PropertyValue
rdf:type
rdfs:label
  • De Havilland Canada DHC-4 Caribou
rdfs:comment
  • 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-designed and produced specialized cargo aircraft with short takeoff and landing (STOL) capability. The Caribou was first flown in 1958 and although mainly retired from military operations, is still in use in small numbers as a rugged "bush" aircraft.
owl:sameAs
dcterms:subject
dbkwik:military/property/wikiPageUsesTemplate
loaded weight main
  • 28500.0
climb rate main
  • 1355.0
number of props
  • 2
length alt
  • 22.12 m
span main
  • 95.58
cruise speed main
  • 181.0
cruise speed alt
  • 291.0
height alt
  • 9.65 m
Introduced
  • 1961
primary user
Type
  • STOL Transport
range alt
  • 240
length main
  • 72.58
power alt
  • 1081.0
area main
  • 912.0
power main
  • 1450.0
height main
  • 31.66
span alt
  • 29.13 m
payload alt
  • 3628.0
range main
  • 1280.0
Manufacturer
max speed main
  • 216.0
engine (prop)
  • Pratt and Whitney R-2000-7M2 Twin Wasp 14-cylinder
Capacity
  • ** 32 troops or ** 24 fully equipped paratroops or ** 14 casualty stretchers
climb rate alt
  • 413
ceiling main
  • 24800.0
empty weight main
  • 16920.0
loaded weight alt
  • 12927.0
area alt
  • 84.7
First Flight
  • 1958-07-30
more users
max speed alt
  • 348.0
jet or prop?
  • prop
empty weight alt
  • 7675.0
plane or copter?
  • plane
ceiling alt
  • 7,559 m
variants with their own articles
payload main
  • 8000.0
Crew
  • Three
Number Built
  • 307
ref
  • MacDonald Aircraft Handbook.
abstract
  • 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-designed and produced specialized cargo aircraft with short takeoff and landing (STOL) capability. The Caribou was first flown in 1958 and although mainly retired from military operations, is still in use in small numbers as a rugged "bush" aircraft.
is Developed From of
is aircraft transport of