Module 6 Material and Hardware.
EASA Part 66 module 6 PDF Book Sample Pagesmodule-6-sample
Materials and Hardware (4164 Questions)
Sample – Materials Exams ( 40 questions 30 min),
Category A – Materials and Hardware Exams ( 52 questions 65 min),
Category B1 – Materials and Hardware Exams ( 72 questions 90 min),
Category B2 – Materials and Hardware Exams ( 60 questions 75 min),
Category B3 – Materials and Hardware Exams ( 60 questions 75 min),
EASA Part 66 Module 6 Book Forum
Module 6: Materials and Hardware
First post and replies | Last post by Aviation Training Exam, 3 months ago
EASA Part 66 Module 6 Book Content:
5.1 Electronic Instrument Systems
Typical systems arrangement and cockpit layout of electronic instrument systems.
5.2 Numbering Systems
Binary, octal, and hexadecimal numbering systems and conversions.
5.3 Data Conversion
Analogue and digital data; Operation and application of analogue/digital converters, inputs and outputs and various limitations.
5.4 Data Buses
Operation of data buses in aircraft systems including knowledge of ARINC, Ethernet and other specifications.
5.5 Logic Circuits
Identification of common logic gate symbols, tables, and equivalent circuits as used in aircraft systems; schematic diagrams, and logic diagrams.
5.6 Basic Computer Science
Computer terminology, operation, layout, and interface in a micro-computer and associated bus systems; single and multi address instruction words; memory terms and devices; data storage systems
functions and operation of a microprocessor including control and processing, register, arithmetic logic elements
5.8 Integrated Circuits.
operation of encoders and decoders, medium, large, and very large scale integration
operation, application and identification in logic diagrams of multiplexers and demultiplexers
5.10 Fiber Optics
Advantages and disadvantages; Fiber optic data bus; terminations; couplers, control terminals, remote terminals; application in aircraft systems.
5.11 Electronic Displays
Operation of common types used in modern aircraft including cathode ray tubes (CRT), light emitting diodes (LED), and liquid crystal displays (LCD).
5.12 Electrostatic Sensitive Devices
Handling of sensitive components; Awareness of risks and personnel anti-static protection devices
5.13 Software Management Control
restrictions, airworthiness requirements and effects of unapproved changes to software programs.
5.14 Electromagnetic Environment
EMC Electromagnetic compatibility; EMI Electromagnetic Interference; HIRF High Intensity Radiated Field; Lightning protection
5.15 Electronic Digital Aircraft Systems
Arrangement of systems and associated BITE (built in test equipment)including:
ACARS-ARINC Communication, addressing and reporting systems, EICAS Engine indication and crew alerting system, FBW Fly by wire, FMS Flight management systems, IRS Inertial reference system, ECAM electronic centralized aircraft monitoring, EFIS Electronic flight instrument system, GPS Global positioning system
TCAS Traffic alert collision avoidance system, Integrated modular avionics, Cabin Systems, Information Systems, Read more: