FORCETALLY
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At a glance
Measured figures
Tucano Replica · Length
Single source7.10 m (23 ft 4 in)[source]
KT-1 · Length
Configuration
| Specification | Flying Legend Tucano Replica | KAI KT-1 Woongbi |
|---|---|---|
| Type | Light-sport aircraft[source] | Basic trainer and light attack aircraft[source] |
| National origin | Italy[source] | South Korea[source] |
| Manufacturer | Flying Legend[source] | Korea Aerospace Industries[source] |
| Status | In production[source] |
10.3 m (33 ft 10 in)[source]
Tucano Replica · Range
Single source900 km (560 mi, 490 nmi)[source]
Ferry; KT-1 · at 6,100 m (20,013 ft) with max internal and external fuel (30 minutes reserve)
Single sourceKT-1 · at 7,620 m (25,000 ft) with max internal fuel (30 minutes reserve)
Single source1,333 km (828 mi, 720 nmi) at 7,620 m (25,000 ft) with max internal fuel (30 minutes reserve)[source]
2,070 km (1,290 mi, 1,120 nmi) at 6,100 m (20,013 ft) with max internal and external fuel (30 minutes reserve)[source]
Tucano Replica · 1 × Rotax 915 iS four cylinder, liquid and air-cooled, four stroke aircraft engine
Single source1 × Rotax 915 iS four cylinder, liquid and air-cooled, four stroke aircraft engine , 104 kW (141 hp)[source]
KT-1 · 1 × Pratt & Whitney Canada PT6A-62 turboprop engine
Single source1 × Pratt & Whitney Canada PT6A-62 turboprop engine, 708.4 kW (950.0 hp)[source]
KT-1 · < at 6,100 m (20,013 ft) with max internal fuel (
Single sourceKT-1 · reserve
Single source<4 hours at 6,100 m (20,013 ft) with max internal fuel (30 minutes reserve)[source]
KT-1 · Service ceiling
Single source11,580 m (37,990 ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
In service[source] |
| Manufactured | 2011-present[source] | 1999–present[source] |
|---|
| Introduction date | 2011[source] | 2000[source] |
|---|
| Capacity | one passenger[source] | — |
|---|
| Fuel capacity | 120 litres (26 imp gal; 32 US gal)[source] | 551 L (146 US gal; 121 imp gal) in two wing tanks with provision for two 189 L (50 US gal; 42 imp gal) drop-tanks on the inboard pylons[source] |
|---|
| Propellers | 4-bladed composite[source] | 4-bladed Hartzell HC-E4N-2/E9512CB-1, 2.44 m (8 ft 0 in) diameter constant-speed fully feathering reversible propeller[source] |
|---|
| Stall speed | 75 km/h (47 mph, 40 kn) flaps up[source] | 132 km/h (82 mph, 71 kn) flaps down[source] |
|---|
| Never exceed speed | 330 km/h (210 mph, 178 kn)[source] | 648 km/h (403 mph, 350 kn)[source] |
|---|
| g limits | +6.0/-3.0[source] | + 7 - 3.5 (aerobatic, clean)[source] |
|---|
| Wing loading | 75 kg/m 2 (15 lb/sq ft)[source] | 206.8 kg/m 2 (42.4 lb/sq ft) with external stores[source] |
|---|
| Designer | — | Agency for Defence Development Korea Aerospace Industries[source] |
|---|
| Primary users | — | Republic of Korea Air Force Indonesian Air Force Turkish Air Force Peruvian Air Force Senegalese Air Force[source] |
|---|
| Number built | — | 186[source] |
|---|
| First flight | — | November 1991[source] |
|---|
| Aspect ratio | — |
|---|
| Airfoil | — | root: NACA 63-218 ; tip: NACA 63-212[source] |
|---|
| Maximum fuel weight | — | 408 kg (899 lb)[source] |
|---|
| Power/mass | — | 0.2137 kW/kg (0.1300 hp/lb)with external stores[source] |
|---|
Maximum take-off; KT-1 · (and Maximum Landing Weight)with external stores
Single source