Bombardier Learjet 25D
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Aircraft Data
The Learjet is a light business jet developed from the designs of Bill Lear, it entered production in 1963 and has become the worlds best selling range of corporate aircraft.The short to medium range Learjet 25 had a slight fuselage stretch (4ft 2in) over the -24, this enabled it to carry up to 8 passengers. The 25 series was then developed through a range of progressive improvements, including the B,D, F and G.
| Country of origin | First flight | No. built | No. in service | Crew | Passengers |
|---|---|---|---|---|---|
| USA | 1966 | 373 | 250 | 2 | 4 - 8 |
Power
2 x General Electric J85/CJ610 (2450 - 2950 lbf) turbojet engines.
Uses the CJ610-6 or -8
Dimensions
| Length | 47 ft. 7 in. |
|---|---|
| Wing Span | 35 ft. 7 in. |
| Height | 12 ft. 7 in. |
| Empty Weight | 8,220 lbs. |
| Max Weight | 15,500 lbs. |
Performance
| Max Speed | 473 kts |
|---|---|
| Cruise Speed | 450 kts |
| Ceiling | 45,000 ft. |
| Normal Range | 1,250nm |
| Max Range | 1,540nm (7 Passengers, with reserves.) |
Updated 7th December 2008
Show using: Metric | Imperial
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