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The Aircraft specification describes how an avionics system transmits information over the unidirectional data bus to other system elements. The Trainer is complete and comprehensive equipment to prepare aircraft maintenance engineers and avionics engineers to understand and maintain modern aircraft. Aircraft specifications define the standard for transfer of digital data between avionics system elements. Aircraft standards are used on virtually all commercial aircraft.
The Aircraft data words define the units, ranges, resolutions, refresh rates, number of significant bits, padbits, etc. for the words transmitted by the different avionics system elements. Trainer simulates signals at two speeds. Words are 32 bits long including a label, parity bit and other fields. The software installed on the trainer is an intuitive, graphical data bus analyzer that simplifies the simulation of Aircraft based avionics systems. The use of this model does not require programming expertise, and trainees do not need to write software programs. All they need to do is consult the comprehensive training manual provided with the trainer, to understand the various menu options. The user-friendly MS Windows-based interfaces allow transmission and reception on data buses with just a few clicks of the mouse. Then, while the bus is running, data and bus activity can be observed in meaningful engineering units, and can be changed on the fly.
Hardware:
The hard ware utilizes a rack-mount PC, 17-inch LCD TFT monitor, ARINC 429 interface, laser printer, instructors panel, patch panel, and power supply unit. The equipment is installed in two 19-inch racks of 18U height.
The trainer is designed to give the students a good understanding aircrafts avionics equipment. Students also develop logical and methodical approach totrouble shoot avionics faults inserted by the instructor. Avionics System Trainer brings the real life experience to the classroom. The trainer provides practical, hands-on training using the real avionics equipment configured and wired just like in an airworthy aircraft.
Standard Equipment:
Air craft avionics trainer provides instruction on the following systems
Global Positioning System
Altitude Encoder
Automatic Direction Finder
Instrument Landing System
Dual NAV. /Comm. Radio
Transponder
DME
Marker Beacon
Microphone
Two NAV Indicators
ADF Indicator
VOR
Intercom System
Headsets
Audio Panel
FaultInsertion Box
LCD NAV Display with GPS built in
Altimeter
Antennas.
The system combines primary flight instrumentation, aircraft systems instrumentation, engine instrumentation, warnings/alerts, and navigational information, all displayed on two LCD color screens. The EFIS / EICASTrainer is based on panel-mount LCD flight and navigation displays. There are separate PFD and MFD screens, with fullreversionary backup for redundancy. This is an advanced technology avionicssuite designed to integrate pilot/aircraft interaction into one central system. The trainer has a full functional primary flight display (PFD) for attitude/directionalguidance with electronic engine monitoring and detailed moving-map multifunction display (MFD) capabilities. The is a complete packaget hat represents EFIS / EMS / EICAS displaying flight instrumentation, position,navigation, communication, and identification information to the pilot using dual 7 wide (800 x 480) flat-panel color displays.
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Almost all the new generation commercial and military aircraft utilize electronic displays in the cockpit. Training imparted on an ARINC 429 based EFIS will prepare the students to easily understand other EFIS based on other versions of commercial and military avionics data busses. EFIS Trainer has been designed to enable avionics students to understand a typical digital bus EFIS system, and to perform maintenance and troubleshooting tasks that are typically encountered by avionics maintenance personnel. Electronic Flight Instrument System is the essential component of Glass Cockpit. he most widely used avionics data interface standards. It has been installed on many commercial passenger and transport aircraft including Airbus A310/A320 and A330/A340, Bell Helicopters, Boeing727, 737, 747, 757, 767. The fault panel allows for the simulation of typical aircraft EFISi nstallation faults including sensor feed faults. The faults are easy to select but not apparent to the student. A numbered switch panel or patching panel with cover is provided. The EFIS Trainer is based on Two Display Units, a Symbol Generator, a Control Unit, a Signal Simulator, and an Instructors Panel. Electronic displays are multi mode with ADI, HIS and Map modes. Map mode allows for superposition of Weather Radar data and sector display. Wiring harnesses in the trainer are representative of aircraft standards in hardware and wiring / looming techniques. Interconnect diagrams and panel circuit and layout diagrams are also provided.
