Overall Dimensions
Wing Span	27'4"	8.33m
Length	21'9"	6.64m
Height	6'4"	1.94m
Wing
Section	NACA 64A 515 modified
Area	134 sqft	12.5 sqm
Aspect Ratio	5.55:1
Dihedra @ 40% chord	6d 18'
Setting at wing root	7d 30'
Linear Warp	-0.0 34'/m
Ailerons	Frise type, statically balanced
Area	2x 5.3sqft	2x 0.49 sqm
Control	Cable
Flaps	Slotted Type, Electric Deployment
Area	2x 6.4 sqft	2x0.6 sqm
Tail Plane	Monoblock
Control	Cable
	Static Balanced at 80%
Area	22.2 sqft	2.06 sqm	(upgraded to 2.35 later)
Anti-Tab	Automatic Trim
Fin and Rudder
Fin Area	3.7 sqft	0.35 sqm
Rudder
Control	Cable
	Static Balance at 45%
	Aerodynamic Balanced by horn
Rudder Area	6.1 sqft	0.57 sqm
Performance Data	OEM	CAA
Empty Weight	515Kg
Maximum Weight	780kg
Cruise Speed	116KT
Range	4.5Hr	554 Miles
Range @ 10,000ft	5.75 Hr	670 Miles
Rate of Climb	750 ft/min	550 ft/min
Ceiling	12800 ft	10800ft
Distance to 50ft	593m	654m
Stall Flaps	50KT	idling
Stall Clean	60KT	idling
Fuel	100LL AVGAS	118L
Engine	Lycoming 0-235-H2C
Max Rated Power	118 HP @ 2700 RPM
Max Continous	108 HP @ 2600
Speeds	Knots
Vne	160
Vno	131
Vc	131
Va	131
Load Limits	Gravity = 1G
Clean Configuration	+ 4.4G - 1.8G
Flaps	+ 2.0G