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Caproni Ca.125

General Aviation and Light Aircraft

The Caproni Ca.125 was a single-engine, tandem two-seat touring biplane built in Italy in 1933 that could be operated either as a landplane or as a seaplane. It was a wire-braced single-bay biplane with slender elliptical wings of unequal span, the lower wing the longer, so that the pairs of parallel interplane struts leaned inwards, and the wings had neither stagger nor sweep, with ailerons on the lower planes only. In contrast to the elegant wing plan the fuselage was deep and portly, partly because of the enclosed tandem cockpits, whose rooflines followed the upper fuselage so that the crew sat low with poor forward views. A 101 kilowatt Colombo S.63 six-cylinder air-cooled inline engine gave a maximum speed of 220 kilometres per hour, and the landplane weighed 545 kilograms empty.

Facts
Year
1933 1
Top Speed (km/h)
220 1
Mass (kg)
545 1
Maximum Mass (kg)
815 1
Engine
Colombo S.63 six-cylinder air-cooled upright inline engine 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Caproni Ca.125 (Wikipedia)

Of Make

Source Caproni Ca.125 (Wikipedia)
Sources
1. Caproni Ca.125 (Wikipedia)
  • Lead
    was a single-engine, tandem two-seat, touring biplane built in Italy in 1933
  • Lead, year
    built in Italy in 1933
  • Specifications (landplane)
    1 × Colombo S.63 six-cylinder air-cooled upright inline
  • Specifications (landplane), top speed
    Maximum speed: 220 km/h (140 mph, 120 kn)
  • Specifications (landplane), mass
    Empty weight: 545 kg (1,202 lb)
  • Specifications (landplane), maximum mass
    Max takeoff weight: 815 kg (1,797 lb)
  • Lead, manufacturer
    The Caproni Ca.125 was a single-engine, tandem two-seat, touring biplane built in Italy in 1933
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