Douglas XA-2

The Douglas XA-2 was an American prototype attack aircraft converted from a Douglas O-2 observation aircraft in the spring of 1926 by Douglas Aircraft. Only one prototype aircraft was built and the type was not ordered into production.


Douglas XA-2
Class Aircraft
Type Attack
Manufacturer Douglas Aircraft Company
Origin United States of America
Country Name Origin Year
United States of America 1926
Country Name Operational Year Retirement Year
United States of America View
ManufacturerName Production From Production To Quantity
Douglas Aircraft Company 1 View

One Douglas O-2, serial number 25-380, was modified for the new role as an attack aircraft, while the basic structure of the aircraft remained, there were several modifications made. The water-cooled Liberty engine (V-1650) of the O-2 was replaced by an inverted air-cooled Allison VG-1410 engine. The reason for this was that a water cooling system was seen as too vulnerable to enemy attack. The lower engine cowlings were omitted to allow for more cooling air flow over the engine. Second, the A-2 was more heavily armed than the O-2. The A-2 had six forward-firing .30-caliber Browning machine guns - two in the nose forward of the cockpit, and two each in the mid-upper and lower wings. Two .30-caliber Lewis guns were put on a flexible mount for use by the observer-gunner in rear defense of the aircraft. The aircraft also had the capacity for a small bomb load of 100 lb (45 kg).

The Douglas XA-2 was evaluated against the Curtiss XA-3 (a conversion of the Curtiss O-1B observation plane). The Douglas aircraft won the initial competition, but the Army realized that the Liberty engine was both underpowered and in dwindling supply. It ordered a second competition with both models upgraded with Packard 1A-1500 engines. The Curtiss aircraft won this time and became the U.S. Army Air Corps' frontline attack aircraft (Curtiss A-3 Attack Falcon) from 1928 to 1935.

Role Attack
National origin United States
Manufacturer Douglas
Status Prototype
Primary user United States Army Air Corps
Number built 1
Developed from Douglas O-2


General characteristics

  • Crew: Two (pilot & observer / gunner)
  • Length: 29 ft 7 in (9.02 m)
  • Wingspan: 39 ft 8 in (12.09 m)
  • Height: 11 ft (3.4 m)
  • Max takeoff weight: 4,985 lb (2,261 kg)
  • Powerplant: 1 × Allison VG-1410 inverted air-cooled V-12 piston engine, 433 hp (323 kW)

Performance

  • Maximum speed: 130 mph (209 km/h; 113 kn)
  • Cruise speed: 100 mph (87 kn; 161 km/h)
  • Range: 400 mi (348 nmi; 644 km)
  • Service ceiling: 15,000 ft (4,572 m)

Armament

  • Guns:
    6 × forward firing .30-cal. (7.62 mm) Browning machine guns, two in the fuselage + one in each wing
    2 × flexible .30-cal. Lewis machine guns
  • Bombs: Provision for 100 lb (45 kg) of bombs mounted on lower wing racks

End notes