DGCA Syllabus for Module Exam
Here You get All Module Exam Syllabus. SYLLABUS/M11 AEROPLANE AERODYNAMICS STRUCTURES AND SYSTEMS SYL…
Topic: Module 4
Module 4 feb 2018 | DGCA
DGCA module 4 Question 1. Emiter positiv wrt base 2. injct majoroty carrier into the base 3. Emitr i…
Article in : Module 4
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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...
- 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 LEVEL 2 GENERAL There are two identical engine driven generators called Integrated Drive Generators (IDGs). They are used a...
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 ...