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庞巴迪挑战者300公务机机组操作手册 Bombardier Challenger-电源(9)

时间:2011-11-12 05:57来源:蓝天飞行翻译 作者:公务机
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FLT
FUEL
A/ICE
ECS
ELEC
HYD
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
07-01-15
ELECTRICAL

CONTROLS AND INDICATIONS (Cont) ELECTRICAL CONTROL PANEL

With optional Hydraulic Motor Driven Generator (HMDG) system.

CFO0701002_003 CFO0701002_010
Volume 2 Flight Crew Operating Manual May 06/2005 CSP 100-6 REV 2
07-01-16

ELECTRICAL
CONTROLS AND INDICATIONS (Cont) ELECTRICAL SYNOPTIC PAGE

 

Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
07-01-17

ELECTRICAL
EICAS MESSAGES
The electrical system messages are shown on the EICAS. In the table below is a list of the electrical system messages, inhibits, and aural warnings. A brief explanation of each message is provided.
MESSAGE  INHIBITS  MEANING  AURAL WARNING 
L (R) BATT OVERHEAT  TO/LAND  Respective battery internal temperature exceeded 70 ° C 
ESSENTIAL POWER ONLY  The essential buses are powered by the batter-ies only. AUX and MAIN buses are automati-cally deactivated in flight 
APU GEN FAIL  TO/LAND  The APU generator failed 
APU GEN OVERLOAD  TO/LAND  The APU generator has exceeded 500 amp 
L (R) BATT FAIL  TO/LAND  Either the respective battery contactor failed 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 failure has occurred that prevents display of electrical indications 
L (R) GEN FAIL  TO/LAND  The affected generator has failed. If the APU generators not on line, the BUS-TIE will auto-matically close and, in-flight, the auxiliary buses will not be powered 
L (R) ESS BUS FAIL  TO/LAND  Affected bus is not powered 
L (R) GEN OVERLOAD  TO/LAND  Respective generator load exceeded 500 amp 
L (R) MAIN BUS FAIL  TO/LAND  The affected MAIN bus is not powered 
L (R) AUX BUS FAIL  TO/LAND  The affected auxiliary BUS is not powered with a power source available 
L (R) AUX BUS OFF  TO/LAND  Respective AUX BUS is selected off 
ELECTRICAL FAULT  TO/LAND  An electrical system fault occurred, resulting in loss of redundancy in the display of electrical indications 

Volume 2 Flight Crew Operating Manual Sep 14/2005 CSP 100-6 REV 4
07-01-18

ELECTRICAL
MESSAGE  INHIBITS  MEANING  AURAL WARNING 
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 
 
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