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]
UTVA 75A21 · Length
Configuration
| Specification | Guizhou JL-9 | UTVA 75 |
|---|---|---|
| Type | Advanced jet trainer Light combat aircraft[source] | Military and civilian trainer aircraft[source] |
| Manufacturer | Guizhou Aviation Industry Import/Export Company (GAIEC)[source] | UTVA[source] |
| Designer | Aero Engine Research Institute of Guizhou Aviation Industry Corporation[source] | — |
| Status | In service[source] | Active[source] |
7.11 m (23 ft 4 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; UTVA 75A21 · Ferry range
Single sourceUTVA 75A21 · Range
Single sourceUTVA 75A21 · 1 × Lycoming IO-360-B1F 4-cyl. air-cooled horizontally-opposed piston engine
Single source1 × Lycoming IO-360-B1F 4-cyl. air-cooled horizontally-opposed piston engine, 134 kW (180 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]
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] |
| — |
| First flight | 13 December 2003[source] | 19 May 1976[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] | standard:160 L (42 US gal; 35 imp gal): with drop tanks 360 L (95 US gal; 79 imp gal)[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] | 2 with a capacity of 150 kg (330 lb) each, with provisions to carry combinations of:[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] | 95 km/h (59 mph, 51 kn) flaps up at idle[source] |
|---|
| g limits | + 8 - 3[source] | +4.4 -2.2[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] | 2 × MAC-AA-52 container with 7.62 mm , or 2 × cargo container 100 kg capacity, or 2 × drop 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] |
|---|
| Primary user | — | Serbia Air Force[source] |
|---|
| Introduction date | — | 1978[source] |
|---|
| Capacity | — | 210 kg (460 lb) max[source] |
|---|
| Aspect ratio | — | 6.5[source] |
|---|
| Propellers | — | 2-bladed Hartzell HC-C2YK-1BF/F7666A variable-pitch metal propeller[source] |
|---|
| Never exceed speed | — | 270 km/h (168 mph, 146 kn)[source] |
|---|
| Takeoff distance to 50 ft (15 m) | — | 501 m grass at Sea Level[source] |
|---|
| Landing distance from 50 ft (15 m) | — | 450 m grass at Sea Level[source] |
|---|
| Rockets | — | 2 × RL 128-02 128 mm (HVAR-5), or 2 × 57 millimetres (2.2 in) rocket launchers with 12 rockets[source] |
|---|
| Bombs | — | 2 × 120 kg bombs, or 4 × 50 kg bombs[source] |
|---|
| standard | — | (model 75) KING KR85 ADF and KING KY 195B[source] |
|---|
| optional | — | (model 75A catalog only) KING KR87 ADF, RNAV KING KNS81 VOR/LOC: KING KN 53, KING KY 197 Indicators: HSI KING KI 525A, and RMI KING KI 229, DME:KING KN 62A, Transponder: KING KT 79, Audio panel: KING KMA 24[source] |
|---|
| Reported operators |
| — |
|---|