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A p p e a r a n c e
F r o m W i k i p e d i a , t h e f r e e e n c y c l o p e d i a
Hindustan Aeronautics started to design an agricultural aircraft in 1968 designated the HAL-31 Mk 1 with a cockpit directly over the wing leading edge. It was re-designed as the HA-31 Mk II Basant and first flew on the 30 March 1972. The Basant is a conventional braced low-wing monoplane with a fixed tailwheel landing gear and powered by a 400 hp (298 kW ) Avco Lycoming IO-720 piston engine. It had a raised cockpit to give the pilot a good all-round view during spraying operations. Production ended in 1980 after 39 aircraft had been built.
Specifications (Mk II) [ edit ]
Data from The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985) , 1985, Orbis Publishing, Page 2160
General characteristics
Crew: One
Length: 29 ft 6.25 in (9.0 m )
Wingspan: 39 ft 4.5 in (12 m )
Height: 8 ft 4.5 in (2.55 m )
Wing area: 251.23 sq ft (23.34 m 2 )
Empty weight: 2,645 lb (1,200 kg )
Gross weight: 5,000 lb (2,270 kg )
Powerplant: 1 × Avco Lycoming IO-720-C1B flat-eight piston engine , 400 hp (298 kW)
Performance
Maximum speed: 140 mph (225 km/h, 120 kn ) [1]
Cruise speed: 115 mph (185 km/h, 100 kn )
Range: 400 mi (645 km, 350 nmi) [1]
Service ceiling: 12,500 ft (3,800 m ) [1]
Rate of climb: 750 ft/min (3.8 m/s) [1]
See also [ edit ]
Aircraft of comparable role, configuration, and era
References [ edit ]
^ a b c d Taylor 1981, pp. 90–91
Bibliography [ edit ]
Taylor, J. W. R. (ed.). Jane's All the World's Aircraft 1980–81 . London: Jane's, 1981. ISBN 0-531-03953-6 .
The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985) , 1985, Orbis Publishing, Page 2160
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C a t e g o r i e s :
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