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Continental IO-550

February 26, 2023

The Continental IO-550 engine is a large family of 9 liter fuel injected six-cylinder, horizontally opposed, air-cooled aircraft engines that were developed for use in light aircraft by Teledyne Continental Motors. The first IO-550 was delivered in 1983 and the type remains in production.[1][2]

IO-550
Continental TSIO-550-C engine installation in a Cessna 400
Type Piston aircraft engine
National origin United States
Manufacturer Teledyne Continental Motors
First run 1983
Major applications Velocity XL
Cirrus SR22
Cessna TTx
Mooney M20
Bellanca Viking
Beechcraft Baron
Beechcraft Bonanza
Produced 1983-present
Developed from Continental O-520

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.[1][2]

This engine family competes with the Lycoming IO-580 series which are also six-cylinder engines with similar power output and weight.[4]

Design and development

The IO-550 family of engines was developed from the IO-520 series, with the stroke increased from 4.00 to 4.25 inches, increasing the displacement to 552 in³ (9.05 L). The engine family covers a power range from 280 hp (209 kW) to 360 hp (268 kW).[1][2]

The engines were first developed in the early 1980s and first certified on a regulatory basis of FAR 33, 1 February 1965 amendment, 33-8, 2 May 1977. The first IO-550 model was certified on 13 October 1983.[1][2]

Variants

IO-550-A
300 hp (224 kW) at 2700 rpm, dry weight 430.72 lb (195.37 kg). Certified 13 October 1983.[1]
IO-550-B
300 hp (224 kW) at 2700 rpm, dry weight 421.61 lb (191.24 kg). Certified 13 October 1983.[1]
IO-550-C
300 hp (224 kW) at 2700 rpm, dry weight 433.20 lb (196.50 kg). Certified 13 October 1983.[1]
IO-550-D
300 hp (224 kW) at 2700 rpm, dry weight 437.1 lb (198.3 kg). Certified 23 June 1988.[1]
IO-550-E
300 hp (224 kW) at 2700 rpm, dry weight 450.50 lb (204.34 kg). Certified 20 December 1989.[1]
IO-550-F
300 hp (224 kW) at 2700 rpm, dry weight 437.1 lb (198.3 kg). Similar to the IO-550-A,B & C, with a top-mounted induction system and 12-quart oil sump. Certified 23 June 1988.[1]
IO-550-G
280 hp (209 kW) at 2500 rpm, dry weight 428.97 lb (194.58 kg). Certified 17 March 1989.[1]
IO-550-L
300 hp (224 kW) at 2700 rpm, dry weight 438.5 lb (198.9 kg). Certified 23 June 1988.[1]
IO-550-N
310 hp (231 kW) at 2700 rpm, dry weight 429.97 lb (195.03 kg). Similar to the IO-550-G with increased power rating. Certified 16 August 1996.[1]
IO-550-P
310 hp (231 kW) at 2700 rpm, dry weight 429 lb (195 kg). Similar to the IO-550-N with oil sump from the IO-550-L. Certified 1 March 2000.[1]
IO-550-R
310 hp (231 kW) at 2700 rpm, dry weight 439.5 lb (199.4 kg). Similar to the IO-550-N but with the oil sump, oil suction tube and mount legs from the IO-550-B. Certified 1 March 2000.[1]

