Search results
Results from the WOW.Com Content Network
Citation Bravo (Model 550 Bravo), [1] updated S/II with new PW530A engines, landing gear and Primus 1000 avionics. [ 28 ] [ unreliable source? ] [ 29 ] The last Citation Bravo rolled off the production line in late 2006, ending a nearly 10-year production run of 337 aircraft.
The Cessna Citation is a family of business jets manufactured by Cessna that entered service in 1972. [1] In the fifty years following the type's first flight in 1969, more than 7,500 Citations were delivered, forming the largest business jet fleet in the world. [2]
Cessna 680 Citation Sovereign: 2002 443 Twin jet engine monoplane business airplane Cessna 680A Citation Latitude: 2014 359+ Twin jet engine monoplane business airplane Cessna 700 Citation Longitude: 2016 100+ Twin jet engine monoplane business airplane Cessna 750 Citation X: 1993 339 Twin jet engine monoplane business airplane Cessna 850 ...
The Citation V (Model 560) is a development of the Citation S/II, retaining the supercritical airfoil and swept wing roots of that aircraft, but with a 1.5 ft (46 cm) fuselage stretch and recontoured interior for increased passenger space. [2]
The jet uses the Citation II's forward fuselage, a new carry-through section, a new laminar flow, supercritical wing developed with NASA and Boeing, and a T-tail. Powered by two 1,900 lbf (8.5 kN) Williams FJ44s, the 10,000 lb (4,500 kg) aircraft has a trailing link undercarriage for smooth landings, and can be flown by a single pilot. Range is ...
The 501 Citation I/SP, certificated for single pilot operations, was delivered in early 1977. Production ended in 1985, it was developed into the Citation II/Bravo and the Citation V/Ultra/Encore. [9] 395 Citations and Citation Is and 296 I/SPs were built between 1971 and 1985.
List of civil aircraft is a list of articles on civilian aircraft with ... Cessna 500 & 501 Citation, ... FFA AS-202 Bravo two-seat basic trainer and aerobatic light ...
The 526 and 525 shared 75% commonality including the wings, engines and landing gear. The electrical- hydraulic- and fuel systems were also common to the two types. The 526 had a redesigned fuselage featuring a tandem two-seat cockpit with zero-zero ejection seats; and a new empennage with a low-mounted tailplane instead of the 525's T-tail. [1]