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Cessna 402

General Aviation and Light Aircraft

The Cessna 401 and 402 are a series of six to ten seat light twin-piston aircraft whose seats are easily removable so that the cabin can be used for cargo. Neither is pressurized nor particularly fast for its installed power; Cessna intended them to be inexpensive to buy and operate, a workhorse for cargo operators and small commuter airlines, and developed them from the Cessna 411 to improve on its poor single-engine handling and avoid its expensive geared engines. They are powered by turbocharged Continental engines of 300 horsepower with three-bladed constant-speed propellers. The 402 was introduced in 1967 with a large cargo door, the 401 was the version without it, and the nose was stretched in 1969 to create the 402A, followed by the 402B in 1970 with optional larger fuel tanks.

Facts
Year
1967 1
Engine Class
Piston 1
Top Speed (km/h)
428 1
Mass (kg)
1849 1
Maximum Mass (kg)
3107 1
Engine
2 x Continental TSIO-520-VB air-cooled turbocharged flat-six engines, 325 hp each 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Source Cessna 402 (Wikipedia)

Of Make

Source Cessna 402 (Wikipedia)
Sources
1. Cessna 402 (Wikipedia)
  • Development, introduction
    The original Cessna 402 was introduced in 1967. A version without the large cargo door called the Cessna 401 was produced at the same time.
  • Specifications (402C Businessliner)
    Powerplant: 2 × Continental TSIO-520-VB air-cooled turbocharged flat-six engines, 325 hp (242 kW) each
  • Specifications (402C Businessliner), empty weight
    Empty weight: 4,077 lb (1,849 kg)
  • Specifications (402C Businessliner), maximum takeoff weight
    Max takeoff weight: 6,850 lb (3,107 kg)
  • Specifications (402C Businessliner), maximum speed
    Maximum speed: 231 kn (266 mph, 428 km/h) at 16,000 ft (4,900 m)
  • Lead
    The Cessna 401 and 402 are a series of 6 to 10 seat, light twin-piston engine aircraft.
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