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Viewed from below, showing wing sweep The 650 has a T-tail and two turbofans. In 1974, Cessna studied a long range model 700 stretch of its original Citation I powered by three JT15Ds called Citation III, with a 17,500 lb gross weight, an 8,000 lb empty weight and a 7,500 lb fuel capacity leaving 2,000 lb for the occupants, and targeting 1978 deliveries. [3]
The II/SP is a single pilot version, the improved S/II first flew on February 14, 1984 and the Citation Bravo, a stretched S/II with new avionics and more powerful P&WC PW530A turbofans, first flew on April 25, 1995. The United States Navy adopted a version of the S/II as the T-47A. Production ceased in 2006 after 1,184 of all variants were ...
The II/SP is a single pilot version, the improved S/II first flew on February 14, 1984 and the Citation Bravo, a stretched S/II with new avionics and more powerful P&WC PW530A turbofans, first flew on April 25, 1995. The United States Navy adopted a version of the S/II as the T-47A. Production ceased in 2006 after 1,184 of all variants were ...
The Cessna 750 Citation X [a] is an American mid-size business jet produced by Cessna; it is part of the Citation family. Announced at the October 1990 NBAA convention, the Model 750 made its maiden flight on December 21, 1993, received its type certification on June 3, 1996, and was first delivered in July 1996.
The Cessna Citation Longitude is a business jet produced by Cessna, part of the Cessna Citation family. It remains the largest business jet by Cessna. It remains the largest business jet by Cessna. Announced at the May 2012 EBACE , the Model 700 made its first flight on October 8, 2016, with certification obtained in September 2019.
The captain's side EFIS of the Citation V was upgraded to a full Honeywell Primus 1000 glass cockpit for both pilots. [4] [6] [7] Deliveries amounted to 279. [1] The Ultra was named Flying magazine's "Best Business Jet" of 1994 [9] and it was produced until 1999. [4] Both the Citation V and Ultra hold 5816 pounds of fuel. [citation needed]
Data from Jane's Civil and Military Aircraft Upgrades 1994-95 General characteristics Crew: Two (One pilot on I/SP) Capacity: 5 passengers Length: 43 ft 6 in (13.26 m) Wingspan: 47 ft 1 in (14.35 m) Height: 14 ft 4 in (4.37 m) Wing area: 278.5 sq ft (25.87 m 2) Aspect ratio: 7.83:1 Empty weight: 6,631 lb (3,008 kg) Max takeoff weight: 11,850 lb (5,375 kg) Fuel capacity: 564 US gal (470 imp gal ...
The Citation XLS+, or simply "Plus" configuration was another upgraded version of the aircraft which began delivery in 2008, with the inclusion of FADEC engine controls, improved PW545C engines, and a completely revised nose design similar to that found on the Citation Sovereign and Citation X.