Frage 1
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WHAT DOES THE AIR FLOW PRODUCE OVER ANY AERODYNAMIC SURFACE? (19030) REF.: AC 65-15A, PAGE 64.
Antworten
-
PRODUCES AN INCREASE IN VELOCITY AND TEMPERATURE.
-
PRODUCES A REDUCTION IN VELOCITY AND TEMPERATURE.
-
PRODUCES CERTAIN REDUCTION IN VELOCITY WITH CORRESPONDING INCREASES IN TEMPERATURE.
-
PRODUCES CERTAIN INCREASES IN VELOCITY WITH CORRESPONDING REDUCTION IN TEMPERATURE.
Frage 2
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HOW MANY GENERAL TYPES OF EXHAUST SYSTEMS IN USE ON RECIPROCATING AIRCRAFT ENGINES ARE THERE? (19299) REF.: AC 12A, PAGE 96.
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IN MOST CASES, WHAT LOADS ARE DESIRABLE FOR STRUCTURAL MEMBERS TO CARRY ON? (18839) REF.: AC 65-15A, PAGE 25.
Antworten
-
END LOADS RATHER THAN SIDE LOADS.
-
SIDE LOADS RATHER THAN END LOADS.
-
AERODYNAMIC LOADS RATHER THAN STRUCTURAL LOADS.
-
STRESS LOADS RATHER THAN STRENGTH LOADS.
Frage 4
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WHERE ARE MOST FLAPS HINGED? (19284) REF.: AC 65-15A, PAGE 21.
Antworten
-
OVER SPECIAL PYLON
-
TO THE MIDDLE SECTION OF THE WINGS.
-
TO THE LOWER TRAILING EDGES OF THE WINGS.
-
TO THE UPPER TRAILING EDGES OF THE WINGS.
Frage 5
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WHICH ARE THE MOST COMMON SYNTHETIC FIBERS USED IN AIRCRAFT? (18843) REF.: AC 65-15A, PAGE 85.
Antworten
-
NYLON, ORLON AND DACRON.
-
NYLON, COTTON AND LINEN.
-
FABRIC, WARP AND PLY.
-
WOOF, WOVEN AND FILLING.
Frage 6
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WHAT IS PROVIDED AT MANY PITOT-STATIC TUBES IN ORDER TO PREVENT ICING DURING FLIGHT? (19273) REF.: AC 65-15A, PAGE 475.
Antworten
-
CHEMICAL HEATING ELEMENTS
-
AERODYNAMIC HEATING ELEMENTS
-
HOT AIR HEATING ELEMENTS.
-
ELECTRICAL HEATING ELEMENTS.
Frage 7
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HOW MANY FACTORS DETERMINE THE AMOUNT OF LIFT AVAILABLE IN HELICOPTER OPERATION? (19025) REF.: AC 65-15A, PAGE 56.
Antworten
-
FEW FACTORS.
-
ONE FACTOR.
-
MANY FACTORS.
-
SOME FACTORS.
Frage 8
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WHAT WILL THE AVIATION MECHANIC NEED THE MATHEMATICS TOOLS FOR? (18646) REF.: FAA-H-8083-30, PAGE 1-1.
Antworten
-
TO SEE, WASH, AND DISPATCH THE AIRPLANE
-
TO WORK, TEST AND CHECK THE AIRPLANES.
-
TO REPAIR, MAINTAIN AND CERTIFY AIRPLANES.
-
TO CONTROL, DISPATCH AND PARK THE AIRPLANES.
Frage 9
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WHAT OLD MATERIAL IS STILL IN USE TODAY TO COVER DIFFERENT AIRCRAFT PARTS? (18844) REF.: AC 65-15A, PAGE 85.
Antworten
-
WOOD.
-
FABRIC.
-
PLASTIC.
-
COMPOSITE.
Frage 10
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WHAT LANDING GEAR ARRANGEMENT IS THE MOST USED IN MODERN AIRCRAFT? (19269) REF.: AC 65-15A, PAGE 341.
Antworten
-
A TAIL WHEEL AND A NOSE SKID GEAR ARRANGEMENT.
-
A TAIL SKID ARRANGEMENT.
-
A TAIL WHEEL GEAR ARRANGEMENT.
-
A TRICYCLE GEAR ARRANGEMENT.
Frage 11
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WHAT ARE THE TYPES OF MAGNETS? (19296) REF.: FAA-H-8083-30, PAGE 10-11.
Frage 12
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WHAT IS THE DEFINITION OF MAGNETISM? (19293) REF.: FAA-H-8083-30, PAGE 10-7.
