Ice and Rain Protection Flashcards
The aircraft’s electrical system is used to heat (5):
Flight deck windshields, Air Data Smart Probes, TAT probes, water lines, static port
What uses bleed air for ice protection?
Engine cowls, three outboard slats
What part of the engine is heated?
Only the engine cowls are anti-iced.
What control surfaces are heated by the wing anti ice system?
3 outboard slats
Can the APU be used to provide bleed air for the anti-ice system?
No.
What happens if there is a single bleed source failure?
The crossbleed automatically opens and uses opposite bleed for both wings.
When in flight with a single AC source available, the ________ windshield will be heated.
Only the left.
In flight with a single AC source available, the ___________ windshield will be heated if the left fails.
Right.
Sources for aircraft anti-icing are:
Bleed air and electric
Which panels on the wing do not have ice protection?
Inboard slats, flaps and spoilers
What uses electrical power to prevent icing?
ADSPs, TAT probes, windshield, static port, water lines
What is heated at engine start?
ADS probes, TAT probes, water lines and static port
If an engine fails, does the opposite wing receive ice protection?
Yes, the crossbleed valve opens and uses opposite bleed for both wings.
If an engine fails, does the respective engine receive icing protection?
No, the failed engine does not receive heat to the engine cowl.
How long will the engine and wing anti-ice system remain on after icing is no longer detected?
2 or 5 minutes (epic load dependent).
Is the ice protection system automatic?
Yes, under normal conditions.
Can the pilot override the automatic ice protection system?
Yes, by selecting the ICE PROTECTION selector knob to ON.