Learjet 85
| Learjet 85 | |
|---|---|
| 300px | |
| Bombardier Learjet 85 Flight Test Vehicle 1 | |
| Role | Business jet |
| Manufacturer | Bombardier |
| First flight | 9 April 2014 |
| Status | Cancelled |
| Number built | 2[citation needed] |
The Learjet 85 was a Learjet development program by aircraft manufacturer Bombardier Aerospace.
The program was launched on October 30, 2007 and a mockup of the aircraft was unveiled in October 2008 at the NBAA show in Orlando. The Learjet 85 was to fit between the midsize and the super midsize segments of the market. Designed for type certification under FAR-25, it was the first Bombardier Aerospace business jet to feature a composite structure. The plane was intended to have a high-speed cruise of Mach 0.82 and a transcontinental range of up to Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value)..
On January 15, 2015, Bombardier announced their decision to suspend the Learjet 85 program and cut 1000 associated jobs.[1][2][3]
On October 29, 2015, Bombardier chief executive Alain Bellemare announced a 2015 $4.9 billion third quarter loss, including the cancellation of the Learjet 85 program.[4]
Design and development
Computer software design tools were used on the project, including CATIA and HyperSizer, and similar wing technology employed as on the Bombardier CSeries.[5]
Bombardier reported nearly 60 Learjet 85 orders at a price of US$17.2 million (2008 dollars). Flexjet announced it would be the initial launch customer with seven orders in 2011.[6][7]
On October 21, 2010, Bombardier opened a Learjet 85 aircraft component manufacturing facility in Querétaro, Mexico. The plant was inaugurated by President Felipe Calderón.[8] Some parts of the wing will be manufactured in Belfast in Northern Ireland.[9]
The first test flight was on 9 April 2014.[10]
The development was "paused" in January 2015 as the aircraft was consuming too much money and orders were lacking. The company suspended the Learjet 85 to concentrate on the CSeries and Global 7000/8000 instead. On October 29, 2015 the project was cancelled.[3][4]
Specifications (Learjet 85)
Data from Bombardier
General characteristics
- Crew: 2
- Capacity: 8
- Length: 20.76 m (68 ft 1 in)
- Wingspan: 18.75 m (61 ft 6 in)
- Height: 6.08 m (19 ft 11 in)
- Wing area: 37.25 m2 (401.0 sq ft)
- Empty weight: 10,977 kg (24,200 lb)
- Max takeoff weight: Lua error in Module:Convert at line 272: attempt to index local 'cat' (a nil value).
- Powerplant: 2 × Pratt & Whitney PW307B Turbine
Performance
- Maximum speed: 871 km/h; 470 kn (541 mph)
- Cruise speed: 829 km/h; 448 kn (515 mph)
- Range: 4,828 km; 2,607 nmi (3,000 mi)
- Service ceiling: 14,935 m (49,000 ft)
Avionics
Rockwell Collins Pro Line Fusion avionics suite
References
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External links
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