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Cessna Citation Model Stats Cessna Citation Model Stats Cessna Citation Sovereign - Dimensions • Length • 63 ft 6 in (19.35 m) • Height • 20 ft 4 in (6.20 m) • Wingspan • 72 ft 4 in (22.04 m) Wing • Wing Area • 516 sq ft (48 sq m) • Wing Sweep • 16.3 degrees • 27 ft 10 in (8.49 m) Wheelbase • 10 ft (3.05 m) Tread Cabin Interior • Height • 68 in (1.73 m) • Width • 66 in (1.68 m) • Length • 25 ft 3 in (7.70 m) • Seating Capacity • 9 - 12 Baggage Capacity • Weight • 1,415 lb (642 kg) • Volume • 135 cu ft (3.82 cu m) • Single Pilot Certified • No Wingspan – 72 ft 4 in (22.04 m) Height 20 ft 4 in (6.20 m) Length – 63 ft 6 in (19.35 m) Weights • Maximum Ramp Weight • 31,025 lb (14,073 kg) • Maximum Takeoff Weight • 30,775 lb (13,959 kg) • Maximum Landing Weight • 27,575 lb (12,508 kg) • Maximum Zero Fuel Weight • 21,000 lb (9,525 kg) Usable Fuel Capacity • Weight • 11,390 lb (5,166 kg) • Volume • 1,700 gal (6,435 l) • Basic Operating Weight • 18,380 lb (8,337 kg) • Useful Load • 12,645 lb (5,736 kg) • Maximum Payload • 2,620 lb (1,188 kg) • Full Fuel Payload • 1,255 lb (569 kg) Performance • Maximum Cruise Speed • 458 ktas (848 km/h) • Range • 3,000 nm (5,556 km) • Takeoff Distance • 3,650 ft (1,113 m) • Landing Distance • 2,680 ft (817 m) • Maximum Operating Altitude • 47,000 ft (14,326 m) • Maximum Climb Rate • N/A fpm (N/A mpm) • Maximum Limit Speed • 0.800 Mach Powerplant Two Pratt & Whitney Canada PW306D turbofan engines are installed on the new Citation Sovereign. The engine is a twin-spool design with a damage resistant wide chord fan. Behind the fan, four axial and one centrifugal compressor stages lead to a high-efficiency, low-emission, through-flow combustor, and five turbine stages. Two-stage variable inlet guide vanes and bleed- off valves are controlled by the FADEC to optimize compressor performance and engine operability. • Manufacturer: Pratt & Whitney Canada • Model: (2) PW306D • Thrust: 5,852 lbf • Time Between Overhaul: 6,000 hr Citation Mustang - Detailed Specifications Performance data is based on the standard Mustang configuration, operating in International Standard Atmosphere (ISA) conditions with zero wind. Takeoff and landing field lengths are based on a level, hard surface and dry runway. Actual performance will vary with factors such as environmental conditions, aircraft configuration and operational/ATC procedures. Dimensions • Length • 40 ft 7 in (12.37 m) • Height • 13 ft 5 in (4.09 m) • Wingspan • 43 ft 2 in (13.16 m) Wing • Wing Area • 210 sq ft (20 sq m) • Wing Sweep • 11.0 degrees Wheelbase • 14 ft 4 in (4.37 m) Tread • 11 ft 10 in (3.61 m) Cabin Interior • Height • 54 in (1.37 m) • Width • 55 in (1.40 m) • Length • 9 ft 9 in (2.97 m) • Seating Capacity • 5 - 5 Baggage Capacity • Weight • 718 lb (326 kg) • Volume • 63 cu ft (1.78 cu m) • Single Pilot Certified • Yes Wingspan – 43 ft 2 in (13.16 m) Height 13 ft 5 in (4.09 m) Length – 40 ft 7 in (12.37 m) Weights • Maximum Ramp Weight • 8,730 lb (3,960 kg) • Maximum Takeoff Weight • 8,645 lb (3,921 kg) • Maximum Landing Weight • 8,000 lb (3,629 kg) • Maximum Zero Fuel Weight • 6,750 lb (3,062 kg) Usable Fuel Capacity • Weight • 2,580 lb (1,170 kg) • Volume • 385 gal (1,457 l) • Basic Operating Weight • 5,590 lb (2,536 kg) • Useful Load • 3,140 lb (1,424 kg) • Maximum Payload • 1,160 lb (526 kg) • Full Fuel Payload • 560 lb (254 kg) Performance • Maximum Cruise Speed • 340 ktas (630 km/h) • Range • 1,150 nm (2,130 km) • Takeoff Distance • 3,110 ft (948 m) • Landing Distance • 2,380 ft (725 m) • Maximum Operating Altitude • 41,000 ft (12,497 m) • Maximum Climb Rate • 3,010 fpm (917 mpm) • Maximum Limit Speed • 0.630 Mach Powerplant Two dual-channel FADEC-controlled, Pratt & Whitney Canada PW615F-A turbofan engines are installed on the Mustang. The engine is a 2.8:1 bypass ratio, counter-rotating twin-spool design with three compression stages and two turbine stages. It produces 1,460 pounds (6.49 kN) of thrust at sea level, static conditions, flat-rated up to 77°F (25°C). The FADEC system also provides time-limited dispatch, diagnostics, and engine synchronization according to switch position. • Manufacturer: Pratt & Whitney • Model: (2) PW615F-A • Thrust: 1,460 lbf • Time between overhaul: 3,500 hr Citation M2 - Detailed Specifications Performance data is based on the standard M2 configuration, operating in International Standard Atmosphere (ISA) conditions