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UF94200
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TMUELE802-P05 LEVEL 1
AC GENERATION - FUEL PUMPS ELECTRICAL POWER SUPPLY IN SMOKE CONFIGURATION - 3) GEN2 OFF
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24 - ELECTRICAL POWER
24-00-00 AC GENERATION - AC/DC SHEDDABLE
BUS SUPPLY
CONTENTS:
Normal Configuration
Emergency Configuration
Cabin System Shedding
TMUELBE02 LEVEL 3
EFFECTIVITY 24-00-00 Page 1
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AC GENERATION - AC/DC SHEDDABLE BUS SUPPLY
NORMAL CONFIGURATION
The AC and DC Sheddable buses are supplied by the
corresponding Essential buses.
TMUELBE02-T01 LEVEL 3
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AC GENERATION - AC/DC SHEDDABLE BUS SUPPLY - NORMAL CONFIGURATION
TMUELBE02-P01 LEVEL 3
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AC GENERATION - AC/DC SHEDDABLE BUS SUPPLY
EMERGENCY CONFIGURATION
In emergency configuration and CSM/G not available the
Static Inverter supplies the AC electrical system.
The ESS Sheddable buses are no longer supplied during
Static Inverter operation (relays 2XB and 6XB
energized).
The AC and DC sheddable buses are also disconnected
during a CSM/G operational test. (relays 16XE and 21XE
relays).
TMUELBE02-T02 LEVEL 3
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TMUELBE02-P02 LEVEL 3
AC GENERATION - AC/DC SHEDDABLE BUS SUPPLY - EMERGENCY CONFIGURATION
EFFECTIVITY 24-00-00 Page 5
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AC GENERATION - AC/DC SHEDDABLE BUS SUPPLY
CABIN SYSTEM SHEDDING
AC and DC sheddable buses are installed in panels 120VU
and 2000VU for cabin related systems.
All sheddable buses are off in single generator
operation (10XA de-energized).
Only the DC buses are shed in single TR operation (1PC2
energized).
If the GALY & CAB p/b (2XA) is released all these buses
and all galleys are shed.
TMUELBE02-T03 LEVEL 3
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TMUELBE02-P03 LEVEL 3
AC GENERATION - AC/DC SHEDDABLE BUS SUPPLY - CABIN SYSTEM SHEDDING
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24 - ELECTRICAL POWER
24-40-00 EXTERNAL POWER - GENERAL
DESCRIPTION
CONTENTS:
Normal Parameters
Abnormal Parameters
Self Examination
TMUELAY01 LEVEL 2
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EXTERNAL POWER - GENERAL DESCRIPTION
The aircraft network can be supplied by a Ground Power
Unit connected to an external receptacle located
forward of the Nose Landing Gear well.
NORMAL PARAMETERS
If the External Power parameters are correct, the
indicator lights on the external power receptacle and
the EXTERNAL POWER AVAILABLE light on the cockpit
　
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