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)
| Label | Occurrences |
|---|---|
| FADEC canonical | 13 |
| FADEC (some later variants) | 1 |
| Full Authority Digital Engine Control | 1 |
How this entity was disambiguated
This entity first appeared as the object of triple T649887 — resolving that mention is where its identity was fixed. The disambiguator weighed these candidate entities and picked the highlighted one (or “None”, minting a new entity). This is how homonymy is resolved: the same surface form can point to different entities.
Target entity: FADEC Context triple: [Pratt & Whitney F135, controlSystem, FADEC]
-
A.
Pratt & Whitney F117-PW-100
The Pratt & Whitney F117-PW-100 is a high-bypass turbofan jet engine used to power the Boeing C-17 Globemaster III military transport aircraft.
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B.
General Electric CF34-10E
The General Electric CF34-10E is a high-bypass turbofan engine developed by GE Aviation to power modern regional jets, particularly optimized for efficiency, reliability, and low emissions.
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C.
Pratt & Whitney F135 engine
The Pratt & Whitney F135 engine is a high-performance turbofan developed for the F-35 Lightning II, notable for its advanced thrust, stealth, and (in the F-35B variant) short takeoff/vertical landing capabilities.
-
D.
Pratt & Whitney JT9D
The Pratt & Whitney JT9D is a high-bypass turbofan jet engine that powered early wide-body airliners and was notably used on the original Boeing 747 series.
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E.
Rolls-Royce RB211
The Rolls-Royce RB211 is a high-bypass turbofan jet engine that was pioneering in its use of advanced materials and technology and became a cornerstone powerplant for wide-body airliners.
- F. None of above. chosen
- G. Unsure - the case is ambiguous/there is not enough information to decide.
Target entity: FADEC Target entity description: 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.
-
A.
Pratt & Whitney F117-PW-100
The Pratt & Whitney F117-PW-100 is a high-bypass turbofan jet engine used to power the Boeing C-17 Globemaster III military transport aircraft.
-
B.
General Electric CF34-10E
The General Electric CF34-10E is a high-bypass turbofan engine developed by GE Aviation to power modern regional jets, particularly optimized for efficiency, reliability, and low emissions.
-
C.
Pratt & Whitney F135 engine
The Pratt & Whitney F135 engine is a high-performance turbofan developed for the F-35 Lightning II, notable for its advanced thrust, stealth, and (in the F-35B variant) short takeoff/vertical landing capabilities.
-
D.
Pratt & Whitney JT9D
The Pratt & Whitney JT9D is a high-bypass turbofan jet engine that powered early wide-body airliners and was notably used on the original Boeing 747 series.
-
E.
Rolls-Royce RB211
The Rolls-Royce RB211 is a high-bypass turbofan jet engine that was pioneering in its use of advanced materials and technology and became a cornerstone powerplant for wide-body airliners.
- F. None of above. chosen
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 ⓘ |
How these facts were elicited
The pipeline generated the facts above by prompting gpt-5.1 with this entity's name + description and the instruction below.
You are a knowledge base construction expert. Given a subject entity and a description of it, return factual statements that you know for the subject as a JSON list of dictionaries(triples), where keys must be "subject", "predicate" and "object". The number of facts may be very high, between 25 to 50 or more, for very popular subjects. For less popular subjects, the number of facts can be very low, like 5 or 10. # Requirements - If you don't know the subject at all, return an empty list. - If the subject is not a named entity, return an empty list. - Include at least one triple where predicate is "instanceOf". - Do not get too wordy. - Separate several objects into multiple triples with one object.
Subject: FADEC Description of subject: 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.
Referenced by (15)
Full triples — surface form annotated when it differs from this entity's canonical label.