Cessna Citation M2

Gemini Sparkle

Key Takeaways:

  • The article provides comprehensive technical specifications for the Cessna Citation M2 aircraft, detailing its engine, weights, and dimensions.
  • Powered by Williams FJ44-1AP engines, it boasts a maximum cruise speed of 400 KTAS and an IFR range of 1300 nm, with a maximum operating altitude of 41,000 ft.
  • The aircraft features a seating capacity of 6+2, an 11-foot cabin length, and a baggage capacity of 725 lbs.
  • Performance highlights include a balanced field length of 3260 ft for takeoff and 2590 ft for landing.
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Cessna Citation M2
Engine Make & Model: Williams FJ44-1AP
Thrust (lbf): 1965
Fuel Type: Jet-A
TBO (hrs.): 3500
Standard Empty Weight: 6791
Max Ramp Weight (lbs.): 10,800
Max T/O Weight (lbs.): 10,700
Max Landing Weight (lbs.): 9900
Max Zero Fuel Weight (lbs.): 8400
Useable Fuel (lbs./gal.): 3309/494
Full Fuel Payload (lbs.): 700
Wingspan (ft.): 47.3
Overall Length (ft.): 42.6
Height (ft.): 13.9
Wing Area (sq. ft.): 240.0
Max Wing Loading (lbs./sq. ft.): 44.6
Cabin Length (ft): 11.0
Seating Capacity as Tested: 6+2
Cabin Width (in.): 58
Cabin Height (in.): 57
Baggage Capacity (lbs.): 725
Baggage Volume (cu. ft.): 46
PERFORMANCE
Max Cruise Speed (KTAS): 400
Maximum Operating Vmo (KIAS)/Mmo: 263/0.710M
IFR Range w/100 nm, NBAA reserve (nm): 1300
Max Operating Altitude (ft.): 41,000
Max Cabin Differential (psi): 8.60
Cabin Altitude At FL 410 (ft.): 8,000
Balanced Field Length for MTW Takeoff: 3260
Runway Length For MLW Landing: 2590

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