description of electrical system of Airbus A-320

1. A320 ELECTRICAL SYSTEM

2. GENERAL DESCRIPTION

3. NORMAL CONFIGURATION

4. On ground when only ground services are required external power can supply the
AC and DC GND /FLT BUSES directly without supply the entire aircraft network.
Personal select this configuration with the MAINT BUS switch in the forward
entrance area

6. FAILURE OF ONE ENGINE GENERATOR

7. FAILURE OF AC BUS 1

8. FAILURE OF TR1

9. FAILURE OF TR2

10. FLIGHT WITH BATERIES ONLY

11. ON GROUND ,BATTERIES(speed<50KT)