Caproni Ca.310

· World War II
Airplanes
Length
12.2 m
Flat Wing Span
16.2 m
Height
3.52 m
Flat Wing Area
38.7 m²
Cruise Speed
285 km/h
Max Speed
365 km/h
Max Ceiling
7000 m
Number of Engines
2
First Flight
1937-02-20
Entry Into service
1938-01-01
Number Built
312
Maximum Take-Off Weight
4.65 t (paragliders: kg)
Maximum Range
1690 km

Pictures

No pictures yet for this family.

Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Caproni Ca.310 4.65 1690

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
Dornier Seastar Pratt & Whitney Canada PT6 12.7 17.74 Compare
Douglas T2D 12.8016 17.3736 Compare
Yakovlev Yak-200 Shvetsov ASh-21 12.95 17.45 Compare
Messerschmitt Me 410 Hornisse 12.192 16.1544 Compare
Kyūshū Q1W Tōkai 12.09 16 Compare
Beijing 1 Ivchenko AI-14 12.15 16.4 10 Compare
All data (22 fields)
Name
Caproni Ca.310
Manufacturer
World War II
Description
The Caproni Ca.310 Libeccio (Italian: southwest wind) was an Italian monoplane, twin-engine reconnaissance aircraft used in World War II.
First Flight
1937-02-20
Entry Into service
1938-01-01
Service End
1948-01-01
Designer
Cesare Pallavicino
Type
Reconnaissance
Length (m)
12.2
Height (m)
3.52
Cockpit Crew
3
Max Speed (km/h)
365
Cruise Speed (km/h)
285
Max Ceiling (m)
7000
Armament
:*3 × 7.7 mm (0.303 in) Breda-SAFAT machine guns (2 fixed forward firing mounted in the wing roots; 1 in a dorsal turret); up to 450 kg (992 lb)
Number Built
312
Powerplant Description
2 × Piaggio Stella P.VII C.16/35 7-cylinder air-cooled radial piston engine, 350 kW (469 hp) each
Primary Users
Regia Aeronautica, Hungarian Air Force, Royal Norwegian Air Force, Air Force of Peru
Wikipedia Article (URL)
en.wikipedia.org/wiki/Caproni_Ca.310
Flat Wing Span (m)
16.2
Flat Wing Area (m²)
38.7
Number of Engines
2