estudiar ingles

if the elevators ____, the nose__. goes down- goes down. will go down - go down. go down - goes down.

once the plane is in the air , you can _____ you seat belts if you wish. undress. unfasten. in lock.

i was looking forward ____ engine 2 for test, but the whole operation was cancelled. to run. to have run. to running.

would you mind ____ these screens a wipe before installing them. to giving. gave. giving.

it wasnt a bad crash and ______ damage was done to the fork lift. little. small. light.

the air conditioning system _____ conditioned air to the control cabin. provides. did not provided. does not provided.

the techbician ended the rigging ____ her torque wrench. by. with. in.

can i park the genie telescopic boom lift here. sorry, i did thet. it,s the same place. only for half an hour.

if the window pane ____ broken ,the cabin mechanics ____ it. was - would replace. were not - not would replace. is - must replace.

when i realized i had dropped a magnetic tip of my screwdiver, i decided to___ my steps. retrace. regress. resume.

choose the correct alternative. the toilet seat was removed according to the procedure. the toilet seat was removed in according to the procedure. the toilet seat were removed according to the procedure.

choose the correct alternative. the engine indications were set to normal configuration. the engine indications were setteed to normal configuration. the engine indications were setted to normal configuration.

choose the correct alternative. the surface was cut in accordance with E/O. the surface was cutted in accordance with E/O. the surface was cuted in accordance with E/O.

14. Choose the correct alternative. The wires were split according to figure 1. The engine indications were setteed to normal configuration. The engine indications were setteed to normal configuration. The engine indications were seted to normal configuration.

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

20. MEL section 01 can be used to identify... The corresponding MEL ENTRY point. The inoperative components. The alternative to troubleshooting actions.

21. False cautions/warnings can be determined by. Abnormal/Emergency procedures. - MEL section 01. Troubleshooting.

22 If a false caution/warning is determined.. - Aircraft dispatch is not allowed. - Aircraft dispatch is allowed. - Aircraft dispatch conditions are considered to be normal. - Aircraft crew must check the systems/components condition.

23. When a caution/warning and "not applicable" dispatch condition column appear together... - Aircraft dispatch is allowed. . - MEL is not to be consulted. - MEL is to be consulted.

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

35. CFM success is based on. Aftermarket low-priced parts. Customer’s cost saving. Engine parts flying time and reliability.

28. QUESTION: Dual precision resolvers sense thrust lever position and provide electrically isolated inputs. - Trust lever position is detected by dual precision resolvers. Trust lever position is provided by dual precision resolvers.

36. These are.. - Pins. - Pins. Rivets. Bolts.

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

37. The bigger logo is on. - The winglets. - The elevators. - The rudder.

30. Packing position is ________ the fuel distribution valve strainer and the adapter. Among. Between. In front o.

31. What happens to the engines once an aircraft retires? -. They are no longer serviceable. - They stay with the aircraft in the Mojave desert. - They may live on for many years.

32. Engine parts which are serviceable in accordance with proper inspection. - Can never be reworked. Can be fixed and returned to the aftermarket. Can be used to build new Airbus aircraft.

33. GE CFM is committed to support the customer. - Through the asset’s entire lifecycle. Until the aircraft’s last flight. - Until parts are available.

34. Aftermarket engine parts are.. - More expensive. - Cheaper. - Certified and cost the same as new parts.

38. These are engine. Vanes. Blades. - IDG.

39. This is.. A slide. - A raft. A floater.

40. The passengers walk over it. - Sidewall panelt. Floor carpet. Armrest.

41. Choose the correct alternative: ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EFIS) CONTROL PANEL. - Panel de control del sistema electrónico de instrumentos de vuelo. - Instrumentos electrónicos del sistema de vuelo del panel de control. - Panel de control electrónico de los instrumentos de vuelo del sistema.

42. In the beginning of the video, the passenger was upset for missing his flight connection to attend... - A medical appointment. A business meeting. His daughter's wedding.

43. GE aviation is working to improve... - Air traffic management. - Engines and composite material. - Passenger and freight experiences.

44. GE expects to look after the aircraft’s... - Unscheduled maintenance. - Health and performance. - Delays.

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

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

26. If either the sliding window or the fixed window heating is faulty, the failure is shown amber on the EWD. - ATA chapter of section 01. -On the EWD, the failure will appear amber when one window heating is faulty. - On the EWD, the failure will appear amber when both sliding and fixed windows heating is faulty.

17. The APU page appears during the APU start sequence and it Will be replaced by the DOOR/OXY page 10seconds after the APU star sequence.The ENG page appears during the Engine start sequence and it Will be replaced by the WHEEL page after the Engine start sequence. - La página APU aparece durante la secuencia de partida del APU y será reemplazada por la página DOOR/OXY 10 segundos después de la secuencia de partida de la APU. La página ENG aparece durante la secuencia de partida del Motor y será reemplazada por la página WHEEL después de la secuencia de partida del Motor. - La página APU aparece durante la partida de la secuencia de la APU y reemplazará a la página DOOR/OXY 10 segundos después de la partida de la secuencia de la APU. La página ENG aparece durante la partida de la secuencia del Motor y reemplazará a la página WHEEL después del inicio de la secuencia del Motor.

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

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

24. When All the landing gear is up and locked ,the LGCIU signals the doors to close while maintaining landing gear UP signal to keep "raise line pressurized.Door uplock proximity detectors signal the LGCIU that the doors are uplocked.As soon as the last door closed and locks, the LGCIU cancels the landing gear "raise" signal and maintains the door close signal as long as the safety valve is open.(LGCIU,Landing Gear Control Interface Unit). - The LGCIU cancels the landing gear "raise" signal after the last door closes and locks. - The LGCIU cancels the landing gear "raise" signal when the safety valve is open. - The LGCIU cancels the landing gear "raise" signal when the landing gear is up.

25. 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 electrically. - The BSCU inhibits inflight braking. - The BSCU controls Normal braking hydraulically.