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56 Cards in this Set
- Front
- Back
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AN AUXILIARY BLEED AIR SYSTEM CAN REACH UP TO WHAT PRESSURE?
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125 PSI |
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WHAT IS ICE THAT IS SMOOTH AND HARD TO DETECT VISUALLY?
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GLAZED ICE |
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WHAT IS ICE THAT IS ROUGH AND EASILY NOTICED?
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RIME |
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WHAT IS FORMED AS A RESULT OF WATER VAPOR BEING TURNED DIRECTLY INTO A SOLID?
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FROST |
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WHAT DOES THE P-3 AIRCRAFT USE TO VISUALLY WARN THE PILOT OF ICING CONDITIONS AND WHERE IS THE WARNING LIGHT INSTALLED?
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ICE DETECTOR SYSTEM CENTER INSTRUMENT PANEL |
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HOW MANY ANTI-ICING MODULATING VALVES DOES THE P-3 HAVE INSTALLED IN EACH WING?
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THREE |
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P-3 ANTI-ICING VALVES ARE _____ CONTROLLED AND _____ OPERATED.
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PNEUMATICALLY |
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THERMOSTATS IN THE OUTBOARD LEADING EDGE PLENUM AREAS ARE SET AT ___ F. THE WING INBOARD AND CENTER SECTION THERMOSTATS ARE SET AT ___ F.
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120 |
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DESCRIBE THE DIFFERENCE BETWEEN ANTI-ICING AND DEICING SYSTEM.
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AN ANTI-ICING SYSTEM IS DESIGNED TO PREVENT ICE FROM FORMING ON THE AIRCRAFT. A DEICING SYSTEM IS DESIGNED TO REMOVE ICE AFTER IT HAS FORMED.
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IN AN ANTI-ICE SYSTEM, WHAT METHODS ARE USED TO REMOVE ICE FORMATION?
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ELECTRICAL HEATERS HOT AIR COMBINATION OF BOTH |
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IDENTIFY THE FOUR MAJOR COMPONENTS OF A P-3 ANTI-ICE SYSTEM. |
SHUTOFF VALVES MODULATING VALVES THERMOSTATS LEADING EDGE TEMP INDICATOR OVERHEAT CIRCUIT LIGHT |
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THE OPEN LIGHT ON THE ICE PROTECTION PANEL WILL ILLUMINATE WHEN WHAT CONDITION OCCURS? |
WHEN THE BLEED AIR VALVE IS OPEN 2 DEGREES OR MORE
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WHAT DOES THE WARM AIR OVERTEMPERATURE SENSOR SENSE?
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IF TEMPERATURE REACHES 375 +/- 25 F |
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WHAT DOES THE WINDSHIELD OVERHEAT TEMPERATURE SENSOR SENSE?
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CLOSES IF AIRFLOW REACHES 280 +/- 5 |
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WHAT IS THE PURPOSE OF AN F-18 WINDSHIELD ANT-ICE/RAIN REMOVAL SYSTEM?
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TO PROVIDE AIRFLOW OVER THE EXTERNAL SURFACE OF THE WINDSHIELD FOR RAIN REMOVAL AND ANTI-ICING
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NAME SEVEN MAJOR COMPONENTS OF AN F-18 WINDSHIELD ANTI-ICE/RAIN REMOVAL SYSTEM.
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WARM AIR TEMP CONTROL VALVE WARM AIR TEMP SENSOR FLOW/TEMP LIMITING ANTI-ICE MODULATING VALVE WINDSHIELD OVHT TEMP SENSOR WINDSHIELD ANTI-ICE/RAIN REMOVAL SWITCH |
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WHAT COMPONENT CONTROLS THE TEMPERATURE ENTERING THE WINDSHIELD ANTI-ICE AND RAIN REMOVAL DUCTS? |
WARM AIR TEMPERATURE CONTROL VALVE
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THE MODES OF OPERATION FOR THE ANTI-ICE/RAIN REMOVAL SYSTEM ARE CONTROLLED BY WHAT COMPONENT? |
WINDSHIELD ANTI-ICE/RAIN REMOVAL SWITCH
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ON AN EA-6B, THE WINDSHIELD WASHING TANK HOLDS ___ GALLONS OF WASHING FLUID.
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1 1/2 |
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DESCRIBE THE MIXUTRE CONTENT ON AN EA-6B WINDSHIELD-WASHER SYSTEM.
