ATA 30 ICE AND RAIN PROTECTION

Which subsystems are part of the ice and rain protection system on the Airbus A320 family aircraft?. All above. Probe ice protection. Windshield ice and rain protection.

How is wing anti-ice supply controlled for both wings?. By a single pushbutton switch on the overhead ANTI ICE panel. By manual control in the cockpit. By the engine's bleed air automatically.

When is engine air intake anti-ice protection available?. In flight or on the ground with the engine running. Automatically when the aircraft is powered. Only on the ground.

What is used to protect the Angle Of Attack (AOA) sensors, pitot probes, static ports, and Total Air Temperature (TAT) probes from ice?. Electrical heating. Engine bleed air. Manual insulation covers.

How is windshield anti-icing provided on the Airbus A320 family aircraft?. Automatically when at least one engine is running. By electrical heating. By hot air from the pneumatic system.

Under what conditions is the drain mast heating switched ON?. When the electrical system is powered. It is always in operation. When the temperature is above a specific value.

The front windshields and side windows are heated ____________ when at least one engine is running. automatically. during takeoff. with wipers.

The Drain Mast Heating is switched ON when the temperature is ____________ a specific value. below. not related to. exactly at.

What subsystem protects the engine air intake from ice?. Engine air intake ice protection. Drain mast ice protection. Windshield ice and rain protection.

Which part of the aircraft's electrical system heats the water and waste system for ice protection?. Hot air from the pneumatic system. Engine bleed air. Electronic ice detection system.

How is the operation of the rain repellent system controlled on the CAPT and F/O sides?. Independently. Manually. Automatically.

What is used to initiate a new cycle of rain repellent fluid spray?. Release and press the P/B again. It starts automatically. Press and hold the P/B.

The wing anti-ice supply to both wings is controlled by a single pushbutton switch on the overhead ANTI ICE panel. true. false.

Engine anti-ice is only available in flight and not on the ground with the engine running. true. false.

the PROBE/WINDOW HEAT pushbutton switch is used to select windshield anti-icing when the engines are shut down. true. false.

each control unit CU regulates the heating temperature of the associated drain mast tube between_____. 6°c (43°f) to 10°c (50°f). 15°c (59°f) to 15°c (59°f). 10°c (50°f) to 20°c (68°f).

the system status is sent to the cabin intercommunication data system CIDS for indication on the_______. flight attendant panel FAP. centralized fault display interface unit CFDIU. Maintenance logbook.

if there is a failure of the heater HTR or CU a________ light is illuminated on the flight attendant panel FAP. CAUTION. MAINTENANCE. RED.

the drain mast data is stored in the ___________. centralized fault display interface unit CFDIU. maintenance logbook. aircraft central server.

to perform a complete test of the drain mast system, two test must be carried out, one from the MCDU and the second one on each. control unit CU. aircraft. flight attendant.

the thermal switch in the AC power supply line within the drain mast open at 120° c (250°f). true. false.

the system status is sent to the centralized fault display interface unit CFDIU for indication. true. false.

if there is a failure of the heater HTR or CU a green light is illuminated on the flight attendant panel FAP. false. true.