Avionics & Glass Cockpit Systems GARMIN

The trainer enables trainees to gain hands-on experience with avionics equipment, Primary Flight Display (PFD) and Engine Monitoring System (EMS). It provides practical training with avionics equipment configured to bring real-life experience to the training environment, supporting a good understanding of avionics and glass cockpit equipment along with a methodical approach to troubleshooting

The system combines navigation, communication, navigational information, primary flight instrumentation and aircraft systems instrumentation. It includes a three-degree-of-freedom ADAHRS pitot-static system, NAV and communication testing, transponder functions, altimeter and encoding altimeter, altitude simulation, and an instructor's panel for fault insertion.

The trainer includes engine sensors, throttle and propeller controls, pitot-static components, contact functions and electronic sensor simulation for practical aircraft systems training.

Manufactured by Atico Export with a focus on precision, durability and consistent performance for technical education and practical training applications.

Components :

• Smart PFD-MFD Screen
• GPS (Global Positioning System)
• Marker Beacon System
• Intercom System with Advanced Audio Control Panel
• Two Pilot Headsets
• Pitot Static Test System
• Power Unit/Panel

Antennas :

• VOR/LOC Antenna
• Marker-Beacon Antenna
• VOR/Glide Slope Antenna Diplexer
• GPS Antenna
• All Antenna Cables

Sensors :

• Oil Temperature 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
• Inductive Sensor

Controls :

• Throttle Lever
• Propeller Lever

Pitot-Static System :

• Pitot Tube
• Fuselage Static Port
• Alternate Static Port
• Static Source Selector Switch
• Two Test Ports for Pitot-Static Test Set

Contacts :

• Pitot Heater
• L/G
• Taxi Light

Electronic Simulation of Sensors :

• Oil Temperature
• Manifold Pressure
• Engine RPM
• Oil Pressure
• Fuel Level
• Fuel Pressure

Components Technical Specifications :

Power Unit/Panel :

• Main power control switch.
• Aircraft circuit breakers for each system.
• DC power unit.

Smart PFD/MFD Screen :

• 10.6-inch touch screen.
• Touch and knob control.
• Dual concentric knobs.
• Primary flight data including attitude, airspeed, altitude, heading and vertical speed.
• HSI accepts VOR/LOC and/or GPS course guidance.
• Synthetic vision technology with 3D depictions of terrain, obstacles and airports.
• Digital ADAHRS provides aircraft position, rate, vector and acceleration data.
• Dedicated buttons for direct course selection to an airport or nearest airports and waypoints.
• Highway-in-the-sky flight path visualization.
• Full-screen PFD, split PFD/MFD and standalone MFD display options.
• Multiple display installation supports PFD, MFD or split-screen configurations.
• Landscape orientation.
• Bright, high-resolution, large-format LCD display. :contentReference[oaicite:2]{index=2}

Air Data Attitude Heading Reference System (ADAHRS) :

• Provides accurate and reliable referencing of aircraft position, rate, vector and acceleration data.
• Designed for aircraft flying up to 465 knots indicated airspeed (IAS).
• Flexible mounting positions.
• Multiple ADAHRS units can be installed for system redundancy.

Magnetometer :

• Accurate three-axis sensing of the Earth's magnetic field.
• Provides data to the ADAHRS for determining aircraft magnetic heading.
• Measures the local magnetic field.
• Microprocessor-based magnetic heading sensing system.
• Functions as an electronic compass for determining aircraft direction relative to magnetic north.

NAV/COMM Radio :

• Full VHF navigation capabilities including VOR/ILS with localizer and glide-slope.
• Communication channels: 760 with 25 kHz spacing; 2280 channels with 8.33 kHz spacing.
• Frequency range: 118.000 to 136.992 MHz.
• Transmit power: 10 W, with optional 16 W enablement.
• Input voltage range: 9–33 V DC.
• Operating temperature: -20 °C to +55 °C.
• Certifications: TSO C169a, TSO C128a, TSO C34e, TSO C36e and TSO C40c.
• Dimensions: 1.35" H × 6.25" W.
• Weight: 2.3 lb unit only; 3.1 lb with mounting rack and connectors.
• Depth: 10.32 inches behind panel including mounting rack and connectors.
• Worldwide frequency database.
• Automatic Morse code station identification.
• Standby VOR frequency monitoring and received radial display.
• Active and standby NAV frequency flip-flop.
• OBS setting and supplemental CDI display for VOR/localizer.
• Distance display to VOR navaid when connected with compatible GPS source.
• Interfaces with CDI, HSI, autopilot systems and primary flight displays.
• Automatic or manual squelch.
• Airport frequency lookup including tower, ground, ATIS and clearance delivery.
• Standby frequency monitoring.
• Frequency memory and recall.
• Emergency frequency selection.
• Built-in count-up/count-down timer.
• Remote tuning through compatible flight display touchscreen. :contentReference[oaicite:3]{index=3}

Advanced Audio Control Panel :

Intercom Functions :

• Positions: 6 including pilot, copilot and 4 passengers.
• Volume controls: 2 including pilot and copilot/passengers.
• VOX: Automatic, 1 per MIC input.
• Modes: Pilot, crew and all.
• MIC impedance: 150 ohms.
• MIC bias: 11 V DC through 470 ohms.
• Keyed ICS: Configurable.

