|
| 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. |
| 16.2 |
53.1 |
19.15 |
206.1 |
310 |
683 |
200 |
441 |
510 |
1124 |
26.63 |
5.45 |
0 |
0 |
| Aspect
ratio: |
13.7 |
| Airfoil: |
NACA 63/2A-615, root; 63/2A-612, tip |
| Structure: |
all metal, except for fabric control surfaces, GFRP wingtips |
| Engine: |
|
Comment:
The Super Blanik, which first flew in 1988, is a
development of the L 13 Blanik, but without
flaps. It has a T-tail, DFS type airbrakes and a
swiveling tail wheel. It retains the semi-
retractable shock absorbed main wheel of the L
13. The opening part of the cockpit canopy is in
two pieces, the front cockpit cover opening
sideways and the rear moving up and back over
the center fuselage. Wingtip extensions are
optional, increasing the span to 18.2 m./ 59.7
ft., however, aerobatics are only permitted when
the extensions are not fitted. ATC |
|
