Cessna Citation CJ1

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The Cessna Citation CJ1 (Model 525) is the first and smallest of the CJ series of Cessna aircraft. It was developed as an improved version of the original Cessna CitationJet (also Model 525). It borrows much of the forward fuselage from the Cessna Citation I (Model 500).^[1] The CJ1 improved on the CitationJet by adding the Collins Pro Line 21 EFIS avionics suite and a moderate increase in maximum takeoff. The CJ1 has a newer cousin, the CJ1+ which shares the same airframe but has an additional updated avionics package and FADEC, to allow the engines to be controlled by computer rather than mechanical controls.

[edit] Specifications for CJ1+

Data from http://cj1plus.cessna.com/specifications.chtml

General characteristics

• Crew: 1
• Capacity: 5 passengers
• Length: 42 ft 7 in (12.98 m)
• Wingspan: 46 ft 11 in (14.30 m)
• Height: (4.19 m)
• Empty weight: 6,765 lb (3,069 kg)
• Useful load: 3,835 lb (1,740 kg)
• Max takeoff weight: 10,700 lb (4,853 kg)
• Powerplant: 2× Williams FJ44-1AP turbofan, 1,965 lbs (8.74 kN) each

Performance

• Maximum speed: 389 ktas (720 km/hr)
• Stall speed: 83 kcas (153 km/hr)
• Range: 1,300 nm (2,408 km)
• Service ceiling: 41,000 ft (12,497 m)

[edit] References