Stearman XA-21

Length
16.18 m
Flat Wing Span
19.81 m
Height
4.32 m
Flat Wing Area
56.39 m²
Cruise Speed
322 km/h
Max Speed
414 km/h
Number of Engines
2
First Flight
1938-01-01
Number Built
1

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Aircraft Weight Variants

Aircraft
Stearman XA-21

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All data (23 fields)
Name
Stearman XA-21
Manufacturer
Boeing
Description
The Stearman XA-21 (Model X-100) was a competitor in a United States Army Air Corps competition for a twin-engined attack aircraft which (after redesigns) led to the Douglas A-20 Havoc, Martin A-22 Maryland and North American B-25 Mitchell.
First Flight
1938-01-01
Designer
Boeing
Type
Ground attack
Length (m)
16.18
Height (m)
4.32
Cockpit Crew
3
Max Speed (km/h)
414
Cruise Speed (km/h)
322
Armament
4 × wing-mounted 0.30 in M1919 Browning machine guns; 1 × nose-mounted 0.30 in in machine gun; 4 × aft-firing 0.30 in in machine guns; 2700 lb
Capacity Description
5,560 lb (2,520 kg)
National Origin
United States of America
Number Built
1
Powerplant Description
2 × Pratt & Whitney R-2180-7 Twin Hornet radial engines, 1030 kW (1381 hp) each
Primary Users
United States Army Air Corps
Status
Prototype
Wikipedia Article (URL)
en.wikipedia.org/wiki/Stearman_XA-21
Flat Wing Span (m)
19.81
Flat Wing Area (m²)
56.39
Aircraft Engine
Pratt & Whitney R-2180-A Twin Hornet
Number of Engines
2