کتب الکترونیکی گروه اویونیک هواپیما

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  1. Electricity And Electronics For Aerospace Vehiles

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  4. Aircraf Radio Systems

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  7. The Advanced Avionics Handbook is a new publication designed to provide general aviation users with comprehensive
    information on advanced avionics equipment available in technically advanced aircraft. This handbook introduces the pilot
    to flight operations in aircraft with the latest integrated “glass cockpit” advanced avionics systems.
    Since the requirements can be updated and the regulations can change, the Federal Aviation Administration (FAA)
    recommends that you contact your local Flight Standards District Office (FSDO), where FAA personnel can assist you
    with questions regarding advanced avionics equipment flight training and/or advanced avionics equipment questions about
    your aircraft.
    This publication is

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  9. The book provides an introduction to the
    principles, operation and maintenance of aircraft
    digital electronic and computer systems. The aim
    has been to make the subject material accessible
    and presented in a form that can be readily
    assimilated. The book provides full syllabus
    coverage of Module 5 of the EASA Part-66
    syllabus with partial coverage of avionic topics in
    Modules 11 and 13. The book assumes a basic
    understanding of aircraft flight controls as well as
    an appreciation of electricity and electronics
    (broadly equivalent to Modules 3 and 4 of the
    EASA Part-66 syllabus).

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  10. Introduction
    This handbook begins with the basic principle of aircraft weight and balance control, emphasizing its importance and
    including examples of documentation furnished by the aircraft manufacturer and by the FAA to ensure the aircraft weight
    and balance records contain the proper data.
    Procedures for the preparation and the actual weighing of an aircraft are described, as are the methods of determining the
    location of the empty weight center of gravity (EWCG) relative to both the datum and the mean aerodynamic chord (MAC).
    Loading computations for general aviation aircraft are discussed using both loading graphs and tables of weight and
    moment indexes.
    Information is included that allows an FAA-certifi ated mechanic or repairman to determine the weight and center of gravity
    (CG) changes caused by repairs and alterations or removal and installation of equipment. This includes instructions for
    conducting adverse-loaded CG checks, also explaining the way to determine the amount and location of ballast needed to
    bring the CG within allowable limits.
    The unique requirements for helicopter weight and balance control are discussed, including the determination of lateral CG
    and the way both lateral and longitudinal CG change as fuel is consumed.
    One chapter includes the methods and examples of solving weight and balance problems using a hand-held electronic
    calculator, E6-B flight computer, and a dedicated electronic flight compute

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  11. Aircraft Electrical Systems

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