M15.20 Flashcards

(50 cards)

1
Q

Why is fire the greatest hazard to aircraft safety?

A

It causes rapid structural damage, loss of critical systems, and potential fuel ignition.

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2
Q

What fire protection systems are required on multi-engine turbine aircraft?

A

Fixed fire detection systems and fixed fire extinguishing systems.

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3
Q

What is a fire zone?

A

An area where fire is likely to occur or would have severe consequences and contains ignition sources and flammable fluids.

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4
Q

What are the main requirements of a fire zone?

A

Detection, extinguishing capability, fire-resistant construction, and sealing.

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5
Q

Examples of typical fire zones

A

Engine sections, APU compartments, combustion equipment, turbine areas with flammable fluids.

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6
Q

Main causes of engine fires

A

Abnormal temperatures, flammable fluid leakage, and component failure.

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7
Q

Two categories of engine fire causes

A

Thermodynamic failures and mechanical failures.

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8
Q

What is thermodynamic turbine failure?

A

Failure caused by loss of cooling airflow controlling turbine temperature.

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9
Q

Why are turbine blades vulnerable to overheating?

A

They operate near material limits and rely on internal cooling and correct fuel-air ratio.

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10
Q

Causes of thermodynamic turbine failure

A

Ice accumulation, bleed air extraction, air leakage, over-fuelling, compressor stall or surge.

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11
Q

Effects of thermodynamic turbine failure

A

Blade melting, distortion, separation, and high-energy debris.

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12
Q

Consequences of thermodynamic turbine failure

A

Casing penetration, tail cone severance, and fire ignition.

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13
Q

What causes mechanical turbine failure?

A

Physical damage, fatigue, overspeed, or material stress.

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14
Q

Typical mechanical turbine failures

A

Blade fracture and disc failure.

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15
Q

Hazards of mechanical turbine failure

A

Turbine case penetration and damage to fuel, oil, or hydraulic lines.

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16
Q

Main components of a fire protection system

A

Detection, extinguishing, cockpit indication, and system testing.

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17
Q

Key performance requirement of fire detection systems

A

Early reliable detection with minimal false warnings.

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18
Q

Why must each engine have a separate fire detection system?

A

To ensure independent and reliable fire protection.

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19
Q

Two main types of fire detection systems

A

Spot detection systems and continuous loop systems.

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20
Q

Where are spot detector systems typically used?

A

Older aircraft, light aircraft, and helicopters.

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21
Q

Types of spot fire detectors

A

Thermal switch, thermocouple, optical, pneumatic thermal.

22
Q

How does a thermal switch fire detector work?

A

A switch closes at a preset temperature to trigger a warning.

23
Q

Advantages of thermal switch systems

A

Simple, reliable, and low cost.

24
Q

Limitations of thermal switch systems

A

Cannot detect slow overheating or rate of temperature rise.

25
What principle does a thermocouple fire warning system use?
The Seebeck effect.
26
What does a thermocouple system detect?
Rapid temperature rise, not absolute temperature.
27
Main components of a thermocouple fire system
Thermocouples, sensitive relay, slave relay, test unit.
28
Disadvantage of thermocouple fire systems
Cannot detect slow overheating and sensitive to wiring faults.
29
What do optical fire detectors sense?
Radiation emitted by flames.
30
Difference between IR and UV fire detectors
IR senses hot carbon particles; UV senses ionised gases.
31
Main limitation of optical fire detectors
Require line-of-sight and are contamination sensitive.
32
Principle behind pneumatic thermal fire detection
Boyle’s and Charles’ gas laws.
33
What gas is used in pneumatic fire detection loops?
Helium.
34
How does average temperature sensing work?
Uniform pressure rise triggers alarm at a preset value.
35
How does discrete temperature sensing work?
Local overheating releases hydrogen causing rapid pressure rise.
36
Key advantage of pneumatic thermal systems
Reversible operation and leak detection.
37
Purpose of dual-loop fire detection systems
Reduce false alarms and improve reliability.
38
Logic used in dual-loop fire detection
AND logic.
39
Advantage of continuous loop fire detection systems
Continuous coverage and high reliability.
40
Fenwal system sensing principle
Melting eutectic salt reduces electrical resistance.
41
Kidde system sensing principle
Thermistor resistance decreases as temperature rises.
42
Benefit of overheat and fire detection from one loop
Early warning prevents fire development.
43
Purpose of cockpit fire test switch
Verify system integrity and warning indications.
44
Function of fire detection control units
Monitor sensors, generate warnings, and manage faults.
45
How many fire extinguisher discharges are required per engine?
Two discharges.
46
Why are two extinguisher shots required?
To ensure sufficient agent concentration and allow reattempt.
47
Common fire extinguishing agent used in aircraft
Halon 1301.
48
Advantages of Halon 1301
Effective, non-conductive, and residue-free.
49
What type of fire extinguisher bottle is used?
High Rate of Discharge bottle.
50
What does a squib do?
Electrically ruptures a frangible disc to release agent.