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Manufacturer: Cessna (image for representation only)
Model: Citation CJ2+
Specifications & Descriptions/Performance
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.
SEATING CAPACITY:08 Max
Specifications & Weights
MaximumCruise Speed
(mid-cruise weight)
Ceiling
AirspeedLimits
Ratesof Climb
StallSpeed
Pressurization
NBAAIFR Range
(100 nm alternate)
AirportPerformance
(dry, level, hard-surfaced runway with zero wind)
Engines
BaggageCapacity
OutsideDimensions
CabinDimensions
(with typical interior installed)
418ktas (774 km/hr), at 31,000 ft (9,449 m)
45,000ft (13,716 m) maximum certified
VMOat 8,000 ft (2,438 m) to 29,123 ft (8,877 m) 278 KIAS (515km/hr)
MMO at 29,123 ft (8,877 m) and above M 0.737(Indicated)
Allengines 4,120 fpm (1,256 m/min)
Single engine 1,123 fpm (342m/min)
86kcas (159 km/hr) MLW, landing configuration
Nominalpressure differential 8.9 psi (61 kP)
1,613nm (2,987 km) with full fuel and maximum takeoff weight
Takeoffdistance (SL, ISA, MTOW) 3,360 ft (1,024 m)
Landing distance(SL, ISA, MLW) 2,980 ft (908 m)
TwoWilliams FJ44-3A-24
Takeoff thrust 2,490 lb (11.08 kN)
Bypassratio 2.2:1
Volume65 ft3 (1.84 m3)
Wingspan49 ft 10 in (15.19 m)
Overall height 14 ft 0 in (4.27m)
Overall length 47 ft 8 in (14.53 m)
Height57 in (1.45 m)
Width 58 in (1.47 m)
Length (excludingcockpit) 163 in (4.14 m)
Design Weights & Fuel Capacity
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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