Quiz
INGLES 1 DGAC (DE LA 1 A LA 50)
Perguntas do quiz (50)
1WHY AIR IS CONSIDERED A FLUID? (19286) REF.: AC 65-15A, PAGE
27.- AA.- BECAUSE IS A SUBSTANCE WHICH MAY BE MADE TO FLOW OR
CHANGE IT´S SHAPE BY THE APPLICATION OF MODERATE
PRESSURE. - B- BECAUSE IT HAS WEIGHT AND VOLUME
- CBECAUSE IT CAN BE USED IN BALLOON AND TIRES.
- DAIR IS NOT CONSIDERED A FLUID.
- AA.- BECAUSE IS A SUBSTANCE WHICH MAY BE MADE TO FLOW OR
2WHAT AIRPLANE SECTION IS CALLED LEADING EDGE? (18822) REF.:
AC 65-15A, PAGE 197.- ATHE FRONT SECTION OF WINGS, STABILIZERS OR OTHER
AIRFOILS. - BTHE AFT SECTION OF WINGS, STABILIZERS OR OTHER AIRFOILS.
- CANY SECTION OF WINGS, STABILIZERS OR AIRFOILS.
- DANY STRUCTURAL PART OF AN AIRCRAFT.
- ATHE FRONT SECTION OF WINGS, STABILIZERS OR OTHER
3ABSOLUTE PRESSURE IS EQUAL TO (18699) REF.: FAA-H-8083-30,
PAGE 3-25.- AINSTRUMENT PRESSURE.
- BATMOSPHERIC PRESSURE.
- CGAUGE PRESSURE PLUS ATMOSPHERIC PRESSURE
- DGAUGE PRESSURE MINUS ATMOSPHERIC PRESSURE.
4IN PLACE OF WHAT, THE SPECIAL FASTENERS THAT PRODUCE HIGH
STRENGTH WITH LIGHT WEIGHT, CAN BE USED? (18759) REF.: FAAH-8083-30,
PAGE 5-66.- AIN PLACE OF STANDARD SA BOLTS AND NUTS
- BIN PLACE OF CONVENTIONAL AN BOLTS AND NUTS
- CIN PLACE OF STRENGTH AND LIGHT AN BOLTS AND NUTS.
- DIN PLACE OF ANY BOLTS AND NUTS IF THEY ARE THE SAME SIZE.
5WHAT HAS TO DO A MECHANIC IN ORDER TO MAKE A RIVET HOLE
OF THE CORRECT SIZE? (19292) REF.: AC 65-15A, PAGE 169.- AAT THE END DRILL A HOLE SLIGHTLY UNDERSIZE.
- BFIRST PUT GREASE AT THE HOLE.
- CFIRST DRILL A HOLE SLIGHTLY UNDERSIZE.
- DFIRST DRILL A HOLE SLIGHTLY OVERSIZE.
6SURFACE CORROSION APPEARS AS A GENERAL: (18772) REF.: FAAH-8083-30,
PAGE 6-4.- AROUGHENING, ETCHING OR PITTING OF THE SURFACE.
- BCONTAMINATION OF THE METAL
- CWHITENNING OF THE METAL
- DHEATING OF THE SURFACE.
7HOW IS THE PROCEDURE FOR WELDING STAINLESS STEEL
COMPARED WITH THE PROCEDURE FOR WELDING CARBON
STEELS? (19132) REF.: AC 65-15A, PAGE 259.- AIT IS EXACTLY THE SAME.
- BIT IS BASICALLY THE SAME.
- CIT COULD BE THE SAME.
- D- BOTH PROCEDURE ARE ABSOLUTELY DIFFERENT
8SELF-LOCKING NUTS ARE USED ON AIRCRAFT TO (18833) REF.: FAAH-8083-30,
PAGE 5-46- APROVIDE TIGHT CONNECTIONS WHICH WILL SHAKE LOOSE
UNDER SEVERE VIBRATIONS. - BPROVIDE POOR CONNECTIONS WHICH WILL NOT SHAKE LOOSE
UNDER SEVERE VIBRATION. - CPROVIDE TIGHT CONNECTIONS WHICH WILL SHAKE LOOSE
UNDER LIGHT VIBRATIONS. - DPROVIDE TIGHT CONNECTIONS WHICH WILL NOT SHAKE LOOSE
UNDER SEVERE VIBRATION.
