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Fact Files  >  CJ2, CE-525A

Cessna - CJ2, CE-525A
Category: Jet < 20,000 lbs.
Years Aircraft Manufactured: 2000 - current
Printer friendy version
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The very successful CitationJet was developed as a replacement for the Citation and Citation 1. The same basic Citation forward fuselage is mounted to a new T-tail configured tailplane and a new supercritical laminar flow wing, and it features Williams Rolls FJ44 turbofans (with paddle thrust reversers) and trailing link main undercarriage. The CJ1 replaced CitationJet, and features an improved avionics suite, Collins Pro Line 21 EFIS and also a moderate increase in maximum takeoff weight. The CJ2 meanwhile is a stretched, faster and more powerful development, featuring a 35in (89cm) stretched cabin and 17in (35cm) tailcone stretch allowing standard seating for six in the main cabin. It also has uprated FJ44-2C engines, increased span wings, larger area tail, six cabin windows per side and greater range. It is certificated for single pilot operation.

Seating (normal) 7 Max Takeoff (lbs) 12,375
Seating (maximum) - Certified Ceiling (ft) 45,000
Engines 2 Wms/RR FJ44-2C To (Sealevel, ISA Temp) (ft) 3,420
Output lbs ea. Flat Rating 2,400/ISA+7 Landing Distance (ft) 2,589
Maximum Mach No. 0.72 Max Range (fuel) (nm) 1,550
High Speed Cruise (Kts) 407 Max Range (payload) (nm) 1,092
Flight Time 300nm 0 + 51 Flight Time 1000nm 2 + 40
Flight Time 600nm 1 + 37    
External Internal
Length (ft) 47.70 Length (ft) 13.80
Height (ft) 13.90 Height (ft) 4.70
Span (ft) 49.80 Width: Max floor (ft) 4.80
 

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