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About: dbkwik:resource/djk14xtvP-afOF20LDQu0A==

PropertyValue
rdf:type
rdfs:label
  • Douglas YOA-5
rdfs:comment
  • The Douglas YOA-5 was an Amphibious aircraft designed for the United States Army Air Corps. Although a prototype was built, it did not enter production.
owl:sameAs
dcterms:subject
dbkwik:military/property/wikiPageUsesTemplate
loaded weight main
  • 20000.0
Guns
  • 3
climb rate main
  • 770.0
number of props
  • 2
length alt
  • 21.3 m
span main
  • 2735.5800000000004
power/mass alt
  • 130
Status
  • Prototype
cruise speed main
  • 152.0
cruise speed alt
  • 132
height alt
  • 6.7 m
Introduced
  • 1935
primary user
Type
type of prop
  • air-cooled radial piston engines
loading main
  • 18
range alt
  • nm, km
length main
  • 2125.98
power alt
  • 600.0
area main
  • 1101.0
power main
  • 800.0
stall speed alt
  • 65
height main
  • 670.5600000000001
span alt
  • 27.4 m
range main
  • mi
Manufacturer
  • Douglas Aircraft Company
max speed main
  • 169.0
engine (prop)
power/mass main
  • 0.080000
climb rate alt
  • 3.9
ceiling main
  • 18900.0
empty weight main
  • 14038.0
stall speed main
  • 75.0
loaded weight alt
  • 9000.0
Developed From
area alt
  • 102.3
First Flight
  • 1935
max speed alt
  • 147
jet or prop?
  • prop
loading alt
  • 89
empty weight alt
  • 6368.0
plane or copter?
  • plane
ceiling alt
  • 5,760 m
Retired
  • 1943
Number Built
  • 1
abstract
  • The Douglas YOA-5 was an Amphibious aircraft designed for the United States Army Air Corps. Although a prototype was built, it did not enter production.