with zero wind. Takeoff and landing field lengths are based on a level, hard surface and dry runway. Actual performance will vary with factors such as environmental conditions, aircraft configuration and operational/ATC procedures. Preliminary data, subject to change. Dimensions • Length • 42 ft 7 in (12.98 m) • Height • 13 ft 11 in (4.24 m) • Wingspan • 47 ft 3 in (14.40 m) Wing • Wing Area • 240 sq ft (22 sq m) • Wing Sweep • 0.0 degrees Wheelbase • 15 ft 4 in (4.67 m) Tread • 13 ft (3.96 m) Cabin Interior • Height • 57 in (1.45 m) • Width • 58 in (1.47 m) • Length • 11 ft (3.35 m) • Seating Capacity • 7 - 7 Baggage Capacity • Weight • 725 lb (329 kg) • Volume • 46 cu ft (1.29 cu m) • Single Pilot Certified • Yes Wingspan – 47 ft 3 in (14.40 m) Height 13 ft 11 in (4.24 m) Length – 42 ft 7 in (12.98 m) Weights • Maximum Ramp Weight • 10,800 lb (4,899 kg) • Maximum Takeoff Weight • 10,700 lb (4,853 kg) • Maximum Landing Weight • 9,900 lb (4,491 kg) • Maximum Zero Fuel Weight • 8,400 lb (3,810 kg) Usable Fuel Capacity • Weight • 3,309 lb (1,501 kg) • Volume • 494 gal (1,870 l) • Basic Operating Weight • 6,991 lb (3,171 kg) • Useful Load • 3,809 lb (1,728 kg) • Maximum Payload • 1,409 lb (639 kg) • Full Fuel Payload • 500 lb (227 kg) Performance • Maximum Cruise Speed • 400 ktas (741 km/h) • Range • 1,300 nm (2,408 km) • Takeoff Distance • 3,250 ft (991 m) • Landing Distance • 2,640 ft (805 m) • Maximum Operating Altitude • 41,000 ft (12,497 m) • Maximum Climb Rate • N/A fpm (N/A mpm) • Maximum Limit Speed • 0.710 Mach Powerplant Two Williams FJ44 turbofan engines are installed on the Citation M2. This engine is a 2.58:1 bypass, twin-spool design with three compression stages and three turbine stages and produces 1,965 pounds (8.74 kN) of takeoff thrust at sea level, static conditions, flat-rated up to 72° F (22° C). Dual-channel full authority digital engine controls (FADECs) provide automation and efficiency in engine management. • Manufacturer: Williams International • Model: (2) FJ44-1AP-21 • Thrust: 1,965 lbf • Time Between Overhaul: 4,000 hr Citation CJ2+ - Detailed Specifications Performance data is based on the standard CJ2+ configuration, operating in International Standard Atmosphere (ISA) conditions with zero wind. Takeoff and landing field lengths are based on a level, hard surface and dry runway. Actual performance will vary with factors such as environmental conditions, aircraft configuration and operational/ATC procedures. Dimensions • Length • 47 ft 8 in (14.53 m) • Height • 14 ft (4.27 m) • Wingspan • 49 ft 10 in (15.19 m) Wing • Wing Area • 264 sq ft (25 sq m) • Wing Sweep • 0.0 degrees Wheelbase • 17 ft 10 in (5.44 m) Tread • 15 ft 11 in (4.85 m) Cabin Interior • Height • 57 in (1.45 m) • Width • 58 in (1.47 m) • Length • 13 ft 7 in (4.14 m) • Seating Capacity • 8 - 9 Baggage Capacity • Weight • 1,000 lb (454 kg) • Volume • 65 cu ft (1.84 cu m) • Single Pilot Certified • Yes Wingspan – 49 ft 10 in (15.19 m) Height 14 ft (4.27 m) Length – 47 ft 8 in (14.53 m) Weights • Maximum Ramp Weight • 12,625 lb (5,727 kg) • Maximum Takeoff Weight • 12,500 lb (5,670 kg) • Maximum Landing Weight • 11,525 lb (5,228 kg) • Maximum Zero Fuel Weight • 9,700 lb (4,400 kg) Usable Fuel Capacity • Weight • 3,930 lb (1,783 kg) • Volume • 587 gal (2,221 l) • Basic Operating Weight • 8,010 lb (3,633 kg) • Useful Load • 4,615 lb (2,093 kg) • Maximum Payload • 1,690 lb (767 kg) • Full Fuel Payload • 685 lb (311 kg) Performance • Maximum Cruise Speed • 418 ktas (774 km/h) • Range • 1,613 nm (2,987 km) • Takeoff Distance • 3,360 ft (1,024 m) • Landing Distance • 2,980 ft (908 m) • Maximum Operating Altitude • 45,000 ft (13,716 m) • Maximum Climb Rate • 4,120 fpm (1,256 mpm) • Maximum Limit Speed • 0.737 Mach Powerplant Producing 2,490 pounds (11.08 kN) of thrust at sea level, the CJ2+ is powered by two Williams FJ44-3A- 24 turbofan engines. Even at the maximum takeoff weight with every passenger seat filled, the CJ2+ will still travel more than 1,150 nautical miles (2,130 km). Take on runways as short as 3,360 feet (1,024-m) and use less fuel than other jets in the category. Climb directly to 45,000 feet (13,716 m) in just 28 minutes — eight minutes faster than the original CJ2. With the addition of full-authority digital engine controls (FADEC) in every CJ, engine control is simplified, reducing pilot workload during the busiest phases of flight.
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