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Consolidated NY

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.[2]

NY
A Consolidated NY-2 in 1928
Role Trainer
Manufacturer Consolidated
First flight November 1925
Introduction May 1926
Retired 1939
Primary user United States Navy
Number built 302[1]
Developed from Dayton-Wright TW-3
Variants Consolidated PT-3

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.[2] 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 (160 kW).[2] The NY-3 aircraft were similar to the NY-2 but had 240 hp (180 kW) Wright R-760-94 engines.[1]

Operational history

The NY-1's first flight was November 1925, with deliveries starting May 1926.[2] 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.[1] 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.[1]

Variants

 
An NY seaplane near Naval Air Station Pensacola, circa 1924.
NY-1
wingspan 34 ft 6 in (10.52 m), 200 hp (150 kW) Wright J-4 Whirlwind, 76 built.
NY-1A
a number of NY-1 aircraft modified for gunnery training with one .30 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 (160 kW) Wright J-5 Whirlwind.
NY-2
wingspan increased to 40 ft (12.19 m), 220 hp J-5, 181 built.
NY-2A
NY-2 aircraft armed for gunnery training, 25 built.
NY-3
similar to the NY-2 with a 240 hp (180 kW) Wright R-760-94 Whirlwind, 20 built.
XN3Y-1
a single NY-2 tested with a Wright R-790-A Whirlwind.

Operators

  Brazil
  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 0 in (12.19 m)
  • Height: 11 ft 10 in (3.61 m)
  • Wing area: 370 sq ft (34.37 m2)
  • Empty weight: 2,145 lb (973 kg)
  • Max takeoff weight: 2,843 lb (1,290 kg)
  • Powerplant: 1 × Wright R-760-8 Whirlwind air-cooled radial, 220 hp (164 kW)

Performance

  • Maximum speed: 78 kn (90 mph, 145 km/h) at sea level
  • Cruise speed: 65 kn (75 mph, 121 km/h)
  • Range: 182.5 nmi (210 mi, 338 km)
  • Service ceiling: 11,000 ft (3,355 m)
  • Rate of climb: 865 ft/min (4.4 m/s)

Armament
None

See also

Related lists

References

  1. ^ a b c d "United States Navy Aircraft Since 1911" by Gordon Swanborough & Peter M. Bowers (Naval Institute Press Annapolis, MD, ISBN 0-87021-968-5) 1976, 546 pp.
  2. ^ a b c d "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.

External links

  • Consolidated NY-1 (NASA) accessed July 16, 2007
  • Consolidated NY-2 (NASA) accessed July 16, 2007
  • accessed July 16, 2007
  • Consolidated NY-1, -2, -3 (NAS GROSSE ILE) accessed July 16, 2007

consolidated, consolidated, model, biplane, trainer, diverted, united, states, navy, trainer, competition, 1925, beat, other, designs, ordered, into, production, 1928role, trainermanufacturer, consolidatedfirst, flight, november, 1925introduction, 1926retired,. 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 2 NYA Consolidated NY 2 in 1928Role TrainerManufacturer ConsolidatedFirst flight November 1925Introduction May 1926Retired 1939Primary user United States NavyNumber built 302 1 Developed from Dayton Wright TW 3Variants Consolidated PT 3 Contents 1 Development 2 Operational history 3 Variants 4 Operators 5 Specifications NY 2 floatplane 6 See also 7 References 8 External linksDevelopment EditThe 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 2 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 160 kW 2 The NY 3 aircraft were similar to the NY 2 but had 240 hp 180 kW Wright R 760 94 engines 1 Operational history EditThe NY 1 s first flight was November 1925 with deliveries starting May 1926 2 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 1 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 1 Variants Edit An NY seaplane near Naval Air Station Pensacola circa 1924 NY 1 wingspan 34 ft 6 in 10 52 m 200 hp 150 kW Wright J 4 Whirlwind 76 built NY 1A a number of NY 1 aircraft modified for gunnery training with one 30 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 160 kW Wright J 5 Whirlwind NY 2 wingspan increased to 40 ft 12 19 m 220 hp J 5 181 built NY 2A NY 2 aircraft armed for gunnery training 25 built NY 3 similar to the NY 2 with a 240 hp 180 kW Wright R 760 94 Whirlwind 20 built XN3Y 1 a single NY 2 tested with a Wright R 790 A Whirlwind Operators Edit BrazilBrazilian Naval Aviation United StatesUnited States Navy United States Marine CorpsSpecifications NY 2 floatplane EditData from The Complete Encyclopedia of World Aircraft Editors Paul Eden amp Soph Moeng 2002 ISBN 0 7607 3432 1 page 478 General characteristicsCrew 2 Length 31 ft 4 25 in 9 56 m Wingspan 40 ft 0 in 12 19 m Height 11 ft 10 in 3 61 m Wing area 370 sq ft 34 37 m2 Empty weight 2 145 lb 973 kg Max takeoff weight 2 843 lb 1 290 kg Powerplant 1 Wright R 760 8 Whirlwind air cooled radial 220 hp 164 kW Performance Maximum speed 78 kn 90 mph 145 km h at sea level Cruise speed 65 kn 75 mph 121 km h Range 182 5 nmi 210 mi 338 km Service ceiling 11 000 ft 3 355 m Rate of climb 865 ft min 4 4 m s Armament NoneSee also EditRelated lists List of United States Navy aircraft designations pre 1962 References Edit a b c d United States Navy Aircraft Since 1911 by Gordon Swanborough amp Peter M Bowers Naval Institute Press Annapolis MD ISBN 0 87021 968 5 1976 546 pp a b c d The Complete Encyclopedia of World Aircraft cover Editors Paul Eden amp Soph Moeng Amber Books Ltd Bradley s Close 74 77 White Lion Street London NI 9PF 2002 ISBN 0 7607 3432 1 1152 pp External links Edit Wikimedia Commons has media related to Consolidated NY Consolidated NY 1 NASA accessed July 16 2007 Consolidated NY 2 NASA accessed July 16 2007 Consolidated NY Trainer US Centennial of Flight Commission accessed July 16 2007 Consolidated NY 1 2 3 NAS GROSSE ILE accessed July 16 2007 Retrieved from https en wikipedia org w index php title Consolidated NY amp oldid 1143604511, wikipedia, wiki, book, books, library,

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