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Bombardier Challenger 605 Technical specifications



Year of manufacture: 2010

Seating capacity: 12 PAX



PERFORMANCE



Two General Electric CF34-3B engines power the Challenger 605 each offering 8,729 pounds of thrust and using 258 gallons per hour (GPH). The range of the Challenger 605 is 4,047 NM operating under NBAA IFR 4 passengers with available fuel.



INTERIOR

The cabin volume for the Challenger 605 is 1,150 cubic feet. Typical configuration features 11 passenger and 2 crew seats.



SPEED

Maximum Cruise Speed:470, kts870 km/h

Long-range Speed:424 kts785 km/h



AIRFIELD PERFORMANCE

Takeoff distance:5,840 ft (1,780 m)(SL, ISA, MTOW)

Landing distance:2,360 ft (719 m)(SL, ISA, MLW)



OPERATING ALTITUDE

Maximum operating altitude: 41,000 ft (12,500 m)



NOISE LEVEL (EPNDB)



Takeoff: 81.2m.

Flyover: 90.3m.

Approach: 86.2m.



WEIGHTS

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.Standard basic operating weight:27,150 lb (12,315 kg)



Embraer Legacy 650

Technical specifications



Year of manufacture: 2012

Seating capacity: 13



PERFORMANCE



Two Rolls-Royce AE3007A2 engines power the Legacy 650, each offering 9,020 pounds of thrust and using 362 gallons per hour (GPH). The range of the Legacy 650 is 3,919 NM operating under NBAA IFR 4 passengers with available fuel.



INTERIOR

The cabin volume for the Legacy 650 is 1,656 cubic feet. Typical configuration features 13 passenger and 2 crew seats.



SPEED

Maximum Cruise Speed: 459, kts850 km/h

Long-range Speed: 425 kts 787 km/h



AIRFIELD PERFORMANCE

Takeoff distance: 5,741 ft (1,750 m) (SL, ISA, MTOW)

Landing distance: 2,346 ft (715 m) (SL, ISA, MLW)



OPERATING ALTITUDE

Maximum operating altitude: 41,000 ft (12,500 m)



NOISE LEVEL (EPNDB)



Takeoff: 78m.

Flyover: 86.9 m.

Approach: 91.7m.



WEIGHTS

A. Maximum ramp weight: 53,727 lb (24,371 kg)

B. Maximum takeoff weight: 53,572 lb (24,300 kg)

C. Maximum landing weight: 44,092 lb (20,000 kg)

D. Maximum zero fuel weight: 36,156 lb (16,400 kg)

E. Standard basic operating weight: 31,217 lb (14,160 kg)



Asking rate available upon request please complete below

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