Test
INGLES 2 DGAC (DE LA 50 A LA 90)
Preguntas del test (40)
1WHAT VERY LIGHT COLOR MAY APPEAR IN SOME STAINLESS STEEL
ALLOYS METAL TEST? (18732) REF.: FAA-H-8083-30, PAGE 5-5.- A- PINK.
- BWHITE
- CBLACK.
- DBROWN.
2WHAT HAPPENS WITH SOME TYPES OF EXTINGUISHING AGENTS?
(19294) REF.: AC 65-15A, PAGE 427.- ARAPIDLY CORRODE ALUMINUM ALLOY AND OTHER METAL.
- BSLOWLY CORRODE ALUMINUM ALLOY AND OTHER METAL.
- CARE HARDENER TO ALUMINUM ALLOY AND OTHER METAL.
- DLEAVE THE ALUMINUM ALLOY VERY BRIGHT.
3FROM WHAT ALLOYS ARE SOME WING PANELS FABRICATED?
(18734) REF.: FAA-H-8083-30, PAGE 5-9.- AFROM COPPER ALLOYS.
- BFROM IRON ALLOYS
- CFROM MAGNESIUM ALLOYS.
- DFROM TITANIUM ALLOYS.
4HOW IS CALLED THE TENDENCY OF AN OBJECT TO REMAIN
STATIONARY WHEN SUPPORTED FROM ITS OWN CENTER OF
GRAVITY? (18690) REF.: AC 65-15A, PAGE 82.- ADYNAMIC BALANCE.
- BSTATIC BALANCE.
- CTRIM TABS BALANCE
- DBALANCED CONDITION
5WHAT PROPELLER BLADES HAVE MORE RESISTANCE TO
ABRASION? (18796) REF.: FAA-H-8083-30, PAGE 6-23.- A- THE STEEL PROPELLER BLADES.
- BTHE ALUMINUM ALLOY PROPELLER BLADES.
- C- THE PURE ALUMINUM PROPELLER BLADES.
- DTHE MAGNESIUM ALUMINUM ALLOY PROPELLER BLADES.
6WHICH MAY BE THE PRINCIPAL REQUIREMENT IN CERTAIN
STRUCTURES? (19275) REF.: AC 65-15A, PAGE 1.- A- THE DURABILITY.
- B- THE STRENGTH.
- CTHE AIRWORTHINESS.
- DTHE STRESSES.
7WHY DOES STRESS CORROSION OCCUR? (18775) REF.: FAA-H-8083-
30, PAGE 6-6.- ASTRESS CORROSION NEVER OCCURS.
- BSTRESS CORROSION OCCURS AS THE RESULT OF MAINTAINING
THE AIRPLANE DIRTY AND IN A DRY ENVIRONMENT. - CSTRESS CORROSION OCCURS AS THE RESULT OF KEEPING THE
AIRPLANE OUT OF THE HANGAR. - DSTRESS CORROSION OCCURS AS THE RESULT OF THE
COMBINED EFFECT OF SUSTAINED TENSILE STRESSES AND
CORROSIVE ENVIRONMENT.
8HOW MAY THE STRESSED SKIN PANELS BE? (18825) REF.: AC 65-
15A, PAGE 24.- ATHEY MAY BE EITHER SMOOTH OR BEADED.
- BTHEY MAY BE STRESSED RESISTANCE OR LITTLE SMOOTH.
- CTHEY MAY BE ROUND OR SQUARE
- DALL THEM ARE OVAL.
9- AT WHAT SPEED IS SAFER TO TAKEOFF AND LAND? (18639) REF.:
FAA-H-8083-30, PAGE 4-1.- AIS SAFER TO TAKEOFF AND LAND AT LOWER AIRSPEEDS THAN
AT HIGHER SPEEDS. - BIS SAFER TO TAKEOFF AND LAND AT HIGHER AIRSPEEDS THAN
AT LOWER SPEEDS. - C- THE SAFEST TAKEOFF AND LANDING SPEED DEPEND ON PILOT'S
ABILITY. - DTHE SAFER TAKEOFF AND LANDING SPEEDS DEPEND ON THE
AIRPLANE MODEL.
- AIS SAFER TO TAKEOFF AND LAND AT LOWER AIRSPEEDS THAN
10WHICH IS A DOMINANT FACTOR THAT AFFECTS THE PHYSICAL
PROPERTIES OF FLUIDS? (18697) REF.: FAA-H-8083-30, PAGE 3-23.- ATHE TEMPERATURE.
- BTHE PRESSURE.
- CTHE DENSITY.
- DTHE ALTITUDE.
