Supriya Ghosh (Editor)

Curtiss Eagle

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Top speed
  
172 km/h

Length
  
11 m

Wingspan
  
19 m

First flight
  
August 1919

Curtiss Eagle httpsuploadwikimediaorgwikipediacommonsthu

Manufacturer
  
Curtiss Aeroplane and Motor Company

The Curtiss Eagle (retroactively designated the Model 19 by Curtiss some years later) was an airliner produced in small numbers in the United States shortly after World War I. The aircraft was a conventional biplane with three-bay, unstaggered wings of equal span. The fuselage was a very advanced design for its day, incorporating careful streamlining of its monocoque structure, and offering the crew as well as the passengers a fully enclosed cabin. The Eagle is sometimes named as the first American tri-motor aircraft; however Curtiss' own Model H flying boat flew with three engines for a time in 1914 before being converted back to twin-engine configuration.

Contents

Development

Curtiss had developed the Eagle in preparation for an anticipated post-war boom in civil aviation. In fact, this boom was far smaller than Curtiss had been hoping for, and practically all of the demand for passenger aircraft was met by the conversion of war-surplus military aircraft that could be purchased extremely cheaply. As such, only around 20 machines were built. The original trimotor Eagle design was followed by a single example of the Eagle II, with twin engines, and by three Eagle IIIs with only one engine. These latter aircraft were purchased by the United States Army Air Service, which used them as staff transports and converted one example into an air ambulance.

Operational history

On 28 May 1921, in one of the first major crashes in aviation history, Army Air Service Curtiss Eagle Serial Number 64243, the air ambulance, of the 1st Provisional Air Brigade, crashed during a severe thunderstorm attempting to land at Morgantown, Maryland while returning to Bolling Field, District of Columbia, from Langley Field, Virginia. The pilot, 1st Lt. Stanley M. Ames, and six passengers were killed. Four of the six were Air Service officers and an enlisted man. Two United States congressmen had chosen not to make the flight because of airsickness on the flight from Washington to Langley. The Army's Inspector General conducted an investigation of the crash and theorized that the aircraft stalled when it encountered an updraft at low altitude while trying to clear trees near the unfamiliar field and fell vertically, nose first, into the ground.

Variants

Curtiss Eagle
Three-engined passenger airliner, accommodating two pilots and eight passengers, powered by three 150-hp (112-kW) Curtiss K-6 piston engines.
Eagle II
Twin-engined version, powered by two 400-hp (298-kW) Curtiss C-12 engines; one built.
Eagle III
Single-engined version, powered by a 400-hp (298-kW) Liberty L-12 engine; three built.

Operators

 United States
  • United States Army
  • Specifications (Eagle I)

    Data from Curtiss Aircraft 1907–1947

    General characteristics

  • Crew: Two pilots
  • Capacity: 6 passengers
  • Length: 36 ft 9 in (11.20 m)
  • Wingspan: 61 ft 4 in (18.69 m)
  • Height: 12 ft 4 in (3.75 m)
  • Wing area: 900 ft2 (83.6 m2)
  • Empty weight: 5,130 lb (2,327 kg)
  • Gross weight: 7,450 lb (3,379 kg)
  • Powerplant: 3 × Curtiss K-6, 150 hp (112 kW) each each
  • Performance

  • Maximum speed: 107 mph (172 km/h)
  • Range: 475 miles (764 km)
  • Rate of climb: 407 ft/min (2.1 m/s)
  • References

    Curtiss Eagle Wikipedia