|Keystone B-3A (S/N 30-281), the first B-3A built.|
|Primary user||United States Army Air Corps|
|Number built||63 B-3A/B-5|
Design and development
It was originally ordered as the LB-10A (a single-tail modification of the Keystone LB-6), but the Army dropped the LB- 'light bomber' designation in 1930.
Although the performance of the B-3A was hardly better than that of the bombers flown at the end of World War I, it had come a long way. In terms of its safety, it was far superior to its oldest predecessors.
The B-3A was the last biplane operated by the US Army; it remained in service until 1940. A few years after it was first produced, the introduction of all-metal monoplanes rendered it almost completely obsolete.
- The last of the 17 LB-6s ordered (S/N 29-27) was converted with a re-designed single fin and rudder and two 525 hp R-1750E engines. Delivered to Wright Field on 7 July 1929, it was wrecked on 12 November 1929.
- This version used Pratt and Whitney R-1690-3 Hornet engines and was slightly smaller, both wingspan and fuselage. a total of 63 were ordered (S/N 30-281/343). It was re-designated as the B-3A before any deliveries were made, and the final 27 were built as B-5A.
- 36 delivered as B-3A (S/N 30-281/316). The first aircraft was delivered in October 1930.
- Ordered as B-3A, re-engined with Wright R-1750-3 Cyclone engines, 27 built (S/N 30-317/343).
- United States Army Air Corps
- 2d Bombardment Group, Langley Field, Virginia
- 4th Composite Group, Nichols Field, Luzon, Philippines
- 5th Composite Group, Luke Field, Territory of Hawaii
- 6th Composite Group, France Field, Panama Canal Zone
- 25th Bomb Squadron - operated B-3A 1932-1936
- 7th Bombardment Group, March Field, California
- 19th Bombardment Group, Rockwell Field, California
- Air Corps Advanced Flying School, Kelly Field, Texas
- 42d Bomb Squadron - operated B-3A and B-5A 1935-1936
- Philippine Army Air Corps
- 10th Bombardment Squadron
- Crew: 5
- Length: 48 ft 10 in (14.9 m)
- Wingspan: 74 ft 8 in (22.8 m)
- Height: 15 ft 9 in (4.8 m)
- Wing area: 1,145 ft² (106.4 m²)
- Empty weight: 7,705 lb (3,495 kg)
- Loaded weight: 12,952 lb (5,875 kg)
- Max. takeoff weight: lb (kg)
- Powerplant: 2 × Pratt & Whitney R-1690-3 radial engines, 525 hp (392 kW) each
- Maximum speed: 114 mph (98 kn, 183 km/h)
- Cruise speed: 98 mph (85 kn, 158 km/h)
- Range: 860 mi (760 nmi, 1,400 km)
- Service ceiling: 12,700 ft (3,870 m)
- Rate of climb: 530 ft/min (2.7 m/s)
- Wing loading: 11.31 lb/ft² (55.42 kg/m²)
- Power/mass: 0.0811 hp/lb (133 W/kg)
- Guns: 3 × .30 in (7.62 mm) machine guns
- Bombs: 2,500 lb (1,100 kg); 4,000 lb (1,800 kg) on short runs
- Related development
- Related lists
- "Fact Sheet - Keystone B-3A." National Museum of the United States Air Force. Retrieved: 18 September 2011.
- Andrade, John. U.S. Military Aircraft Designations and Serials since 1909. Leicester, UK: Midland Counties Publications, 1979, pp. 43, 135. ISBN 0-904597-22-9.
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). London: Orbis Publishing, 1985, p. 2255.
- Maurer, Maurer. Combat Squadrons of the Air Force, World War II. Maxwell AFB, Alabama: Air Force Historical Studies Office, 1982. ISBN 0-89201-097-5.
|Wikimedia Commons has media related to Keystone B-3.|
- Encyclopedia of American Aircraft
- Photograph of B-3 on the ground
- USAF Museum article on LB-10
- USAF Museum article on B-3