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The Model 401 was a derivative of the Cessna
411. Lighter, and cheaper to operate, it was specifically aimed at the
business market. The Model 401A (132 built) had minor improvements and
was followed by the Model 401B (91 built) with minor changes. Production
ended in 1972 and many are still in use.
G-ROAR
c/n 401-0166
USA
8 seat business aircraft first flown in 1965
Engines: 2X 300hp(223kW) Continental TSIO-520-E
Length: 33’9"(10.28m)
Height: 11’8"(3.55m)Wingspan: 39’10"(12.14m)
No.built: 183 Range: 1180miles(1899km)
Cruising speed: 215mph(346kmh) Empty weight: 3665lb(1664kg)
Maximum take-off weight: 6300lb(2860kg)
An example of the Cessna 401A
is illustrated below.
C-GJGC
c/n 401A-0025
A Cessna 401B is illustrated below.
C-GCXN c/n 401B-0003 |
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