PASSENGER AIRCRAFT
BOMBARDIER LEARJET 60 60XR
Aircraft Summary
The Bombardier Learjet 60 60XR is a mid-size cabin, medium-range business jet aircraft manufactured by Bombardier Aerospace in the United States. Bombardier launched a new variant in 2005 designated the Learjet 60XR and following certification, deliveries started in 2007. The Learjet 60XR has an upgraded cabin, Rockwell Collins Pro Line 21 advanced avionics suite and three-disc steel wheel brakes. The Bombardier Learjet 60 (60XR) is capable of transporting up to 7 passengers.
History and Features
The Learjet 60 is an improved version of the Learjet 55, with a longer fuselage and more powerful turbofan engines. It first flew on 10 October 1990 and received FAA certification in January 1993.
The modifications that converted the Learjet Model 55 into a Model 60 resulted from an aerodynamics improvement program and a need to increase the capacity of the Learjet product line. Several of these modifications were a first for Learjet, including an all-new inboard wing cuff added to the inboard sections of the “Longhorn” wing and an all-new wing-to-body fairing. By increasing the wing chord and the leading edge droop, the wing cuff improved handling during approach and landing, while the wing-to-body fairing reduced the interference drag between the wing and the fuselage. Since the engines were new for this aircraft, a new engine pylon had to be designed.
The lines of the cockpit have not changed but the fuselage was lengthened. In addition, the blend between the fuselage and the empennage was all new. While it appears as if area ruling was the intention of the blending, the blend design was really driven by attaching the original Learjet Model 35 empennage onto the larger Learjet Model 60 fuselage.
The final aerodynamic improvements to the Model 60 included the creation of the distinctive “ogive” winglet trailing edge. This lengthening of the chord near the interface of the winglet and the wing improved the interaction of the wing’s pressure spike with the winglet’s pressure spike. The result was a significant lowering of the drag in this area and a significant improvement of the wing’s efficiency. On the prior “Longhorn” wing the interference between the winglet and the wing nearly canceled the effects of the winglet. The single ventral fin was also replaced with two ventral fins that Learjet called “Delta Fins” to improve stall characteristics and promote aerodynamic stability.
Production of the Learjet 60 ended in 2007 after 318 aircraft had been built. The Learjet 60XR was a variation with upgraded Proline 21 avionics and slight improvements to the cabin, with production from beginning at serial number 319.
Bombardier launched a new variant in 2005 designated the Learjet 60XR and following certification deliveries started in 2007.
Grandfathered on the 1966 Learjet 24 type certificate, it was built until 2013. Cabin space is better utilized with five floor plans, LED lighting, better insulation and improved cabin management system.
The 60XR has the largest Learjet cabin, its cross-section is competitive but its length is 2 to 5 ft (0.61 to 1.52 m) shorter than other mid-size jets like the Hawker 800XP. The small 265 sq ft (24.6 m2) wing evolved from the Learjet 23, with the tip tanks replaced by winglets, and runway requirements are long for the 23,500 lb (10,700 kg) aircraft.
In September 2018, there were 112 Model 60XRs in service.
Aircraft of similar role, configuration and era are: Cessna Citation VII, Gulfstream G150, Hawker 800XP.
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OVERVIEW
PASSENGERS*
7
CRUISE SPEED
778 kph / 483 mph
SPECIFICATIONS
CABIN LENGTH
5.1 m / 16’8″
CABIN WIDTH
1.8 m / 5’10”
CABIN HEIGHT
1.74 m / 5’8″
LUGGAGE SPACE
1.65 m / 5’4″
ENCLOSED LAVATORY
Yes
ENTERTAINMENT CENTRE
Yes
COMPARABLE AIRCRAFT
Aircraft of comparable role, configuration and era