Citation 551 Weights

It has a maximum payload of 1,400 kg and a fuel capacity of 862 us gal. A further model to appear was the 501 citation i/sp, which is certificated for single pilot operation.

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Citation 551 weights. 8,059 lb (3,656 kg) max takeoff weight: The cessna citation ii is a stretched development of the cessna 500 citation i (+1,29m / 4ft 3in). 15 ft 0 in (4.57 m) max takeoff weight:

Announced in october 1983, the s550 first flew on 14 february, 1984. 47 ft 8.5 in (14.542 m) wingspan: 0 to +2.0 weight model 550 model 551 max ramp weight 13,500 lbs.

746 km/h) at 35,000 ft (11,000 m) max payload: The maximum operating altitude for the model 551 is 43,000´. Attachment buckles are made of nonmetal delrin, designed for rugged outdoor use.

Performance (above 29,315 ft (8,935 m)) maximum speed: 862 us gal (718 imp gal; General specs (cessna s550 citation sii) crew:

Certification, including an exemption for single pilot. The windshield cover comes with a duffle bag. The i/sp was delivered in early 1977.

Maximum takeoff and landing weights may be additionally restricted due to altitude, temperature and. Description the cessna citation ii was the first of the model 550 series of citation jets, which are light corporate jet built by cessna. 15,100 lb (6,849 kg) performance.

* with a minimal modification to the aircraft, the medical unit mounts to the seat tracks. It was launched to the public in 1983. Improvements were made to the design for the model s550 citation s/ii.

Production of the citation i ceased in 1985, its place in the citation line left vacant until the arrival of the. Max zero fuel weight (optional) 11,000 lbs. The citation ii model 550 is the initial variant and a larger stretched development of the model 500.

* this fully self contained critical care system is equipped with 3300 liters of oxygen, an air. The model ii/sp citation 551 is the single pilot version. Max takeoff weight 13,300 lbs.

But the rest of the airplane’s specifications are essentially the same as those for the straight ii. Max landing weight 12,700 lbs. The cessna 550/551 citation ii is a light corporate jet built between 1978 and 2006.

The maximum takeoff weight for the model 551 is 12,500 lbs. Citation 550/551 phase inspection services download report comments However you should not view the original citation ii as a real jet;

52 ft 2.5 in (15.913 m) height: 15,100 lb (6,849 kg) fuel capacity: Cessna citation 501 and 551 series.

Max zero fuel weight (standard) 9,500 lbs.

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