ATA 30 - Ice And Rain Protection Flashcards

1
Q

When to use engine anti ice ?

A

OAT (ground) or TAT (inflight) =< 10°C + visible moisture/contaminated surfaces
except during climb or cruise if SAT =< -40°C ( not descent)

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2
Q

If engine anti ice is ON, continuous ignition is automatically ON. True or False ?

A

True ( only on some MSN )

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3
Q

How is engine anti iced ?

A

Air from HP compressor into leading edge of the nacelle

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4
Q

What is the position of engine anti ice valve when in emergency electrical configuration ?

A

OPEN

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5
Q

Which slats are anti iced ?

A

Slats 5, 4, 3
___ ___ ___ ___ ___|
5 4 3 2 1

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6
Q

When wing anti ice is used ?

A

Ice on ice indicator or/and on wipers

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7
Q

Can wing anti ice be used on ground ?

A

No. If you put it ON —> 30s self test only

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8
Q

Position of the wing anti ice valve if emergency electrical configuration ?

A

CLOSED if on BAT only.
If EMER GEN running —> available !

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9
Q

Position of the wing anti ice valve in case of leak detected ?

A

CLOSED

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10
Q

How many Window Heat Computer ?

A

2 WHC, 1 each side

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11
Q

When windows/windscreen is heated ?

A

AUTO: inflight or on ground 1 engine running
ON: …

Windows: 1 level of heat
Windscreen: Low on ground, High in flight

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12
Q

How many Probe Heat Computer ?

A

3 PHC (1CdB, 1 Sby, 1FO)

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13
Q

When probes are heated ?

A

AUTO: inflight or on ground 1 engine running
ON: …

AoA & SAT: 1 level
Pitot: Low on ground, high inflight
TAT: inflight only

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14
Q

On ground, when is the rain repellent system inhibited?

A

Both engine off

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15
Q

The ENGINE ANTI-ICE VALVE closes in case of low AIR PRESSURE. True or False ?

A

True. E.g. in case of engine shutdown.

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16
Q

In case of window heat computer failure, the other computer can replace the failed one ?

A

No. One computer per side

17
Q

What is the consequence on N1 idle and max limit of the ENG or WING A/I ?

A

N1 idle is increased and max limit is decreased

18
Q

Can you land with WINGS A/I ON ?

A

No except if severe icing conditions (cf SOP when extending flaps Full)

19
Q

After how many seconds ECAM msg ICE NOT DETECTED is displayed ?

A

190s

20
Q

Which probe between AoA, TAT, SAT and pitot is not heated on ground ?

A

TAT

21
Q

What are the impact on climb gradient in case of an open WING A/I valve ? (MEL)

A

5000kg in case of «hot T°» (ISA+5)

22
Q

ENG A/I may be operative even if ENG BLEED off. True or False ?

A

True (cf Bleed system diagram)