The Learjet 35 is stretched, turbofan powered developments of the initial Learjet models 23, 24 and 25.
Learjet 35 prototype first flew on August 22 1973.
The Learjet 35 has seating for up to eight. The 35 were certificated in July 1974.
Improvements to the model led to the 35A from 1976, with higher standard max takeoff weights.
The Learjet 35 model remained in production until 1994. Learjet became a Bombardier subsidiary in 1990.
 
 
Country of Origin
United States of America
 
Powerplants
35 - Two 15.6kN (3.500lb) Garrett (now AlliedSignal) TFE731-2-2B turbofans.
 
Performances
35A Max speed 872km/h (470kt), max cruising speed 852km/h (460kt), economical cruising speed 774km/h (418kt). Service ceiling 41,000ft. Range with four passengers, max fuel and reserves 4.070km (2.195nm).
 
Weight
35A Empty equipped 4.590kg (10.120lb), max takeoff 8.300kg (18.300lb). 
 
Dimensions
35A Wing span (over tip tanks) 12.04m, length 14.83m, height 3.73m. Wing area 23.5mq. 
 
Capacity
Flight crew of two. Seating for up to eight in main cabin. Can be configured as an AIR AMBULANCE with one or two stretchers and two medical attendants.
 
Production
738 Learjet 35s were built, including 674 model 35s.
At late 2002 630 Learjet 35s, were in service.
 
Type
Light corporate jets.
 
   
   
   
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