Learjet 28
From Wikipedia, the free encyclopedia
Learjet 28 | |
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Type | Business jet |
Manufacturer | Learjet |
Maiden flight | August 24, 1977 |
Primary users | Private Military NASA |
The Learjet 28 is an eight to ten seat (two crew and six to eight passengers), twin-engined, high speed business jet. Manufactured by Learjet as the successor to the Learjet 25.
Contents |
[edit] History
The first flight of a Learjet 28 took place on 24 August 1977.
The Learjet 28 was based on the LJ25, and received a completely new wing fitted with winglets. The Learjet 29 is constructed identically, however is intended for a higher range. However, due to high engine noise and fuel consumption, the model did not achieve commercial success.
Only five production aircraft of the Learjet 28 model were built before it was replaced then by the further developed Learjet 35. In the year 1998 were from the Learjet 28 still all 5 machines in use.
[edit] Specifications
technical data Span: 13.35 m Length: 14.50 m Height: 3.73 m Max one. Takeoff weight: 6805 kg Maximum speed: 883 km/h Optimal cruising speed: 756 km/h Service ceiling: 15545 m Range: 2660 km Passengers: maximally 10 Engines 2x General Electric CJ-610-8A to ever 13.1 kN
[edit] References
[edit] External link
[edit] Related content
Designation sequence
LJ23 - LJ24 - LJ25 - LJ28 - LJ29
Related lists
Learjet 23 • Learjet 24 • Learjet 25 • Learjet 28 • Learjet 29 • Learjet 31 • Learjet 35 • Learjet 36 • Learjet 40 • Learjet 45 • Learjet 55 • Learjet 60 • Learjet C-21