review for quiz 1 Flashcards

1
Q

2 Subsytems

A
  1. Fire/Overheat Detection & Warning
  2. Fire Extinguishing
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2
Q

3 Types of Fire/Overheat Detection & Warning

A
  1. Unit Spot Type
  2. Continuous Loop/ Firewire
  3. Smoke Detection
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3
Q

2 Types of Fire Warning

A
  1. Bell
  2. Light Indicator
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4
Q

2 Types of Continuous Loop

A
  1. Dual Loop
  2. Pressure Type
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5
Q

3 Fire Zones

A
  1. Fireproof Bulkheads
  2. Engine Fire Prevention
  3. Cockpit & Cabin Interiors
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6
Q

4 Types of Smoke Detectors

A
  1. Carbon Monoxide Detector
  2. Photoelectric Detector
  3. Ionisation Type
  4. Flame Detector
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7
Q

is the most dangerous threat to the safety of an a/c.

A

Fire

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8
Q

Fire Protection System will include as many as possible of the ff. features:

A

•Rapid warning of fire/overheat & its accurate location
•Must not cause false warnings
•Continuous warning for duration of fire/overheat
•Confirmation that the fire has been extinguishing
•Indication that the fire has re-ignited
•A means of testing the system from the flight deck
•Detectors that arw proof against oil, water, vibration & high temp.
•Detectors that are easily accesible throughout the a/c
•Detectors & extinguishers hot wired electrically or powered from emer. electrical buses
•Aduquate visual & aural indication on the flight deck & vital areas on the a/c
•Separate warnings for each engine & specific areas as determined by the a/c manufacturers

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9
Q

are used mainly to detect high temp. leaks from bleed air ducts amd normally positioned at pipe connections.

A

Unit Spot Type / Spot Detectors

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10
Q

This type is fitted at various strategic pts w/in the fire/overheat zone and takes the form of a thermally activated switch.

A

Unit Spot Type/ Spot Detector

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11
Q

They are electrically connected in parallel with each other and in series with the audio/visual warning system.

A

Unit Spot Type/ Spot Detector

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12
Q

This arrangent allows any switch to operate the warning, even if other switches have failed in the remainder of the system.

A

Unit Spot Type/ Spot Detector

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13
Q

This method permits more complete coverage of a fire hazard area than any type of spot-type of temperature detectors.

A

Continuous Loop (Fire Wire) Detectors

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14
Q

The continuous loop uses the principle of capacitance and resistance to indicate a rise in temperature at any point along the length of the detector loop.

A

Continuous Loop (Fire Wire) Detectors

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15
Q

The commonest type has a stainless steel or Inconel outer tube, an inner pure nickel wire surrounded by ceramic beads wetted by eutectic salt.

A

Continuous Loop (Fire Wire) Detectors

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16
Q

The effect of this design is that a rise in temperature causes a sharp fall in electrical resistance, as well as a rise in capacitance.

A

Continuous Loop (Fire Wire) Detectors

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17
Q

Most aircraft use the dual loop system of indication.

A

Dual Loop System

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18
Q

e Each sensing circuit has dual sensing loops.

Each Loop A and Loop B is independent of each other.

A

Dual Loop System

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19
Q

When the loop selector switch is set to BOTH, both loops must detect a fire condition before the warning system is activated.

A

Dual Loop System

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20
Q

If only onc loop detects a fire, the associated loop fault light will illuminate. If the selector is switched to a single loop (A or B) full fire warnings will activate if the selected loop senses a fire condition.

A

Dual Loop System

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21
Q

Pressing the loop test button simulates a fire condition on the respective loop.

A

Dual Loop System

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22
Q

This is done by earthing the inner electrode of the loop that functionally checks the system and checks the continuity of the loop.

A

Dual Loop System

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23
Q

The pressure type detection system uses a continuous loop for the detection element.

A

Pressure-Type Sensor

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23
Q

This loop is made from sealed stainless steel tube that contains an element that absorbs gas when it is cold but releases the gas when it is heated,

