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CIDS WARNINGS Airbus A320
GENERAL All BITE results are stored in the director (DIR) BITE dedicated memory with failure indication shown on the Cabin Intercommunicatio...
IDG COOLING SYSTEM
IDG COOLING SYSTEM GENERAL The Integrated Drive Generator (IDG) oil cooling system consists of a self-contained oil circuit and a fuel/oil h...
Electrical Power A320
ELECTRICAL POWER LEVEL 2 GENERAL There are two identical engine driven generators called Integrated Drive Generators (IDGs). They are used a...
Full-Authority Digital Electronic Control (FADEC) System Description
A FADEC is a solid-state digital electronic ignition and electronic sequential port fuel injection system with only one moving part that con...
Airbus A320 Airconditioning System
ATA 21 Airconditioning ZC (Zone Controller) × 1 Main Functions: -Optimized Temperature Control -Basic Temperature Regulation Elaboration -...
Airbus A320 Flight Control Surfaces Working Principle
A. General The roll and pitch controls of the aircraft are electrical. They are based on two different types of digital computers (ELAC and ...
Airbus ECAM display and system
ECAM The ECAM (Electronic Centralized Aircraft Monitoring) system is made up of two primary components, two SDAC’s (System Data Acquisition ...
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