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COMENTARIOS ESTADÍSTICAS RÉCORDS
REALIZAR TEST
Título del Test:
Ingles

Descripción:
Dick Traicy

Fecha de Creación: 2025/07/16

Categoría: Idiomas

Número Preguntas: 87

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Can I park the Genie telescopic boom lift here?. It's the same place. Sorry, I did that. Only for haft an hour.

If the windows pane_broken, the cabin mechanics_ it. Was - would replaced. Were not - not would replaced. Is - must to replace.

The ground strap is... Riveted to the bolt. Attached to the bolt. Built in the bolt.

If a false caution/warning is determined... Aircraft crew must check the system/components condition. Aircraft dispatch is not allowed. Aircraft dispatch is allowed.

Aircraft dispatch conditions are considered to be normal. If either the sliding window or the fixed window heating is faulty. The failure is shown amber on the EWD. On the EWD, the failure will appear amber when both sliding and fixed windows heating is faulty. On the EWD, the failure will appear amber when one window heating is faulty.

These are engine (foto de motor palas). IDGs. Vanes. Blades.

Next generation aircraft will demand ___ 4 times more power than today. Up to. For. Until.

video: In the begining of the video the passenger was upset for missing his flight connection to attend.... His daughter's wedding. A medical appointment. A business Meeting.

This is (foto de avión con deslizador extendido). A floate. A slide. A raft.

Would you mind_these screens a wipe before installing them?. Gived. To giving. Giving. Gave.

If the elevators__ the nose__. Goes down - Goes down. Go down - goes down. Will go down - go down.

Choose the correct alternative. The surface was cutted in accordance with EO. The surface was cut in accordance with EO. The surface was cuted in according to the EO.

the air fan modulating valve opens and closes in response to pressure signals from the air temperature sensor. El aire del fan está modulando la válvula para que se abra y cierre en respuesta a las señales de presión desde el sensor de temperatura del aire del fan. La válvula moduladora del aire del fan se abre y cierra en respuesta a las señales de presión desde el sensor de temperatura del aire del fan.

Once the plane is in the air, you can your seat belts ir you wish. Unfasten. Unlock. Untie. Undress.

The APU page appears during the APU start sequence and it will be replaced by the DOOR/OXY page 10 seconds after de APU start sequence. The engine page appears during the engine start sequence and it will replaced by the WHEEL page after the engine start sequence. La página de APU aparece durante la secuencia de la partida del APU y será reemplazada por la página de DOOR/OXY 10 segundos después de la secuencia de la partida del APU. La página de ENG aparece durante la secuencia de partida del motor y será reemplazada por la página de WHEEL después de la secuencia de partida del motor. La página de APU aparece durante la partida de la secuencia de la APU y reemplazará la página de DOOR/OXY 10 segundos después de la partida de la secuencia de la APU la página de ENG aparece durante la partida de la secuencia del motor y reemplaza la página de WHEEL después del inicio de la secuencia del motor.

The passengers Walker over it (foto de pasillo de pasajeros). Sidewalk panel. Floor carpet. Arm rest.

The hydraulic braking operation is identical for automatic braking, manual braking and inflight braking. Note that during inflight braking, anti-skid function is inhibited by the BSCU. Normal braking and anti-skid regulation are electrically controlled by the Braking and Steering Control Unit. The BSCU controls normal braking hydraulically. The BSCU controls normal braking electrically. The BSCU inhibits inflight braking.

figure: Packing position is distribution valve strainer and the adapter. In front of. Between. Among.

The engine fuel-feed system distributes fuel to the main engines (AMM 28-22-00-001) and the APU (AMM 28- 25-00/001). El sistema de alimentación de combustible del motor distribuye combustible a los motores principales (AMM 28-22-00-001) y a la APU (AMM 28-25-00/001). El combustible del motor que alimenta el sistema distribuye combustible a los motores principales (AMM 28-22-00-001) y a la APU (AMM 28-25-00/001).

The air conditioning system control cabin. Provides. Did not provided. Does not provided.

