Airplane Flight Manual Supplement

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. D
Page 64 of 117
• 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)
These procedures should be conducted after completing the airplane’s AFM BEFORE TAKEOFF
(FINAL ITEMS) checklist.
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
This procedure should be conducted after brake release during the takeoff roll but before
becoming airborne.
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
These procedures should be conducted after the Battery and Generator Switches have been
turned OFF in the AFM SHUTDOWN AND SECURING checklist, and before the flight crew
vacates the cockpit.
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)