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ELECTRICAL

Sep 14/2005

Flight Crew Operating Manual

Volume 2

REV 4

CSP 100-6

07-01-19

STBY INST BATT 

FAULT

TO/LAND

At least one of the following has occurred:

Standby instrument heater is inoperative

- Standby instrument battery charger is inopera-

tive

- Standby instrument battery temperature is

greater than 80 

°

C

- At least two cells of the standby instrument

battery have failed

APU GEN OFF

APU GEN switch has been selected OFF

L (R) BATT OFF

The affected battery has been selected OFF

BUS TIE MAN OPEN

The bus tie has been manually selected open. 
This prevents automatic operation of the bus 
tie. Pressing the BUS TIE switch a second time 
restores automatic control

ELEC HYD GEN ON

The optional hydraulic motor driven generator 
(HMDG) has been activated

L (R) GEN OFF

The affected engine generator switch has been 
selected OFF

MESSAGE

INHIBITS

MEANING

AURAL 

WARNING

REV 4

Summary of Contents for Challenger 300

Page 1: ...Pilot Circuit Breaker Panel Typical 07 01 07 CB 2 Copilot Circuit Breaker Panel Typical 07 01 08 CB 3 Left Side Equipment Rack Circuit Breaker Panel Typical 07 01 09 CB 4 Right Side Equipment Rack Ci...

Page 2: ......

Page 3: ...ation A separate battery powers the independent standby instrument system An optional hydraulically driven electrical generator is available to provide electrical power generation in the event all eng...

Page 4: ...INTRODUCTION Cont RIGHT CIRCUIT BREAKER PANEL RIGHT SECONDARY POWER CENTER LEFT CIRCUIT BREAKER PANEL LEFT SECONDARY POWER CENTER RIGHT DC POWER CENTER RIGHT BATTERY LEFT GENERATOR APU GENERATOR EXTER...

Page 5: ...y are fed by the distribution buses of the secondary distri bution centers and distribute electrical power to loads which require pilot access to the associated circuit breaker The electrical system i...

Page 6: ...cation of amps drawn from the GPU is provided With the external power cable connected the following indications are annunciated on the ELECTRICAL synoptic display EXT PWR symbol and line are white whe...

Page 7: ...ment for a limited duration Standby Instrument power is supplied by a dedicated 24 vdc battery The standby instrument is activated by a separate STBY INST switch located on the ELECTRICAL power panel...

Page 8: ...LECTRICAL cockpit control panel CIRCUIT BREAKER PANELS Two circuit breaker panels are located in the cockpit and are fed by the distribution buses of the secondary power centers They distribute power...

Page 9: ...D L DCP L PFD ATT HDG 1 AIR DATA 1 DISPLAYS INDICATING RECORDING L BLEED VALVES PRESS 1 PACK ENVIRONMENTAL DCU A RDC A CTRL 1 L PWR 1 R PWR 2 ANNUNCIATOR L PITOT TAT VANE CASE CTRL PWR L ENG INDICATIN...

Page 10: ...WR 2 L DC PUMP PTU R SOV R IND LDG GEAR HYDRAULIC DISPLAYS INDICATING RECORDING FDR L PWR 2 R PWR 1 CTRL 2 RDC B DCU B ANNUNCIATOR EMER DOME LIGHTS R ENG R WING BLD LK PWR CTRL R ICE DET CASE VANE R S...

Page 11: ...NGINE ELEC L ENG SOV GRAVITY X FLOW QTY 1 FUEL FLIGHT CONTROL PAX DOOR ENVIRONMENT L SIDE WINDOW ANTI ICE L FORCE SNSR MSTR DISC AUTO FLT TRIM ENTRY LIGHTS L CKPT PED CABIN SIGNS WING INSP MAP STOW BC...

Page 12: ...DJ AUTO FLT TRIM MSTR DISC FLIGHT CONTROL CABIN LIGHTS BUS CTRL PWR 1 PWR 2 INDICATING RECORDING 3 3 3 3 3 3 3 3 5 3 3 3 5 50 50 10 3 5 10 NORM 20 HYD GEN APU GEN R GEN R BATT SEC BUS 7 5 3 PWR TEST H...

Page 13: ...BUS L SPC BAT BUS R DCPC ESS BUS AVNX ENGINE FIREX FCTL LIGHTS ELECTRICAL EXT BAG AFT BAY 5 5 25 5 3 3 7 5 25 5 CFO0106002_002 FAN PWR 1 AVNX 35 PWR 2 GROUND SERVICE PWR 1 25 25 ELECT 5 EDC PWR HF 2 P...

Page 14: ...L BATT BUS CBP R ESS BUS CBP R MAIN BUS CBP R BATT BUS CBP CB2 C6 STBY INST R ESS BUS SPC R MAIN BUS SPC R AUX BUS SPC R BATT BUS SPC R BATT BUS DCPC R ESS BUS DCPC R MAIN BUS DCPC R AUX BUS DCPC L SE...

Page 15: ...U APU STRT RIGHT GEN LEFT AUX BUS LEFT MAIN BUS LEFT ESS BUS RIGHT ESS BUS RIGHT MAIN BUS RIGHT AUX BUS LBAT BUS RBAT BUS R BATT OFF R GEN OFF L GEN OFF CAGE STD B R T D I M BARO 240 220 200 180 M 47...

Page 16: ...ght Crew Operating Manual May 06 2005 07 01 14 CSP 100 6 REV 2 CONTROLS AND INDICATIONS EXTERNAL POWER CONTROL PANEL CFO0501002_006 EXTERNAL POWER CONTROL PANEL ON Gnd Service EXT DC AVAIL IN USE APU...

Page 17: ...t Crew Operating Manual Volume 2 REV 1 CSP 100 6 07 01 15 CONTROLS AND INDICATIONS Cont ELECTRICAL SUMMARY PAGE CFO0701002_009 CAS CKLST SKIP FRMT TFC TR WX ENTER A ICE FLT FUEL HYD L R ECS AUTO PLAN...

Page 18: ...Motor Driven Generator HMDG system CFO0701002_010 EXT PWR L BATT R BATT OFF AVAIL ON ELECTRICAL OFF OFF OFF ON BUS TIE L GEN APU GEN R GEN R ESS R MAIN R AUX L ESS L AUX L MAIN STBY INST OFF CFO07010...

Page 19: ...TRIM V T 600 600 93 0 61 0 NI MACH HOLD ITT N2 OIL PRESS OIL TEMP FF PPH 84 7 46 115 7300 84 7 46 115 7300 APU RPM 100 250 APU EGT FUEL QTY LBS TOTAL 12000 6000 6000 S T A R T S T A R T STAB AIL LWD...

Page 20: ...d or the battery has been automatically discon nected for overheat protection ELEC HYD GEN FAIL TO LAND The hydraulic generator has failed to come on line ELECTRICAL FAULT TO LAND An electrical system...

Page 21: ...f the standby instrument battery have failed APU GEN OFF APU GEN switch has been selected OFF L R BATT OFF The affected battery has been selected OFF BUS TIE MAN OPEN The bus tie has been manually sel...

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