Overview

The Cessna T210 Turbo Centurion is the turbocharged variant of the Cessna 210 family, produced alongside the normally aspirated 210 from 1966 to 1986. Where the naturally aspirated 210 Centurion is a capable mid-altitude cross-country aircraft, the T210 is built for the flight levels: the Continental TSIO-520-R maintains rated power to altitude, enabling cruise in the mid-teens to low twenties with true airspeeds the normally aspirated variant cannot approach. It shares the 210’s cantilever high wing, hydraulic retractable gear, and six-seat cabin, adding the complexity of a turbocharged powerplant.

The T210N (1979 to 1985) is the most developed variant of the line, with mature systems, strong useful load, and good avionics provisions. Like the 210N, it benefits from the wider, deeper fuselage and bladder fuel tanks introduced in the late-1960s redesign. Choose the Cessna T210 Turbo Centurion when you need flight-levels cruise and weather-topping reach in a six-seat single, and you will fly it high enough, often enough, to justify the turbo system’s added cost and management discipline over the normally aspirated 210.

Key Features for GA Buyers

• Altitude performance. The TSIO-520-R maintains 310 hp to its critical altitude, allowing the T210 to cruise at 185 to 195 KTAS in the mid-teens on 14 to 16 GPH. This is the aircraft’s primary differentiator from the NA 210.
• Weather avoidance. The ability to cruise at FL180 to FL200 puts the T210 above a significant fraction of en-route weather. Combined with a capable IFR platform and good useful load, it becomes a serious cross-country tool for instrument-rated owners flying in varied conditions.
• Six-seat cabin and useful load. A useful load around 1,535 lb lets four adults fly with full fuel and baggage on most trips, meaningful for the mission, and the 4,000 lb gross gives the T210N a touch more weight margin than the NA 210.
• Shared 210 airframe. Operators transitioning from the NA 210 find identical handling, the same gear system, and the same bladder tank configuration. The airframe differences are minor; the powerplant is the substantive change.

Trade-offs

• Turbo system complexity and cost. The TSIO-520-R adds a turbocharger, wastegate, and associated plumbing to the 210’s already complex maintenance profile. Budget meaningfully more for annuals than the NA 210; $3,500 to $5,000 or more is realistic on a well-maintained example.
• Shorter TBO and higher reserve. The TSIO-520-R carries a 1,400-hour TBO versus 1,700 for the IO-520-L, and the catalogue reserves a standard-shop overhaul of about $56,000, so the per-hour engine reserve runs higher than the NA variant.
• Engine management discipline. Turbocharged Continentals demand active management of cylinder head temperature and turbine inlet temperature. Shock cooling during descent is a primary cause of premature cylinder failure. Confirm the previous owner managed the engine correctly; a borescope is essential at pre-purchase.
• Bladder tanks. Identical concern to the NA 210: deterioration with age and disuse, expensive to replace at $5,000 to $10,000 for the pair, and a frequent source of surprises.
• Oxygen required at altitude. Despite its high service ceiling, the T210 is unpressurised. Supplemental oxygen is required for the crew above 12,500 ft for extended operations and for all occupants above 14,000 ft, and it is worth using well before that on long legs.

See Also

• Cessna 210 Centurion – the normally aspirated sibling; lower operating cost and a simpler powerplant, reduced altitude performance. Compare
• Riley Super P210 – the pressurised Centurion derivative; eliminates the oxygen requirement for high-altitude cruise. Compare
• Beechcraft Bonanza A36 – the low-wing six-seat benchmark; club cabin and refined handling, normally aspirated. Compare
• Cessna 206 Stationair – the fixed-gear six-seat hauler; simpler systems and more payload, slower and lower. Compare