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 59 of 179
FLASHING AMBER MODE ANNUNCIATION
NOTE
Abnormal mode transitions (those not initiated by the pilot or by normal sequencing of the AFCS)
will be annunciated by flashing the disengaged mode in amber on the PFD. Upon loss of a
selected mode, the system will revert to the default mode for the affected axis, either ROL or PIT.
After 10 seconds, the new mode (PIT or ROL) will be annunciated in green.
LOSS OF SELECTED VERTICAL MODE (FLC, VS, VPTH, ALT, GS, GP)
1. Autopilot mode controls....................................................... SELECT ANOTHER VERTICAL MODE
If on an instrument approach, disconnect autopilot and continue manually or execute missed approach:
2. AP/YD DISC / TRIM INTRPT Button ............................................................ PRESS and RELEASE
LOSS OF SELECTED LATERAL MODE (HDG, VOR, GPS, LOC, VAPP, BC)
1. Autopilot mode controls.................. ............................... ......SELECT ANOTHER LATERAL MODE
If on an instrument approach, disconnect autopilot and continue manually or execute missed approach:
2. AP/YD DISC / TRIM INTRPT Button ............................................................ PRESS and RELEASE
YAW DAMPER AUTOMATIC DISCONNECT (Amber Flashing ‘YD’)
Flashing amber ‘YD’ in flight indicates that yaw damper has disconnected. If the disconnect was
not pilot initiated, the flashing amber ‘YD’ annunciation will be accompanied by a red or amber
YAW annunciation in the AFCS status field on the PFD. Refer to Section 3 – Emergency
Procedures, YAW AXIS FAILURE, for further information.