Experimental
Piston

LSA

Jet

4 Place Experimental

Wing span
Wing Cord (root)
Wing cord (tip)
Wing area
Wing airfoil section
Wing aspect ratio
Wing loading (gross weight)
Carnard span
Carnard chord (root)
Carnard chord (tip)
Carnard area
Carnard airfoil section
Carnard aspect ratio
Horizontal tail span
Horizontal tail chord
Horizontal tail area
Horizontal tail airfoil section
Horizontal tail aspect ratio
Length overall
Fuel capacity
Empty weight
Gross weight
Wheel base
Landing gear

30.00 ft.
4.91 ft.
3.16 ft.
125. sq. ft.
NASA (NLF-0215)
7.44
12.18 lb./sq. ft.
7.9 ft.
1.33 ft.
.067 ft.
7.90 sq. ft.
NASA (NLF-0215)
8.35
7.90 ft.
2.00 ft.
15.80 sq. ft.
NASA (63218)
3.96
17.92 ft.
30 gallons
860 lbs.
1620 lbs.
71 in.
Fixed

I
N

D
E
V
E
L
O
P
M
E
N
T

I
N

D
E
V
E
L
O
P
M
E
N
T

I
N

D
E
V
E
L
O
P
M
E
N
T

X-Piston PERFORMANCE:
Engine:

Max speed level flight sea level
Cruising speed 75% power
Stall speed (gross weight)
Initial rate of climb at sea level
Range @ 75% power (no reserve)
Maneuvering speed
Never exceed speed
G-limits at gross weight

200 mph
170 mph
58 mph
1500 ft/min
714 miles
135 mph
240 mph
+6.4 / -3.2

CABIN SPECIFICATIONS:

Cabin width
Cabin height
Seating
Controls
Baggage area

43.00 in.
39.00 in.
2 place (side by side)
Center stick / dual controls
24 cubic feet