Overview
KAI KC-100 Naraon — single-engine utility aircraftThe KC-100 first flew in 2011 and entered service shortly thereafter. It features a low-wing configuration and composite airframe construction. The aircraft was designed for both civil and military training roles.A Continental piston engine producing approximately 210 horsepower powers the KC-100. Cruise speed approaches 140 knots (259 km/h). Maximum takeoff weight exceeds 3,000 pounds (1,361 kg).The Naraon represents a step forward in Korea’s light aircraft manufacturing. It supports pilot training and utility missions. Production remains limited but ongoing.
Live Fleet Activity (KC100)
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Specifications
- Engine
- 1 × Continental TSIOF-550-K
- Engine type
- Piston
- Power
- 315 hp · 235 kW
- Avionics
- Avidyne
- Wing tips
- No winglets
- Seats
- 4
- Crew
- —
- Cabin width
- 4 ft 3 in · 1.30 m
- Cabin height
- 4 ft 7 in · 1.40 m
- Cabin length
- 9 ft 2 in · 2.80 m
- Exterior length
- 27 ft 11 in · 8.50 m
- Tail height
- 9 ft 5 in · 2.87 m
- Fuselage diameter
- 4 ft 8 in · 1.42 m
- Wing span
- 37 ft 4 in · 11.37 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 3,600 lb · 1,650 kg
- Max landing weight
- 2,400 lb · 1,100 kg
- Max payload
- 1,200 lb · 550 kg
- Fuel capacity
- 90 gal · 300 L · 200 kg (AvGas)
- Max cruise speed
- 210 kt · 242 mph · 389 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 68 kt · 78 mph · 126 km/h
- Range
- 1,200 nm · 1,380 mi · 2,220 km
- Fuel burn
- —
- Ceiling
- 17,400 ft · 5,300 m
- Rate of climb
- 1,250 ft/min · 6 m/s
- Takeoff distance
- —
- Landing distance
- —
Gallery