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| Specification
& Weight
Reaching speeds of up to 474 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.
|
 |
Maximum Cruise Speed
(mid-cruise weight) |
412 ktas (763 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 29,300 ft (8,931 m) 275 kcas (510 km/hr)
MMO at 29,300 ft (8,931 m) and above M 0.734 (Indicated)
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Rates of Climb |
All engines 3,870 fpm (1,180 m/min)
Single engine 1,123 fpm (342 m/min)
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Stall Speed |
91 kcas (169 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) |
1,580 nm (2,926 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) 3,420 ft (1,042 m)
Landing distance (SL, ISA, MLW) 3,050 ft (930 m)
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Engines |
Two Williams FJ44-3A-24
Takeoff thrust 2,400 lb (10.68 kN)
Bypass ratio 2.2:1
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Baggage Capacity |
Volume 70.4 ft3 (1.99 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)
|
 Design Weights
& Fuel Capacity
| 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* |
7,695 lb (3,490 kg) |
| One pilot plus furnishings |
200 lb (91 kg) |
| Typical basic operating weight (BOW) |
7,895 lb (3,581 kg) |
| Useful load** |
4,730 lb (2,145 kg) |
| Payload with full fuel |
800 lb (363 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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