FAA Approved Airplane Flight Manual Supplement

190-00716-02 Rev. 3 Hawker Beechcraft King Air 300/300LW
Page 115 of 167
Section 7 - Systems Description
Table of Contents
GENERAL ................................................................................................................... 116
G1000 INTEGRATED AVIONICS ............................................................................... 116
SYSTEM OVERVIEW ........................................................................................................................... 116
INSTRUMENT PANEL .......................................................................................................................... 116
FLIGHT CONTROLS .................................................................................................. 125
AFCS, AUTOPILOT, FLIGHT DIRECTOR AND RUDDER BOOST .................................................... 125
ELECTRIC ELEVATOR TRIM .............................................................................................................. 129
ELECTRONIC STABILITY & PROTECTION (ESP) ............................................................................ 130
FLIGHT INSTRUMENTS ............................................................................................ 134
G1000 FLIGHT INSTRUMENTS ........................................................................................................... 134
STANDBY FLIGHT INSTRUMENTS .................................................................................................... 134
ENGINE INSTRUMENTATION ................................................................................... 135
PROPELLER SYNCHROPHASER ...................................................................................................... 136
ELECTRICAL SYSTEM .............................................................................................. 136
INVERTERS .......................................................................................................................................... 136
POWER DISTRIBUTION ...................................................................................................................... 136
STANDBY BATTERY POWER SUPPLY ............................................................................................. 140
LIGHTING SYSTEMS ................................................................................................. 141
COCKPIT .............................................................................................................................................. 141
PITOT AND STATIC SYSTEM ................................................................................... 141
PITOT .................................................................................................................................................... 141
STATIC .................................................................................................................................................. 142
GROUND COMMUNICATIONS .................................................................................. 142
SYNTHETIC VISION ................................................................................................... 143
TAWS AND GPWS ..................................................................................................... 147
GTS 8000 TCAS II ...................................................................................................... 148
APPROACH BARO VNAV ......................................................................................... 157