Continental IO-360

History

The IO-360 was first certified by the Federal Aviation Administration on 15 May 1962 to the CAR 13 certification standard, effective June 15, 1956, as amended by 13-1 thru 13–3. The engine is produced by Continental under Production Certificate No. 508.

The turbocharged TSIO-360 series was first certified on 11 October 1966 to the Federal Aviation Regulations Part 33 standard effective February 1, 1965, as amended by 33–1. This series is manufactured under Production Certificate No. 7, except the TSIO-360-D which is under Production Certificate No. 508.

Variants

IO-360

;IO-360-A :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Base IO-360 model: a six-cylinder air-cooled, horizontally opposed direct drive, fuel injected engine. Uses a TCM 639230A3 fuel injector. The crankshaft has two 6th order dampers. ;IO-360-AB :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639230A3 fuel injector. Same as the IO-360-A except for modified crankshaft. The crankshaft has one 6th and one 4½ order damper.

;IO-360-AF :180 hp, designed to run on lower octane fuels such as the proposed 94UL avgas. The designation of "AF" stands for alternative fuel. The version incorporates lower-compression pistons, giving a 7.5 to 1 compression ratio and a revised fuel injection system. ;IO-360-B :180 hp at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 6.0:1. Uses a TCM 639230A3 or 6006 fuel injector. Same as IO-360-A except for reduced compression ratio and rated power. The crankshaft has two 6th order dampers. ;IO-360-C :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-D except for accessory drive provisions. The crankshaft has two 6th order dampers. ;IO-360-CB :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-C except for modified crankshaft. The crankshaft has one 6th and one 4½ order damper. ;IO-360-D :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-A except for power rating and oil cooled pistons. The crankshaft has two 6th order dampers. ;Rolls-Royce Continental IO-360-D :Licence production in the United Kingdom by Rolls-Royce ;IO-360-DB :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-D except for modified crankshaft. The crankshaft has one 6th and one 4½ order damper. ;IO-360-E :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-D except for oil sump and suction tube. The crankshaft has two 6th order dampers.

;IO-360-ES :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Same as the IO-360-HB except for the modified spider induction system and the use of a TCM 639289A95 fuel injector. The crankshaft has one 6th and one 4½ order damper. ;IO-360-G :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-C except for crankshaft counterweight tuning. The crankshaft has one 6th and one 4½ order damper. ;IO-360-GB :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-G except for modified crankshaft. The crankshaft has one 6th and one 4½ order damper. ;IO-360-H :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-D except for crankshaft counterweight tuning. The crankshaft has one 6th and one 4½ order damper. ;IO-360-HB :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-H except for modified crankshaft. The crankshaft has one 6th and one 4½ order damper. ;IO-360-J :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-H except for power rating. The crankshaft has one 6th and one 4½ order damper. ;IO-360-JB :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-J except for modified crankshaft. The crankshaft has one 6th and one 4½ order damper. ;IO-360-K :195 hp at 2600 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-H except for power rating. The crankshaft has one 6th and one 4½ order damper. ;IO-360-KB :195 hp at 2600 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-K except for modified crankshaft. The crankshaft has one 6th and one 4½ order damper.