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50% WATER-MTHYL ALCOHOL MIXTURE
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WHAT TYPE OF VALVE IS THE WINDSHIELD-WASHING SHUTOFF VALVE?
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SOLENOID-OPERATED VALVE
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WHAT EVENT TAKES PLACE IF THE PRESSURE IN THE WINDSHIELD-WASHING TANK GOES ABOVE 13 +/- .5 PSIG? |
THE RELIEF VALVE INSIDE THE WINDSHIELD-WASHING SHUTOFF VALVE OPENS AND PRESSURE IS REDUCED
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WHAT IS THE CAPACITY OF THE WINDSHIELD-WASHING TANK?
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1 1/2 GALLONS
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IDENTIFY THE PURPOSE OF AN ANTI-G SYSTEM.
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REDUCES THE FATIGUING EFFECT OF REPEATED EXPOSURE TO POSITIVE OR NEGATIVE G FORCES, ALSO PROVIDES A METHOD BY WHICH THE CREWMEMBER CAN RELIEVE FATIGUE AND PHYSICAL TENSION DURING EXTENDED FLIGHT
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MOST ANTI-G SYSTEMS CONSIST OF WHAT COMPONENTS?
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ANTI-G VALVE ANTI-G SYSTEM FILTER QUICK DISCONNECTS |
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THE ANTI-G VALVE REGULATES HIGH-PRESSURE BLEED AIR TO WHAT MAXIMUM PRESSURE FOR DELIVERY TO THE G-SUIT?
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10 PSI
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DESCRIBE THE OPERATION OF AM ANTI-G SYSTEM.
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AS HIGH G FORCES OCCUR, THE ANTI-G VALVES ACTIVATING WEIGHT IS FORCED DOWN TO CLOSE THE EXHAUST AND OPEN THE DEMAND VALVE.
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A VENT-AIR SYSTEM IS USED FOR WHAT PURPOSE?
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PROVIDES A MEASURE OF PERSONAL COMFORT, OFFSETTING THE DISCOMFORT CAUSED BY THE WEARING OF THE ANTI EXPOSURE SUIT OR HEAT CREATED BY COCKPIT EQUIPMENT AND RESULTING HIGH TEMPERATURE AMBIENT
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WHERE IS THE VENT SUIT TEMPERATURE SENSOR LOCATED? |
IN A MNAIFOLD DOWNSTREAM OF THE VENT SUIT TEMPERATURE VALVE
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IDENTIFY THE SIX MAJOR COMPONENTS OF A VENT-AIR SYSTEM. |
VENT SUIT TEMP VALVE OVER TEMP SENSOR PRESSURE TEMP REGULATING VALVE PRESSURE RELIEF VALVE AIR HOSE ASSEMBLY |
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WHAT ARE THE TWO MODES OF OPERATION FOR A VENT-AIR SYSTEM? |
AUTOMATIC AND MANUAL
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DESCRIBE THE PURPOSE OF THE F-18 AIRCRAFT RADAR LIQUID COOLING SYSTEM.
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CIRCULATES LIQUID COOLANT TO REMOVE HEAT FROM THE RADAR TRANSMITTER HIGH-VOLTAGE RF ENERGY MODULES.
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DURING GORUND OPERATION, WHAT COMPONENT SUPPLIES COOLING AIR FOR THE HEAT EXCHANGER?
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GROUND COOLING FAN
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NAME THE EIGHT MAJOR COMPONENTS OF THE RADAR LIQUID COOLING SYSTEM.
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LIQUID TO AIR HEAT EXCHANGER LIQUID COOLANT PUMP AIRFLOW VALVE GROUND COOLING FAN COOLANT SYSTEM FILTER LOW PRESSURE SENSOR HIGH TEMPERATURE SENSOR COOLANT TEMPERATURE SENSOR |
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DESCRIBE THE OPERATION OF THE GROUND COOLING FAN. |
THE GROUND COOLING FAN IS ELECTRICALLY POWERED AND SUPPLIES A FLOW OF AMBIENT AIR FOR HEAT TRANSFER FROM THE LIQUID HEAT EXCHANGER DURING AIRCRAFT GROUND OPERATIONS
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WHAT IS CF3BR?
