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TEST BORRADO, QUIZÁS LE INTERESETest in English for Maintenance Licenses

COMENTARIOS ESTADÍSTICAS RÉCORDS
REALIZAR TEST
Título del test:
Test in English for Maintenance Licenses

Descripción:
de 151 a 201

Autor:
AVATAR

Fecha de Creación:
26/04/2019

Categoría:
Psicotécnicos

Número preguntas: 50
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Temario:
152.- WHAT ALLOYS ARE PRIMARILLY USED IN THE CONSTRUCTION OF THE SEMIMONOCOQUE FUSELAGE? (19276) REF.: AC 65-15A, PAGE 3. A.- THE ALLOYS OF ALUMINUM AND METALS. B.- THE ALLOYS OF ALUMINUM AND TITANIUM. C.- THE ALLOYS OF ALUMINUM AND MAGNESIUM. D.- THE ALLOYS OF ALUMINUM AND COPPER. .
153.- WHAT MUST BE AVOIDED WHEN USING MECHANICAL CLEANING MATERIAL? (18800) REF.: FAA-H-8083-30, PAGE 6-25. A.- USING THE CLEANING MATERIAL IN CLOSE PLACE. B.- BREATHING OF THE CLEANING FUMES. C.- EYE AND SKIN CONTAMINATION. D.- DAMAGE TO THE FINISHES AND SURFACES.
154.- WHAT PARTS HAVE THE SELF-PLUGGING (FRICTION LOCK) BLIND RIVETS? (18754) REF.: FAA-H-8083-30, PAGE 5-60. A.- A RIVET HEAD WITH A HOLLOW SHANK OR SLEEVE AND A STEM THAT EXTENDS THROUGH THE HOLLOW SHANK. B.- A RIVET HEAD WITH A SOLID SHANK OR SLEEVE AND A STEM THAT EXTENDS THROUGH THE ENTIRE SHANK. C.- A PLAINHEAD RIVET WITH A HOLLOW SHANK OR SLEEVE AND A STEM THAT EXTENDS THROUGH THE SPECIAL SHANK. D.- A FLATHEAD RIVET WITH A COPPER SHANK OR SLEEVE AND A STEM THAT EXTENDS THROUGH THE HOLLOW SHANK.
155.- WHAT HAS TO BE CONSIDERED DURING THE SELECTION OF THE TYPE OF MATERIALS TO BE USED IN AIRCRAFT CLEANING? (18784) REF.: FAA-H-8083-30, PAGE 6-10. A.- THE NATURE OF THE MATTER TO BE REMOVED. B.- THE NATURE OF THE MATERIAL TO BE CLEANED. C.- THE HELP NEEDED FOR A GOOD CLEANING. D.- THE KNOWLEDGE OF CLEANING PERSONNEL.
156.- WHAT DOES THE RESULTANT FORCE IN A POSITIVE ANGLE OF ATTACK HAVE? (19039) REF.: AC 65-15A, PAGE 31. A.- IT HAS MAGNITUDE, LONGITUDE AND FORCE. B.- IT HAS MAGNITUDE, DIRECTION AND LOCATION. C.- IT HAS LIFT, DRAG AND EFFECT. D.- IT HAS AIRFOIL, CHORD AND LIFT.
157.- WHAT IS ONE RULE FOR THE LOCATION OF THE DATUM? (18715) REF.: FAA-H-8083-30, PAGE 4-2. A.- IT HAS HAVE AN EXACT MEASURE FROM THE AIRCRAFT NOSE. B.- IT HAS TO BE KNOWN. C.- IT DOES NOT CHANGE DURING THE LIFE OF THE AIRCRAFT. D.- IT HAS TO BE CLOSE TO THE AIRCRAFT NOSE.
158.- WHAT ARE THE MAIN TYPES OF PINS USED IN AIRCRAFT STRUCTURE? (18767) REF.: FAA-H-8083-30, PAGE 5-79. A.- THEY ARE THE ROLL PIN, WIRE PIN AND COTTER PIN. B.- THEY ARE THE TAPER PIN, FLATHEAD PIN AND COTTER PIN. C.- THEY ARE THE LANDING GEAR PIN, NUT PIN AND SECURITY PIN. D.- THEY ARE THE SAFETY CLIP PIN, ROUNDHEAD PIN AND ROLL PIN.
