Test
ingles 2015 41-80
Preguntas del test (26)
1WHAT FORCES ACT ON AN AIRCRAFT, WHETHER IT IS ON THE
GROUND OR IN FLIGHT? (19042) REF.: AC 65-15A, PAGE 131.- ATHE FORCES ARE CUTING, PUSHING OR BENDING
- BTHE FORCES ARE PULLING, PUSHING OR TWISTING
- CTHE FORCES ARE WEIGHT, THRUST OR DRAG
- DTHE FORCES ARE LIFTING, PUSHING OR DOWNWARD
2HOW MUST THE MIXTURE BE IN ORDER FOR AN ENGINE TO
DEVELOP MAXIMUN POWER AT FULL THROTTLE? (19115) REF.: AC
65-12A, PAGE 121.- ATHE FUEL MIXTURE MAY BE RICHER THAN FOR CRUISE.
- BTHE FUEL MIXTURE IS THE SAME ALL THROUGH THE FLIGHT.
- CTHE FUEL MIXTURE MUST BE RICHER THAN FOR CRUISE.
- DTHE FUEL MIXTURE MUST BE LEANER THAN FOR CRUISE
3WHAT ARE THE FACTORS TO CONSIDER IN THE SELECTION OF
THE CORRECT RIVET FOR INSTALLATION? (18757) REF.: FAA-H-
8083-30, PAGE 5-61.- AINSTALLATION LOCATION, PROTECTION OF THE MATERIAL
BEING RIVETED, DIAMETERS OF THE MATERIAL BEING RIVETED
AND STRESS DESIRED - BINSTALLATION PLACE, COMPOSITION OF THE TOOLS BEING
USED, THINNESS OF THE MATERIAL BEING RIVETED AND
STRENGTH DESIRE. - CWORK LOCATION, ILUMINATION OF THE PLACE, COMPOSITION
OF THE MATERIAL BEING RIVETED, THICKNESS OF THE MATERIAL
BEING RIVETED AND QUALITY OF THE TOOLS. - DINSTALLATION LOCATION, COMPOSITION OF THE MATERIAL
BEING RIVETED, THICKNESS OF THE MATERIAL BEING RIVETED
AND STRENGTH DESIRED.
- AINSTALLATION LOCATION, PROTECTION OF THE MATERIAL
4WHAT IS THE ADVANTAGE OF EXTERNAL AIRCRAFT SURFACES
WITH REGARD TO INSPECTION AND MAINTENANCE? (18782) REF.:
FAA-H-8083-30, PAGE 6-9.- AIT HAS NO SPECIAL ADVANTAGES.
- BVERY EASY TO READ.
- CREADILY VISIBLE AND ACCESSIBLE.
- DDEPENDS ON THE AIRCRAFT TYPE.
5WHAT IS NEEDED IN ORDER TO PRODUCE EXTENSIVE PITTING
DAMAGE IN DISSIMILAR METAL PARTS? (18773) REF.: FAA-H-8083-
30, PAGE 6-4.- ATHE PRESENCE OF SALT.
- BTHE PRESENCE OF A CONDUCTOR.
- CTHE ABSENCE OF ZINC CHROMATE PRIMER.
- DBIG CHANGE IN TEMPERATURES.
6WHAT MAY HAPPEN IF THE PROPELLER BLADES HAVE CRACKS?
(18799) REF.: FAA-H-8083-30, PAGE 6-23.- AMAY NEED TO BE REWORKED.
- BMAY NEED TO BE REJECTED.
- CMAY TEND TO OXIDIZE.
- DMAY BE CUT.
7WHAT MUST EVERY PRINT HAVE? (18649) REF.: FAA-H-8083-30,
PAGE 2-4.- ATHE BEST INK.
- BSOME MEANS OF IDENTIFICATION.
- CSOME MEANS OF ISSUE.
- DA POOR PAPER.
