ENGLISH FOR MAINTENANCELICENSES 2

31.- HOW LONG HAVE HIGH TENSION IGNITION SYSTEMS BEEN IN USE? (19298) REF.: AC 65-12A, PAGE 186. A.- FOR MORE THAN HALF A CENTURY. B.- FOR MORE THAN A CENTURY. C.- FOR MORE THAN SIXTY YEARS. D.- FOR MANY TIMES.

32.- 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. A.- IN THE LIQUID IT WEIGHS LESS THAN IN THE FREE SPACE. B.- IN THE LIQUID IT WEIGHS MORE THAN IN THE FREE SPACE. C.- IN THE LIQUID IT WEIGHS EQUAL THAN IN THE FREE SPACE. D.- IN THE LIQUID IT WEIGHS 10% LESS THAN IN THE FREE SPACE.

33.- WHAT MUST A HELICOPTER STRUCTURAL MEMBERS RESIST? (18837) REF.: AC 65-15A, PAGE 25. A.- SHOCK. B.- LOADS. C.- FORCE. D.- STRESS.

34.- WHAT IS HEAT? (18696) REF.: FAA-H-8083-30, PAGE 3-19. A.- IS A FORM OF ENERGY. B.- IS A FORM OF TEMPERATURE. C.- IS A FORM OF RADIATION. D.- IS A FORM OF WORK.

35.- WHAT HAPPENS IF HEAT IS APPLIED TO A METAL? (18729) REF.: FAA-H-8083-30, PAGE 5-2. A.- WILL CAUSE IT TO CONTRACT OR BECOME LARGER. B.- WILL CAUSE IT TO EXPAND OR BECOME LARGER. C.- WILL CAUSE IT TO EXPAND OR BECOME SHORTER. D.- WILL CAUSE IT TO INCREASE THE WEIGHT OR BECOME HEAVIER.

36.- WHAT SEWING METHOD IS NECESSARY TO CLOSE THE FINAL OPENING IN THE COVERING? (18846) REF.: AC 65-15A, PAGE 90. A.- MACHINE SEWING. B.- DOUBLE STITCH SEWING. C.- AUTOMATIC SEWING. D.- HAND SEWING.

37.- WHAT IS THE RIVETS GRIP LENGTH? (18761) REF.: FAA-H-8083-30, PAGE 5-64. A.- THE TOTAL SHEET THICKNESS PLUS THE RIVET LENGTH. B.- THE NOMINAL RIVET LENGTH. C.- THE SHANK DIAMETER. D.- THE MAXIMUN TOTAL SHEET THICKNESS TO BE RIVETED.

38.- WHAT ARE THE METHODS TO COVER FUSELAGES? (18851) REF.: AC 65-15A, PAGE 95. A.- THE SLEEVE OR BLANKET METHOD. B.- THE FABRICS SLEEVE OR PLASTIC BLANKET METHOD. C.- THE PARTIAL O TOTAL COVERING METHOD. D.- THER ARE NO METHODS TO COVER FUSELAGES.

39.- IN WHAT IS NOT BASED THE MINIMUM FUEL FOR TURBINE ENGINE POWERED AIRCRAFT? (18718) REF.: FAA-H-8083-30, PAGE 4-5. A.- ON ENGINE SPEED. B.- ON ENGINE HORSEPOWER. C.- ON ALTITUDE OF FLIGHT. D.- ON FLIGHT DISTANCE.

40.- WHAT MUST BE MAINTAINED FOR EFFICIENT OPERATION OF SHOCK STRUTS? (19271) REF.: AC 65-15A, PAGE 345. A.- THE PROPER CLEANNESS AND CORRECT O-RING. B.- THE PROPER FLUID LEVEL AND AIR PRESSURE. C.- THE PROPER TIRE PRESSURE AND FLUID LEVEL. D.- THE PROPER WHEEL, BRAKES AND FLUID.

41.- WHAT FORCES ACT ON AN AIRCRAFT, WHETHER IT IS ON THE GROUND OR IN FLIGHT? (19042) REF.: AC 65-15A, PAGE 131. A.- THE FORCES ARE CUTING, PUSHING OR BENDING. B.- THE FORCES ARE PULLING, PUSHING OR TWISTING. C.- THE FORCES ARE WEIGHT, THRUST OR DRAG. D.- THE FORCES ARE LIFTING, PUSHING OR DOWNWARD.

