The Caspar C 33 was a training aircraft developed in Germany in the late 1920s.

Specifications

Data from ^[1]

General characteristics

• Crew: 2
• Length: 5.30 m (17 ft 5 in)
• Wingspan: 8.00 m (26 ft 3 in)
• Empty weight: 490 kg (1,080 lb)
• Gross weight: 750 kg (1,653 lb)
• Powerplant: 1 × Armstrong-Siddeley Mongoose 5-cylinder air-cooled radial piston engine, 101 kW (135 hp)
• Propellers: 2-bladed fixed pitch propeller

Performance

• Maximum speed: 160 km/h (99 mph, 86 kn)
• Cruise speed: 130 km/h (81 mph, 70 kn)