Description
Cessna 414 / 414A Aircraft Service Manual
SUPPLEMENTAL INSPECTION Manual
These are not Updated Manuals – they are For Reference ONLY!!!
Cessna 414 / 414A Aircraft Service Manual AMM
$35.00
1970
Thru
1985
MODEL 414 AND
414A CHANCELLOR
https://en.wikipedia.org/wiki/Cessna_414
The pressurized 414 was developed to appeal to owners of unpressurized, twin-engined aircraft, and was based on the fuselage of the Cessna 421 and used the wing design of the Cessna 401. The 414 is a low-wing cantilever monoplane with a conventional tail unit and a retractable tricycle landing gear. It is powered by two wing-mounted 310 hp (231 kW) Continental TSIO-520-J horizontally opposed, six-cylinder engines. The prototype, registered N7170C, first flew on 1 November 1968, and production aircraft were available in a number of optional seating arrangements and avionics packages. The name Chancellor was used for models marketed from 1976. An improved variant the Cessna 414A Chancellor was introduced in 1978 with the major change being a redesigned and increased-span wing with integral fuel tanks and an extended nose to give more baggage space.
