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Year
1978

Specifications

Performance (across variants)

Range
·
2,300 nm
Cruise
·
403 kt
Service ceiling
·
45,000 ft
MTOW
·
6,800 kg
Passengers
·
Up to 12

Description

Aircraft Information General Performance & Specifications Description Aircraft Information Year: 1978 – 1994 Make: Citation Model: II Active Fleet: 578 – For Sale/Lease: 95 Average Asking Price – February 2014: $821,000 Range: 1,220 – 1,520 nm Contact Number: 1-847-726-5000 General Performance & Specifications Cabin Height: 4.7 Feet Cabin Width: 4.8 Feet Cabin Length: 15.75 Feet Baggage Volume Internal: 36.0 Cubic Feet Baggage Volume External: 41.0 Cubic Feet Seats Executive: 2/7 Max. Take-Off Weight: 14,100 lbs. Max. Landing Weight: 13,500 lbs. Maximum Payload: 2,350 lbs. Balance Field Length: 4,580 Feet Landing Distance: 3,500 Feet Rate of Climb – All Engines: 3,130 Feet / Minute Rate of Climb – One Engine Out: 930 Feet / Minute Normal Cruise Speed: 355 ktas Max. Cruise Speed: 355 ktas Service Ceiling Max. Weight: 41,000 Feet Number of Engines: 2 Engine Manufacturer: Pratt & Whitney Engine Model: JT15D-4 Description The Citation II, Model 550, was a direct development from the Citation I. The earlier aircraft’s success in the market led Cessna to believe there was demand for a larger aircraft that utilized the same design philosophy. The result was the Citation II, which had a maximum seating capacity of 10. In addition to more seats, the plane had more powerful JT15D4 engines, faster speeds and longer range. First flight was on January 31, 1977, and the aircraft was certified for two-pilot operation in March 1978. A total of 603 aircraft were built before the Citation II was replaced by the Bravo in the production line. Citation II/SP Like the Citation I/SP, the Model 551 Citation II/SP as Cessna’s means of competing in the turboprop market, which predominantly are operated single-pilot, so the aircraft was re-certified for single-pilot operations.

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