Douglas YOA-5

Length
21.0312 m
Flat Wing Span
27.1272 m
Height
6.46 m
Max Speed
271.9791 km/h
Number of Engines
2
First Flight
1935-01-01
Entry Into service
1935-01-01
Number Built
1

Pictures

No pictures yet for this family.

Aircraft Weight Variants

Aircraft
Douglas YOA-5

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
Avro Manchester 21.336 27.432 Compare
CASA C-207 Azor Bristol Hercules 20.85 27.8 40 Compare
Blohm & Voss BV 144 BMW 801 21.8 27 Compare
Saab 90 Scandia Pratt & Whitney R-2180-E Twin Wasp E 21.3 28 24 Compare
Vickers VC.1 Viking 19.812 27.1272 Compare
CASA/IPTN CN-235 General Electric T700 21.4 25.81 51 Compare
All data (20 fields)
Name
Douglas YOA-5
Manufacturer
Douglas Aircraft Corporation
Description
The Douglas YOA-5 was an amphibious aircraft designed for the United States Army Air Corps, based on the Navy's Douglas XP3D.
First Flight
1935-01-01
Entry Into service
1935-01-01
Service End
1943-01-01
Designer
Douglas Aircraft Corporation
Type
Seaplane bomber
Length (m)
21.0312
Height (m)
6.46
Cockpit Crew
4
Max Speed (km/h)
271.9791
Armament
3× .30 in (7.62 mm) machine guns in open bow and fuselage positions
Number Built
1
Powerplant Description
2 × Wright R-1820-25 Cyclone 9-cylinder air-cooled radial piston engines, 559 kW (750 hp) each
Primary Users
United States Army Air Corps
Status
Prototype
Wikipedia Article (URL)
en.wikipedia.org/wiki/Douglas_YOA-5
Flat Wing Span (m)
27.1272
Number of Engines
2