Untitled Quiz DE AVION TIPO

1-    The ice and rain protection system prevents ice formation from the subsequent airplane parts:

• -       Wing Leading Edges (pneumatically de-iced)

  -       Engine Inlet Cowls (pneumatically de-iced)

  -       Air Data Probes (electrically de-iced)

  -       Flight Compartment Windows (electrically de-iced)

  -       Water & Waste System Lines and Drains (electrically de-iced)

• -       Window Leading Edges (pneumatically de-iced)

  -       Engine Inlet Cowls (pneumatically de-iced)

  -       Air Data Probes (electrically de-iced)

  -       Flight Compartment Wing (electrically de-iced)

  -       Water & Waste System Lines and Drains (electrically de-iced)

The controls and indications for the ice and rain protection system

• are on the P-5 panel.

•   are on the P-4 panel.

The wing thermal anti-ice and the engine inlet cowl thermal anti-ice systems use

• use hot engine bleed air to prevent ice formation

• use hot electrically to prevent ice formation

The air data probes use:

• use electric heat to prevent ice.

• use heat pneumatic bleed to prevent ice.

Flight deck windows use electric heat to do these things:

• -       Decided ice formation on the wings

  -       Prevent fog on the wing

  -       Improve windshield impact strength.

• -       Prevent ice formation on the windows

  -       Prevent fog on the windows

  -       Improve windshield impact strength.

The windshields have these features to improve forward vision in heavy rain:

• -       Windshield wipers

  -       Hydrophobic (rain repellent) coatings.

• -       Windshield wipers

  -       Hydrophonetic (rain repellent) coatings.

    Electric heaters prevent freezing in the water and waste systems components

• false

• true

The pitot and static anti—icing system keeps ice off the air data probes.

•  This prevents false air data signals that ice causes.

•  This generated false air data signals that ice causes.

The air data probes use electric power for heat

• The probes have integral heaters

• The probes have integral pitot static

  The pitot and static anti—icing system supplies heat to these probes:

• -       Alpha vanes(2)

  -       Total air temperature probe (1)

  -      Pitot probes (5).

• -       Probe vanes(2)

  -       Total air temperature probe (1)

  -      Pitot probes (9).