN B11
ADG DEPLOY AUTO DC BATTERYDC BATTERY BUS 2 N6
ADG DEPLOY MAN 2 N7
ADG DEPLOY SENS AC BUS 1 1 C10
STBY PWR CONT MAIN BATTERY DIRECT BUS 5 A7
ACAC Distribution A
C
Essential BusBus AC ESS FEED ADG BUS 3 A8
AC ESS FEED AC BUS 1 1 C2
ESS PWR CONT APU BATTERY DIRECT BUS 5 B13
ESS AC XFR CONT DC BATTERY BUS 11 Q9
AC UtilitAC Utility B 1Bu
s
1 AC UTLY BUS FEED ACUTILITY 1AC UTILITY 1 E2
PWR SENS E7
AC UTLY BUS CONT DC BUS 2 J4
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本文链接地址：庞巴迪CRJ200公务机机组操作手册 Bombardier CRJ-电源(10)
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