IAR-818
# IAR-818

The IAR-818 was a Romanian multipurpose aircraft based on the IAR-817. It was developed by IAR in both landplane and floatplane forms.

## Variants

### IAR-818

    Landplane utility aircraft

### IAR-818H

    Floatplane with twin floats and added ventral fin

## Specifications

Data from Romanian Aeronautical Constructions 1905–1974

General characteristics

* Crew: 1 or 2
* Capacity: 5-6
* Length: 9.9 m (32 ft 6 in)
* Wingspan: 12.1 m (39 ft 8 in)
* Height: 3.3 m (10 ft 10 in)
* Wing area: 25.4 $m^2$ (273 sq ft)
* Empty weight: 805 kg (1,775 lb)
* Gross weight: 1,180 kg (2,601 lb)
* Max takeoff weight: 1,300 kg (2,866 lb)
* Powerplant: 1 × Avia M-337 6-cylinder inverted air-cooled in-line piston engine, 155 kW (208 hp)
* Propellers: 2-bladed variable-pitch propeller

Performance

* Maximum speed: 185 km/h (115 mph, 100 kn)
* Cruise speed: 165 km/h (103 mph, 89 kn)
* Stall speed: 60 km/h (37 mph, 32 kn)
* Range: 500 km (310 mi, 270 nmi)
* Ferry range: 1,100 km (680 mi, 590 nmi)
* Service ceiling: 4,000 m (13,000 ft)
* Take-off run: 80–100 m (260–330 ft)
* Landing run: 40 m (130 ft)
