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ramp using emergency brakes.
13. Directional Control . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN with nosewheel steering
PROCEDURE COMPLETED
3-38 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
AUTOPILOT MALFUNCTION (POSSIBLE RED AFCS ON PFD)
NOTE
If red AFCS is displayed, the autopilot, yaw damper, and manual electric pitch trim will
be inoperative.
PROCEDURE COMPLETED
PITCH TRIM FAILURE (RED PTRM ON PFD)
1. Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GRIP FIRMLY
2. AP/TRIM DISC Button (if required) . . . . . PRESS (high elevator control forces possible)
3. Trim. . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED USING MANUAL TRIM WHEEL
4. Actuate each half of the pilot and copilot manual electric trim switches separately for at
least 3 seconds each.
• IF RED PTRM MESSAGE CLEARS
PROCEDURE COMPLETED
• IF RED PTRM MESSAGE REMAINS OR POSTS DURING SWITCH
ACTIVATION
5. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DO NOT RE-ENGAGE
PROCEDURE COMPLETED
ROLL AXIS AUTOPILOT FAILURE (RED ROLL ON PFD)
Indicates a failure of the roll axis of the autopilot. The autopilot will be inoperative.
PITCH AXIS AUTOPILOT FAILURE (RED PTCH ON PFD)
Indicates a failure of the pitch axis of the autopilot. The autopilot will be inoperative.
YAW AXIS AUTOPILOT FAILURE (RED YAW ON PFD)
Indicates a failure of the yaw axis of the autopilot. The autopilot and yaw damper will be
inoperative.
1. Refer to Abnormal Procedures, YAW DAMPER INOPERATIVE.
1. AP / TRIM DISC Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
510FM-07 AA 3-39
SECTION III - OPERATING PROCEDURES MODEL 510
EMERGENCY PROCEDURES
FAA APPROVED
U.S. Configuration
AILERON TRIM RUNAWAY
5. AP/TRIM DISC Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE
NOTE
If aileron trim goes to full travel before stopping, airspeed may need to be reduced to
130 KIAS or less to reduce the force sufficiently.
6. Land as soon as practical. Refer to Abnormal Procedures, AILERON TRIM INOPERATIVE.
PROCEDURE COMPLETED
RUDDER TRIM RUNAWAY
4. AP/TRIM DISC Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE
5. Land as soon as practical. Refer to Abnormal Procedures, RUDDER TRIM INOPERATIVE.
PROCEDURE COMPLETED
PITCH TRIM RUNAWAY
5. AP/TRIM DISC Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE
6. Land as soon as practical.
PROCEDURE COMPLETED
HYDRAULIC WHEEL BRAKE FAILURE
3. Directional Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN with nosewheel steering
4. Landing Distance:
(Continued Next Page)
1. Control Wheel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GRIP FIRMLY
2. AP/TRIM DISC Button . . . . . . . . PRESS and HOLD (high aileron control forces possible)
3. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE (as required to minimize control forces)
4. AILERON TRIM Circuit Breaker (left circuit breaker panel) . . . . . . . . . . . . . . . . . . . . PULL
1. RUDDER PEDALS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HOLD FIRMLY
2. AP / TRIM DISC Button . . . . . . . PRESS AND HOLD (high rudder control forces possible)
3. RUDDER TRIM Circuit Breaker (left circuit breaker panel) . . . . . . . . . . . . . . . . . . . . PULL
1. CONTROL WHEEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GRIP FIRMLY
2. AP / TRIM DISC Button . . . . . . PRESS AND HOLD (high elevator control forces possible)
3. Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED USING MANUAL TRIM WHEEL
4. AFCS Circuit Breaker (left circuit breaker panel) . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL
1. Brake Pedals. . . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVE FEET FROM BRAKE PEDALS
2. EMERGENCY BRAKE Handle . SMOOTH PULL AS REQUIRED and HOLD until stopped
STALL WARNING-NORMAL MULTIPLY normal Flap LAND landing distance by 1.83.
STALL WARNING-HIGH MULTIPLY normal Flap TO/APR landing distance by 1.96.
3-40 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
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Citation Mustang airplane flight manual 1(46)
