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 70 of 179
LOSS OF INTEGRITY (LOI) MODE - ACTIVE WHEN THE AIRPLANE IS WITHIN 30NM OF THE
DESTINATION OR DEPARTURE AIRPORT (AS CALCULATED FROM THE PREVIOUS GPS OR DR
POSITION):
1. Navigation - Fly towards known visual conditions. Use ATC or other information sources as
possible.
NOTE
 All information derived from GPS or DR will be removed from the displays.
 TAWS is inoperative.
 The airplane symbol is removed from most maps. The map will remain centered at the last
known position. “NO GPS POSITION” will be annunciated in the center of the map.
 MAP – TRAFFIC MAP display is not dependent on GPS information. The position of
displayed traffic relative to the airplane symbol on the map is still accurate.
GPS APPROACH INTEGRITY LIMITS EXCEEDED
During a GPS LP, LPV, LNAV/VNAV, or LNAV+V approach using SBAS, if the Horizontal or
Vertical integrity limits are exceeded, the G1000 System will downgrade the approach. This will
be annunciated in the ALERTS window and may also be accompanied by a change in the
indicated approach type on the HSI. GPS glide path vertical guidance will be removed from the
PFD unless the minimum can still be supported using Baro VNAV. The approach may be
continued as annunciated.
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During any GPS approach in which both precision and non-precision integrity limits are exceeded,
the G1000 System will flag the lateral guidance and display a system message “ABORT
APPROACH loss of navigation”. Immediately upon viewing the message, the unit will revert to
Terminal navigation mode integrity limits. If the position integrity is within these limits lateral
guidance will be restored and the GPS may be used to execute the missed approach, otherwise
alternate means of navigation must be utilized.