Piper PA-28-201T Turbo Dakota

Piper introduced the PA-28-201T Turbo Dakota in 1979 as a turbocharged variant of the PA-28-236 Dakota. The Turbo Dakota used a Continental TSIO-360-FB at 200 hp instead of the normally-aspirated Lycoming O-540-J3A5D in the standard Dakota. The choice of engine was unusual: Piper used a Continental in a Cherokee airframe that otherwise standardized on Lycoming powerplants. The TSIO-360 selection was driven by the desire to use a proven turbocharged engine that fit the Cherokee airframe envelope.

Production lasted one year. Piper built about 94 Turbo Dakotas before discontinuing the model. The reasons for the short production run included weak market demand (buyers in 1979 either wanted the normally-aspirated Dakota at lower cost or stepped up to the more capable Turbo Arrow IV for retractable-gear turbo capability), the unfamiliarity of the Continental engine in a Piper airframe, and the broader contraction of the GA market in the late 1970s and early 1980s.

The Turbo Dakota became a used-market curiosity after 1979. The small fleet has been well-maintained by enthusiast owners. Parts for the TSIO-360-FB engine remain reasonable through Continental, and airframe parts are common with other PA-28-236 Dakotas. Piper Owner Society covers the Turbo Dakota in its broader Dakota community resources. The airplane retains a small but devoted following among pilots who specifically value the turbocharged altitude capability in a four-seat Piper.

The Turbo Dakota cruises at about 156 KTAS at high-altitude cruise (12,000 to 15,000 ft) burning 12 gph of 100LL. At long-range cruise at lower altitudes, the airplane drops to about 140 KTAS on 10.5 gph. The turbocharger maintains rated power up to about 15,000 feet, giving the airplane meaningful altitude capability that the normally-aspirated Dakota lacks. Service ceiling is 20,000 ft on paper, though practical operations are limited to oxygen-equipped altitudes (typically 12,000 to 14,000 ft for non-IFR operations).

Useful load on a Turbo Dakota is about 1,100 to 1,200 pounds, slightly less than the normally-aspirated Dakota due to the turbo system weight. Full fuel (72 gallons usable) leaves about 750 to 850 pounds for people and bags. Four adults plus light luggage fits within gross with typical loading. Range with reserves is about 800 nm at long-range cruise. The Turbo Dakota's altitude capability is the airplane's defining feature and the reason buyers choose it over the normally-aspirated Dakota.

The Continental TSIO-360-FB is the engine on every Turbo Dakota. It's a six-cylinder, horizontally opposed, fuel-injected, turbocharged piston rated at 200 hp at 2,575 RPM. Continental's published TBO is 1,800 hours (2,000 hours for serial number 1006000 and later) per Continental Service Information Letter SIL 98-9E. The TSIO-360 family also powers the Mooney M20K, the Piper Seneca II/III/IV/V (in twin-engine configuration), and the Cessna T210K through T210L variants.

Field overhauls at Western Skyways, Mattituck, or other reputable Continental turbo shops run $40,000 to $58,000 in 2026 prices. The turbo system adds substantially to overhaul cost compared to non-turbocharged six-cylinders. Plan on additional $3,000 to $6,000 for turbocharger work at overhaul time. The TSIO-360 has accumulated decades of fleet experience across the Mooney 231/252 and Seneca families, so parts and shop expertise are reasonable.

Oil consumption on a healthy TSIO-360-FB runs about 0.4 to 0.6 quarts per hour. The engine demands disciplined CHT and TIT management during operation. Cylinder work at top-overhaul intervals (around 800 to 1,200 hours on hard-flown engines) is more common on turbo TSIO-360 variants than on normally-aspirated O-540 alternatives in the broader Cherokee family.

Plan on $175 to $245 per flight hour at 100 hours a year of utilization, all-in. The Turbo Dakota's operating cost runs about $25 to $35 above a normally-aspirated Dakota due to the turbo. Fuel and oil run about $66 to $84 per hour at 12 gph and $5.50 to $7 for 100LL. Engine overhaul reserve is $22 to $32 per hour based on a $40,000 to $58,000 overhaul amortized across the 1,800-hour TBO. Airframe maintenance reserve is $20 to $32 per hour, slightly higher than normally-aspirated Cherokees due to the turbo system inspection items.

Annual fixed costs (hangar, insurance, annual inspection) add another $45 to $80 per hour at 100 hours a year of utilization. Insurance on the Turbo Dakota is moderate. The turbo adds to underwriter risk calculations but the airplane is fixed-gear and four-seat, which keeps insurance below comparable retractable turbos. First-time turbo owners pay $2,800 to $5,500 a year typically. Established Turbo Dakota pilots pay $2,000 to $3,500.

Acquisition cost in mid-2026: A Turbo Dakota with mid-time engine and steam-gauge panel runs $80,000 to $110,000. A Turbo Dakota with fresh engine and modern Garmin panel runs $110,000 to $145,000. The market is small enough that pricing has wider variance than for higher-volume Cherokees.

Piper Owner Society covers the Turbo Dakota in its broader Dakota community. Annual dues are about $80. The Turbo Dakota's small fleet means community knowledge is meaningfully thinner than for high-volume Cherokees. Owners often consult Mooney M20K resources for TSIO-360 engine operating guidance.