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Three degrees of freedom instrument panel permits full demon stration of attitude and directional gyro functions. The Cockpit Instrumentation System with Electronic Flight Instruments and electronic engine display.
Standard Features:
Functional engine monitoring system connected to engine sensors
Provision of engine sensor simulation
Functional digital primary flight display mounted on a panel that can simulate roll,pitch, and yaw movements controlled by a mechanism operated by a control yoke.
Functional pitot- static system with provision for conducting pitot static system checks
Standby Instruments installed.
The EFIS used in is a versatile unit that includes several features representing a modern EFIS display. The Basic EFIS Trainer provides an introduction to a general aviation Electronic Flight Instruments System (EFIS).
EFIS Features:
External GPS Receiver with database
Autopilot Interface
GPS Interface
ILS Interface
NAV Interface
External Remote Compass System
Interface
H.S.I Resolver Interface
Emergency Power Battery
Altitude Encoder Interface
The GPS trainer provi desin-depth knowledge and hands-on experience to maintain and troubleshoot GP S equipment. A fault panel lets the instructor insert commonly encountered faults so that trainees can learn how to troubleshoot and repair the GPS equipment in actual situations. GPS has become an indispensable aid for airborne, land and marine navigation. Correct usage and effective maintenance of GPS equipment require a good knowledge of GPS principles, operation and equipment circuitry. Optional system components may be added and interfaced to the system which increase its features and capabilities. Some of these optional components include an external course deviation indicator (CDI) or horizontal situation indicator (HSI), autopilot, and external annunciators. The GPS Trainer equipment consists of a panel mounted IFR- approved GPS receiver, a GPS antenna, and a GPS signal simulator. Asimul at or for altitude input is included to provide full navigation and operational capabilities.
GPS Functional Features:
Panel-mount IFR GPS capable of performing GPS approaches
Eight- channel parallel GPS receiver
Direct- To feature for easy navigation
Easy-to-readmap display
Comprehensive Jeppesen database
Altitude input for increased accuracy
Database can store up to 500 user-defined way points along with user comments for up to 200airports
Capable of B- RNAV compliance.
Can beinter faced to external CDI or HSI, RMI, fuel management system, external moving map display, and air data system
Operates on any voltage 11-33Vdc.
Air craft Radio Altimeter System Trainer is a fully functional radio altimeter system comprising of actual airborne avionics equipment. They are also abbreviated as Rad. Alt. in avionics terminology. The terms Radio Altimeter and Radar Altimeter are used interchangeably and essentially mean the same.
The Radio Altimeter System Trainer is comprised of the following items:
Bench-mounted mobile workstation
Radio Altimeter Tx and Rx Antennas
Radio Altimeter Transmitter/Receiver
Radio Height Indicator
Test Set Antenna Couplers, qty. 2
Test Set
Power Supply
All necessary wiring harnesses
Features:
Solid-stat eRadio Altimeter Receiver/ Transmitter Unit
Digital altitude processor for long, drift-free operation
Rugged,die-cast construction of the Receiver/Transmitter Unit
Radio Altitude Indicator
Operates on28 volt DC power
Has serial digital output for use by other avionics equipment like FMS and Autopilots
Self test to enable rapid verification of proper system function
Standard radio altimeter antenna used in general aviation aircraft
Adjustable Decision Height function provided to alert pilot via lamp and aural tone that the aircraft has descended to a selected altitude
Aircraft in the air simulation
Fixed, linear variable, and flight profile altitude simulation
Aircraft on Ground simulation
Para metrictesting functions.
GPS Navigation Trainer with Moving Map is a valuable hands-on training system that allows the students to explore the functionalities offered by modern GPSnavigation systems. The system offers Enhance Situational Awareness through severalusing on a high-resolution terrain page showing hazards relative to thealtitude and a vertical profile of terrain along the route of flight. The bright 7-inch diagonal highde finition sunlight-readable display makes detailed mapping easy to see you can even viewan entire approach plate on the large-format display. For easy operation, the bezel around the screen includes soft keys and a joystick control. And with afast 5 Hz GPS update rate, the rendering of graphics and flight data is smoothand continuous. It comes with a builtin database, and an Americas, Atlantic or Pacific terrain database.Using this information, the system displays flight route over contour terrainmapping. The user caneven customize the minimum clearance levels to receive terrain cautions. With information from the terrain database, it monitors the current position in relation to surrounding terrain to provide alerts.
