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8  PITCH TRIM RUNAWAY
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
510CLEAP-07 AA 51
M
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
1. Actuate both halves of pilot and copilot trim switches to check for stuck
switch.
2. AFCS Circuit Breaker (L circuit breaker panel) - - - - - - - - - - - - - - - RESET
• IF STILL INOPERATIVE
3. Manual Elevator Trim - - - - - - - - - - - - - - - - - - - - - - - - -AS REQUIRED
4. If unable to trim using manual trim wheel, refer to JAMMED ELEVATOR
TRIM TAB procedure; Tab N2.
PROCEDURE COMPLETED
• IF OPERATIVE
PROCEDURE COMPLETED
• DURING CRUISE
1. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - MAINTAIN
trim airspeed as long as practical
2. Land as soon as practical.
3. Descent - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - MAINTAIN
a continuous descent to landing, if
possible, to minimize elevator force
4. Flaps - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -AS REQUIRED
5. Landing Gear - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -AS REQUIRED
PROCEDURE COMPLETED
• TAKEOFF OR GO-AROUND
1. Throttle - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REDUCE
(at safe altitude)
2. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 150 KIAS OR LESS
BEFORE LANDING
3. Landing Gear - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -DOWN
4. Flap Handle - - - - - - - - LAND (TO/APR if STALL WARN HI is displayed)
5. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -VREF+10
6. Landing Distance/Weight:
C A U T I O NCAUTION
Avoid landing with a tailwind.
PROCEDURE COMPLETED
1  ELECTRIC ELEVATOR TRIM INOPERATIVE
2  JAMMED ELEVATOR TRIM TAB
STALL
WARNING FLAPS *MULTIPLY LANDING
DISTANCE BY:
*REDUCE MAX LANDING
WEIGHT BY:
NORMAL LAND 1.28 50 lbs.
HIGH TO/APR 1.22 40 lbs.
* Basic landing distance and maximum landing weight values must be obtained from the
appropriate landing performance charts based on the STALL WARNING and ANTI-ICE system
settings.
52 AA 510CLEAP-07
N
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
1. AP/TRIM DISC Button- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -PRESS
2. Either Control Wheel - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - APPLY
opposite roll input
3. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REDUCE
(if required to reduce control force)
4. Rudder - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - TRIM
as required up to 1/2 bar slip/skid displacement to reduce roll control forces
5. FUEL TRANSFER Knob - - - - - - - - - - - - - - - - - - - - - - - - - AS REQUIRED
6. YD or AP Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - AS DESIRED
7. Land as soon as practical.
PROCEDURE COMPLETED
1. AP/TRIM DISC Button- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -PRESS
2. Rudder - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - APPLY
opposing control input as required
3. Aileron- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - APPLY
opposing control input and TRIM as required
4. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REDUCE
(if required to reduce control force)
5. FUEL TRANSFER Knob - - - - - - - - - - - - - - - - - - - - - - - - - AS REQUIRED
6. YD or AP Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - AS DESIRED
7. Land as soon as practical.
PROCEDURE COMPLETED
1. L/R SPEED BRAKE Circuit Breakers - - - - - - - - - - - - - - - - - - - - - CHECK
2. SPD BRK Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - RETRACT
(try switches on both throttle knobs)
3. Land as soon as practical. If enroute, consider effect of extended speed
brakes on range.
4. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - VREF + 10
5. Landing Distance/Weight:
C A U T I O NCAUTION
　
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