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• Maximum crosswind limit is 10 knots.
• Avoid landing with a tailwind.
PROCEDURE COMPLETED
3  AILERON TRIM INOPERATIVE
4  RUDDER TRIM INOPERATIVE
5  SPEED BRAKES FAIL TO RETRACT
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.
510CLEAP-07 AA 53
N
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
1. L/R SPEED BRAKE Circuit Breakers - - - - - - - - - - - - - - - - - - - - - CHECK
2. SPEED BRAKE Switch - - - - - - - - - - - - - - - - - - - RETRACT OR EXTEND
to achieve zero roll
• IF SPEED BRAKES ARE EXTENDED
3. Refer to SPEED BRAKES FAIL TO RETRACT; Tab N5.
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
C A U T I O NCAUTION
• Avoid landing with a tailwind.
• Maximum crosswind limit is 10 knots.
• The amount of aileron trim required will increase as flap deflection is
increased. At flaps land and VREF, nearly full opposite aileron trim may be
required.
PROCEDURE COMPLETED
1  SPEED BRAKES OPERATE ASYMMETRICALLY
FLAPS STALL
WARNING
WEIGHT - POUNDS
6000 6500 7000 7500 8000 *8645
TO/APR NORMAL
HIGH
97
108
101
112
105
115
108
119
111
122
115
127
LAND NORMAL 92 95 98 101 104 108
* Use in an emergency which requires landing at weights in excess of 8000 pounds.
FLAPS STALL
WARNING
*MULTIPLY LANDING DISTANCE
BY
*REDUCE MAXIMUM LANDING
WEIGHT BY
TO/APR NORMAL
HIGH
1.37
1.22
50 lbs
40 lbs
LAND NORMAL 1.28 50 lbs
* Basic landing distance and weight values must be obtained from the appropriate landing
performance charts based on the STALL WARNING and ANTI-ICE system settings.
54 AA 510CLEAP-07
O
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
1. FLAP Handle - - - - - - - - - - - - - - - - - - - - RESET TO PREVIOUS DETENT
2. FLAPS Circuit Breaker - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
(L circuit breaker panel)
• IF FLAPS FAIL CAS MESSAGE AND RED “X” ON FLAP INDICATOR
CLEAR, AND FLAPS OPERATE NORMALLY
PROCEDURE COMPLETED
• IF FAILURE INDICATIONS REMAIN DISPLAYED OR FLAPS FAIL TO
MOVE
 IF FLAP POSITION IS KNOWN
3. Airspeed - Stay below appropriate flap limit speed:
a. Flaps UP- - - - - - - - - - - - - - - - - - - - - - - -250 KIAS MAXIMUM
b. Flaps TO/APR - - - - - - - - - - - - - - - - - - - -185 KIAS MAXIMUM
c. Flaps LAND- - - - - - - - - - - - - - - - - - - - - -150 KIAS MAXIMUM
o IF FLAPS ARE IN UP OR TO/APR POSITION
4. Refer to FLAPS INOPERATIVE APPROACH AND LANDING
(Flaps not in Landing Position); Tab AC2.
PROCEDURE COMPLETED
o IF FLAPS ARE IN THE LAND POSITION
4. Land as soon as practical.
5. Landing data - Use normal landing data and procedures.
PROCEDURE COMPLETED
 IF FLAP POSITION IS UNKNOWN (RED “X” ON FLAP INDICATOR)
1. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - -150 KIAS MAXIMUM
2. Refer to FLAP INOPERATIVE APPROACH AND LANDING (Flaps
not in Landing Position); Tab AC2.
PROCEDURE COMPLETED
2  FLAPS FAIL (FLAPS FAIL TO MOVE, OR FLAPS MOVE
UNCOMMANDED, RED “X” ON FLAP INDICATOR)
510CLEAP-07 AA 55
O
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
Indicates engine inlet temperature is below safe level for satisfactory ice protection.
1. ENGINE ANTI-ICE Switches (both sides) - - - - - - - - - - - - - - OFF then ON
2. Throttle (affected engine) - - - - - - - - - - - - - - - - - - - - - - - - - - - INCREASE
3. Respective ENGINE ANTI-ICE circuit breaker - - - - - - - - - - - - - - - CHECK
• IF MESSAGE REMAINS DISPLAYED
4. Respective ENGINE ANTI-ICE circuit breaker - - - - - - - - - - - - - - -PULL
5. Monitor engine inlet. If ice is accumulating, exit icing environment.
　
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