Cessna T207 Turbo Stationair 7: Difference between revisions
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Revision as of 12:41, 29 April 2025
Overview
The Cessna T207 Turbo Stationair 7 is a high-performance, turbocharged variant of the Stationair line, designed to carry up to seven occupants and cargo over rugged terrain with reliable, fixed landing gear. Introduced in the late 1960s, it served missions including passenger service, bush operations, and air cargo.
Specifications
- Engine: Continental TSIO-520-M, 310 hp
- Max Takeoff Weight: 3,800 lbs (1,724 kg)
- Empty Weight: 2,254 lbs (1,022 kg)
- Fuel Capacity: 61 gallons (231 liters)
- Length: 32 ft 2 in (9.80 m)
- Wingspan: 35 ft 10 in (10.92 m)
- Height: 9 ft 7 in (2.92 m)
Performance
- Cruise Speed: 161 knots (298 km/h)
- Maximum Speed: 170 knots (315 km/h)
- Stall Speed: 59 knots (109 km/h)
- Range: 583 nmi (1,080 km)
- Service Ceiling: 26,000 ft (7,925 m)
- Rate of Climb: 885 ft/min (4.5 m/s)
- Takeoff Distance: 1,100 ft (335 m)
- Landing Distance: 765 ft (233 m)
Operational Uses
Ideal for air taxi, remote area supply, and personal transport. Features a large cabin and cargo doors, with optional modern avionics upgrades.