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31 Cards in this Set

  • Front
  • Back

What do the amber arrows mean?

The batteries are discharging

The DC generators...

... Are not connected as long as GPU is ON (EXT PWR priority)

In flight DC generator one fails...

... You expect the BTC to close automatically

In flight...

... DC bus 2 has failed

In case of a dual DC generator loss...

... An automatic switching allows the batteries to supply some DC buses

With the engines shutdown and the BAT switch off...

... The batteries remain connected to their respective HOT BAT busses

What is the function of the EMER BAT while the ENG START rotary selector is set to START or CRANK?

It provides positive power to protect critical items from power transient.


It never powers the starters.

Once the starter generator has started the engine, it switches to the generator mode when the engine speed accelerates past:

NH 61.5%

Aircraft on ground, engines running, DC EXT power available and selected ON:

DC EXT PWR has priority over ENG DC GEN

Assuming normal operation in flight, when are the DC EMER and DC ESS buses connected to DC bus 1 and/or DC bus 2?

Always through the BAT CHG connectors and respective HOT EMER or HOT MAIN BAT bus

In flight with OEI, which indication would be displayed on the shutdown engines DC GEN pushbutton?

Amber FAULT of push button is depressed (in)

With all four aircraft generator push buttons in, and EXT PWR supplying both ACW and DC, which light should be illuminated in all four generator pushbuttons?

Amber FAULT

The UND/V light illuminates amber when:

DC STBY bus voltage is less than 19.5 volts

With the engines shut down and the BAT switch on:

Allows EXT PWR operation, or a reduced DC supply

When the DC starter/generator is functioning as a starter during a battery start:

It is electrically supplied from the HOT MAIN BAT bus

Assuming normal operation in flight, how is the constant frequency AC power obtained?

From the DC buses through two inverters

In the event of thermal runaway of the MAIN BAT and the MAIN BAT CHG FAULT light illuminates (BAT CHG contactor opens) and:

The MAIN BAT supplies the HOT MAIN BAT bus and DC ESS bus is transferred to DC bus 1

Illumination of one emergency power indicator (arrow) in flight shows:

The supply of DC ESS or DC EMER bus from the corresponding HOT BAT bus

What is the function of the OVRD position for the BAT toggle switch?

Overrides all automatic operation to ensure that the buses are supplied by their respective battery

With the STBY bus OVRD push button set to OVRD, where will the DC STBY bus and AC STBY bus (via INV 1) be supplied from?

The HOT EMER BAT bus

From where is the DC GND HLDG bus powered?

HOT MAIN BAT bus or DC SVCE bus

With the aircraft on the ground, BAT switch is Off and the EXT PWR AVAIL light illuminated, what must be done to fully power the DC electrical system?

Place the BAT switch to ON and after the self test process is complete press the EXT PWR push button

Following an inverter failure the INV light illuminates and:

The associated AC bus is supplied by the other inverter.

In the event that both DC bus 1 and DC bus 2 are lost INV 1 will be supplied automatically by the HOT MAIN BAT bus or:

By the HOT EMER BAT bus in the OVRD configuration, or the TRU if selected on

With the DC BTC pb selected to NORM, when will the flow bar illuminate?

Only during EXT PWR, Hotel mode or single generator operation

With batteries only, when will both AC bus 1 and AC bus 2 be supplied?

Never

If the number one inverter fails:

The AC bus 1 BUS OFF light will illuminate for 10 seconds, and then extinguish and INV FAULT light illuminates

During the start sequence on the ground, the cross start system:

Uses the MAIN BAT and opposite DC GEN

The EMER BAT CHG light will illuminate when:

-battery overheat occurs (automatic disconnection)


-no battery charge when required


With batteries only, AC bus 1 and 2 are:

Never supplied

With only the BAT switch ON, which battery powers the DC STBY bus?

The main battery