8WHAT MUST ELEMENTS HAVE IN ORDER TO BE GOOD
CONDUCTORS? (18931) REF.: FAA-H-8083-30, PAGE 10-3.- AMANY FREE ELECTRONS.
- BVERY LOW WEIGHT
- CBE VERY SOFT.
- DBE VERY EXPENSIVE.
9WHAT IS REQUIRED FOR THE ELECTRONS TO STAY IN AN ORBIT?
(18930) REF.: FAA-H-8083-30, PAGE 10-2.- AA HIGH TEMPERATURE.
- BA CERTAIN AMOUNT OF ELECTRICITY.
- CA CERTAIN AMOUNT OF HEAT.
- DA CERTAIN AMOUNT OF ENERGY.
10WHAT ARE THE FORCES THAT ACT IN THE HELICOPTER DURING
FLIGHT? (18979) REF.: AC 65-15A, PAGE 49.- ALIFT, THRUST, WEIGHT AND DRAG.
- BCUT, TORSION, FORWARD AND AFT.
- CBENDING, COMPRESSION, SHEAR AND TORSION.
- DBACK, FORWARD, UP AND DOWN.
11WHAT IS THE LINK BETWEEN THE ENGINEERS WHO DESIGN AN
AIRCRAFT AND THE WORKERS WHO BUILD, MAINTAIN, AND
REPAIR IT? (18647) REF.: FAA-H-8083-30, PAGE 2-1.- ATHE HANGARS, TOOLS, TECHNICAL ORDERS AND LADDERS.
- BTHE HANGARS AND LADDERS.
- CTHE TOOLS AND TECHNICAL ORDERS.
- DTHE DRAWINGS AND PRINTS.
12WHAT MAY DAMAGE THE DRACON? (18848) REF.: AC 65-15A, PAGE
93.- ATHE EXCESSIVE WATER.
- BTHE EXCESSIVE HEAT.
- CTHE EXCESSIVE SUN.
- DTHE EXCESSIVE WIND.
13WHAT CREATES THE DISSYMMETRY OF LIFT IN AN HELICOPTER?
(18989) REF.: AC 65-15A, PAGE 51.- ATHE DIFFERENTIAL TORQUE BETWEEN TWO ROTORS.
- BTHE WIND DURING HOVERING OR VERTICAL FLIGHT.
- CTHE HORIZONTAL FLIGHT OR THE DIFFERENTIAL TILT.
- DTHE HORIZONTAL FLIGHT OR WIND DURING HOVERING.
14WHAT IS AN IMPORTANT CONSIDERATION WHEN CHOOSING
MATERIAL TO USE IN AIRPLANE PARTS? (18728) REF.: FAA-H-8083-
30, PAGE 5-1.- ATHE DENSITY OF MATERIALS.
- BTHE VOLUME OF MATERIALS.
- CTHE HARDNESS.
- DTHE STRENGTH
15WHAT SIDE HAVE TO BE DEBURRED DURING A TUBING FLARING
JOB? (18808) REF.: FAA-H-8083-30, PAGE 7-6.- ABOTH ENDS BY THE INSIDE AND THE OUTSIDE TUBING.
- BTHE OUTSIDE.
- CTHE INSIDE.
- DTHE INSIDE AND THE OUTSIDE.
16IN HOW MANY GROUP ARE DAMAGES CLASSIFIED? (19041) REF.:
AC 65-15A, PAGE 131.- AFROM SMALL DENTS TO HOLES.
- BFROM NEGLIGIBLE TO BIG DAMAGES.
- CINTO FOUR SPECIFIC GROUPS
- DINTO FOUR GENERAL GROUPS.
17WHENEVER POSSIBLE, HOW SHOULD DAMAGED TUBING AND
FLUID LINES BE REPAIRED? (18803) REF.: FAA-H-8083-30, PAGE 7-
2.- ASHOULD BE REPAIRED WITH GOOD PARTS.
- BSHOULD BE REPAIRED WITH BRIGHT PARTS.
- CSHOULD BE REPAIRED WITH NEW PARTS.
