Learjet Learjet 25
Corporate Jet
The Learjet 25 is a twin-engined corporate jet aircraft produced by the US-American manufacturer Lear Jet Industries Inc. (later Gates Learjet Corporation, today Bombardier Aerospace, Canada).
The Learjet 25 is a stretched development of the
Learjet 24.
| Propulsion | 2 Turbojet Engines |
| Engine Model | General Electric CJ610-8A |
| Engine Power (each) | 13,1 kN | 2950 lbf |
| Speed | 878 km/h | 474 kts
545 mph |
| Service Ceiling | 13.716 m | 45.000 ft |
| Range | 2.663 km | 1.438 NM
1.655 mi. |
| Empty Weight | 3.465 kg | 7.639 lbs |
| max. Takeoff Weight | 6.805 kg | 15.000 lbs |
| Wing Span | 10,84 m | 35 ft 7 in |
| Wing Area | 21,5 m² | 231 ft² |
| Length | 14,50 m | 47 ft 7 in |
| Height | 3,73 m | 12 ft 3 in |
| First Flight | 12.08.1966 |
| Production Status | out of production |
| Total Production | 373 |
| Developed from | Learjet 24 |
| ICAO Code | LJ25 |
| FAA TCDS | A10CE |
| Data for (Version) | Learjet 25D |
| Variants | Learjet 25A, Learjet 25B, Learjet 25C, Learjet 25D |
