Oral: Ice Protection/Detection Questions

Question 1

What sources are used for aircraft anti-icing and de-icing?

Answer 1

• Bleed air heat

* Electric heat

Question 2

What uses bleed air for ice protection?

Answer 2

• Engine lips

* 3 outboard slats

Question 3

What uses electric heat for ice protection?

Answer 3

• Smart probes
• Total Air Temperature (TAT) probes
• Windshields
• Water lines
• Pressurization static port

Question 4

If an engine fails does the opposite wing and engine receive ice protection?

Answer 4

• Yes. The crossbleed valve opens to provide symmetrical ice protection for both wings
• The failed engine does not receive heat to the engine lip

Question 5

How many ice detectors must be working to have icing detection?

Answer 5

One. There are two for redundancy

Question 6

How long will the de-icing system remain on after icing is no longer detected?

Answer 6

5 minutes

Question 7

If ‘ICING’ on the MCDU is set to ‘OFF’ and on takeoff roll icing conditions are encountered, will the de-icing systemturn on?

Answer 7

•Not until 1700 ft.or 2 minutes after takeoff (whichever happens first)

Question 8

Can the APU be used to provide bleed air for anti-icing?

Answer 8

No

Question 9

What is protected from ice & rain?

Answer 9

• Engine inlets
• Wing leading edge
• Smart probesand total air temperature probes
• Windshields
• Water & waste drain systems

Question 10

Is the ice protection system automatic?

Answer 10

Yes, under normal conditions

Question 11

Can the pilot override the automatic system?

Answer 11

Yes

Question 12

How is ice detected in flight?

Answer 12

1. 2 ice detectors
2. Vibrating sensor element that changes frequency when ice builds up around it
3. Once ice is detected, the sensor element heats, the ice melts, the normal vibrating characteristics arerestored, and the heating process stops. The cycle repeats as ice rebuilds on the probes

Question 13

What compressor stage is bleed air tapped for anti-icing operations?

Answer 13

10th High Stage Valve (HSV)

Question 14

How is bleed air directed for pneumatic anti-ice?

Answer 14

Engines&raquo_space;> Independent

Wings&raquo_space;> Onside bleed

Question 15

What happens if there is a single bleed source failure?

Answer 15

The crossbleed automatically opens

Question 16

How should the MCDU be set if there are icing conditions present on the ground?

Answer 16

‘ALL’

Question 17

What does selecting ‘ALL’ on the MCDU provide?

Answer 17

• Engine anti-ice&raquo_space;> ON when engines are running

* Wing anti-ice&raquo_space;> ON at 40 kts. wheel speed

Question 18

If ‘ALL’ is selected on the ground, at what point will the anti-ice system become automatic?

Answer 18

700’ AGL or 2minutes after takeoff (whichever happens first)

Question 19

If ‘OFF’ is selected on the ground, at what point will the anti-ice system become automatic?

Answer 19

1700’ AGL or 2 minutes after takeoff (whichever happens first)

Question 20

How does the failure of one of the two power sources affect the windshield heating system?

Answer 20

• On ground Inhibited

* In Flight Left side is heated (right heats if left has failed)

Question 21

What does the ‘TIMER’ selection on the windshield wiper switch do?

Answer 21

Activates the associated wiper in 8-second intervals

Question 22

What happens if the wiper is operated on a dry windshield?

Answer 22

The wiper will stopTo reset wiper move switch to ‘OFF’

Question 23

When do the smart probes heat?

Answer 23

When an engine is running

Question 24

Is there a test for the anti-ice system?

Answer 24

Yes, but maintenance performs this test

Question 25

How should the aircraft be configured for de-icing?

Answer 25

1. ) Bleeds :: OFF
2. ) Packs :: OFF
3. ) Stab trim :: Full nose down
4. ) Flaps :: UP
5. ) Engines and APU :: ON or OFF