159.- HOW MANY WAYS OF GROUPING AIRCRAFT INSTRUMENTS ARE THERE? (18806) REF.: AC 65-15A, PAGE 469. A.- THERE ARE MANY WAYS OF GROUPING AIRCRAFT INSTRUMENTS. B.- THERE ARE TWO WAYS OF GROUPING AIRCRAFT INSTRUMENTS. C.- THERE ARE VARIOUS WAYS OF GROUPING AIRCRAFT INSTRUMENTS. D.- THE AIRCRAFT INSTRUMENTS DISTRIBUTION DEPEND THE COCKPIT SIZE.
160.- HOW MANY SIMPLE MACHINES ARE THERE? (18664) REF.: FAA-H-8083-30, PAGE 3-8. A.- THERE ARE ONLY TWO SIMPLE MACHINES. B.- THERE ARE ONLY TWENTY TWO SIMPLE MACHINES. C.- THERE ARE EIGHT SIMPLE MACHINES. D.- THERE ARE ONLY SIX SIMPLE MACHINES.
161.- WHAT FORM DO THE HEATING ELEMENTS HAVE IN THE ELECTRICITY HEATED FURNACE? (18998) REF.: FAA-H-8083-30, PAGE 5-15. A.- WIRE OR RIBBON. B.- CABLE OR TAPE. C.- RULE OR LEAD. D.- ROUND OR SQUARE.
162.- WHAT MAY RESULT, AS A GENERAL RULE, IF FURNACES ARE USED AT DIFFERENT TEMPERATURE RANGE? (18735) REF.: FAA-H-8083-30, PAGE 5-15. A.- THE OBJECT WILL HAVE EXTRA STRENGTH. B.- THE RESULTS IN WORK WILL BE OF DIFFERENT ALLOYS. C.- THE RESULTS IN WORK WILL BE OF SUPERIOR QUALITY. D.- THE RESULTS IN WORK WILL BE OF INFERIOR QUALITY.
163.- HOW MANY TYPES OF CLEANING AGENTS APPROVED FOR USE IN CLEANING AIRCRAFT ARE THERE? (18791) REF.: FAA-H-8083-30, PAGE 6-19. A.- VERY FEW TYPES. B.- HUNDREDS OF DIFFERENT TYPES. C.- ABOUT FOUR OR FIVE DIFFERENT TYPES. D.- MANY DIFFERENT TYPES.
164.- WHAT ADVANTAGES DOES THE USE OF THE SEMIMONOCOQUE FUSELAGE CONSTRUCTION HAVE? (19277) REF.: AC 65-15A, PAGE 5. A.- ALL CONSTRUCTION HAVE THE SAME DISADVANTAGES. B.- ALL CONSTRUCTION HAVE THE SAME ADVANTAGES. C.- IT HAS NO ADVANTAGES. D.- IT HAS A NUMBER OF ADVANTAGES.
165.- WHAT DO PROPELLERS OF AIRCRAFT POWERED BY RECIPROCATING OR TURBOPROP ENGINES DO WITH RESPECT TO THE AIR? (19102) REF.: AC 65-12A, PAGE 1. A.- ACCELERATE A SMALL MASS OF AIR THROUGH A LARGE VELOCITY CHANGE. B.- ACCELERATE A LARGE MASS OF AIR THROUGH A SMALL VELOCITY CHANGE. C.- ACCELERATE A LARGE MASS OF AIR THROUGH A LARGE VELOCITY CHANGE. D.- ACCELERATE A SMALL MASS OF AIR THROUGH A SMALL VELOCITY CHANGE.
166.- WHAT FURNISHES THE POWER NEEDED TO ROTATE THE PROPELLER BLADES? (19308) REF.: AC 65.12A, PAGE 325 A.- THE FIRE SYSTEM. B.- THE PISTONS. C.- THE ENGINE. D.- THE CYLINDERS.
167.- WHERE IS TYPICAL TO FIND THE PLANETARY SUN GEAR SYSTEM? (18667) REF.: FAA-H-8083-30, PAGE 3-12. A.- IN MANY TURBINE AND RECIPROCATING ENGINES. B.- IN AN ACCESORY REDUCTION GEARBOX. C.- IN A PROPELLER REDUCTION GEARBOX. D.- IN A TURBINE REDUCTION GEARBOX.
