Airplane Flight Manual Supplement

190-00915-02 Rev. 8 Hawker Beechcraft 200, 200C, B200, B200C,
FAA APPROVED B200GT and B200CGT King Air
Page 91 of 179
NOTE
The standby compass is erratic during windshield anti-ice and/or air conditioner operation.
Windshield anti-ice and air conditioner must be OFF for heading verification check.
e. Verify turn rate and slip indicator display appropriately.
BEFORE TAKEOFF (RUN-UP)
The following procedures supersede the same procedures in the airplane’s AFM BEFORE
TAKEOFF (RUNUP) checklist items.
1. Electric Elevator Trim ............................................................................................................ CHECK
a. Pilot’s Control Wheel
• 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)
• Manually Operate Elevator Tab Wheel ...... VERIFY Pitch Trim Servo is Not Engaged
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
2. Press GA Button on Left power lever ................ VERIFY FD Command Bars show Takeoff Attitude
‘TO / / TO’ is Annunciated in Mode Window on Both PFDs