Choose the correct alternative. The wires were splitted according to figure 1. The wires were split according to figure 1. The wires were splited according to figure 1.

When I realised o has dropped a magnetic tip of my screwdriver, | decided to__my steps. Retrace. Return. Regress. Resume.

Choose the correct alternative. The engine indications were seted to normal configurations. The engine indications were setted to normal configuration. The engine indications were set to normal Configuration.

These are (foto de tornillos con tuerca). Bolts. Rivets. Pins.

Electronic flight instrument system (EFIS) control panel. Instrumentos electrónicos del sistema de vuelo del panel de control. Panel de control electrónico de los instrumentos de vuelo del sistema. Panel de control del sistema electrónico de instrumentos de vuelo.

Choose the correct alternative. Prior the engine operation, make sure that the area is clear. Prior to the engine operation, making sure that the area Is clear. Prior to the engine operation, to make sure that the area is clear.

The bigger logo is on (foto de avión Latam). Elevator. Winglets. Rudder.

The plug furnishes the EEC with information identifying engine basic thrust rating. The EEC will set the engine basic thrust rating. The EEC is fed with information by the plug. The plug is provided wuth information by the EEC.

Choose the correct alternative. The toilet seat was removed according to the procedure. The toilet seat were removed according to the procedure. The toilet seat was removed in according with the procedure.

It wasn't a bad crash and damage was done to the fork lift. Light. Mere. Little. Small.

I was looking forward _engine 2 for test, but the whole operation was cancelled. Running. To run. To have fun. To running.

False cautions/warnings can be determined by... Troubleshooting. MEL section 01. Abnormal/Emergency Procedure. ATA Chapter of section 01.

Dual precision resolvers sense thrust lever position and provide electrically isolated inputs. Thrust lever position is detected by dual precision resolvers. Electrically isolated inputs are sensed by dual precision resolvers. Thrust lever position is provided by dual precision resolvers.

When a caution/warning and "not applicable" dispatch condition column apperar together. MEL in not to be consulted. MEL item number is the MEL entry point. MEL is to be consulted. Aircraft dispatch is allowed.

An intelligent smart grid will be used to optimize... Electrical power supply and demand. Fuel cell and batteries. Auxiliary and emergency power.

GE expects to look after the aircraft's. Delay. Health and performance. Unscheduled maintenance.

This image shows... Flap. Slat. Rudder.

This image shows. RAT. MLG. NLG.

THIS IMAGE SHOWS. Ecam. Flight attendants panel. The heads up display.

This image shows... VHF Antenna. Ram Air Turbine. Pitot tube.

This image shows. Rivets. Washer. Bolts.

The technician ended the rigging her torque wrench. With. In. As. By.

When ALL the landing gear is up and locked, the LGIU signals the doors to close while maintaining landing gear UP signal to keep the "raise" line pressurized. Door uplock proximity detectors signal the LGCIU that the doors are uplocked. As soon as the last door closes and locks, the LGCIU cancels the landing gear " raise" signal and maintains the door close signaal as long as the safety valve is open (LGCIU, Landing gear control interface unit). The LGCIU cancel the landing gear "raise" signal after the last door closes and locks. The LGIU cancel the landing gear " raise" signal when the safety valve is open. The LGIU cancel the landing gear " raise" signal when the landing gear is up.

Have you got time to discuss your work now or are you __ to leave?. Thinking. Planned. About.

She came to work as a supervisor here __a month ago. Almost. Beyond. Quite.

I left my last job because I had no ___ to travel. Place. Position. Opportunity.

I'd rather you ___ to her why we can't deliver this task on time. Would explain. Explained. To explain.

Before making a decision, the leader considered all ___ of the argument. Sides. Features. Shades.

This new printer is recommended as being_reliable. Greatly. Highly. Strongly.

This loud noise is somewhere in the ___ . of the north airport facilities. Quarter. Vicinity. District.

The new towbarless tractor is a ___ vehicle. It runs ___. Fast-fastly. Fastly-fast. Fast_fast.

Shall we go to the gym after work?. I'm too tired. It’s very good. Not at all.

