References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2COMMUNICATION SYSTEMS TRANSFERRING DATA THROUGH ELECTROMAGNETIC WAVE SIGNALS..VHF - 30 MHz to 300 MHz, HF - 3 and 30 MHz. UHF - 300 MHz to 3 GHz (MODER AIRCRAF)ACARS / AIRCOM-(Aircraft Communications Addressing and Reporting System) - Short message servicesSecal decoders SELECTIVE CALLER-FILTERSATCOM Communication purpose 1 to 40 GHZ

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2NAVIGATION SYSTEMS - PROCESS OF MONITORING AND CONTROLLING THE MOVEMENT OF A CRAFT OR VEHICLE FROM ONE PLACE TO ANOTHERVOR -108.0 MHz and 117.95 MHzADF - 190 Khz. to 1750 KhzILS loc, GS, MBMLS 5000MHZCDI Flight path variationHSI - Roll, Pitch, Yaw

RADIO ALTIMETERS- AGL (above ground level) DME 1025 to 1115 MHZGPS - 2 to 6 GHZTranspondersELT Emergency Transmitter Locator

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

VOR/DME/ILSReferences: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

MLS/GPS/FBWReferences: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

INS/FMS(N,G,P,F)/HOTASReferences: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

TCAS Indicates the range and bearing of aircraft within a selected range, usually 15 40 nautical miles forward, 5 15 nautical miles aft, and 10 20 nautical miles on each side. The system also warns of aircraft within 8700 ft of the aircraft's own altitude.

DVI/TOUCH SCREEN Speech recognition as input to the system to active the particular actionPressure transducers will be used to convert the touched pressure sensing effect to enable the machine

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

NavigationPilotageDead ReckoningElectromagnetic Wave(VOR/DME/ADF )Advanced methods-GPSCelestial Navigation galaxy objectsBy landmarksBy previous position(time, distance , speed, position)References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

CRT SHADOW MASK,BEAM PENETRATION (SINGLE GUN- NO MASK), BEAM INDEXING(INDEXING TUBE ON THE PH PLATE): TOUCH SCREEN/MFKDReferences: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

COMPARISON OF DISPLAY(PLASMA PANEL, LED,LCD,ELECTRONICS LUMINOUSReferences: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

HUD/HLD-Re focusing time /HMDReferences: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

LAYING OUT THE COCKPITMIL-STD-203 - Aircrew Station Controls and Displays FAR 25.1303 - Flight and Navigation Instruments

T Configuration:

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

Glass Cockpit/ Panorama DisplayFlight management systemsEFISPrimary flight displayMFDEngine Indicating and Crew Alerting SystemElectronic Centralised Aircraft Monitor

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

Electronic Radar Warfare/ Reliability/MaintainabilityONBOARD TESTING Equipment:BITE Build in Testing EquipmentATE Automatic Testing EquipmentFMEA Failure Mode Effect AnalysisFTA - Fault Tree AnalysisTACAS Traffic Collision Avoidance SystemReferences: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

Altitude height above the sea levelHeight vertical distance between two points(reference nodes)Course original flight pathHeading Direction nose pointingPlasma display Large screen,(>30 inches) small cells containing electrically charged ionized gases, which are plasmasReferences: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2

References: Aircraft Electricity and Electronics pg: 294-328, AC 43.13-1B Chapter 12 Section 2