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were installed on the upper wings only. The upper wing span was 38 feet, while the lower wing span was 35 feet. Overall length was 24 feet, at a height of 9 feet. Empty weight was 1500 pounds. The landing gear had a split-axle design, with hydraulic struts and rubber bungee cords.
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with its fuselage frame manufactured from thin-walled steel tubing, as were the horizontal and vertical stabilizers, the elevators and rudder. The wings had
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Corporation. Only one example was manufactured, at the original
Stearman factory in
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First flight was in March 1927. Initially powered by a 90 hp (67 kW)
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with the pilot in the aft cockpit and two passengers in the forward cockpit.
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106:(or Stearman Sport Commercial Model 1) was the first type of
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494:This article on an aircraft of the 1920s is a
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458:United Aircraft and Transport Corporation
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186:Stearman Aircraft: A Detailed History
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141:. The aircraft had two tandem open
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184:Phillips, Edward (2006).
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169:and designated the C1X.
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74:March 1927
539:Categories
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128:sesquiwing
446:Companies
550:Biplanes
244:Aircraft
147:Ailerons
143:cockpits
130:type of
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132:biplane
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38:Role
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382:BT-5
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367:A-21
336:X-91
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190:ISBN
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