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CNIAR / IAR IAR-817

 CNIAR-817-01
 
In 1955, a prototype of a new utility aircraft, the IAR-817, was first flown at the URMV-3 works of Industria Aeronautică Română at Brașov. The URMV-3 works had been formed at the Sovromtractor tractor factory, itself on the site of the Industria Aeronautică Română aircraft works. It was a single-engine high-wing monoplane with a pod-and-boom type fuselage of welded steel tube construction and fabric-covered wooden wings. It had a fixed tricycle undercarriage. The aircraft was powered by a single 120 kW (160 hp) Walter Minor 6-III air-cooled six-cylinder inverted inline engine.
 
 CNIAR-817-02
 
An air-ambulance version of the IAR-817, the IAR-817S, entered production in 1957, with over 60 built.
 
 CNIAR-817-03
 
The type formed the basis of the IAR-818, built from 1961.
 
Engine: 1 × Walter Minor 6-III, 120 kW (160 hp)
Propeller: 2-bladed variable-pitch
Wingspan: 12.6 m (41 ft 4 in)
Wing area: 25.4 m2 (273 sq ft)
Length: 9.8 m (32 ft 2 in)
Height: 3.4 m (11 ft 2 in)
Empty weight: 800 kg (1,764 lb)
Max takeoff weight: 1,150 kg (2,535 lb)
Maximum speed: 175 km/h (109 mph, 94 kn)
Cruise speed: 165 km/h (103 mph, 89 kn)
Stall speed: 70 km/h (43 mph, 38 kn)
Range: 560 km (350 mi, 300 nmi)
Ferry range: 930 km (580 mi, 500 nmi)
Service ceiling: 3,000 m (9,800 ft)
Time to 1,000 m (3,300 ft): 7 minutes 30 seconds
Take-off run: 150–180 m (490–590 ft)
Landing run: 60 m (200 ft)
Crew: 1 or 2
Seats: 4-5
 
 CNIAR-817-04
 
 
 
 
 


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