168.- WHAT MUST ALSO KNOW THE PEOPLE WHO MAINTAIN AND REPAIR AIRCRAFT? (18651) REF.: FAA-H-8083-30, PAGE 3-1 A.- SHOULD HAVE A KNOWLEDGE OF ONWARD PHYSICS B.- SHOULD HAVE A KNOWLEDGE OF BASIC CHEMISTRY. C.- SHOULD HAVE A KNOWLEDGE OF BASIC METEOROLGY. D.- SHOULD HAVE A KNOWLEDGE OF BASIC PHYSICS.
169.- WHAT LIMITS OIL PRESSURE TO THE VALUE SPECIFIED BY THE ENGINE MANUFACTURER? (19297) REF.: AC 65-12A, PAGE 300. A.- THE OIL COOLER SYSTEM. B.- ALL THE OIL CONTROL SYSTEM. C.- THE OIL PRESSURE REGULATOR. D.- THE OIL PRESSURE RELIEF VALVE.
170.- WHICH IS THE MOST OFTEN USED LIFT-MODIFYING DEVICE, FOR SMALL AND LARGE AIRPLANE? (18710) REF.: FAA-H-8083-30, PAGE 3-48. A.- THE WING FLAPS AND THE LEADING EDGES. B.- THE MAIN FLIGHT CONTROLS. C.- THE ENTIRE WING. D.- THE WING FLAPS.
171.- WHAT DOES THE MONOSPAR WING INCORPORATE IN ITS CONSTRUCTION? (19278) REF.: AC 65-15A, PAGE 7. A.- ONLY ONE MAIN LONGITUDINAL MEMBER. B.- TWO MAIN LONGITUDINAL MEMBERS. C.- SEVERAL MAIN LONGITUDINAL MEMBERS. D.- ONE MAIN LONGITUDINAL MEMBER AND ONE SECONDARY MEMBER.
172.- WHAT DETERMINES THE RATIO OF FUEL TO AIR IN THE MIXTURE? (19106) REF.: AC 65-12A, PAGE 115. A.- THE AIRCRAFT SPEED. B.- THE MIXTURE CONTROL SYSTEM. C.- THE ENGINE POWER. D.- THE AIRCRAFT ALTITUDE AND ACTITUDE.
173.- IN WHAT APPLICATIONS CAN BE USED THE MECHANICAL LOCK TYPE OF SELF-PLUGGING RIVET? (18758) REF.: FAA-H-8083-30, PAGE 5-63. A.- THEY CAN BE USED IN THE SAME APPLICATIONS AS THE FRICTION LOCK RIVET. B.- THEY CAN BE USED IN THE SAME APPLICATIONS AS THE PULL-THRU RIVET. C.- THEY CAN BE USED IN THE SAME APPLICATIONS AS THE BULBED CHERRYLOCK RIVET. D.- THEY CAN BE USED IN THE SAME APPLICATIONS AS THE ROUNDHEAD RIVET.
174.- WHAT IS THE MAXIMUN WEIGHT OF AN AIRCRAFT? (18716) REF.: FAA-H-8083-30, PAGE 4-3. A.- IS THE WEIGHT OF AN AIRCRAFT SHOWED IN THE SCALE. B.- IS THE MAXIMUN AUTHORIZED LOAD WEIGHT OF THE AIRCRAFT AND THE FUEL. C.- IS THE MAXIMUN WEIGHT OF THE AIRCRAFT WEIGHED IN ANY MOMENT. D.- IS THE MAXIMUN AUTHORIZED WEIGHT OF THE AIRCRAFT AND ITS CONTENTS.
175.- WHICH AIRPLANE PARTS ARE EQUIPPED WITH AN AXLE ATTACHED TO THE LOWER CYLINDER TO PROVIDE FOR INSTALLATION OF THE WHEELS? (19270) REF.: AC 65-15A, PAGE 343. A.- THE SHOCK STRUTS. B.- THE FLAPS. C.- THE ENGINE. D.- THE MAIN FLIGHT CONTROLS.
176.- WHICH ARE THE MAIN STRUCTURAL PARTS OF A WING? (19279) REF.: AC 65-15A, PAGE 8. A.- THE LEADING EDGE, THE TRAILING EDGE AND THE CHORD LINE. B.- THE SPARS, THE RIBS OR BULKHEADS AND THE STRINGERS OR STIFFENERS. C.- THE METAL SPAR SHAPES, THE SKIN AND THE STRINGERS OR STIFFENERS. D.- THE FLAPS, THE AILERON, THE SPEED BRAKES OR FLIGHT SPOILERS AND THE LEADING EDGES.
