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Douglas T2D / P2D

 

douglast2d


In July 1925 the US Navy Bureau of Aeronautics ordered three Douglas XT2D-1 twin-engined torpedo-bomber/ general-purpose biplanes. They were required to be suitable for use with wheel or float landing gear, and for operation from aircraft-carriers. Two months earlier a single XTN-1 aircraft, with similar general characteristics, had been ordered from the US Naval Aircraft Factory.


The first XT2D-1 prototype flew on 27 January 1927 as a landplane. Soon afterwards its 373kW Wright P-2 radial engines were replaced by Wright R-1750s and the other two prototypes were similarly re-engined. The three aircraft participated successfully in trials with US Navy Torpedo Squadron VT-2 in spring 1927 and, nine examples of the production T2D-1 were purchased.


The basic configuration of the XT2D-1 prototypes was retained, a large single fin and rudder, wide-track divided landing gear capable of easy conversion to take twin floats, and two-bay equal-span wings with rounded tips. The fuselage of the T2D-1 was 0.90m shorter than that of the XT2D-1 and the engine nacelles were repositioned. A crew of four was carried, the pilot and co-pilot in tandem open cockpits, with gunner/ bomb-aimer in the nose and radio-operator/gunner in the fourth cockpit amidships.


The T2D-1 performed satisfactorily in service, operating from aircraft-carriers (being the first twin-engined aircraft to do so) during the 1928 US Navy fleet exercises. However, its size precluded embarkation of the carrier's full aircraft complement and, as a result, the type was re-allocated to patrol squadrons. T2D-1s flew subsequently with VP-1 and VP-2 from Pearl Harbor, Hawaii, operating on wheels or twin floats as required until scrapped in 1933.


Variant
P2D-1: in June 1930 the Douglas company received an order for 18 aircraft based on the T2D-1, but intended specifically for over-sea patrol duties; these new P2D-1 aircraft had twin fins and rudders to ensure better flight characteristics, particularly with one engine inoperative, and were powered by 429kW Wright R-1820-E radial engines; deliveries were completed by the end of 1931 and the P2D-1s, almost always in twin-float configuration, flew with VP-3 of the US Navy stationed in the Panama Canal Zone, until withdrawn from first-line service in 1937.

T2D-1
Engine: 2 x Wright R-1750 radial piston engines, 391kW
Take-off weight: 4773 kg / 10523 lb
Empty weight: 2726 kg / 6010 lb
Wingspan: 17.37 m / 56 ft 12 in
Length: 12.80 m / 41 ft 12 in
Height: 4.85 m / 15 ft 11 in
Wing area: 82.31 sq.m / 885.98 sq ft
Max. speed: 201 km/h / 125 mph
Ceiling: 4215 m / 13850 ft
Range: 735 km / 457 miles

 


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