Cessna 404 Titan

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Cessna 404 Titan
Role Light passenger/cargo aircraft
National origin United States
Manufacturer Cessna
First flight February 26, 1975
Introduction 1976
Produced 1976–1982
Number built 396
Developed from Cessna 402
Developed into Reims-Cessna F406 Caravan II
Cessna 441 Conquest II

The Cessna Model 404 Titan is an American twin-engined, light aircraft built by Cessna Aircraft. It was the company's largest twin piston-engined aircraft at the time of its development in the 1970s. Its US military designation is C-28, and Swedish Air Force designation Tp 87.[1]

Design and development

The aft doors on the left side

The Cessna 404 was a development of the

Continental Motors GTSIO-520 piston engines. Two versions were offered originally; the Titan Ambassador passenger aircraft for ten passengers, and the Titan Courier utility aircraft for passengers or cargo. By early 1982 seven different variants were available, including a pure cargo version, the Titan Freighter. The Freighter was fitted with a strengthened floor, cargo doors, and its interior walls and ceiling were made from impact-resistant polycarbonate
materials to minimize damage in the event of cargo breaking free in-flight.

Variants

Operators

Civilian operators

 Australia
 United States
 United Kingdom
  • Air UK

Military operators

 Bahamas
 Bolivia
 Colombia
 Dominican Republic
  • Dominican Republic Air Force[5]
 Hong Kong
 Jamaica
 Mexico
 Nicaragua
 Sweden
 Tanzania
 United States
 Puerto Rico

Specifications (Ambassador I)

Data from Jane's All the World's Aircraft 1980–81[11]

General characteristics

  • Crew: 2
  • Capacity: 6–8 passengers
  • Length: 39 ft 6+14 in (12.046 m)
  • Wingspan: 46 ft 8+14 in (14.230 m)
  • Height: 13 ft 3 in (4.04 m)
  • Wing area: 242.0 sq ft (22.48 m2)
  • Aspect ratio: 9.0:1
  • Empty weight: 4,816 lb (2,185 kg)
  • Max takeoff weight: 8,400 lb (3,810 kg)
  • Fuel capacity: 340 US gal (280 imp gal; 1,300 L)

Performance

  • Maximum speed: 267 mph (430 km/h, 232 kn) at 16,000 ft (4,900 m)
  • Cruise speed: 188 mph (302 km/h, 163 kn) (econ cruise) at 20,000 ft (6,100 m)
  • Stall speed: 81 mph (130 km/h, 70 kn) flaps down, power off
  • Never exceed speed: 274 mph (441 km/h, 238 kn) (Calibrated airspeed)
  • Range: 2,120 mi (3,410 km, 1,840 nmi)
  • Service ceiling: 26,000 ft (7,900 m)
  • Rate of climb: 1,575 ft/min (8.00 m/s)
  • Take-off run to 50 ft (15 m): 2,367 ft (721 m)
  • Landing run from 50 ft (15 m): 2,130 ft (650 m)

See also

Cessna 421
(right) with round windows

Related development

Aircraft of comparable role, configuration, and era

References

  1. ^ Urban Fredriksson (October 4, 2006). "Swedish Military Aircraft Designations". Retrieved September 26, 2012.
  2. ^ Johnson 2013, p. 375
  3. ^ Hagedorn 1993, p. 140
  4. ^ Gaines Flight International 6 November 1982, p. 1386
  5. ^ Hagedorn 1993, p. 111
  6. ^ Air International April 1986, p. 170
  7. ^ Hagedorn 1993, p. 138
  8. ^ ANUARIO LATINOAMERICANO DE DEFENSA 2020. Grupo Edefa. 2020. p. 176.
  9. ^ "FDRA - Fuerza Aérea: Fuerzas Aéreas: Fuerza Aérea - Ejército de Nicaragua". December 2015.
  10. ^ Gaines Flight International 6 November 1982, p. 1374
  11. ^ Taylor 1980, pp. 326–327

External links