Features:
Moving map
Audibleter rain alerts
Smart Airspace Feature
Instruments page
IFR map mode
Traffic Information Services (TIS) alerts compatible
Separateserial and USB interfaces
Built-in HSI:yes
Automaticlog book.
This trainer is consists of three axes flight control computer, Mode Controller, Mode Annunciat or, Pitch / Yaw / Roll servos, Flight Director, and a magnetic slaved HSI System integrated with cockpit controls and includes control linkages to the control surfaces of a model aircraft.
The Autopilot/ Automatic Flight Controls Trainer is an excellent resource for teaching the principles of automatic flight controls by demonstration using a complete system that encompasses all the aspects of auto pilot and automatic flight controls. This is dedicated to bridging the gap between classroom instruction and practical,hands on training. This is representative of autopilot systems used on large commercial aircraft.
This is equipped with a complete control mechanism linked to a control yoke and rudder pedals. The visual display of realistic effects enhances the perception and understanding of flight controls. The trainer, in the standard configuration consists of a large model airplane with all the main control surfaces. Any movement in control yoke and rudder pedals results in the proportional movement of the control surfaces.
Aircraft quality electrical shielded wiring, cables, connectors, and harness assemblies and easily removable AD Fantenna with coaxial cable connections. All interconnections are of aircraft quality electrical shielded wiring, cables, connectors, and harnesses. Aircraft Automatic Direction Finder Equipment Trainer is designed to provide hands-on training on a real and operational equipment approved for aircraft installation. Using Avionics Instructors can effectively teach students on installing, removing, and testing an ADF unit. Students also develop proper understanding and learn how to trouble shoot the ADF equipment. The equipment is mounted on a mobile workstation containing air craft ADF unit, ADF indicator, and ADF loop and sense antenna assembly package. The work station includes a test panel console for bench testing of ADF equipment.
Features:
Durable,steel frame, Vertical standing panel with sturdy casters
Adjustable height test panel
ADF Indicator
Wood shelf
Accessories storage case
Adjustable height equipment panels
Avionics panel, complete with Allied Signal KX 155 with Indicator
Aircraft Antenna mounted on rotating machanis
Power Supply with voltage and current meters, power cord
Installation and mounting kit.
Aircraft Distance Measuring Equipment (DME) System Trainer is designed to provide hands-on training on a real and operational equipment approved for aircraft installation. The trainer includes aircraft quality electrical shielded wiring, cables,connectors, and harness assemblies and DME antenna with coaxial cable connections. The equipment is mounted on a mobile workstation containing air craft DME unit with built-in indicator, and DME antenna, and a test set. The trainer includes a test panel console for bench testing of DME equipment.
Features:
Durable,steel frame, Vertical standing panel with sturdy casters
Built-in DCP ower Supply
Simulation of Distance, and Speed
Avionics panel complete with Honeywell DME with built-in Indicator for distance, speed,and time
Accessories storage drawers & cabinet.
Aircraft quality electrical shielded wiring, cables, connectors, and harness assemblies are used to interconnect all units. All units are easily removable. The workstation includes two test panel consoles for bench testing of ILS receiver equipment. Instrument Landing System (ILS) Trainer is designed to provide hands-on training on a real and operational equipment approved for aircraft installation. The equipment is mounted on a mobile workstation containing aircraft ILS receiver units, NAV/VOR/GS indicator, marker indicator, marker antenna, NAV and Glide- Slope antenna.
Features:
Avionics test panels Honeywell ILS Receivers
NAV/LOC/GS Indicator
Durable,steel frame, with sturdy casters
Power Supply with voltage and current meters
Accessories storage drawers and cabinet.
