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| Specification
& Weight
This impressive business jet offers exactly the same cabin height
and width as Cessna's flagship Citation X. The constant cross-section
cabin provides passengers with a continuous width of 67 inches.
Further contributing to passenger comfort is the huge external
baggage compartment. There's a total volume of 80 cubic feet and
a weight capacity of 700 pounds - nearly twice that of most light
jets.
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Maximum Cruise Speed |
433 ktas (802 km/hr), 35,000 ft (10,668 m), mid-cruise weight
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NBAA IFR Range (100nm alternate) |
1,939 nautical miles (3,593 km) (full fuel, maximum takeoff weight)
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Airport Performance |
Takeoff distance (SL, ISA, MTOW) 3,560 ft (1,085 m) Landing distance (SL, ISA, MLW) 3,180 ft (969 m)
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Ceiling |
Maximum certified 45,000 ft (13,716 m) Single engine 28,600 ft (8717 m)
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Rates of climb |
All engine 3,500 ft/min (1,063 m/min) Single engine 800 ft/min (244 m/min)
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Airspeed Limits |
VMO from 8,000 ft (2,438 m) to 26,515 ft (8,082 m) 305 ktas (565 km/hr) MMO at 26,515 ft (8,082 m) and above M 0.75 (indicated)
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Stall Speed |
90 ktas (167 km/hr) MLW
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Pressurization |
Nominal pressure differential is 9.3 psi (64 kP)
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Outside dimensions |
Overall length 51 ft 10 in (15.79 m) Overall height 17 ft 5 in (5.30 m) Wingspan 55 ft 8 in (16.98 m)
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Cabin Dimensions (with typical interior installed) |
Length (forward bulkhead to aft bulkhead) 24 ft (7.3 m)
Width 67 in (1.70 m)
Height 68 in (1.73 m)
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Engines |
Two Pratt & Whitney PW545B Takeoff thrust 3,991 lb (17.75 kN) Bypass ratio 3.8:1
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Design Weights & Fuel Capacity
| Maximum ramp weight |
20,400 lb (9,253 kg) |
| Maximum takeoff weight |
20,200 lb (9,163 kg) |
| Maximum landing weight |
18,700 lb (8,482 kg) |
| Maximum zero fuel weight |
15,100 lb (6,849 kg |
| Maximum fuel capacity @ 6.7 lbs/gal |
6,740 lb (3,057 kg) |
| Typical empty weight* |
12,400 lb (5,625 kg) |
| Two crew plus furnishings |
400 lb (181 kg) |
| Typical basic operating weight (BOW) |
12,800 lb (5,806 kg) |
| Useful load** |
7,600 lb (3,447 kg) |
| Payload with full fuel |
860 lb (381 kg) |
*Reflects standard aircraft with typical options, typical interior
and unusable fuel and oil.
** Amount of payload and fuel that can be carried, over and above crew
(based on ramp weight).
Note: Performance conditions are based on the International Standard
Atmosphere. Takeoff and landing field lengths are based on level, hard-surface,
dry runways with no wind.
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