Caproni Ca.125

The Caproni Ca.125 was a single-engine, tandem two-seat, Prototype Reconnaissance biplane built in Italy in 1933.

A Ca.125 idro version was also flown, its wheels replaced by a pair of duralumin floats, attached by struts to the lower fuselage

Specifications

Capacity

Two

Length

7.25 m (23 ft 9 in)

Wingspan

8.85 m (29 ft 0 in)

Height

2.25 m (7 ft 5 in)

Wing area

19.0 m2 (205 sq ft)

Empty weight

545 kg (1,202 lb)

Max take-off weight

815 kg (1,797 lb)

Fuel capacity

120L (31.7gal; 26.4 Impgal)

Powerplant

1 × Colombo S.63 six-cylinder air-cooled upright inline, 101 kW (135 hp)

Propellers

2-bladed

Performance

Maximum speed

220 km/h (140 mph, 120 kn)

Stall speed

80 km/h (50 mph, 43 kn)

Range

900 km (560 mi, 490 nmi)

Service ceiling

5,500 m (18,000 ft)