AM1 STUDY TIRES/TUBES

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fishphinfan
ID:
201582
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AM1 STUDY TIRES/TUBES
Updated:
2013-02-18 19:58:24
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AM1 STUDY TIRES TUBES
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AM1 STUDY TIRES/TUBES
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  1. WHAT OPERATIONS PLACE EXTRA DEMANDS ON TIRE MAINTENANCE?
    CARRIER
  2. WHAT WILL DIFFUSE THROUGH THE MATERIALS OF AIRCRAFT TIRES RESULTING IN A DAILY PRESSURE LOSS AND THE NEED FOR FREQUENT CHECKS?
    NITROGEN
  3. TIRE PRESSURES EXCEEDING WHAT PSI ON OPERATING AIRCRAFT SHALL BE CHECKED AND SERVICED DURING EACH DAILY INSPECTION?
    50 PSI
  4. WHAT IS THE SINGLE MOST FREQUENTLY OCCURRING TIRE PROBLEM IN THE NAVY?
    UNDERINFLATION
  5. WHAT REDUCES THE TREAD CONTACT AREA CAUSING THE TIRE TO WEAR FASTER IN THE CENTER?
    OVERINFLATION
  6. WHAN A TIRE/WHEEL ASSEMBLY SHOWS A REPEATED PRESSURE LOSS EXCEEDING WHAT PERCENT OF THE CORRECT OPERATING INFLATION PRESSURE IN A 24 HOUR PERIOD, IT SHALL BE REMOVED FROM THE AIRCRAFT AND SENT TO THE IMA?
    5%
  7. NEVER CHECK AND ADJUST TIRE PRESSURES OF AIRCRAFT TIRES PARKED ON WHAT?
    CATAPULT TRACK
  8. TEMPERATURE CHANGES AFFECT TIRE PRESSURE. A CHANGE OF 5F PRODUCES APPROXIMATELY 1% CHANGE IN PRESSURE. PRESSURE MEASUREMENTS SHOULD BE MADE AT LEAST HOW LONG AFTER A FLIGHT TO ALLOW TIRE/WHEEL ASSEMBLY TO COOL?
    2 HOURS
  9. WHAT ELIMINATES FOREIGN CONATMINANTS AND LEAKS, MAKING IT AN IMPORTANT COMPONENT OF THE TIRE/WHEEL ASSEMBLY?
    VALVE CAP
  10. ALL TUBE-TYPE AIRCRAFT TIRES WITH INFLATION PRESSURE OF WHAT PSI OR LESS AND ALL HELICOPTER TUBE TYPE TIRES SHALL BE INSPECTED FOR TIRE SLIPPAGE?
    150PSI
  11. WHAT INDICATORS ARE HOLES IN THE RIBS OF THE TIRE TREAD?
    WEAR DEPTH
  12. WHAT PATTERNS CAN BE A GOOD MAINTENANCE TOOL TO DETECT WHEEL ALIGNMENT OR TIRE INFLATION PROBLEMS?
    TREAD WEAR PATTERNS
  13. TIRES WITH EXPOSED CASING PLIES MAY BE SEVERLY WEAKENED AND CAN FAIL CATASTROPHICALLY AFTER AIRCRAFT IS PARKED. ALLOW TIRE TO COOL FOR HOW LONG BEFORE APPROACHING TIRE? 
    2 HOURS
  14. WHAT IS A NORMAL CONDITION FOR A NYLON TIRE, WHICH WILL USUALLY DISAPPEAR AFTER THE AIRCRAFT HAS BEEN TAXIED AND IS THERFORE NOT A REASON TO CHANGE THE TIRE?
    FLAT SPOTTING
  15. WHAT IS DUE TO THE NORMAL OXIDATION OF THE RUBBER FROM EXPOSURE TO SUNLIGHT AN TRACES OF OZONE IN THE ATMOSPHERE?
    WEATHER CRACKING
  16. WHAT ARE USUALLY FOUND IN THE LOWER SIDEWALL AREA AND CAN BE CAUSED BY IMPROPER MOLD FLOW DURING MANUFACTURING?
    CIRCUMFERENTIAL CRACKS
  17. WHAT USUALLY APPEAR ON THE UPPER SIDEWALL SHOULDER AREA AND ARE CAUSED BY IMPROPER SIDEWALL VENTING?
    RADIAL CRACKS
  18. OPERATING TIRES ON GROOVED RUNWAYS MAY RESULY IN THE CUTTING OF THE TREAD SURFACE, A CONDITION TERMED WHAT?
    CHEVERON CUTTING
  19. TREAD DAMAGE FROM WHAT RESULTS IN AN OVAL SHAPED SKID IN THE TREAD AREA WITH THE APPEARANCE OF MELTED RUBBER?
    HYDROPLANING
  20. THE AIRCRAFT LANDING GEAR SHALL BE JACKED UP IN ACCORADANCE WITH APPLICAPLE WHAT ENSURING THAT THE AIRCRAFT IS CHOCKED AND OR TIED DOWN TO PREVENT SLIPPING OF THE JACK?
    MAINTENANCE INSTRUCTION MANUAL
  21. ENSURE THAT THE WHELL BEARING, BEARING CUPS, WHEEL BORES ARE CLEANED, INSPECTED AND PACKED WITH GREASE IN ACCORDANCE WITH WHAT?
    NA-04-10-1
  22. WHEN A BLOW OUT OCCURE ON A DUAL WHEEL INSTALLATION, BOTH TIRES SHALL BE REMOVED FROM SERVICE AND SENT TO THE WHAT FOR CONDEMNATION?
    IMA
  23. THE PRIMARY MEANS OF RECOMMENDED FOR COOLING OVERHEATED WHEEL, BRAKE, AND TIRE ASSEMBLIES IS TO PARK THE AIRCRAFT IN AN ISOLATED LOCATION AND ALLOW THE ASSEMBLY TO COOL IN AMBIENT AIR FOR HOW LONG?
    3 HOURS
  24. WHAT IS DESIGNED TO MELT AND RELIEVE THE PRESSURE AT A TEMPERATURE BELOW THE DANGER LEVEL FOR THE WHEEL ASSEMBLY?
    THERMAL FUSE PLUGS

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