Cessna T207 Turbo Stationair 7: Difference between revisions

From AviationSafetyX Wiki
Jump to navigation Jump to search
← Older edit
VisualWikitext
No edit summary
No edit summary
 
(2 intermediate revisions by 2 users not shown)
Line 1: Line 1:
The Cessna T207 Turbo Stationair 7 is a seven-seat, single-engine, high-wing aircraft equipped with a turbocharged engine, known for its versatility and ruggedness. It's widely used for bush flying, cargo hauling, and general aviation, especially in remote areas.
[[File:N91025a 300.jpg|thumb|right|375px|Cessna T207 Turbo Stationair 7]]
== 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.


== Key Features and Specifications ==
== Specifications ==
* '''Engine:''' Turbocharged Continental TSIO-520-M engine, up to 310 horsepower.
* '''Engine''': Continental TSIO-520-M, 310 hp
* '''Capacity:''' Seats up to seven passengers.
* '''Max Takeoff Weight''': 3,800 lbs (1,724 kg)
* '''Range:''' Approximately 671 miles.
* '''Empty Weight''': 2,254 lbs (1,022 kg)
* '''Service Ceiling:''' 26,000 feet above sea level.
* '''Fuel Capacity''': 61 gallons (231 liters)
* '''Performance:''' 810 ft/min climb rate, top speed of 196 mph.
* '''Length''': 32 ft 2 in (9.80 m)
* '''Dimensions:''' Length: 32 ft 2 in, Height: 9 ft 7 in, Wingspan: 36 ft.
* '''Wingspan''': 35 ft 10 in (10.92 m)
* '''Utility:''' Ideal for short field operations and bush flying.
* '''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.
 
[[Category:Cessna aircraft]]
[[Category:Single-engine aircraft]]
[[Category:Turboprop aircraft]]
[[Category:ASX Aircraft Pages]]

Latest revision as of 12:58, 29 April 2025

Cessna T207 Turbo Stationair 7

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.

Retrieved from "https://wiki.alsresume.com/index.php?title=Cessna_T207_Turbo_Stationair_7&oldid=30927"