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BUS and via ESS TR, the DC ESS BUS.
As the nose landing gear is now compressed, the AC ESS
BUS and DC ESS BUS are respectively supplied by the
STATIC INVERTER and the BATTERY 2.
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EMERGENCY GENERATION AUTOMATIC OPERATION
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EMERGENCY ELECTRICAL POWER LOGIC DESCRIPTION
EMERGENCY GENERATION MANUAL OPERATION IN FLIGHT
If AC BUS 1 and 2 are lost and the Ram Air Turbine
does not extend, FAULT light comes on red on the EMER
ELEC PWR panel.
The Ram Air Turbine must be manually extended to power
the emergency generator. This is done by pressing the
guarded MAN ON pushbutton on the emergency electrical
power panel.
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EMERGENCY GENERATION AUTOMATIC OPERATION IN FLIGHT
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EMERGENCY ELECTRICAL POWER LOGIC DESCRIPTION
EMERGENCY GENERATION MANUAL OPERATION ON GROUND
WARNING:
If the MAN ON pushbutton is pressed in, the RAT extends,
even in cold aircraft.
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EMERGENCY GENERATION MANUAL OPERATION ON GROUND
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EMERGENCY ELECTRICAL POWER LOGIC DESCRIPTION
Emergency Generator Test
The emergency generator operational test is carried
out to check the emergency generator parameters and
the corresponding network supply.
For test purposes the blue hydraulic system must be
pressurized thanks to the BLUE PUMP OVRD pushbutton
and the EMER GEN TEST pushbutton must be held pressed
in.
As the Emergency generator is connected, check the
generator parameters on the ECAM display.
TMUELE502-T04 LEVEL 1
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EMERGENCY GENERATOR TEST
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SELF EXAMINATION
After activation of the blue pump what happens
during the EMER GEN test ?
A - The Ram Air Turbine is extended.
B - The emergency generator comes on line.
C - The RAT is extended and the emergency
generator comes on line.
On ground, in a cold aircraft configuration what
does the activation of the RAT & EMER GEN MAN ON
pushbutton cause ?
A - Ram Air Turbine extension
B - Nothing
C - Emergency generator activation
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24 - ELECTRICAL POWER
24-24-00 AC GENERATION - RAM AIR TURBINE
ACTIVATION
CONTENTS:
Automatic Activation
Manual Activation
Manual Activation From Hydraulic Panel
Self Examination
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AC GENERATION - RAM AIR TURBINE ACTIVATION
AUTOMATIC ACTIVATION
In flight, when the two AC main buses are lost and
when speed is higher than 100 knots, Ram Air Turbine
solenoid 1 is energized by HOT BATTERY BUS 1 and the
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