XLR8

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.

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.

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.

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.

The FMS does navigation and performance calculations for optimum flight performance. El FMS realiza cálculos de navegación y actuación para un vuelo óptimo. El FMS no hace cálculos de navegación y rendimiento para un desempeño óptimo del vuelo. El 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 hidráulica es monitoreada si el servo del autopilot necesita presión hidráulica. La presión hidráulica será monitoreada si el servo del autopilot necesitara poder hidráulico. La presión hidráulica es monitoreada si el servo del 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 aprenderás en esta unidad son el indicador de velocidad vertical, el medidor de Mach y los indicadores de temperatura.

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 during routine maintenance. During flight.

Why does the priority valve cut off supply to the flaps and leading edge devices 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.

"The temperature in the pneumatic system must not exceed acceptable values. A built-in precooler is used to cool the engine bleed air temperature. Cooling air is taken from the engine fan duct. The cooling air is simply fan air. The cooling effect depends on the mass and temperature of fan air. You can probably guess that in order to vary the cooling effect, the mass of fan air must also be varied. A fan air valve is used to allow more or less fan air to pass the precooler." 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.

"The skin panels form the exterior surface of the wing. and they are reinforced by stringers on the inner surface of the skin. The thickness of the wing skin panel is tapered depending on the joints and openings. The upper skin panel carries mainly compression loads to the fuselage structure and is made of a zinc aluminum alloy. The lower skin panel carries mainly tension loads to the fuselage structure and is made of a copper aluminum alloy." 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.

The oil filter has an indicator button to monitor for filter clogs. 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), the indicator button extends. 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. What does it indicate if a light does not come on when you push the FAULT/INOP test switch, and how does the system provide information about the fault?. It indicates that the circuit is functioning correctly, and the FAULT DISPLAY lights show the system status. It indicates a faulty circuit operation, and the FAULT DISPLAY lights show the type of fault and the detector location. It indicates that the test switch is not working properly, and the FAULT DISPLAY lights show the battery status. It indicates normal operation, and the FAULT DISPLAY lights show the power levels.

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.