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a. 115 percent of the two-engine horizontal takeoff distance from
start to a height of 35 feet above runway surface.
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.
510FM-S4-01 S4-AA S4-77
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
ADVERSE 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 S4-11
(Flaps UP) or Figure S4-12 (Flaps 15°), determine the takeoff field length for the precipitation type
and depth.
NOTE
• Interpolation of data between depths of contamination is not permitted.
• Wet Snow Covered Runway performance data is the same as Slush Covered
Runway performance data.
EXAMPLE FOR TAKEOFF WITH FLAPS UP:
From Takeoff Field Length - Feet, Flaps UP (Anti-Ice ON) in Section IV, PERFORMANCE, TAKEOFF
of the basic FAA Approved Airplane Flight Manual, the Takeoff Field Length is 3200 FEET (dry
runway, anti-ice on).
V1 = 98 KNOTS, VR = 99 KNOTS, V2 = 108 KNOTS, VENR = 118 KNOTS.
From Figure S4-11 for a takeoff on a runway covered with 0.2 inches of slush, the takeoff field length
is 7700 FEET. V1 = 98 KNOTS, VR = 99 KNOTS, V2 = 108 KNOTS, VENR = 118 KNOTS.
EXAMPLE FOR TAKEOFF WITH FLAPS 15°:
From Takeoff Field Length - Feet, Flaps 15° (Anti-Ice ON) in Section IV, PERFORMANCE, TAKEOFF
of the basic FAA Approved Airplane Flight Manual, the Takeoff Field Length is 2400 FEET (dry
runway, anti-ice ON).
V1 = 83 KNOTS, VR = 84 KNOTS, V2 = 93 KNOTS, VENR = 118 KNOTS.
From Figure S4-12 for a takeoff on a runway covered with 0.2 inches of slush, the takeoff field length
is 5250 FEET. V1 = 83 KNOTS, VR = 84 KNOTS, V2 = 93 KNOTS, VENR = 118 KNOTS.
Pressure Altitude = 1000 FT Runway Gradient = ZERO (level)
Gross Weight = 8000 POUNDS Anti-Ice = ON
Ambient Temperature = +10°C Runway Condition = 0.2 INCHES OF SLUSH
Wind = 10 KNOTS (HEADWIND)
Pressure Altitude = 5000 FEET Runway Gradient = ZERO (level)
Gross Weight = 7500 POUNDS Anti-Ice = ON
Ambient Temperature = +5°C Runway Condition = 0.2 INCHES OF SLUSH
Wind = 20 KNOTS (HEADWIND)
S4-78 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-11*
510FM-S4-01 S4-AA S4-79
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-12*
S4-80 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
ADVERSE RUNWAY LANDING PERFORMANCE
Determine the 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 S4-13 (VREF, Stall Warning - NORMAL), Figure S4-14 (VREF + 10 KNOTS, Stall Warning -
NORMAL), Figure S4-15 (VREF, Stall Warning - HIGH), and Figure S4-16 (VREF + 10 KNOTS, Stall
Warning - HIGH) determine the landing distances 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
• Multiplying landing distances from Figures S4-13, S4-14, S4-15 and S4-16 by
1.15 can be used in showing compliance with JAR Operations (JAR-OPS 1.520).
• Interpolation of data between depths of contamination is not permitted.
• 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 WITH FLAPS LAND:
From Landing Distance - Feet, Flaps Land, in Section IV, PERFORMANCE, APPROACH AND
LANDING, of the basic FAA Approved Airplane Flight Manual, the Landing Distance is 2000 FEET
(dry runway, anti-ice OFF). VAPP = 95 KNOTS, VREF = 88 KNOTS.
From Figure S4-13 for a landing at VREF (VREF = 88 KNOTS) on a runway covered with 0.125 inches
of water, the landing distance is 3150 FEET.
FOR COMPARISON OF OVERSPEED:
From Figure S4-14 for a landing at VREF + 10 KNOTS (VREF = 98 KNOTS) on a runway covered with
0.125 inches of water, the landing distance is 4000 FEET.
　
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