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Cessna 404 Flight Manual

  1. Cessna 404 Titan For Sale
  2. Cessna 404 Performance
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CESSNA 404 TITAN AMBASSADOR 1980 SPECIFICATIONS

1.1 History of the flight On 11 August 2003, at about 1535 Western Standard Time, a Cessna Aircraft Company 404 Titan (C404) aircraft, registered VH-ANV, took off from runway 24 right (24R) at Jandakot Airport, WA. One pilot and five passengers were on board the aircraft. The flight was being. This is library of Cessna 404 manuals on a AUTORUN MENU DRIVEN CD. Covers all 404 series 1977 - 1981 Titan Ambassador, freighter Courier. These manuals are on a CD in PDF format so you can view zoom and print any or all pages for a perfect copy of the original document. Cessna 404 Parts manual P559-13-12. Cessna 404 maintenance service Manual D2517-15-13. A/C and other misc manuals.

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:
Landing ground roll:
Landing over 50-foot obstacle:
Service ceiling:
Single-engine service ceiling:
Source: Cessna Aircraft
404

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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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