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 ⓘ
cycleType four-stroke ⓘ
cylinderArrangement flat-six ⓘ
displacement 541 cubic inches ⓘ
approximately 8.9 litres ⓘ
engineFamily 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 Lycoming Engines ⓘ
linked to: Avco Lycoming
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 series ⓘ
linked to: Lycoming TEO‑540‑C1A