TEST BORRADO, QUIZÁS LE INTERESE:
Engines "Another One Bites the Dust"
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Título del Test:
Engines "Another One Bites the Dust" Descripción: Test acerca de sapos para sapos Autor: Sapos OTROS TESTS DEL AUTOR Fecha de Creación: 26/03/2023 Categoría: Otros Número Preguntas: 10 |
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During EEC "SOFT" Alternate mode what happens with the engine? The ENG gives a greater thrust rating than the one the engine is designed to. EEC uses last valid flight conditions to define engine parameters. Engine relaxes and avoid any kind of unwanted commands to occur. When operating in "HARD" mode what can we expect? Maximum rated thrust is reached at a thrust lever position less than full forward. Both engines will double their fuel flow, therefore endurance will be reduced. Protections are degraded but still have some. The correct settings of idle operation are: Floor minimum idle, in-flight idle, Approach idle. Ground minimum idle, in-flight idle, Approach idle. Ground minimum idle, flight minimum idle, Approach idle. EEC automatically selects Approach Idle when: In flight flaps in landing configuration, 2.500ft RA or Wing anti-ice ON. In flight if flaps are in landing configuration o engine anti-ice ON for either engine. In flight if flaps grater than 10º, landing light ON and landing gear down and locked. Where does the EEC meters the fuel to meet thrust requirements? SPAR VALVE. ENGINE VALVE SENSORS. HMU (HYDRO-MECHANICAL UNIT). Fuel flow indications comes from the fuel that just passed the: After passing through the engine fuel shutoff valve. After passing the HMU. When fuel is taken from any fuel tank. The main function of the oil scavenge pumps is to recover oil from the engine bearings and accessory gearbox. True. False. Not stated in the FM of the B737. When we position the Engine Start Switch in the GRD position... Bleed from the APU enters the engine making it to turn very fast until N1 is at 56%. Engine start switch uses battery power to close the Engine Bleed Air Valve and opens the Start Valve to allow pressure to rotate the starter. None of the above is correct. A flame out can be detected when: Uncommanded rapid decrease in N2 occurs or N2 below idle RPM. Uncommanded rapid decrease in N1 occurs or N1 below idle RPM. Looking outside the window and there's a lot of smoke coming from the engine. Conditions for the use of thrust reversers are: When both thrust levers are left at idle at least 3 seconds after touch down. Either RA senses -10ft or when air/ground safety sensor is in ground mode. Either RA senses 10ft or when air/ground safety sensor is in ground mode. |
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