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]
FTC-2000 · excluding nose-probe
Configuration
| Specification | Embraer EMB 312 Tucano | Guizhou JL-9 |
|---|---|---|
| Type | Trainer and light attack aircraft[source] | Advanced jet trainer Light combat aircraft[source] |
| National origin | Brazil[source] | — |
| Manufacturer | Embraer[source] | Guizhou Aviation Industry Import/Export Company (GAIEC)[source] |
| Status | In service[source] | In service[source] |
14.555 m (47 ft 9 in) excluding nose-probe[source]
Empty; standard EMB 312 · Empty weight
Single sourceMaximum take-off; standard EMB 312 · Max takeoff weight
Single source1,810 kg (3,990 lb)[source]
3,175 kg (7,000 lb)[source]
Gross; FTC-2000 · clean
Single sourceMaximum take-off; FTC-2000 · Max takeoff weight
Single sourceCruise; 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]
Cruise; FTC-2000 · Cruise speed
Single sourceMaximum; FTC-2000 · / Mach 0.89
Single sourcestandard EMB 312 · Range
Single source1,916 km (1,191 mi, 1,035 nmi)[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]
FTC-2000 · 1 × Guizhou Liyang WP-13F (C) afterburning turbojet thrust dry
Single sourceFTC-2000 · thrust dry and
Single sourceFTC-2000 · with afterburner
Single sourceFTC-2000 · with afterburner (1 × WP-14C Kunlun-3 for FTC-2000G
Single source1 × Guizhou Liyang WP-13F (C) afterburning turbojet, 43.15 kN (9,700 lbf) thrust dry, 63.25 kN (14,220 lbf) with afterburner (1 × WP-14C Kunlun-3 for FTC-2000G, 53.89 kN (12,110 lbf) thrust dry and 76.53 kN (17,200 lbf) with afterburner.)[source]
FTC-2000 · Endurance
Single source3 hours[source]
FTC-2000 · (30,000 ft/min) at sea level
Single source150 m/s (30,000 ft/min) at sea level[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] |
People's Liberation Army Air Force People's Liberation Army Navy Air Force Myanmar Air Force Sudanese Air Force[source] |
| Number built | 637[source] | — |
|---|
| Manufactured | 1980–1996[source] | — |
|---|
| Introduction date | September 1983[source] | — |
|---|
| First flight | 16 August 1980[source] | 13 December 2003[source] |
|---|
| Variant | Short Tucano[source] | — |
|---|
| Developed into | Embraer EMB 314 Super Tucano[source] | — |
|---|
| Fuel capacity | 694 litres (183 US gal; 153 imp gal)[source] | 2,000 kg (4,409 lb) internal + up to 1,302 kg (2,870 lb) in external tanks[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] | 1 × 23 mm cannon[source] |
|---|
| Hardpoints | 4 under-wing pylons with a capacity of 1,000 kg (2,200 lb)[source] | 5 with a capacity of 2,000 kg (4,409 lb) maximum, with provisions to carry combinations of: Other: up to 3 x fuel tanks[source] |
|---|
| Airfoil | root: NACA 63A415 ; tip: NACA 63A212[source] | — |
|---|
| Propellers | 4-bladed constant-speed propeller[source] | — |
|---|
| Stall speed | 124 km/h (77 mph, 67 kn)[source] | 125 km/h (78 mph, 67 kn)[source] |
|---|
| Never exceed speed | 539 km/h (335 mph, 291 kn)[source] | — |
|---|
| g limits | + 6 /- 3[source] | + 8 - 3[source] |
|---|
| Wing loading | 164 kg/m 2 (34 lb/sq ft)[source] | 374.8 kg/m 2 (76.8 lb/sq ft)[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 | — | Aero Engine Research Institute of Guizhou Aviation Industry Corporation[source] |
|---|
| Developed from | — | Chengdu JJ-7[source] |
|---|
| Unstick and touchdown speed | — | 260 km/h (160 mph; 140 kn)[source] |
|---|
| Minimum flying speed | — | 210 km/h (130 mph; 110 kn)[source] |
|---|
| Thrust/weight | — | 0.00645 kN/kg (0.658 lb f /lb)[source] |
|---|
| Take-off run | — | 400–500 m (1,300–1,600 ft)[source] |
|---|
| Landing run | — | 700 m (2,300 ft)[source] |
|---|
| Other | — | up to 3 x fuel tanks[source] |
|---|
| Missiles | — | ** Short range air-to-air missile 2 × PL-8 AAMs (on inboard pylons) 2 × PL-9 AAMs (on outboard pylons) Beyond-visual-range air-to-air missiles SD-10 (Only on FTC-2000G) Anti-radiation missiles CM-102 (Only on FTC-2000G)[source] |
|---|
| Beyond-visual-range air-to-air missiles | — | SD-10 (Only on FTC-2000G)[source] |
|---|
| Anti-radiation missiles | — | CM-102 (Only on FTC-2000G)[source] |
|---|
| Country of origin | — | Volksrepublik China[source]Country of design · Entwurfsland |
|---|
| Reported operators | — |
|
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