Super Blanik L 23 LET   


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General Details
Manufacturer: LET
Plane Name:

Super Blanik L 23

Classified as: Unclassified
Country Of Origin: Czech Republic
Designer:
No. of Seats 2
No. Built 0
   
Performance:
L/DMax: 27 87 kph / 47 kt / 54 mph
   
MinSink: 0.85 m/s / 2.8 fps / 1.66 kt
   


 

Specifications:
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


           

Your Comments:
   RE: 264
        Manufacturer - 264 - Posted by: Michal Stepan (07/Jan/2005) Reply

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