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[[Douglas O-43]]
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->{{Infobox Aircraft
|name = 0-43
|type = Observation
|manufacturer = [[Douglas Aircraft Company]]
|image =Image:Douglas O-43.jpg
|caption = Douglas O-43
|designer =
|first flight =
|introduced = 1930
|retired =
|status =
|primary user = [[United States Army Air Corps]]
|more users =
|produced =
|number built =
|unit cost =
|variants with their own articles =
}}
The [[Douglas Aircraft Company|Douglas]] '''O-43''' was a monoplane observation [[aircraft]] used by the [[United States Army Air Corps]].

Five '''Y1[[O-31]]A''' service-test aircraft were ordered in 1931, and delivered to the USAAC in early 1933 designated '''Y1O-43'''. They differed from the final configuration of the O-31A, with a wire-braced parasol wing, and a new fin and rudder. An order for 23 '''O-43A''' aircraft was completed during 1934, with a deepened fuselage, which eliminated the need for the ventral bulge under the observer's position. Powered by a single 675hp Curtiss V-1570-59, it also had taller vertical surfaces with an inset rudder similar to the O-31A. The canopy was enlarged, and fully enclosed both cockpits. The O-43 and O-43A served with the USSAC observation squadrons for several years before being assigned to reserve National Guard units, such as the [[111th Observation Squadron]] [[Brownwood Regional Airport|Brownwood Airfield Texas]], 15th Observation Squadron [[Fort Sill]] Oklahoma, and 3rd Observation Squadron [[Langley Field]] Virginia.

The 24th airframe of the O-43A contract was completed as the '''XO-46''' prototype.(See [[Douglas O-46]])

==Specifications (O-43)==
{{aircraft specifications
|plane or copter?=plane
|jet or prop?=prop
|ref=
|crew=
|capacity=
|payload main=
|payload alt=
|length main= 33 ft 11 in
|length alt= 10.34 m
|span main= 45 ft 8 in
|span alt= 13.92 m
|height main=
|height alt=
|area main=
|area alt=
|airfoil=
|empty weight main=
|empty weight alt=
|loaded weight main= 1165 lbs
|loaded weight alt= 528 kg
|useful load main=
|useful load alt=
|max takeoff weight main=
|max takeoff weight alt=
|more general=
|engine (prop)= [[Curtiss V-1570-59]]
|type of prop=
|number of props=1
|power main= 675 hp
|power alt= 540 kW
|power original=
|max speed main=
|max speed alt=
|cruise speed main=
|cruise speed alt=
|stall speed main=
|stall speed alt=
|never exceed speed main=
|never exceed speed alt=
|range main=
|range alt=
|ceiling main= 22,400 ft
|ceiling alt= 6827.52 m
|climb rate main=
|climb rate alt=
|loading main=
|loading alt=
|thrust/weight=
|power/mass main=
|power/mass alt=
|more performance=
|armament=
* 1 .30 cal (7.62 mm) [[Browning machine gun]]
|avionics=
}}
{{aero-specs}}

{{Douglas aircraft}}
{{aviation lists}}

[[Category:U.S. military utility aircraft 1930-1939|O-43, Douglas]]

[[de:Douglas O-43]]

==References==
*[http://www.usaaf.net/has/jops/O43.htm The United States Army Air Forces in World War II]
*[http://www.boeing.com/history/ Boeing History]
*[http://www.aerofiles.com/ Aerofiles]
*The complete Encyclopedia of World Aircraft [http://images.barnesandnoble.com/images/5490000/5496066.gif cover] Editors: Paul Eden & Soph Moeng, Amber Books Ltd. Bradley's Close, 74-77 White Lion Street, London, NI 9PF, 2002, 1152 pp.

Latest revision as of 04:38, 23 April 2007

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