Light Jets

CESSNA CITATION CJ2/CJ2+



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AIRCRAFT DESCRIPTION

The Cessna CitationJet/CJ series (Model 525) are American turbofan-powered light corporate jets built by the Cessna Aircraft Company in Wichita, Kansas. The Citation brand of business jets encompasses seven distinct "families" of aircraft. The Model 525 CitationJet was the basis for one of these families, which encompasses the CJ, CJ1, CJ1+, CJ2, CJ2+, CJ3, and CJ4 models. The Cessna Citation CJ2 (Model 525A) is a 5' stretch extension of the Cessna Citation CJ1 (Model 525) first delivered in the year 2000. The 525A comes in two forms, the original CJ2 and the newer CJ2+, which has updated avionics, increased performance, and FADEC controls. The CJ2+ was first delivered in April 2006.

The CJ2 is quite fuel-efficient, with an average fuel burn of 140 gallons per hour. The economy of its fuel burn can be largely attributed to Cessna’s choice of engines. It uses two Williams/Rolls-Royce FJ44-2C turbofan engines, each of which delivers 2,400 lbs of thrust on takeoff (400 lbs more than the CJ1 and CJ1+).

The CJ2 can take off in 3,420 feet at sea level, or in 5,080 feet on a runway at an altitude of 5,000 feet. It takes seventeen minutes to climb to 37,000 feet. At its maximum certified flight ceiling of 45,000 feet, it reaches its long range cruise speed of 352 knots. Its high speed cruise is 407 knots. All of the cabin’s pressurization systems (certified to 8.9 psi) are controlled digitally, able to maintain a sea-level cabin pressure at 23,586 feet.

The cabin typically holds six passengers and has a total volume of 243 cubic feet. Its three baggage compartments can carry a total of 1,100 pounds of luggage, all but 100 of which can be stored externally for a less cramped cabin..


AIRCRAFT CHARACTERISTICS & SPECIFICATIONS(CJ2)


External Dimensions

Engine
2 X Williams FJ44-3A-24
Power
2,490.00 lbf
Avionics
Rockwell Collins Pro Line 21
Max Cruise Speed
774.00 km per hr    480.96 mph
Service Ceiling
13,716.00 metres  45,000.00 feets
Rate of Climb
1,255.78 mpm   4,120.00 fpm
Cabin Height

1.45 metres  4.76 feets

Cabin Width
1.47 metres  4.82 feets
Cabin Length
4.14 metres  13.58 feets
Exterior Length
14.53 metres  47.67 feets
Wingspan

15.19 metres  49.84 feets

Baggage Volume
1.84 cubic metre  64.98 \cubic feet
Max Take Off Weight
5,670.00 kgs  12,500.00 lbs
Maximum Payload
2,131.92 kgs  4,700.00 lbs
Fuel Tank Capacity
587.00 gallon  2,222.03 litres
Fuel Economy
1.16 km per litre  2.74 NM per gallon
Min Take Off Distance
1,024.13 metres  3,360.00 feets
Min Landing Distance
908.30 metres  2,980.00 feets
Manufactured from
2001 - Present
Seating Chart /Seats
5
Travel Range
1,613.00 Nautical Miles 2,987 Kilometer
Country of Manufacture
United States

 

AIRCRAFT AVERAGE PRICE USED/NEW (17 TO 45 CRORE)

 

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