Antworten
-
IS DEFINED AS THE QUALITY OF AN OBJECT TO ATTRACT THE IRON METAL.
-
IS THE PROPERTY OF AN OBJECT TO ATTRACT ALL SUBSTANCES.
-
IS THE PROPERTY OF AN OBJECT TO ATTRACT ALL METALLIC SUBSTANCES.
-
IS THE PROPERTY OF AN OBJECT TO ATTRACT CERTAIN METALLIC SUBSTANCES.
Frage 13
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USUALLY, WHERE DOES THE MAGNESIUM SKIN CORROSION OCCUR? (18787) REF.: FAA-H-8083-30, PAGE 6-15.
Antworten
-
AROUND THE INSULATING WASHERS.
-
OVER WASHERS AND BOLTS.
-
NEVER AROUND EDGES OF SKIN PANELS.
-
AROUND EDGES OF SKIN PANELS.
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WHY CAN BE CONSTRUCTED THE FUSELAGES IN FIXED-WING AIRCRAFT AND HELICOPTERS? (18822) REF.: AC 65-15A, PAGE 24.
Antworten
-
FUSELAGES MAY BE CONSTRUCTED WELDED, BOLTED TRUSS OR SOME FORM OF SEMI-MONOCOQUE CONSTRUCTION.
-
FUSELAGES MAY BE WELDED TRUSS OR SOME FORM OF MONOCOQUE CONSTRUCTION.
-
FUSELAGES MAY BE RIVETED, WELDED, GLUED OR SOME FORM OF MONOCOQUE CONSTRUCTION.
-
FUSELAGES ARE CONSTRUCTED ONLY LIKE SEMIMONOCOQUE OR MONOCOQUE CONSTRUCTION.
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WHAT IS LIFT FORCE IN A HELICOPTER? (18980) REF.: AC 65-15A, PAGE 50.
Antworten
-
IS THE FORCE REQUIRED TO FLY THE HELICOPTER.
-
IS THE FORCE REQUIRED TO SUPPORT THE WEIGHT OF THE HELICOPTER.
-
IS THE FORCE REQUIRED TO SUPPORT THE TORQUE ROTORS.
-
IS THE FORCE REQUIRED TO LOAD AND UNLOAD THE HELICOPTER.
Frage 16
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KEEPING THE INTERIOR OF THE AIRCRAFT CLEAN IS JUST AS IMPORTANT AS MAINTAINING? (18793)
REF.: FAA-H-8083-30, PAGE 6-20.
Antworten
-
A BRIGHT AND CLEAN COCKPIT.
-
A CLEAN EXTERIOR SURFACE.
-
ALL AIRPLANE IN GOOD CONDITION.
-
A CLEAN HOUSE.
Frage 17
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IN THE CONVERGING PART OF THE VENTURI, WHAT HAPPEN WITH VELOCITY AND PRESSURE? (18705) REF.: FAA-H-8083-30, PAGE 3-40.
Antworten
-
VELOCITY AND STATIC PRESSURE WOULD INCREASE.
-
THE VELOCITY AND STATIC PRESSURE WOULD DECREASE.
-
VELOCITY WOULD DECREASE AND STATIC PRESSURE WOULD
INCREASE.
-
VELOCITY WOULD INCREASE AND STATIC PRESSURE WOULD
DECREASE.
Frage 18
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WHAT IS BASICALLY INSTRUMENTATION? (18805) REF.: AC 65-15A, PAGE 469.
Antworten
-
THE SCIENCE OF MEASUREMENT.
-
THE SCIENCE OF INDICATION.
-
THE SCIENCE OF SHOWING DATA.
-
INSTRUMENTS AND ADVERTISING.
Frage 19
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WHAT DO YOU HAVE TO USE TO INSPECT FOR CORROSION IN AN AIRPLANE AND BE SURE THAT NO AREA IS LEFT UNINSPECTED? (18777) REF.: FAA-H-8083-30, PAGE 6-8.
Antworten
-
INSTRUMENT.
-
CHECKLISTS.
-
TWO OR THREE METHODS.
-
LEVEL TWO MECHANIC.
Frage 20
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WHERE ARE POWER PLANTS USUALLY MOUNTED IN MULTIENGINE HELICOPTERS? (18834) REF.: AC 65-15A, PAGE 24.
Antworten
-
THEY ARE MOUNTED IN SEPARATE ENGINE NACELLES.
