
A-3

Skywarrior

First flight
1953
In service
1953
info
Total in database
Crashed
0
info
Displays
info
Land Leased





Variant | First Flight | Max Speed | Max Range | Max Weght | Max Celling: | Wing Span | length | height |
|---|---|---|---|---|---|---|---|---|
XBT-4 | 01/01/1940 | experimental only | — | 1939 | — | — | — | — |
A3D-1 (A-3A) | 01/01/1952 | 610 | 2100 | ~70000 | 40500 | 22.9 | 76.4 | 72.6 |
XA3D-1 | 01/01/1952 | 610 | 2100 | ~70000 | 40500 | 22.9 | 76.4 | 72.6 |
YA3D-1 (YA-3A) | 01/01/1953 | 610 | 2100 | ~70500 | 40500 | 22.9 | 76.4 | 72.6 |
A3D-1Q (EA-3A) | 01/01/1956 | 610 | 2000 | ~73000 | 40000 | 22.9 | 76.4 | 72.6 |
A3D-2 (A-3B) | 01/01/1956 | 610 | 2100 | ~82000 | 40500 | 22.9 | 76.4 | 72.6 |
A3D-1P (RA-3A) | 01/01/1956 | 610 | 2100 | ~72000 | 40500 | 22.9 | 76.4 | 72.6 |
A3D-2T (TA-3B) | 01/01/1959 | 610 | 2100 | ~82000 | 40500 | 22.9 | 76.4 | 72.6 |
A3D-2P (RA-3B) | 01/01/1959 | 610 | 2100 | ~82000 | 40500 | 22.9 | 76.4 | 72.6 |
A3D-2Q (EA-3B) | 01/01/1960 | 610 | 2000 | ~82000 | 40000 | 22.9 | 76.4 | 72.6 |
NRA-3B | 01/01/1960 | 610 | 2000 | ~82000 | 40000 | 22.9 | 76.4 | 72.6 |
NTA-3B | 01/01/1960 | 610 | 2000 | ~82000 | 40000 | 22.9 | 76.4 | 72.6 |
A VA-3B | 01/01/1963 | 610 | 2100 | ~82000 | 40500 | 22.9 | 76.4 | 72.6 |
VA-3B | 01/01/1963 | 610 | 2100 | ~82000 | 40500 | 22.9 | 76.4 | 72.6 |
EKA-3B | 01/01/1967 | 610 | 2000 | ~82000 | 40000 | 22.9 | 76.4 | 72.6 |
ERA-3B | 01/01/1967 | 610 | 2000 | ~82000 | 40000 | 22.9 | 76.4 | 72.6 |
KA-3B | 01/01/1967 | 610 | 2000 | ~82000 | 40000 | 22.9 | 76.4 | 72.6 |
The Douglas XBT-4 was an experimental development of the U.S. Navy’s BT-2 two-seat scout bomber, intended to evaluate the feasibility of retractable landing gear on carrier-based aircraft. Built in 1935 as a single prototype, the XBT-4 served as an engineering testbed rather than a true combat aircraft. Although only one was constructed, it played a small but significant role in shaping U.S. Navy carrier aircraft design philosophy during the late interwar period.
Development and Role
The XBT-4 was born from the Navy’s desire to improve the performance of its carrier aircraft, which still relied heavily on fixed landing gear and drag-inducing structures. Building on the Douglas BT-2 airframe, engineers sought to test whether retractable landing gear could provide meaningful performance advantages without compromising ruggedness for deck operations.
Its intended roles included:
Experimental evaluation of retractable landing gear in a carrier environment
Test platform for aerodynamic refinements on naval dive/scout bombers
Proof-of-concept for structural reinforcement and weight distribution in carrier-capable airframes
Although not meant for combat, the lessons learned from the XBT-4 directly informed later production aircraft, particularly the Northrop BT-1 and Douglas SBD Dauntless.
Powerplant and Enhancements
The XBT-4 was powered by a Pratt & Whitney R-1535 Twin Wasp Junior radial engine, producing around 700 horsepower.
Performance highlights included (estimated, based on BT-2 baseline figures):
Maximum speed: ~190 mph
Range: ~600 miles
Service ceiling: ~20,000 feet
Enhancements and differences compared to the BT-2 included:
Retractable main landing gear, significantly reducing drag
Structural strengthening to handle additional stresses of carrier landings with the new gear arrangement
Slightly modified engine cowling and fuselage fairings to accommodate cleaner airflow
While these changes improved aerodynamic efficiency, the Navy considered the overall gains too limited to warrant further development of the design itself.
Configuration and Equipment
The XBT-4 closely followed the configuration of the BT-2 with modifications for its test role:
Two-seat cockpit, with pilot in front and observer/rear gunner in the rear position
Fixed armament of two .30 in machine guns (one forward-firing, one flexible in rear cockpit)
Internal structure adapted to support retractable gear mechanisms
Wooden-and-metal construction typical of mid-1930s U.S. Navy designs
Provision for a light bomb load, though never intended for operational strike use
The clean, retracted landing gear marked its most distinguishing feature compared to earlier naval types.
Operational Use
The sole XBT-4 underwent a series of evaluation flights during 1935–36. Testing showed that retractable landing gear did indeed reduce drag and increase speed, but not by a margin large enough to transform the BT-2’s performance. Moreover, the added complexity raised maintenance concerns for carrier operations.
Although the XBT-4 itself did not advance beyond prototype stage, its lessons informed the Navy’s acceptance that retractable gear would become standard in the next generation of carrier aircraft, including the Douglas SBD Dauntless and subsequent dive bombers.
Crew Experience
Test pilots reported that the XBT-4 handled much like the BT-2, with only marginal improvements in speed and climb rate when the gear was retracted. While the concept proved workable, the gear system was judged somewhat fragile for repeated deck use. Observers noted that the aircraft retained the cramped workspace and limited visibility of its BT-2 predecessor. Overall, it was regarded as a useful experiment rather than a service-ready aircraft.
Conclusion
The Douglas XBT-4 was a minor but noteworthy stepping stone in U.S. naval aviation development. Though only a single prototype was built and it offered limited performance gains, the aircraft validated the Navy’s shift toward retractable landing gear in future carrier-based bombers and fighters. While the XBT-4 itself was a dead-end, its design experiments helped set the stage for the more advanced SBD Dauntless and the broader modernization of U.S. carrier aviation on the eve of World War II.
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