Lycoming TEO‑540‑C1A

E253880

The Lycoming TEO‑540‑C1A is a turbocharged, electronically controlled, horizontally opposed six-cylinder aircraft engine used in light twin-engine aircraft.

All labels observed (2)

Label Occurrences
Lycoming TEO‑540 series 1
Lycoming TEO‑540‑C1A canonical 1

How this entity was disambiguated

Statements (32)

Predicate Object
instanceOf aircraft engine
piston aircraft engine
application general aviation aircraft
light twin‑engine aircraft
aspiration turbocharged
configuration horizontally opposed
controlFeature automatic ignition timing control
automatic mixture control
electronic engine management
controlSystem FADEC
coolingMethod air-cooled
countryOfOrigin United States of America
surface form: United States
cycleType four-stroke
cylinderArrangement flat-six
displacement 541 cubic inches
approximately 8.9 litres
engineFamily Lycoming TEO‑540‑C1A self-linksurface differs
surface form: Lycoming TEO‑540 series
engineType reciprocating engine
familyDesignationMeaning TEO indicates turbocharged and electronically controlled opposed engine
fuelSystem electronically controlled
fuelType aviation gasoline
ignitionSystem dual ignition
intendedInstallation twin‑engine piston aircraft
manufacturer Avco Lycoming
surface form: Lycoming Engines
manufacturerParentCompany Textron
mountingConfiguration horizontally opposed engine mount
numberOfCylinders 6
seriesDesignation 540 cubic inch class
useCase civil aviation
private aviation
training aircraft
valveTrain overhead valve

How these facts were elicited

Referenced by (2)

Full triples — surface form annotated when it differs from this entity's canonical label.

Tecnam P2012 Traveller engineModel Lycoming TEO‑540‑C1A
Lycoming TEO‑540‑C1A engineFamily Lycoming TEO‑540‑C1A self-linksurface differs
this entity surface form: Lycoming TEO‑540 series