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MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
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TMUELAX01 LEVEL 3
EFFECTIVITY 24-24-00 Page 14
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 244
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24 - ELECTRICAL POWER
24-28-00 AC GENERATION - STATIC INVERTER
D/O
CONTENTS:
General
Emergency Configuration (V above 100 Kts)
Emergency Configuration (V between 50 and 100 Kts)
Emergency Configuration (V below 50 Kts)
Monitoring
Test
Self Examination
TMUELBC01 LEVEL 3
EFFECTIVITY 24-28-00 Page 1
Jun 30/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 245
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AC GENERATION - STATIC INVERTER D/O
GENERAL
A Static Inverter transforms the direct current from
battery 1 into a single phase alternating current.
The Static Inverter characteristics are:
- 1 KVA nominal power.
- 115V, 400Hz, single phase.
The Static Inverter is used in the following cases:
- APU start (supply of fuel pump).
- Ram Air Turbine deployment.
- Engine start on battery (ignition).
- Emergency configuration.
TMUELBC01-T01 LEVEL 3
EFFECTIVITY 24-28-00 Page 2
Jun 30/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 246
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AC GENERATION - STATIC INVERTER D/O - GENERAL
TMUELBC01-P01 LEVEL 3
EFFECTIVITY 24-28-00 Page 3
Jun 30/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 247
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AC GENERATION - STATIC INVERTER D/O
EMERGENCY CONFIGURATION (V above 100 Kts)
In this configuration the Constant Speed
Motor/Generator supplies the AC ESSential Bus and DC
ESSential Bus through the Essential Rectifier unit.
The Static Inverter is not electrically supplied.
TMUELBC01-T02 LEVEL 3
EFFECTIVITY 24-28-00 Page 4
Jun 30/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 248
ALL
AC GENERATION - STATIC INVERTER D/O - EMERGENCY CONFIGURATION (V above 100 Kts)
TMUELBC01-P02 LEVEL 3
EFFECTIVITY 24-28-00 Page 5
Jun 30/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 249
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AC GENERATION - STATIC INVERTER D/O
EMERGENCY CONFIGURATION (V between 50 and 100 Kts)
In this configuration the Emergency Generator is no
longer connected to the aircraft network. The AC
ESSential Bus is supplied by the Static Inverter which
is supplied from battery 1.
On the other hand, the DC ESSential Bus is directly
supplied by battery 2.
The AC STATIC Inverter Bus is also supplied by the
Static Inverter. This bus is used for the APU fuel
pump supply.
The DC and AC SHED ESSential Buses (circuits PH and
XH) are no longer supplied.
TMUELBC01-T03 LEVEL 3
EFFECTIVITY 24-28-00 Page 6
Jun 30/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 250
ALL
AC GENERATION - STATIC INVERTER D/O - EMERGENCY CONFIGURATION (V between 50 and 100 Kts)
TMUELBC01-P03 LEVEL 3
EFFECTIVITY 24-28-00 Page 7
Jun 30/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 251
ALL
AC GENERATION - STATIC INVERTER D/O
EMERGENCY CONFIGURATION (V below 50 Kts)
In this configuration the AC ESSential Bus is no longer
connected to the Static Inverter.
The DC ESS Bus and the AC STATIC INVerter Bus remain
supplied.
TMUELBC01-T04 LEVEL 3
EFFECTIVITY 24-28-00 Page 8
Jun 30/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 252
ALL
AC GENERATION - STATIC INVERTER D/O - EMERGENCY CONFIGURATION (V below 50 Kts)
TMUELBC01-P04 LEVEL 3
EFFECTIVITY 24-28-00 Page 9
Jun 30/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 253
ALL
AC GENERATION - STATIC INVERTER D/O
　
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