Credit
Alan Wilson from Peterborough, Cambs, UK · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
1976 150M Commuter II · Length
Single source23 ft 11 in (7.29 m)[source]
FTC-2000 · excluding nose-probe
Configuration
| Specification | Cessna 150 | Guizhou JL-9 |
|---|---|---|
| Type | Light utility aircraft, basic trainer[source] | Advanced jet trainer Light combat aircraft[source] |
| Manufacturer | Cessna[source] | Guizhou Aviation Industry Import/Export Company (GAIEC)[source] |
| Status | In service[source] | In service[source] |
| Number built | 23,839[source] | — |
| Manufactured |
14.555 m (47 ft 9 in) excluding nose-probe[source]
Empty; 1976 150M Commuter II · Empty weight
Single sourceMaximum take-off; 1976 150M Commuter II · Max takeoff weight
Single source1,122 lb (509 kg)[source]
1,600 lb (726 kg)[source]
Gross; FTC-2000 · clean
Single sourceMaximum take-off; FTC-2000 · Max takeoff weight
Single sourceCruise; 1976 150M Commuter II · at 10,000 ft (3,050 m) (econ cruise)
Single sourceMaximum; 1976 150M Commuter II · at sea level
Single source109 kn (125 mph, 202 km/h) at sea level[source]
82 kn (94 mph, 152 km/h) at 10,000 ft (3,050 m) (econ cruise)[source]
Cruise; FTC-2000 · Cruise speed
Single sourceMaximum; FTC-2000 · / Mach 0.89
Single source1976 150M Commuter II · econ cruise, standard fuel
Single source420 nmi (480 mi, 780 km) (econ cruise, standard fuel)[source]
1976 150M Commuter II · 1 × Continental O-200-A air-cooled horizontally-opposed engine
Single source1 × Continental O-200-A air-cooled horizontally-opposed engine, 100 hp (75 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.
1958–1977[source] |
| — |
| First flight | September 12, 1957[source] | 13 December 2003[source] |
|---|
| Variant | Cessna 152[source] | — |
|---|
| Capacity | one passenger (plus two children not exceeding 120 lb (54 kg) on optional bench seat in baggage space)[source] | — |
|---|
| Fuel capacity | 22.5 US gal (18.7 imp gal; 85 L) usable internal fuel[source] | 2,000 kg (4,409 lb) internal + up to 1,302 kg (2,870 lb) in external tanks[source] |
|---|
| Aspect ratio | 6.7:1[source] | — |
|---|
| Airfoil | NACA 2412[source] | — |
|---|
| Propellers | 2-bladed McCauley 1A102/OCM metal fixed-pitch propeller, 5 ft 9 in (1.75 m) diameter[source] | — |
|---|
| Stall speed | 42 kn (48 mph, 78 km/h) (flaps down, power off)[source] | 125 km/h (78 mph, 67 kn)[source] |
|---|
| Never exceed speed | 140 kn (160 mph, 260 km/h)[source] | — |
|---|
| Take-off run to 50 ft (15 m) | 1,385 ft (422 m)[source] | — |
|---|
| Landing run from 50 ft (15 m) | 1,075 ft (328 m)[source] | — |
|---|
| Country of origin | United States[source] | Volksrepublik China[source]Country of design · Entwurfsland |
|---|
| 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] |
|---|
| Developed from | — | Chengdu JJ-7[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] |
|---|
| 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] |
|---|
| 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] |
|---|
| Reported operators | — |
|
|---|