TSIO-360

;TSIO-360-A :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Base TSIO-360 model: a six-cylinder air-cooled, horizontally opposed direct drive, fuel injected, tuned induction, turbocharged engine with internal piston cooling oil jets. ;TSIO-360-AB :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-A except for a modified crankshaft. ;TSIO-360-B :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-A except for accessory drive provisions. ;TSIO-360-BB :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-B except for modified crankshaft and different dampers. ;TSIO-360-C :225 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-A except for rating, crankshaft dampers provision for cabin pressurization. ;TSIO-360-CB :225 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-C except for a modified crankshaft. ;TSIO-360-D :225 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-C except for cabin pressurization. ;TSIO-360-DB :225 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-D except for a modified crankshaft. ;TSIO-360-E :215 hp at 2575 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-C except for rating, engine mounted turbocharger, freon compressor drive and cabin pressurization. ;TSIO-360-EB :215 hp at 2575 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-E except for a modified crankshaft. ;TSIO-360-F :200 hp at 2575 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-E except for the power output rating and the exhaust system configuration. ;TSIO-360-FB :200 hp at 2575 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-F except for a modified crankshaft. ;TSIO-360-G :210 hp at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-E except for the power output rating and the exhaust system configuration. ;TSIO-360-GB :210 hp at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-G except for a modified crankshaft. ;TSIO-360-H :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-G except for rating and cabin pressurization. ;TSIO-360-HB :210 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-H except for a modified crankshaft. ;TSIO-360-JB :225 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-HB except for the increased power output rating. ;TSIO-360-KB :220 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-EB except for the increased power output rating. ;TSIO-360-LB :210 hp 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. ;TSIO-360-MB :210 hp at 36" mp and 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-LB except for intercooler, wastegate controller, maximum manifold pressure, and cluster manifold. ;TSIO-360-NB :210 hp at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-LB except for an intercooler. ;TSIO-360-PB :200 hp at 2600 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-MB but not equipped with an intercooler. ;TSIO-360-RB :220 hp at 2600 rpm, Minimum fuel grade 100 or 100LL avgas, RH95/130 or B95/130 CIS, compression ratio 7.50:1. Same as the TSIO-360-KB except the manifold pressure is controlled with a wastegate controller, an intercooler is installed in the induction system, and uses a Precision Airmotive RSA-5AD2 fuel injection servo. ;TSIO-360-SB :220 hp at 39" mp and 2600 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-MB except for the manifold pressure, RPM, and power output rating.

LTSIO-360

;LTSIO-360-E :215 hp at 2575 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-E except for direction of rotation. ;LTSIO-360-EB :215 hp at 2575 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the LTSIO-360-E except for a modified crankshaft. ;LTSIO-360-KB :220 hp at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the LTSIO-360-EB except for the increased power output rating. ;LTSIO-360-RB :220 hp at 2600 rpm, Minimum fuel grade 100 or 100LL avgas, RH95/130 or B95/130 CIS, compression ratio 7.50:1. Same as the TSIO-360-RB except for direction of rotation.

Applications

• Aero Boero AB-210
• AVE Mizar
• Beriev Be-103
• Cessna 160
• Cessna R172K Hawk XP
• Cessna Skymaster and military O-2 Skymaster
• Cirrus SR20
• Cierva CR Twin
• Flight Design C4
• Goodyear GZ-20
• Ilyushin Il-103
• Irkut A-002
• Maule M-4
• Maule M-5
• Mooney M20
• PAC CT/4
• Piper PA-28R-201T Turbo Arrow
• Piper PA-28-201T Turbo Dakota
• Piper PA-34 Seneca
• PZL M-20 Mewa
• Reims FR172J Reims Rocket
• Ryan XV-8
• Sasin Spraymaster
• T-41 Mescalero
• White Lightning WLAC-1

Specifications (IO-360-A)

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References

Notes

Bibliography

• Taylor, J.W.R. (ed.). Jane's All the World's Aircraft 1976-77. London: Jane's, 1976. .

References

1. AvWeb Staff. (December 2010). "Teledyne-Continental Bought by Chinese Interests". AvWeb.
2. Teledyne Technologies Incorporated. (December 2010). "Teledyne Technologies Agrees to Sell Teledyne Continental Motors to AVIC International". Business Wire.
3. Taylor 1976, pp. 792–793
4. Federal Aviation Administration. (September 2007). "Type Certificate Data Sheet No. E1CE Revision 15".
5. Federal Aviation Administration. (July 2008). "Type Certificate Data Sheet No. E9CE Revision 20".
6. Bertorelli, Paul. (September 2011). "Continental Introduces New Lower-Octane Engine". AVweb.