C-28 Titan
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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
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CessnaUnited States
ArchivoAéreo Editorial Team
A group of aviation researchers and enthusiasts dedicated to documenting and preserving global aeronautical history. All articles are reviewed to ensure historical accuracy.
Sources & Accuracy
The information presented in this technical sheet has been compiled from declassified flight manuals, historical archives, and specialized literature. While we strive for maximum accuracy, some performance data may vary depending on the specific variant or operational conditions.