| 1 |
Ice and Rain Protection (ATA 30) |
De-icing systems: Electric, with hot air,
pneumatic, chemical; Rain removal;
Heating of probes and drains; |
- |
| 2 |
Ice and Rain Protection (ATA 30)
Landing Gear (ATA 32) |
Wiper/wiper Systems.
structure, shock absorption;
Opening and collection systems; Normal and emergency; |
- |
| 3 |
Landing Gear (ATA 32) |
Indicators and warnings;
Wheels, brakes, anti-slip and auto-braking; |
- |
| 4 |
Landing Gear (ATA 32) |
Tires;
Steering (rudder);
Air location sensing. |
- |
| 5 |
Oxygen (ATA 35) |
System layout; cockpit, cabin;
Resources, storage, filling and distribution; |
- |
| 6 |
Oxygen (ATA 35) |
Supply setting;
Indicators and warnings. |
- |
| 7 |
Pneumatic/Vacuum (ATA 36) |
System layout;
Resources; Engine/API, compressors, reservoirs, ground supply; |
- |
| 8 |
- |
MID-TERM EXAM |
- |
| 9 |
Pneumatic/Vacuum (ATA 36) |
pressure control;
Distribution; |
- |
| 10 |
Pneumatic/Vacuum (ATA 36) |
Indicators and warnings;
Interface with other systems. |
- |
| 11 |
Water/Waste (ATA 38) |
Water system plan, replenishment, distribution, service and evacuation;
Toilet system layout, flushes and service. |
- |
| 12 |
Integrated Modular Avionics (ATA 42) |
Functions that can typically be integrated into Integrated Modular Avionics (IMA) modules include, among others:
Bleed Management, Air Pressure Control, Air Ventilation and Control, Avionics and Cockpit Ventilation Control, Temperature Control, Air Traffic Communication, Avionic Communication Router, Electrical Load Management, Circuit Breaker Monitoring, Electrical Systems BITE, Fuel Management, Braking Control, Steering Control, Landing Gear Opening and Closing, Tire Pressure Indicator, Oleo Pressure Indicator, Brake Temperature Monitoring, etc.;
Main System; Network Components. |
- |
| 13 |
Integrated Modular Avionics (ATA 42) |
Functions that can typically be integrated into Integrated Modular Avionics (IMA) modules include, among others:
Bleed Management, Air Pressure Control, Air Ventilation and Control, Avionics and Cockpit Ventilation Control, Temperature Control, Air Traffic Communication, Avionic Communication Router, Electrical Load Management, Circuit Breaker Monitoring, Electrical Systems BITE, Fuel Management, Braking Control, Steering Control, Landing Gear Opening and Closing, Tire Pressure Indicator, Oleo Pressure Indicator, Brake Temperature Monitoring, etc.;
Main System; Network Components. |
- |
| 14 |
Integrated Modular Avionics (ATA 42) |
Functions that can typically be integrated into Integrated Modular Avionics (IMA) modules include, among others:
Bleed Management, Air Pressure Control, Air Ventilation and Control, Avionics and Cockpit Ventilation Control, Temperature Control, Air Traffic Communication, Avionic Communication Router, Electrical Load Management, Circuit Breaker Monitoring, Electrical Systems BITE, Fuel Management, Braking Control, Steering Control, Landing Gear Opening and Closing, Tire Pressure Indicator, Oleo Pressure Indicator, Brake Temperature Monitoring, etc.;
Main System; Network Components. |
- |
| 15 |
- |
FINAL EXAM |
- |
| 16 |
- |
FINAL EXAM |
- |
| 17 |
- |
FINAL EXAM |
- |