Avionics and Cockpit Instrumentation System Trainer

quick overview :

Features:

1. The system combine Navigation(ADF-DME-VOR-ILS-GPS-XPDR) instrumentation, Communication(VHF) instrumentation, navigational information. primary flight instrumentation, aircraft systems instrumentation and engine instrumentation.
2. Roll, pitch and yaw motions can be operated from the side yoke to be able to demonstrate aircraft attitude and directional gyro functions.
3. Functional engine monitoring system be connected to engine sensors.
4. Primary flight display be mounted on a panel that can simulate roll, pitch, and yaw movements controlled by a mechanism operated by a control yoke.
5. Provision of engine sensor simulation.
6. Pitot-static system to conduct pitot static system checks for digital instrument at the trainer.
7. NAV system testing
8. Comm System Testing
9. Indication Testing
10. Encoder Altimeter Testing
11. Altitude simulation
12. Altimeter and Transponder run in sync
13. TXPDR Ident
14. DME Channel selection
15. 6(six) metal drawers.
16. All required cabling, coupler ,splitter and socket
17. Extension cable for GPS Antenna
18. Tripod stand for mounting GPS Antenna
19. The system mounted on a metal/aluminum mobile stand.
20. Metal/aluminum frame with 4 wheels. 2 of 4 wheels are lockable

Components:

1. Smart PFD-MFD Screen
2. Engine Data Modules
3. Nav/Com Radio ( Vor/ ILS )
4. Nav Indicators ( Analog )
5. GPS (Global Positioning System )
6. ADF (Automatic Direction Finder )
7. ADF Indicator
8. ILS (Instrument Landing System )
9. DME (Distance Measuring Equipment)
10. Transponder
11. Marker Beacon
12. Altitude Encoder
13. Intercom System
14. Two Pilot Headsets
15. Dynamic Microphone
16. Vacuum Pump
17. Dc Power Box
18. Aircraft circuit breaker
19. Antennas
• VOR/LOC antenna
• ADF antenna
• Marker-Beacon antenna
• GS antenna
• VHF-COM antenna
• TRANSPONDER antenna
• All antennas cables
20. Sensors:
• Oil Temperature Sensor
• Carburetor Air Temp Sensor
• Manifold Pressure Sensor
• Fuel Level Sensor
• Oil Pressure Sensor
• Fuel Pressure Sensor
• Engine RPM Sensor
• Fuel Flow Sensor
• Ammeter Shunt
• CHT Thermocouples (Qty 4)
• EGT Thermocouples (Qty 4)
• OAT Sensor
• Pitot Tube
• Static Port
• Inductive sensor
21. Throttle Lever
22. Pitot-Static System:
• Pressure Pump to Create Pitot Pressure
• Vacuum Pump to Create Static Pressure
• Pitot Tube (not operate)
• Fuselage Static Port (not operate)
• Alternate Static Port(not operate)
• Static Source Selector Switch (not operate)
• Two Test Ports for Pitot-Static Test Set
23. Contacs:
• Pitot Heater
• L/G
• Taxi Light
24. Electronic Simulation of Sensors:
• Oil Temperature Manifold Pressure
• Engine RPM
• Oil Pressure
• Fuel Level
• Fuel Press 

