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DYNAMIC WT9
PERFORMANCE - SPECIFICATIONS - 3 View Drawing |
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SPECIFICATIONS
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Wing span
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29.2 ft.
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Wing area
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110.87 sq ft
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Wing aspect ratio
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7.82
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Length
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21 ft.
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Height
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6.5 ft
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Cockpit Width
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46 in
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Mean Aerodynamic
Chord (MAC)
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46.65 in
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Control
surfaces
Aileron
span
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49.21 in
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Aileron area
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423.15 sq in
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Flap span
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7.48 ft.
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Flap area
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8.07 sq ft
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Horizontal tail
span
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7.78 ft.
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Horizontal tail
area
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18.08 sq ft
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Vertical tail
span
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3.35 ft
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Vertical tail
area
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10.98 sq ft
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Landing gear
Wheel spacing
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4.88 ft.
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Wheel base
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7.44 ft.
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Main wheel
diameter
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13.78 in
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Nose wheel
diameter
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12.6 in
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Weights
Empty weight
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660 lbs
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Maximum take-off
weight
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1212 lbs
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Useful load
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552 lbs
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Fuel tanks
capacity
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26.4 US
gal
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PERFORMANCE
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SLSA
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EAB
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Takeoff Distance
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610 ft.
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610 ft.
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Takeoff Distance 50 ft object
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1450 ft.
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1450 ft.
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Rate of Climb
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1200 fpm
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1200 fpm
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Max operating altitude
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10000 ft.
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18000 ft.
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Stall speed w /flaps Vs0
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32 mph |
32 m.p.h.
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Maximum cruise speed
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138 mph
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174 m.p.h.
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Cruise range w/reserve
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750 nm |
750 n.m.
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Landing Distance
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600 ft
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600 ft.
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Landing Distance 50-ft. obstacle
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1400 ft |
1400 ft.
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Velocity Maneuvering Va
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98 mph |
98 m.p.h.
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Velocity Never Exceed
Vne
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174 mph
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174 m.p.h.
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ROTAX 912 UL
(59,6 kW) Max Take Off RPM 5800 1/min
ROTAX 912 ULS (73 kW) Max Take Off
RPM 5800 5/min
Figures based on DUC SWIRL 3-bladed ground
adjustable propeller. Propeller diameter is
66,93 in.
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