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The Learjet 40 (LJ40) is a light business jet produced by Bombardier Aerospace.
| Learjet 40 | |
|---|---|
 | |
| Role | Business jet |
| Manufacturer | Bombardier Aerospace |
| First flight | August 31, 2002 |
| Introduction | January 2004 |
| Produced | 2002–2013 |
| Developed from | Learjet 45 |
| Developed into | Learjet 70/75 |
Design and development
The Learjet 40 is derived from the Learjet 45, but with a shorter fuselage (by 24.5 inches/60 cm), and is powered by two Honeywell TFE731-20AR engines. These are known as the "AR" engines. The 40 model takes the place of the discontinued Learjet 31a in the Learjet model line, with several performance and comfort improvements taken from the 45 model.
The prototype aircraft, a rebuilt Model 45, first flew on August 31, 2002, and the first production aircraft performed its maiden flight on September 5, 2002. Both flights took place from the Wichita Mid-Continent Airport. The LJ40 entered into service in January, 2004.[1]
The Learjet 40XR is an upgraded version introduced in October, 2004, offering higher takeoff weights, faster cruise speeds and faster time-to-climb rates as compared to the LJ40. The increases are due to the upgrading of the engines to the TFE731-20BR configuration. These are the "BR" engines. LJ40 owners can upgrade their aircraft through the incorporation of several service bulletins.[2]
By 2018, Learjet 40XRs start at $2 million.[3]
Specifications (Learjet 40)
Data from Jane's All the World's Aircraft 2004–2005[4]
General characteristics
- Crew: 2
- Capacity: 7 passengers
- Length: 55 ft 6 in (16.92 m)
- Wingspan: 47 ft 9+1⁄4 in (14.561 m)
- Height: 14 ft 4+1⁄2 in (4.382 m)
- Wing area: 311.6 sq ft (28.95 m2)
- Aspect ratio: 7.3:1
- Empty weight: 12,740 lb (5,779 kg)
- Max takeoff weight: 20,350 lb (9,231 kg)
- Fuel capacity: 905 US gal (754 imp gal; 3,430 L)
- Powerplant: 2 × Honeywell TFE731-20AR turbofan engines, 3,500 lbf (16 kN) thrust each
Performance
- Maximum speed: Mach 0.81 (MMO)
- Cruise speed: 464 kn (534 mph, 859 km/h) (max cruise)
- Range: 1,857 nmi (2,137 mi, 3,439 km) (2 crew and 4 passengers)
- Service ceiling: 51,000 ft (16,000 m)
- Time to altitude: 22 minutes to Flight level 430
See also
Related lists
- List of civil aircraft
References
- Specifications from Flug-Revue Archived 2006-12-09 at the Wayback Machine
- "Bombardier Aerospace Launches Learjet 40XR High Performance Light Jet." from Wings over Kansas Archived 2006-11-14 at the Wayback Machine
- Mark Huber (December 2018). "For many models, market hitting the apex" (PDF). Aviation International News. pp. 20–21, 24.
- Jackson 2004, pp. 690, 692
- Jackson, Paul, ed. (2004). Jane's All the World's Aircraft 2004–2005. Coulsdon, UK: Jane's Information Group. ISBN 0-7106-2614-2.
External links
На других языках
[de] Learjet 40
Der Bombardier Learjet 40 ist ein zweistrahliges Geschäftsreiseflugzeug in Tiefdeckerauslegung der kanadischen Firma Bombardier.- [en] Learjet 40
[fr] Learjet 40
Le Learjet 40 (LJ40) est un avion d'affaire léger produit par Bombardier Aerospace.[it] Learjet 40
Il Learjet 40 è un business jet statunitense bigetto prodotto dalla Learjet.[ru] Learjet 40
Learjet 40 (LJ40) — реактивный административный (бизнес-джет) самолёт производства компании Bombardier Aerospace, созданный на базе Learjet 45. Именуется также как Bombardier Learjet 40.Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.
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