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RADIO ALTM #2 CP J-4
DADC #2 CP G-3
SYM GEN #2 CP L-3
DISPLAY UNIT #2 CP F-6
DISPLAY UNIT #6 CP J-6
IRU #2 DC CP L-5
CDU #2 CP E-7
NAV CMPTR #2 CP E-8
NAV/DME CONT #2 CP E-9
TOTAL TEMP VALVE CP M-10
R PITOT HT CONT CP M-12
W RDR CONT #2 CP G-14
STAB AUG SERVO #2 CPO B-6
FGC #2 CPO B-7
A/P SERVO #2 CPO D-8
STALL BARR VALVE #2 CPO B-12
STALL WARN CMPTR #2 CPO B-11
FLT GNDC PNL #2 CPO D-7
SPZ-8000 SHUT OFF CP L-4
COPILOT 2 PDB RIGHT DC
R WSHLD WIPER CP K-11
A/T SERVO #2 CPO D-9
STALL BARRIER #2 CPO B-9
OPERATING MANUAL
PRODUCTION AIRCRAFT SYSTEMS 2A-24-00
Page 65
May 30/02
Revision 7
Circuit Breaker Name CB Panel Location (PDB Section)
SHAKER #2 CPO B-10
PERF #2A CPO D-11
STEER BY WIRE #2 CPO D-12
NOSE COMPT COOL VLV CP L-1
BTMS CP D-10
COPILOT 3 PDB RIGHT DC
DISPLAY UNIT #4 CP H-6
DME #2 CP G-10
VHF COMM #2 CP I-9
VHF COMM CONT #2 CP I-10
ADF CONT #2 CP G-12
TDR/CAD #2 CP I-11
TDR/CAD CONT #2 CP I-12
AOA PRB HTR #2 CP M-14
IRS BATT CHGR #2 CP I-13
DISPLAY CONT #2 CP G-5
PED COOL FAN CP J-1
#2 HF MIC ADAPTER
(1000 - 1095) CP G-8
R STBY ENG INSTR CP B-11
ADF #2
(1144 & Subs CP G-11
NAV RCVR #2
(1144 & Subs CP G-9
DISPLAYS FAN #2 CP D-6
NOSE COMPT COOL FAN
(1096 & Subs) CP M-1
HF RT/CPLR #2
(1168 & Subs) CP E-12
HF CONT #2
(1168 & Subs) CP E-11
ACCESS PDB RIGHT DC
L ALT BOOST PUMP PDB RIGHT DC
R ALT BOOST PUMP PDB RIGHT DC
OPERATING MANUAL
2A-24-00 PRODUCTION AIRCRAFT SYSTEMS
Page 66
May 30/02
Revision 7
Components Powered By The Emergency Batteries
Table 13
Battery Function No. 1 Emergency Battery No. 2 Emergency Battery
Emergency
Buses
Inboard Anti-Skid Outboard Anti-Skid
No. 1 Clock No. 2 Clock
No. 1 Standby DDRMI/DBDI No. 2 Standby DDRMI/DBDI
No. 1 Comm Standby Horizon
No. 1 Comm Control Left Fuel Quantity Indicator
No. 1 Audio Right Fuel Quantity Indicator
No. 1 Transponder (TDR) and
Control Adapter (CAD)
Left Standby Engine
Instruments
Standby Mach/Airspeed
Indicator
Right Standby Engine
Instruments
Standby Altimeter Cockpit Lights Control Box
Standby Electrical Power Panel Landing Gear Position Lights
BCS Channel 1 Flap/Horizontal Stabilizer
Position Indicator
Memory Keep
Alive
No. 1 COMM No. 2 COMM
No. 1 TDR/CAD No. 2 TDR/CAD
No. 1 NAV No. 2 NAV
No. 1 DME No. 2 DME
No. 1 ADF No. 2 ADF
Note for SN 1467 and subs: When activated, the No. 3 and 4 emergency batteries
will automatically power the interior emergency lighting and main entrance door
emergency lighting (if main entrance door is open).
B. Crew Alerting System (CAS) Messages:
(1) Caution (Amber) CAS messages associated with the DC electrical
power system are:
CAS Message Possible Cause(s)
BATT 1-2 CHGR FAIL Battery or Battery Charger has failed, or input power CB is
open.
BATT ON BUS Essential DC Bus powered by batteries only.
L-R CONV FAN FAIL A converter cooling fan has failed.
L-R CONV HOT Converter temperature is above 220° F (104° C).
DC ESS ON BATT (1) Essential DC Bus powered by batteries only.
L-R DC POWER FAIL DC output from converter has dropped off line.
EPMP BATT SW OFF BATT 1 (or BATT 2) switch is selected to OFF.
TRU FAIL Transformer-rectifier unit has no output.
TRU HOT Transformer-rectifier unit temperature above 374° F (190°
C).
NOTE(S):
(1) For SPZ-8000 equipped airplanes having ASC 415 incorporated.
OPERATING MANUAL
PRODUCTION AIRCRAFT SYSTEMS 2A-24-00
Page 67
May 30/02
Revision 7
Annunciation Cause or Meaning
DC RESET light
(amber) illuminated on
EPMP.
DC Bus fault indicated.
BATT 1 or BATT 2
CHGR FAIL light
(amber) illuminated on
EPMP.
Battery or battery charger has failed, Left Main AC bus or
Right Main AC bus has failed, or input power circuit
breaker is open.
(2) Advisory (Blue) CAS messages associated with the AC electrical
power system are:
CAS Message Possible Cause(s)
BATT ON BUS (1) Battery chargers are in T/R mode (APU start or AUX pump
ON), or Essential DC bus is on battery power.
DC EXT POWER DC external power is connected to airplane.
E BATT 1-2 DISCH (2) Indicated emergency battery is discharging.
E BATT 1-2 FAIL (3) Indicated emergency battery has failed.
EXT BATT SWITCH
ON
External battery switch is ON.
　
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