FORCETALLY
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At a glance
Measured figures
T-7 · Length
Single source8.59 m (28 ft 2 in)[source]
FTC-2000 · excluding nose-probe
Single sourceConfiguration
| Specification | Fuji T-7 | Guizhou JL-9 |
|---|---|---|
| Type | Primary/Basic Trainer[source] | Advanced jet trainer Light combat aircraft[source] |
| National origin | Japan[source] | — |
| Manufacturer | Fuji Heavy Industries[source] | Guizhou Aviation Industry Import/Export Company (GAIEC)[source] |
| Status | Active[source] | In service[source] |
| Primary user |
14.555 m (47 ft 9 in) excluding nose-probe[source]
T-7 · 1 × Rolls-Royce 250-B17F turboprop engine
Single source1 × Rolls-Royce 250-B17F turboprop engine, 336 kW (451 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 · Service ceiling
Single source16,000 m (52,000 ft)[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.
Japan Air Self-Defense Force[source] |
| — |
| Number built | 49[source] | — |
|---|
| Manufactured | 2002-present[source] | — |
|---|
| Developed from | Fuji T-3[source] | Chengdu JJ-7[source] |
|---|
| Airfoil | root: NACA 23016.5 ; tip: NACA 23012[source] | — |
|---|
| Propellers | 3-bladed constant-speed propeller, 2.12 m (6 ft 11 in) diameter[source] | — |
|---|
| Stall speed | 104 km/h (65 mph, 56 kn) flaps and gear down[source] | 125 km/h (78 mph, 67 kn)[source] |
|---|
| Wing loading | 96.1 kg/m 2 (19.7 lb/sq ft)[source] | 374.8 kg/m 2 (76.8 lb/sq ft)[source] |
|---|
| Power/mass | 0.2114 kW/kg (0.1286 hp/lb)[source] | — |
|---|
| Take-off distance to 15 m (49 ft) | 608 m (1,995 ft)[source] | — |
|---|
| Landing distance from 15 m (49 ft) | 566 m (1,857 ft)[source] | — |
|---|
| Designer | — | Aero Engine Research Institute of Guizhou Aviation Industry Corporation[source] |
|---|
| Primary users | — | People's Liberation Army Air Force People's Liberation Army Navy Air Force Myanmar Air Force Sudanese Air Force[source] |
|---|
| First flight | — | 13 December 2003[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] |
|---|
| 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] |
|---|
| g limits | — | + 8 - 3[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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