FAA Approved Airplane Flight Manual Supplement

Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev.4

Page 46 of 173 FAA APPROVED

LOAD MANAGEMENT TABLE

This table replaces the Load Management Table published in the AFM.

EQUIPMENT

OPERATING TIME

(Minutes)

REDUCTION IN MAIN BATTERY

DURATION (Minutes)

Standby Altimeter Continuous None*

Standby Airspeed Indicator Continuous None*

Standby Attitude Indicator Continuous None*

Comm 1 Xmit Continuous -----

Pilot Audio Continuous -----

Nav 1 Continuous -----

ADC 1 Continuous -----

Pilot PFD Continuous -----

AHRS 1 Continuous -----

Transponder 1 Continuous -----

GEA 1 Continuous -----

MFD Continuous -----

Copilot PFD Continuous -----

Nav 2 Continuous -----

ADC 2 Continuous -----

AHRS 2 Continuous -----

GEA 2 Continuous -----

Instrument Indirect /Emergency Lights Continuous None*

Cabin Lights 5 2

Ice Lights 5 0.5

Beacon Lights Continuous -----

Taxi Lights 1 0.3

Digital OAT Continuous -----

Fuel Quantity Indicators Continuous -----

Single Standby Fuel Pump 5 1

Left Bleed Air Valve Continuous -----

Pressurization Control Continuous -----

Cabin Temperature Control Continuous -----

Engine Ignition 0.5 0.1

Surface Deice 5 cycles 0.1

Left and Right Main Engine Anti-ice Single Operation 0.1

Manual Prop Deice 3 3

Windshield Wiper 1 0.2

Left Pitot Heat Continuous -----

Landing Gear Single Operation 0.5