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: ENGLISH FOR MAINTENANCE LICENSES.parte 10

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Título del Test:
: ENGLISH FOR MAINTENANCE LICENSES.parte 10

Descripción:
mecanico en mantenimiento

Fecha de Creación: 2025/11/06

Categoría: Otros

Número Preguntas: 10

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91.- WHAT CHARGE DO ELECTRONS POSSESS? (18977) REF.: FAA-H- 8083-30, PAGE 10-4. A.- DEPEND ON THE CURRENT FLOW DIRECTION. B.- NEUTRAL CHARGE. C.- NEGATIVE CHARGE. D.- POSITIVE CHARGE.

92.- WHAT IS THE NAME OF THE PHENOMENON THAT CAUSES FLOW CHANGE? (19029) REF.: AC 65-15A, PAGE 59. A.- SUPERSONIC FLOW. B.- WAVE FORMATIONS. C.- WAVE COMPRESSION. D.- FLOW DIRECTION.

93.- WHAT DO WE HAVE TO DO WHEN WE FIND DEEP PIT IN THE TEETH OF A GEAR? (19311) REF.: AC 65-12A, PAGE 413. A.- SEND IT TO MANUFACTURER. B.- REJECT IT. C.- REWORK IT. D.- CHANGE THE TEETH.

94.- WHAT TYPE OF CONTINUOUS MAINTENANCE PROGRAM UTILIZE THE AIRLINES? (18818) REF.: FAA-H-8083-30, PAGE 8-15. A.- A 100 HOURS AND ANNUAL INSPECTIONS. B.- A ROUTINE AND DETAILED INSPECTIONS. C.- PROGRESSIVE ANNUAL INSPECTIONS. D.- A DIFFERENT LEVEL OF INSPECTIONS.

95.- WHAT IS THE PRINCIPAL FLUID USED FOR PROPULSION IN EVERY TYPE OF POWERPLANT EXCEPT THE ROCKET? (19103) REF.: AC 65-12A, PAGE 1. A.- NAPHTA. B.- PETROLEUM. C.- AIR. D.- FUEL.

96.- WHAT ARE THE GROUPS THAT NUTS CAN BE DIVIDED INTO? (18747) REF.: FAA-H-8083-30, PAGE 5-45. A.- ALUMINUM AND NON -ALUMINUM NUTS. B.- METAL AND NON-METAL NUTS. C.- NON-SELF-LOCKING AND SELF LOCKING NUTS. D.- BIG AND SMALL NUTS.

97.- WHICH IS THE BASIC COMPONENT OF A CABLE? (18766) REF.: FAA-H-8083-30, PAGE 5-75. A.- THE WIRE. B.- THE ENVELOPE. C.- THE METAL. D.- THE LINE.

98.- IN WHAT HEAT TREATMENT ALLOYS EXISTS A SERIOUS POTENTIAL FIRE HAZARD? (18739) REF.: FAA-H-8083-30, PAGE 5- 27. A.- IN ANY ALLOYS. B.- IN ALUMINUM ALLOYS. C.- IN TITANIUM ALLOYS. D.- IN MAGNESIUM ALLOYS.

99.- WHAT MUST BE DONE AFTER AN NDT INSPECTIÓN? (18854) REF.: FAA-H-8083-30, PAGE 8-27. A.- THE PART MUST BE STORED. B.- THE PART MUST BE RINSED. C.- THE PART MUST BE DEMAGNETIZED. D.- THE PART MUST BE CLEANED.

100.- WHAT IS THE WINGSPAN? (18828) REF.: FAA-H-8083-30, PAGE 1-20. A.- THE CHORD OF THE WING. B.- THE LENGHT OF THE WING FROM LEADING EDGE TO TRAILING EDGE. C.- THE LENGHT OF THE WING FROM WINGTIP TO WINGTIP. D.- THE LENGHT OF THE WING FROM WINGTIP TO WINGROOT.

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