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Keystone B-4

From Wikipedia, the free encyclopedia
American bomber aircraft
B-4
Keystone Y1B-4 (S/N 30-281)
General information
TypeLight bomber
ManufacturerKeystone Aircraft
StatusRetired
Primary userUnited States Army Air Corps
Number built5 Y1B-4
25 B-4A
History
Developed fromKeystone B-3

TheKeystone B-4 was abiplanebomber, built by theKeystone Aircraft company for theUnited States Army Air Corps.

Design and development

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Originally ordered by theUnited States Army Air Corps as theLB-13 light bomber. When theLB- designation was dropped in 1930, the first five planes were redesignatedY1B-4. (TheY1B- designation indicates that funds for the design did not come from the normal annual funds.)

The firstB-3A (S/N 30-281) was converted to Y1B-4 configuration with the addition of R-1860-7 radial engines and low pressure tires. Because of more powerful engines, the performance of the Y1B-4 was a slight improvement on the B-3, but the only difference between the two planes was their engines. On April 28, 1931, the army ordered 25 improved Y1B-4s as theKeystone B-4A. This production version was part of the last biplane bomber order made by the Army Air Corps (along with 39 B-6As, identical in all respects except their make of engine), and the B-4As, delivered between January and April 1932, were the last biplane bombers delivered to the Air Corps.

Operational history

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The B-4 was the last of the Keystone biplane bombers ordered by the U.S. Army in late 1931. These aircraft were used primarily as observation and reconnaissance aircraft as early as 1934 when theMartin B-10B went into operational service. Some remained in service into the early 1940s.

Variants

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LB-13
Seven aircraft ordered but delivered as the Y1B-4 andY1B-6 with different engine installations.
Y1B-4
Five pre-production aircraft, as theLB-10 but with two 575 hp (429 kW)Pratt & Whitney R-1860-7 engines.
B-4A
Production version of the Y1B-4, 25 built.

Operators

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United States

Specifications (B-4A)

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Keystone B-4A in flight in the Philippines

General characteristics

  • 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 sq ft (106.4 m2)
  • Empty weight: 7,951 lb (3,607 kg)
  • Gross weight: 12,952 lb (5,875 kg)
  • Powerplant: 2 ×Pratt & Whitney R-1860-7radial engines, 575 hp (429 kW) each

Performance

  • Maximum speed: 130 mph (210 km/h, 110 kn)
  • Cruise speed: 103 mph (167 km/h, 90 kn)
  • Range: 850 mi (1,400 km, 760 nmi)
  • Service ceiling: 14,000 ft (4,300 m)
  • Rate of climb: 580 ft/min (30 m/s)
  • Wing loading: 11.31 lb/sq ft (55.22 kg/m2)
  • Power/mass: 0.0888 hp/lb (146 W/kg)

Armament

  • Guns: 3 × .30 in (7.62 mm)Browningmachine guns
  • Bombs: 2,500 lb (1,100 kg); 4,000 lb (1,800 kg) on short runs

See also

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Related development

Related lists

External links

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Wikimedia Commons has media related toKeystone B-4.
Manufacturer designations
Bombers
Trainers
Patrol aircraft
Observation aircraft
Scout aircraft
Names
USAAS/USAAC/USAAF/USAF bomber designations, Army/Air Force andTri-Service systems
Original sequences
(1924–1930)
Light bomber
Medium bomber
Heavy bomber
Main sequence
(1930–1962)
Long-range bomber
(1935–1936)
Tri-Service sequence
(1962–current)
Non-sequential
Redesignated A-series
Fighter-bomber, in F-series
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1 Assigned to multiple types
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