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TMUELBG02-P06 LEVEL 3
EFFECTIVITY 24-56-00 Page 13
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
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SELF EXAMINATION
In which of the following configurations is the whole
galley network shed when an overload occurs ?
- A - In flight with two IDG supply.
- B - On ground with APU supply only.
- C - On ground with EXT PWR only.
What does the GALLEY FAULT light indicate ?
- A - The AFT galley has been shed.
- B - The galleys have been shed.
- C - An overload on any generator (APU or IDG).
TMUELBG02 LEVEL 3
EFFECTIVITY 24-56-00 Page 14
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
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24 - ELECTRICAL POWER
24-56-00 AC AND DC LOAD DISTRIBUTION -
GALLEY SUPPLY COMPONENTS
CONTENTS:
Galley Supply Contactors
TMUELBH02 LEVEL 3
EFFECTIVITY 24-56-00 Page 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
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AC AND DC LOAD DISTRIBUTION - GALLEY SUPPLY COMPONENTS
GALLEY SUPPLY CONTACTORS
IDENTIFICATION
FIN: 4MC, 5MC, 6MC, 13MC, 15MC, 17MC
LOCATION
ZONE: 220
TMUELBH02-T01 LEVEL 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
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AC AND DC LOAD DISTRIBUTION - GALLEY SUPPLY COMPONENTS - GALLEY SUPPLY CONTACTORS
TMUELBH02-P01 LEVEL 3
EFFECTIVITY 24-56-00 Page 3
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THIS PAGE INTENTIONALLY LEFT BLANK
TMUELBH02 LEVEL 3
EFFECTIVITY 24-56-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
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24 - ELECTRICAL POWER
24-67-00 AC AND DC LOAD DISTRIBUTION -
REFUELING ON BATTERY
CONTENTS:
General
Ground Service Configuration
Battery Only Configuration
Self Examination
TMUELCB02 LEVEL 3
EFFECTIVITY 24-67-00 Page 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
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AC AND DC LOAD DISTRIBUTION - REFUELING ON BATTERY
GENERAL
The refueling electrical network consists of busbars
501PP and 502PP. It is supplied as soon as the refuel
door located on the fuselage below the right wing is
opened.
Two supplies are then possible:
- 28VDC service bus 601PP (supplied from normal
network or via MAINT BUS switch).
- Hot bus 701PP if no other power is
available.
TMUELCB02-T01 LEVEL 3
EFFECTIVITY 24-67-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
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AC AND DC LOAD DISTRIBUTION - REFUELING ON BATTERY - GENERAL
TMUELCB02-P01 LEVEL 3
EFFECTIVITY 24-67-00 Page 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 429
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AC AND DC LOAD DISTRIBUTION - REFUELING ON BATTERY
GROUND SERVICE CONFIGURATION
NOTE: MAINT BUS switch is set to ON.
As soon as refuel door is opened, relay 8PR is energized
by service bus 601PP via relay 5PR.
Refueling busbars 501PP and 502PP are then supplied
by service bus 601PP via relay 8PR.
NOTE: in normal supply configuration, contactor 3PX
is opened and contactor 8PN is closed.
TMUELCB02-T02 LEVEL 3
EFFECTIVITY 24-67-00 Page 4
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MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
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AC AND DC LOAD DISTRIBUTION - REFUELING ON BATTERY - GROUND SERVICE CONFIGURATION
TMUELCB02-P02 LEVEL 3
EFFECTIVITY 24-67-00 Page 5
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
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AC AND DC LOAD DISTRIBUTION - REFUELING ON BATTERY
BATTERY ONLY CONFIGURATION
　
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