Credit
MilborneOne · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
Measured figures
Cessna 152 · Length
Single source24 ft 1 in (7.34 m)[source]
FTC-2000 · excluding nose-probe
Single sourceConfiguration
| Specification | Cessna 152 | Guizhou JL-9 |
|---|---|---|
| Type | Basic trainer , GA private aircraft[source] | Advanced jet trainer Light combat aircraft[source] |
| National origin | United States[source] | — |
| Manufacturer | Cessna[source] | Guizhou Aviation Industry Import/Export Company (GAIEC)[source] |
| Primary users | Mexican Navy Bangladesh Army Bolivian Air Force[source] | People's Liberation Army Air Force People's Liberation Army Navy Air Force Myanmar Air Force Sudanese Air Force |
14.555 m (47 ft 9 in) excluding nose-probe[source]
Cessna 152 · Range
Single sourceFerry; Cessna 152 · with long-range tanks
Single source477 mi (768 km, 415 nmi)[source]
795 mi (1,279 km, 691 nmi) with long-range tanks[source]
Ferry; FTC-2000 · with maximum internal and external fuel
Single sourceFTC-2000 · on internal fuel
Single sourceCessna 152 · 1 × Lycoming O-235 -L2C flat-4 engine
Single source1 × Lycoming O-235 -L2C flat-4 engine , 110 hp (82 kW)[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.
| Number built | 7,584[source] | — |
|---|
| Manufactured | 1977–1985[source] | — |
|---|
| Introduction date | 1977[source] | — |
|---|
| Developed from | Cessna 150[source] | Chengdu JJ-7[source] |
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| Capacity | one passenger (plus two children not exceeding 120 lb (54 kg) on optional baggage compartment bench seat)[source] | — |
|---|
| Propellers | 2-bladed fixed pitch, 69 inches (175 cm) McCauley or 72 in (183 cm) Sensenich propeller[source] | — |
|---|
| Stall speed | 49 mph (79 km/h, 43 kn) (power off, flaps down)[source] | 125 km/h (78 mph, 67 kn)[source] |
|---|
| Designer | — | Aero Engine Research Institute of Guizhou Aviation Industry Corporation[source] |
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| Status | — | In service[source] |
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| 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] |
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| 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] |
|---|
| 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] |
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| Landing run | — | 700 m (2,300 ft)[source] |
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| 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 |
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| Reported operators | — |
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