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b. Accelerate-stop distance.
c. The engine-out accelerate-go distance to 15 feet.
d. The Dry Takeoff Field Length.
No specific identification is made on the charts as to which of these
distances governs a specific case.
Wet Runway: A runway is considered wet when there is sufficient moisture on the surface
to appear reflective, but without significant areas of standing water.
7-4 AA 510FM-03
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
WET RUNWAY TAKEOFF PERFORMANCE (Continued)
EXAMPLE FOR TAKEOFF WITH FLAPS UP ON A WET RUNWAY:
Pressure Altitude = 2000 FEET Runway Gradient = ZERO (level)
Gross Weight = 8000 POUNDS Anti-Ice = OFF
Ambient Temperature = 10°C Runway Condition = WET
Wind = 10 KNOTS (HEADWIND)
From Figure 4-26, the Takeoff Field Length is 3320 FEET (dry runway, anti-ice systems off).
From Figure 7-2, the Takeoff Field Length is 3460 FEET (wet runway, anti-ice systems off). V1 = 86
KNOTS, VR = 99 KNOTS, V2 = 108 KNOTS, VENR = 118 KNOTS.
Takeoff Field Length for above conditions = 3460 FEET. V1 = 86 KNOTS, VR = 99 KNOTS, V2 = 108
KNOTS, VENR = 118 KNOTS.
EXAMPLE FOR TAKEOFF WITH FLAPS 15° ON A WET RUNWAY:
Pressure Altitude =3000 FEET Runway Gradient = ZERO (level)
Gross Weight = 7000 POUNDS Anti-Ice = ON
Ambient Temperature = 5°C Runway Condition = WET
Wind = 10 KNOTS (HEADWIND)
From Figure 4-32, the Takeoff Field Length is 2320 FEET (dry runway, anti-ice systems on).
From Figure 7-8, the Takeoff Field Length is 3180 FEET (wet runway, anti-ice systems on). V1 = 79
KNOTS, VR = 84 KNOTS, V2 = 94 KNOTS, VENR = 118 KNOTS.
Takeoff Field Length for above conditions = 3180 FEET. V1 = 79 KNOTS, VR = 84 KNOTS, V2 = 94
KNOTS, VENR = 118 KNOTS.
CONTAMINATED RUNWAY TAKEOFF PERFORMANCE
Determine the dry runway takeoff field length, V1, VR, V2, and VENR as described in Procedures for
Use of Takeoff Performance tables in Section IV of the basic FAA Approved Airplane Flight Manual.
Any runway gradient adjustment for runway field length and V1 should be applied. From Figure 7-9
(flaps UP), or Figure 7-10 (flaps 15°), determine the takeoff field length for the precipitation type and
depth.
EXAMPLE FOR TAKEOFF WITH FLAPS UP ON A CONTAMINATED RUNWAY:
Pressure Altitude = 3000 FEET Runway Gradient = ZERO (level)
Gross Weight = 8000 POUNDS Anti-Ice = OFF
Ambient Temperature = -10°C Runway Condition = 1.0 INCHES OF DRY SNOW
Wind = 10 KNOTS (HEADWIND)
From Figure 4-26, the Takeoff Field Length is 3200 FEET (dry runway, anti-ice systems off), and V1 =
98 KNOTS, VR = 99 KNOTS, V2 = 108 KNOTS, VENR = 118 KNOTS.
From Figure 7-9, for a takeoff on a runway covered with 1.0 INCHES of DRY SNOW, the takeoff field
length is 6100 FEET. V1 = 98 KNOTS, VR = 99 KNOTS, V2 = 108 KNOTS, VENR = 118 KNOTS.
510FM-05 AA 7-5
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
CONTAMINATED RUNWAY TAKEOFF PERFORMANCE (Continued)
EXAMPLE FOR TAKEOFF WITH FLAPS 15° ON A CONTAMINATED RUNWAY:
Pressure Altitude = 1000 FEET Runway Gradient = ZERO (level)
Gross Weight = 8000 POUNDS Anti-Ice = ON
Ambient Temperature = 0°C Runway Condition = 0.2 INCHES OF SLUSH
Wind = 10 KNOTS (HEADWIND)
From Figure 4-32, the Takeoff Field Length is 2400 FEET (dry runway, anti-ice systems on), and
V1 = 85 KNOTS, VR = 85 KNOTS, V2 = 93 KNOTS, VENR = 118 KNOTS.
From Figure 7-10, for a takeoff on a runway covered with 0.2 INCHES of slush, the takeoff field
length is 5250 FEET. V1 = 85 KNOTS, VR = 85 KNOTS, V2 = 93 KNOTS, VENR = 118 KNOTS.
WET AND CONTAMINATED RUNWAY LANDING PERFORMANCE
Determine the Stall Warning-NORMAL or Stall Warning-HIGH dry runway landing distance, VAPP, and
VREF as described in Procedures for Use of Approach and Landing Performance Tables in Section IV
of the basic FAA Approved Airplane Flight Manual. Any runway gradient adjustment for runway
landing distance should be applied. From Figure 7-11 (VREF, Stall Warning-NORMAL), Figure 7-12
(VREF+10 KNOTS, Stall Warning-NORMAL), Figure 7-13 (VREF, Stall Warning-HIGH), and Figure 7-14
(VREF+10 KNOTS, Stall Warning-HIGH), determine the landing distance for the precipitation type and
depth. The difference between the VREF table and the VREF+10 KNOTS table presents the
comparison in distances of an overspeed at VREF.
NOTE
The published limiting maximum tailwind component for this airplane is 10 knots,
however, landings on precipitation covered runways with any tailwind component are
not recommended.
EXAMPLE FOR LANDING ON A WET OR CONTAMINATED RUNWAY:
Pressure Altitude = 1000 FEET Runway Gradient = ZERO
Gross Weight = 7000 POUNDS Stall Warning = NORMAL
Ambient Temperature = 5°C Runway Condition = WET
　
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