177.- WHICH IS THE AIRCRAFT PART THAT SUPPORTS THE AIRCRAFT DURING LANDING OR WHILE IT IS RESTING OR MOVING ABOUT ON THE GROUND? (19285) REF.: AC 65-15A, PAGE 23. A.- THE FIVE MAIN PARTS OF THE AIRCRAFT. B.- THE AIRFOIL AND THE POWER PLANTS. C.- THE POWER PLANTS. D.- THE LANDING GEAR.
178.- WHAT INSPECTION PROCESS CONSISTS IN MAGNETIZING THE PART AND THEN APPLYING FERROMAGNETIC PARTICLES TO THE SURFACE AREA TO BE INSPECTED? (18842) REF.: FAA-H-8083-30, PAGE 8-24. A.- THE FERROMAGNETIC INSPECTION. B.- THE LIQUID PENETRANT INSPECTION. C.- THE ACOUSTIC EMISSION INSPECTION. D.- THE MAGNETIC PARTICLE INSPECTION.
179.- WHAT ARE THE FUNDAMENTAL LAWS GOVERNING THE ACTION OF AIR ABOUT A WING? (19036) REF.: AC 65-15A, PAGE 30. A.- THE LAW OF VELOCITY AND SPEED. B.- THE BERNOULLI'S PRINCIPLE. C.- THE PASCAL'S LAW OF MOTION. D.- THE NEWTON'S LAW OF MOTION.
180.- WHAT MUST BE CAREFULLY DETERMINED IN ANY DAMAGED PART? (19125) REF.: AC 65-15A, PAGE 130. A.- THE ADJACENT PART. B.- THE FASTENER OF THE PART. C.- THE ALLOY OF THE PART. D.- THE FUNCTION OF THE PART.
181.- WHAT MUST BE KNOWN IN ORDER TO KNOW THE DENSITY OF A SUBSTANCE? (18654) REF.: FAA-H-8083-30, PAGE 3-2. A.- ITS VOLUME AND COMPOSITION. B.- ITS BASIC ELEMENTS AND ATOMIC WEIGHT. C.- ITS WEIGHT AND VOLUME. D.- ITS COMPOSITION AND GRAVITY.
182.- WHAT RIVETS ARE USED ON INTERIOR STRUCTURES? (18751) REF.: FAA-H-8083-30, PAGE 5-59. A.- THE SHEAR STRENGTH RIVET AND THE HEAT TREAT RIVET. B.- THE COUNTERSUNK HEAD RIVET AND THE SOLID RIVET. C.- THE FLATHEAD RIVET LIKE THE ROUNDHEAD RIVET. D.- THE BRAZIER HEAD RIVET AND THE UNIVERSAL HEAD RIVET.
183.- WHAT IS THE FIRST IMPORTANT CONSIDERATION IN THE HEAT TREATMENT OF A STEEL PART? (18737) REF.: FAA-H-8083-30, PAGE 5-19. A.- IS TO KNOW ITS PHYSICAL COMPOSITION. B.- IS TO KNOW ITS CHEMICAL COMPOSITION. C.- IS TO KNOW THE OVEN TEMPERATURE. D.- IS TO KNOW THE COOLING PROCEDURE.
184.- WHAT IS THE TERMINATING COMPONENT OF THE BASIC ENGINE? (19304) REF.: AC 65-12A, PAGE 59. A.- THE JET NOZZLE. B.- THE TAILPIPE. C.- THE EXHAUST CONE ASSEMBLY D.- THE THRUST REVERSE.
185.- IN WHAT CONSISTS THE ENVELOPE METHOD OF COVERING WING WITH FABRIC? (18850) REF.: AC 65-15A, PAGE 93. A.- CONSIST IN GLUEING FABRIC OVER THE METAL TO MAKE AN ENVELOPE OR FOLD. B.- CONSIST IN EMBROIDERING COTTON TO MAKE AN ENVELOPE OR SLEEVE. C.- CONSISTS IN GLUEING FABRIC TO MAKE AN ENVELOPE OR SLEEVE. D.- CONSISTS IN SEWING FABRIC TO MAKE AN ENVELOPE OR SLEEVE.