Audio Inputs :

• Impedance: 600 ohms.
• Maximum input: 5 Vrms.
• Isolation: 60 dB minimum.
• Bandwidth: 100 Hz to 6.5 kHz.
• Transceiver: 3 including TEL.
• Receiver: 5 including NAV1, NAV2, AUX1, AUX2 and AUX3.
• Alerts: 4 unswitched.
• Telephone input: 1.

Bluetooth :

• Supported profiles: A2DP and AVRCP for music and HFP for phone.
• Paired devices stored: 10.
• Connections allowed: 1 device.
• Supported devices: Phones, tablets and compatible devices.
• Volume set by device and adjustable on display.
• Distortion: <0.1% THD+N typical at full power over full bandwidth.
• Firmware updates: Free and field-loadable by SD card.

Headsets Outputs :

• Three stereo output amplifiers for pilot, copilot and passenger.
• Output power: 65 mW into 150 ohms for pilot and copilot.
• Output power: 260 mW into 37.5 ohms for passenger.
• Distortion: <3% THD+N at 10% power; <10% THD+N at full power.
• Frequency response: 20 Hz to 20 kHz.
• Rated impedance: 150 ohms for pilot/copilot and 37.5 ohms for passenger.
• Supports 4–150 ohm headsets.
• Supported impedance: 150 to >600 ohms.

USB Charge Port :

• Rated power: 10 W.
• Maximum charge current: 2.1 A.
• Over-current protection above 2.3 A.
• Supports any USB device.
• Charging scheme: DCP.

Speaker :

• Outputs: 1.
• 28 V aircraft: 10 W into 4 ohms; 7 W into 8 ohms.
• 14 V aircraft: 3 W into 4 ohms.
• Bandwidth: 350 Hz to 6.5 kHz.
• Distortion: <10% THD+N at full power; <3% THD+N at 10% power.

Voice Recorder :

• Maximum recording time: 1 minute.

Code Load Options :

• SD Card.

Environmental Specifications :

• Operating temperature: -20 °C to +55 °C.
• Altitude range: up to +55,000 ft MSL, unpressurized.
• Power requirements: 11–33 V DC input.

Pitot/Static Test System :

• System control switch.
• Pitot source control valve.
• Static source control valve.
• Cross control valve.
• Relief valve.
• Two special pumps.
• Hoses.

Dual Headset :

• 24 dB NRR hearing protection.
• 3.5 mm music input port.
• Noise-reflective cup microphone.
• Performance audio speakers.
• Foam-fit comfort ear seals.
• Deep-pocket ear canals.
• Wind-block foam microphone muff.
• Stainless-steel adjustable headband.
• Industry-standard 3.5 mm music input jack.

VOR/LOC/GS Antenna :

• Application: VOR/LOC/GS, receive only.
• Frequency: 108–118 MHz, 328–336 MHz.
• Impedance: 50 ohms nominal.
• VSWR: 2.0:1 maximum.
• Pattern: Omni-directional.
• Connector: Threaded studs to accept transmission line assembly with integral balun transformer.
• Maximum weight: 11 oz.
• FAA TSO: C40c.
• Width across tips: 23-1/2".

COM Antenna :

• Application: Airborne communications.
• Frequency: 118–137 MHz.
• Impedance: 50 ohms nominal.
• VSWR: 2.0:1 maximum.
• Polarization: Vertical.
• Pattern: Omni-directional.
• Connector: Type BNC female.
• Maximum weight: 8 oz.
• Maximum height: 20-1/4".
• RF power capacity: 25 W.

Marker Beacon Antenna :

• Application: Marker beacon.
• Frequency: 75 MHz.
• Impedance: 50 ohms nominal.
• VSWR: 1.4:1 maximum.
• Maximum weight: 0.5 lb.
• Maximum height: 2.2.
• RF power capacity: Receive only.

GPS Antenna :

• GPS antenna.

OAT Temperature Probe :

• Provides raw air temperature data.

Transponder :

• IFR-certified 250 W transponder.
• Optional 1090 MHz ES broadcast technology.
• Easy-to-read LCD display.
• Traffic Information System (TIS-A) alerts on compatible displays.
• Pressure altitude and dedicated VFR squawk button.
• Panel-mounted Mode S digital transponder with traffic data link capability.
• Mode A/C and S.
• Transmit power: 250 W nominal.

Engine Data Modules :

• Supports popular four- and six-cylinder engine installations.
• Measures engine and environmental parameters including:
  • 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
  • Flap and Trim Potentiometers
  • External Contacts

• Navigation instrumentation including VOR, ILS and GPS.
• Communication instrumentation with VHF.
• Navigational information.
• Primary flight instrumentation.
• Aircraft systems instrumentation.
• Three degrees of freedom system for ADAHRS pitot-static system.
• Pitot-static system for conducting pitot-static system checks for digital instruments.
• NAV system testing.
• COM system testing.
• Transponder – Mode A/C-S.
• Altimeter.
• Encoding altimeter.
• Altitude simulation.
• Six metal drawers.
• All required cabling, couplers, splitters and sockets.
• Instructor's panel for fault insertion.
• Extension cable for GPS antenna.
• Tripod stand for mounting GPS antenna.
• System mounted on a metal/aluminum mobile stand.
• Metal/aluminum frame with four wheels; two of four wheels are lockable.