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Reaching speeds of up to 481 mph, the CJ2+ is 40 percent faster than a comparably priced B200 turboprop. You can also climb to 45,000 feet and cruise above turbulent weather, icing and traffic.
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Specifications
& Weights
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ENGLISH
(METRIC)
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Maximum Cruise Speed
(mid-cruise weight) |
418 ktas (774 km/hr), at 31,000 ft (9,449 m)
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Ceiling |
45,000 ft (13,716 m) maximum certified
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Airspeed Limits |
VMO at 8,000 ft (2,438 m) to 29,123 ft (8,877 m) 278 KIAS (515 km/hr)
MMO at 29,123 ft (8,877 m) and above M 0.737 (Indicated)
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Rates of Climb |
All engines 4,120 fpm (1,256 m/min)
Single engine 1,004 fpm (306 m/min)
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Stall Speed |
86 kcas (159 km/hr) MLW, landing configuration
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Pressurization |
Nominal pressure differential 8.9 psi (61 kP)
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NBAA IFR Range
(100 nm alternate) |
1,613 nm (2,989 km) with full fuel and maximum takeoff weight
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Airport Performance
(dry, level, hard-surfaced runway with zero wind) |
Takeoff distance (SL, ISA, MTOW) 3,360 ft (1,024 m)
Landing distance (SL, ISA, MLW) 2,980 ft (908 m)
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Engines |
Two Williams FJ44-3A-24
Takeoff thrust 2,490 lb (11.08 kN)
Bypass ratio 2.2:1
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Baggage Capacity |
Volume 65 ft3 (1.84 m3)
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Outside Dimensions |
Wingspan 49 ft 10 in (15.19 m)
Overall height 14 ft 0 in (4.27 m)
Overall length 47 ft 8 in (14.53 m)
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Cabin Dimensions
(with typical interior installed) |
Height 57 in (1.45 m)
Width 58 in (1.47 m)
Length (excluding cockpit) 163 in (4.14 m)
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Design
Weights & Fuel Capacity
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ENGLISH
(METRIC)
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TOP
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| Maximum ramp weight |
12,625 lb (5,726 kg) |
| Maximum takeoff weight |
12,500 lb (5,669 kg) |
| Maximum landing weight |
11,525 lb (5,227 kg) |
| Maximum zero fuel weight |
9,700 lb (4,399 kg) |
| Maximum fuel capacity (6.7 lb/gal) |
3,930 lb (1,783 kg) |
| Typical empty weight* |
7,725 lb (3,504 kg) |
| One pilot plus furnishings |
200 lb (91 kg) |
| Typical basic operating weight (BOW) |
7,925 lb (3,595 kg) |
| Useful load** |
4,700 lb (2,132 kg) |
| Payload with full fuel |
770 lb (349 kg) |
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.
*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). |
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08/08/2006 |
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