FAA Approved Airplane Flight Manual Supplement

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.1

Page 40 of 137 FAA APPROVED

LOAD MANAGEMENT TABLE

This table replaces the Load Management Table published in the AFM. Use of the following

equipment will reduce battery duration by the approximate times listed below. Multiple usage of the

following equipment is additive.

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 3

Ice Lights 5 0.6

NAV Lights 60 7

Taxi Lights 5 2

Digital OAT Continuous -----

Single Standby Fuel Pump 5 2

Left Bleed Air Valve Continuous -----

Pressurization Control Continuous -----

Cabin Temperature Control Continuous -----

Surface Deice 1 0.1

Left and Right Main Engine Anti-ice Single Operation 0.1

Manual Prop Deice 5 6

Windshield Wiper 5 1

Left Pitot Heat Continuous -----