Components Technical

1. NAV/COM Device
• NAV/COMM Transceiver
• 200-channel NAV receiver
• Built-in VOR Converter
• Maximum 25 kHz channel spacing
• Frequency (COM) 118.000 to 136.975
• Nav frequency 108.00 MHz to 117.95 MHz in 50 kHz spacing
• VOR/LOC converter
• Input voltage 28 VDC
• Built-in VOR/Localizer converter
• Flip-flop frequencies
• Volume control
• Frequency memory and recall
• Display
• Original installation manual.
2. NAV INDICATOR Device
• Navigation Indicator containing VOR/LOC left-right needle
• To-From Indicator
• VOR/LOC Warning Flag
• OBS
• Integral VOR/LOC Converter
• Glideslope Deviation needle
• Metal bezel with glass lens
• Original installation manual.
3. Transponder Device
• Transmitter Frequency; 1090 MHz +-3 MHz
• Receiver Sensitivity: -73dBm (nominal); -69dBm (min. for 90% reply)
• Mode A,C
• Input voltage 14/28 VDC
4. DME Device
• 200-channel receiver
• CHANNELING SOURCES: External control head providing BCD code, 2×5 code, slip code, or serial code
• RMT/FREQ/GS-T mode
• DME two concentric freq knop
• Freq Display
• Original installation manual.
5. ADF Device
• FREQUENCY RANGE: 200KHz to 1799KHz in 1 KHz increments
• BEARING ACCURACY: +- 3 degrees from 70 uV/m to 0.5 V/m RF input signal level
• Receiver sensitivity: 150uV/m max for s+n/n = 6dB
• Receiver Selectivity: 6dB bandwidth: +-2 KHz max off center frequency; 80dB bandwidth: +-7 KHz max off center frequency
• POWER REQUIREMENTS: 11 to 33 VDC – 12watt
• ADF button
• BFO button
• FRQ button
• FLT/ET button
• SET/RST button
• VOL/Off knop
• Freq display
• Original installation manual.
6. ADF Indicator
• Single needle ADF indicator for use with ADF receiver
• Adf Bearing Input: DC sine and cosine voltages, +-3.0VDC max across each winding
• Power Requirements: Compass Card Drive: 12VDC at 0.12A
• Lighting: 14VDC at 0.16A or 28VDC at 0.08A
7. Audio Panel
• Audio Inputs;
• Impedance: 600 ohms
• Max input: 5 Vrms
• Isolation: 60 dB minimum
• Bandwidth: 100 Hz to 6.5 kHz
• Transceiver: 3 (including TEL)
• Receiver: 5 (NAV1, NAV2, AUX1, AUX2, AUX3)
• Alerts: 4 (unswitched)
• Telephone input: 1
• Intercom Functions;
• Positions: 6 (pilot, copilot, 4 passengers)
• Volume control: 2 (pilot, copilot/passengers)
• VOX: Automatic (1 per MIC input)
• Modes: Pilot, crew, all
• MIC impedance: 150 ohms
• MIC Bias: 11 VDC through 470 ohms
• Keyed ICS: Configurable
• Music functions;
• Inputs: 2 (independent from Bluetooth audio)
• Impedance: 600 ohms (differential)
• input: 3.0 Vrms
• Gain: +24 dB Max/-96dB min
• Input level: < 200 mVrms at max gain for full power out 3dB@1kHz Bandwidth 20 Hz to 20 kHz
• Distortion: < 0.1% THD+N typical at full power over full bandwidth
• Muting: Selectable and configurable
• Volume control: Knob controlled (pilot and copilot/passenger)
• Headphone Outputs
• Output amplifiers: 3 Stereo (pilot, copilot, passenger)
• Output power: 65 mW into 150 Ohms Pilot and Copilot, 260 mW into 37.5 Ohms passenger
• Distortion: < 3% THD+N at 10% Power, < 10% THD+N at full power
• Frequency response: 20 Hz to 20 kHz
• Impedance rated: 150 Ohm pilot/copilot, 37.5 Ohm Passenger (4-150 Ohm headsets)
• Impedance supported: 150 to > 600 Ohm
• Speaker;
• Outputs: 1
• 28 Volt: 10 Watt into 4 Ohm; 7 Watt into 8 Ohm
• 14 Volt: 3 Watt into 4 Ohm 3dB@1kHz Bandwidth 350 Hz to 6.5 kHz
• Distortion: < 10% THD+N at full power, < 3% THD+N at 10% power
8. Smart PFD-MFD Screen
• NOTE: Smart PFD-MFD Screen brand/model and some technical specs can be change due to market availability. ( Dynon-Bendix-Garmin or similar )
• Screen is very bright and high-resolution driven by advanced graphics processors create highly visible and readable display.
