HAL Pushpak
| HUL-26 Pushpak | |
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| HUL-26 Pushpak displayed at HAL Museum | |
| Role | Two-seat cabin monoplane |
| Manufacturer | Hindustan Aeronautics Limited |
| First flight | 1958 |
| Number built | 160+ |
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The Hindustan HUL-26 Pushpak was a 1950s Indian two-seat cabin monoplane designed and built by Hindustan Aeronautics Limited, based on the Aeronca Chief.[1] The Pushpak was a high-wing braced monoplane with a fixed tailwheel landing gear.[1] The fuselage was built from metal tubing, the wing a aluminum ribs on a wooden spar, all covered in fabric.[1] The Pushpak first flew on 28 September 1958 and was powered by a 90 hp (67 kW) Continental flat-four engine.[1] Around 160 aircraft were produced for Indian flying clubs for use as basic trainers.[1]
Operators
Former
- One gifted by India
Specifications (HUL-26)
Data from Jane's All The World's Aircraft 1965–66[2]
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)
- Cruising speed: 112 km/h (70 mph; 60 kn)
- Range: 400 km (249 mi; 216 nmi)
- Endurance: 3 hr
- Service ceiling: 4,270 m (14,009 ft)
- Rate of climb: 2.5 m/s (500 ft/min)
References
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Wikimedia Commons has media related to HUL-26 Pushpak. |
- Notes
- 1 2 3 4 5 Orbis 1985, p. 2172
- ↑ Taylor 1965, p. 80
- Bibliography
- Taylor, John W. R. (1965). Jane's All The World's Aircraft 1965–66. London: Sampson Low, Marston & Co., Ltd.
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, p. 2172.
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