FANDOM

251,246 Pages

Model 8A-5/A-33
Douglas A-33.jpg
Northrop A-17/Douglas A-33
Role Ground-attack fighter
Manufacturer Douglas Aircraft Company
Introduction 1941
Primary user US Army Air Corps
Number built 36
Variants Northrop A-17

The Douglas A-33 (Model 8A-5) was an updated version of the Northrop A-17 for the export market, with a more powerful engine and increased bomb load.

Design and developmentEdit

In 1932, the Northrop Corporation had been formed as a partly owned subsidiary of Douglas and by 1937, the Northrop Model 8 became known as the Douglas 8A produced in the El Segundo Division of Douglas aircraft. The 8A-5 was powered by a 1,200 hp Wright R-1820-87 engine and was the most powerful and best armed of the series, fitted with four wing mounted 0.30 in machine guns, two 0.50 in machine guns in pods below the wing and two rear-firing flexibly mounted 0.30 in guns, and could carry up to 1,800 lb of bombs.

Operational historyEdit

Early in 1940, The Norwegian Government ordered 36 8A-5s which not had been delivered before Norway was invaded by the Germans. Completed between October 1940 and January 1941, the aircraft were delivered to a training centre in Canada that had been set up for the Norwegian Government-in-Exile, at Island Airport, Toronto, Ontario. After the loss of two aircraft and a reassessment of the training needs now met by the use of other aircraft, the remaining total of 34 Model 8A-5Ps were sold to Peru, however 31 were repossessed by the Army Air Corps at the start of World War II. These aircraft, designated A-33, were used for training, target tug, and utility duties.[1]

VariantsEdit

Model 8A-5 
A-33 

OperatorsEdit

Flag of Norway.svg Norway
Flag of Peru.svg Peru
US flag 48 stars.svg United States

Specifications (A-33)Edit

Data from McDonnell Douglas Aircraft since 1920[2]

General characteristics
  • Crew: two
  • Length: 32 ft 6 in (9.91 m)
  • Wingspan: 47 ft 9 in (14.55 m)
  • Height: 9 ft 4 in (2.84 m)
  • Wing area: 363 sq ft (33.7 m²)
  • Empty weight: 5,510 lb (2,499 kg)
  • Loaded weight: 8,600 lb (3,901 kg)
  • Max. takeoff weight: 9,200 lb (4,173 kg)
  • Powerplant: 1 × Wright GR-1820-G205A Cyclone radial engine, 1,200 hp (895 kW)

Performance

  • Maximum speed: 248 mph (216 knots, 399 km/h) at 15,700 ft (4,785 m)
  • Service ceiling: 29,000 ft (8,840 m)
  • Climb to 10,000 ft (3,050 m): 5.8 min</ul></ul>Armament
  • Guns:
    • 4 × forward .30 machine guns
    • 2 × .30 machine guns in rear cockpit
  • Bombs: 1,800 lb (820 kg)
 </ul>

See alsoEdit

ReferencesEdit

Notes
  1. Pelletier Air Enthusiast September/October 1998, pp. 3–4.
  2. Francillon 1979, p. 222.
Bibliography
  • Francillon, René J. McDonnell Douglas Aircraft since 1920. London: Putnam, 1979. ISBN 0-370-00050-1.
  • Pelletier, Alain J. "Northrop's Connection: The unsung A-17 attack aircraft and its legacy, Part 1". Air Enthusiast No 75, May–June 1998, pp. 62–67. Stamford, Lincolnshire: Key Publishing. ISSN 0143-5490.
  • Pelletier, Alain J. "Northrop's Connection: The unsung A-17 attack aircraft and its legacy, Part 2". Air Enthusiast No 77, September–October 1998, pp. 2–15. Stamford, Lincolnshire: Key Publishing. ISSN 0143-5490.
  • Wagner, Ray. American Combat Planes of the 20th Century, Third Enlarged Edition. New York: Doubleday, 1982. ISBN 978-0-930083-17-5.
</dl>

External linksEdit

This page uses Creative Commons Licensed content from Wikipedia (view authors).
Community content is available under CC-BY-SA unless otherwise noted.