FAA Approved Airplane Flight Manual Supplement

Hawker Beechcraft 200, 200C, B200, B200C, 190-00915-02 Rev. 7
B200GT and B200CGT King Air FAA APPROVED
Page 64 of 179
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
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.