ENGLISH FOR MAINTENANCE LICENSES.parte 14

131.- WHY THE LANDING GEAR OF MOST HIGH-SPEED OR LARGE AIRCRAFT IS RETRACTED? (19281) REF.: AC 65-15A, PAGE 14. A.- TO INCREASE LOAD CAPABILITY AND DECREASE VOID PLACE. B.- TO INCREASE WIND RESISTANCE DURING LANDING. C.- TO REDUCE NOISE AND TURBULENCE DURING ALL FLIGHT. D.- TO REDUCE WIND RESISTANCE DURING FLIGHT.

132.- HOW MANY SYSTEMS HAS EACH CARBURATOR TO PROVIDE FOR ENGINE OPERATION UNDER VARIOUS LOADS AND AT DIFFERENT ENGINE SPEEDS? (19105) REF.: AC 65-12A, PAGE 115. A.- EACH CARBURATOR HAS SIX SYSTEMS. B.- EACH CARBURATOR HAS MANY SYSTEMS. C.- EACH CARBURATOR HAS NINE SYSTEMS. D.- THE CARBURATOR DOES NOT HAVE OTHER SYSTEMS.

133.- UNTIL WHEN THE MECHANICS HAVE TO TIGHTEN THE NUTS BY HAND? (18811) REF.: FAA-H-8083-30, PAGE 7-14. A.- UNTIL THE NUTS ARE READY TO GIVE TORQUE. B.- THE NUTS MUST BE INSTALLED WITH A SPECIAL WRENCH. C.- UNTIL AN INCREASE IN RESISTANCE TO TURNING IS ENCOUNTERED. D.- UNTIL THE NUT IS INSTALLED ON THE BOLT.

134.- WHAT PROVIDES THE NECESSARY TO HOLD THE AIRPLANE IN LEVEL UNACCELERATED FLIGHT? (19104) REF.: AC 65-12A, PAGE. A.- THE FLIGHT CONTROLS. B.- THE DRAG. C.- THE LIFT. D.- THE ENGINE OR ENGINES.

135.- WHAT IS THE IMPORTANCE OF THE GROUND EFFECT FOR A HELICOPTER? (19024) REF.: AC 65.15A, PAGE 54. A.- AIDS IN INCREASING THE ENGINE POWER. B.- AID IN SUPPORTING THE HELICOPTER WHILE HOVERING. C.- THE AID IS THEORETICAL ONLY. D.- THE GROUND EFFECT PRODUCES ADVERSE EFFECTS.

136.- WHAT IS THE MEANING OF THE WORD HELICOPTER THAT COMES FROM GREEK? (18982) REF.: AC 65-15A, PAGE 49. A.- HORIZONTAL ROTATING WING AND VERTICAL ROTATING WING. B.- OVER CABIN WING AND TAIL WING. C.- HELICAL WING OR ROTATING WING. D.- OVER WING OR LONG ROTATING WING.

137.- WHEN OR WHERE SHOULD BE PERFORMED THE AIRCRAFT WASHING? (18792) REF.: FAA-H-8083-30, PAGE 6-20. A.- IN THE SHADE WHENEVER POSSIBLE. B.- ONLY INSIDE THE HANGAR. C.- DURING NIGHT. D.- ONLY DURING CLOUDY DAYS.

138.- WHAT COMBINATION IS THE UNIVERSAL HEAD RIVET? (18752) REF.: FAA-H-8083-30, PAGE 5-59. A.- THE UNIVERSAL HEAD RIVET INCLUDES ALL RIVETS TYPE. B.- IS A COMBINATION OF ROUNDHEAD, PLANEHEAD AND CHERRY HEAD RIVET. C.- IS A COMBINATION OF SQUAREDHEAD, BRIGHTHEAD AND BRAZIER HEAD RIVET. D.- IS A COMBINATION OF ROUNDHEAD, FLATHEAD AND BRAZIER HEAD RIVET.

139.- WHAT DETERMINES THE OVERALL LENGTH OF THE SHANK OF THE RIVET? (18755) REF.: FAA-H-8083-30, PAGE 5-61. A.- THE WIDTH AND HEIGH OF THE SHOP HEAD. B.- THE THICKNESS OF THE MATERIAL BEING RIVETED. C.- THE STRESS REQUIRED. D.- THE STRENGTH OF THE MATERIAL BEING RIVETED.

140.- WHAT CHANGES WHEN THE AIRCRAFT ATTITUDE CHANGES? (18814) REF.: AC 65-15A, PAGE 31. A.- THE YAW ANGLE. B.- THE ANGLE OF ATTACK. C.- THE LANDING ANGLE. D.- THE TRACK ANGLE.