- APROVIDE TIGHT CONNECTIONS WHICH WILL SHAKE LOOSE
9HOW IS DEFINED MOTION? (18684) REF.: FAA-H-8083-30, PAGE 3-16.
- AIS A CONTINUED CHANGE OF POSITION OR PLACE.
- BIS CONTINUED CHANGE OF MASS AND DIAMETER.
- CIS AN ALTERATION IN POSITION OR PLACE.
- D- IS SPEED OR VELOCITY.
10HOW IS CALLED THE MOVEMENT ABOUT THE LONGITUDINAL AXIS?
(18994) REF.: AC 65-15A, PAGE 55.- AMOVEMENT.
- BYAW
- CPITCH
- DROLL.
11WHAT PRODUCES THE MOVEMENT ABOUT THE VERTICAL AXIS?
(18992) REF.: AC 65-15A, PAGE 55.- A- FLARE.
- B- DRAG.
- C- YAW.
- DPITCH.
12WHICH IS THE USE OF NACELLES AND OR PODS? (19280) REF.: AC
65-15A, PAGE 13.- ATO HOUSE THE AUXILIARY POWER UNIT.
- BTO HOUSE BAGGAGE.
- CTO HOUSE THE ENGINES.
- DTO HOUSE FUEL.
13WHAT METAL OR METAL ALLOY ARE NEARLY ALL ELASTIC STOP
NUTS MADE OF? (18748) REF.: FAA-H-8083-30, PAGE 5-48.- ATHEY ARE MADE OF ALUMINUM OR STEEL ALLOY
- BTHEY ARE MADE OF COPPER OR MAGNESIUM ALLOY.
- CTHEY ARE MADE OF IRON OR ALUMINUM ALLOY.
- DTHEY ARE MADE OF STEEL OR ALUMINUM ALLOY.
14WHAT COMPOUND DOES THE SYNTHETIC RUBBER CALLED
NEOPRENE HAVE? (18812) REF.: FAA-H-8083-30, PAGE 7-17.- A- IT HAS A PHOSPHATE BASE.
- B- IT HAS A SYNTHETIC BASE.
- CIT HAS A NATURAL BASE.
- DIT HAS AN ACETYLENE BASE.
15WHAT MUST YOU NEVER DO WHEN WEIGHING AN AIRCRAFT?
(18722) REF.: FAA-H-8083-30, PAGE 4-16.- AWEIGH IT WITH THE FUEL TANKS EMPTY.
- BWEIGH IT WITH THE OIL TANKS PARTIALLY FULL.
- CWEIGH IT WITH THE HYDRAULIC TANKS PARTIALLY FULL.
- DWEIGH IT WITH THE FUEL TANKS PARTIALLY FULL.
16HOW ARE USUALLY ATTACHED THE NONSTRUCTURAL MEMBERS
THAT ARE NOT REMOVABLE FROM THE HELICOPTER? (18840) REF.:
AC 65-15A, PAGE 25.- ATHEY ARE ATTACHED BY BOLTING OR STRUCTURAL WELDING.
- B- THEY ARE ATTACHED BY RIVETING OR SPOT WELDING.
- C- THEY ARE ATTACHED BY GLUEING OR SPOT WELDING.
- DTHEY ARE ATTACHED BY SOLDERING, BOLTING, RIVETING OR
ANY KIND OF WELDING.
17- WHEN IS IT NECESSARY TO MAKE REVISON TO A DRAWING? (18650)
REF.: FAA-H-8083-30, PAGE 2-6.- AWHEN THERE IS A CHANGE OF YEAR.
- BWHEN THERE IS A CHANGE IN AIRWORTHINESS CONDITION
- CWHEN CHANGES IN DIMENSIONS, DESIGN OR MATERIALS ARE
MADE. - DWHEN THERE IS A CHANGE IN AIRCRAFT CERTIFICATION.
18BY WHICH METHODS ARE NUTS, BOLTS, AND SCREWS SAFETIED
WITH WIRE? (18769) REF.: FAA-H-8083-30, PAGE 5-80.- A- BY THE SHORT WIRE OR LONG AND EXTRA LONG WIRE METHOD.
