Airplane Flight Manual Supplement
190-00915-02 Rev. 8 Hawker Beechcraft 200, 200C, B200, B200C,
FAA APPROVED B200GT and B200CGT King Air
Page 83 of 179
TAWS N/A and TAWS FAIL
1. If the amber status annunciator is displayed on the PFDs and MFD, the system will
no longer provide TAWS alerting or display relative terrain and obstacle elevations. The crew must
maintain compliance with procedures that ensure minimum terrain and obstacle separation.
2. If the amber
status annunciator is displayed on the PFDs and MFD, the system will
no longer provide TAWS alerting or display relative terrain and obstacle elevations. The crew must
maintain compliance with procedures that ensure minimum terrain and obstacle separation.
NOTE
The GPWS functions will continue to function if GPWS is available on a Class A TAWS system.
Forward Looking Terrain Awareness alerts and Premature Descent Alerts will be unavailable.
GPWS FAIL (TAWS-A only)
(Yellow on PFD and MFD)
If the amber
status annunciator is displayed on the PFDs and MFD, the G1000 will no
longer provide GPWS alerting. The crew must maintain compliance with procedures that ensure
minimum terrain separation as well proper airplane landing gear and flap configuration.
NOTE
Forward Looking Terrain Awareness alerts, Premature Descent Alerts, and Altitude Voice Callouts
will continue to function if TAWS is available.
TCAS II
TCAS II TRAFFIC ADVISORY
(Amber on PFD and aural “TRAFFIC, TRAFFIC” advisory)
Conduct a visual search for the intruder. If successful, maintain visual acquisition to ensure safe
separation.
The pilot should not initiate evasive maneuvers using information from the traffic map display only on a
traffic advisory (TA) without visually sighting the traffic. These displays and advisories are intended
only for assistance in visually locating the traffic and lack the flight path trends necessary for use in
evasive maneuvering. However, unnecessary resolution advisories can be issued by TCAS II when
other aircraft are operating at an altitude adjacent to the one that has been assigned to the climbing or
descending TCAS aircraft. When climbing or descending in an environment where these unnecessary
advisories are considered likely to occur (based on either airspace design, air traffic communications,
visual acquisition or utilization of traffic displays), a reduction in vertical velocity is recommended until
reaching the assigned altitude. As appropriate, the vertical velocity should be reduced to a rate
between 500 and 1,500 ft/min, when approaching an altitude between 1,000 and 2,000 ft. above or
below the altitude assigned in the ATC instruction or clearance.










