| Specifications |
|---|
| Manufacturer (Airframe): | The Dougals Aircraft Company, Inc., Santa Monica Calif. |
| Manufacturer (Engines): | Designed by the General Electric Co.; built by Chevrolet Div. of General Motors Corporation |
| Nomenclature | Light Bomber |
| Length/Span: | 51.4/71.2 ft. |
| Wing Area: | 563 sq. ft. |
| Engines: | Two st J35 engines capable of 3,820-lbs. of thrust |
| Takeoff Ground Run: | 7,080 ft. (Contractor's guarantee) |
| Rate of Climb at Sea Level: | 2,470 (Contractor's estimate) |
| Ceiling: | 41,800 (combat weight/mil power) |
| Average Cruise Speed: | 365 knots |
| Maximum Speed: | 437 knots (Contractor's estimate) |
| Combat Cruising Radius: | 470 nautical miles |
| Crew: | Three |
| Armament: | None |
| Maximum Bombload: | 8,000 lbs. |
| Maximum Bomb Size: | 4,000 lbs. |
