This quiz assesses knowledge of fire suppression systems in jet aircraft, focusing on the mechanics of liquid fire-extinguishing agents and system indicators. It is crucial for roles in aircraft maintenance and safety, testing understanding of system components and emergency responses.
Convert the liquid to a gas upon discharge.
Expel the agent from its bottle.
Assist in extinguishing the fire.
Stabilize the temperature.
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Break easily.
Break cleanly into large pieces.
Allow the pieces to enter the strainer unclogging it.
Enable the pieces to pass easily through the strainer.
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Releases a fine mist vapor.
Releases nitrogen into the area.
Removes oxygen from the fire.
Disperses a heavy concentration of liquid.
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Damage.
Leakage.
Destruction.
Contamination.
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Decreases metal fatigue.
Adds strength to the cylinder.
Decreases cylinder expansion.
Increases cylinder corrosion resistance.
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Ears.
Eyes.
Nose.
Lungs.
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Black and red.
Blue and yellow.
Green and white.
Brown and orange.
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Wastes oxygen.
Is unusable below 10,000 feet
Is usable only above 20,000 feet
Delivers oxygen at varying pressures
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Opening the oxygen bottles.
Using a liquid oxygen cryotainer.
Using a gaseous oxygen-servicing trailer.
Opening the system to the environment for six hours.
An overheat condition.
An air valve is closed.
A fuel valve is open.
A fire.
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Do nothing.
Wipe the oil off.
Reject the part and clean again.
Reject the part and put in the scrap metal bin.
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Squib.
Frangible disc.
Bonnet assembly.
Rubber O-ring packing.
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93 percent nitrogen.
16 man-minutes of oxygen.
93 percent oxygen-enriched gas.
100 percent oxygen-enriched gas.
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Charge in a well ventilated area.
Allow no one to enter the controlled area.
Wear your dosimeter badge to ensure proper levels of nitrogen.
Place the high-pressure cylinders up on the table to get a good flow of liquid.
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Check the component for leaks.
Check the component for proper operation.
Service with LOX and perform an evaporation check.
Apply a small amount of anti-seize tape to the first three threads.
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Fill.
Repair.
Replace.
Stabilize.
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Cycling through the components.
Directing coolant across the components.
Cycling conditioned air throughout the system.
Directing conditioned air across the components.
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Leakage.
Contamination.
Nothing happens
Damage or failure
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Cam.
Rupture disc.
Locking sleeve.
Check valve seat.
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20 inches.
15 inches.
10 inches.
5 inches.
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Inspect the area with a bright light.
Inspect the area in natural sunlight.
Install a serviceable tag and place it in a bag.
Install an oxygen use only tag and place it in a bag.
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600 to 1.
680 to 1.
800 to 1.
860 to 1.
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Allow it to stabilize 2 hours before taking next reading.
Allow it to stabilize 6 hours before taking next reading.
Leak check the system.
Sign off the servicing.
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1/2
1
1 1/2
2
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Cause damage to the life raft.
Change the hose weight amount.
Cause the charging hose to detach.
Require a new check valve control head.
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Filler.
Check.
Shutoff.
Pressure reducing.
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Reroute control cables.
Bend or reroute the tubing.
Inspect for possible burn marks.
Clamp the tubing to the control cables.
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Remove any dust or loose debris with a damp cheesecloth.
Remove any dust or loose debris with filtered air.
Check with an ultraviolet light.
Wash the components.
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Perlite settling.
Low tank pressure.
Excessive boil off.
Vacuum valve leakage.
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Pressure switch opens.
Pressure switch closes.
Safety outlet port opens.
Safety outlet port closes.
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Causes a low-pressure condition.
Activates the filter delta pressure switch.
Forces the thermal modulating valve closed.
Reduces the cooling capability of the coolant.
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Thermal pilot.
Thermal modulating.
Delta system bypass.
Over-pressure relief.
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Crew.
Troop.
Low-pressure
High-pressure.
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Opening the manifold valves manually.
Opening the servicing valves manually.
Venting the excess pressure off with the recharge valves.
Venting the excess pressure off with the pressure regulator valves.
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Vacuum down the storage space of the tank.
Vacuum down the annular space on the tank.
Check the reading again with another vacuum gauge.
Verify the reading on another cryotainer’s annular space.
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220 degrees Fahrenheit (°F).
250°F.
320°F.
350°F
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Perilate.
Aluminized polyester film.
High-grade glass wool.
Fiberglass and styrofoam.
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Air inlet valve.
Demand valve.
Diluter aneroid.
Pressure breathing aneroid.
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Remove air from the servicing cart.
Remove contaminants from the system.
Prevent air from entering the system.
Prevent moisture from entering the servicing cart.
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Relief.
Closing.
Control.
Reducer.
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Iron.
Brass.
Copper.
Aluminum.
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Negative signal from the pressure-demand valve.
Negative signal from the emergency flow valve.
Positive signal from the diluter valve.
Positive signal from the anti-G valve.
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Diffuser plug.
Seating sleeve.
Cartridge filter.
Discharge valve.
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Flush with large quantities of distilled water.
Dry by purging with oil-free air or specified nitrogen.
Inspect visually for complete internal moisture removal.
Dry in an oven with a temperature less than 250 degrees Fahrenheit (deg F).
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Record the oxygen gauge pressure immediately.
Record the ambient temperature immediately.
Wait for the system to cool for three hours.
Wait for the system to cool for one hour.
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Bronze.
Copper.
Titanium.
Aluminum.
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Continue to allow the unit to cool the cryotainer to 120 degrees Fahrenheit (°F).
Continue to allow the unit to cool the cryotainer to 150°F.
Turn off the unit and let the cryotainer to cool down to 120°F.
Turn off the unit and let the cryotainer to cool down to 150°F.
Slow pressure buildup
Rapid venting of system pressure
Filler access door from closing in the vent position
Liquid oxygen system pressure loss during maintenance
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Quiz Review Timeline (Updated): Mar 20, 2023 +
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