42.- HOW MUST THE MIXTURE BE IN ORDER FOR AN ENGINE TO DEVELOP MAXIMUN POWER AT FULL THROTTLE? (19115) REF.: AC 65-12A, PAGE 121. A.- THE FUEL MIXTURE MAY BE RICHER THAN FOR CRUISE. B.- THE FUEL MIXTURE IS THE SAME ALL THROUGH THE FLIGHT. C.- THE FUEL MIXTURE MUST BE RICHER THAN FOR CRUISE. D.- THE FUEL MIXTURE MUST BE LEANER THAN FOR CRUISE.

43.- WHAT ARE THE FACTORS TO CONSIDER IN THE SELECTION OF THE CORRECT RIVET FOR INSTALLATION? (18757) REF.: FAA-H8083-30, PAGE 5-61. A.- INSTALLATION LOCATION, PROTECTION OF THE MATERIAL BEING RIVETED, DIAMETERS OF THE MATERIAL BEING RIVETED AND STRESS DESIRED. B.- INSTALLATION PLACE, COMPOSITION OF THE TOOLS BEING USED, THINNESS OF THE MATERIAL BEING RIVETED AND STRENGTH DESIRE. C.- WORK LOCATION, ILUMINATION OF THE PLACE, COMPOSITION OF THE MATERIAL BEING RIVETED, THICKNESS OF THE MATERIAL BEING RIVETED AND QUALITY OF THE TOOLS. D.- INSTALLATION LOCATION, COMPOSITION OF THE MATERIAL BEING RIVETED, THICKNESS OF THE MATERIAL BEING RIVETED AND STRENGTH DESIRED.

44.- WHAT IS THE ADVANTAGE OF EXTERNAL AIRCRAFT SURFACES WITH REGARD TO INSPECTION AND MAINTENANCE? (18782) REF.: FAA-H-8083-30, PAGE 6-9. A.- IT HAS NO SPECIAL ADVANTAGES. B.- VERY EASY TO READ. C.- READILY VISIBLE AND ACCESSIBLE. D.- DEPENDS ON THE AIRCRAFT TYPE.

45.- WHAT IS NEEDED IN ORDER TO PRODUCE EXTENSIVE PITTING DAMAGE IN DISSIMILAR METAL PARTS? (18773) REF.: FAA-H-8083- 30, PAGE 6-4. A.- THE PRESENCE OF SALT. B.- THE PRESENCE OF A CONDUCTOR. C.- THE ABSENCE OF ZINC CHROMATE PRIMER. D.- BIG CHANGE IN TEMPERATURES.

46.- WHAT MAY HAPPEN IF THE PROPELLER BLADES HAVE CRACKS? (18799) REF.: FAA-H-8083-30, PAGE 6-23. A.- MAY NEED TO BE REWORKED. B.- MAY NEED TO BE REJECTED. C.- MAY TEND TO OXIDIZE. D.- MAY BE CUT.

47.- WHAT MUST EVERY PRINT HAVE? (18649) REF.: FAA-H-8083-30, PAGE 2-4. A.- THE BEST INK. B.- SOME MEANS OF IDENTIFICATION. C.- SOME MEANS OF ISSUE. D.- A POOR PAPER.

48.- WHAT MUST ELEMENTS HAVE IN ORDER TO BE GOOD CONDUCTORS? (18931) REF.: FAA-H-8083-30, PAGE 10-3. A.- MANY FREE ELECTRONS. B.- VERY LOW WEIGHT. C.- BE VERY SOFT. D.- BE VERY EXPENSIVE.

49.- WHAT IS REQUIRED FOR THE ELECTRONS TO STAY IN AN ORBIT? (18930) REF.: FAA-H-8083-30, PAGE 10-2. A.- A HIGH TEMPERATURE. B.- A CERTAIN AMOUNT OF ELECTRICITY. C.- A CERTAIN AMOUNT OF HEAT. D.- A CERTAIN AMOUNT OF ENERGY.

50.- WHAT ARE THE FORCES THAT ACT IN THE HELICOPTER DURING FLIGHT? (18979) REF.: AC 65-15A, PAGE 49. A.- LIFT, THRUST, WEIGHT AND DRAG. B.- CUT, TORSION, FORWARD AND AFT. C.- BENDING, COMPRESSION, SHEAR AND TORSION. D.- BACK, FORWARD, UP AND DOWN.

