Ice And Rain Protection Flashcards
1
Q
How is anti-icing provided to the aircraft?
A
- Bleed air
- Electrical heating
2
Q
Which components of the aircraft have anti-icing?
A
- 3 outboard wing slats (bleed)
- leading edge of engine nacelles (bleed)
- pitot tubes (electrical)
- Static ports (electrical)
- waste water drain masts (electrical)
- Flight deck windows (electrical)
3
Q
When do icing conditions exist?
A
- OAT is 10°C or below
- Visible moisture is present
4
Q
Can wing anti-ice be used with slats extend it?
A
Yes, but should be avoided
5
Q
How is window heating controlled?
A
With the two window heat computers (WHC)
6
Q
When are the windows heated?
A
- Automatically on the ground with one engine running
- in-flight
- When the probe/window heat pb is pushed
7
Q
What is the limitation for using the windshield wipers?
A
- 230 kts
- Do not use on dry window
8
Q
What’s a limitation exists for the rain repellent?
A
- Do not use on dry window
- use only on moderate to heavy rain conditions
9
Q
How is probe heating controlled?
A
Probe heat computer (1/2/3)
10
Q
When are the probes heated?
A
- On the ground with one engine running
- in-flight
- when probe/window heat pb is on