8) This describes the essential skills and knowledge and their level, required for this unit. Evidence shall show that knowledge has been acquired of safe working practices and diagnosing, rectifying faults and commissioning air navigation systems. All knowledge and skills detailed in this unit should be contextualised to current industry practices and technologies. KS01-EH191A Electronic communications - air navigation systems Evidence shall show an understanding of electronic communications - air navigation systems to an extent indicated by the following aspects: T1 Aviation navigation services and principles encompassing: role of navigation aids in providing Air Traffic Control Services. functions provided by navigational aids Rho Theta concept in context of navigational aids used within aviation. relevant ICAO (Annex 10) specifications Monitoring – equipment, status and pilot T2 Principle of operation of the NDB encompassing: simple block diagram of an NDB frequency band of operation parameters ICAO requires to be monitored typical radiation hazard issues simple block diagram of the aircraft Automatic Direction Finding (ADF) display NDB is used by Pilots and ATC T3 Principle of operation of the CVOR/DVOR encompassing: simple block diagram of a CVOR labelling each part. basic principles of variable and reference information RF phasing and far field space modulation frequency band of operation. features of a typical aircraft display possible errors and their cause in a CVOR. typical CVOR and DVOR facilities. main differences of operation between CVOR and DVOR. T4 Principle of operation of the DME encompassing: simple block diagram of a DME typical timing diagram from interrogation to reply. features of aircraft display system frequency band of operation modes of operation. T5 Principle of operation of the ILS frequency band of operation simple diagram of the localiser antenna pattern marking on it the zero DDM line, the represented colour and modulating frequency of each lobe and the clearance signal. simple sketch showing the glide path and the location of the marker beacons listing their identification, frequency and duration. simple block diagram to show the generation of the Carrier and Sidebands and Sideband only signals. ILS antenna arrays and farfield radiation patterns Far field phasing and space modulation terms DDM, and SDM. performance requirements for CAT I, CAT II and CAT III ILS T6 Principle of Global Navigation Satellite System (GNSS) basic principles of the Wide Area Differential Global Positioning System (WADGPS) basic principles of the Local Area Differential Global Positioning System (LADGPS) T7 NDB Technology and Maintenance. key functional modules of a contemporary NDB transmitter. function of the aerial coupling unit. radiation hazard issues, site restrictions and safety considerations in context of an NDB facility. signals in and out of the main components key features and theory of operation of an NDB antenna (Field Pattern, Capacity hat and Ground Plane) hardware configurations of current models of NDB used in the National Airways System of Australia. indicators on NDB equipment that may be used to determine status and locate a fault method(s) for conducting routine performance measurements on NDB equipment. process for removing an NDB from service. correct test equipment based on measurement tolerance and parameter being measured. correct use of selected test equipment. process for returning the aid to service locate and identify appropriate NDB documentation (AEIs) Flight Check of an NDB is mandated. T8 DME Technology and Maintenance. key functional modules of a contemporary DME beacon. modes of operation and relevant channel spacing for the Interrogation and Reply of the Beacon. purpose of the “squitter”. typical DME Block Diagram, the signal flow through the Beacon from incoming interrogation to outgoing Reply. function of each module in a contemporary DME. term “Gaussian Shaped Pulse” and why it is used. operation and purpose of the identification signal including test transmissions. define “Dead Time” monitored parameters of a DME. controls and indicators correct ON/OFF sequence process for removing a DME from service. auto-recycle operation typical function of the CTU for testing typical Alarm Registers measurement of parameters such as: Beacon Delay, Pulse Spacing, Pulse Width, Ident, Beacon Sensitivity, Selectivity, Reply Rate, Dead Time, Frequency, Monitor limits, Antenna VSWR, using the correct test equipment. correct use of test equipment. correlate the measurements to the Standard Operating Conditions (SOC) maintenance actions that may be performed without the requirements of a flight inspection Flight Calibration Check of an DME is mandated. process for returning the aid to service locate and identify appropriate DME documentation (AEIs) T9 CVOR Technology and Maintenance. principles of operation of a VOR and how the component signals are generated in a contemporary CVOR beacon. basic operation and functionality of the; Transmitter, Goniometer, Modulation Eliminator, Monitor, Antenna typical monitored parameters for a CVOR purpose of monitor bypass correct use of test equipment and interpretation of results, SOCs measurement of performance parameters using the correct test equipment. correct use of test equipment. correlate the measurements to the Standard Operating Conditions (SOC). maintenance actions that may be performed without the requirements of a flight inspection maintenance actions that do require a flight inspection importance of beacon accuracy T10 DVOR Technology and Maintenance. principles of operation of a DVOR and how the component signals are generated in a contemporary DVOR beacon. basic operation and functionality of the; modules used in the following sub systems; Carrier generation and modulation, Timing sequence generation, Sideband amplifier and modulator, Sideband antenna commutation, Monitor and Controller front panel indications under normal and fault conditions operation and functionality of the following circuits; Carrier amplifier and modulation (CGD, CPA, CDC, CMP), Timing signals generation (TSD), Reference phase generator (RPG), Antenna switching (ASD, ADS), Sideband generator (SGN, SMA, SCU), Control unit (CTU), Monitor unit (MRF, MSC, MFI, MBD, MSD). typical monitored parameters for a DVOR correct use of test equipment and interpretation of results, SOCs measurement of performance parameters using the correct test equipment correct use of test equipment. correlate the measurements to the Standard Operating Conditions (SOC). maintenance actions that may be performed without the requirements of a flight inspection maintenance actions that do require a flight inspection importance of beacon accuracy T11 ILS Technology and Maintenance. ILS functional blocks and typical cabinet modules of a Localiser and Glide Path (NM7000 series). main functional elements of a contemporary marker beacon. location and function of modules and system interconnections; Transmitter, Changeover, Monitor, Transmitter controller, Remote control, RMS/RMM, Power block diagram illustrate at specified points, the signal flow out from the distribution side and/or return via the recombination side of a Localiser and/or Glide Path operation of a specified Localiser antenna array. operation of an ‘M’-Array or other specified Glide Path antenna array the features and function of the RMM and/or RMS. performance requirements for CAT I, CAT II and CAT III ILS and how these are provisioned in the system hardware and monitoring. function of equipment indicators and controls, including the correct operation of controls to achieve a nominated function typical monitored parameters for a Localiser, Glide Path and Marker beacon correct use of test equipment (BITE and external) and interpretation of results, SOCs measurement of performance parameters using the correct test equipment. correct use of test equipment. correlate the measurements to the Standard Operating Conditions (SOC). maintenance actions that may be performed without the requirements of a flight inspection maintenance actions that do require a flight inspection typical tests and maintenance actions required during a flight calibration of an ILS |