The Textron Aviation 210 T210N Turbo Centurion II is a high-performance, single-engined, high-wing light aircraft featuring retractable landing gear and seating for six occupants. Designed for general-aviation pilots seeking high-speed travel and utility, the aircraft combines a spacious cabin layout with advanced turbocompression.
The type underwent substantial design evolution across its production run, transitioning from an initial four-seat configuration derived from earlier models to a wider fuselage, cantilever wing design, and tubular steel landing gear struts that accommodated full-sized rear seats. Offered in normally aspirated, turbocharged, and pressurized variants, the aircraft became a staple of private aviation until production concluded. Operational service has seen the issuance of multiple airworthiness directives and mandatory service inspections concerning structural integrity and fatigue cracking within the wing spar and carry-through components.
Engines fitted
174 aircraft
Engine
Power
Share of fleet
Aircraft
Continental IO-470
260 hp
161
Continental IO-520
285 hp
6
Continental O-470
230 hp
4
Continental TSIO-520
300 hp
3
This page covers the Cessna 210-5, 210-5(205), 210-5A, 210-5A(205A), 210A, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, 210K, 210L, 210M, 210N, 210R, Cessna 210: the same aircraft under other designations.