Ice & rain - Fire Protection - Electrical Flashcards

(50 cards)

1
Q

What is the source of heating for wing and cowl anti-ice?

A

6th or 10th stage bleed air

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2
Q

When is cowl anti-ice required to be ON during ground operations?

A

OAT ≤ 10°C

  1. in visible moisture
    (fog with visibility 1 sm or less, rain, snow, sleet, ice crystals),
  2. on contaminated ramps, taxiways or runways
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3
Q

When is cowl anti-ice required to be ON during flight?

A

TAT ≤ 10°C

  1. in visible moisture (such as clouds, rain, snow, sleet,
    or ice crystals) (except when SAT is ≤ -40°C),

or when ICE is annunciated

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4
Q

When is wing anti-ice required to be ON during ground operations?

A

OAT ≤ 5°C in visible moisture
(fog with visibility 1sm or less, rain, snow, sleet, ice crystals),

OAT ≤ 5°C on contaminated runways.

If Type II, Type III or Type IV deicing fluid has been applied,
select wing anti-ice ON just prior to thrust increase for takeoff.

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5
Q

When is wing anti-ice required to be ON during flight operations?

A

TAT ≤ 10° C in visible moisture (such as clouds,
rain, snow, sleet, or ice crystals)

with airspeed < 230 KIAS

except when SAT is ≤ -40° C, or when ICE is annunciated.

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6
Q

What is a good ICE detector test indication?

A

ICE caution message

ICE switchlight illuminated

ADS HEAT TEST OK advisory message.

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7
Q

What is the purpose of the Wing A/I cross-bleed switch?

A

To allow the bleed air from one engine to anti-ice

the opposite wing

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8
Q

What occurs with the Windshield Heat on LOW?

A

All 4 panels are heated to 24°C.

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9
Q

What occurs with the Windshield Heat on HIGH?

A

Side windows are heated to 24°C and both windshields

are heated to 41°C.

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10
Q

How many fire detection loops are installed on each engine?

A

Two, dual loops mounted in parallel.

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11
Q

How many firex bottles are available for an engine fire?

A

Two

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12
Q

What type of Halon is in the engine firex bottles?

A

Halon 1301 pressurized with dry nitrogen.

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13
Q

How is an engine fire detected by the crew?

A

Appropriate ENG FIRE PUSH switchlight illuminates,

fire bell sounds, and an EICAS warning message

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14
Q

What occurs when the ENG FIRE PUSH switchlight is pushed?

A

Fuel SOV closes,

HYD SOV closes,

Bleed air SOVs close,

generator is de-energized

and the appropriate squibs are armed

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15
Q

Can we blow both bottles into one engine, if necessary?

A

Yes.

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16
Q

How many fire detection loops are inside the APU containment case?

A

Two, dual loops

mounted in parallel.

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17
Q

How is an in-flight APU fire detected by the crew?

A

APU FIRE PUSH switchlight illuminates,

fire bell sounds,

APU FIRE warning message on EICAS.

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18
Q

How many firex bottles are available for an APU fire?

A

One.

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19
Q

What type of extinguishing agent is used in the APU firex bottle?

A

Halon 1301 pressurized with dry nitrogen.

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20
Q

What occurs during an unattended APU fire on the ground?

A

APU ECU shuts down the APU.

5 seconds later, the APU bottle will discharge automatically.

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21
Q

What occurs during an APU fire in flight?

A

The APU ECU shuts down the APU.

The bottle does not discharge automatically, the crew must discharge the bottle.

22
Q

How many smoke detectors are there in the aft cargo compartment?

23
Q

How many smoke detectors are there in the fwd cargo compartment?

24
Q

What are the flight deck indications of cargo smoke?

A
Triple chime
Master warning flashers,
“SMOKE” aural,
SMOKE AFT CARGO warning message,
or SMOKE FWD CARGO warning message.
Either FWD or AFT
CARGO SMOKE PUSH
switchlights illuminate.
25
How many firex bottles are there for cargo smoke?
Two, one is a slow metered standard bottle that should last approximately 60 minutes, and the other is a quick discharge bottle
26
How many smoke detectors are located in the lavatories?
One in the fwd and | one in the aft.
27
What indication do we have for smoke in a lavatory?
Triple chime, master warning flashers, SMOKE FWD LAV or SMOKE AFT LAV warning message.
28
What protection do we have for a lavatory waste compartment fire?
A firex bottle with heat sensitive capsules that will melt to discharge Halon 1301 directly into the waste compartment.
29
What indication will we get with a waste compartment fire?
None, unless it generates enough smoke to set off | a smoke detector.
30
Location of Main Battery?
Nose compartment
31
Location of the APU Battery/
Aft equipment bay
32
Max Engine Generator load?
40 KVA
33
Max APU Generator load?
40 KVA
34
Max Transformer rectifier unit (TRU) load?
120 amps
35
Max permissible time for ground operations with battery power only?
5 minutes
36
What is the reason for the previous limitation?
To prevent ED1 and ED2 from overheating | fans are AC powered
37
How many TRUs are installed in the CRJ 900?
4
38
Where are the TRUs located?
nose compartment
39
The Main Battery is rated to?
17 ampere hour/24 volts
40
APU Battery is rated to?
43 ampere hour/24 volts
41
How many generators are installed?
4, 2 engine generators, 1 APU generator, 1 ADG
42
What is the function of the 4 TRUs?
To convert 115 V AC | to 28 V DC
43
How are the TRU’s cooled?
Individual fans
44
Which buses are powered when the Battery Master switch is selected on?
Main battery direct bus, APU battery direct bus, | DC Battery bus
45
If the main buses are powered, are the essential buses automatically powered?
Yes
46
Is there an on/off switch for the TRU'S?
No, they are automatically powered when the | AC busses are powered
47
What controls the DC tie contactors?
The DC Power Centers (DCPC) automatically control DC tie operation.
48
When will the Air Driven Generator (ADG) automatically deploy?
With complete loss of A/C power
49
With the ADG deployed, what are the basic items that are powered?
AC ESS Bus, Hydraulic pump 3B, flaps/slats, STAB trim CH 2
50
What is the ADG max load?
15 KVA