Aircraft › Cessna › Cessna 404 Titan › Cessna 404 Titan
Cessna 404 Titan
The FAA approved the 404 Titan in July 1976. Its two Continental GTSIO-520-M engines are turbocharged and geared, rated at 375 horsepower, and turn three-blade McCauley propellers up to 90 inches across. The maximum take-off weight is 8,400 lb, or 3,810 kg, and the two wing tanks hold 344 US gallons of usable fuel on airplanes from serial number 404-0201. The data sheet allows from one to eleven seats, a number that includes the crew. Its ICAO code is C404. No acceptable source read gives its dimensions or speeds, so this page has no drawing.
- Engines
- Two piston engines on the wings: Continental GTSIO-520-M
- Max takeoff weight
- 8,400 lb (3,810 kg)
Photos from members
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Specifications
| Fuel capacity | 340 US gal (1,302 L) |
|---|---|
| Status | In service |
| Type codes | ICAO C404 |
Who flies it now
37 flights by other operators
From flights seen in US airspace in the last 14 days (public flight data).
In the air now
No aircraft of this type in the air right now
Flights of this type in the air now, from public flight data.