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Contents

   



(Top)
 


1 Development and design  





2 Operational history  





3 Variants  





4 Operators  





5 Specifications (O-40B)  





6 References  





7 External links  














Curtiss O-40 Raven






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From Wikipedia, the free encyclopedia
 


O-40 Raven
The original prototype YO-40
Role Observation aircraft
National origin United States of America
Manufacturer Curtiss-Wright
First flight 1932
Introduction 1933
Retired 1939
Primary user United States Army Air Corps
Number built 5

The Curtiss O-40 Raven was an American observation aircraft of the 1930s which was built and used in small numbers. A single example of the YO-40, a single-engined Sesquiplane with a retractable undercarriage was built, followed by four examples of a modified monoplane version, the O-40B, which remained in use until 1939.

Development and design

[edit]

In 1931, in response to a United States Army Air Corps requirement for a new observation aircraft, Curtiss designed the Model 62, a single-engined biplane with the lower wing much smaller than the upper, known as a sesquiplane (i.e. "one-and-a-half wings"), while the outer panels of the upper wings were swept back to avoid centre-of-gravity problems. It was of all-metal construction, with a monocoque fuselage and had a retractable tailwheel undercarriage with inwards retracting mainwheels, and was powered by a Wright Cyclone radial engine. The crew of two sat in tandem in open cockpits.[1][2][3]

A prototype, designated YO-40, flew in February 1932. Although it crashed in May that year, it was rebuilt with stronger wings and an enclosed cockpit as the YO-40A. A further four YO-40As were ordered, but they were redesigned as monoplanes by removing the lower wing, the resultant aircraft being designated Y1O-40B.[2][4]

Operational history

[edit]

The four Y1O-40Bs were delivered in June 1933, and after service tests, were redesignated O-40B,[5] being operated by the 1st Observation Squadron of the USAAC.[6] While the aircraft's performance and manoeuvrability were good, the Air Corps was disappointed with the cockpit arrangements and the low fuel capacity,[2] and no more orders followed. The last O-40B was withdrawn from use in 1939.[5]

Variants

[edit]
YO-40
Prototype powered by 653 hp (487 kW) Wright R-1820E Cyclone engine.[7]
YO-40A
YO-40 rebuilt with stronger wings and enclosed cockpit. Scrapped 1938.[2][5]
Y1O-40B
Monoplane derivative with lower wing removed. Powered by 670 hp (500 kW) R-1820-27. Four built.[5]
O-40B
Redesignation of Y1O-40B.[5]

Operators

[edit]
 United States

Specifications (O-40B)

[edit]

Data from Curtiss Aircraft 1907–1947[5]

General characteristics

Performance

Armament

References

[edit]
Notes
  1. ^ Bowers 1979, pp. 331–332.
  • ^ a b c d "Curtiss:K through Z". aerofiles. 24 January 2009. Retrieved 10 March 2010.
  • ^ Flight 4 January 1934, p.20.
  • ^ Bowers 1979, pp. 332–333.
  • ^ a b c d e f Bowers 1979, p.333.
  • ^ "Factsheets : 1 Reconnaissance Squadron (ACC) Archived 2011-09-13 at the Wayback Machine". Air Force Historical Research Agency, United States Air Force. Retrieved 10 March 2010.
  • ^ Bowers 1979, p.332.
  • Bibliography
    • Bowers, Peter M. Curtiss Aircraft 1907-1947. London:Putnam, 1979. ISBN 0-370-10029-8.
  • "A Modern American Observation Aircraft:The Curtiss "Raven" (Wright "Cyclone F") developed for the U.S. Army Air Corps". Flight, 4 January 1934, p. 20.
  • [edit]
    Retrieved from "https://en.wikipedia.org/w/index.php?title=Curtiss_O-40_Raven&oldid=993812503"

    Categories: 
    1930s United States military reconnaissance aircraft
    Curtiss aircraft
    Single-engined tractor aircraft
    Sesquiplanes
    Aircraft first flown in 1932
    Hidden categories: 
    Webarchive template wayback links
    Articles with short description
    Short description is different from Wikidata
    Commons category link is on Wikidata
     



    This page was last edited on 12 December 2020, at 16:58 (UTC).

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