Northrop Delta

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Delta
Northrop Delta 1.jpg
Role Transport aircraft
Manufacturer Northrop Corporation
Designer Jack Northrop
First flight May 1933
Introduction 1933
Primary user Royal Canadian Air Force
Number built 32
Developed from Northrop Gamma

The Northrop Delta was an American single-engined passenger transport aircraft of the 1930s. Closely related to Northrop's Gamma mail plane, 13 were produced by the Northrop Corporation, followed by 19 aircraft built under license by Canadian Vickers Limited.

Development and design

When Jack Northrop set up the Northrop Corporation as a joint venture with the Douglas Aircraft Company in 1932, he set out to design two closely related single-engined aircraft as the new company's first products, a mailplane/record breaking aircraft, which was designated the Gamma and a passenger transport, the Delta.[1] The Delta was a low-winged monoplane, with a fixed tailwheel undercarriage. It was of all-metal stressed skin construction, with streamlining spats covering the main landing gear. While the Delta's wings were common with those of the Gamma, it had a new, wider fuselage, which seated the pilot in an enclosed cockpit immediately behind the engine, and had accommodation for eight passengers in a cabin behind the pilot.[2][3]

The first Delta was flown in May 1933, and received an airworthiness certificate in August that year.[3]

Operational history

Although it was intended that the Delta would be sold in both airliner and executive transport (initially named "Victoria") versions,[4] a change to the regulations governing commercial air transport in the United States in October 1934, prohibiting the use of single-engined aircraft to carry passengers at night or over rough terrain which would prevent a forced landing, stopped the market for single-engined airliners in the United States, and only three aircraft, all ordered before the passing of this regulation, were built.[3] These consisted of the prototype, leased to Trans World Airlines for use to carry airmail, which crashed on 10 November 1933, one sold to Pan-Am for use by its Mexican subsidiary, destroyed by a fire in May 1934 and one sold to AB Aerotransport of Sweden, delivered in April 1934. AB Aerotransport purchased a second Delta, but this was a dedicated mailplane which more closely resembled the Gamma, with a slim fuselage carrying its cargo in a compartment ahead of the cockpit.

A single aircraft was built for the United States Coast Guard. Designated the Northrop RT-1, this was used as the personal transport of Henry Morgenthau, Jr., the Secretary of the Treasury and as a staff transport.[5] Seven more aircraft were built as executive transports for private owners. Of these, three were purchased by the Spanish Republicans for use in the Spanish Civil War. Two of these aircraft were captured by the Nationalists when the ship carrying them (along with four Vultee V-1s, a Fairchild 91 and a Lockheed Electra) was captured at sea. These two Deltas were used as Transports by Franco's forces, while the third Delta was used by the Republican airline Lineas Aéreas Postales Españolas (LAPE) until the end of the civil war when it was handed over to Franco's air force.[6]

In 1935, Canada selected the Delta for use as a photographic survey aircraft for use by the Royal Canadian Air Force (RCAF), to be built by Canadian Vickers under license.[2] One aircraft, the last Delta built by Northrop, was supplied as a part assembled pattern to Canadian Vickers, first flying on 16 August 1936 and being delivered to the RCAF on 1 September that year.[7] It was followed by a further 19 aircraft built wholly by Canadian Vickers, production continuing until October 1940.[8] The Northrop Delta was the first all metal stressed skin aircraft built in Canada.

The Deltas, which were capable of being operated from wheeled, ski or float undercarriages, proved capable survey aircraft, well suited to operations in the North of Canada, but in August 1939, when the outbreak of the Second World War loomed, Canada found itself short of coastal patrol aircraft, and the Deltas were diverted to this role, being fitted with floats and carrying out long anti-submarine missions. The Deltas were less successful as patrol floatplanes, as they were damaged by ocean swell and by salt water corrosion, and they were forced to revert to landplane use after two months. The Delta was withdrawn from operations in late 1941, then being used as instructional airframes in training schools.[8]

Variants

Delta 1A
Prototype. Powered by 710 hp (530 kW) Wright SR-1820-F3 Cyclone radial engine. One built.[3]
Delta 1B
Passenger airliner for Pan-Am. Powered by 660 hp (492 kW) Pratt & Whitney Hornet. One built.[9]
Delta 1C
Passenger airliner for AN Aerotransport. Powered by 700 hp (522 kW) Hornet.[9]
Delta 1D
Executive aircraft, powered by Cyclone or Hornet engines. Eight built, including one Northrop RT-1, powered by 735 hp (548 kW) Cyclone for United States Coast Guard.
Delta 1E
Airmail carrier for AB Aerotransport. One built. Powered by 660 hp (492 kW) Hornet.[10]
Delta I
Survey aircraft for RCAF. Powered by 775 hp (578 kW) SR-1820-F52 Cyclone. Three built, including pattern aircraft and two license built.
Delta II
Revised version with provision for armament, including bombs, a dorsal turret mounting a .30 in Browning machine gun (later removed) and two wing mounted machine guns. Nine built.[11]
Delta III
Fitted with enlarged tail surfaces to counter tail buffeting from turret. Eight built.[11]

Military Operators

Canadian Northrop Delta in 1939
 Australia
 Canada
23x15px Spain
 United States

Civil Operators

 Australia
 Mexico
 Sweden
 United States

Specifications (Delta 1D-5)

Data from McDonnell Douglas Aircraft since 1920 [12]

General characteristics

  • Crew: 1
  • Capacity: 8 Passengers (passenger variants)
  • Length: 33 ft 1 in (10.08 m)
  • Wingspan: 47 ft 9 in (14.55 m)
  • Height: 10 ft 1 in (3.07 m)
  • Wing area: 363 ft² (33.7 m²)
  • Empty weight: 4,504 lb (2,059 kg)
  • Loaded weight: 7,350 lb (3,334 kg)
  • Powerplant: 1 × Wright SR-1820-F2 Nine-cylinder air-cooled radial engine, 735 hp (548 kW)

Performance

See also

Related development
Aircraft of comparable role, configuration and era
Related lists

References

Notes
  1. Francillon 1979, pp.23-24, 143.
  2. 2.0 2.1 Green 1967, p.57.
  3. 3.0 3.1 3.2 3.3 Francillon 1979, p.157.
  4. Flight 8 February 1934, p.123.
  5. Francillon 1979, p.163.
  6. Francillon 1979, pp.159-161.
  7. Green 1967, p.58.
  8. 8.0 8.1 Green 1967, p.60.
  9. 9.0 9.1 Francillon 1979, p.158.
  10. Francillon 1979, p.159.
  11. 11.0 11.1 Green 1967, p.593
  12. Francillon 1979, p.165.
Bibliography

External links