Caspar C 36
Type
2-seat reconnaissance
2-seat reconnaissance floatplane  , W
Engine
1 BMW VI 6.0 Z with 2-blade wooden prop. Ø 3.92 m and pitch 2.76 m
Dimensions
Length , height , span 14.0 m, wingarea 49.5 m2
Length 11.56 m, height 4.43 m, span 14.0 m, wingarea 49.5 m2
Weights
Empty 2264 kg, crew 160 kg, fuel and oil 481 kg, flying weight 3000 kg
Empty 2564 kg, crew 160 kg, fuel and oil 481 kg, flying weight 3300 kg, fuel
880 l, oil 55 l
Performance
Max. speed at sea level 255 km/h, climb to 1000 m 3 min., cruising speed
225 km/h, landing speed 110 km/h
Max. speed at sea level 243 km/h, at 2000 m 238 km/h, at 4000 m 219 km/h,
at 5000 m 195 km/h, climb to 1000 m 3 min.36 sec., to 2000 m 8 min., to
4000 m 21 min. 42 sec., to 5000 m 44 min.,  cruising speed 180 km/h,
landing speed 116 km/h, range 1050 km, service ceiling 5360 m, take off run
360 m
Type
Werk.Nr
Registration
History
Land , W , aW
7013
D-1316
In June 1929 to RDL Erprobungsstelle , Travem√ľnde. Unregistered from Jan. 1932
aW = modified with slots