Cessna 404 Titan

Airplanes

Length

11.8872 m

Flat Wing Span

14.0208 m

Height

3.9624 m

Flat Wing Area

22.48 m²

Flat Wing Aspect Ratio

Max Seating

Cruise Speed

301.8757 km/h

Max Speed

429.6636 km/h

Max Ceiling

7924.8 m

Number of Engines

First Flight

1975-02-26

Entry Into service

1976-01-01

Number Built

396

Maximum Take-Off Weight

3.8102 t (paragliders: kg)

Total Fuel Capacity

1287.04

Maximum Range

3407.68 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Cessna 404 Titan	3.8102	1287.04	3407.68

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Tecnam P2012 Traveller		11.8	14	9	Compare
Scaled Composites Triumph	Williams FJ44	11.8872	14.6304		Compare
Rockwell 685	Continental IO-520	12.8016	14.0208	8	Compare
Piaggio P.166		11.88	13.51	8	Compare
Cessna 425	Pratt & Whitney Canada PT6	10.668	13.4112		Compare
Percival Merganser	De Havilland Gipsy Queen	11.8872	14.3256	5	Compare

All data (27 fields)

Name: Cessna 404 Titan
Manufacturer: Cessna Aircraft Company
Description: The Cessna 404 Titan is an American twin-engined, light aircraft built by Cessna Aircraft.
ICAO Code: C404
First Flight: 1975-02-26
Entry Into service: 1976-01-01
Production End: 1982-01-01
Designer: Cessna Aircraft Company
Type: Light passenger/cargo aircraft
Length (m): 11.8872
Height (m): 3.9624
Cockpit Crew: 2
Max Seating: 8
Max Speed (km/h): 429.6636
Cruise Speed (km/h): 301.8757
Min Speed (km/h): 129.6399
Max Ceiling (m): 7924.8
Rate of Climb (m/s): 8.001
Capacity Description: 6–8 passengers
National Origin: United States of America
Number Built: 396
Wikipedia Article (URL): en.wikipedia.org/wiki/Cessna_404_Titan
Flat Wing Span (m): 14.0208
Flat Wing Area (m²): 22.48
Flat Wing Aspect Ratio: 9
Wake Category: L
Number of Engines: 2