His eyes were __ bad that he couldn't read the part number. Too. So. Very.

The company needs to decide ___ and for all what its Safety Policy is on this issue. Once. First. Finally.

Don't put the lubricant bottle on the ___ of the bench. someone will knock it off. -. Outside. Boundary. Edge.

I'm sorry - I didn't ___to distract you. Hope. Think. Mean.

_____ tired Melissa is when she gets home from the airport, she always makes time to change clothes before entering the house. No matter how. However much. Although.

It was only ten days ago ___ she started her new job at the warehouse. Then. That. After.

The wheel shop didn't have the spacers I required, but they've ____ some with AOG priority. Booked. Ordered. Commanded.

I can't understand this Engineering Order. Would you like some help?. Don't you know?. I suppose you can.

What slide will you install first?. I hope it was right. We can't decide. It wasn't very difficult.

I'd like two tickets for tomorrow's early morning flight. How much did you pay?. Afternoon and evening. I'll just check for you.

The FMS does navigation and performance calculations for optimum flight performance.*. EI FMS realiza cálculos de navegación y actuación para un vuelo óptimo. EI FMS no hace cálculos de navegación y rendimiento para un desempeño óptimo del vuelo. EI FMS realiza cálculos de navegación y rendimiento para un desempeño óptimo del vuelo.

"Hydraulic pressure is monitored if the autopilot servo needs hydraulic power.*. La presión hidáulica es monitoreada si el servo del autopilot necesita presión hidráulica. La presión hidráulica será monitoreada si el servo del autopilot necesitara poder hidáulico. La presión hidáulica es monitoreada si el servo de autopilot necesita poder hidráulico.

As the elevator accelerates there is an additional force which increases the weight.*. A medida que el elevador acelera, hay una fuerza adicional que aumenta el peso. Cuando el elevador acelera, hay una fuerza extra que reduce el peso. A medida que el elevador acelera, hay una fuerza adicional que disminuye el peso.

Additional flight instruments which you will learn about in this unit are the Vertical speed indicator, the Mach meter and the temperature indicators.*. Instrumentos de vuelo adicionales que vas a aprender sobre en esta unidad son el indicador de velocidad vertical, el medidor de Mach y los indicadores de presión. Los instrumentos de vuelo adicionales que aprendiste en esta unidad son el indicador de velocidad vertical, el medidor de Mach y los indicadores de temperatura. Los instrumentos de vuelo adicionales que aprenderas en esta unidad son el indicador de velocidad vertical, el medidor de Mach y los indicadores de temperatura.

The discrepancy forms ____. were checked according with the procedures. were checked in according with the procedures. were checked according to the procedures.

Choose the correct sentence. Rolls Royce has developed the Trent family to meet the market demand. Rolls Royce has developed the Trent family to meeting the market demand. Rolls Royce has developed the Trent family meet the market demand.

Choose the correct sentence.*. Each engine to have one power pack. Each engine have one power pack. Each engine has one power pack.

Choose the correct sentence. The ECC has complete its power up checks (6% N2). The ECC has completed its power up checks (6% N2). The ECC has completing its power up checks (6% N2).

Choose the correct sentence. These members to transfer shear loads from one component to another. These members transfers shear loads from one component to another. These members transfer shear loads from one component to another.

Choose the correct sentence.*. During the last flight, the lightning hit the radome first. During the last flight, the lightning hitted the radome first. During the last flight, the lightning hits the radome first.

How is hydraulic power supplied to the surfaces that control the movement of the aircraft around the three axes?*. Via priority valves. Via leak measurement valves. Through the electrical system. Through the main engines.

What happens to the priority valve when the hydraulic pressure from the green system falls?*. It opens to supply the flaps and leading edge devices. It automatically closes and cuts off supply to the flaps and leading edge devices. It maintains the current pressure levels. It deactivates all primary flight controls.

When are the leak measurement valves used to perform checks?*. When the aircraft is on the ground. Only during emergencies. Only douring routine maintenance.

