Lycoming IO-580

This article is about the 1997 era fuel-injected, six-cylinder aircraft engine series. For the 1959 eight-cylinder, geared, supercharged engine, see Lycoming GSO-580.
IO-580
Lycoming AEIO-580 installed in an Extra 330LC
Type Piston aero engine
Manufacturer Lycoming Engines
First run 1996
Major applications Expedition E350
Extra 330



The Lycoming IO-580 engine is a horizontally opposed, six-cylinder aircraft engine featuring three cylinders per side, manufactured by Lycoming Engines.[1]

There is no carburetted version of the engine, which would have been designated O-580 and therefore the base model is the IO-580.[2]

This engine family competes with the Continental IO-550 series which are also six-cylinder engines with similar power output and weight.[3]

Design and development

The IO-580 family of engines covers a range from 300 to 315 hp (224 to 235 kW). The engine has a fuel injection system which meters fuel in proportion to the induction airflow through air-bled nozzles at the individual cylinder intake ports. The engine has a displacement of 583 cubic inches (9.554 litres) and produces a maximum of 315 hp (235 kW) in its B1A version. The cylinders have air-cooled heads cast from aluminum-alloy with a fully machined combustion chamber.[1][4]

The first IO-580 was type certified on 12 August 1997 on the regulatory basis of FAR 33 effective February 1, 1965 as amended to 33-1 through 33-18. The engine is certified for use in either tractor or pusher configuration installations.[2]

Variants

IO-580-A1A
Six-cylinder, horizontally opposed, air-cooled direct drive, 583 cubic inches (9.55 litres), 300 hp (224 kW) at 2500 rpm, dry weight 444 lb (201 kg), PAC-RSA-10ED1 fuel-injection system, certified 12 August 1997[2]
IO-580-B1A
Six-cylinder, horizontally opposed, air-cooled direct drive, 583 cubic inches (9.55 litres), 315 hp (235 kW) at 2700 rpm, dry weight 434 lb (197 kg), PAC-RSA-10ED1 fuel-injection system, certified 23 March 2001[2]
AEIO-580-B1A
Six-cylinder, horizontally opposed, air-cooled direct drive, 583 cubic inches (9.55 litres), 315 hp (235 kW) at 2700 rpm, dry weight 446 lb (202 kg), certified 13 August 2007. This model has an aerobatic fuel and oil system. It may be equipped with either the PAC-RSA-10ED1 fuel-injection system or a Lycoming FM-250 system.[2]

Applications

IO-580-B1A
AEIO-580-B1A

Specifications (IO-580-A1A)

Data from Lycoming Specialty Datasheet and TYPE CERTIFICATE DATA SHEET NO. E00004NY, Revision 1.[2][4]

General characteristics

Components

Performance

See also

Related development
Comparable engines
Related lists

References

Wikimedia Commons has media related to Lycoming IO-580.
  1. 1 2 Lycoming Engines (n.d.). "Lycoming IO-580". Retrieved 2009-01-03.
  2. 1 2 3 4 5 6 Federal Aviation Administration (August 2007). "TYPE CERTIFICATE DATA SHEET NO. E00004NY, Revision 1". Retrieved 2009-01-03.
  3. ↑ Federal Aviation Administration (March 2007). "TYPE CERTIFICATE DATA SHEET NO. E3SO Revision 10". Retrieved 2008-12-28.
  4. 1 2 Lycoming Engines (2004). "Specialty datasheet" (PDF). Retrieved 2008-12-20.
  5. ↑ Found Aircraft (n.d.). "SPECIFICATIONS FOR THE STANDARD EXPEDITION E350". Retrieved 2009-01-03.
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