| Attribute | Value |
| General |
| Manufacturer | Lockheed Martin Aeronautics |
| Model | Lockheed P-38 Lightning |
| Country | United States |
| Manufactured from | 1941 year |
| Manufactured to | 1945 year |
| Type | Military Propellor Planes |
| Icao | P38 |
| Performance |
| Engine | 2x Allison V-1710-111/113 |
| Power, hp | 1,600 hp |
| Power, lbf | Add |
| Avionics | Add |
| Max cruise speed | 667 km/h |
| Approach speed | 169 km/h |
| Travel range | 3,695 km |
| Fuel economy | Add |
| Service ceiling | 13,411 m |
| Rate of climb | 24.13 m/sec |
| Take off distance | 670 m |
| Landing distance | 700 m |
| Weights |
| Max take off weight | 9,798 kg |
| Max landing weight | 7,938 kg |
| Max payload | 1,800 kg |
| Fuel tank capacity | 4,399 l |
| Baggage volume | Add |
| Dimensions |
| Seats | 1 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | Add |
| Exterior length | 11.53 m |
| Tail height | 3.9 m |
| Fuselage diameter | 1 m |
| Wing span | 15.85 m |
| Wing tips | No Winglets |