CAUDRON C.60 Civil Aircraft Model Details

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General Information of CAUDRON C.60

Developed From : Caudron C.59

Manufacturer : Caudron

Primary Users : French Air Force; Finnish Air Force; Latvian Navy; Venezuelan Air Force; Spanish Republican Air Force

Role : Training aircraft

General characteristics of CAUDRON C.60

Crew : two

Empty Weight : 505 kg (1,111 lb)

Height : 2.60 m (8 ft 6 in)

Length : 7.50 m (26 ft 7 in)

Loaded_Weight : kg (lb)

Max Takeoff Weight : 862 kg (1,896 lb)

Powerplant : 1 × Clerget 9B radial engine, 97 kW (130 hp)

Useful Load : kg (kg)

Wing Area : 26.00 m² (279.7 ft²)

Wingspan : 10.24 m (33 ft 7 in)

Performance of CAUDRON C.60

Cruise Speed : km/h (knots, mph)

Maximum Speed : 150 km/h (81 knots, 93 mph)

Never Exceed Speed : km/h (knots, mph)

Power/Mass : W/kg (hp/lb)

Range : km (nm, mi)

Rate Of Climb : m/s (ft/min)

Service Ceiling : 4,000 m (13,120 ft)

Stall Speed : km/h (knots, mph)

Wing Loading : kg/m² (lb/ft²)

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