ENGLISH FOR MAINTENANCE LICENSES.parte 13

121.- WHAT IS BECOMING LESS OF A PROBLEM WITH THE INTRODUCTION OF SEALED LEAD-ACID BATTERIES AND THE USE OF NICKEL-CADMIUM BATTERIES? (18762) REF.: FAA-H-8083-30, PAGE 6-3. A.- THE SPILLED BATTERY ACID IS A LESS OF A PROBLEM. B.- THE BATTERY DRAINAGE IS LESS OF A PROBLEM. C.- THE BATTERY MAINTENANCE IS A LESS OF A PROBLEM. D.- THE BATTERY COST IS A LESS OF A PROBLEM.

122.- WHAT MUST BE KNOWN WHEN AN AIRCRAFT IS BEING WEIGHTED? (18638) REF.: FAA-H-8083-30, PAGE 4-16. A.- THE TARE AND EMPTY WEIGHT MUST BE KNOWN. B.- THE LEVELING POINTS MUST BE KNOWN. C.- THE ARMS MUST BE KNOWN. D.- THE SCALE MUST BE KNOWN.

123.- WHAT SHOULD BE USED WHEN A FLUID LINE PASSES THROUGH A UNIVERSAL BULKHEAD FITTING, AND IT IS DESIRED TO SECURE THE LINE TO THE BULKHEAD? (18809) REF.: FAA-H-8083-30, PAGE 7-10. A.- A BULKHEAD FITTING SHOULD BE USED. B.- A BULKHEAD FITTING MAY BE USED. C.- TWO OR THREE SOFT OR MEDIUM HARD CLAMPS. D.- RUBBER-CUSHIONED CLAMPS SHOULD BE USED.

124.- WHAT ELEMENTS CONNECT UP THE COCKPIT CONTROLS TO CONTROL CABLES AND SURFACE CONTROLS? (19290) REF.: AC 65-15A, PAGE 68. A.- VARIOUS MECHANICAL LINKAGES. B.- MANY MECHANICAL LINKAGES CABLE. C.- SOME MECHANICAL AND ELECTRICAL LINKAGES. D.- VARIOUS PUSH-PULL RODS.

FLARING BE USED? (18807) REF.: FAA-H-8083-30, PAGE 7-6. A.- IN HARD COPPER, ANY ALUMINUM, AND STEEL ALLOYS TUBING. B.- IN SOFT COPPER, ALCLAD OR ALUMINUM, AND BURRS TUBING. C.- IN SOFT COPPER, ALUMINUM, AND BRASS TUBING. D.- IN CORROSION RESISTANT STEEL, TITANIUM, AND BRASS TUBING.

126.- IN WHAT TYPE OF MATERIAL DOES THE ULTRASONIC INSPECTION EQUIPMENT DETECT DEFECTS? (18841) REF.: FAA-H-8083-30, PAGE 8-21. A.- IN ALL TYPES OF CERAMIC MATERIALS. B.- IN ALL TYPES OF METAL MATERIALS. C.- IN ALL TYPES OF MATERIALS. D.- IN ALL TYPES OF COMPOSITES MATERIALS.

127.- WHAT ARE THE TRIM TABS SURFACES AND WHERE ARE THEY ATTACHED? (18709) REF.: FAA-H-8083-30, PAGE 3-47. A.- THEY ARE SMALL FIXED SURFACES AND ARE INSTALLED TO THE WING TRAILING EDGE. B.- THEY ARE SOME MOVABLE CONTROLS AND ARE ATTACHED TO THE FLAPS. C.- THEY ARE SMALL MOVABLE SURFACES AND ARE ATTACHED TO THE TRAILING EDGE OF FLIGHT CONTROLS. D.- THEY ARE BIG MOVABLE SURFACES AND ARE ATTACHED TO THE LEADING EDGE OF FLIGHT CONTROLS.

128.- WHY YOU MUST NEVER APPLY COMPOUND TO THE FACE OF THE FITTING OR THE FLARE? (18836) REF.: FAA-H-8083-30, PAGE 7-13. A.- BECAUSE THE COMPOUND IS VERY CORROSIVE AND DANGEROUS. B.- BECAUSE ANY FLUID WILL DISSOLVE THE COMPOUND. C.- BECAUSE THE COMPOUND WILL DESTROY THE METAL-TO- METAL CONTACT. D.- BECAUSE THE COMPOUND WILL FORM A GUM WITH THE LIQUID.

129.- WHAT OTHER STRESSES INCLUDE THE TORSION STRESS? (18672) REF.: FAA-H-8083-30, PAGE 3-14. A.- BENDING AND CUT. B.- TENSION AND COMPRESSION. C.- TENSION AND TORSION. D.- SHEAR AND CUT.

130.- TORQUE IS A VERY INTERESTING CONCEPT AND OCCURRENCE, AND IT IS DEFINITELY SOMETHING THAT NEEDS TO BE DISCUSSED IN CONJUNCTION WITH? (18660) REF.: FAA-H-8083-30, PAGE 3-7. A.- TOOLS AND MECHANICS. B.- WORK AND POWER. C.- METALS AND COMPOSITES. D.- STRESS AND STRENGTH.