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]
M26 01 · Length
Configuration
| Specification | Guizhou JL-9 | PZL M26 Iskierka |
|---|---|---|
| Type | Advanced jet trainer Light combat aircraft[source] | Trainer aircraft[source] |
| Manufacturer | Guizhou Aviation Industry Import/Export Company (GAIEC)[source] | PZL Mielec[source] |
| Designer | Aero Engine Research Institute of Guizhou Aviation Industry Corporation[source] | — |
| Status | In service[source] | in production[source] |
8.295 m (27 ft 3 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]
M26 01 · 30 min reserve fuel
Single source1,410 km (880 mi, 760 nmi) 30 min reserve fuel[source]
M26 01 · 1 × Textron Lycoming AEIO-540-L1B5 6-cylinder horizontally-opposed air-cooled piston engine
Single source1 × Textron Lycoming AEIO-540-L1B5 6-cylinder horizontally-opposed air-cooled piston engine, 224 kW (300 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]
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] | US civilian aviation Poland Venezuela[source] |
|---|
| First flight | 13 December 2003[source] | July 15, 1986[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] | 369 L (97 US gal; 81 imp gal) in four wing tanks; Oil capacity 18 L (4.8 US gal; 4.0 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] | — |
|---|
| 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] | — |
|---|
| g limits | + 8 - 3[source] | +6 / -3 Aerobatic mission; +4.4 / -1.76 Utility mission at Max take-off weight[source] |
|---|
| Wing loading | 374.8 kg/m 2 (76.8 lb/sq ft)[source] | 93.9 kg/m 2 (19.2 lb/sq ft) Aerobatic mission; 100 kg/m 2 (20 lb/sq ft) Utility mission[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 | — |
|---|
| Number built | — |
|---|
| Aspect ratio | — | 5.3[source] |
|---|
| Airfoil | — | NACA65 2 -415[source] |
|---|
| Propellers | — | 3-bladed Hoffman HO-V123K-V/200AH-10 OR Hartzell HC-C3YR-4BF, 1.9 m (6 ft 3 in) diameter constant-speed propeller[source] |
|---|
| Never exceed speed | — | 395 km/h (245 mph, 213 kn) Aerobatic mission; 371 km/h (231 mph; 200 kn) Utility mission[source] |
|---|
| Power/mass | — | 5.88 kg/kW (9.66 lb/hp) Aerobatic mission; 6.26 kg/kW (10.29 lb/hp) Utility mission[source] |
|---|
| National origin | — | Poland[source] |
|---|
| Reported operators |
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Maximum take-off; M26 01 · Utility mission
Single source1,040 kg (2,293 lb)[source]
1,315 kg (2,899 lb) Aerobatic mission; 1,400 kg (3,100 lb) Utility mission[source]
330 km/h (210 mph, 180 kn) Aerobatic mission; 321 km/h (199 mph; 173 kn) Utility mission[source]