Credit
Alert5 · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
FTC-2000 · excluding nose-probe
Single source14.555 m (47 ft 9 in) excluding nose-probe[source]
G-4M · Length
Configuration
| Specification | Guizhou JL-9 | Soko G-4 Super Galeb |
|---|---|---|
| Type | Advanced jet trainer Light combat aircraft[source] | Military trainer aircraft[source] |
| Manufacturer | Guizhou Aviation Industry Import/Export Company (GAIEC)[source] | SOKO[source] |
| Designer | Aero Engine Research Institute of Guizhou Aviation Industry Corporation[source] | Aeronautical Technical Institute[source] |
| Status | In service[source] | In service |
12.25 m (40 ft 2 in)[source]
Ferry; FTC-2000 · with maximum internal and external fuel
Single sourceFTC-2000 · on internal fuel
Single source863 km (536 mi, 466 nmi) on internal fuel[source]
2,400 km (1,500 mi, 1,300 nmi) with maximum internal and external fuel[source]
Ferry; G-4M · maximum internal and external fuel
Single sourceG-4M · Internal fuel
Single sourceG-4M · Combat range
Single sourceG-4M · with cannon pack and four BL755 cluster bombs (combat radius
Single source1,300 km (810 mi, 700 nmi) with cannon pack and four BL755 cluster bombs (combat radius 485 km)[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]
G-4M · 1 × Rolls-Royce Viper 632-46 turbojet thrust
Single source1 × Rolls-Royce Viper 632-46 turbojet , 17.8 kN (4,000 lbf) thrust[source]
FTC-2000 · Endurance
Single source3 hours[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | People's Liberation Army Air Force People's Liberation Army Navy Air Force Myanmar Air Force Sudanese Air Force[source] | Serbian Air Force Myanmar Air Force Montenegrin Air Force (historical) Yugoslav Air Force (historical)[source] |
|---|
| First flight | 13 December 2003[source] | 17 July 1978[source] |
|---|
| Developed from | Chengdu JJ-7[source] | — |
|---|
| Fuel capacity | 2,000 kg (4,409 lb) internal + up to 1,302 kg (2,870 lb) in external tanks[source] | 1,882 kg (maximum internal and external fuel)[source] |
|---|
| Guns | 1 × 23 mm cannon[source] | — |
|---|
| Hardpoints | 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] | — |
|---|
| Unstick and touchdown speed | 260 km/h (160 mph; 140 kn)[source] | — |
|---|
| Minimum flying speed | 210 km/h (130 mph; 110 kn)[source] | — |
|---|
| Stall speed | 125 km/h (78 mph, 67 kn)[source] | 180 km/h (97 mph, 112 kn) (flaps and undercarriage down)[source] |
|---|
| g limits | + 8 - 3[source] | -4.2 to +8[source] |
|---|
| Wing loading | 374.8 kg/m 2 (76.8 lb/sq ft)[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 | — |
|---|
| National origin | — | Yugoslavia[source] |
|---|
| Number built | — | 85[source] |
|---|
| Manufactured | — | 1984–1991[source] |
|---|
| Introduction date | — | 1983[source] |
|---|
| Aspect ratio | — | 5.01[source] |
|---|
| Never exceed speed | — | 921 km/h (572 mph, 497 kn) 0.9M at 11,000 m[source] |
|---|
| Time to altitude | — | 6 minutes to 8,000m[source] |
|---|
| Reported operators |
| — |
|---|
Maximum take-off; G-4M · Max takeoff weight
Single source