FADEC models

IOF-550-B
300 hp (224 kW) at 2700 rpm, dry weight 447.1 lb (202.8 kg). Similar to the IO-550-B with an Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.[1]
IOF-550-C
300 hp (224 kW) at 2700 rpm, dry weight 453.2 lb (205.6 kg). Similar to the IO-550-C with an Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.[1]
IOF-550-D
300 hp (224 kW) at 2700 rpm, dry weight 455.0 lb (206.4 kg). Similar to the IO-550-D with an Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.[1]
IOF-550-E
300 hp (224 kW) at 2700 rpm, dry weight 462.8 lb (209.9 kg). Similar to the IO-550-E with an Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.[1]
IOF-550-F
300 hp (224 kW) at 2700 rpm, dry weight 460.1 lb (208.7 kg). Similar to the IO-550-F with an Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.[1]
IOF-550-L
300 hp (224 kW) at 2700 rpm, dry weight 455.0 lb (206.4 kg). Similar to the IO-550-L with an Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.[1]
IOF-550-N
310 hp (231 kW) at 2700 rpm, dry weight 460.0 lb (208.7 kg). Similar to the IO-550-N with an Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.[1]
IOF-550-P
310 hp (231 kW) at 2700 rpm, dry weight 460.0 lb (208.7 kg). Similar to the IO-550-P with an Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.[1]
IOF-550-R
310 hp (231 kW) at 2700 rpm, dry weight 470.5 lb (213.4 kg). Similar to the IO-550-R with an Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.[1]

Turbocharged models

TSIO-550-A
360 hp (268 kW) at 2600 rpm, dry weight 442 lb (200 kg) plus two turbochargers of 28.2 lb (12.8 kg) each.[2]
TSIO-550-B
350 hp (261 kW) at 2700 rpm, dry weight 442 lb (200 kg) plus two turbochargers of 28.2 lb (12.8 kg) each. Similar to the TSIO-550-A except with a 12 quart sump, sonic venturii removed and the two stage fuel pump replaced by a single stage fuel pump.[2]
TSIO-550-C
310 hp (231 kW) at 2600 rpm, dry weight 442 lb (200 kg) plus two turbochargers of 28.2 lb (12.8 kg) each.[2]
TSIO-550-E
350 hp (261 kW) at 2700 rpm, dry weight 442 lb (200 kg) plus two turbochargers of 28.2 lb (12.8 kg) each. Similar to TSIO-550-C with the oil sump and maximum continuous power rating of the TSIO-550-B.[2]
TSIO-550-G
310 hp (231 kW) at 2700 rpm, dry weight 554 lb (251 kg) plus two turbochargers of 28.2 lb (12.8 kg) each. Similar to the TSIO-550-E with smaller surface area intercoolers, different oil sump capacity and power rating.[2]
TSIO-550-K
315 hp (235 kW) at 2500 rpm, dry weight 522 lb (237 kg) plus two turbochargers of 28.2 lb (12.8 kg) each. Similar to the TSIO-550-E with new oil sump and capacity, decreased maximum continuous power, increased turbo boost pressure, decreased engine speed rating and tapered cylinder barrel fins.[2]

Turbocharged & FADEC models

 
TSIOF-550-D
TSIOF-550-D
350 hp (261 kW) at 2600 rpm, dry weight 558 lb (253 kg) plus two turbochargers of 35.2 lb (16.0 kg) each. Similar to the TSIOF-550-J except the exhaust system and low voltage harness.[2]
TSIOF-550-J
350 hp (261 kW) at 2600 rpm, dry weight 558 lb (253 kg) plus two turbochargers of 35.2 lb (16.0 kg) each. Similar to the TSIO-550-E except for FADEC fuel injection and ignition control, turbochargers, tapered cylinder barrel fins, oil sump and capacity, maximum continuous speed and manifold pressure rating.[2]
TSIOF-550-K
315 hp (235 kW) at 2500 rpm, dry weight 537.3 lb (243.7 kg) plus two turbochargers of 28.2 lb (12.8 kg) each. Similar to the TSIO-550-K but with FADEC fuel injection and ignition control.[2]

