Avionics & Glass Cockpit System Trainer 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. :contentReference[oaicite:0]{index=0}

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, pitot-static testing, NAV and communication testing, altitude simulation and an instructor's panel for fault insertion. :contentReference[oaicite:1]{index=1}

The trainer includes engine sensors, throttle and propeller controls, electronic sensor simulation and an engine data monitoring system for practical aircraft systems training. It is mounted on a mobile metal/aluminum stand with four wheels, two of which are lockable.

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
• NAV/COM Radio with VOR/ILS and VHF COMM
• 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
• VHF-COM Antenna
• VHG-COM 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.

Music Functions :

• Inputs: 2, independent from Bluetooth audio.
• Impedance: 600 ohms differential.
• Maximum input: 3.0 Vrms.
• Gain: +24 dB maximum / -96 dB minimum.
• Input level: <200 mVrms at maximum gain for full power output.
• 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 for pilot and copilot/passenger.

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 :

• 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.

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.
• Pitot tube included as part of the system.
• NAV system testing.
• COM system testing.
• 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.