11WHAT DOES THE TENSION FORCE TRY TO DO? (18668) REF.: FAA-H-
8083-30, PAGE 3-14.- AIT TRIES TO COMPRES AN OBJECT.
- B- IT TRIES TO CRUSH AN OBJECT.
- C- IT TRIES TO PRESS AN OBJECT.
- D- IT TRIES TO PULL AN OBJECT APART.
12WHAT ARE THE ADJUSTABLE WRENCHS? (18858) REF.: FAA-H-8083-
30, PAGE 9-5.- ATHEY ALSO ARE OPEN-END WRENCHES
- BTHEY CAN REPLACE HANDY UTILITY TOOLS
- CTHEY ARE HANDY UTILITY TOOLS.
- D- THEY ARE MANUAL UTILITY TOOLS.
13HOW MANY BRAKES APPLICATIONS CAN BE MADE WITH THE AIR
BOTTLE THAT HAS NORMAL COMPRESSED AIR? (19268) REF.: AC 65-
15A, PAGE 336.- ASEVEN APPLICATION OF THE BRAKES.
- BONE APPLICATION UNTIL A COMPLETE AIRCRAFT STOP.
- CSEVERAL APPLICATIONS OF THE BRAKES.
- DTWO FULL BRAKES APPLICATION.
14WHAT IS THE PURPOSE OF DEVELOPING SPECIAL TOOLS AND
DEVICES? (19046) REF.: AC 65-15A, PAGE 133.- ATO HELP THE MECHANIC MAKE HIS HOME-WORK ON TIME,
COMPLEX AND UP TO DATE. - BTO HELP THE MECHANIC MAKE HIS JOB SWIFT, THE BEST AND
GOOD. - CTO HELP THE MECHANIC MAKE HIS WORK SOFT, RELAXED AND
QUICKLY. - DTO HELP THE MECHANIC MAKE HIS WORK FASTER, SIMPLER AND
BETTER.
- ATO HELP THE MECHANIC MAKE HIS HOME-WORK ON TIME,
15WHICH IS USUALLY THE MOST CONVENIENT LOCATION FOR
TEMPORARY BALLAST? (18644) REF.: FAA-H-8083-30, PAGE 4-23.- ATHE BAGGAGE COMPARTMENT.
- BTHE CABIN COMPARTMENT.
- CTHE TAIL COMPARTMENT.
- DTHE WING ROOT COMPARTMENT.
16HOW DO STRESSES USUALLY ACT? (19044) REF.: AC 65-15A, PAGE
132.- ATHEY ACT BREAKING THE PIECES THAN DO NOT HAVE RIGHT
TORQUE. - BTHEY ACT IN A HORIZONTAL MANNER.
- C- THEY ACT IN COMBINATION RATHER THAN SINGLY.
- DTHEY ACT SINGLY RATHER THAN IN COMBINATION.
- ATHEY ACT BREAKING THE PIECES THAN DO NOT HAVE RIGHT
17HOW IS CALLED THE BASIC BODY AND TAIL BOOM SECTIONS OF A
TYPICAL HELICOPTER? (18824) REF.: AC 65-15A, PAGE 24.- A- MONOCOQUE.
- BREINFORCED.
- CSTANDARD.
- DCONVENTIONAL.
18WHAT IS USED TO DESIGN THE BASIC COMPONENT OF A CABLE?
(18765) REF.: FAA-H-8083-30, PAGE 5-75.- ANUMBERS AND LETTERS.
- BTHE WIRE METAL.
- CTHE AMOUNT OF WIRES IN EACH STRAND AND THE QUANTITY
OF CABLES. - DTHE NUMBER OF STRANDS AND THE NUMBER OF WIRES IN EACH
STRAND.
19WHAT DOES THE BLADE FLAPPING ACTION CREATE IN A
HELICOPTER? (19023) REF.: AC 65-15A, PAGE 53.- ACREATES AN UNBALANCE CONDITION WITH RESULTING
VIBRATION. - B- CREATES A BIG LIFT CONDITION WITH RESULTING IN A SMOOTH
FLIGHT. - CCREATES SOME ADDITIONAL DRAG AND THE ENGINE HAS TO
DEVELOP MORE POWER. - DCREATES A BALANCE CONDITION WITH RESULTING IN LESS
VIBRATION.
- ACREATES AN UNBALANCE CONDITION WITH RESULTING
20WHAT 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. - BTHE QUANTITY OF THE AIR THAT IS IN THE CYLINDERS.
- CTHE TEMPERATURE OF THE AIR BEFORE IT ENTERS THE
CARBURATOR. - DTHE PRESSURE AND THE TEMPERATURE OF THE AIR AFTER IT
ENTERS THE CARBURATOR.