A

Pressure-Type Sensor

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24
This tube is connected to a pressure switch that will close when the -pressure reaches a pre-determined level.
Pressure-Type Sensor
25
The commonest make of this type of system is the Systron-Donner system which uses a centre titanium centre wire and the expansion of both helium and hydrogen gas to give the two-stage warnings.
Pressure-Type Sensor
26
These prevent fire from spreading to other areas. Auxiliary power units and tail mounted engines are normally contained within such bulkhead compartments separating them from the rest of the airframe.
Fireproof Bulkheads
27
The (?) also contain a firewall to separate the — engine from the wing.
engine pylons
28
These are made from titanium br stainless steel and all joints are sealed with fireproof sealants.
Fireproof Bulkheads
29
There area number of techniques used to help prevent a fire occurring around engines. These are, the use of flameproof or flame resistant materials, use of bonding strips to prevent arcing, drainage of spilt fuel/oil and efficient cooling.
Engine Fire Prevention
30
All pipes which carry fuel, oil or hydraulic fluids are made (?) and all electrical components and connections are made (?).
1. fire resistant 2. flame proof
31
It is essential that a fire staring in any zone is contained within that zone and is not allowed to spread to any other part of the aircraft.
Fireproof Bulkheads
32
The engine cowlings form a natural container but they are usually made from (?) and would not contain a ground fire for long.
light alloy
33
In flight however (?) through the cowlings, provide sufficient cooling to render the cowlings fireproof.
cooling airflow’s
34
The fireproof bulkheads and any cowling' that has no cooling airflow are usually made from (?).
titanium or stainless steel
35
All wool, cotton and synthetic fabrics used in interior trim are treated to render them flame resistant.
Cockpit and Cabin Interiors
36
(?) conducted have shown that whilst the foam used in seat cushions is flammable, if covered with a flame-resistant fabric, there is little danger of fire from accidental contact with a cigarette, for example.
Tests
37
Fire protection for the aircraft interior is usually provided by (?).
hand-held extinguishers
38
Various types extinguishers are available including, (?). Each type is best used on one kind of fire but may be used on other kinds.
Water, CO, and Dry Powder
39
On light aircraft, the only Protection against fire is a (?), dividing the engine bay from the cabin and the rest of the aircraft.
stainless steel or titanium bulkhead (firewall)
40
Larger aircraft have the complete (?) isolated from the airframe/wing assemblies and. in addition, aircraft cowlings can be divided into a number of ‘fire zones’, each one usually having its own warning and extinguishing system.
engine cowlings
41
The example has four zones around the engine that only (?) have firewires and extinguishing.
two
42
Engines are usually split into (?).
Hot And Cool Zones
43
The hot zone comprises the (?).
combustion chamber, turbines and exhaust areas
44
the cool zone comprises the (?).
intake, compressors and accessory drives
45
A (?) monitors certain areas of the aircraft for the presence of smoke, which is could be indicative of a fire condition.
SMOKE DETECTION/ DETECTORS
46
These may include cargo and baggage compartments and the toilets of transport category aircraft.
SMOKE DETECTION/ DETECTORS
47
A (?) is used where the type of fire anticipated is expected to generate a substantial amount of smoke before temperature changes are sufficient to actuate a heat/fire detection system.
SMOKE DETECTION/ DETECTORS
48
The presence of (?), is dangerous to flight crew and passengers alike and may indicate a fire condition as it is a by-product of combustion.
Carbon Monoxide (CO), or Nitrous Oxides (N,O)
49
Detection of the presence of either or both of these gases could be the earliest warning of a possible dangerous situation.
Carbon Monoxide Detector
50
is very dangerous, firstly due to the minute amount required to cause loss of attention and headaches; (this is approximately 2 parts in 10,000). It is colourless, ocdlourless, tasteless and a non-irritant.
Carbon Monoxide
51
The detector is usually a (?) with a transparent pocket containing (?) that have been treated with a chemical, which changes colour to green or black when they are exposed to carbon monoxide.
small card silica fel crystals
52
(?) are usually used in cabin and cockpit areas.
Carbon Monoxide detectors
53
Air from the monitored compartment is drawn through the detector chamber and a light beam is shone on it.
Photoelectric Smoke Detectors
54
A photoelectric cell installed in the chamber senses the (?) that is refracted by the smoke particles.
light
55
The photocell is installed in a (?) that measures any changes, in the amount of current that it‘ conducts.
bridge circuit
56
A small amount of radioactive material is mounted on the side of the detector chamber.
Ionisation Type Smoke Detector
57
This material bombards the oxygen and nitrogen molecules in the air flowing through the chamber and ionises it to the extent that a reference current can flow across the chamber through the ionised gas to an external circuit.
Ionisation Type Smoke Detector
58
Smoke flowing through the chamber changes the level of ionisation and decreases the current. When the current reduces to a specific level the external circuit initiates a smoke warning signal.
Ionisation Type Smoke Detector
59
This system uses a photoelectric cell to detect a sharp rise in light, such as that from a flame in a closed bay.
Flame Detectors