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New Standard D-29
Type of aircraft From Wikipedia, the free encyclopedia
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The New Standard D-29 is a trainer aircraft produced in the US from 1929 to 1930. It was a conventional biplane design with a fuselage constructed from duralumin members riveted and bolted together, and the wings were made with spruce spars and bass-wood and plywood built-up ribs. Deliberately built to be rugged and simple the D-29 was moderately successful, but had to compete with the Swallow TP.[1]
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Variants
Data from: Aerofiles[2]
- D-29
- initial version 85 hp Cirrus III engine, one built.
- D-29A
- production aircraft with 100 hp (75 kW) Kinner K-5. Six supplied to US Navy as the NT-1 trainer in 1930.(Note: The US Navy designation NT-2 does not refer to a version of the D-29, but to two New Standard D-25s captured from smugglers and used by the US Coast Guard).[3]
- D-29 Special
- D-29A with Menasco B-4.
- D-29S – Sport version with coupe cockpit (also known as D-25C).
- D-31 Special
- D-29A with Kinner B-5.
- D-32 Special
- three-seater D-29A with Wright J-6.
- D-33 Special
- three-seater D-29A with Kinner B-5.
- NT-1
- Six D-29A trainers supplied to the US Navy.[3]
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Operators
Specifications (D-29A)
Data from U.S. Civil Aircraft Vol.2[1]
General characteristics
- Crew: 2
- Length: 24 ft 11 in (7.59 m)
- Wingspan: 30 ft 0 in (9.14 m)
- Height: 9 ft 0 in (2.74 m)
- Wing area: 248 sq ft (23.0 m2)
- Empty weight: 1,097 lb (498 kg)
- Gross weight: 1,632 lb (740 kg)
- Powerplant: 1 × Kinner B-5 5-cylinder air-cooled radial piston engine, 100 hp (75 kW)
- Propellers: 2-bladed fixed-pitch propeller
Performance
- Maximum speed: 88 mph (142 km/h, 76 kn)
- Cruise speed: 75 mph (121 km/h, 65 kn)
- Range: 300 mi (480 km, 260 nmi)
- Service ceiling: 10,000 ft (3,000 m)
- Rate of climb: 400 ft/min (2.0 m/s)
See also
Aircraft of comparable role, configuration, and era
References
External links
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