Cessna Citation Model Stats - ANTN Digicast Citation Models...Two, dual-channel FADEC-controlled,...

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 • Wing Sweep

• 516 sq ft (48 sq m) • 16.3 degrees

Wheelbase • 27 ft 10 in (8.49 m)

Tread • 10 ft (3.05 m)

Cabin Interior

• Height • Width • Length

• 68 in (1.73 m) • 66 in (1.68 m) • 25 ft 3 in (7.70 m)

• Seating Capacity • 9 - 12

Baggage Capacity

• Weight • Volume

• 1,415 lb (642 kg) • 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


• 11,390 lb (5,166 kg) • 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


• 210 sq ft (20 sq m) • 11.0 degrees


Tread • 11 ft 10 in (3.61 m)

Cabin Interior


• 54 in (1.37 m) • 55 in (1.40 m) • 9 ft 9 in (2.97 m)


Baggage Capacity


• 718 lb (326 kg) • 63 cu ft (1.78 cu m)

• Single Pilot Certified • Yes



Length – 40 ft 7 in (12.37 m)

Weights







• 2,580 lb (1,170 kg) • 385 gal (1,457 l)


• Useful Load • 3,140 lb (1,424 kg)

• Maximum Payload • 1,160 lb (526 kg)

• Full Fuel Payload • 560 lb (254 kg)

Performance


• Range • 1,150 nm (2,130 km)

• Takeoff Distance • 3,110 ft (948 m)



• Maximum Climb Rate • 3,010 fpm (917 mpm)


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.


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


• 240 sq ft (22 sq m) • 0.0 degrees


Tread • 13 ft (3.96 m)

Cabin Interior


• 57 in (1.45 m) • 58 in (1.47 m) • 11 ft (3.35 m)


Baggage Capacity


• 725 lb (329 kg) • 46 cu ft (1.29 cu m)




Length – 42 ft 7 in (12.98 m)

Weights







• 3,309 lb (1,501 kg) • 494 gal (1,870 l)





Performance


• Range • 1,300 nm (2,408 km)






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.


Dimensions

• Length • 47 ft 8 in (14.53 m)

• Height • 14 ft (4.27 m)

• Wingspan • 49 ft 10 in (15.19 m)

Wing




Tread • 15 ft 11 in (4.85 m)

Cabin Interior


• 57 in (1.45 m) • 58 in (1.47 m) • 13 ft 7 in (4.14 m)


Baggage Capacity


• 1,000 lb (454 kg) • 65 cu ft (1.84 cu m)



Height 14 ft (4.27 m)

Length – 47 ft 8 in (14.53 m)

Weights







• 3,930 lb (1,783 kg) • 587 gal (2,221 l)





Performance


• Range • 1,613 nm (2,987 km)




• Maximum Climb Rate • 4,120 fpm (1,256 mpm)


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. It also ensures proper power output, engine synchronization, and maximum fuel efficiency.

• Manufacturer: Williams International • Model (Number): FJ44-3A-24 (2) • Thrust: 2,490 lbf each (11.08 kN) • Time Between Overhauls: 4,000 hrs

Citation CJ3 -

Detailed Specifications Performance data is based on the standard CJ3 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.


Dimensions

• Length • 51 ft 2 in (15.59 m)

• Height • 15 ft 2 in (4.62 m)

• Wingspan • 53 ft 4 in (16.26 m)

Wing



Wheelbase • 20 ft (6.10 m)

Tread • 16 ft (4.88 m)

Cabin Interior


• 57 in (1.45 m) • 58 in (1.47 m) • 15 ft 8 in (4.78 m)


Baggage Capacity


• 1,000 lb (454 kg) • 65 cu ft (1.84 cu m)




Length – 51 ft 2 in (15.59 m)

Weights







• 4,710 lb (2,136 kg) • 703 gal (2,661 l)





Performance


• Range • 1,875 nm (3,472 km)






Powerplant

Two, dual-channel FADEC-controlled, Williams FJ44-3A turbofan engines are installed on the CJ3. The engine is a medium-bypass, twin-spool design with five compression stages and three turbine stages. It produces 2,820 pounds (12.54 kN) of thrust at sea level, static conditions, flat-rated up to 79°F (26°C). The FADEC system also provides time-limited dispatch, diagnostics, and engine synchronization.

• Manufacturer: Williams International • Model: (2) FJ44-3A • Thrust: 2,820 lbf • Time Between Overhaul: 4,000 hrs

Citation CJ4 -



Dimensions

• Length • 53 ft 4 in (16.26 m)

• Height • 15 ft 4 in (4.67 m)

• Wingspan • 50 ft 10 in (15.49 m)

Wing

• Wing Area

• 330 sq ft (31 sq m)

• Wing Sweep • 12.5 degrees


Tread • 12 ft 4 in (3.76 m)

Cabin Interior


• 57 in (1.45 m) • 58 in (1.47 m) • 17 ft 4 in (5.28 m)


Baggage Capacity


• 1,040 lb (472 kg) • 77 cu ft (2.18 cu m)




Length – 53 ft 4 in (16.26 m)

Weights







• 5,828 lb (2,644 kg) • 870 gal (3,293 l)





Performance


• Range • 1,920 nm (3,556 km)






Powerplant

Two dual-channel, FADEC-controlled, Williams FJ44-4A turbofan engines are installed on the CJ4. This engine is a medium-bypass, twin-spool design with four compression stages and three turbine stages. It produces 3,621 pounds (16.11 kN) of takeoff thrust at sea level, static conditions, flat-rated up to 79°F (26°C). The FADEC system also provides time-limited dispatch, diagnostics, and engine synchronization.


