Engine Power Assurance Test
Use this procedure to make sure that the engine will make rated takeoff thrust within the EGT and N…
Topic: Engineering Knowledge
A320 Landing Gear
Main Gear and Doors (1) Takeoff On takeoff the loads on the MLG decrease. As the aircraft becomes a…
AIRCRAFT STATIC DISCHARGER
PURPOSE The aircraft behaves like a Faraday cage and should be discharged. The static dischargers av…
Passenger Addressing Handset
GENERAL Each attendant station has a handset for public announcement, interphone dialing and communic…
PASSENGER LIGHT SYSTEM
GENERAL No Smoking (NS) signs on is achieved by a 3-position switch (ON/AUTO/OFF) in the flight comp…
IFR Aircraft Electronic Flight Information Systems
In an effort to increase the safety of operating complicated aircraft, computers and computer syste…
Article in : Engineering Knowledge
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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 ...