FAA Approved Airplane Flight Manual Supplement

Hawker Beechcraft 200, 200C, B200, B200C, 190-00915-02 Rev. 7
B200GT and B200CGT King Air FAA APPROVED
Page 60 of 179
ELECTRONIC STABILITY AND PROTECTION
MANUAL ESP DISENGAGEMENT
If necessary, ESP may be manually disconnected using any one of the following methods.
1. AP/YD DISC / TRIM INTRPT Button ................................................................... PRESS and HOLD
(Pilot’s or Copilot’s control wheel)
2. CWS Button (Pilot’s or Copilot’s control wheel) ................................................... PRESS and HOLD
3. AFCS SERVOS Circuit Breaker ................................................................................................ PULL
(Right circuit breaker panel)
4. AUX – SYSTEM SETUP 2 Page on MFD ...................... DISABLE STABILITY AND PROTECTION
G1000 INTEGRATED AVIONICS SYSTEM
ALTITUDE MISCOMPARE
This message is displayed when the G1000 detects a difference of 200 feet or greater between
the pilot’s and copilot’s altitude information. Refer to the G1000 Cockpit Reference Guide for
additional information.
1. Altimeter Settings ................................................................. VERIFY both pilot and copilot have the
correct barometric altimeter setting
2. Pilot’s and Copilot’s Altitude ........................................................ COMPARE with Standby Altimeter
THE STANDBY ALTIMETER USES THE SAME STATIC SOURCE AS THE COPILOT’S SIDE
AIR DATA COMPUTER (ADC2). DO NOT USE STANDBY ALTIMETER AS SOLE SOURCE
IN DETERMINING CORRECT ALTITUDE.
WARNING