Airplane Flight Manual Supplement

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. D
Page 108 of 117
TRIPLE FED BUS HOT BATTERY BUS STANDBY BATTERY
LIGHTS LIGHTS LIGHTS
Entrance & Aft Dome Lights
Standby Altimeter Internal
Lighting
Standby Attitude Indicator Internal
Lighting
Standby Airspeed Indicator
Internal Lighting
Cabin Flour Lights
Instruments Indirect Lights
Navigation Lights
PROPELLERS
Propeller Governor Test
WARNING/ANNUNCIATORS
Annunciator Indicator
Annunciator Power
L Oil Pressure Warning
Landing Gear Position Indicator
Landing Gear Warning Horn
R Oil Pressure Warning
Stall Warning
L Fuel Pressure Warning
R Fuel Pressure Warning
L Auxiliary Fuel Quantity
Warning
R Auxiliary Fuel Quantity
Warning
WEATHER
L Pitot Heat
STANDBY BATTERY POWER SUPPLY
The G1000 installation incorporates a 24 vdc, 5 Ah JET model PS-835 Standby Battery
that provides electrical power for the standby attitude gyro, standby altimeter vibrator,
and internal lighting for the three standby instruments for a minimum of 30 minutes
following a total loss of aircraft power including the aircraft’s battery.
A push button switch located directly below the standby airspeed indicator controls the standby battery
power system. The switch is a push ON (switch latches in), push OFF (switch pops out) type of switch.
The system has three modes: OFF, ON, and ARM.