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Consolidated NY

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The Consolidated Model 2 was a PT-1 biplane trainer diverted to the United States Navy for a trainer competition in 1925. It beat out 14 other designs, and was ordered into production as the NY-1[1].

Development

The NY-1 was essentially a PT-1 with provisions for the wheeled landing gear to be replaced by a single large float under the fuselage and two stabilising floats under the tips of the lower wing. A larger vertical tail was added to counter the effect of the floats[1]. The NY-2 had a longer span wing fitted to overcome the high wing-loading issue of the seaplane version. Tested with complete success during October 1926, the Navy ordered 181 with the uprated R-790-8 Wright Whirlwind J-5 engine of 220 hp (164 kW)[1]. The NY-3 aircraft were similar to the NY-2 but had 240 hp (179 kW) Wright R-760-94 engines[2].

Operational history

The NY-1's first flight was November 1925, with deliveries starting May 1926[1]. The NY-2's first flight was October 1926. The Navy had 108 in active use in 1929, with 35 more assigned to reserve squadrons[2]. The NY-3 was delivered in 1929. The NY series was being phased out in the mid 1930s, with 15 in service in 1937, and one in service in 1939[2].

Variants

NY-1
wingspan 34 ft 6 in, 200 hp (149 kW) Wright J-4 Whirlwind engine, 76 built
NY-1A
a number of NY-1 aircraft modified for gunnery training with one 0.3 in (7.62 mm) trainable machine-gun in the rear cockpit
NY-1B
a number of retrofitted NY-1 aircraft with the long-span wings of the NY-2 and the 220 hp Wright J-5 Whirlwind engine
NY-2
wingspan increased to 40 ft (12.19 m), 220 hp (164 kW) Wright J-5 Whirlwind engine, 181 built
NY-2A
NY-2 aircraft armed for gunnery training, 25 built
NY-3
similar to the NY-2 with a 240 hp (179 kW) Wright R-760-94 Whirlwind engine, 20 built
XN3Y-1
a single NY-2 tested with a Wright R-790-A Whirlwind engine

Operators

Template:Country data United States

Specifications (NY-2 floatplane)

Data from "The Complete Encyclopedia of World Aircraft" Editors: Paul Eden & Soph Moeng, 2002, ISBN 0-7607-3432-1), page 478.

General characteristics

  • Crew: 2
  • Length: 31 ft 4.25 in (9.56 m)
  • Wingspan: 40 ft (12.19 m)
  • Height: 11 ft 10 in (3.61 m)
  • Wing area: 370 ft² (34.37 m²)
  • Empty weight: 2,145 lb (973 kg)
  • Max takeoff weight: 2,843 lb (1,290 kg)
  • Powerplant:Wright R-760-8 Whirlwind radial, 220 hp (164 kW)

Performance

Armament

none


References

  1. 1.0 1.1 1.2 1.3 "The Complete Encyclopedia of World Aircraft" cover Editors: Paul Eden & Soph Moeng, (Amber Books Ltd. Bradley's Close, 74-77 White Lion Street, London, NI 9PF, 2002, ISBN 0-7607-3432-1), 1152 pp.
  2. 2.0 2.1 2.2 "United States Navy Aircraft Since 1911" by Gordon Swanborough & Peter M. Bowers (Naval Institute Press Annapolis, MD, ISBN 0870219685) 1976, 546 pp.

External links

See also

Related lists

Template:USN trainer aircraft

This article is licensed under the GNU Free Documentation License.
It uses material from the Wikipedia article "Consolidated NY".