-
THEY ARE MOUNTED IN THE SAME NACELLE
-
THEY ARE MOUNTED ONE BACK AND ONE FORWARD.
-
THEY ARE MOUNTED IN TANDEM.
Frage 21
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IN GENERAL, WHAT WILL BE THE FLASHPOINT FOR SOLVENT CLEANERS USED IN AIRCRAFT CLEANING? (18797) REF.: FAA-H-8083-30, PAGE 6-23.
Frage 22
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THE PRIMARY GROUP OF FLIGHT CONTROL SURFACES CONSISTS OF (18830) REF.: AC 65-15A, PAGE 18.
Antworten
-
AILERONS, ELEVATORS AND RUDDERS.
-
FLAPS, TRIM TABS AND STABILIZERS.
-
SPEED BRAKES, LONGERONS AND ELEVATORS.
-
WING TIPS, GROUND SPOILERS AND RIBS.
Frage 23
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WHAT HAPPENS IN A TWO-BLADED SYSTEM HELICOPTER? (19032) REF.: AC 65-15A, PAGE 53.
Antworten
-
THE BLADES FLAP AS A UNIT.
-
THE BLADES FLAP INDEPENDENTLY.
-
THE BLADES DO NOT FLAP.
-
THE BLADES FLAP ONLY OCCASIONALY.
Frage 24
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WHAT HAPPENS IN A HOVERING FLIGHT, IF LIFT AND THRUST ARE LESS THAN WEIGHT AND DRAG? (18987) REF.: AC 65-15A, PAGE 50.
Antworten
-
THE HELICOPTER ENGINE IDLES.
-
THE HELICOPTER STAYS IN A HOVERING FLIGHT.
-
THE HELICOPTER DESCENDS VERTICALLY.
-
THE HELICOPTER ASCENDS VERTICALLY.
Frage 25
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WHAT ARE USED IN SOME SYSTEMS IN ADDITION TO TURNBUCKLES? (19031) REF.: AC 65-15A, PAGE 65.
Antworten
-
WIRE CONNECTORS, PULLEYS AND SHROUD MUST BE USED.
-
CABLE CONNECTORS AND PULLEYS ARE ALWAYS USED.
-
CABLE CONNECTORS ARE NEVER USED.
-
CABLE CONNECTORS ARE USED.
Frage 26
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WHAT MAY BE WRONG IF THE POINTER FAILS TO RESPOND ENTIRELY? (19272) REF.: AC 65-15A, PAGE 474.
Antworten
-
THE GLASS COVER MAY BE BROKEN.
-
THE TRANSMISION MECHANISM IS DISCONNECTED.
-
THE MECHANISM IS, IN ALL PROBABILITY, DEFECTIVE.
-
THE ELECTRICAL POWER IS CUT OFF.
Frage 27
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WHAT MUST BE DONE IN ADDITION TO ROUTINE MAINTENANCE INSPECTIONS IN AMPHIBIANS OR SEAPLANES? (18778) REF.: FAAH-8083-30, PAGE 6-8.
Antworten
-
COULD BE CHECKED OCCASSIONALLY AND CRITICAL AREAS CLEANED OR TREATED EVERY DAY.
-
MAY BE CHECKED MONTHLY AND CRITICAL AREAS WIPED OR TREATED, AS NECESSARY.
-
SHOULD BE CHECKED DAILY AND CRITICAL AREAS CLEANED OR TREATED, AS NECESSARY.
-
SHOULD BE CHECKED WEEKLY AND CRITICAL AREAS PAINTED, CLEANED OR TREATED, AS NECESSARY.
Frage 28
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WHAT IS THE SIMPLEST FORM OF AN ATOM? (18929) REF.: FAA-H-8083-30, PAGE 10-2.
Antworten
-
THE NITROGEN ATOM.
-
THE COPPER ATOM.
-
THE HYDROGEN ATOM.
-
THE OXYGEN ATOM.
Frage 29
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WHAT QUALITY HAVE THE HUMAN WASTE PRODUCTS AND THE CHEMICALS USED IN LAVATORIES? (18781) REF.: FAA-H-8083-30,PAGE 6-9.
Antworten
-
ARE VERY EXPENSIVE AND DIFFICULT TO GET.
-
ARE VERY CORROSIVE TO COMMON AIRCRAFT METALS.
-
SMELL VERY BAD AND ARE CHEAP TO BUY.
-
ARE VERY DANGEROUS TO COMPOSITES.
Frage 30
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HOW OFTEN IS THE INSPECCION FOR CORROSION IN ANY AIRCRAFT RECOMENDED? (18779) REF.: FAA-H-8083-30, PAGE 6-8.
