Credit
George Trussell · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
standard EMB 312 · Length
Single source9.86 m (32 ft 4 in)[source]
KT-1 · Length
Configuration
| Specification | Embraer EMB 312 Tucano | KAI KT-1 Woongbi |
|---|---|---|
| Type | Trainer and light attack aircraft[source] | Basic trainer and light attack aircraft[source] |
| National origin | Brazil[source] | South Korea[source] |
| Manufacturer | Embraer[source] | Korea Aerospace Industries[source] |
| Status | In service[source] | In service |
10.3 m (33 ft 10 in)[source]
Cruise; standard EMB 312 · Cruise speed
Single sourceMaximum; standard EMB 312 · at 4,115 metres (13,500 ft)
Single source458 km/h (285 mph, 247 kn) at 4,115 metres (13,500 ft)[source]
441 km/h (274 mph, 238 kn)[source]
Maximum; KT-1 · at 4,570 m (14,993 ft)
Single source644 km/h (400 mph, 348 kn) at 4,570 m (14,993 ft)[source]
standard EMB 312 · Range
Single source1,916 km (1,191 mi, 1,035 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]
standard EMB 312 · 1 × Pratt & Whitney Canada PT6A-25C turboprop engine
Single source1 × Pratt & Whitney Canada PT6A-25C turboprop engine, 552 kW (740 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 · (3,500 ft/min) at sea level, clean
Single source17.78 m/s (3,500 ft/min) at sea level, clean[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | Brazilian Air Force Egyptian Air Force Argentine Air Force Peruvian Air Force[source] | Republic of Korea Air Force Indonesian Air Force Turkish Air Force Peruvian Air Force Senegalese Air Force[source] |
|---|
| Number built | 637[source] | 186[source] |
|---|
| Manufactured | 1980–1996[source] | 1999–present[source] |
|---|
| Introduction date | September 1983[source] | 2000[source] |
|---|
| First flight | 16 August 1980[source] | November 1991[source] |
|---|
| Variant | Short Tucano[source] | — |
|---|
| Developed into | Embraer EMB 314 Super Tucano[source] | — |
|---|
| Fuel capacity | 694 litres (183 US gal; 153 imp 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] |
|---|
| Guns | ** Gun pods : AN/M-B machine gun 12,7 mm machine gun 7,62 mm machine gun (500 rounds) Rocket Machine Gun pod: RMP LC with a 12.7mm M3P and (4x) 70 mm[source] | — |
|---|
| Hardpoints | 4 under-wing pylons with a capacity of 1,000 kg (2,200 lb)[source] | — |
|---|
| Airfoil | root: NACA 63A415 ; tip: NACA 63A212[source] | root: NACA 63-218 ; tip: NACA 63-212[source] |
|---|
| Propellers | 4-bladed constant-speed propeller[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 | 124 km/h (77 mph, 67 kn)[source] | 132 km/h (82 mph, 71 kn) flaps down[source] |
|---|
| Never exceed speed | 539 km/h (335 mph, 291 kn)[source] | 648 km/h (403 mph, 350 kn)[source] |
|---|
| g limits | + 6 /- 3[source] | + 7 - 3.5 (aerobatic, clean)[source] |
|---|
| Wing loading | 164 kg/m 2 (34 lb/sq ft)[source] | 206.8 kg/m 2 (42.4 lb/sq ft) with external stores[source] |
|---|
| Rocket Machine Gun pod | RMP LC with a 12.7mm M3P and (4x) 70 mm[source] | — |
|---|
| Rockets | ** 127 mm HVAR ground rockets Rocket pods: SBAT (7x) 37 mm SBAT (7x) 70 mm[source] | — |
|---|
| Rocket pods | SBAT (7x) 37 mm SBAT (7x) 70 mm[source] | — |
|---|
| Bombs | ** General-purpose bomb : Mk 81 Mk 82 Practice bomb: MK 76 (20 lb)[source] | — |
|---|
| Practice bomb | MK 76 (20 lb)[source] | — |
|---|
| Others | Ferry tanks: 2x 660 litres (170 US gal) or 330 litres (87 US gal)[source] | — |
|---|
| Ferry tanks | 2x 660 litres (170 US gal) or 330 litres (87 US gal)[source] | — |
|---|
| Designer | — | Agency for Defence Development Korea Aerospace Industries[source] |
|---|
| Aspect ratio | — |
|---|
| 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