|
| Span |
Area |
Empty Weight |
Payload |
Gross Weight |
Wing Load |
Water Ballast |
| m |
ft |
sq.m |
sq.ft |
kg |
lb. |
kg |
lb. |
kg |
lb. |
kg
/sq.m |
lb.
/sq.ft |
kg |
lb. |
| 15 |
49.2 |
13.77 |
148.2 |
268 |
590 |
100 |
220 |
368 |
819 |
26.73 |
5.47 |
0 |
0 |
| Aspect
ratio: |
16.2 |
| Airfoil: |
Gottingen 549 |
| Structure: |
wood, plywood, ceconite |
| Engine: |
|
Comment:
The Chiricahua was designed to comply with the
Standard Class rules existing at the time
construcion started, 1959, the first flew in
1970. It has a fixed main wheel and top surface
Schempp-Hirth type airbrakes for approach control. |
|