KAMOV KA-126 Civil Aircraft Model Details

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General Information of KAMOV KA-126

Designer : Kamov

Developed From : Kamov Ka-26

Developed Into : Kamov Ka-226

First Flight : 32499

Introduction : 1989

Manufacturer : Industria Aeronautica Romana

Number Built : 17

Produced : 1989-1991

Role : Light utility

Status : Active

General characteristics of KAMOV KA-126

Capacity : 6 passengers (cargo/passenger pod)

Crew : 2

Disc Area : 265.5 m² (2,856 ft²)

Empty Weight : 1,915 kg (4,222 lb)

Height : 4.155 m (13 ft 7½ in)

Length : 7.775 m (25 ft 6 in)

Max Takeoff Weight : 3,250 kg (7,165 lb)

Payload : 1,000 kg (2,205 lb) (slung load) or 1000 L (220 Imp Gallons) chemical hopper

Powerplant : 1 × Omsk TVO-100 turboshaft, 522 kW (700 hp)

Rotor Diameter : 13.00 m (42 ft 7¾ in)

Performance of KAMOV KA-126

Cruise Speed : 160 km/h (86 knots, 99 mph)

Endurance : 5 hr 36 min

Maximum Speed : 180 km/h (97 knots, 112 mph)

Range : 713 km (384nmi, 443 mi)

Rate Of Climb : 6.6 m/s (1,300 ft/min)

Service Ceiling : 3,850 m (12,630 ft)

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