Flat Wing Area
21.5321 m²
Flat Wing Aspect Ratio
5.01
Cruise Speed
774.0945 km/h
Entry Into service
1966-11-09
Maximum Take-Off Weight
6.1235 t (paragliders: kg)
Total Fuel Capacity
3179.746
Maximum Range
2727.838 km
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Learjet 24 |
6.1235 |
3179.746 |
2727.838 |
Similar airplanes
All data (29 fields)
- Name
- Learjet 24
- Manufacturer
- Learjet
- Description
- The Learjet 24 is an American six-to-eight-seat (two crew and four to six passengers) twin-engine, high-speed business jet, which was manufactured by Learjet as the successor to the Learjet 23.
- ICAO Code
- LJ24
- First Flight
- 1966-01-24
- Entry Into service
- 1966-11-09
- Production End
- 1977-01-01
- Designer
- Learjet
- Type
- Business jet
- Length (m)
- 13.1064
- Height (m)
- 3.6576
- Max Seating
- 6
- Max Speed (km/h)
- 877.0925
- Cruise Speed (km/h)
- 774.0945
- Min Speed (km/h)
- 160.9344
- Max Ceiling (m)
- 13716
- Rate of Climb (m/s)
- 34.544
- Capacity Description
- 6 passengers
- National Origin
- Azerbaijan
- Number Built
- 259
- Powerplant Description
- 2 × General Electric CJ610-6 turbojets
- Status
- Active
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Learjet_24
- Flat Wing Span (m)
- 10.668
- Flat Wing Area (m²)
- 21.5321
- Flat Wing Aspect Ratio
- 5.01
- Wake Category
- L
- Aircraft Engine
- General Electric CJ610
- Number of Engines
- 2