Cessna 414A Chancellor Wallpapers

Cessna 414A Chancellor aircraft, Megawallpapers: The Cessna 414 is a light, twin-engine personal transport aircraft built by Cessna from 1968 until the mid 1980s, when decreased demand across the general aviation industry forced nearly all manufacturers to cut down on production models. It remains a popular aircraft on the used market. A model featuring geared engines is the Cessna 421. [br]The Cessna 421 Golden Eagle is a development of the earlier Cessna 414 light, twin-engine personal transport aircraft. The main difference is the switch to geared engines rather than the traditional direct drive models, meaning that rather than the drive shaft being direct connected to the propellor, they are connected through a series of reduction gears. This further meant that the engines had to operate at different RPM settings from traditional engines; this led to a number of complaints regarding the longetivity of the engines as pilots often ignored these special needs. Nevertheless the aircraft remains a popular high-performance pressurized personal aircraft despite continuing high prices and the fact that production ended in the 1980s due to decreased demand across the general aviation industry. [br]The 421 was first produced in 1968 and was redesigned in 1970 (421B). In 1976 the 421C appeared which featured "wet wings" (sealed wings holding fuel) and the absence of wing tip fuel tanks. Some Cessna 421 aircraft have been modified to accept turboprop engines. [br]Powerplants: [br] 421A - Two 280kW (374hp) Continental GTSIO-520-D geared, turbocharged and fuel injected flat six piston engines, driving three blade constant speed McCauley propellers. [br]414A - Two 230kW (310hp) TSIO-520-NBs. [br]Performance: [br]421A - Max speed 444km/h (240kt), max cruising speed 420km/h (227kt), long range cruising speed 364km/h (197kt). Initial rate of climb 1680ft/min. Service ceiling 27,000ft. Range with no reserves and standard fuel 1570km (847nm), with optional fuel 2756km (1488nm). [br]414A - Max speed 436km/h (235kt), cruising speed 420km/h (227kt), economical cruising speed 340km/h (183kt). Initial rate of climb 1520ft/min. Service ceiling 30,800ft. Range with reserves at economical cruising speed 2460km (1327nm), at max cruising speed 2036km (1100nm). [br]Weights: [br] 421A - Empty equipped 2132kg (4700lb), max takeoff 3103kg (6840lb). [br]414A - Empty 1976kg (4356lb), max takeoff 3062kg (6750lb). [br]Dimensions: [br]421A - Wing span 12.15m (39ft 10in), length 10.29m (33ft 9in), height 3.56m (11ft 8in). Wing area 18.6m2 (200sq ft). [br]414A - Wing span 13.45m (44ft 2in), length 11.09m (36ft 5in), height 3.49m (11ft 6in). Wing area 21.0m2 (225.8sq ft). [br]Capacity: [br]Standard seating for six, optional seating for eight in 421 and 414A, seven in 414. [br] [br] [br]

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Cessna 414A Chancellor Wallpapers @ Mega Wallpapers (08 Edition)
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