- A- INDICATE THE CYLINDERS TEMPERATURE AND THE AIR AROUND
21WHAT DOES THE CARBURETOR HAVE IN ORDER TO SHUT OFF THE
FUEL TO STOP THE ENGINE? (19107) REF.: AC 65-12A, PAGE 115.- AA FUEL INYECTION AND A MANUAL START SYSTEM.
- B- AN AUTOMATIC SELECTOR VALVE IN THE CARBURATOR
- CAN IDLE CUTOFF SYSTEM.
- DA FUEL CONTROL IN THE COCKPIT.
22HOW MAY BE CONSIDERED THE CENTER OF GRAVITY IN AN
AIRCRAFT? (19287) REF.: AC 65-15A, PAGE 33.- AAS A POINT AT WHICH THE BALANCE OF THE AIRCRAFT IS
OPTIMUM. - BAS A POINT AT WHICH ALL THE WEIGHT OF THE AIRCRAFT IS
CONCENTRATED. - CAS THE REAR AND FRONT POINT AT WHICH ALL THE WEIGHT OF
THE AIRCRAFT IS LIMITED. - DAS A PLACE WHERE ALL THE LOAD IN THE AIRCRAFT IS
CONCENTRATED.
- AAS A POINT AT WHICH THE BALANCE OF THE AIRCRAFT IS
23WHAT IS THE CENTER OF GRAVITY RANGE FOR AN AIRCRAFT?
(18724) REF.: FAA-H-8083-30, PAGE 4-17.- AIS THE AFT AND REAR BALANCE LIMITS.
- BIS THE LIMITS WITHIN WHICH THE AIRCRAFT MUST BALANCE.
- CARE ALL THE DISTANCES THAT ARE CONSIDERED DURING
WEIGHING. - DIS WHERE THE WEIGH IS CONCENTRATED.
24WHAT IS THE CHORD OF AN AIRFOIL OR WING SECTION? (19040)
REF.: AC 65-15A, PAGE 31.- AIS A ROPE USED TO TIE THE WING FROM THE LEADING EDGE TO
TRAILING EDGE. - BIS A STRAIGHT LINE WHICH CROSSES THE WING FROM THE
ROOT TO THE WING TIP. - CIS 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.
- AIS A ROPE USED TO TIE THE WING FROM THE LEADING EDGE TO
25HOW ARE THE CONTROL SURFACES OF SOME AIRCRAFT
COVERED? (19283) REF.: AC 65-15A, PAGE 18.- AARE COMPOSITE COVERED.
- BARE FABRIC COVERED.
- CARE FABRIC AND METAL COVERED.
- DARE PLASTIC, FABRIC, METAL AND COMPOSITE COVERED.
26WHAT TEMPERATURE WILL INDICATE THE CYLINDER HEAD
TEMPERATURE INDICATOR PRIOR TO OPERATE THE ENGINE?
(19307) REF.: AC 65-12A, PAGE 322.- AWILL INDICATE THE CYLINDER TEMPERATURE.
- B- WILL INDICATE THE FREE OUTSIDE AIR TEMPERATURE.
- CWILL INDICATE ANY FREE TEMPERATURE.
- DWILL INDICATE THE ENGINE GENERAL TEMPERATURE.
27IN 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.
- DINTO FOUR OR SIX SECTIONS.
28WHAT 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.
- CIS ITS COLOR AND WEIGHT PER UNIT OF VOLUME
- DIS ITS CHEMISTRY COMPOSITION AND PHYSICAL RESISTANCE.
29IN WHAT NUMERALS IS THE DIAL FACE OF THE TYPICAL ALTIMETER
GRADUATED? (19274) REF.: AC 65-15A, PAGE 476.- AIS GRADUATED WITH NUMERALS FROM ZERO TO NINE
INCLUSIVE. - BIS GRADUATED WITH NUMERALS, LETTERS AND SYMBOLS
INCLUSIVE. - CTHE GRADUATION DEPENDS ON THE AIRPLANE
MANUFACTURER. - DTHE GRADUATION DEPENDS ON THE INSTRUMENT
MANUFACTURER.
- AIS GRADUATED WITH NUMERALS FROM ZERO TO NINE
30WHERE IS LOCATED THE DISCHARGE NOZZLE IN A CARBURATOR?
(19109) REF.: AC 65-12A, PAGE 115.- ADIRECTLY IN THE MANIFOLD PRESSURE.
- BIN THE HIGH PRESSURE SIDE OF THE CARBURATOR.
- C- IN THE THROAT PRESSURE SIDE OF THE VENTURI.
- DIN THE THROAT OF THE VENTURI.
