The Fiat CR.42 Falco, meaning falcon, was a single-seat sesquiplane fighter built by Fiat Aviazione and flown mainly by the Italian Regia Aeronautica. It developed the earlier CR.32, adding a more powerful supercharged Fiat A.74 air-cooled radial engine and other improvements. Although a biplane that was outclassed in speed and firepower by monoplane fighters, it was strongly built and very agile because of its low wing loading. It entered service in May 1939 and fought in the Battle of France, the Battle of Britain, over Malta, North Africa and Greece, and later on the Eastern Front and in Iraq. Belgium, Sweden and Hungary also flew it. More than 1,800 were built, making it the most numerous Italian aircraft used in the Second World War, and it later served as a trainer and with the Luftwaffe.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Fiat CR.42 Falco (Wikipedia)
Of Make
Source Fiat CR.42 Falco (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Fiat CR.42 Falco (Wikipedia)LeadQuote, Lead
The Fiat CR.42 Falco (Falcon, plural: Falchi) is a single-seat sesquiplane fighter developed and produced by Italian aircraft manufacturer Fiat Aviazione.
Originated In
Also in Geography Atlas: where this subject originated.
Source Fiat CR.42 Falco (Wikipedia)LeadQuote, Lead
The Fiat CR.42 Falco (Falcon, plural: Falchi) is a single-seat sesquiplane fighter developed and produced by Italian aircraft manufacturer Fiat Aviazione.
Sources
1. Fiat CR.42 Falco (Wikipedia)
Lead
The Fiat CR.42 Falco (Falcon, plural: Falchi) is a single-seat sesquiplane fighter developed and produced by Italian aircraft manufacturer Fiat Aviazione.
Origins
During May 1939, the CR.42 entered service with the Regia Aeronautica
Specifications (CR.42)
Powerplant: 1 × Fiat A.74 R.C.38 14 cylinder air-cooled radial piston engine, 627 kW (841 hp)
Specifications (CR.42), top speed
Maximum speed: 441 km/h (274 mph, 238 kn) at 6,100 m (20,000 ft)
Specifications (CR.42), mass
Empty weight: 1,782 kg (3,929 lb)
Specifications (CR.42), maximum mass
Gross weight: 2,295 kg (5,060 lb)
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