Aircraft Information
| Years Manufactured: | 1978-1994 |
| Manufacturer: | Citation |
| Model: | II |
| Active Fleet: | 663 |
| Average Ask Price - August 2010: | $1,337,195 |
| Range: | 1,220 - 1,520 nm |
| Contact Number: | 1-847-726-5000 |
| Current Market Price / Availability: | Request Market Update Report |
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.
General Performance & Specifications
| Cabin Height: | 4.70 ft. |
| Cabin Width: | 4.80 ft. |
| Cabin Length: | 15.75 ft. |
| Baggage Volume Internal: | 36.0 cu.ft. |
| Baggage Volume External: | 41.0 cu.ft. |
| 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 ft. |
| Landing Distance: | 3,500 ft. |
| ate of Climb - All Engines: | 3,130 ft./min. |
| Rate of Climb - One Engine Out: | 930 ft./min. |
| Normal Cruise Speed: | 355 ktas |
| Max. Cruise Speed: | 355 ktas |
| Service Ceiling Max. Weight: | 41,000 ft. |
| Number of Engines: | 2 |
| Engine Model: | JT15D-4 |
| Engine Manufacturer: | Pratt & Whitney |