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• 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
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 lbs.
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 maximum landing weight values must be obtained from the
appropriate landing performance charts based on the STALL WARNING and ANTI-ICE system
settings.
3-82 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 FLAPS FAIL (FLAPS FAIL TO MOVE OR FLAPS MOVE
UNCOMMANDED, RED “X" ON FLAP INDICATOR)
1. FLAP Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RESET TO PREVIOUS DETENT
2. FLAPS Circuit Breaker (L circuit breaker panel) . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
• 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 Abnormal Procedures, FLAP INOPERATIVE APPROACH AND
LANDING.
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)
3. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 150 KIAS Maximum
4. Refer to Abnormal Procedures, FLAP INOPERATIVE APPROACH AND LANDING.
PROCEDURE COMPLETED
510FM-07 AA 3-83/3-84

MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
ICING
 ENG A/I COLD L-R - AMBER (ENGINE ANTI-ICE COLD)
Indicates that the 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.
PROCEDURE COMPLETED
• IF MESSAGE CLEARS
PROCEDURE COMPLETED
 P/S HTR L-R (PITOT-STATIC HEATER)
Indicates that no current is flowing to the pitot probe or static port heaters.
• IN FLIGHT
1. Pitot-Static Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PITOT-STATIC
2. Circuit Breaker . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
3. Airspeed/Altitude (affected system) . . . . . . . . . . . . COMPARE with unaffected system
NOTE
If pilot system is affected, the standby airspeed and altitude will also be affected.
 IF AIRSPEED AND ALTITUDE NOT NORMAL
4. SENSOR Softkey (affected side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
5. ADC1/2 Softkey. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS appropriate softkey
6. PFD ADI Displays . . CONFIRM “BOTH ON ADC1 or 2" is displayed on both PFDs
7. Exit icing environment. Consider impact on RVSM capability.
PROCEDURE COMPLETED
 IF AIRSPEED AND ALTITUDE NORMAL
4. Continue to monitor.
　
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