Antworten
-
ANNUALLY.
-
IN ANY INSPECTION.
-
WEEKLY.
-
DAILY BASIS.
Frage 31
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HOW LONG HAVE HIGH TENSION IGNITION SYSTEMS BEEN IN USE? (19298) REF.: AC 65-12A, PAGE 186.
Frage 32
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HOW IS THE WEIGHT OF A SOLID BODY SUBMERGED IN A LIQUID OR A GAS TO BE IT IN FREE SPACE? (18701) REF.: FAA-H-8083-30, PAGE 3-28.
Antworten
-
IN THE LIQUID IT WEIGHS LESS THAN IN THE FREE SPACE.
-
IN THE LIQUID IT WEIGHS MORE THAN IN THE FREE SPACE.
-
IN THE LIQUID IT WEIGHS EQUAL THAN IN THE FREE SPACE.
-
IN THE LIQUID IT WEIGHS 10% LESS THAN IN THE FREE SPACE.
Frage 33
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WHAT MUST A HELICOPTER STRUCTURAL MEMBERS RESIST? (18837) REF.: AC 65-15A, PAGE 25.
Antworten
-
SHOCK.
-
LOADS.
-
FORCE.
-
STRESS.
Frage 34
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WHAT IS HEAT? (18696) REF.: FAA-H-8083-30, PAGE 3-19.
Frage 35
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WHAT HAPPENS IF HEAT IS APPLIED TO A METAL? (18729) REF.: FAA-H-8083-30, PAGE 5-2
Antworten
-
WILL CAUSE IT TO CONTRACT OR BECOME LARGER.
-
WILL CAUSE IT TO EXPAND OR BECOME LARGER.
-
WILL CAUSE IT TO EXPAND OR BECOME SHORTER.
-
WILL CAUSE IT TO INCREASE THE WEIGHT OR BECOME HEAVIER.
Frage 36
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WHAT SEWING METHOD IS NECESSARY TO CLOSE THE FINAL OPENING IN THE COVERING? (18846) REF.: AC 65-15A, PAGE 90.
Antworten
-
MACHINE SEWING.
-
DOUBLE STITCH SEWING.
-
AUTOMATIC SEWING.
-
HAND SEWING.
Frage 37
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WHAT IS THE RIVETS GRIP LENGTH? (18761) REF.: FAA-H-8083-30, PAGE 5-64.
Antworten
-
THE TOTAL SHEET THICKNESS PLUS THE RIVET LENGTH.
-
THE NOMINAL RIVET LENGTH.
-
THE SHANK DIAMETER.
-
THE MAXIMUN TOTAL SHEET THICKNESS TO BE RIVETED.
Frage 38
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WHAT ARE THE METHODS TO COVER FUSELAGES? (18851) REF.: AC 65-15A, PAGE 95.
Antworten
-
THE SLEEVE OR BLANKET METHOD.
-
THE FABRICS SLEEVE OR PLASTIC BLANKET METHOD.
-
THE PARTIAL O TOTAL COVERING METHOD.
-
THER ARE NO METHODS TO COVER FUSELAGES.
Frage 39
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IN WHAT IS NOT BASED THE MINIMUM FUEL FOR TURBINE ENGINE POWERED AIRCRAFT? (18718) REF.: FAA-H-8083-30, PAGE 4-5.
Antworten
-
ON ENGINE SPEED.
-
ON ENGINE HORSEPOWER.
-
ON ALTITUDE OF FLIGHT.
-
ON FLIGHT DISTANCE.
Frage 40
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WHAT MUST BE MAINTAINED FOR EFFICIENT OPERATION OF SHOCK STRUTS? (19271) REF.: AC 65-15A, PAGE 345.
Antworten
-
THE PROPER CLEANNESS AND CORRECT O-RING.
-
THE PROPER FLUID LEVEL AND AIR PRESSURE.
-
THE PROPER TIRE PRESSURE AND FLUID LEVEL.
-
THE PROPER WHEEL, BRAKES AND FLUID.
Frage 41
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WHAT FORCES ACT ON AN AIRCRAFT, WHETHER IT IS ON THE GROUND OR IN FLIGHT? (19042) REF.: AC 65-15A, PAGE 131.
Antworten
-
THE FORCES ARE CUTING, PUSHING OR BENDING.
-
THE FORCES ARE PULLING, PUSHING OR TWISTING.
-
THE FORCES ARE WEIGHT, THRUST OR DRAG.
