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PAF JF-17 Thunder Specifications
PAF JF-17 Thunder
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| Data for Aircraft | PAF JF-17 Thunder |
| Year Introduced | March 2007 |
| Number Built | 34 |
| Rotor Diameter | |
| Wingspan | 24.4 m² |
| Aspect Ratio | |
| Disc Loading | |
| Height | 15 ft 8 in |
| Wing Area | |
| Wing Loading | |
| Length | 15.80 |
| Lift-to-Drag Ratio | |
| Engine Type | 1 × Klimov RD-93 or WS-13 turbofan |
| Country of Origin | China, Pakistan JV |
| Empty Weight | 6,411 kg |
| Max Landing Weight | |
| Max Ramp Weight | |
| Useful Load | |
| Seats | Single |
| Crew | |
| Power Loading | |
| Thrust to Weight | |
| Cockpit Length | |
| Cockpit Width | |
| Cockpit Height | |
| Load Limit Negative | |
| Load Limit Positive | |
| Fuel Capacity | 2300 kg |
| Oil Capacity |
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