YAW DAMP EMERGENCY DISCONNECTION - TM-1-1510-224-CL

BATTERY CHARGE ANNUNCIATOR ILLUMINATED - TM-1-1510-224-CL_25

LANDING GEAR EMERGENCY EXTENSION - TM-1-1510-224-CL_27

TM-1-1510-224-CL Army RC-12P Aircraft and Army RC-12Q Aircraft Manual
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TM 1-1510-224-CL FLIGHT CONTROL MALFUNCTIONS AUTOPILOT EMERGENCY DISCONNECTION 1. Pressing the AP & YD/TRIM DISC switch. 2. Pressing the AP ENGAGE pushbutton on the autopilot controller. 3. Pressing the GO-AROUND switch (yaw damper will remain on). 4. Pulling the AP CONTR and AFCS DIRECT circuit breakers. 5. Setting AVIONICS MASTER POWER switch to the off (aft) position. 6. Setting aircraft MASTER SWITCH to the OFF position. 7. Setting the AUTO PLT power switch to off position. YAW DAMP EMERGENCY DISCONNECTION 1. Pressing the AP & YD/TRIM DISC switch. 2. Pressing the AP ENGAGE pushbutton on the autopilot controller. 3. Setting the RUDDER BOOST/YAW CONTROL TEST switch to the YAW CONTROL TEST position. 4. Pulling the AP CONTR circuit breaker. 5. Pulling the RUDDER BOOST circuit breaker. 6. Setting AVIONICS MASTER POWER switch to the off (aft) position. 7. Setting aircraft MASTER switch to the OFF position. 8. Setting the AUTO PLT power switch to off. UNSCHEDULED RUDDER BOOST ACTIVATION 1. AP & YD/TRIM DISC switch - Disconnect and hold (hold to first level). (2.) RUDDER BOOST switch - OFF. 3. RUDDER BOOST circuit breaker - Pull (provided that rudder boost does not deactivate). 4. AP & YD/TRIM DISC switch - Release. (5.) Yaw damper - Reengage (if RUDDER BOOST circuit breaker is not pulled). E-12

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