FAA Approved Airplane Flight Manual Supplement

190-00716-02 Rev. 3 Hawker Beechcraft King Air 300/300LW
FAA APPROVED Page 61 of 167
If Pilot’s and Copilot’s Altitude Agree:
3. Airspeed 120 KIAS MINIMUM on slowest indicator.
4. Monitor all three airspeed indicators during changes in power or altitude to determine which
indicators are inaccurate. Indications of inaccurate airspeed include:
 No change in indicated airspeed when power change and altitude maintained.
 Indicated airspeed increases when climbing or decreases when descending.
5. Use SENSOR softkey to select most accurate ADC on the affected PFDs.
6. Airspeed ……………………………………………………….RESUME NORMAL SPEEDS
If Pilot’s and Copilot’s Altitude Do Not Agree:
3. Refer to Abnormal Procedures, ALT MISCOMP procedure to determine most accurate ADC.
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.