Features:

1. Understanding fundamentals of aircraft Cabin Pressurization and its components.
2. The set is functional and configured like a typical aircraft Cabin Pressurization system.
3. The trainer includes the following panels that will work functionally.
   • Aircraft Cabin Pressurization panel
   • Aircraft air condition panel
   • Aircraft auto-pilot panel
   • Test panel
   • Master power panel
   • Master caution panel
4. Two transparent cabins in the training set to simulate the interior of the cabin.
5. Two (2) outflow valves, one (1) negative pressure safety valve, and  one (1) positive pressure safety valve (as a substitution) are in the transparent cabin.
6. The valves in the cabin pressurization system operate automatically during the take-off and landing.
7. Cabin pressurization valves are both controlled manually and automatically.
8. The trainer is able to perform fully automatic take-off and landing.
9. Indicators, panels and valves work simultaneously in landing and take-off simulations.
10. Take-off and landing simulations are controlled from the autopilot panel.
11. Vertica speed and altitude are determined and selected during take-off and landing.
12. Valve failures are easily observed on gauges and panels.
13. PACK VALVE, BLEED AIR, PACK FLOW and TEMPERATURE selections are made at the air condition panel.
14. Landing field elevation, MODE SELECT, MAN V/S CONTROL and DITCHING are done at the cabin pressurization.
15. The selections made in the panels are visible on the screen.
16. Wirings on the trainer are connected via terminals.
17. Wires should have clear identification labels for each wire.
18. All wires should be coded and labeled for troubleshooting.
19. The system mounted on a metal/aluminum mobile stand.
20. Metal/aluminum frame with 4 wheels. 2 of 4 wheels are lockable.
21. Delivered fully assembled tested and ready to operate
22. Colored Ultraviolet printing method on aluminum composite panel

Components:

1. Aircraft air condition panel

   • Pack-1 control

   • Pack-2 control

   • ENG 1 Bleed

   • ENG 2 Bleed

   • APU Bleed

   • Pack Flow Selector

   • X bleed control

   • Hot air Vale button

   • Cockpit, Forward Cabin, Aft Cabinet Temperature Knob

2. Aircraft Cabin Pressurization panel

   • Man V/S Control Switch

   • Mode selector Button

   • LDG ELEV Knob

   • Ditching Button

3. Aircraft auto-pilot control panel

   • Vertical Speed Selector

   • Altitude Knob

   • Sys Switch

   • Master switch and light

   • Circuit Breakers

4. Master power panel

   • Master power light

   • Master caution light

   • Aural warning horn

   • Test button

5. 10 inch Lower ECAM

   • Vertical speed indicator

   • Altimeter indicator

   • Cabin Altimeter

   • Cabin pressure

   • Air pressure

   • Differential pressure

   • Status area

     • Flow status

     • Pack flow status

     • Bleed status

     • Auto pilot status

     • Pressurization mode

     • Temp

     • Air/ground

6. Firewall Shutoff Valve – Pack Valve

7. Muffler

8. Heat Exchanger

9. Flow Control Valve and Pressure Control Valve

10. System Indicators – altimeter and cabin pressure

11. PSU (Passenger Service Unit)

12. Simulated Aircraft Cabin

    • Forward Out Flow Valve

    • Aft Out Flow Valve

    • Negative Pressure Safety Valve

    • Positive Pressure Safety Valve

13. Simulated Engine Bleed Valves

    • ENG-1 Bleed Air Valve

    • ENG-2 Bleed Air Valve

    • APU Bleed Air Valve

    • Cross-feed Valve

14. LAN output

15. Static Inverter to feed the Firewall Shutoff Valve (Pack Valve)

16. Compressor Connection Point to Simulate the Bleed Air