FADEC

E81243

FADEC (Full Authority Digital Engine Control) is an automated, computer-based system that manages and optimizes all aspects of an aircraft engine’s performance and operation.

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Observed surface forms (1)

Surface form Occurrences
Full Authority Digital Engine Control 1

Statements (50)

Predicate Object
instanceOf avionics system
engine control system
controls aircraft engine
bleed valves
fuel flow
ignition
propeller pitch (in turboprops)
thrust settings
variable stator vanes
fullForm FADEC self-linksurface differs
surface form: Full Authority Digital Engine Control
improves engine maintainability
engine reliability
pilot workload management
interfacesWith aircraft avionics
cockpit throttle controls
flight management system
limits engine operating parameters
maximum rotational speed
maximum temperature
maximum thrust
monitors aircraft conditions
engine speed
engine temperature
fuel pressure
oil pressure
optimizes emissions
engine life
engine performance
fuel efficiency
thrust response
provides automatic engine control
automatic restart capability (in many designs)
automatic start sequence
engine health monitoring data
engine protection
fault diagnostics
replaces hydromechanical engine control
manual engine control functions
requires redundant channels
reliable electrical power supply
usedIn modern commercial aircraft
modern military aircraft
turbofan engines
turbojet engines
turboprop engines
turboshaft engines
uses actuators
digital computer
electronic engine control unit
sensors

Referenced by (3)

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

subject surface form: Pratt & Whitney F135
FADEC fullForm FADEC self-linksurface differs
this entity surface form: Full Authority Digital Engine Control