Cessna 404 Flight Manual

The Cessna 404 produced by Cessna. Specs, range, speed, operating weights and performance for the Cessna 404 here. C404, Kulusuk Greenland, 2002 (On 1 August 2002, a Cessna 404, en-route at FL130 over Greenland, experienced sudden power loss on both engines, probably as a result of ice in the induction systems, leading to loss of control. The crew regained control at 3000 feet.

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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

Propellers:

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

Engine TBO:

Length:

Wingspan:

Height:

Wing area:

Seating capacity:

Standard empty weight:

Max. takeoff weight:

Landing weight:

Max. useful load:

Baggage allowance:

PERFORMANCE

Max. speed:

Cruise speed (at 10,000 feet):

Cruise speed (at 20,000 feet):

Stall speed (flaps up, power off):

Stall speed (flaps down, power off):

Rate of climb at sea level:

Rate of climb (one engine):

Takeoff ground roll:

Takeoff over 50-foot obstacle:

Cessna Flight Training Center

Landing ground roll:

Landing over 50-foot obstacle:

Service ceiling:

Single-engine service ceiling:

Cessna 402 Flight Manual

Source: Cessna Aircraft