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TRIFLOUROBROMOMETHANE |
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WHAT IS THE MOST COMMON EXTINGUISHING AGENT USED IN AIRCRAFT FIRE-EXTINGUISHING SYSTEMS?
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CF3BR |
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THE P-3 FIRE-EXTINGUISHING SYSTEM CONTROLS FIRES WITHIN ____ ENGINE NACELLES AND EQUIPPED WITH ____ INDEPENDENT ELECTRICALLY CONTROLLED FIRE SYSTEM.
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TWO |
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EACH CONTAINER IS PRESSURIZED TO _____ PSI AND CHARGED WITH ____ POUNDS OF EXTINGUISHING AGENT.
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10.5 |
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UNDER NORMAL ATMOSPHERIC PRESSURE AND TEMPERATURE, DESCRIBE THE CHARACTERISTICS OF CF3BR.
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IT IS A MORE EFFICIENT EXTINGUISHING SYSTEM THAN CO2 AND UNDER NORMAL ATMOSPHERIC PRESSURE AND TEMPERATURE, IT IS ODORLESS AND TASTELESS
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HOW MANY INDEPENDENT FIRE-EXTINGUISHING SYSTEMS DOES A P-3 AIRCRAFT USE?
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TWO
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LIST THE DIFFERENT PORTS FOR A TRANSFER CHECK VALVE.
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TWO INLET PORTS AND ONE OUTLET PORT, AND A POPPET THAT SHUTS OFF THE INLET PORT
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WHAT IS THE INTERNAL VOLUME OF A P-3 FIRE EXTINGUISHER CONTAINER? |
400 (+200, -15) CUBIC INCHES
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AVIONICS PRESSURIZATION ASSEMBLY REMOVES 100 PERCENT OF PARTICLES LARGER THAN ___ MICRONS AND 98 PERCENT OF PARTICLES LARGER THAN ___ MICRONS.
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25 10 |
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DESCRIBE THE PURPOSE OF AN AUXILIARY POWER UNIT FIRE DETECTION AND EXTINGUISHING SYSTEM. |
PROVIDES DETECTION AND EXTINGUISHING FOR THE APU COMPARTMENT ON THE GROUND AND IN FLIGHT.
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WHAT IS/ARE INDICATIONS GIVE IF A FIRE IS PRESENT IN THE APU? |
A HORN SOUNDS AND A WARNING LIGHT ILLUMINATES.
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WHERE ARE THE TWO WAVEGUIDE AIR DESICATORS LOCATED?
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DOWNSTREAM FROM THE WAVEGUIDE FLUID PRESSURE REGULATING VALVES
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WHAT ARE THE WAVEGUIDE AIR DESICATORS USED FOR?
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ECM AND RADAR |
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WHAT IS THE PURPOSE OF AN F-18 WAVEGUIDE PRESSURIZATION SYSTEM?
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TO CONTAIN AND TRANSPORT THE REGULATED, FILTERED, DRY AIR TO THE RADAR AND ECM WAVEGUIDE CAVATIES
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WHAT PERCENTAGE OF PARTICLES WILL THE FILTER ASSEMBLY REMOVE IF THEY ARE 25 MICRONS OR LARGER?
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100%
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THE WAVEGUIDE PRESSURE REGULATING VALVE HAS HOW MANY ANEROID ASSEMBLIES TO REGULATE AIR PRESSURE? |
TWO
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DESCRIBE THE PURPOSE OF THE MISSILE COOLING SYSTEM.
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TO PROVIDE THERMAL CONDITIONING FOR THE RADAR SYSTEM OF THE WCS AND MISSILE
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WHAT IS THE PURPOSE OF THE MISSILE HOT AIR MODULATING VALVE?
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THE VALVE HEATS THE COOLANT DURING SYSTEM WARM UP
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THE COOLANT PUMP CIRCULATES WHAT AMOUNT OF COOLANT PER MINUTE? |
18 GALLONS |
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WHAT TYPE OF PROTECTIVE MEASURES MUST YOU TAKE WHEN SERVICING THE MISSILE LIQUID COOLING SYSTEM? |
RESPIRATOR OR AM AREA WITH FORCED VENTILATION, AND CHEMICAL SPLASH PROOF GOGGLES AND GLOVE
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PRIOR TO TAKING A COOLANT SAMPLE, THE COOLANT MUST HAVE CIRCULATED FOR WHAT AMOUNT OF TIME?
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5 MINUTES
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