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Lembaga Industri Penerbangan Nurtanio NU-25 Kunang / NU-35 Kunang
Development of the original NU-25 Kunang was started in 1957, to provide Indonesian flying clubs with an economical single-seat ultra-light trainer.
The original tapered wing, with fixed slots, was replaced by a constant-chord wing of 25 percent greater area during 1960. At the same time, the Volkswagen engine has been uprated from 25 to 35 h.p. and a cockpit canopy has been fitted. Now designated NU-35, the Kunang is of conventional wooden construction, with fabric covering.
NU-35 Kunang
Engine: Volkswagen, 35 hp
Span: 23 ft ll in
Height: 5 ft 11 in
Wing area: 102.6 sq.ft
Gross weight: 743 1b
Empty weight: 504 lb
Cruising speed: 80 mph
Max rate of climb at SL: 300 ft/min

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