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HAL Pushpak
Type of aircraft From Wikipedia, the free encyclopedia
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The Hindustan HUL-26 Pushpak (lit. 'Flower')[1] was a 1950s Indian two-seat cabin monoplane designed and built by Hindustan Aeronautics Limited, based on the Aeronca Chief.[2]
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Construction and operation
The Pushpak was a high-wing braced monoplane with a fixed tailwheel landing gear.[2] The fuselage was built from metal tubing, the wing aluminum ribs on a wooden spar, all covered in fabric.[2] The Pushpak first flew on 28 September 1958 and was powered by a 90 hp (67 kW) Continental flat-four engine.[2]
Around 160 aircraft were produced for Indian flying clubs for use as basic trainers.[2] Two examples were gifted to Malaysia and were later sold to private pilot owners in the United Kingdom. These examples remained in active operation in 2013.[3]
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Operators
Former
Specifications (HUL-26)
Data from Jane's All The World's Aircraft 1965–66[4]
General characteristics
- Crew: 2
- Length: 6.40 m (21 ft 0 in)
- Wingspan: 10.97 m (36 ft 0 in)
- Height: 2.77 m (9 ft 1 in)
- Wing area: 16.2 m2 (174 sq ft)
- Empty weight: 395 kg (871 lb)
- Max takeoff weight: 613 kg (1,351 lb)
- Fuel capacity: 56 L (12 imp gal; 15 US gal)
- Powerplant: 1 × Continental C90-8F air-cooled flat-four, 67 kW (90 hp)
Performance
- Maximum speed: 144 km/h (89 mph, 78 kn)
- Cruise speed: 112 km/h (70 mph, 60 kn)
- Range: 400 km (250 mi, 220 nmi)
- Endurance: 3 hr
- Service ceiling: 4,270 m (14,000 ft)
- Rate of climb: 2.5 m/s (500 ft/min)
See also
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References
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