Engine Fire Protection Systems Flashcards

1
Q

Which of the following fire detection systems are commonly used in an engine nacelle?

A

Kidde continuous-loop.

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2
Q

What is the function of a fire detection system?

A

To activate a warning device in the event of a powerplant fire.

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3
Q

(Refer to Figure 2.) Determine the fire extinguisher container pressure limits when the temperature is 75 degrees F.

A

338 minimum and 424 maximum.

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4
Q

How are most aircraft turbine engine fire-extinguishing systems activated?

A

Electrically discharged cartridges.

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5
Q

How does carbon dioxide (CO2) extinguish an aircraft engine fire?

A

Contact with the air converts the liquid into snow and gas which smothers the flame.

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6
Q

What retains the nitrogen charge and fire extinguishing agent in high rate of discharge (HRD) container?

A

Breakable disk and fusible disk.

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7
Q

A continuous-loop fire detector is what type of detector?

A

Overheat detector.

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8
Q

What is the operating principle of the spot detector sensor in a fire detection system?

A

A bimetallic thermoswitch that closes when heated to a high temperature.

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9
Q

How is the fire-extinguishing agent distributed in the engine section?

A

Spray nozzles and perforated tubing.

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10
Q

Which of the following is the safest fire-extinguishing agent to use from a standpoint of toxicity and corrosion hazards?

A

Bromotrifluoromethane (Halon 1301)

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11
Q

Which of the following is NOT used to detect fires in reciprocating engine nacelles?

A

Smoke detectors.

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12
Q

What is the principle of operation of the continuous-loop fire detector system sensor?

A

Core resistance material which prevents current flow at normal temperatures.

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13
Q

The most satisfactory extinguishing agent for a tailpipe or intake fire is what?

A

carbon dioxide.

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14
Q

The explosive cartridge in the discharge valve of a fire-extinguisher container is what?

A

a life-dated unit.

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15
Q

Why does one type of Fenwal fire detection system use spot detectors wired in parallel between two separate circuits?

A

So that a single fault may exist in the system without sounding a false alarm.

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16
Q

Which of the following fire detection systems measures temperature rise compared to a reference temperature?

A

Thermocouple.

17
Q

The pulling out (or down) of an illuminated fire handle in a typical large jet aircraft fire protection system commonly accomplishes what events?

A

Closes fuel shutoff, closes hydraulic shutoff, disconnects the generator field, and arms the fire-extinguishing system.

18
Q

A fire detection system operates on the principle of a buildup of gas pressure within a tube proportional to temperature. Which of the following systems does this statement define?

A

Lindberg continuous-element system.

19
Q

The fire detection system that uses a single wire surrounded by a continuous string of ceramic beads in a tube is the what?

A

Fenwal system.

20
Q

The fire detection system that uses two wires imbedded in a ceramic core within a tube is the what?

A

Kidde system.

21
Q

A fuel or oil fire is defined as a what?

A

Class B fire.

22
Q

A fire detection system that operates on the rate-of-temperature rise is a what?

A

thermocouple system.

23
Q

A fire involving energized electrical equipment is defined as a what?

A

Class C fire.

24
Q

Two continuous-loop fire detection systems that will not test due to a broken detector element are the what?

A

Kidde system and the Fenwal system.

25
Q

Which statement best describes the blowout type indicator disk on a fixed fire extinguishing system?

A

When the yellow indicator disk is missing, it indicates the fire extinguishing system has been normally discharged.

26
Q

The most satisfactory extinguishing agent for an electrical fire is what?

A

carbon dioxide.

27
Q

Which of the following fire detection systems will detect a fire when an element is inoperative but will not test when the test circuit is energized?

A

The Kidde system and the Fenwal system.

28
Q

Which of the following fire detection systems uses heat in the normal testing of the system?

A

The thermocouple system and the Lindberg system.

29
Q

After a fire is extinguished, or overheat condition removed in aircraft equipped with a Systron-Donner fire detector, the detection system…

A

automatically resets.

30
Q

The use of water on Class D fires…

A

will cause the fire to burn more violently and can cause explosions.

31
Q

For fire detection and extinguishing purposes, aircraft powerplant areas are divided into fire zones based on what?

A

the volume and smoothness of the airflow through engine compartments.

32
Q

(Refer to Figure 3.) What are the fire-extinguisher container pressure limits when the temperature is 50 degrees F?

A

475 - 625 psig.