TEST BORRADO, QUIZÁS LE INTERESE:
AGK1 PILOTO PRIVADO
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AGK1 PILOTO PRIVADO Descripción: TEST AVIACIÓN Autor:
Fecha de Creación: 26/09/2023 Categoría: Otros Número Preguntas: 25 |
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During a descent a blocked pitot pressure supply line causes the ASI to: over-indicate under-indicate over-indicate then under-indicate be unaffected. Detonation occurs in a reciprocating aircraft engine when the spark plugs are fouled or shorted out or the wiring is defective. the unburned charge in the cylinders explodes instead of burning normally. hot spots in the combustion chamber ignite the fuel/air mixture in advance of normal ignition. A DGI in an aircraft is updated to the magnetic compass immediately before a turn is made. During the turn, the: DGI is more accurate than the magnetic compass. DGI is the more accurate in the northern hemisphere but the magnetic compass is more accurate in the southern hemisphere. Magnetic compass is more accurate than the DGI. DGI and magnetic compass are equally accurate. What does the octane rating indicate? The fuel resistance to vapour locking. The fuel resistance to pre ignition. The fuel resistance to waxing. The fuel resistance to detonation. A positive ammeter indication means that: The battery's discharge rate. The generator is charging the battery The battery is out of service. The generator is failing. An aircraft flies at 35 000 ft, OAT = -45°C, RAS = 270 kt. The TAS will be: 480 kt. 470 kt. 484 kt. 466 kt. If the grade of fuel used in an aircraft engine is lower than specified for the engine, it will most likely cause: preignition lower cylinder head temperatures. a mixture of fuel and air that is not uniform in all cylinders. detonation. Connecting two 12 volt, 20 ampere-hour, capacity batteries in parallel will provide a battery of: 12 volts and 40 ampere-hours capacity. 12 volts and 20 ampere-hours capacity. 24 volts and 20 ampere-hours capacity. 24 volts and 40 ampere-hours capacity. Complete the following sentence by choosing the most correct of the four options to make an accurate statement. In a dry sump lubricating system: a separate oil storage tank is not required. oil pressure gauges are unnecessary. a scavenge pump returns the oil from the sump to a separate oil storage tank. the oil is stored in the sump itself. . Manual flight controls that allow the pilot to feel the air load on the control surface as it being moved are referred to as Reversible primary flight controls. Electro static primary flight controls. Hydro static primary flight controls. Irreversible primary flight controls. A cowling fitted to an air-cooled aircraft engine is to: Form an protective envelope around the engine and to retain heat. Duct air around the cylinders to cool the evenly and to increase drag. Duct air around the cylinders to cool the evenly and to reduce drag. Duct air around the cylinders to heat them evenly and to reduce drag. AVGAS 100LL is: Coloured blue and has the same octane rating as 100L. Coloured green and has the same resistance to detonation as 100L. Coloured green and has a higher octane rating than 100L. Coloured green and contains less lead than 100L. The most common type of wing structure for a modern jet transport aircraft is A multi-spar torsion box cantilever design. A single spar semi-monocoque design. A single spar monocoque design. A multi-spar torsion box strut braced design. Applying carburetor heat will: not affect the fuel/air mixture. result in more air going through the carburetor. increases power of the engine. enrich the fuel/air mixture. During flight you suspect that the static line may be blocked and elect to use the alternate static source. When compared to the main static source, alternate static pressure is: Higher. Either higher or lower depending on the ambient pressure. The same. Lower. A Direction Indicator (Dl) may be aligned with the magnetic compass: to eliminate the effect of liquid swirl. when the wings are level and the aircraft is in either accelerated or un-accelerated flight. by using the caging knob to rotate the Dl azimuth card when the aircraft's wings are level and the aircraft is in un-accelerated flight. periodically, to offset the effect of acceleration during a turn. If there are metallic objects close to an aircraft's magnetic compass: They should have no effect on compass indications. They will have a significant effect on magnetic variation. They will cause errors in the indications of the compass. The Direction Indicator will not be able to be synchronized with the compass. If a magneto switch fails to close the circuit what will be the result? The engine will not start. The magneto will be permanently live even if that magneto's switch is not on. During magneto checks the engine will cut when the other magneto is selected off. During magneto checks the RPM will not decrease when the other magneto is selected off. In a low wing monoplane with the fuel tanks in the wing what is the safeguard against fuel starvation should the engine driven pump fail? The use of an emergency hand pump. The presence of the accelerator pump in the carburettor. The presence of the electric fuel pump. The principle of Gravity Feed. Excessively high engine temperatures will cause damage to heat-conducting hoses and warping of the cylinder cooling fins. cause loss of power, excessive oil consumption, and possible permanent internal engine damage. not appreciably affect an aircraft engine. A propeller blade is twisted from root to tip: because the local angle of attack of the segment is dependent on segment movement in the plane of rotation and the aircraft true air speed. to provide maximum thrust at the root. because the local angle of attack of the segment is dependent on segment movement in the plane of rotation and the segment velocity. to provide maximum thrust at the tip. . If the engine gets too hot, the mixture may ignite before the spark plug fires: The mixture should be weakened to assist in cooling the engine. The throttle should be opened to assist in cooling the engine. This is called detonation. This is called pre-ignition. An aircraft flies at 25 000 ft, OAT = -38°C, RAS = 270 kt. The TAS will be: 396 kt. 405 kt. 184 kt. 389 kt. If an altimeter setting is not available before flight, to which altitude should the pilot adjust the altimeter? The elevation of the departure area. Pressure altitude corrected for nonstandard temperature. The elevation of the nearest airport corrected to mean sea level. A double pole electrical system; is not required in aircraft which are made of non-conductive materials. has the return current flowing back through the metal of the airframe to complete the circuit. is fail-safe, and so does not require a battery. requires one cable taking the current to the component and another to complete the circuit back to the negative side of the generator or alternator. |
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