Specifications | |||
Performance | |||
Maximum Range [size=-1](Mach 0.80, 8 passengers, 4 crew, NBAA IFR reserves) | 6,500 nm | 12,046 km | |
Long Range Cruise Speed | Mach 0.80, 459 ktas, 851 km/h | ||
Mmo [size=-1](Maximum Allowable Mach Number) | Mach 0.885 | ||
Takeoff Distance [size=-1](SL, ISA, MTOW) | 5,990 ft | 1,826 m | |
Landing Distance [size=-1](SL, ISA, MLW) | 3,170 ft | 966 m | |
Initial Cruise Altitude | 41,000 ft | 12,497 m | |
Maximum Cruise Altitude | 51,000 ft | 15,545 m | |
Weights | |||
Maximum Takeoff Weight | 90,500 lb | 41,051 kg | |
Maximum Landing Weight | 75,300 lb | 34,156 kg | |
Maximum Zero Fuel Weight | 54,500 lb | 24,721 kg | |
Basic Operating Weight [size=-1](including 4 crew) | 48,000 lb | 21,773 kg | |
Maximum Payload | 6,500 lb | 2,948 kg | |
Payload with Maximum Fuel | 1,600 lb | 726 kg | |
Maximum Fuel Weight | 41,300 lb | 18,734 kg | |
Allowance for outfitting and operating items | 8,500 lb | 3,856 kg | |
Design Standards | |||
Engines (2) | BMW Rolls-Royce BR710 | ||
Rated Takeoff Thrust ea. | 14,750 lb | 65.6 kN | |
Passengers (Maximum) | 19 | ||
Passengers (Typical Outfitting) | 13-15 | ||
Cabin Pressure Differential | 10.17 psid, 6,000 ft cabin at 51,000 ft | ||
Interior | |||
Cabin Length | 50 ft 1 in | 15.3 m | |
Cabin Height | 6 ft 2 in | 1.9 m | |
Cabin Width | 7 ft 4 in | 2.2 m | |
Cabin Volume | 1,669 cu ft | 47.3 cu m | |
Baggage Compartment Volume | 226 cu ft | 6.4 cu m | |
Exterior | |||
Length | 96 ft 5 in | 29.4 m | |
Height | 25 ft 10 in | 7.9 m | |
Wingspan | 93 ft 6 in | 28.5 m |
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