FAA Approved Airplane Flight Manual Supplement

190-00915-02 Rev. 7 Hawker Beechcraft 200, 200C, B200, B200C,
FAA APPROVED B200GT and B200CGT King Air
Page 65 of 179
PITCH MISCOMPARE
This message is displayed in the upper right corner of the PFD when the G1000 detects a
difference between the pilot’s and copilot’s pitch attitude of more than 5 degrees. Refer to
GARMIN G1000 Cockpit Reference Guide for additional information.
1. Refer to STANDBY ATTITUDE indicator to determine which AHRS is providing the most accurate
data.
2. Use SENSOR softkey to select the most accurate AHRS on the affected PFD.
ROLL MISCOMPARE
This message is displayed in the upper right corner of the PFD when the G1000 detects a
difference between the pilot’s and copilot’s roll attitude of more than 6 degrees. Refer to the
GARMIN G1000 Cockpit Reference Guide for additional information.
1. Refer to STANDBY ATTITUDE indicator to determine which AHRS is providing the most accurate
data.
2. Use SENSOR softkey to select the most accurate AHRS on the affected PFD.
HEADING MISCOMPARE
This message is displayed in the upper right corner of the PFD when the G1000 detects a
difference between the pilot’s and copilot’s heading information. Refer to the GARMIN G1000
Cockpit Reference Guide for additional information.
1. WSHLD ANTI-ICE Switches (PILOT and COPILOT) ................................................................. OFF
2. CABIN TEMP MODE selector ..................................................................................................... OFF
3. ELEC HEAT ................................................................................................................................ OFF
4. Refer to Magnetic Compass to determine which AHRS is providing the most accurate heading
information.
5. Use SENSOR softkey to select the most accurate AHRS on the affected PFD.
6. WSHLD ANTI-ICE Switches ..................................................................................... AS REQUIRED
7. CABIN TEMP MODE ................................................................................................... AS DESIRED
8. ELEC HEAT .............................................................................................................. AS REQUIRED
NOTE
The magnetic compass is affected by windshield anti-ice and/or air conditioner operation.
These items must be turned OFF prior to referencing magnetic compass heading, and then
may be reselected ON. With windshield anti-ice OFF, fog or frost may form on the inside
surface of the windshield. The windshield anti-ice should be turned off only long enough to
reference magnetic compass or the pilot should descend to a warmer altitude if terrain, fuel,
and endurance permit.