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FLAPS STALL
WARNING
WEIGHT - POUNDS
6000 6500 7000 7500 8000 *8645
UP or
UNKNOWN
NORMAL
HIGH
98
110
102
114
106
118
109
122
113
126
117
131
TO/APR NORMAL
HIGH
87
98
91
102
95
105
98
109
101
112
105
117
*Use in an emergency which requires landing at weights in excess of 8000 pounds.
FLAPS STALL
WARNING
*MULTIPLY LANDING DISTANCE BY *REDUCE MAX
LANDING
WEIGHT BY
LANDING WEIGHT
8000 LBS. OR LESS
** LANDING WEIGHT
ABOVE 8000 LBS.
UP or
UNKNOWN
NORMAL
HIGH
1.57
1.89
1.87
2.06
***40 lbs.
70 lbs.
TO/APR NORMAL
HIGH
1.12
1.00
1.12
1.00
0 lbs.
0 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.
** Use in an emergency which requires landing at weights in excess of 8000 lbs.
*** The 40 lbs. maximum landing weight reduction is only required if landing above 12,000 feet
MSL with a downhill runway gradient. Other conditions require no weight reduction.
82 AA 510CLEAP-07
AC
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
 FLAPS INOPERATIVE APPROACH AND LANDING (FLAPS NOT IN
LANDING POSITION) (Continued)
C A U T I O NCAUTION
• Avoid landing with a tailwind.
• Avoid excessive flare upon landing.
• The following systems may be inoperative:
• Stall warning horn with automatic autopilot disconnect
• Low speed awareness range on airspeed indicator
• On-speed circle
2. Seats and Seat Belts - - - - - - - - - - - - - - - - - - ADJUST AND SECURE
3. Avionics and Flight Instruments - - - - - - - - - - - - - - - - - - - - - - - CHECK
4. Minimums - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - SET
5. Passenger Seats - - - - - - - - - - - - - - - - - - - - - CHECK FULL UPRIGHT
6. PAX SAFETY Switch - - - - - - - - - - - - - - - - - - - - - - - - - - PAX SAFETY
7. FUEL TRANSFER Knob - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF
8. Anti-Ice/Deice Systems- - - - - - - - - - - - - - - - - - - - - - - - AS REQUIRED
9. ANTISKID Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -ON
10. LANDING Light Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -ON
11. CAS Messages - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
12. Crew Briefing - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - COMPLETE
BEFORE LANDING
13. LANDING GEAR Handle- - - - - - - - - - - - - - - - - -DOWN AND LOCKED
14. Pressurization - - - - - - - - - - - - - - - - - - CHECK ZERO DIFFERENTIAL
15. Autopilot and Yaw Damper - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF
16. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - VREF
17. Speed Brakes - - - - - - - - - - - - - - RETRACT PRIOR TO 50 FEET AGL
PROCEDURE COMPLETED
510CLEAP-07 AA 83
AC
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
A failed flight control is defined as a flight control surface that does not respond to
control input. The most probable cause would be a severed flight control cable. This
condition typically results in the control surface trailing to the neutral position.
• AILERON
1. Use rudder for primary directional and lateral control. Use aileron trim as
required to supplement rudder for lateral control.
C A U T I O NCAUTION
Limit bank angles to 15° maximum.
2. If possible, choose a runway with the least possible crosswind.
PROCEDURE COMPLETED
• ELEVATOR
1. Elevator Trim - - - - - - - - - - - - - - - - - - - - USE MANUAL TRIM WHEEL
in small increments to control pitch attitude
2. Make small pitch and power changes and set up landing configuration
early.
3. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -VREF+10
4. Landing Distance/Weight:
5. After touch down and nose wheel on ground, apply wheel brakes as
soon as possible.
C A U T I O NCAUTION
Avoid landing with a tailwind.
PROCEDURE COMPLETED
• RUDDER
1. RUDDER TRIM - - - - - - - - - - - - - - - - - - - - - TRIM for coordinated flight
2. If possible, choose a wide runway with the least possible crosswind.
3. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - VAPP MINIMUM
　
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