Dual Cooling of Engine
The dual cooling function was developed and aims to reduce the overall time to start both engines o…
Topic: ATA 80 Starting
Gas Turbine Engine Starters
Gas turbine engines are started by rotating the high-pressure compressor. On dual-spool, axial flow…
Article in : ATA 80 Starting
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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 ...