Citation XLS+ -



Dimensions

• Length • 53 ft 4 in (16.26 m)

• Height • 15 ft 4 in (4.67 m)

• Wingspan • 50 ft 10 in (15.49 m)

Wing


• 330 sq ft (31 sq m) • 12.5 degrees


Tread • 12 ft 4 in (3.76 m)

Cabin Interior


• 57 in (1.45 m) • 58 in (1.47 m) • 17 ft 4 in (5.28 m)


Baggage Capacity


• 1,040 lb (472 kg) • 77 cu ft (2.18 cu m)




Length – 53 ft 4 in (16.26 m)

Weights







• 5,828 lb (2,644 kg) • 870 gal (3,293 l)





Performance


• Range • 1,920 nm (3,556 km)






Powerplant



Citation Latitude -



Dimensions

• Length • 53 ft 4 in (16.26 m)

• Height • 15 ft 4 in (4.67 m)

• Wingspan • 50 ft 10 in (15.49 m)

Wing


• 330 sq ft (31 sq m) • 12.5 degrees


Tread • 12 ft 4 in (3.76 m)

Cabin Interior


• 57 in (1.45 m) • 58 in (1.47 m) • 17 ft 4 in (5.28 m)


Baggage Capacity


• 1,040 lb (472 kg) • 77 cu ft (2.18 cu m)




Length – 53 ft 4 in (16.26 m)

Weights







• 5,828 lb (2,644 kg) • 870 gal (3,293 l)





Performance


• Range • 1,920 nm (3,556 km)






Powerplant


• Manufacturer: Williams International • Model: (2) FJ44-4A • Thrust: 3,621 lbf

• Time Between Overhaul: 5,000 hrs

Citation X -

Detailed Specifications Performance data is based on the standard X 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.



Dimensions

• Length • 73 ft 7 in (22.43 m)

• Height • 19 ft 3 in (5.86 m)

• Wingspan • 69 ft 2 in (21.09 m)

Wing


• N/A sq ft (N/A sq m) • 37.0 degrees


Tread • 10 ft 7 in (3.23 m)

Cabin Interior


• 68 in (1.73 m) • 66 in (1.68 m) • 25 ft 2 in (7.67 m)


Baggage Capacity


• 775 lb (352 kg) • 104 cu ft (2.93 cu m)




Length – 73 ft 7 in (22.43 m)

Weights







• 12,931 lb (5,865 kg) • 1,930 gal (7,306 l)


• Useful Load • 14,436 lb (6,548 kg)

• Maximum Payload • 2,514 lb (1,140 kg)

• Full Fuel Payload • 1,505 lb (683 kg)

Performance


• Range • 3,242 nm (6,004 km)


• Landing Distance • 3,430 ft (1,045 m)




Powerplant

Two dual-channel FADEC-controlled Rolls-Royce AE3007C2 turbo fan engines power the Citation X. The AE3007C2 features two spools with a 14-stage axial flow compressor, a two-stage high-pressure turbine, and a three-stage low-pressure turbine. The engine has a bypass ratio of 5:1 and a static takeoff thrust at sea level of 7,034 pounds (31.29 kN) flat rated up to 86°F (30°C). Hydraulically actuated, target-type thrust reversers are attached to each engine. An APU is incorporated for engine start and other benefits.

• Manufacturer: Rolls-Royce • Model: (2) AE3007C2 • Thrust: 7,034 lbf • Time between overhaul: 4,500 hrs

Citation Longitude -

Detailed Specifications Performance data is based on the standard Longitude 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.



Dimensions

• Length • 87 ft (26.52 m)

• Height • 26 ft (7.92 m)

• Wingspan • 86 ft (26.21 m)

Wing


• N/A sq ft (N/A sq m) • 30.0 degrees

Wheelbase • N/A (N/A m)

Tread • N/A (N/A m)

Cabin Interior


• 72 in (1.83 m) • 77 in (1.96 m) • 28 ft 11 in (8.81 m)


Baggage Capacity


• N/A lb (N/A kg) • 100 cu ft (2.83 cu m)


Wingspan – 86 ft (26.21 m)

Height 26 ft (7.92 m)

Length – 87 ft (26.52 m)

Weights

• Maximum Ramp Weight • N/A lb (N/A kg)

• Maximum Takeoff Weight • N/A lb (N/A kg)

• Maximum Landing Weight • N/A lb (N/A kg)

• Maximum Zero Fuel Weight • N/A lb (N/A kg)



• N/A lb (N/A kg) • N/A gal (N/A l)

• Basic Operating Weight • N/A lb (N/A kg)

• Useful Load • N/A lb (N/A kg)

• Maximum Payload • N/A lb (N/A kg)

• Full Fuel Payload • N/A lb (N/A kg)

Performance


• Range • 4,000 nm (7,408 km)


• Landing Distance • N/A (N/A m)




Powerplant

The Snecma Silvercrest® SC-2C is the next-generation business jet engine and is making its debut in the Citation Longitude. With Silvercrest, Snecma gives Citation its best-in-class technologies, based on its long-standing expertise in military aircraft engines, as well as 36 years of experience within the CFM joint venture (GE and Snecma) for the best-selling CFM56 commercial aero-engine.

• Manufacturer: Snecma Silvercrest® SC-2C • Thrust: Over 11,000 lbf each at takeoff • Fuel burn: 15% lower than engines with similar thrust • Noise level: Up to 20 EPNdB vs. Stage 4 • Emission: 50% margin vs. CAEP/6

Cessna Citation Model Stats - ANTN Digicast Citation Models...Two, dual-channel FADEC-controlled,...

Documents

Transcript of Cessna Citation Model Stats - ANTN Digicast Citation Models...Two, dual-channel FADEC-controlled,...