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| The Learjet 60 was announced in October 1990 as the replacement for the mid-size Model 55C, from which it is derived, and a proof of concept airframe flew for the first time on 18 October 1990 powered by one Garrett TFE331-3A and one PW305 engine. The first twin-PW305-powered Learjet 60 made its first flight from Mid-Continent Airport, Wichita, on 13 June 1991, and certification and early deliveries are tar-getted for the end of 1992. The Model 60 is the largest of the Learjet family and incorporates new fuel-efficient engines, a fuselage 0.07m wider and stretched by 1.43m, a 'glass cockpit', 'steer by wire' nosewheel, and an optional higher MTOW of 10478kg. Thrust reversers and single-point refuelling are also standard equipment, and the aircraft features a full galley, together with an aft toilet. By mid-1991, Learjet claimed to have sold the first full year's production to customers in seven countries.
| ENGINE | 2 x Pratt & Whitney Canada PW305 turbofans, 1995kg |
| WEIGHTS |
| Take-off weight | 10319 kg | 22750 lb |
| DIMENSIONS |
| Wingspan | 13.34 m | 44 ft 9 in |
| Length | 17.88 m | 59 ft 8 in |
| Height | 4.47 m | 15 ft 8 in |
| Wing area | 24.57 m2 | 264.47 sq ft |
| PERFORMANCE |
| Max. speed | 858 km/h | 533 mph |
| Ceiling | 15545 m | 51000 ft |
| Range | 4441 km | 2760 miles |
| mark, e-mail, 18.12.2009 10:10 can i get more specifications of this model reply | | mark, e-mail, 18.12.2009 10:09 this is very cute reply |
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