Liquid-cooled models

TSIOL-550-A
350 hp (261 kW) at 2700 rpm, dry weight 402 lb (182 kg). Similar to the TSIO-520-NB but with a new cylinder design that uses liquid cooling. The coolant manifold is on top of the cylinder head, with a coolant pump fitted to the starter adapter, driven by the starter adapter shaft and the oil cooler is mounted on the airframe, not the engine. The engine has an AiResearch TA81 turbocharger.[3]
TSIOL-550-B
325 hp (242 kW) at 2700 rpm, dry weight 557 lb (253 kg). Similar to the TSIO-520-UB but with a new cylinder design that uses liquid cooling. The coolant manifold is on top of the cylinder head, with a coolant pump fitted to the starter adapter, driven by the propeller shaft using sheaves, the oil cooler is mounted on the airframe, not the engine. A coolant tank and coolant lines are added to the installation. The engine has an AiResearch TS06 turbocharger.[3]
TSIOL-550-C
350 hp (261 kW) at 2600 rpm, dry weight 546 lb (248 kg). Similar to the TSIOL-550-A but with the exhaust system and turbocharger bracket from the TSIOL-550-B. The engine is modified to accept the AiResearch TA81 turbocharger. Neither oil nor coolant radiators are provided with the engine.[3]

Geared models

GIO-550-A
A special non-certified geared engine developed for the RU-38 Twin Condor covert reconnaissance aircraft, incorporating 3:2 gear reduction to 2267 rpm.[5][6][7]

Applications

 
Lancair IV-P equipped with a TSIO-550
IO-550
TSIO-550
TSIOF-550
TSIOL-550
GIO-550

Specifications (IO-550-A)

Data from Type Certificate Data Sheet E3SO.[1]

General characteristics

Components

Performance

See also

Comparable engines

Related lists

References

  1. ^ a b c d e f g h i j k l m n o p q r s t u v w x y z Federal Aviation Administration (March 2007). (PDF). Archived from the original on June 8, 2011. Retrieved December 28, 2008.
  2. ^ a b c d e f g h i j k l m n Federal Aviation Administration (March 2010). (PDF). Archived from the original (PDF) on January 5, 2018. Retrieved June 21, 2010.
  3. ^ a b c d Federal Aviation Administration (August 1997). . Archived from the original on January 5, 2018. Retrieved December 28, 2008.
  4. ^ Federal Aviation Administration (August 2007). . Archived from the original on January 5, 2018. Retrieved January 3, 2009.
  5. ^ Stoll, Alex (September 2001). "Schweizer RU-38A Twin Condor". Retrieved June 4, 2008.
  6. ^ Parsch, Andreas (February 2008). "Designations Of U.S. Military Aero Engines". Retrieved July 14, 2009.
  7. ^ Federal Aviation Administration (November 4, 1999). . Archived from the original on January 5, 2018. Retrieved September 9, 2014.
  8. ^ "IO550". Summit Aviation. Retrieved February 10, 2022.
  9. ^ Cessna 210 Centurion, Disciples of Flight, 2/21/15, Aircraft Engine Upgrade section.

External links

 
Wikimedia Commons has media related to Continental IO-550.

