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1 (8310) - Which of the following fire detectors are commonly used in the power section of an engine nacelle?
C- Rate-of-temperature-rise detectors.
2 (8311) - What is the function of a fire detection system?
B- To activate a warning device in the event of a powerplant fire.
3 (8312) - (Refer to Figure 2.) Determine the fire-extinguisher container pressure limits when the temperature is 75°F.
C- 338 minimum and 424 maximum.
4 (8313) - How are most aircraft turbine engine fire-extinguishing systems activated?
A- Electrically discharged cartridges.
5 (8314) - How does carbon dioxide (CO(2)) extinguish an aircraft engine fire?
A- Contact with the air converts the liquid into snow and gas which smothers the flame.
6 (8315) - What retains the nitrogen charge and fire-extinguishing agent in a high rate of discharge (HRD) container?
A- Breakable disk and fusible disk.
7 (8316) - A continuous-loop fire detector is what type of detector?
B- Overheat detector.
8 (8317) - What is the operating principle of the spot detector sensor in a fire detection system?
B- A conventional thermocouple that produces a current flow.
9 (8318) - How is the fire-extinguishing agent distributed in the engine section?
C- Spray nozzles and perforated tubing.
10 (8319) - Which of the following is the safest fire-extinguishing agent to use from a standpoint of toxicity and corrosion hazards?
C- Bromotrifluoromethane (Halon 1301).
11 (8320) - Which of the following is NOT used to detect fires in reciprocating engine nacelles?
A- Smoke detectors.
12 (8321) - What is the principle of operation of the continuous-loop fire detector system sensor?
B- Core resistance material which prevents current flow at normal temperatures.
13 (8322) - The most satisfactory extinguishing agent for a carburetor or intake fire is
A- carbon dioxide.
14 (8323) - The explosive cartridge in the discharge valve of a fire-extinguisher container is
A- a life-dated unit.
15 (8324) - Why does one type of Fenwal fire detection system use spot detectors wired in parallel between two separate circuits?
C- So that a single fault may exist in the system without sounding a false alarm.
16 (8325) - Which of the following fire detection systems measures temperature rise compared to a reference temperature?
A- Thermocouple.
17 (8326) - The pulling out (or down) of an illuminated fire handle in a typical large jet aircraft fire protection system commonly accomplishes what events?
B- Closes fuel shutoff, closes hydraulic shutoff, disconnects the generator field, and arms the fire-extinguishing system.
18 (8327) - 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?
B- Lindberg continuous-element system.
19 (8328) - The fire detection system that uses a single wire surrounded by a continuous string of ceramic beads in a tube is the
A- Fenwal system.
20 (8329) - The fire detection system that uses two wires imbedded in a ceramic core within a tube is the
C- Kidde system.
21 (8330) - A fuel or oil fire is defined as a
A- class B fire.
22 (8331) - A fire detection system that operates on the rate-of-temperature rise is a
B- thermocouple system..
23 (8332) - A fire involving energized electrical equipment is defined as a
C- class C fire.
24 (8333) - Two continuous-loop fire detection systems that will not test due to a broken detector element are the
B- Kidde system and the Fenwal system.
25 (8334) - In a fixed fire-extinguishing system, there are two small lines running from the system and exiting overboard. These line exit ports are covered with a blowout type indicator disc. Which of the following statements is true?
B- When the yellow indicator disc is missing, it indicates the fire-extinguishing system has been normally discharged.
26 (8335) - The most satisfactory extinguishing agent for an electrical fire is
B- carbon dioxide.
27 (8336) - 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?
B- The Kidde system and the Fenwal system.
28 (8337) - 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 (8338) - After a fire is extinguished, or overheat condition removed in aircraft equipped with a Systron-Donner fire detector, the detection system
B- automatically resets.
30 (8339) - The use of water on class D fires
B- will cause the fire to burn more violently and can cause explosions.
31 (8340) - For fire detection and extinguishing purposes, aircraft powerplant areas are divided into fire zones based on
B- the volume and smoothness of the airflow through engine compartments.
32 (8341) - (Refer to Figure 3.) What are the fire-extinguisher container pressure limits when the temperature is 50°F?
C- 475 - 625 PSIG.