|
Specifications |
|
|
 |
 |
|
Length |
18' 3" |
5.56 m |
20.5' |
6.25
m |
|
Wing Span |
24' |
7.32 m |
28' |
8.5
m |
|
Height |
4' 8" |
1.42 m |
7'
2" |
2.2
m |
| Cabin Width |
23" |
cm |
28" |
71
cm |
|
Wing Area |
84.4 sq ft |
7.841 mē |
126 sq ft |
11.7 mē |
| Wing Loading |
10
lbs / sq ft |
4.54 kg /
0.09
mē |
10 lbs / 0.09
mē |
4.54 kg / 0.09
mē |
|
Empty Weight |
560 lbs |
254 kg |
721 lbs |
327
kg |
|
Gross Weight |
850 lbs |
385 kg |
1320 lbs |
599
kg |
|
Useful Load |
290 lbs |
131.5 kg |
599 lbs |
272
kg |
|
Design Load |
3.8 G's |
3.8 G's |
|
Fuel (92
Octane Auto) |
10.5 Gal |
39.7 L |
20.0 Gal |
77.6 L |
|
Engine |
1700cc
VW 55 Hp
(Optional: 1835cc through 2180cc) |
Revmaster R2300
85 Hp |
|
Propeller |
54/38 |
56/48 Combo
54/50 Cruise |
|
Electrical
System |
Starter,
Alternator |
|
Brakes |
Hydraulic
Disc/Toe Brakes |
|
Airframe
Construction |
6061-T6 Aluminum
- Airframe
Fiberglass - Cowl, wing tips & wheel pants |
|
Notes |
-
The "Wide &
Tall" version began
with plans number 102.
-
Aircraft
may be flown with canopy off, but not open.
The
wings are removable for transport in ~20 minutes.
|
|
|
Performance |
|
|
(at 750 lb / 340 kg with 1700cc
Engine)
|
|
|
Cruise (75%
Power) |
125 mph |
201
km/h |
120 mph |
193 km/h |
|
Stall (Vso) |
40 mph |
64 km/h |
42 mph |
67.6
km/h |
|
Rate of Climb (Vy) |
850 fpm at
75 mph |
259 m/min at
120 km/h |
1000 fpm
at 75 mph |
305 m/min at 120 km/h |
|
Never Exceed
Speed (Vne) |
155 mph |
km/h |
155 mph |
249.4 km/h |
|
Best Decent
Speed |
63 mph |
101 km/h |
65 mph |
105 km/h |
|
Best Angle of
Climb (Vx) |
63 mph |
101 km/h |
65 mph |
105 km/h |
|
Take-Off Roll |
700 ft |
213 m |
700 ft |
213 m |
|
Max. Ceiling |
10,000 ft |
3048 m |
10,000 ft |
3048 m |
|
CX4
Load Test Photo's |
|
3.8G
Load Test - CX4
5.7G
Load Test - CX4
Fin Load Test - CX4
Stabilizer Load Test - CX4
|