186.- WHAT DOES THE EMPTY WEIGHT OF AN AIRCRAFT INCLUDE? (18717) REF.: FAA-H-8083-30, PAGE 4-4. A.- INCLUDES ALL OPERATING EQUIPMENT THAT HAS A FIXED LOCATION AND IS ACTUALLY INSTALLED IN THE AIRCRAFT. B.- INCLUDES ALL EQUIPMENT WEIGHT THAT HAS A MOVABLE LOCATION AND IS ACTUALLY CHECKED. C.- INCLUDES SOME OPERATING EQUIPMENT THAT HAS A POSITION AND ITS AIRWORTHINESS. D.- INCLUDES THE ENTIRE OPERATING EQUIPMENT THAT HAS A FIXED OR MOVABLE LOCATION AND IS ACTUALLY INSTALLED IN THE AIRCRAFT.
187.- WHERE IS LOCATED THE DISCHARGE NOZZLE IN A CARBURATOR? (19109) REF.: AC 65-12A, PAGE 115. A.- DIRECTLY IN THE MANIFOLD PRESSURE. B.- IN THE HIGH PRESSURE SIDE OF THE CARBURATOR. C.- IN THE THROAT PRESSURE SIDE OF THE VENTURI. D.- IN THE THROAT OF THE VENTURI.
188.- IN WHAT NUMERALS IS THE DIAL FACE OF THE TYPICAL ALTIMETER GRADUATED? (19274) REF.: AC 65-15A, PAGE 476. A.- IS GRADUATED WITH NUMERALS FROM ZERO TO NINE INCLUSIVE. B.- IS GRADUATED WITH NUMERALS, LETTERS AND SYMBOLS INCLUSIVE. C.- THE GRADUATION DEPENDS ON THE AIRPLANE MANUFACTURER. D.- THE GRADUATION DEPENDS ON THE INSTRUMENT MANUFACTURER.
189.- WHAT IS THE DENSITY OF A SUBSTANCE? (18653) REF.: FAA-H-8083-30, PAGE 3-2. A.- IS ITS VOLUME PER UNIT OF WEIGHT. B.- IS ITS WEIGHT PER UNIT OF VOLUME. C.- IS ITS COLOR AND WEIGHT PER UNIT OF VOLUME D.- IS ITS CHEMISTRY COMPOSITION AND PHYSICAL RESISTANCE.
190.- IN HOW MANY SECTIONS IS THE DATA SHEET DIVIDED? (18817) REF.: FAA-H-8083-30, PAGE 8-5. A.- INTO ONE OR MORE SECTIONS. B.- INTO THREE OR MORE SECTIONS. C.- AT LEAST INTO TWELVE SECTIONS. D.- INTO FOUR OR SIX SECTIONS.
191.- WHAT TEMPERATURE WILL INDICATE THE CYLINDER HEAD TEMPERATURE INDICATOR PRIOR TO OPERATE THE ENGINE? (19307) REF.: AC 65-12A, PAGE 322. A.- WILL INDICATE THE CYLINDER TEMPERATURE. B.- WILL INDICATE THE FREE OUTSIDE AIR TEMPERATURE. C.- WILL INDICATE ANY FREE TEMPERATURE. D.- WILL INDICATE THE ENGINE GENERAL TEMPERATURE.
192.- WHAT IS THE CHORD OF AN AIRFOIL OR WING SECTION? (19040) REF.: AC 65-15A, PAGE 31. A.- IS A ROPE USED TO TIE THE WING FROM THE LEADING EDGE TO TRAILING EDGE. B.- IS A STRAIGHT LINE WHICH CROSSES THE WING FROM THE ROOT TO THE WING TIP. C.- IS AN IMAGINARY STRAIGHT LINE WHICH PASSES THROUGH THE SECTION FROM THE LEADING EDGE TO TRAILING EDGE. D.- IS A REAL STRAIGHT LINE WHICH UNITES THE SECTION FROM THE LEADING EDGE TO TRAILING EDGE.
193.- WHAT IS THE CENTER OF GRAVITY RANGE FOR AN AIRCRAFT? (18724) REF.: FAA-H-8083-30, PAGE 4-17. A.- IS THE AFT AND REAR BALANCE LIMITS. B.- IS THE LIMITS WITHIN WHICH THE AIRCRAFT MUST BALANCE. C.- ARE ALL THE DISTANCES THAT ARE CONSIDERED DURING WEIGHING. D.- IS WHERE THE WEIGH IS CONCENTRATED.