The trainer includes secondary radar equipment, and radio navigation equipment. The may be upgraded with the optional feature to include satellite navigation(GPS). The Aircraft Navigation Systems Trainer consists of fully functional aircraft navigational equipment used in a typical general aviation aircraft. The trainer is a realistic mock-up of aircraft navigational systems with functions and capabilities that facilitate the following aspects of hands-on training:
Test the equipment using simulated navigation/flight data in compliance with standard technical procedures.
The emphasis in design is to allow the students gain hands-on experience.
Conduct practical training for flight line tasks like physical removal, installation, operation, and maintenance testing by using ramp tester.
Perform diagnostic testing as done in an avionics maintenance shop, using real time navigation transmission and reception with aDME/Transponder bench test set.
The Attitude Director Indicator (ADI)provides a consolidated and easy-to-read display of aircraft roll and pitch attitudes and command bugs. The Horizontal Situation Indicator (HSI) to provide a consolidated display to a pilot for more efficient cockpit resource management. All modern military and commercial aircraft are equipped with autopilots for automatic flight control, and Horizontal Situation Indicator (HSI) for navigational information presentation to the pilot. All wire harnesses are routed through terminal strips to enable students to measure and monitor electrical signals, and to troubleshoot the instructor induced faults. The equipment is mounted on a mobile workstation containing Horizontal Situation Indicator, with bootstrap Directional Gyro, Flux Valve,Slaving Accessory, ADI, and a simulator box to generate all other required signals needed by the system.
Functional Description:
Magnetic Heading and course information from VOR/LOC, and GPS is combined on the HSI.
Remote mounted compass system consisting of Pictorial Navigation Indicator, Remote Directional Gyro, Magnetic Azimuth Transmitter, simulated NAV signals unit, and Slaving Accessory. The ADI system comprises of vacuum driven attitude gyros,and simulated autopilot deviation signal unit. The HSI also provides outputs for autopilot or flight director, OR receivers, and additional compass loads. The HSI provides a pictorial display of the horizontal navigation situation and also provides manual controls for course and heading datum selection. It includes dual glide-slope pointers which are in view during a simulated ILS approach.
Features:
Durable,metal frame with sturdy casters
Control Yoke operated roll, pitch, and yaw simulation
Installed units are actual aircraft equipment
Fault insertion module
Simulated NAV inputs
Interface trainers
CBT included.
It has a modular design. It may be installed and operated as a roll axis only autopilot, roll and pitch axis, or a roll, pitch, and yaw axis autopilot. Autopilot Trainer is based on a Century 2000 Autopilot. The advanced design provides very smooth and precise corrections in aircraft attitude. Theflexible design provides the economy of expand ability. The complete Century 2000 is a true 3-axes, flight director/autopilot.
System Components:
Roll Axis Control
The complete roll axis autopilot features continuous roll/NAV/voltage monitors, heading select, heading hold, NAV, /LOC/BCanticipative intercept and track automatic soft track, about 45 degree intercept and all angle intercept with HSI.
System Components:
Directional Gyro/Indicator
Roll Servo
Autopilot Computer/Control Unit
Attitude Indicator / Flight Director
Moveable Control Surfaces
Turn & Slip Indicator
Altitude Pre-selector
Autopilot Annunciator
Rate of Climb Indicator
Altitude Sensor
Yaw Servo
Pitch Servo.
The can serve the purposes of training students on new generation of digital autopilots, as well as familiarizing the students with the essential features of EFIS. The Two-axis digital autopilot trainer is based on an EFI Swith autopilot interface, usually found in light aircraft.
The interface to the EFIS results in autopilot operation in the following modes:
Heading Mode
GPS Navigation Mode
VOR Navigation Mode
Ground Track Mode
GPS Steering Mode
Altitude Mode
Turn-Around Mode
Localizer Tracking Mode.
The EFIS Display has the following characteristics:
Display Type: LCD, TFT (Thin Film Transistor)
Resolution: 854 x 480 color pixels.
Back light: at least 800 nits
Size: 7.0 diagonal (178 mm).