31WHAT DOES THE EMPTY WEIGHT OF AN AIRCRAFT INCLUDE?
(18717) REF.: FAA-H-8083-30, PAGE 4-4.- AINCLUDES 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. - DINCLUDES THE ENTIRE OPERATING EQUIPMENT THAT HAS A
FIXED OR MOVABLE LOCATION AND IS ACTUALLY INSTALLED IN THE
AIRCRAFT.
- AINCLUDES ALL OPERATING EQUIPMENT THAT HAS A FIXED
32IN WHAT CONSISTS THE ENVELOPE METHOD OF COVERING WING
WITH FABRIC? (18850) REF.: AC 65-15A, PAGE 93.- ACONSIST IN GLUEING FABRIC OVER THE METAL TO MAKE AN
ENVELOPE OR FOLD. - B- CONSIST IN EMBROIDERING COTTON TO MAKE AN ENVELOPE OR
SLEEVE - CCONSISTS IN GLUEING FABRIC TO MAKE AN ENVELOPE OR
SLEEVE. - DCONSISTS IN SEWING FABRIC TO MAKE AN ENVELOPE OR
SLEEVE.
- ACONSIST IN GLUEING FABRIC OVER THE METAL TO MAKE AN
33HOW DOES THE ENVIRONMENT AFFECT THE CONDITIONS UNDER
WHICH AN AIRCRAFT IS MAINTAINED AND OPERATED? (18776) REF.:
FAA-H-8083-30, PAGE 6-7.- ATHE ENVIRONMENT AFFECTS GREATLY THE CORROSION
CHARACTERISTICS. - B- THE ENVIRONMENT AFFECTS ONLY MINIMALLY THE CORROSION
CHARACTERISTICS. - CTHE ENVIRONMENT DOES NOT AFFECT THE CORROSION
CHARACTERISTICS. - D- THE SALT WATER AND NOT THE ENVIROMENT AFFECTS
GREATLY THE CORROSION CHARACTERISTICS.
- ATHE ENVIRONMENT AFFECTS GREATLY THE CORROSION
34WHAT IS THE TERMINATING COMPONENT OF THE BASIC ENGINE?
(19304) REF.: AC 65-12A, PAGE 59.- ATHE JET NOZZLE.
- B- THE TAILPIPE.
- C- THE EXHAUST CONE ASSEMBLY.
- DTHE THRUST REVERSE.
35WHAT 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.
- BIS TO KNOW ITS CHEMICAL COMPOSITION.
- C- IS TO KNOW THE OVEN TEMPERATURE.
- DIS TO KNOW THE COOLING PROCEDURE
36WHAT 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.
- BTHE COUNTERSUNK HEAD RIVET AND THE SOLID RIVET.
- CTHE FLATHEAD RIVET LIKE THE ROUNDHEAD RIVET
- DTHE BRAZIER HEAD RIVET AND THE UNIVERSAL HEAD RIVET.
37WHAT MUST BE KNOWN IN ORDER TO KNOW THE DENSITY OF A
SUBSTANCE? (18654) REF.: FAA-H-8083-30, PAGE 3-2.- AITS VOLUME AND COMPOSITION
- BITS BASIC ELEMENTS AND ATOMIC WEIGHT.
- C- ITS WEIGHT AND VOLUME.
- DITS COMPOSITION AND GRAVITY.
38WHAT MUST BE CAREFULLY DETERMINED IN ANY DAMAGED PART?
(19125) REF.: AC 65-15A, PAGE 130.- ATHE ADJACENT PART.
- BTHE FASTENER OF THE PART.
- CTHE ALLOY OF THE PART.
- DTHE FUNCTION OF THE PART.
39WHAT ARE THE FUNDAMENTAL LAWS GOVERNING THE ACTION OF
AIR ABOUT A WING? (19036) REF.: AC 65-15A, PAGE 30.- ATHE LAW OF VELOCITY AND SPEED.
- BTHE BERNOULLI'S PRINCIPLE.
- CTHE PASCAL'S LAW OF MOTION.
- DTHE NEWTON'S LAW OF MOTION.
40HOW IS CALLED THE GEAR WITH THE IMPUT FORCE? (18666) REF.:
FAA-H-8083-30, PAGE 3-11.- AIS CALLED THE MAIN GEAR.
- BIS CALLED THE DRIVE GEAR
- CIS CALLED THE DRIVEN GEAR.
- DIS CALLED THE FIRST CLASS GEAR.
Información
- Descripción
- ACTUALIZACION MARZO 2012
- Autor
- erick garcia
- Idioma
- Español
- Visitas
- 6
- Etiquetas
- Valoración
- Aún sin valoraciones Valora este test