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3. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE if required to reduce control force
4. RUDDER TRIM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 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
NOTE
• If time permits, transfer fuel to create a fuel imbalance of up to 200 lbs, to assist in
reducing roll control forces.
• An amber AIL or AIL message may be displayed with the autopilot engaged.
The autopilot will function normally with this message displayed. Expect some
aileron control force when the autopilot is disconnected.
7. Land as soon as practical.
PROCEDURE COMPLETED
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.
3-80 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 RUDDER TRIM INOPERATIVE
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
NOTE
• If time permits, transfer fuel to create a fuel imbalance of up to 200 lbs to assist in
reducing rudder control forces.
• An amber RUD or RUD message may be displayed with the autopilot
engaged. The autopilot will function normally with this message displayed. Expect
some rudder control force when the autopilot is disconnected.
7. Land as soon as practical.
PROCEDURE COMPLETED
 SPEED BRAKES FAIL TO RETRACT
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:
CAUTION
• Maximum crosswind limit is 10 knots.
• Avoid landing with a tailwind.
PROCEDURE COMPLETED
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.
510FM-07 AA 3-81
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 SPEED BRAKES OPERATE ASYMMETRICALLY
1. L/R SPEED BRAKE Circuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
2. SPD BRK Switch . . . . . . . . . . . . . . . . . . . . . . RETRACT OR EXTEND to achieve zero roll
• IF SPEED BRAKES ARE EXTENDED
3. Refer to Abnormal Procedures, SPEED BRAKES FAIL TO RETRACT.
PROCEDURE COMPLETED
• IF SPEED BRAKES ARE RETRACTED
3. Land as soon as practical.
PROCEDURE COMPLETED
• IF UNABLE TO ACHIEVE SYMMETRIC SPEED BRAKE
DEPLOYMENT
3. AILERON TRIM . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED to reduce control forces
4. Land as soon as practical. If enroute, consider effect on range.
5. If field length permits, use Flaps TO/APR for landing.
6. Landing Data - Refer to the following tables:
VREF (KIAS)
Landing Distance / Maximum Landing Weight
CAUTION
• Avoid landing with a tailwind.
• Maximum crosswind limit is 10 knots.
　
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