A battery discharge condition is indicated by the battery load indicator showing:
The buses in the DC system which can be manually tied by the crew are:
The function of the TRUs is to:
The left TRU supplies the:
The bus bar protection unit:
When external DC is selected, the aircraft’s electrical system is protected from a faulty external power unit by:
When the BATTERY MASTER switch is selected on:
When a battery temperature monitor indicates an over temperature condition: