Condor 4 Schleicher   


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General Details
Manufacturer: Schleicher
Plane Name:

Condor 4

Classified as: Unclassified
Country Of Origin: Germany
Designer: Heini Dittmar
No. of Seats 2
No. Built 18
   
Performance:
L/DMax: 31 80 kph / 43 kt / 50 mph
   
MinSink: 0.70 m/s / 2.3 fps / 1.36 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.
18 59.2 21.2 230 358 789 202 445 560 1234 26.4 5.37 0 0
Aspect ratio: 15.2
Airfoil: Go 532, NACA 0012
Structure: wood/ fabric wings and tail, steel-tube/ fabric fuselage
Engine:

Comment:
A postwar development of the pre-World War II single-seat Condor seriesm the two-seat Condor 4 first flew in 1953. It has balanced DFS upper and lower surface airbrakes for approach control and a skid with jettisonable dolly for takeoff.


           

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