    February 26, 2023
    continental, engine, large, family, liter, fuel, injected, cylinder, horizontally, opposed, cooled, aircraft, engines, that, were, developed, light, aircraft, teledyne, continental, motors, first, delivered, 1983, type, remains, production, 550continental, tsi. The Continental IO 550 engine is a large family of 9 liter fuel injected six cylinder horizontally opposed air cooled aircraft engines that were developed for use in light aircraft by Teledyne Continental Motors The first IO 550 was delivered in 1983 and the type remains in production 1 2 IO 550Continental TSIO 550 C engine installation in a Cessna 400Type Piston aircraft engineNational origin United StatesManufacturer Teledyne Continental MotorsFirst run 1983Major applications Velocity XL Cirrus SR22 Cessna TTx Mooney M20 Bellanca Viking Beechcraft Baron Beechcraft BonanzaProduced 1983 presentDeveloped from Continental O 520The 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 1 2 This engine family competes with the Lycoming IO 580 series which are also six cylinder engines with similar power output and weight 4 Contents 1 Design and development 2 Variants 2 1 FADEC models 2 2 Turbocharged models 2 3 Turbocharged amp FADEC models 2 4 Liquid cooled models 2 5 Geared models 3 Applications 4 Specifications IO 550 A 4 1 General characteristics 4 2 Components 4 3 Performance 5 See also 6 References 7 External linksDesign and development EditThe IO 550 family of engines was developed from the IO 520 series with the stroke increased from 4 00 to 4 25 inches increasing the displacement to 552 in 9 05 L The engine family covers a power range from 280 hp 209 kW to 360 hp 268 kW 1 2 The engines were first developed in the early 1980s and first certified on a regulatory basis of FAR 33 1 February 1965 amendment 33 8 2 May 1977 The first IO 550 model was certified on 13 October 1983 1 2 Variants EditIO 550 A 300 hp 224 kW at 2700 rpm dry weight 430 72 lb 195 37 kg Certified 13 October 1983 1 IO 550 B 300 hp 224 kW at 2700 rpm dry weight 421 61 lb 191 24 kg Certified 13 October 1983 1 IO 550 C 300 hp 224 kW at 2700 rpm dry weight 433 20 lb 196 50 kg Certified 13 October 1983 1 IO 550 D 300 hp 224 kW at 2700 rpm dry weight 437 1 lb 198 3 kg Certified 23 June 1988 1 IO 550 E 300 hp 224 kW at 2700 rpm dry weight 450 50 lb 204 34 kg Certified 20 December 1989 1 IO 550 F 300 hp 224 kW at 2700 rpm dry weight 437 1 lb 198 3 kg Similar to the IO 550 A B amp C with a top mounted induction system and 12 quart oil sump Certified 23 June 1988 1 IO 550 G 280 hp 209 kW at 2500 rpm dry weight 428 97 lb 194 58 kg Certified 17 March 1989 1 IO 550 L 300 hp 224 kW at 2700 rpm dry weight 438 5 lb 198 9 kg Certified 23 June 1988 1 IO 550 N 310 hp 231 kW at 2700 rpm dry weight 429 97 lb 195 03 kg Similar to the IO 550 G with increased power rating Certified 16 August 1996 1 IO 550 P 310 hp 231 kW at 2700 rpm dry weight 429 lb 195 kg Similar to the IO 550 N with oil sump from the IO 550 L Certified 1 March 2000 1 IO 550 R 310 hp 231 kW at 2700 rpm dry weight 439 5 lb 199 4 kg Similar to the IO 550 N but with the oil sump oil suction tube and mount legs from the IO 550 B Certified 1 March 2000 1 FADEC models Edit IOF 550 B 300 hp 224 kW at 2700 rpm dry weight 447 1 lb 202 8 kg Similar to the IO 550 B with an Aerosance FADEC fuel and ignition control system Certified 4 February 2002 1 IOF 550 C 300 hp 224 kW at 2700 rpm dry weight 453 2 lb 205 6 kg Similar to the IO 550 C with an Aerosance FADEC fuel and ignition control system Certified 4 February 2002 1 IOF 550 D 300 hp 224 kW at 2700 rpm dry weight 455 0 lb 206 4 kg Similar to the IO 550 D with an