Anti-Skid & Auto-Break System Training Set (Two Wheels)
Categories: Aviation Maintenance Training EquipmentFeatures: Understanding fundamentals of aircraft auto-brake/anti-skid and its components. Anti-skid and auto-brake system able to work together and independently Non operations o...
Product
Description
Features:
- Understanding fundamentals of aircraft
auto-brake/anti-skid and its components.
- Anti-skid and auto-brake system able to work together
and independently
- Non operations of auto-brake scenario are implemented
- Operations of auto-brake scenario are implemented
- Take off scenario is implemented
- Landing scenario is implemented
- Auto-brake scenarios is implemented
- Rejected take off scenario is implemented
- Some of Trainer Functions
- Auto-brake function
- Anti-skid function
- Food brake function
- Rejected take off function
- WOW switch function
- Brake fan function
- Pump’s fault function
- ECAM functions
- Single chime functions
- Master caution functions
- Master warning functions
- Some of Trainer Processes
- Take-off process
- Landing process
- Anti-skid fault process
- System test process
- Some of 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 gear instrument light
- Landing gear unlock instrument light
- Hydraulic pump control illuminated
pushbutton
- Hydraulic pump fault instrument
light
- Three (3) aircraft circuit breaker
- 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 (like EICAS or ECAM)
- Landing gear position
- Landing door position
- Numeric pressure value
- Sensor’s status
- Anti-Skid/Auto-Brake position status
- Numeric Simulated air speed 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 Tire
- Two (2) pieces Aircraft Wheel
- Two (2) pieces Aircraft Brake system
- Two (2) pieces AC motor for turning
the wheels
- Plexiglass cover
- Aircraft foot Brake Pedal
- Aircraft foot Brake master cylinder
- Brake microswitch
- Two (2) pieces AC motor for turning the wheels
- Two (2) pieces AC motor driver
- Fault & instructor port
- Lockable Fault & instructor box
quick overview :
Features:
- Understanding fundamentals of aircraft
auto-brake/anti-skid and its components.
- Anti-skid and auto-brake system able to work together
and independently
- Non operations of auto-brake scenario are implemented
- Operations of auto-brake scenario are implemented
- Take off scenario is implemented
- Landing scenario is implemented
- Auto-brake scenarios is implemented
- Rejected take off scenario is implemented
- Some of Trainer Functions
- Auto-brake function
- Anti-skid function
- Food brake function
- Rejected take off function
- WOW switch function
- Brake fan function
- Pump’s fault function
- ECAM functions
- Single chime functions
- Master caution functions
- Master warning functions
- Some of Trainer Processes
- Take-off process
- Landing process
- Anti-skid fault process
- System test process
- Some of 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 gear instrument light
- Landing gear unlock instrument light
- Hydraulic pump control illuminated
pushbutton
- Hydraulic pump fault instrument
light
- Three (3) aircraft circuit breaker
- 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 (like EICAS or ECAM)
- Landing gear position
- Landing door position
- Numeric pressure value
- Sensor’s status
- Anti-Skid/Auto-Brake position status
- Numeric Simulated air speed 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 Tire
- Two (2) pieces Aircraft Wheel
- Two (2) pieces Aircraft Brake system
- Two (2) pieces AC motor for turning
the wheels
- Plexiglass cover
- Aircraft foot Brake Pedal
- Aircraft foot Brake master cylinder
- Brake microswitch
- Two (2) pieces AC motor for turning the wheels
- Two (2) pieces AC motor driver
- Fault & instructor port
- Lockable Fault & instructor box
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