Electrical Power Systems Flashcards
DC Voltmeter indicates:
Voltage on the Battery-Charging bus
When a GPU is used for engine start, the output value should be :
Regulated to 28 VDC and limited to 500 amps minimum and 1100 amps maximum.
Buses that the airplane batteries power are:
All buses including AC if an inverters is on
A generator failure is indicated when:
The GEN switch is in the ON position and the GEN light remains illuminated after activating RESET
IF airplane electrical power fails and the EMER PWR BAT 1 switch is ON, the systems powered by the emergency battery are:
Standby attitude gyro
Landing Gear
Flaps
If both 275-amp current limiters fail in flight:
The essential buses will remain powered by the air craft batteries and generators
Illumination of a PRI or SEC inverter light indicates:
-The inverter output is less than 90 VAC, or there is less than a 10 volt-ampere draw on the inverter
OR
-The inverter switch is off
The AC voltmeter will indicate:
Left AC bus voltage when the AC BUS switch is in PRI
IF an overload sensor shuts off power to a main bus power may be restored by:
Resetting the control CB after the overload sensor resets
To unlock the entrance door when batteries are dead:
Remove both batteries for charging and reinstall
With a dual-generator failure in flight the airplane batteries will support the minimum night IFR equipment load for approximately:
30 minutes
Inverter output is :
115 VAC, 400 Hz
The approved AFM recommends that the GPU be used for engine start when the ambient temperature is:
32F (0°C) or below
When either the primary or secondary inverter light illuminates the first step of corrective action is:
Check for open INV or AC BUS circuit breaker(s)
Primary DC electrical power is provided by
Two engine-driven brushless DC generators