Aerosance FADEC fuel and ignition control system Certified 4 February 2002 1 IOF 550 E 300 hp 224 kW at 2700 rpm dry weight 462 8 lb 209 9 kg Similar to the IO 550 E with an Aerosance FADEC fuel and ignition control system Certified 4 February 2002 1 IOF 550 F 300 hp 224 kW at 2700 rpm dry weight 460 1 lb 208 7 kg Similar to the IO 550 F with an Aerosance FADEC fuel and ignition control system Certified 4 February 2002 1 IOF 550 L 300 hp 224 kW at 2700 rpm dry weight 455 0 lb 206 4 kg Similar to the IO 550 L with an Aerosance FADEC fuel and ignition control system Certified 4 February 2002 1 IOF 550 N 310 hp 231 kW at 2700 rpm dry weight 460 0 lb 208 7 kg Similar to the IO 550 N with an Aerosance FADEC fuel and ignition control system Certified 4 February 2002 1 IOF 550 P 310 hp 231 kW at 2700 rpm dry weight 460 0 lb 208 7 kg Similar to the IO 550 P with an Aerosance FADEC fuel and ignition control system Certified 4 February 2002 1 IOF 550 R 310 hp 231 kW at 2700 rpm dry weight 470 5 lb 213 4 kg Similar to the IO 550 R with an Aerosance FADEC fuel and ignition control system Certified 4 February 2002 1 Turbocharged models Edit TSIO 550 A 360 hp 268 kW at 2600 rpm dry weight 442 lb 200 kg plus two turbochargers of 28 2 lb 12 8 kg each 2 TSIO 550 B 350 hp 261 kW at 2700 rpm dry weight 442 lb 200 kg plus two turbochargers of 28 2 lb 12 8 kg each Similar to the TSIO 550 A except with a 12 quart sump sonic venturii removed and the two stage fuel pump replaced by a single stage fuel pump 2 TSIO 550 C 310 hp 231 kW at 2600 rpm dry weight 442 lb 200 kg plus two turbochargers of 28 2 lb 12 8 kg each 2 TSIO 550 E 350 hp 261 kW at 2700 rpm dry weight 442 lb 200 kg plus two turbochargers of 28 2 lb 12 8 kg each Similar to TSIO 550 C with the oil sump and maximum continuous power rating of the TSIO 550 B 2 TSIO 550 G 310 hp 231 kW at 2700 rpm dry weight 554 lb 251 kg plus two turbochargers of 28 2 lb 12 8 kg each Similar to the TSIO 550 E with smaller surface area intercoolers different oil sump capacity and power rating 2 TSIO 550 K 315 hp 235 kW at 2500 rpm dry weight 522 lb 237 kg plus two turbochargers of 28 2 lb 12 8 kg each Similar to the TSIO 550 E with new oil sump and capacity decreased maximum continuous power increased turbo boost pressure decreased engine speed rating and tapered cylinder barrel fins 2 Turbocharged amp FADEC models Edit TSIOF 550 D TSIOF 550 D 350 hp 261 kW at 2600 rpm dry weight 558 lb 253 kg plus two turbochargers of 35 2 lb 16 0 kg each Similar to the TSIOF 550 J except the exhaust system and low voltage harness 2 TSIOF 550 J 350 hp 261 kW at 2600 rpm dry weight 558 lb 253 kg plus two turbochargers of 35 2 lb 16 0 kg each Similar to the TSIO 550 E except for FADEC fuel injection and ignition control turbochargers tapered cylinder barrel fins oil sump and capacity maximum continuous speed and manifold pressure rating 2 TSIOF 550 K 315 hp 235 kW at 2500 rpm dry weight 537 3 lb 243 7 kg plus two turbochargers of 28 2 lb 12 8 kg each Similar to the TSIO 550 K but with FADEC fuel injection and ignition control 2 Liquid cooled models Edit TSIOL 550 A 350 hp 261 kW at 2700 rpm dry weight 402 lb 182 kg Similar to the TSIO 520 NB but with a new cylinder design that uses liquid cooling The coolant manifold is on top of the cylinder head with a coolant pump fitted to the starter adapter driven by the starter adapter shaft and the oil cooler is mounted on the airframe not the engine The engine has an AiResearch TA81 turbocharger 3 TSIOL 550 B 325 hp 242 kW at 2700 rpm dry weight 557 lb 253 kg Similar to the TSIO 520 UB but with a new cylinder design that uses liquid cooling The coolant manifold