Avionics Trainer with PFD System

The trainer enables trainees to gain hands-on experience with avionics equipment and a Primary Flight Display (PFD) system. It provides practical training using original avionics equipment configured to bring real-life experience into the training environment, supporting a good understanding of avionics and cockpit equipment and a methodical approach to troubleshooting. :contentReference[oaicite:0]{index=0}

The trainer is delivered as a plug-and-play system with necessary antennas, transmitters, receivers, wiring and indicators. It can also be customized with indicators and avionics devices according to specific training requirements. :contentReference[oaicite:1]{index=1}

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

Differences from Previous Configuration :

• No Engine Monitoring System
• No Pitot / Static System and Test Set
• No Engine Sensors
• No Throttle Lever
• No Contact Sensors
• No Electronic Simulation of Sensors
• No Dynamic Microphone

Components :

• Smart PFD-MFD Screen
• NAV/COM Radio with VOR/ILS
• Analog NAV Indicators
• GPS (Global Positioning System)
• ADF (Automatic Direction Finder)
• ADF Indicator
• ILS (Instrument Landing System)
• DME (Distance Measuring Equipment)
• Transponder
• Marker Beacon
• Intercom System
• Two Pilot Headsets
• DC Power Box
• Aircraft Circuit Breaker

Antennas :

• VOR/LOC Antenna
• ADF Antenna
• Marker-Beacon Antenna
• Antenna Splitter
• VHF-COM Antenna
• Transponder Antenna
• All Antenna Cables

Components Technical Specifications :

NAV/COM Device :

• NAV/COMM transceiver.
• 200-channel NAV receiver.
• Built-in VOR converter.
• Maximum 25 kHz channel spacing.
• COM frequency: 118.000 to 136.975 MHz.
• NAV frequency: 108.00 to 117.95 MHz in 50 kHz spacing.
• VOR/LOC converter.
• Input voltage: 28 V DC.
• Built-in VOR/Localizer converter.
• Flip-flop frequencies.
• Volume control.
• Frequency memory and recall.
• Display.
• Frequency stability: ±0.0015%.

NAV Indicator :

• Navigation indicator containing VOR/LOC left-right needle.
• To-From indicator.
• VOR/LOC warning flag.
• OBS.
• Integral VOR/LOC converter.
• Glide-slope deviation needle.
• Metal bezel with glass lens.

Transponder :

• Transmitter frequency: 1090 MHz ±3 MHz.
• Receiver sensitivity: -73 dBm nominal; -69 dBm minimum for 90% reply.
• Mode A, C.
• Input voltage: 14/28 V DC.

DME Device :

• 200-channel receiver.
• Channeling sources through external control head providing BCD code, 2×5 code, slip code or serial code.
• RMT/FREQ/GS-T mode.
• DME two-concentric-frequency knob.
• Frequency display.

ADF Device :

• Frequency range: 200 kHz to 1799 kHz in 1 kHz increments.
• Bearing accuracy: ±3 degrees from 70 µV/m to 0.5 V/m RF input signal level.
• Receiver sensitivity: 150 µV/m maximum for S+N/N = 6 dB.
• Receiver selectivity:
  • 6 dB bandwidth: ±2 kHz maximum off-center frequency.
  • 80 dB bandwidth: ±7 kHz maximum off-center frequency.
• Power requirements: 11 to 33 V DC, 12 W.
• ADF button.
• BFO button.
• FRQ button.
• FLT/ET button.
• SET/RST button.
• VOL/OFF knob.
• Frequency display.

ADF Indicator :

• Single-needle ADF indicator for use with ADF receiver.
• ADF bearing input: DC sine and cosine voltages, ±3.0 V DC maximum across each winding.
• Compass card drive: 12 V DC at 0.12 A.
• Lighting: 14 V DC at 0.16 A or 28 V DC at 0.08 A.

Audio Panel :

Audio Inputs :

• Impedance: 600 ohms.
• 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.

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.

Music Functions :

• Inputs: 2, independent from Bluetooth audio.
• Impedance: 600 ohms differential.
• 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.

Headphone Outputs :

• Output amplifiers: 3 stereo 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.

Speaker :

• Outputs: 1.
• 28 V: 10 W into 4 ohms; 7 W into 8 ohms.
• 14 V: 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.

Headsets :

• 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.

Smart PFD-MFD Screen :

• High-brightness, high-resolution display driven by advanced graphics processors.
• Display resolution: 1280 × 800 pixels.
• 1200+ nit TFT active-matrix capacitive multi-touch LCD screen.
• High-definition touch screen.
• 37-pin DIN connector for the main wiring harness.
• Four RS-232 connector ports for connection to compatible equipment.
• Configurable baud rates and data formats for serial ports.
• Two USB connectors.
• Ethernet connector for synchronizing data between displays.
• Operating voltage: 10–30 V DC.
• Displays engine instrument data.
• Displays flight instrument data.

Screen Dimensions :

• Width: 7.64"
• Height: 5.59"
• Depth: 3.13"

Display Controls and Functions :

• Two knobs.
• Two buttons integrated into the knobs.
• Eight buttons along the bottom of the display bezel.
• Touch gestures through the display screen.
• GPS moving map.
• Automatic backlight adjustment through ambient light sensor.
• Manual brightness adjustment through buttons.
• Default screen layout includes PFD, MAP and ENGINE.
• 100% window or 50%/50% split windows.
• Count-up/count-down timer.

PFD Page Layout :

• Airspeed Indicator
  • Ground Speed (GS)
  • True Airspeed (TAS)
• Airspeed Bug
• Airspeed Trend Rate
• Attitude Indicator
• Flight Path Marker
• Altimeter
  • Barometric Setting (BARO)
• Altitude Bug
• Altitude Trend Rate
• Barometer Setting
• 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 :

• Six Pack
• G-meter
• Terrain Alert
• Airport Flags
• HSI SRC
• Bugs

Main Menu Functions :

• NRST – Nearest
• Info Page
• FPL – Flight Plan
• INFO
• MENU
• Message: NO MSG / MESSAGE / CAUTION / WARNING

Knob Functions :

• Adjust Bug values such as HDG and ALT or BARO value.
• Change map scale.
• Activate and/or move cursor.

Flight Data Modules :

• All sensors are solid-state.
• Accelerometers measure forces in all three directions.
• Rotational rate sensors sense rotation about all three axes.
• Pressure transducers measure air data.
• Magnetometers on all three axes measure magnetic heading.

Documentation :

• User's Manual
• Study Guide
• Instructor's Guide
• Device's Original Manual
• Device's Original Wiring Diagrams
• Training Video for Teachers

Power Specifications :

• Electrical Box
• Residual Current Device
• Emergency Button
• Energy Signal Lamp
• 110 VAC, 60 Hz or 220–240 VAC, 50 Hz

Accessories :

• Instructor's Panel Control Box for Scenario and Fault Simulation

• Navigation instrumentation including ADF, DME, VOR, ILS, GPS and transponder.
• Communication instrumentation with VHF.
• Navigational information.
• Primary flight instrumentation.
• Aircraft systems instrumentation.
• Roll, pitch and yaw motions can be operated from the side yoke to demonstrate aircraft attitude and directional gyro functions.
• Primary flight display mounted on a panel capable of simulating roll, pitch and yaw movements controlled by a mechanism operated by a control yoke.
• NAV system testing.
• COM system testing.
• Transponder identification.
• DME channel selection.
• Six metal drawers.
• All required cabling, couplers, splitters and sockets.
• 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.