• Display is 1280 x 800 pixel, 1200+ nit TFT active-matrix capacitive multi- touch LCD screen.
• High-Definition Touch Screen
• Display Connectors Specification
• There are 37-Pin DIN Connector for the main wiring harness.
• There are four (4) RS-232 connector ports for connection to compatible
  equipment.
• All serial ports have configurable baud rates and data formats for use as general-purpose inputs and output.
• There are minimum three (2) USB Connectors.
• There is an Ethernet Connector to be used to synchronize data between
  displays.
• Displays operate between 10- and 30-volts DC.
• Display show “engine instrument data”
• Display show “flight instrument data”
• Screen Dimensions
• 7.64” Wide
• 5.59” High
• 3.13” Deep
• Users are able to interact via the two knobs, two buttons integrated into the knobs, and eight buttons along the bottom of the display’s bezel and via touch gestures on the display screen itself.
• Display have a robust GPS moving map.
• Display back-lighting is controlled by its ambient light sensor to actively adjust the brightness based on the current lighting conditions or user is able to adjust the brightness by buttons.
• The default layout of screen show below
• Pfd
• Map
• Engine
• Screen switch into 100% window or 50%/50% split windows.
• There is Count-Up/Count-Down timer in the display.
• PFD Page Layout have at least the following:
• Airspeed Indicator
• Ground Speed (GS)
• True Airspeed (TAS)
• Airspeed Bug
• Airspeed Trend Rate
• Attitude Indicator
• Flight Path Marker
• Altimeter
• Setting Barometer (BARO)
• Altitude Bug
• Altitude Trend Rate
• Barometer Setting, and Density Altitude.
• Vertical Speed Indicator
• Vertical Speed (VS) BUG.
• Heading Indicator/Directional Gyro
• Heading (HDG) BUG
• Slip Ball
• Angle of Attack Indicator
• OAT(Outside air temperature)
• Winds Aloft magnitude and vector
• Artificial Horizon/Synthetic Vision
• Menu Page have at least the following:
• Six Pack
• G-meter
• Terrain Alert
• Airport Flags
• HSI SRC
• Bugs
• There is a Six-Pack presentation options on the PFD
• Main Menu bar are at the bottom of the screen and include following functions:
• NRST – Nearest:
• Info page
• FPL – Flight Plan
• INFO
• MENU
• Message( NO MSG / Message / Caution / Warning )
• Knob’s functions have at least the following:
• Adjust Bug (HDG, ALT, etc.)or BARO value
• Change Map scale
• Activate and/or move cursor
• Flight Data Modules have at least the following:
• All sensors are solid state.
• Accelerometers, which measure forces in all three directions
• Rotational rate sensors, which sense rotation about all three axes
• Pressure transducers for measuring air data
• Magnetometers on all three axes for measuring magnetic heading.
• Engine Data Modules have at least the following:
• These modules support popular four and six-cylinder engine installations and measure a variety of engine and environmental parameters, such as:
• RPM
• Manifold pressure
• Oil temperature
• Oil pressure
• Exhaust gas temperature (EGT)
• Cylinder head temperature (CHT)
• Fuel levels for multiple tanks
• Voltage
• Current
• Fuel pressure
• Fuel flow
• Carburetor air temperature
• Coolant pressure and temperature
• Flap and trim potentiometers
• External contacts
• Fuel Computer
• Pitch Trim Indicator
• Roll Trim Indicators
• Flap Indicator
9. Headsets
• 24 dB NRR hearing protection
• 3.5mm Music input port
• EM56 noise reflective cup mic
• Clear Hear performance audio speakers
• Foam Fit comfort ear seals
• Deep Pocket ear canals
• Wind block foam mic muff
• Stainless steel adjustable headband
10. DYNAMIC MICROPHONE
• Impedance: 50-600 ohms.
• Includes: 5 ft. coiled cord with right-angle plug and hanger bracket.
• Right angle plug
• Hanger bracket