is on top of the cylinder head with a coolant pump fitted to the starter adapter driven by the propeller shaft using sheaves the oil cooler is mounted on the airframe not the engine A coolant tank and coolant lines are added to the installation The engine has an AiResearch TS06 turbocharger 3 TSIOL 550 C 350 hp 261 kW at 2600 rpm dry weight 546 lb 248 kg Similar to the TSIOL 550 A but with the exhaust system and turbocharger bracket from the TSIOL 550 B The engine is modified to accept the AiResearch TA81 turbocharger Neither oil nor coolant radiators are provided with the engine 3 Geared models Edit GIO 550 A A special non certified geared engine developed for the RU 38 Twin Condor covert reconnaissance aircraft incorporating 3 2 gear reduction to 2267 rpm 5 6 7 Applications Edit Lancair IV P equipped with a TSIO 550 IO 550Beechcraft Baron Beechcraft Bonanza Bellanca 17 30 Cessna 182 STC SA09133SC modification 8 Cessna 206 modification 9 Cessna 210 modification 10 Cessna 350 Cirrus SR22 Cirrus VK 30 Freedom Aviation Phoenix Lancair Barracuda Lancair ES Lancair Legacy Mooney M20 Seawind 300C Velocity XL RG Washington T 411 Wolverine Yakovlev Yak 112TSIO 550Adam A500 Cessna 400 Lancair IV Mooney M20TN Velocity TXL RG Cirrus SR22TTSIOF 550Diamond DA50 Cobalt Co50 Valkyrie KAI KC 100TSIOL 550Extra EA 400 Viper Aircraft ViperfanGIO 550RU 38 Twin CondorSpecifications IO 550 A EditData from Type Certificate Data Sheet E3SO 1 General characteristics Type 6 cylinder air cooled horizontally opposed aircraft piston engine Bore 5 25 in 133 4 mm Stroke 4 25 in 108 0 mm Displacement 552 in 9 05 L Dry weight 430 72 lb dry 195 37 kg Components Fuel system TCM fuel injection Fuel type 100LL avgas Cooling system Air cooledPerformance Power output 300 hp 224 kW at 2 700 rpm Specific power 0 54 hp in 24 6 kW L Compression ratio 8 5 1 Power to weight ratio 0 70 hp lb 1 15 kW kg See also EditComparable engines Lycoming O 540 Lycoming IO 580Related lists List of aircraft enginesReferences Edit a b c d e f g h i j k l m n o p q r s t u v w x y z Federal Aviation Administration March 2007 Type Certificate Data No E3SO Revision 10 PDF Archived from the original on June 8 2011 Retrieved December 28 2008 a b c d e f g h i j k l m n Federal Aviation Administration March 2010 Type Certificate Data No E5SO Revision 6 PDF Archived from the original PDF on January 5 2018 Retrieved June 21 2010 a b c d Federal Aviation Administration August 1997 TYPE CERTIFICATE DATA SHEET NO E4SO Revision 1 Archived from the original on January 5 2018 Retrieved December 28 2008 Federal Aviation Administration August 2007 TYPE CERTIFICATE DATA SHEET NO E00004NY Revision 1 Archived from the original on January 5 2018 Retrieved January 3 2009 Stoll Alex September 2001 Schweizer RU 38A Twin Condor Retrieved June 4 2008 TELEDYNE CONTINENTAL October 2005 MANDATORY SERVICE BULLETIN MSB94 4G PDF Archived from the original PDF on November 16 2009 Retrieved July 14 2009 Parsch Andreas February 2008 Designations Of U S Military Aero Engines Retrieved July 14 2009 Federal Aviation Administration November 4 1999 Supplemental Type Certificate STC Number SA09133SC Archived from the original on January 5 2018 Retrieved September 9 2014 IO550 Summit Aviation Retrieved February 10 2022 Cessna 210 Centurion Disciples of Flight 2 21 15 Aircraft Engine Upgrade section External links Edit Wikimedia Commons has media related to Continental IO 550 Continental Specification Sheet IO 550 N Retrieved from https en wikipedia org w index php title Continental IO 550 amp oldid 1126543596, wikipedia, wiki, book, books, library,

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