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]
Yak-130 · Length
Configuration
| Specification | Guizhou JL-9 | Yakovlev Yak-130 |
|---|---|---|
| Type | Advanced jet trainer Light combat aircraft[source] | Lead-in fighter trainer / Light combat aircraft[source] |
| Manufacturer | Guizhou Aviation Industry Import/Export Company (GAIEC)[source] | Yakovlev, Sokol, Yakovlev Corporation[source] |
| Designer | Aero Engine Research Institute of Guizhou Aviation Industry Corporation[source] | Yakovlev[source] |
| Status | In service[source] | Active |
11.49 m (37 ft 8 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]
Yak-130 · Range
Single source2,100 km (1,300 mi, 1,100 nmi)[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]
Yak-130 · 2 × Ivchenko-Progress AI-222-25 turbofan engines thrust each
Single source2 × Ivchenko-Progress AI-222-25 turbofan engines, 24.52 kN (5,510 lbf) thrust each[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] | Russian Aerospace Forces Bangladesh Air Force Algerian Air Force Myanmar Air Force Islamic Republic of Iran Air Force[source] |
|---|
| First flight | 13 December 2003[source] | 25 April 1996 ( 1996-04-25 ) (Yak/AEM-130) 30 April 2004 ( 2004-04-30 ) (Yak-130)[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] | — |
|---|
| Guns | 1 × 23 mm cannon[source] | SNPU-130 gun pod[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] | 8 (1 on each wingtip, usable only for flares/chaff, 3 under each wing) with a capacity of up to 3,000 kg (6,614 lb), with provisions to carry combinations of: Rockets: 80 mm S-8 rocket, S-25 rocket Missiles: R-73 infrared-homing short-range air-to-air missiles Bombs: FAB-M62, ZB-500, KAB-500Kr[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] | 165 km/h (103 mph, 89 kn)[source] |
|---|
| g limits | + 8 - 3[source] | + 8.0 − 3.0[source] |
|---|
| Wing loading | 374.8 kg/m 2 (76.8 lb/sq ft)[source] | 276.4 kg/m 2 (56.6 lb/sq ft)[source] |
|---|
| Thrust/weight | 0.00645 kN/kg (0.658 lb f /lb)[source] | 0.70[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] | R-73 infrared-homing short-range air-to-air missiles[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 | — | Russia[source] |
|---|
| Built by | — | Irkut Corporation Sokol Aircraft Plant[source] |
|---|
| Number built | — | 219[source] |
|---|
| Introduction date | — | 19 February 2010[source] |
|---|
| Variant | — | Alenia Aermacchi M-346 Master[source] |
|---|
| Rockets | — | 80 mm S-8 rocket, S-25 rocket[source] |
|---|
| Bombs | — | FAB-M62, ZB-500, KAB-500Kr[source] |
|---|
| Alternative designation | — | Yak-130[source] |
|---|
| Reported operators |
| — |
|---|
Maximum take-off; Yak-130 · Max takeoff weight
Single source