Origins and Development
The C-28 Titan is a light transport aircraft developed by the American company Cessna, based on the Cessna Model 404 Titan light passenger aircraft.
Operational History
Serial production of the aircraft began in 1976. The aircraft was used by the U.S. Navy in a liaison role.
Technical Specifications
| Modification | S-28 |
| Wingspan, m | 14.12 |
| Aircraft length, m | 12.04 |
| Aircraft height, m | 4.04 |
| Wing area, m2 | 22.48 |
| Empty weight | 2190 |
| Maximum takeoff weight | 3810 |
| Internal fuel, l | 1287 |
| Engine type | 2 Piston engine Teledyne Continental GTSIO-520-M |
| Power, hp | 2 x 375 |
| Maximum speed, km/h | 430 |
| Cruising speed, km/h | 404 |
| Practical range, km | 2810 |
| Practical ceiling, m | 7925 |
| Crew, crew members | 2 |
| Payload | 10 passengers |
Image and diagram gallery of the C-28 Titan
![]() C-28 Titan |
![]() C-28 Titan |
![]() C-28 Titan |
![]() C-28 Titan |
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APA: C-28 Titan (). C-28 Titan. wp.archivoaereo.com. https://wp.archivoaereo.com/en/c-28-titan-2/
VANCOUVER: C-28 Titan [online]. wp.archivoaereo.com; [cited 2026-06-17]. Available at: https://wp.archivoaereo.com/en/c-28-titan-2/




