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.

All labels observed (3)

How this entity was disambiguated

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 Full Authority Digital Engine Control
linked to: FADEC
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

How these facts were elicited

Referenced by (15)

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

Pratt & Whitney F135 controlSystem FADEC
subject linked to: Pratt & Whitney F135 engine
FADEC fullForm Full Authority Digital Engine Control
linked to: FADEC
General Electric F404 controlSystem FADEC (some later variants)
linked to: FADEC
Thielert Centurion 1.7 controlSystem FADEC
Volvo RM12 abbreviation FADEC
subject linked to: Volvo RM12 turbofan