- BBY THE SINGLE WIRE FOR ELECTRICAL CONNECTORS OR
DOUBLE TWIST METHOD FOR PLUG AND BOLTS - C- BY THE SINGLE WIRE OR DOUBLE TWIST METHOD.
- DBY THE TRIPLE WIRE OR UNIQUE TWIST METHOD.
19WHICH IS ONE OF THE DIFFERENCES BETWEEN A HELICOPTER AND
A FIXED-WING AIRCRAFT? (18978) REF.: AC 65-15A, PAGE 49.- AIS THE TYPE OF FLIGHT.
- B- IS THE MAIN AND COCKPIT CABIN.
- C- IS THE MAIN SOURCE OF DRAG.
- DIS THE MAIN SOURCE OF LIFT.
20IN WHAT CONSISTS A RADIAL ENGINE? (19303) REF.: AC 65-12A,
PAGE 5.- AIN A ROW OR ROWS OF CYLINDERS ARRANGED RADIALLY
ABOUT A CENTRAL CRANKSHAFT. - BIN A ROW OR ROWS OF CYLINDERS ARRANGED RADIALLY
ABOUT A CENTRAL CRANKCASE. - CIN A ROW OR ROWS OF CYLINDERS ARRANGED OPPSOSITE
ABOUT A CENTRAL CRANKCASE. - DIN A LINE OR LINES OF CYLINDERS ARRANGED IN LINE ABOUT A
CRANKCASE.
- AIN A ROW OR ROWS OF CYLINDERS ARRANGED RADIALLY
21WHERE IS STAMPED THE ALLOY DESIGNATION ON LARGE
ALUMINUM ALLOY TUBING? (18802) REF.: FAA-H-8083-30, PAGE 7-2.- AIN THE INTERIOR.
- BON THE SURFACE.
- CWITH A TAG.
- DWITH A FORM 8130-3 ATTACHED.
22ON LARGER AIPLANES, FROM PRIVATE BUSINESS JETS TO LARGE
JUMBO JETS, IN RELATION OF WHAT ARE IDENTIFIED THE CENTER
OF GRAVITY AND ITS RANGE? (18727) REF.: FAA-H-8083-30, PAGE 4-
31.- A- IN RELATION TO THE CHORD LINE.
- BIN RELATION TO THE ROOT WIDTH OF THE WING.
- C- IN RELATION TO THE LENGTH OF THE WING.
- D- IN RELATION TO THE WIDTH OF THE WING.
23WHAT NONSTRUCTURAL MEMBERS OF AIRCRAFT CAN BE WELDED
SATISFACTORILY? (19133) REF.: AC 65-15A, PAGE 259.- AALL METALLICS MEMBERS.
- BONLY IRON ALLOY MEMBERS.
- CONLY STAINLESS STEEL MEMBERS.
- DONLY ALUMINUM ALLOY MEMBERS.
24WHAT TYPE OF FABRIC OR CLOTH ARE USED IN THE MANUFACTURE
OF AIRCRAFT COVERING? (18845) REF.: AC 65-15A, PAGE 85.- ADOMESTIC OR IMPORTED FIBERS
- BNATURAL AND ARTIFICIAL FIBERS.
- CORGANIC AND SYNTHETIC FIBERS.
- DGLUED OR SEWING FIBERS
25WHAT DOES AN ORIGINAL SURFACE TREAMENT FOR STEEL PARTS
ALSO INCLUDE TO REMOVE ALL TRACES OF DIRT, OIL, GREASE,
OXIDES, AND MOISTURE? (18790) REF.: FAA-H-8083-30, PAGE 6-17.- AALSO INCLUDES A WEAR RESISTANCE PROCEDURE.
- BIT INCLUDES AN ORIGINAL SURFACE TREATMENT.
- CUSUALLY INCLUDES A CLEANING TREATMENT.
- DALSO INCLUDES A PARTS REMOVAL.
26WHAT TYPE OF DEFECT WILL THE PENETRANT INSPECTION
DETECT? (18821) REF.: FAA-H-8083-30, PAGE 8-19.- AWILL DETECT SURFACE CRACKS OR POROSITY DEFECT.
