Aircraft FADEC System
A380V/SB747-AIRCRAFT/FADEC-ENGINE GENERAL The Full Authority Digital Engine Control (FADEC) system ma…
Topic: AIRBUS
PACK OZONE CONTROL
OZONE FILTER An ozone filter is installed upstream of each Flow Control Valve (FCV). It is used for…
A-380 v/s B 747
Airbus A-380 v/s Boeing 747 : A380 The Airbus A380 is a wide-body aircraft manufactured by Airbus. It…
Airbus Information and Aircraft Series
Airbus Aircraft What is Airbus? Airbus SE, from 2000 to 2020 known as the European Aeronautic Defence…
Article in : AIRBUS
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AS CLIENT
- GENERAL All BITE results are stored in the director (DIR) BITE dedicated memory with failure indication shown on the Cabin Intercommunicatio...
- ELECTRICAL POWER LEVEL 2 GENERAL There are two identical engine driven generators called Integrated Drive Generators (IDGs). They are used a...
- IDG COOLING SYSTEM GENERAL The Integrated Drive Generator (IDG) oil cooling system consists of a self-contained oil circuit and a fuel/oil h...
A FADEC is a solid-state digital electronic ignition and electronic sequential port fuel injection system with only one moving part that con...
ATA 21 Airconditioning ZC (Zone Controller) × 1 Main Functions: -Optimized Temperature Control -Basic Temperature Regulation Elaboration -...
A. General The roll and pitch controls of the aircraft are electrical. They are based on two different types of digital computers (ELAC and ...
ECAM The ECAM (Electronic Centralized Aircraft Monitoring) system is made up of two primary components, two SDAC’s (System Data Acquisition ...