Keystone B-6

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In 1931, the United States Army Air Corps received five working models (Y1B-6s) of the B-6 bomber. (The Y1B- designation, as opposed to a YB- designation, indicates funding outside normal fiscal year procurement). Two of these were diverted from an order of LB-13s; three were modified B-3As. The performance of the Y1B-6s was very similar to that of the Keystone B-4s, due to an engine of equivalent power.

The production model, called the B-6A, was the last biplane bomber purchased by the Army. The performance of the B-6A varied little from the Martin NBS-1 ordered in 1921. Its successor, the monoplane bomber, had a hard time getting accepted. The Douglas Y1B-7 and Fokker XB-8 were originally designed as high-speed reconnaissance planes.

Specifications (B-6A)

{{airtemp

|plane or copter?=plane |jet or prop?=prop


|crew=5 |length main=48 ft 10 in |length alt=14.9 m |span main=74 ft 8 in |span alt=22.8 m |height main=15 ft 9 in |height alt=4.8 m |area main=1,145 ft² |area alt=106.4 m² |empty weight main=8,057 lb |empty weight alt=3,665 kg |loaded weight main=13,350 lb |loaded weight alt=6,056 kg |max takeoff weight main= lb |max takeoff weight alt= kg

|number of props=2 |engine (prop)=Wright R-1820-1 |type of prop=radial engines |power main=575 hp |power alt=429 kW

|max speed main=120 mph |max speed alt=100 kt, 190 km/h |cruise speed main=103 mph |cruise speed alt=89 kt, 166 km/h |range main=825 mi |range alt=717 kt, 1,330 km |ceiling main=14,100 ft |ceiling alt=6,400 m |loading main=11.66 lb/ft² |loading alt=56.92 kg/m² |power/mass main=0.0861 hp/lb |power/mass alt=142 W/kg

|guns=3× .30 in (7.62 mm) Browning machine guns |bombs=2,500 lb (1,100 kg); 4,000 lb (1,800 kg) on short runs

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