FAA Approved Airplane Flight Manual Supplement

Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev. 1
Page 54 of 141 FAA APPROVED
AIRSPEED MISCOMPARE
This message is displayed when the G1000 detects a difference of 7 KIAS or greater between the
pilot’s and copilot’s airspeed indicators (10 KIAS difference during takeoff or landing roll). Refer to
the G1000 Cockpit Reference Guide for additional information.
1. Pilot’s and Copilot’s Airspeed ...................................... COMPARE with Standby Airspeed Indicator
THE STANDBY AIRSPEED INDICATOR USES THE SAME PITOT-STATIC SOURCES AS THE
COPILOT’S SIDE AIR DATA COMPUTER (ADC2). DO NOT USE STANDBY AIRSPEED
INDICATOR OR STANDBY ALTIMETER AS SOLE SOURCE IN DETERMINING CORRECT
AIR DATA INFORMATION.
If Pilot and Standby Airspeed Indicator Agree (Copilot Airspeed Differs):
NOTE
The standby altimeter must be corrected for position error using the Altimeter Correction – Standby
System chart in the Performance section of this supplement.
2. SENSOR Softkey (Copilot’s PFD) ......................................................................................... PRESS
3. ADC1 Softkey ......................................................................................................................... PRESS
4. PFD Displays ........................... CONFIRM
annunciator is displayed on both PFDs
• In RVSM airspace:
5. Altitude ................................................................ CROSS-CHECK USING STANDBY ALTIMETER
Record each altimeter reading for contingency procedure use
NOTE
The standby altimeter must be corrected for position error using the Altimeter Correction –
Standby System chart in the Performance section of this supplement.
6. Advise ATC of loss of redundancy of primary altimetry systems. Perform appropriate RVSM
contingency procedures outlined in the operator’s RVSM manual for the loss of redundancy of
primary altimetry systems.
If Copilot and Standby Airspeed Indicator Agree (Pilot Airspeed Differs):
NOTE
The standby altimeter must be corrected for position error using the Altimeter Correction – Standby
System chart in the Performance section of this supplement.
2. Pilot and Copilot ALTITUDE .................................................................................................... NOTE
WARNING