7ER Anti-Ice Flashcards

(33 cards)

1
Q

How can you tell if an ice detector is installed?

A

The presence of an ICING light, either below the ENG ANTI-ICE switches (757) or above the ENGINE ANTI-ICE selectors (767)

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2
Q

How many TAT probes are there?

A

752: one or two

753: two

767: one

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3
Q

What is the meaning of an EICAS advisory ICE DET OFF?

A

Ice is no longer detected (the ICING light will go out)

Only present on “switch” aircraft

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4
Q

What does an EICAS advisory WINDOW HEAT mean?

A

Two or more flight deck windows are not being heated

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5
Q

When is engine anti-ice required on the ground?

A

After engine start and during all ground operations when icing conditions exist or are expected

Not required when OAT is less than -40c

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6
Q

What is the definition of icing conditions on the ground?

A

TAT of 10c and below

Visible moisture (including visibility of <1sm or <1600m), or standing water/slush/snow/ice

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7
Q

When is engine anti-ice required in flight (757)?

A

When in visible moisture with a TAT of 10c or below

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8
Q

When is anti-ice required in flight (767)?

A

When in visible moisture, except during climb and cruise when SAT is less than -40c (required for descent regardless of temperature)

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9
Q

When is wing anti-ice required?

A

In flight, with ice accumulation on window frames, wiper arms, or side windows

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10
Q

When are the probes heated?

A

When at least one engine is operating

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11
Q

Can APU air be used for anti-ice?

A

No. It is physically possible, but will not provide enough bleed air

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12
Q

During single-engine taxi with engine anti-ice on, what is the required pack configuration?

A

Single pack, same side as operating engine

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13
Q

On “selector airplanes”, what is the configuration on the ground when anti-ice is required, and how is it changed during the After Takeoff Flow?

A

Wing - OFF, Engines - ON

after takeoff, all selectors to AUTO

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14
Q

On “selector airplanes”, what is the configuration on the ground when anti-ice is not required, and how is it changed during the After Takeoff Flow?

A

WING - OFF, engines - AUTO

After takeoff, all to AUTO

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15
Q

When is wing anti-ice inhibited?

A

On the ground

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16
Q

On what aircraft will the EICAS advisories ICE DET ON and ICE DET OFF display?

A

“Switch” aircraft that are equipped with ice detectors

17
Q

What parts of the wing does wing anti-ice heat?

A

The three midwing slats (757)

The three outboard slats (767)

18
Q

What is the bleed air source for wing anti-ice?

A

The bleed air manifold

19
Q

What is the meaning of an illuminated CAPT or FO PITOT light?

A

The affected probe is not being heated when it should be, or both engines are not running on the ground (normal before engine start, will not generate an EICAS message)

20
Q

What is the meaning of an illuminated ICING light on “switch” aircraft?

A

“Switch” aircraft: the ice detector has detected ice (EICAS advisory ICE DET ON displayed)

21
Q

On “Selector” aircraft, what would be the indications of a failed anti-ice valve?

A

Selectors AUTO, ICING light, and VALVE light.

(EICAS caution ICING ENGINE or advisory ICING WING, and associated advisory ENG ANTI-ICE or WING ANTI-ICE)

22
Q

What is the meaning of a Window Heat INOP light?

A

The affected window is not being heated

23
Q

On “Selector” aircraft, what is the meaning of an ICE DET light?

A

The ice detection system has failed (EICAS advisory ICE DETECTOR message)

24
Q

What is the indication of the wing anti-ice being automatically turned on?

A

There are none, unless you see the VALVE lights momentarily light up as the valves move

25
How is each side’s wIper controlled?
Either captain’s or FO’s wiper switch controls both wipers
26
If engine anti-ice is selected on, but there is insufficient pneumatic pressure, what position do the valves move to?
They stay closed
27
What effect does engine anti-ice have on N1 limits? (GE only)
The N1 limit will decrease when engine anti-ice is on
28
If a landing is made with wing anti-ice on, what will happen at touchdown?
The valves will close
29
How are the engine and wing anti-ice valves controlled and operated? Do they have a fail position?
Electrically controlled, pneumatically operated. The fail position is the last position
30
When should wing anti-ice not be used in flight?
When TAT is greater than 10c
31
How many windows does each window heat switch control?
FWD - one SIDE - two
32
On “Selector” aircraft, what position will the anti-ice valves be in if AUTO is selected on the ground?
The valves will be closed, and must be manually opened if needed by moving the selector to ON
33
What is the meaning of an ICING light on “selector” aircraft?
The ice detector has detected ice and engine and/or wing anti-ice is selected OFF or an anti-ice valve is closed (EICAS caution ICING ENGINE and/or advisory ICING WING displayed).