Cessna T210 Turbo Centurion

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 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 that the NA 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 (1979–1985) is the most refined and most commonly traded variant, offering the best balance of systems maturity, useful load, and avionics provisions. Like the 210N, it benefits from the wider, deeper fuselage and bladder fuel tanks introduced in the late-1960s redesign.

Key Features for GA Buyers

Altitude performance. The TSIO-520-R maintains 310 HP to its critical altitude, allowing the T210 to cruise at 185–195 KTAS in the mid-teens on 14–16 GPH. This is the aircraft’s primary differentiator from the NA 210 and makes it genuinely competitive with light twins on block time for long trips.

Weather avoidance. The ability to cruise at FL180–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. Useful load of approximately 1,535 lbs allows four adults with full fuel and baggage on most trips — meaningful for the mission.

Shared 210 airframe. Operators transitioning from the NA 210 will 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, intercooler, and associated plumbing to the 210’s already complex maintenance profile. Budget meaningfully more for annuals than the NA 210 — $3,500–5,000+ is realistic on a well-maintained example.
• Shorter TBO. The TSIO-520-R carries a 1,400-hour TBO versus 1,700 hours for the IO-520-L. Overhaul costs run $28,000–40,000 at reputable shops — a higher per-hour reserve than the NA variant.
• Engine management discipline. Turbocharged Continentals require active management of cylinder head temperature (CHT) and turbine inlet temperature (TIT). Shock cooling during descent is a primary cause of premature cylinder failure. Buyers should confirm the previous owner managed the engine correctly — a borescope inspection is essential pre-purchase.
• Bladder tanks. Identical concern to the NA 210: deterioration with age and disuse, expensive to replace ($5,000–10,000 for the pair), and a frequent source of surprises.
• Cost of entry. Late-model T210N examples in good condition typically run $175,000–$275,000. Total annual operating costs for a 150-hour/year owner fall in the $40,000–60,000 range including all reserves — higher than the NA 210 primarily due to fuel burn and engine reserve.
• Oxygen required at altitude. Despite its high service ceiling, the T210 is unpressurized. Supplemental oxygen is required for all occupants above 12,500 ft MSL for extended operations, and recommended well before that on long legs.

See Also

• Cessna 210 Centurion — normally aspirated variant; lower operating costs and simpler powerplant, reduced altitude performance
• Riley Super P210 — pressurized Centurion derivative; eliminates the oxygen requirement for high-altitude operations