- BWILL DETECT UNDER-SURFACE CRACKS OR VOIDS DEFECT.
- CWILL DETECT ELECTRICAL DISCONTINUITY OR FLAWS.
- DWILL DETECT INVISIBLE CRACKS OR SPOT POINTS.
27HOW ARE NEUMATIC SYSTEMS PROTECTED AGAINST DIRT? (19267)
REF.: AC 65-15A, PAGE 335.- A- BY MEANS OF VARIOUS TYPES OF VALVES
- BBY MEANS OF VARIOUS TYPES OF FILTERS.
- CBY MEANS OF VARIOUS TYPES OF PACKING AND O-RINGS.
- DBY MEANS OF VARIOUS TYPES OF LIQUIDS.
28HOW IS POTENTIAL ENERGY DEFINED? (18655) REF.: FAA-H-8083-30,
PAGE 3-3.- AENERGY THAT IS POWERFUL.
- BENERGY THAT HAS HIGH POWER.
- CENERGY THAT IS IN MOTION OR ENERGY THAT IS READY TO BE
USED. - DENERGY THAT IS AT REST OR ENERGY THAT IS STORED.
29HOW IS CALLED THE AMOUNT OF FORCE ACTING ON A SPECIFIC
AMOUNT OF SURFACE AREA? (18698) REF.: FAA-H-8083-30, PAGE 3-
24.- APOWER.
- BPRESSURE
- CFORCE.
- DQUANTITY.
30HOW MUCH VARIES THE PROPELLER EFFICIENCY? (19309) REF.: AC
65-12A, PAGE 325.- AIT DEPENDS OF ENGINE POWER.
- BFROM 25% TO 50%.
- CFROM 75% TO 99%
- DFROM 50% TO 87%.
31WHAT DOES PROPELLER EFICIENCY DEPEND ON? (20001) REF.: AC
65-12A, PAGE 325.- A- HOW MUCH THE PROPELLER SLIPS.
- BTHE CHORD LINE OF PROPELLER.
- CTHE PROPELLER LENGTH.
- DTHE NUMBERS OF BLADES.
32WHAT ARE THE ANCIENT ENEMIES OF AIR TRANSPORTATION?
(19134) REF.: AC 65-15A, PAGE 285.- ATHE FOG, CLOUD AND LIGHTNING.
- BTHE METAL COST AND PROTECTION.
- CTHE FUEL PRICE AND THE NOISE.
- DTHE RAIN, SNOW AND ICE.
33FROM WHAT METAL ARE REAMERS MADE? (18864) REF.: FAA-H-8083-
30, PAGE 9-13.- ATHEY ARE MADE FROM EITHER VANADIUM TOOL STEEL OR HIGHPOWER
STEEL. - BTHEY ARE MADE FROM EITHER CARBON TOOL STEEL OR HIGHSPEED
STEEL. - C- THEY ARE MADE FROM HARD TEMPERED STEEL.
- DTHEY ARE MADE FROM EITHER CROMO NIQUEL VANADIUM
STEEL OR LOW-SPEED STEEL.
- ATHEY ARE MADE FROM EITHER VANADIUM TOOL STEEL OR HIGHPOWER
34WHEN IS RELATIVELY LITTLE CORROSION TROUBLE EXPERIENCED
WITH MAGNESIUM SKINS? (18783) REF.: FAA-H-8083-30, PAGE 6-9.- AWHEN THE CORROSION IS ABSENT FROM THE SURFACE AND
INSULATION IS ADEQUATELY MAINTAINED. - BWHEN THE SURFACE FINISH HAS ZINC CHROMATE AND
INSULATION IS ADEQUATELY COVERED. - CWHEN THE REWORKED SURFACE FINISH AND INSULATION ARE
ADEQUATELY MAINTAINED - DWHEN THE ORIGINAL SURFACE FINISH AND INSULATION ARE
ADEQUATELY MAINTAINED.
