|
|
 |
|
 |
 |
|
|
Gates Learjet - Learjet 24F, LR-24F
| Category: Jet < 20,000 lbs. |
| Years Aircraft Manufactured: 1976 - 1979 |
|
Printer friendy version
|
|
|
|
|
|
 |
| The Learjet family began with the original six to eight seat Lear Jet 23 which first flew on October 7 1963. The aerodynamics and many other characteristics of the 23 were taken over from the P-16 Fighter. Although it was originally planned to manufacture at least the first 25 Lear Jets in Switzerland, production was transferred to the United States, where Lear had founded Lear Jet Corporation. The diminutive Model 23 pioneered an entirely new market segment for the light business jets, and proved very successful. The first production 23 was delivered in October 1964, but was replaced by the improved Model 24 in 1966 after 104 had been built. The 24, which introduced uprated engines and a number of detail changes, first flew in February 1966 and was delivered from the middle of that year. Developments of the 24 included the 24D, E and F, introducing improvements such as increased weights, thrusts, and range. The Learjet 25 introduced a 1.27m (4ft 2in) fuselage stretch allowing seating for up to eight passengers and was first flown on August 12 1966, and, like the 24, a number of subsequent developments were built, including the B, D, F and G. |
|
|
|
|
| Seating (normal) |
6 |
Max Takeoff (lbs) |
13,500 |
| Seating (maximum) |
- |
Certified Ceiling (ft) |
- |
|
| Engines |
2 GE CJ610-8A |
To (Sealevel, ISA Temp) (ft) |
3,297 |
| Output lbs ea. Flat Rating |
2,950 |
Landing Distance (ft) |
- |
| Maximum Mach No. |
0.82 |
Max Range (fuel) (nm) |
1,321 |
| High Speed Cruise (Kts) |
451 |
Max Range (payload) (nm) |
631 |
|
| Flight Time 300nm |
0 + 59 |
Flight Time 1000nm |
2 + 45 |
| Flight Time 600nm |
1 + 40 |
|
|
|
| External |
|
Internal |
|
| Length (ft) |
43.30 |
Length (ft) |
9.00 |
| Height (ft) |
12.30 |
Height (ft) |
4.30 |
| Span (ft) |
35.60 |
Width: Max floor (ft) |
4.90 |
|
|
|
 |
|
 |
|
|
|