Under what conditions does the indicator button on the oil filter extend, and why are these specific conditions important for monitoring filter clogs?. The indicator button extends when the oil temperature exceeds 70°F (21°C) to ensure the oil remains cool. The indicator button extends when the pressure difference across the filter is less than 30 to 40 psi, indicating low pressure. The indicator button extends when there is a pressure difference of more than 30 to 40 psi across the filter and the oil temperature is more than 70°F (21°C), indicating potential filter clogs that could affect engine performance. The indicator button extends when the oil temperature is less than 70°F (21°C) to prevent the oil from becoming too cold. When you push and hold the system annunciator lights, the recall signal goes to all the components which cause the lights on the system annunciators to come on. This causes all the lights on the system annunciators to come on. When you release the system annunciator lights, the system annunciator lights show only the systems which have faults.

What is the purpose of pushing and holding the system annunciator lights?. Pushing and holding the system annunciator lights sends a recall signal to all components, causing all annunciator lights to come on. Pushing and holding the system annunciator lights turns off all the system lights, helping to conserve power. Pushing and holding the system annunciator lights resets all the system components to their default state. Pushing and holding the system annunciator lights activates the emergency lighting system for the aircraft When you push the FAULT/INOP test switch, faults are simulated to do a check of the circuit ability to detect a fault. If the circuits operate correctly, all lights on the front panel come on. If a light does not come on, it shows a faulty circuit operation. The FAULT DISPLAY lights show the type of fault and the detector location.

Why is it significant that different materials are used for the upper and lower panels, and how does this choice relate to the type of loads each panel carries?. The upper skin panel is made of a zinc aluminum alloy because it primarily carries tension loads, which require a material capable of stretching without breaking. The lower skin panel is made of a copper aluminum alloy because it mainly carries compression loads, which necessitate a material that can withstand crushing forces. Both the upper and lower skin panels are made of the same alloy to uniformly distribute loads across the wing structure, but the thickness varies to manage joints and openings effectively. the material choice for the upper and lower skin panels is arbitrary, and the primary concern is the overall weight reduction of the wing structure rather than load management. The upper skin panel is made of a zinc aluminum alloy to efficiently carry compression loads, which are predominant on the upper surface due to the aerodynamic forces during flight. The lower skin panel is made of a copper aluminum alloy to handle tension loads, as the lower surface experiences pulling forces. This material differentiation is crucial for optimizing the structural integrity and performance of the wing.

Why does the priority valve cut off supply to the flaps and leading edge device when the hydraulic pressure falls?. To allow the system pressure to build up again and provide adequate supply to the primary flight controls. To reduce the weight of the aircraft and provide adequate supply to the primary flight controls. To deactivate the flight control system. To save hydraulic fluid.

What mechanism is used to adjust the cooling effect of the precooler, and how does it achieve this adjustment?. A temperature sensor adjusts the cooling effect by changing the temperature of the engine bleed air. The cooling effect is adjusted by altering the speed of the engine fan. The cooling effect is controlled by a pressure regulator that changes the pressure of the fan air. A fan air valve is used to vary the mass of fan air passing through the precooler, thereby adjusting the cooling effect.

What is the main advantage of GE's connected Flight Management System (FMS)?*. Greater gains in efficiency and economy for individual flights. Onboard high bandwidth connectivity. Powerful fleet management solution in every phase of flight.

GE Aviation is working to improve...*. Flight data for analysis during the flight. Flight data for analysis in route or post flight. Flight data only during the flight.

How does the connected FMS reduce pilot workload?*. By enabling pre-flight tasks to happen off aircraft. By improving situational awareness for the pilot and dispatch. By providing access to ATC information.

What is the largest potential for gains and operational efficiencies?*. Improved aircraft usage and route optimization. Fuel savings and improved fleet operations and maintenance. Real-time analytics.

What does GE Aviation provide to app developers to leverage the power of data access?*. Flight management system software modules. Onboard high bandwidth connectivity. Connected FMS software development kit.

The Valve Control Unit ___The RDC.*. receives data from. bypasses. feeds.

MLG is located... Between FWD Cargo Compt and NWW. In front of AFT E/E. Among AC Bay.

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