Airplane Flight Manual Supplement

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C
Page 52 of 95
• Pilot’s Trim Override.................................................................................................... CHECK
Activate the copilot’s Pitch Trim Switches nose down. Verify elevator tab wheel is
moving nose down. While the tab wheel is moving in the DN direction, activate the
pilot’s Pitch Trim Switches nose up. Verify the elevator tab wheel begins to move in the
UP direction. Release both pilot’s and copilot’s Pitch Trim switches and reset elevator
tab as required.
• Manually Operate Elevator Tab Wheel...... VERIFY Pitch Trim Servo is Not Engaged
3. Press GA Button on Left Throttle ...................... VERIFY FD Command Bars show Takeoff Attitude
‘TO / / TO’ is Annunciated in Mode Window on Both PFDs
BEFORE TAKEOFF (FINAL ITEMS)
1. PFD Attitude and Heading ..................................................................................................NORMAL
2. GPS Position.................................................................. VALID, ‘LOI’ NOT ANNUNCIATED on HSI
3. Standby Attitude Indicator.......................................... ERECT and NORMAL, Fail Flag not in view
ON TAKEOFF ROLL
1. Verify correspondence of PFD airspeed display and standby airspeed
CLIMB, CRUISE, AND DESCENT
Disengage autopilot and yaw damper and retrim the airplane in roll and yaw following a power
change, change in airspeed, or if a slight wing rocking is observed. Re-engage the autopilot and
yaw damper after trimming the airplane.
SHUTDOWN AND SECURING
1. Standby Battery Switch..................................................................................................PRESS OFF
a. Standby Battery Switch...................................................... [ARMED] and [ON] EXTINGUISHED
b. Standby attitude fail flag displayed after BAT – MASTER SWITCH is OFF
c. Standby altimeter vibrator should not be heard (BAT – MASTER SWITCH OFF)