Cessna 404 Flight Manual

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The 404’s flaps, landing gear and wet wing would all be used on future Cessna aircraft including Citations. This stable airplane received a vertical tail that spans 7.6 feet, and the rudder trim tab has 4:1 servo. The Titan was fitted with two 375 hp GTSIO-520-M engines, with no intercooler or cowl flaps. CESSNA AIRCRAFT MANUALS - 404 The handbook is designed To help you operate your plane with safety and confidence. To more fully acquaint you with the basic performance and handling characteristics of the airplane.

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ABOUT THIS AIRCRAFT

The 404 Titan remains Cessna�s largest twin-piston-engine aircraft, since the time of its development in the 70s, with the ability to seat up to nine passengers. The Titan underwent minor modifications from 1980. These included a redesign of the wingtips, increasing the wing span and adding features, such as a pressurised cabin and optional lavatory. The 421 was first produced in 1967, followed by the 421C Golden Eagle in 1975. The latter was developed with a pressurised cabin, the absence of wingtip fuel tanks and landing gear which was altered from straight-leg to a trailing-link design. Production ended in 1985, after 1,901 aircraft had been delivered.

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CESSNA 404 TITAN AMBASSADOR 1980 SPECIFICATIONS

GENERAL CHARACTERISTICS

Powerplant:

(2) Continental Motors GTSIO-520-M engines, 375 hp each

Cessna 404 Performance

Propellers:

Constant speed, full feathering, three-blade, 90 inch propellers

Engine TBO:

Length:

Wingspan:

Height:

Wing area:

Seating capacity:

Standard empty weight:

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Max. takeoff weight:

Landing weight:

Max. useful load:

Baggage allowance:

PERFORMANCE

Max. speed:

Cessna 404 Titan Fsx

Cruise speed (at 10,000 feet):

Cruise speed (at 20,000 feet):

Stall speed (flaps up, power off):