Anti skid & Auto brake System Training Set Two Wheels

Our Anti-Skid and Auto-Braking System Trainer is designed to represent the anti-skid braking system, which is one of the essential components of modern jet aircraft.

This training set provides practical maintenance training for technicians. Hands-on training ensures that trainees not only understand the theory but are also well prepared to maintain anti-skid braking systems in practice. The training set includes a typical hydraulic brake system along with anti-skid assemblies and components.

This training set contains two wheels.

Manufactured by Atico Export with quality-focused production and attention to engineering specifications for teaching and training purposes.

Trainer Functions :

• Auto-brake function
• Anti-skid function
• Foot brake function
• Rejected take-off function
• WOW switch function
• Brake fan function
• Pump fault function
• ECAM functions
• Single chime functions
• Master caution functions
• Master warning functions

Trainer Processes :

• Take-off process
• Landing process
• Anti-skid fault process
• System test process

Trainer Cases :

• Brake hot
• Park brake fault
• Hydraulic fault
• Auto-brake fault
• Instructor's panel for fault insertion

Components :

Control Panel :

• Aural warning horn

• Master warning resettable illuminated pushbutton

• Master caution resettable illuminated pushbutton

• Auto-brake – low illuminated pushbutton

• Auto-brake – medium illuminated pushbutton

• Auto-brake – max illuminated pushbutton

• Auto-brake – RTO illuminated pushbutton

• Auto-brake – disarm instrument

• Anti-skid INOP instrument

• Brake fan control illuminated pushbutton

• Brake fan hot instrument

• Nose landing gear instrument light

• Left wing landing gear instrument light

• Right wing landing gear instrument light

• Landing gear unlock instrument light

• Hydraulic pump control illuminated pushbutton

• Hydraulic pump fault instrument light

• Three (3) aircraft circuit breakers

• Guarded master power switch

• Master power lamp

• Lockable landing gear control lever

• AC engine on/off switch

• Air/ground switch

• Skid simulation panel

• 10-inch screen similar to EICAS or ECAM

  • Landing gear position
  • Landing door position
  • Numeric pressure value
  • Sensor status
  • Anti-skid/Auto-brake position status
  • Numeric simulated airspeed value

• Electronic Control Box (Antiskid Control Computer)

• Antiskid Valve

• TQ – Throttle Quadrant

• Electrically Driven Hydraulic Pump

• Hydraulics Filter

• Hydraulic Fluid Reservoir

• Hydraulics Tank Drain Valve

• Check Valve

• Brake Fan

• 0–100 bar Hydraulic System Analog Pressure Gauge

• 0–100 bar Hydraulic System Pressure Sensor

Aircraft Landing Gear Module :

• Two (2) pieces aircraft tires

• Two (2) pieces aircraft wheels

• Two (2) pieces aircraft brake systems

• Two (2) pieces AC motors for turning the wheels

• Plexiglass cover

• Aircraft Foot Brake Pedal

• Aircraft Foot Brake Master Cylinder

• Brake Microswitch

• Two (2) pieces AC motors for turning the wheels

• Two (2) pieces AC motor drivers

• Fault & Instructor Port

• Lockable Fault & Instructor Box

• The system is mounted on a metal/aluminum mobile stand

• Metal/aluminum frame with 4 wheels; 2 of 4 wheels are lockable

• Training video for teachers

• Delivered fully assembled, tested and ready to operate

• Colored ultraviolet printing method on aluminum composite panel

Documentation :

• User's Manual
• Study Guide
• Instructor's Guide
• Components Diagrams

Power Specs :

• Electrical box
• Residual current device
• Emergency button
• Energy signal lamp
• 110 VAC, 60 Hz or 220–240 VAC, 50 Hz

Dimensions and Weight :

• Height: 200 cm
• Width: 140 cm
• Depth: 85 cm
• Weight: 150 kg

• Understanding fundamentals of aircraft auto-brake/anti-skid systems and their components
• Anti-skid and auto-brake systems can work together and independently
• Non-operation of auto-brake scenario is implemented
• Operation of auto-brake scenario is implemented
• Take-off scenario is implemented
• Landing scenario is implemented
• Auto-brake scenarios are implemented
• Rejected take-off scenario is implemented