Learjet Learjet 24
Corporate Jet
The Learjet 24 is a light 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 24 is a development of the
Learjet 23.
| Propulsion | 2 Turbojet Engines |
| Engine Model | General Electric CJ610-8A |
| Engine Power (each) | 13,1 kN | 2950 lbf |
| Speed | 880 km/h | 475 kts
547 mph |
| Service Ceiling | 13.716 m | 45.000 ft |
| Range | 2.732 km | 1.475 NM
1.697 mi. |
| Empty Weight | 3.204 kg | 7.064 lbs |
| max. Takeoff Weight | 6.124 kg | 13.500 lbs |
| Wing Span | 10,85 m | 35 ft 7 in |
| Wing Area | 21,5 m² | 231 ft² |
| Length | 13,18 m | 43 ft 3 in |
| Height | 3,73 m | 12 ft 3 in |
| First Flight | 24.02.1966 |
| Production Status | out of production |
| Total Production | 258 |
| ICAO Code | LJ24 |
| FAA TCDS | A10CE |
| Data for (Version) | Learjet 24F |
| Variants | Learjet 24A, Learjet 24B, Learjet 24D |
