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 82 of 179
NOTE
The GPWS INHIBIT feature will not inhibit altitude voice callouts or Glideslope/Glidepath deviation
alerting.
FLAP OVERRIDE (TAWS-A Only)
For airplanes equipped with TAWS-A, the GPWS flap configuration alerting function may be inhibited
to stop alerting if desired. Refer to GARMIN G1000 Cockpit Reference Guide for additional
information.
To Override Flap Altering:
1. Display the MAP – TAWS A page
2. FLAP OVR Softkey ................................................................................................................ PRESS
3. Verify a
annunciation displays on both PFDs and in the lower right corner of the
MFD.
To Enable Flap Alerting if Overridden:
1. Display the MAP – TAWS A page
2. FLAP OVR Softkey ................................................................................................................ PRESS
3. Verify the annunciation is removed from both PFDs and the MFD.
GLIDESLOPE/GLIDEPATH DEVIATION INHIBIT (TAWS-A Only) or
For airplanes equipped with TAWS-A, the glideslope or glidepath deviation alerting function may be
inhibited to stop alerting if desired. Refer to GARMIN G1000 Cockpit Reference Guide for additional
information.
To Inhibit Glideslope or Glidepath Alerting:
1. Display the MAP – TAWS A page
2. GS INH or GP INH Softkey .................................................................................................... PRESS
3. Verify a
or a annunciation displays on both PFDs and in the lower right corner
of the MFD.
To Enable Glideslope or Glidepath Alerting if Inhibited:
1. Display the MAP – TAWS A page
2. GS INH or GP INH Softkey .................................................................................................... PRESS
3. Verify the
or annunciation is removed from both PFDs and the MFD.
NOTE
The GS INH or GP INH softkeys are only available for selection below 1000’ radar altitude with the
landing gear DOWN and the airplane sufficiently below the Glideslope or Glidepath to generate a
deviation alert.