194.- HOW MAY BE CONSIDERED THE CENTER OF GRAVITY IN AN AIRCRAFT? (19287) REF.: AC 65-15A, PAGE 33. A.- AS A POINT AT WHICH THE BALANCE OF THE AIRCRAFT IS OPTIMUM. B.- AS A POINT AT WHICH ALL THE WEIGHT OF THE AIRCRAFT IS CONCENTRATED C.- AS THE REAR AND FRONT POINT AT WHICH ALL THE WEIGH OF THE AIRCRAFT IS LIMITED. D.- AS A PLACE WHERE ALL THE LOAD IN THE AIRCRAFT ISCONCENTRATED.
195.- WHAT DOES THE CARBURETOR HAVE IN ORDER TO SHUT OFF THE FUEL TO STOP THE ENGINE? (19107) REF.: AC 65-12A, PAGE 115. A.- A FUEL INYECTION AND A MANUAL START SYSTEM. B.- AN AUTOMATIC SELECTOR VALVE IN THE CARBURATOR. C.- AN IDLE CUTOFF SYSTEM. D.- A FUEL CONTROL IN THE COCKPIT.
196.- WHAT DOES THE CARBURETOR AIR TEMPERATURE GAGE INDICATE? (19312) REF.: AC 65-12A PAGE 431. A.- INDICATE THE CYLINDERS TEMPERATURE AND THE AIR AROUND THE CARBURATOR. B.- THE QUANTITY OF THE AIR THAT IS IN THE CYLINDERS C.- THE TEMPERATURE OF THE AIR BEFORE IT ENTERS THE CARBURATOR. D.- THE PRESSURE AND THE TEMPERATURE OF THE AIR AFTER IT ENTERS THE CARBURATOR.
197.- WHAT DOES THE BLADE FLAPPING ACTION CREATE IN A HELICOPTER? (19023) REF.: AC 65-15A, PAGE 53. A.- CREATES AN UNBALANCE CONDITION WITH RESULTING VIBRATION. B.- CREATES A BIG LIFT CONDITION WITH RESULTING IN A SMOOTH FLIGHT. C.- CREATES SOME ADDITIONAL DRAG AND THE ENGINE HAS TO DEVELOP MORE POWER. D.- CREATES A BALANCE CONDITION WITH RESULTING IN LESS VIBRATION.
198.- WHAT IS USED TO DESIGN THE BASIC COMPONENT OF A CABLE? (18765) REF.: FAA-H-8083-30, PAGE 5-75. A.- NUMBERS AND LETTERS. B.- THE WIRE METAL. C.- THE AMOUNT OF WIRES IN EACH STRAND AND THE QUANTITY OF CABLES. D.- THE NUMBER OF STRANDS AND THE NUMBER OF WIRES IN EACH STRAND.
199.- WHICH IS USUALLY THE MOST CONVENIENT LOCATION FOR TEMPORARY BALLAST? (18644) REF.: FAA-H-8083-30, PAGE 4-23. A.- THE BAGGAGE COMPARTMENT. B.- THE CABIN COMPARTMENT. C.- THE TAIL COMPARTMENT. D.- THE WING ROOT COMPARTMENT.
200.- WHAT IS THE PURPOSE OF DEVELOPING SPECIAL TOOLS AND DEVICES? (19046) REF.: AC 65-15A, PAGE 133. A.- TO HELP THE MECHANIC MAKE HIS HOME-WORK ON TIME, COMPLEX AND UP TO DATE. B.- TO HELP THE MECHANIC MAKE HIS JOB SWIFT, THE BEST AND GOOD. C.- TO HELP THE MECHANIC MAKE HIS WORK SOFT, RELAXED AND QUICKLY. D.- TO HELP THE MECHANIC MAKE HIS WORK FASTER, SIMPLER AND BETTER.
201.- HOW MANY BRAKES APPLICATIONS CAN BE MADE WITH THE AIR BOTTLE THAT HAS NORMAL COMPRESSED AIR? (19268) REF.: AC 65-15A, PAGE 336. A.- SEVEN APPLICATION OF THE BRAKES. B.- ONE APPLICATION UNTIL A COMPLETE AIRCRAFT STOP. C.- SEVERAL APPLICATIONS OF THE BRAKES. D.- TWO FULL BRAKES APPLICATION.
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