Airplane Flight Manual Supplement

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. D
Page 34 of 117
power the G1000, the standby battery will automatically power the standby attitude indicator,
altimeter vibrator, and the internal lighting of the three standby instruments for an additional 30
minutes.
11. Consider a Flaps UP Landing and Landing Gear Manual Extension to conserve battery power for
an instrument approach if needed.
TAWS
TAWS WARNING
(Red on PFD and aural “PULL UP”)
1. AP/YD DISC / TRIM INTRPT Button............................................. PRESS and RELEASE
(To disconnect the autopilot)
2. Aircraft Attitude.......................................................PULL BACK ON CONTROL WHEEL
3. Power.......................................................................................... MAXIMUM ALLOWABLE
4. Airspeed........................................................................BEST ANGLE OF CLIMB SPEED
After Warning Ceases
5. Power ......................................................................................... MAXIMUM CONTINUOUS
6. Altitude ...............................................................CLIMB AND MAINTAIN SAFE ALTITUDE
7. Advise ATC of Altitude Deviation, if appropriate
NOTE
Only vertical maneuvers are recommended, unless either operating in visual meteorological
conditions (VMC), or the pilot determines, based on all available information, that turning in
addition to the escape maneuver is the safest course of action, or both.
TAWS FAIL
(Red on PFD and MFD)
Indicates the G1000 will no longer provide TAWS alerting or display relative terrain elevation. The crew
must maintain compliance with procedures that ensure minimum terrain and obstacle separation.