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Bloch MB.162 ✕ De Havilland Canada DHC-4 Caribou ✕
Manufacturer Société des Avions Marcel Bloch De Havilland Canada
Description The Bloch MB.162 was a French four-engine, long-range bomber developed by Société des Avions Marcel Bloch in the late 1930s. The de Havilland Canada DHC-4 Caribou (designated by the United States military as the CV-2 and later C-7 Caribou) is a Canadian specialized cargo aircraft with short takeoff and landing (STOL) capability developed by de Havilland Canada.
ICAO Code DHC4
First Flight 1940-06-01 1958-07-30
Entry Into service 1943-01-01 1961-01-01
Production End 1968-01-01
Service End 2009-01-01
Designer Société des Avions Marcel Bloch De Havilland Canada
Type Heavy Bomber STOL transport aircraft
Length (m) 21.91 21.9456
Height (m) 3.76 9.4488
Cockpit Crew 5 2
Max Seating 30
Max Speed (km/h) 551 346.3237
Cruise Speed (km/h) 292.6157
Min Speed (km/h) 109.2679
Max Ceiling (m) 9000 7559.04
Rate of Climb (m/s) 6.8834
Armament 2 × 7.5 mm (.295 in) MAC 1934 machine guns in nose and ventral positions; 2 × 20 mm Hispano-Suiza HS.404 cannon in ventral and dorsal positions; 3600 kg of bombs
Capacity Description 30 pax (civil) / 32 troops / 26 fully-equipped paratroops / 22 stretchers, 4 sitting patients and 4 attendants
National Origin France Canada
Number Built 1 307
Powerplant Description 2 × Gnome-Rhône 14N-48 14-cylinder two-row air-cooled radial engine, 820 kW (1100 hp) each 2 × Pratt & Whitney R-2000-7M2 Twin Wasp 14-cylinder air-cooled radial piston engines, 1081 kW (1450 hp) each
Primary Users Luftwaffe Royal Canadian Air Force, United States Army, United States Air Force, Royal Australian Air Force
Status In limited service
Wikipedia Article (URL) en.wikipedia.org/wiki/Bloch_MB.162 en.wikipedia.org/wiki/De_Havilland_Canada_DHC-4_Caribou
Flat Wing Span (m) 28.1 28.956
Flat Wing Area (m²) 109 84.7276
Flat Wing Aspect Ratio 10
Wake Category M
Number of Engines 2 2