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庞巴迪挑战者605公务机介绍 Bombardier Challenger 605

时间:2011-11-11 15:25来源:蓝天飞行翻译 作者:航空 点击:


(From cockpit divider to end
of pressurized compartment)
 
Weights 重量
A. Maximum ramp weight: 48,300 lb   21,909 kg 
B. Maximum takeoff weight: 48,200 lb   21,863 kg 
C. Maximum landing weight: 38,000 lb   17,237 kg 
D. Maximum zero fuel weight: 32,000 lb   14,515 kg 
E. Typical basic operating weight: 27,150 lb   12,315 kg 
F. Maximum fuel weight: 20,000 lb   9,072 kg 
Payload – full fuel (A-E-F): 1,150 lb   522 kg 
Maximum payload (D-E): 4,850 lb   2,200 kg 
Fuel with maximum payload (A-D): 16,300 lb   7,394 kg  
 
航程
Range
Maximum range 4,000 NM 4,603 SM 
 7,408 km 
(Theoretical range at M 0.74 with 6 passengers/2 crew, NBAA IFR reserves, ISA, typical BOW and maximum allowable fuel. Actual range will be affected by speed, weather, selected options and other factors)
 
Speed Mach kt mph km/h 
High-speed cruise 0.82 470 541 870 
Typical cruise speed 0.80 459 528 850 
Long-range cruise speed 0.74 425 489 787 
 
Airfield Performance 跑道性能
Takeoff distance: 5,840 ft   1,780 m 
(SL, ISA, MTOW)
 
Landing distance 着陆距离
(SL, ISA, MLW): 2,775 ft   846 m 
 
Operating Altitude 飞行高度
Maximum operating altitude: 41,000 ft   12,497 m 
Initial cruise altitude: 37,000ft      
(11,278 m)
 
Noise Level Flyover Approach 
 Lateral 
EPNdB 81.2 90.3 
 86.2 
 
 
Engines 发动机
General Electric CF34-3B turbofans
Thrust: 8,729 pounds (38.84 kN) thrust at takeoff
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