FAA Approved Airplane Flight Manual Supplement

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 3

Page 88 of 167 FAA APPROVED

b. Copilot’s Control Wheel (If Installed)

 Left and Right Segments .............................................................. ACTUATE INDIVIDUALLY

(Verify there is no elevator tab wheel movement)

 Left and Right Segments ................................................................... ACTUATE TOGETHER

(Verify proper elevator tab wheel movement)

 With Elevator Tab Wheel in Motion,

AP/YD DISC / TRIM INTRPT Button ....................................................... PRESS AND HOLD

(verify elevator tab wheel motion stops)

 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

c. Press GA Button on Left power lever ......... VERIFY FD Command Bars show Takeoff Attitude

‘TO / / TO’ is Annunciated in Mode Window on Both PFDs

BEFORE TAKEOFF (FINAL ITEMS)

The following procedures supersede the same procedures in the airplane’s AFM BEFORE

TAKEOFF (FINAL ITEMS) checklist items.

1. V

, V

, Minimum Takeoff Power .......................................................................... SET OR CONFIRM

These procedures should be conducted after completing the airplane’s AFM BEFORE TAKEOFF

(FINAL ITEMS) checklist.

2. PFD Attitude and Heading .................................................................................................. NORMAL

3. GPS Position .................................................................. VALID, ‘LOI’ NOT ANNUNCIATED on HSI

4. Standby Attitude Indicator .......................................... ERECT and NORMAL, Fail Flag not in view

TAKEOFF

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.