-
THE FORCES ARE LIFTING, PUSHING OR DOWNWARD.
Frage 42
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HOW MUST THE MIXTURE BE IN ORDER FOR AN ENGINE TO DEVELOP MAXIMUN POWER AT FULL THROTTLE? (19115) REF.: AC 65-12A, PAGE 121.
Antworten
-
THE FUEL MIXTURE MAY BE RICHER THAN FOR CRUISE.
-
THE FUEL MIXTURE IS THE SAME ALL THROUGH THE FLIGHT.
-
THE FUEL MIXTURE MUST BE RICHER THAN FOR CRUISE.
-
THE FUEL MIXTURE MUST BE LEANER THAN FOR CRUISE
Frage 43
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WHAT ARE THE FACTORS TO CONSIDER IN THE SELECTION OF THE CORRECT RIVET FOR INSTALLATION? (18757) REF.: FAA-H-8083-30, PAGE 5-61.
Antworten
-
INSTALLATION LOCATION, PROTECTION OF THE MATERIAL BEING RIVETED, DIAMETERS OF THE MATERIAL BEING RIVETED AND STRESS DESIRED.
-
INSTALLATION PLACE, COMPOSITION OF THE TOOLS BEING USED, THINNESS OF THE MATERIAL BEING RIVETED AND STRENGTH DESIRE.
-
WORK LOCATION, ILUMINATION OF THE PLACE, COMPOSITION OF THE MATERIAL BEING RIVETED, THICKNESS OF THE MATERIAL BEING RIVETED AND QUALITY OF THE TOOLS.
-
INSTALLATION LOCATION, COMPOSITION OF THE MATERIAL BEING RIVETED, THICKNESS OF THE MATERIAL BEING RIVETED AND STRENGTH DESIRED.
Frage 44
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WHAT IS THE ADVANTAGE OF EXTERNAL AIRCRAFT SURFACES WITH REGARD TO INSPECTION AND MAINTENANCE? (18782) REF.:FAA-H-8083-30, PAGE 6-9.
Antworten
-
IT HAS NO SPECIAL ADVANTAGES.
-
VERY EASY TO READ.
-
READILY VISIBLE AND ACCESSIBLE.
-
DEPENDS ON THE AIRCRAFT TYPE.
Frage 45
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WHAT IS NEEDED IN ORDER TO PRODUCE EXTENSIVE PITTING DAMAGE IN DISSIMILAR METAL PARTS? (18773) REF.: FAA-H-8083-30, PAGE 6-4.
Antworten
-
THE PRESENCE OF SALT.
-
THE PRESENCE OF A CONDUCTOR.
-
THE ABSENCE OF ZINC CHROMATE PRIMER.
-
BIG CHANGE IN TEMPERATURES.
Frage 46
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WHAT MAY HAPPEN IF THE PROPELLER BLADES HAVE CRACKS? (18799) REF.: FAA-H-8083-30, PAGE 6-23.
Antworten
-
MAY NEED TO BE REWORKED.
-
MAY NEED TO BE REJECTED.
-
MAY TEND TO OXIDIZE.
-
MAY BE CUT.
Frage 47
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WHAT MUST EVERY PRINT HAVE? (18649) REF.: FAA-H-8083-30, PAGE 2-4.
Frage 48
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WHAT MUST ELEMENTS HAVE IN ORDER TO BE GOOD CONDUCTORS? (18931) REF.: FAA-H-8083-30, PAGE 10-3.
Antworten
-
MANY FREE ELECTRONS.
-
VERY LOW WEIGHT.
-
BE VERY SOFT.
-
BE VERY EXPENSIVE.
Frage 49
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WHAT IS REQUIRED FOR THE ELECTRONS TO STAY IN AN ORBIT? (18930) REF.: FAA-H-8083-30, PAGE 10-2.
Antworten
-
A HIGH TEMPERATURE.
-
A CERTAIN AMOUNT OF ELECTRICITY.
-
A CERTAIN AMOUNT OF HEAT.
-
A CERTAIN AMOUNT OF ENERGY.
Frage 50
Frage
WHAT ARE THE FORCES THAT ACT IN THE HELICOPTER DURING FLIGHT? (18979) REF.: AC 65-15A, PAGE 49.
Antworten
-
LIFT, THRUST, WEIGHT AND DRAG.
-
CUT, TORSION, FORWARD AND AFT.
-
BENDING, COMPRESSION, SHEAR AND TORSION.
-
BACK, FORWARD, UP AND DOWN.