Ads
related to: citation x specifications cabin dimensions performance standard 2 door
Search results
Results From The WOW.Com Content Network
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.
1980 Citation X-11. Produced as a separate trim level, the Citation X-11 was a variant featuring cosmetic, chassis, and powertrain upgrades over the standard Citation. While less powerful than the Camaro Z28 (and later Monte Carlo SS), the Citation X-11 would also take over the role of the similarly sized Chevrolet Monza.
The cockpit features EFIS avionics; fuselage length is reduced 11 inches (27 cm) compared to the Citation I, and cabin length is reduced by 1 ft 6 in (46 cm), but with a lowered center aisle for increased cabin height. [2] [5] The cockpit side windows are slightly smaller than those on earlier Citations to lessen interior temperature ...
[citation needed] Interior standing room is an average of six feet. [17] This composite construction also makes the aircraft lighter than a standard aluminum structure, allowing a maximum range of 3,445 nautical miles, and a service ceiling of 45,000 feet (14,000 m). [18]
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.
Data from Gulfstream General characteristics Crew: 2 Capacity: seating for 10 in executive style and 4,050 pounds (1,840 kg) payload Length: 66 ft 10 in (20.3 m) Wingspan: 63 ft 0 in (19.2 m) Height: 21 ft 4 in (6.5 m) Wing area: 495 sq ft (46 m 2) Empty weight: 24,150 lb (10,954 kg) Max takeoff weight: 39,600 lb (17,960 kg) Powerplant: 2 × Honeywell HTF7250G turbofans, 7,624 lbf (33.91 kN ...
The Citation II (Model 550) was developed to provide the same docile low-speed handling and good short-field performance as the preceding Citation I while addressing a primary criticism of that aircraft — its relatively slow cruise speed of around 350 kn (650 km/h) at altitude. [2] The II stretches the Citation I fuselage by 1.14m (3 ft 9in ...
The Citation Excel fuselage was stretched for a 6.6 ft (2.0 m) longer cabin and joined with a large, newly designed 515.9 sq ft (47.93 m 2) wing with large trailing edge flaps for good runway performance, 16.3° wing sweep and a relatively high critical Mach number for efficient 445 kn (824 km/h) TAS cruise.