- DSHOULD BE REPAIRED WITH OVERHAULED PARTS.
18WHAT DOES A COMPRESSION FORCE TRY TO DO? (18670) REF.:
FAA-H-8083-30, PAGE 3-14.- AIT TRIES TO CRUSH AN OBJECT.
- BIT TRIES TO TWIST AN OBJECT.
- CIT TRIES TO SLICE OR TO CUT AN OBJECT.
- DT TRIES TO STRESS AN OBJECT.
19IN WHAT BODY PARTS OF THE BODY CAN COMPOSITE PRODUCTS
BE VERY HARMFUL? (18740) REF.: FAA-H-8083-30, PAGE 5-33.- AIN THE SKIN, EYES AND LUNGS.
- BIN THE HAND, FEET AND HAIR.
- CIN THE CHEST, ARMS AND FACE.
- DIN THE ELBOW, FINGERS AND NOSE.
20WHAT EFFECT CAN GREASE AND DIRT ACCUMULATION PRODUCE
ON THE AIR-COOLED ENGINE? (18794) REF.: FAA-H-8083-30, PAGE
6-23.- APRODUCE A COOLING EFFECT.
- BPRODUCE A REFRIGERATING EFFECT.
- CPRODUCE AN INSULATION EFFECT.
- DPRODUCE A WEIGHT INCREASE.
21WHY IS ZINC CHROMATE PRIMER APPLIED TO METALLIC
SURFACES? (18847) REF.: AC 65-15A, PAGE 115.- ABECAUSE THE COVERING IS CORROSION RESISTANT.
- BBECAUSE THE COVERING HAS A NICE COLOR.
- CBECAUSE IT PROTECTS IT FROM THE SUN.
- DBECAUSE THE COVERING IS ENAMEL OR LACQUER.
22WHICH ARE CORROSION RESISTANT METALS? (18731) REF.: FAAH-
8083-30, PAGE 5-4.- ANICKEL STEELS OR ALUMINUM METALS.
- BCHROME-VANADIUM OR CHROMIUM-IRON METALS.
- CALUMINUM OR COPPER METALS.
- DCHROME-NICKEL OR STAINLESS STEELS METALS.
23WHAT PRECAUTIONS MUST BE TAKEN WHEN CLEANING
ASSEMBLED AIRCRAFT WITH CHEMICAL CLEANERS? (18801) REF.:
FAA-H-8083-30, PAGE 6-25.- ATHEY MUST BE USED WITH GREAT CARE.
- BTHEY MUST BE USED IN OPEN PLACES.
- CTHEY MUST NOT BE USED WITH SUN LIGHT.
- DTHEY MUST BE USED WITH MASK AND SPECIAL WORK CLOTH.
24WHAT IS THE COMMON NAME FOR THE CORROSION BETWEEN
DIFFERENT METALS? (18789) REF.: FAA-H-8083-30, PAGE 6-16.- AELECTROLYTIC OR DISSIMILAR METALS CORROSION.
- BINTERGRANULAR OR DISSIMILAR METALS CORROSION.
- CCHEMICAL OR DISSIMILAR METALS CORROSION.
- DSPOT WELDING OR SIMILAR METALS CORROSION.
25WHAT DO YOU HAVE TO CHECK BEFORE USING THE GRINDER?
(19128) REF.: AC 65-15A, PAGE 141.- ATHE BENCH GRINDER.
- BTHE ABRASIVE GRAIN.
- CTHE WHEEL FOR CRACKS.
- DTHE ELECTRICAL POWER.
26WHAT TYPE OF ENERGY IS VELOCITY OF THE AIR? (18702) REF.:
FAA-H-8083-30, PAGE 3-32.- APOTENTIAL ENERGY.
- BKINETIC ENERGY.
- CWORK ENERGY.
- DSTATIC ENERGY.
Información
- Descripción
- Test en ingles 2015 41-80, creado por erick garcia en 24/01/2018.
- Autor
- erick garcia
- Idioma
- Español
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