Article · Wikipedia archive · Last revised Jun 11, 2026

HAL HUL-26 Pushpak

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.

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HUL-26 Pushpak
HUL-26 Pushpak displayed at HAL Museum
General information
TypeTwo-seat cabin monoplane
ManufacturerHindustan Aeronautics Limited
Primary usersAero clubs
Private pilot owners
Number built160+
History
First flight1958
Developed fromAeronca Chief
Developed intoHAL HAOP-27 Krishak

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

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

Operators

Airworthy Hindustan Pushpak privately owned in the United Kingdom source ↗

Former

 India
 Malaysia
 United Kingdom
 Sri Lanka

Specifications (HUL-26)

Data from Jane's All The World's Aircraft 1965–664

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

See also

Related development

References

References

Notes

Bibliography