TM 1-1510-223-CL
E-18
5. Setting AVIONICS MASTER POWER switch
(overhead control panel) to the off (aft)
position.
6. Setting
aircraft
MASTER
SWITCH
(overhead control panel) to the OFF position.
7. Setting the AUTO PLT power switch
(overhead control panel) to off position.
YAW DAMP EMERGENCY DISCONNECTION
1. Pressing the AP & YD/TRIM DISC switch
(control wheels).
2. Pressing the AP ENGAGE pushbutton on the
autopilot controller (pedestal extension).
3. SETTING THE RUDDER BOOST/YAW
CONTROL
TEST
switch
(pedestal
extension) to the YAW CONTROL TEST
position.
4. Pulling the AP CONTR circuit breaker
(overhead control panel).
5. Pulling the RUDDER BOOST circuit breaker
(overhead control panel).
6. Setting AVIONICS MASTER POWER switch
(overhead control panel) to the off (aft)
position.
7. Setting aircraft MASTER switch (overhead
control panel) to the OFF (aft) position.
8. Setting the AUTO PLT power switch
(overhead control panel) to off.