- AWHEN THE CORROSION IS ABSENT FROM THE SURFACE AND
35WHEN IS RELATIVELY LITTLE CORROSION TROUBLE EXPERIENCED
WITH MAGNESIUM SKINS? (18783) REF.: FAA-H-8083-30, PAGE 6-9.- A- WHEN THE CORROSION IS ABSENT FROM THE SURFACE AND
INSULATION IS ADEQUATELY MAINTAINED. - BWHEN THE SURFACE FINISH HAS ZINC CHROMATE AND
INSULATION IS ADEQUATELY COVERED. - C- WHEN THE REWORKED SURFACE FINISH AND INSULATION ARE
ADEQUATELY MAINTAINED. - DWHEN THE ORIGINAL SURFACE FINISH AND INSULATION ARE
ADEQUATELY MAINTAINED.
- A- WHEN THE CORROSION IS ABSENT FROM THE SURFACE AND
36WHY ARE RELIEF VALVES USED IN PNEUMATIC SYSTEMS? (19266)
REF.:AC 65-15A, PAGE 334.- ATO PREVENT DAMAGE.
- BTO PROTECT THEE O-RINGS.
- CTO RELIEF PRESSURE.
- DTO MAINTAIN PRESSURE IN LIMITS.
37WHAT IS A TYPICAL ALUMINUM CORROSION TREATMENT? (18786)
REF.: FAA-H-8083-30, PAGE 6-14.- AREMOVE HYDRAULIC, SKIDROL, OIL AND SURFACE DIRT FROM
THE ALUMINUM SURFACE USING ANY CAUSTIC SUITABLE MILD
CLEANER. - BREMOVE OLD PAINT, CORROSION, OIL AND SURFACE WASTE
FROM THE ALUMINUM SURFACE USING ANY SUITABLE MILD
CLEANER. - CREMOVE OIL AND SURFACE DIRT FROM THE ALUMINUM
SURFACE USING ANY SUITABLE MILD CLEANER. - DREMOVE OIL, GREASE AND SURFACE DIRT FROM THE ALUMINUM
SURFACE USING ANY SUITABLE MILD CLEANER OR SOAP.
- AREMOVE HYDRAULIC, SKIDROL, OIL AND SURFACE DIRT FROM
38WHERE IS THE EXCEPTION IN THE USE OF ROUNDHEAD RIVETS IN
THE INTERIOR OF THE AIRCRAFT? (18749) REF.: FAA-H-8083-30,
PAGE 5-59.- AWHERE CLEARANCE IS REQUIRED FOR ADJACENT MEMBERS.
- BWHERE EXTRA STRENGTH IS REQUIRED.
- CWHERE TOLERANCE IS REQUIRED FOR MAIN MEMBERS.
- DWHERE PASSENGER SEATS ARE CLOSE TO THE WINDOW.
39WHAT OPERATION OF MODERN AIRCRAFT IS DEPENDENT UPON
THE USE OF INSTRUMENTS? (18804) REF.: AC 65-15A, PAGE 469.- ATHE FLIGHT OPERATIONAL SAFETY, ECONOMICAL ARRIVAL AND
RELIABLE GROUND OPERATION. - BTHE ON-TIME DISPATCH, ECONOMICAL AND RELIABLE
OPERATION. - CTHE MAINTENANCE WORK, FLIGHT SAFETY AND RELIABLE
OPERATION. - DTHE SAFE, ECONOMICAL AND RELIABLE OPERATION.
- ATHE FLIGHT OPERATIONAL SAFETY, ECONOMICAL ARRIVAL AND
40WHAT ARE THE MOST COMMONLY USED THREADED FASTENING
DEVICES ON AIRCRAFT? (18763) REF.: FAA-H-8083-30, PAGE 5-70.- ATHE BOLTS.
- BTHE SCREWS.
- CTHE FORKS.
- DTHE STUD BOLTS.
41WHAT IS THE OBJECT OF SEALS IN THE AIRPLANES HYDRAULIC
SYSTEM? (18746) REF.: FAA-H-8083-30, PAGE 5-36.- ATO PREVENT FLUID FROM BEING CONTAMINATED.
- B- TO PREVENT FLUID FROM PASSING A CERTAIN POINT.
- CTO RE-USE THE LIQUIDS MANY TIMES
- D- TO AVOID LOSS OF LIQUID AND TO CANCEL THE FLIGHT.
42WHAT PROCEDURES MUST BE OBSERVED WHEN SELECTING A SAW
BLADE? (18861) REF.: FAA-H-8083-30, PAGE 9-9.- A- CHECK THE MATERIAL THAT YOU HAVE TO CUT.
