Curtiss A-8

The A-8 was a low-wing monoplane ground-attack aircraft built by the United States company Curtiss, designed in response to a 1929 United States Army Air Corps requirement for an attack aircraft to replace the A-3 Falcon. The Model 59 "Shrike" was designated XA-8 (the "Shrike" nickname was not officially adopted).


Curtiss A-8
Class Aircraft
Type Attack
Manufacturer Curtiss Aeroplane and Motor Company
Origin United States of America
Country Name Origin Year
United States of America 1931
ManufacturerName Production From Production To Quantity
Curtiss Aeroplane and Motor Company 13 View

The XA-8 won a competition against the General Aviation/Fokker XA-7, after which 13 service test aircraft were ordered (five as YA-8s and eight as Y1A-8s). After the completion of testing, 11 of these aircraft were redesignated A-8.

The A-8 was the first Curtiss machine of all-metal low-wing monoplane configuration with advanced features such as automatic leading edge slats and trailing-edge flaps.

Four forward-firing .30 in (7.62 mm) machine guns were mounted in the wheel fairings, and an additional weapon of the same calibre was fitted in the observer's cockpit for rear defense. The standard bomb load was four 100 lb (45 kg) bombs.

One YA-8 was fitted with a radial engine and designated YA-10, while another was used for testing of the Curtiss V-1570 Conqueror engine as the Y1A-8A. This aircraft was redesignated A-8 upon the completion of testing.

46 aircraft were ordered as A-8Bs, however the order was changed to the Model 60 A-12s before production began.

The A-8 created a sensation in US aviation circles when it went into service with the 3rd Attack Group at Fort Crockett, Texas in April 1932. All other standard aircraft were of biplane configuration, and the first monoplane fighter (the Boeing P-26A) did not become operational until eight months later.

Role Attack
Manufacturer Curtiss
Designer Don Berlin
First flight June 1931
Introduction April 1932
Primary user U.S. Army Air Corps
Produced 13
Variants YA-10 Shrike
A-12 Shrike


General characteristics

  • Crew: Two
  • Length: 32 ft 10 in (10.00 m)
  • Wingspan: 44 ft 0 in (13.41 m)
  • Height: 9 ft 0 in (2.74 m)
  • Wing area: 256 sq ft (23.78 m²)
  • Empty weight: 3,910 lb (1,777 kg)
  • Loaded weight: 5,888 lb (2,676 kg)
  • Powerplant: 1 × Curtiss V-1570-31 Conqueror Vee, 600 hp (447 kW)

Performance

  • Maximum speed: 183 mph (159 knots, 295 km/h)
  • Cruise speed: 153 mph (133 knots, 246 km/h)
  • Range: 480 mi (417 nmi, 773 km)
  • Service ceiling: 18,100 ft (5,500 m)
  • Rate of climb: 1,325 ft/min (6.7 m/s)Armament
  • Guns:
    4 × forward-firing 0.3 in (7.62 mm) M1919 Browning machine guns were mounted in the wheel fairings
    1 × 0.3 in (7.62 mm) machine gun mounted in the observer's cockpit for rear defense
  • Bombs: Up to 4 × 100 lb (45 kg) bombs carried under the wings or up to 10 × 30 lb (13.6 kg) fragmentation bombs in fuselage chutes either side of the main fuel tank

End notes