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VREF (KIAS)
LANDING DISTANCE
CAUTION
• 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
(Continued Next Page)
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 lbs.
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.
510FM-07 AA 3-121
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 FLAPS INOPERATIVE APPROACH AND LANDING
(FLAPS NOT IN LANDING POSITION) (Continued)
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
 LANDING WITH FAILED PRIMARY FLIGHT CONTROL
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.
NOTE
Establish a long, straight-in final and minimize maneuvering.
• AILERON
1. Use rudder for primary directional and lateral control. Use aileron trim as required to
supplement rudder for lateral control.
CAUTION
Limit bank angles to 15maximum.
2. If possible, choose a runway with the least possible crosswind.
PROCEDURE COMPLETED
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3-122 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
　
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