Our Cessna turboprop is the perfect craft for short flights (up to four or five hours, depending on the load) and for its ability to operate in smaller airfields. The executive style interior comfortably seats up to nine passengers.
Aircraft Specifications: Speed 355 mph or 310 knots, Altitude Maximum 35,000 ft., Interior The executive interior provides first class seating for eight passengers plus one pilot. Cargo 820 lbs, including passengers and baggage. Range Fully loaded, the Cessna Conquest will fly 4 hours or 1,100 miles. With four persons on board, the range is 5.3 hours or 1,700 miles.
Technical Data
Wing span: 49.33 ft, Length: 39.02 ft, Height: 13.14 ft, Max Ramp Weight: 10,240 lbs, Max Take off Weight: 10,165 lbs Max Fuel Weight: 3,600 lbs, Engine: 2 Garrett TPE331 Turbine Engines, Max speed: 245 KIAS/.55M, Max ceiling: 35,000 ft
The IAI-1125 Astra is comprehensively upgraded development of the successful IAI-1124 Westwind, with a number of key changes to improve performance and increase cabin volume. It is now part of the expanded Gulfstream stable, designated G100.
The Astra is based on the basic Westwind II fuselage and tail, mated with an all new high speed swept wing (initially lacking winglets). Aside from the aerodynamic and hence performance benefits of the new wing, it was also repositioned low on the fuselage (as opposed to mid mounted on the Westwind), where it does not intrude on internal cabin space.
The original 1125 Astra was replaced in production by the Astra SP. Thirty seven were built before it was replaced by the SPX. The SPX, renamed G100 from September 2002, first flew in August 1994. It features more powerful FADEC equipped 18.9kN (4250lb) Honeywell TFE731-40R-200Gs, winglets and Collins Pro Line 4 avionics.
Cruise speed : 850 km/h, Maximum range : 5700 km, Crew : 2, Passengers : 7
Cessna Citation II is a light corporate jet built by Cessna. Developed in the 1970s, it first flew on January 31 1977. The improved S550 Citation SII first flew on February 14 1984. Improvements included a new wing designed using supercritical technology and JT15D4B turbofans. The SII replaced the II in production from 1984, but the II returned to the lineup from late 1985. Both remained in production until the introduction of the Bravo.
Horsepower: 2500.0000, Gross Weight: 14100 lbs, Top Speed: kts, Empty Weight: 7706 lbs, Cruise Speed: 385 kts, Fuel Capacity: 5008.00 gal,
Rate Of Climb: 3050 fpm Rate of Climb (One Engine): 930 fpm, Ceiling: ft Ceiling (One Engine): 25200 ft
Special features / applications
In July 1975 Cessna announced it was developing a new piston twin suitable for airline, freight and corporate work, capable of taking off with a 1560kg (3500lb) payload from a 770m (2530ft) strip, similar in concept to the successful 402, but larger overall. The resulting aircraft was the Model 404 Titan, Cessna's largest piston engined twin developed thus far. It shares the same basic fuselage as the turbine powered 441 Conquest which was developed concurrently, but differs in having geared 280kW (375hp) piston engines and it is unpressurised. Other features include a bonded wet wing (then appearing on a number of 400 series Cessna twins) and the trailing link main undercarriage design shared with the Conquest.
The prototype Titan first flew on February 26 1975, production deliveries got underway in October the following year. Throughout the Titan's model life it was offered in three major versions, each differing in internal equipment fit. The Titan underwent minor modifications from 1980 when the wing span was increased and the wingtips redesigned, but production was to last for only another two years until 1982, by which time 378 had been built.
Specifications
Cessna 404 Titan Ambassador II
Horsepower: 375.0000 Gross Weight: 8400 lbs, Top Speed: 232 kts Empty Weight: 4965 lbs, Cruise Speed: 217 kts Fuel Capacity: 348.00 gal Stall Speed (dirty): 70 kts Range: 553 nm, Takeoff Landing - Ground Roll: 1788 ft Ground Roll 1100 ft,Over 50 ft obstacle: 2367 ft Over 50 ft obstacle: 2130 ft Rate Of Climb: 1575 fpm Rate of Climb (One Engine): 230 fpm Ceiling: 26000 ft Ceiling (One Engine): 10100 ft -->
The Cessna 208 Caravan first flew in 1982 and is now the mainstay of integrator feeder operations in the US domestic market. Cessna developed the original passenger- and cargo-carrying 208A into FedEx's Cargomaster. Cargomasters have higher weights, more cargo tie-down points, an underbelly cargo pannier, a taller fin and rudder, and new avionics. Cabin windows and the starboard rear door are deleted. At FedEx's request, Cessna also developed a larger 208B. Dubbed Super Cargomasters and entering service in October 1986, they have a 1.22m (4ft) fuselage stretch and can carry up to 1,910kg (4,215lb) of cargo. Some have a more powerful 503skW (675shp) engine, as fitted to the Cessna 208 Grand Caravan. By early 2002, Cessna had built more than than 1,000 208-based aircraft. All can operate from unprepared strips and require low maintenance.
Powerplant Top - 1 x 503skW (675shp) P&W Canada PT6A-114A turboprop - Max Take Off Weight: 3,970kg 8,750lb Max Landing Weight: 3,855kg 8,500lb - Max Zero Fuel Weight: 3,855kg 8,500lb - Structural Payload: 2,040kg 4,500lb Main Deck Useable Volume: 12m3 35ft3 4in3 - Wing Span: 15.8m 52ft 1in - Overall Length: 11.5m 37ft 7in Overall Height: 4.3m 14ft