- B- SELECT AN APPROPRIATE SAW BLADE.
- CCHECK THE WEATHER.
- DCHECK THE ELECTRICAL GENERATOR.
43WHAT OTHER USE CAN BE GIVEN TO SEVERAL MATERIALS USED
FOR THINNING, SPECIFIC PAINTS AND LACQUERS? (19122) REF.: AC
65-15A, PAGE 113.- ATHEY ARE ALSO AVAILABLE FOR SOLVENT CLEANING.
- BTHEY ARE ALSO AVAILABLE FOR PAINT REMOVER AND
CORROSION CONTROL. - C- THEY ARE ALSO AVAILABLE FOR PAINT FINISHING.
- DTHEY ARE ALSO AVAILABLE TO JOIN COMPOSITES.
44WHAT ARE PERMITED TO REPAIR FABRIC-COVERED SURFACES?
(18852) REF.: AC 65-15A, PAGE 99.- AONLY SEWN REPAIRS ARE PERMITED.
- BSEWN AND UNSEWN REPAIRS ARE PERMITED.
- CONLY UNSEWN REPAIRS ARE PERMITED.
- DTHE REPAIR DEPEND THE LONG DAMAGE.
45WHICH ARE THE INCREMENTS OF RIVETS SHANK DIAMETERS?
(18760) REF.: FAA-H-8083-30, PAGE 5-64.- A1/54-INCH.
- B1/16-INCH
- C- 1/32-INCH.
- D1/64-INCH.
46IN WHAT FORMS AND SHAPES ARE STEEL AND STEEL ALLOYS
MANUFACTURED? (18730) REF.: FAA-H-8083-30, PAGE 5-2.- A- ROLLER BARS, WELDING SHEETS, FLIXIBLE TUBING, FORGINGS
AND CASTINGS. - BTHIN, THICK, MEDIUM, SMALL SIZE AND BIG SIZE.
- CBARS, SHEETS, TUBING, EXTRUSIONS, FORGINGS AND
CASTINGS. - DCOOL, WARM, HOT, ICED, FROZEN AND REFRIGERATE.
- A- ROLLER BARS, WELDING SHEETS, FLIXIBLE TUBING, FORGINGS
47WHICH ARE THE MOST WIDELY USED SEMICONDUCTOR
MATERIALS? (18976) REF.: FAA-H-8083-30, PAGE 10-3.- AGLASS, CERAMIC AND PLASTICS.
- BSILICON AND GERMANIUM.
- CGOLD, COPPER AND SILVER.
- DMATERIAL WITH FREE ELECTRONS.
48WHICH IS THE PROPERTY OF SILICONE RUBBERS? (18745) FAA-H-
8083-30, PAGE 5-35.- A- HAVE EXCELLENT HEAT STABILITY.
- BREACTS FAVORABLY WITH AROMATIC GASOLINES.
- CIS VERY EASE TO WORK.
- D- RESISTS THE STRIKES VERY WELL .
49IF SOME AIRCRAFT ARE NOT WEIGHED WITH THE WHEELS ON THE
SCALES, WHERE ARE THEY WEIGHED? (18723) REF.: FAA-H-8083-30,
PAGE 4-16.- AAT THE JACKING POINTS OR AT SPECIAL WEIGHED POINTS.
- BAT THE WHEELS POINTS OR AT SPECIAL WEIGHED POINTS.
- CAT THE JACKING POINT OR AT SPECIAL WEIGHED POINT.
- DAT THE NOSE AND TAIL POINTS OR AT SPECIFIC WEIGHED
POINTS.
50SOME AIRCRAFT ARE REQUIRED TO BE WEIGHED AND HAVE THEIR
CENTER OF GRAVITY CALCULATED ON A PERIODIC BASIS,
TYPICALLY HOW OFTEN IS THIS? (18713) REF.: FAA-H-8083-30, PAGE
4-2.- A- EVERY FIVE YEARS.
- BEVERY THREE YEARS
- CALMOST EVERY MONTH.
- DWHEN THE OWNER WANTS.
Informações
- Descrição
- ACTUALIZACIÓN 2012
- Autor
- erick garcia
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