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 61 of 179
If Pilot and Standby Altimeter Agree (Copilot Altimeter 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.
3. SENSOR Softkey (Copilot PFD) ............................................................................................ PRESS
4. ADC1 Softkey ......................................................................................................................... PRESS
5. PFD Displays ............................ CONFIRM annunciator is displayed on both PFDs
 In RVSM Airspace:
6. Altitude ............................................................... CROSS-CHECK USING STANDBY ALTIMETER
Record each altimeter reading for contingency procedure use
7. 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 primary altimetry
systems.
If Copilot and Standby Altimeter Agree (Pilot Altimeter 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.
3. Autopilot ALT Mode .................................................................................................... DISENGAGED
4. Pilot’s Static Air Source .................................................................................. SELECT ALTERNATE
A sudden sustained change in rate-of-climb indication accompanied by abnormal indicated
airspeed and altitude changes beyond normal calibrated differences observed on the Pilot’s
PFD would indicate a blockage of the pilot’s static system.
 If Pilot’s and Copilot’s altimeters agree within normal calibrated differences with Pilot’s Alternate
Static Air Source in the ALTERNATE position:
Refer to Section 5, PERFORMANCE in the aircraft AFM for Airspeed Calibration-Alternate
System and Altimeter Correction–Alternate System for the Pilot’s Altimeter.
 In RVSM Airspace:
5. Altitude ............................................................... CROSS-CHECK USING STANDBY ALTIMETER
Record each altimeter reading for contingency procedure use
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.