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First run in 1963 as a development of the IO-346, it has been produced in versions incorporating fuel injection (IO-520), turbo-charging (TSIO-520), and gearing (GTSIO-520). Design and development [ edit ]
The IOF-550 is an Aerosance FADEC equipped version of the same basic engine, the TSIO-550 is a dual turbocharged version and the TSIOL-550 is a liquid-cooled variant. [ 1 ] [ 2 ] [ 3 ] There is no O-550 engine, which would be a carburetor-equipped variant, hence the base model is the IO-550.
There was a TU206 turbocharged version powered by the Continental TSIO-520-C engine producing 285 hp (213 kW). After 1967, the turbo TU206 was powered by a TSIO-520-F of 300 hp (220 kW). The extra 15 hp (11 kW) was obtained by turning the engine at a higher rpm, and was allowed for only five minutes. [2]
Same as the TSIO-360-EB except for the increased power output rating. [5] TSIO-360-LB 210 hp (157 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-GB but with a larger throttle body, larger induction elbows, relocated overboost valve, magneto pressurization and an exhaust muffler. [5] TSIO ...
Cessna 414A Chancellor 414 Initial production variant, 516 built [5] 414A Chancellor Improved 414 with narrower vertical tail, longer span bonded wet wing without tip tanks, a lengthened nose, redesigned landing gear, and powered by two 310 hp (231kW) TSIO-520-N engines, 554 built.
Manufacturers have a team of technical engineers, writers and illustrators who compile information for these service manuals. Some companies create aftermarket repair manuals for the general public to purchase such as Clymer Haynes [1] and Triple M FZCO. [2] These manuals are also generally available as online auto repair manuals.
Data from Mooney website General characteristics Crew: one Capacity: 1,000 lb (454 kg) useful load or three passengers Length: 26 ft 8 in (8.13 m) Wingspan: 36 ft 6 in (11.13 m) Height: 8 ft 4 in (2.54 m) Empty weight: 2,380 lb (1,080 kg) Gross weight: 3,380 lb (1,533 kg) Max takeoff weight: 3,368 lb (1,528 kg) Powerplant: 1 × Continental TSIO-550-G air-cooled, 6-cylinder, horizontally ...
The main competitors are the Continental IO-520 and IO-550 series. An AEIO version was developed for high-performance competition aerobatics aircraft. Starting at 260 hp (190 kW) the power was eventually increased to 300 hp (220 kW). The AEIO-540 family has achieved considerable success in aircraft such as the Extra 300, CAP 232, and Zivko Edge 540