Caspar C.36

In 1928, Caspar Werke AG released a reconnaissance seaplane, designated as the Caspar C.36. This two-seater, single-strut biplane was equipped with a powerful 660 hp BMW VI 6Z engine.

Development and Technical Specifications

The sole prototype of the aircraft (Werk.N. 7013) underwent extensive testing, both as a floatplane (C.36w) and as a wheeled aircraft for land use. Despite its design and successful tests, no orders were received, which sadly became one of the reasons for the company’s bankruptcy.

Operational History and Final Fate

In June 1929, the C.36 was transferred to the RDL Erprobungs Stelle, where it was assigned the civilian registration number D-1316. Its service was brief, as in January 1932, the aircraft was officially written off.

Technical Specifications

Modification	C.36w
Wingspan, m	14.00
Length, m	11.56
Height, m	4.43
Wing area, m2	49.50
Empty weight	2264
Maximum takeoff weight	3000
Engine type	1 Piston engine BMW VI 6Z
Power, hp	1 x 660
Maximum speed, km/h	255
Cruising speed, km/h	225
Practical range, km	1050
Rate of climb, m/min	333
Practical ceiling, m	5360
Crew, crew members	2

Image gallery of the Caspar C.36