FAA Approved Airplane Flight Manual Supplement

190-00915-02 Rev. 7 Hawker Beechcraft 200, 200C, B200 , B200C,
B200GT and B200CGT King Air
Page 143 of 179
PROPELLER SYNCHROPHASER
A push button ON/OFF switch is located on the instrument panel below the pilot’s PFD that
turns the propeller synchrophaser ON and OFF. To turn the propeller synchrophaser ON, push
the PROP SYNC switch. A green ON annunciator will illuminate when the system is on. To
turn the propeller synchrophaser OFF, push the PROP SYNC switch.
Refer to the Systems Description section in the airplane’s original Pilot’s Operating Handbook and FAA
Approved Airplane Flight Manual for a description of the synchrophaser and its operation.
ELECTRICAL SYSTEM
INVERTERS
The two solid-state inverters are not needed with the G1000 system and have been removed.
POWER DISTRIBUTION
There are no changes to the electrical power generation, power feeders, control, or fault protection. Only
the Avionics power distribution has changed.
AVIONICS/ELECTRICAL EQUIPMENT BUS CONNECTION
A/C SERIAL NUMBER BB-2 THROUGH BB-1485 EXCEPT BB-1484, BL-1 THRU BL-140
NO. 1 DUAL FEED
BUS
NO. 2 DUAL FEED
BUS
NO. 3 DUAL FEED
BUS
NO. 4 DUAL FEED
BUS
AVIONICS AVIONICS
Avionics Master Switch Cabin Audio
Aural Warning PFD/GIA 2 Fan
Autopilot Mode
Controller
AHRS 2
Essential Bus
Secondary Power
Air Data 2
PFD/GIA 1 Fan GIA 2
Voice Recorder PFD 2
AHRS 1 Secondary Pwr
Air Data 1 Secondary
Pwr
GIA 1 Secondary Pwr
PFD 1 Secondary Pwr
ELECTRICAL ELECTRICAL
Left Generator Control Right Generator Control
ENGINE ENGINE ENGINE ENGINE
L Engine Instrument
Power
R Engine Instrument
Power
L Igniter Power R Igniter Power
L Engine Fuel Control
Heat
R Engine Fuel Control
Heat
L Start Control R Start Control