Caspar CLE 16 From Wikipedia, the free encyclopedia Type of aircraft The Caspar CLE 16 was an airliner built in Germany in the early 1920s. Only one CLE 16 was built (registration D-294), and it took part in the International Air Exhibition in Gothenburg (Sweden) in July 1923.[1] Specifications Data from [1]General characteristics Crew: One Capacity: 3 passengers Length: 6.72 m (22 ft 1 in) Wingspan: 12.00 m (39 ft 4 in) Height: 2.20 m (7 ft 3 in) Wing area: 19.00 m2 (204.5 sq ft) Empty weight: 450 kg (992 lb) Gross weight: 830 kg (1,830 lb) Powerplant: 1 × Siemens-Halske Sh 5 7-cylinder air-cooled radial piston engine, 60 kW (80 hp) Propellers: 2-bladed fixed pitch propeller Performance Maximum speed: 130 km/h (81 mph, 70 kn) Cruise speed: 105 km/h (65 mph, 57 kn) Range: 480 km (300 mi, 260 nmi) Endurance: 6 hours Service ceiling: 3,000 m (9,800 ft) References 1 2 "Caspar CLE 16". Histaviation.com. Retrieved 27 February 2019. This article on an aircraft of the 1920s is a stub. You can help Wikipedia by expanding it.vte Related Articles~TimelinesTop QsFact Checks