51.- WHAT IS THE LINK BETWEEN THE ENGINEERS WHO DESIGN AN AIRCRAFT AND THE WORKERS WHO BUILD, MAINTAIN, AND REPAIR IT? (18647) REF.: FAA-H-8083-30, PAGE 2-1. A.- THE HANGARS, TOOLS, TECHNICAL ORDERS AND LADDERS. B.- THE HANGARS AND LADDERS. C.- THE TOOLS AND TECHNICAL ORDERS. D.- THE DRAWINGS AND PRINTS.

52.- WHAT MAY DAMAGE THE DRACON? (18848) REF.: AC 65-15A, PAGE 93. A.- THE EXCESSIVE WATER. B.- THE EXCESSIVE HEAT. C.- THE EXCESSIVE SUN. D.- THE EXCESSIVE WIND.

53.- WHAT CREATES THE DISSYMMETRY OF LIFT IN AN HELICOPTER? (18989) REF.: AC 65-15A, PAGE 51. A.- THE DIFFERENTIAL TORQUE BETWEEN TWO ROTORS. B.- THE WIND DURING HOVERING OR VERTICAL FLIGHT. C.- THE HORIZONTAL FLIGHT OR THE DIFFERENTIAL TILT. D.- THE HORIZONTAL FLIGHT OR WIND DURING HOVERING.

54.- WHAT IS AN IMPORTANT CONSIDERATION WHEN CHOOSING MATERIAL TO USE IN AIRPLANE PARTS? (18728) REF.: FAA-H-8083- 30, PAGE 5-1. A.- THE DENSITY OF MATERIALS. B.- THE VOLUME OF MATERIALS. C.- THE HARDNESS. D.- THE STRENGTH.

55.- WHAT SIDE HAVE TO BE DEBURRED DURING A TUBING FLARING JOB? (18808) REF.: FAA-H-8083-30, PAGE 7-6. A.- BOTH ENDS BY THE INSIDE AND THE OUTSIDE TUBING. B.- THE OUTSIDE. C.- THE INSIDE. D.- THE INSIDE AND THE OUTSIDE.

56.- IN HOW MANY GROUP ARE DAMAGES CLASSIFIED? (19041) REF.: AC 65-15A, PAGE 131. A.- FROM SMALL DENTS TO HOLES. B.- FROM NEGLIGIBLE TO BIG DAMAGES. C.- INTO FOUR SPECIFIC GROUPS. D.- INTO FOUR GENERAL GROUPS.

57.- WHENEVER POSSIBLE, HOW SHOULD DAMAGED TUBING AND FLUID LINES BE REPAIRED? (18803) REF.: FAA-H-8083-30, PAGE 7- 2. A.- SHOULD BE REPAIRED WITH GOOD PARTS. B.- SHOULD BE REPAIRED WITH BRIGHT PARTS. C.- SHOULD BE REPAIRED WITH NEW PARTS. D.- SHOULD BE REPAIRED WITH OVERHAULED PARTS.

58.- WHAT DOES A COMPRESSION FORCE TRY TO DO? (18670) REF.: FAA-H-8083-30, PAGE 3-14. A.- IT TRIES TO CRUSH AN OBJECT. B.- IT TRIES TO TWIST AN OBJECT. C.- IT TRIES TO SLICE OR TO CUT AN OBJECT. D.- IT TRIES TO STRESS AN OBJECT.

59.- IN WHAT BODY PARTS OF THE BODY CAN COMPOSITE PRODUCTS BE VERY HARMFUL? (18740) REF.: FAA-H-8083-30, PAGE 5-33. A.- IN THE SKIN, EYES AND LUNGS. B.- IN THE HAND, FEET AND HAIR. C.- IN THE CHEST, ARMS AND FACE. D.- IN THE ELBOW, FINGERS AND NOSE.

60.- WHAT EFFECT CAN GREASE AND DIRT ACCUMULATION PRODUCE ON THE AIR-COOLED ENGINE? (18794) REF.: FAA-H-8083-30, PAGE 6-23. A.- PRODUCE A COOLING EFFECT. B.- PRODUCE A REFRIGERATING EFFECT. C.- PRODUCE AN INSULATION EFFECT. D.- PRODUCE A WEIGHT INCREASE.