Airplane Flight Manual Supplement

190-00915-02 Rev. 8 Hawker Beechcraft 200, 200C, B200, B200C,
FAA APPROVED B200GT and B200CGT King Air
Page 75 of 179
LOSS OF ALTITUDE ALERTER IN RVSM AIRSPACE
1. Autopilot ALT Mode ......................................................................................................... ENGAGED.
2. Altitude ...................................................... MONITOR
AND MAINTAIN ASSIGNED ALTITUDE
3. Perform appropriate RVSM contingency procedures for the loss of altitude alerting, outlined in the
operator’s RVSM procedures manual.
FAILED ATTITUDE AND/OR HEADING
(ATTITUDE FAIL AND/OR RED "X" OVER HEADING DISPLAY ON PFD)
This indicates a loss of pitch, roll, and/or heading information from AHRS. Refer to GARMIN
G1000 Cockpit Reference Guide and Pilot’s Guide for additional information. Interference from
GPS repeaters operating inside nearby hangars or magnetic anomalies caused by nearby
structures can cause an intermittent loss of attitude and heading displays while the airplane is on
the ground. This is usually accompanied by a BOTH ON GPS 1, BOTH ON GPS 2, or LOI
annunciation. Moving the airplane more than 100 yards away from the source of the interference
should alleviate the condition.
Taxiing the airplane before a valid GPS position has been acquired can cause attitude and/or
heading display to indicate a failed condition. As soon as the airplane acquires a valid GPS
position, attitude and heading should return to normal.
DO NOT TAKE OFF WITHOUT VALID, NORMAL ATTITUDE AND HEADING DISPLAYS
In Flight, If Both Sides:
1. Attitude .................................................................................. MONITOR using standby attitude gyro
2. WSHLD ANTI-ICE Switches (Pilot and Copilot).......................................................................... OFF
NOTE
The magnetic compass is erratic during windshield anti-ice and/or air conditioner operation.
With windshield anti-ice OFF, windshield may form fog or frost on the inside surface. The
windshield anti-ice should be turned off only long enough to reference magnetic compass or
the pilot should descent to a warmer altitude if terrain, fuel, and endurance permit.
3. ELEC HEAT ................................................................................................................................ OFF
4. CABIN TEMP MODE switch ....................................................................................................... OFF
5. Heading .................................................................................... MONITOR using magnetic compass
WARNING