Douglas T2D

Airplanes

Length

12.8016 m

Flat Wing Span

17.3736 m

Height

4.572 m

Flat Wing Area

82.3121 m²

Max Speed

201.168 km/h

Max Ceiling

4215.384 m

Number of Engines

First Flight

1927-01-27

Entry Into service

1927-01-01

Number Built

Maximum Take-Off Weight

4.7732 t (paragliders: kg)

Maximum Range

735.4702 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Douglas T2D	4.7732	735.4702

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Yakovlev Yak-200	Shvetsov ASh-21	12.95	17.45		Compare
Dornier Seastar	Pratt & Whitney Canada PT6	12.7	17.74		Compare
Bristol Type 143		13.1064	17.0688	8	Compare
Caproni Ca.310		12.2	16.2		Compare
Blackburn H.S.T.10	Napier Rapier	12.8	17.5	12	Compare
Messerschmitt Bf 162		12.75	17.16		Compare

All data (21 fields)

Name: Douglas T2D
Manufacturer: Douglas Aircraft Corporation
Description: The Douglas T2D was an American twin-engined torpedo bomber contracted by the military, and required to be usable on wheels or floats, and operating from aircraft carriers.
First Flight: 1927-01-27
Entry Into service: 1927-01-01
Service End: 1937-01-01
Designer: Douglas Aircraft Corporation
Type: Torpedo bomber
Length (m): 12.8016
Height (m): 4.572
Cockpit Crew: 4
Max Speed (km/h): 201.168
Max Ceiling (m): 4215.384
Armament: 2 × .30 in M1919 Browning machine guns; 1 ×1618 lb torpedo or equivalent bombload
Number Built: 31
Powerplant Description: 2 × Wright R-1750 Cyclone 9-cylinder air-cooled radial piston engines, 391 kW (525 hp) each
Primary Users: United States Navy
Wikipedia Article (URL): en.wikipedia.org/wiki/Douglas_T2D
Flat Wing Span (m): 17.3736
Flat Wing Area (m²): 82.3121
Number of Engines: 2