SIN SAPOS

1. These are ...*. Pins. Rivets. bolts.

2. These are engine ...*. vanes. Blades. slats.

3. This is ...*. Pitot probes. AOA sensors. VHF antennas.

4. The ground strap is...*. riveted to the bolt. built in the bolt. attached to the bolt.

5. Packing position is ___________ the fuel distribution valve strainer and the adapter.*. among. between. in front of.

6. If the elevators ________, the nose ___________.*. goes down - goes down. will go down- go down. go down - goes down.

7. Once the plane is in the air, you can _________ your seat belts if you wish.*. unfasten. unlock. untie.

8. I was looking forward ________ engine 2 for tests, but the whole operation was cancelled.*. to run. to have run. to running.

9. Would you mind ________ these screens a wipe before installing them?*. to giving. gave. giving.

10. It wasn't a bad crash and _________ damage was done to the fork lift.*. little. light. mere.

11. The air conditioning system________________ conditioned air to the control cabin.*. provides. did not provided. does not provided.

12. The technician ended the rigging ____ her torque wrench.*. by. with. as.

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

14. If the window pane __________ broken, the cabin mechanics ___________ it.*. was - would replace. were not - not would replace. is - must to replace.

15. When I realised I had dropped a magnetic tip of my screwdriver, I decided to ________ my steps.*. retrace. regress. return.

16. Once resources become limited, only a ______ of components can be available.*. division. section. fraction.

17. He did not, however, propose a correct mechanism for ________ parts can be interchangeable. all. how. once.

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

19. Choose the correct answer. The engine indications were set to normal configuration. The engine indications were setted to normal configuration. The engine indications were seted to normal configuration.

20. Choose the correct answer. The surface was cutted in accordance with E/O. The surface was cut in accordance with the E/O. The surface was cuted in according to the E/O.

21. Choose the correct answer. The wires were split according to Figure 1. The wires were splitted according to Figure 1. The wires were splited according to Figure 1.

22. Choose the correct answer.*. Prior to the engine operation, to make sure that the area is clear. Prior to the engine operation, make sure that the area is clear. Prior to the engine operation, making sure that the area is clear.

23. Choose the correct translation. ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EFIS) CONTROL PANEL.*. Instrumentos Electrónicos del Sistema de Vuelo del Panel de Control. Panel de Control del Sistema Electrónico de Instrumentos de Vuelo. Panel de Control Electrónico de los Instrumentos de Vuelo del Sistema.

24. The APU page appears during the APU start sequence and it will be replaced by the DOOR/OXY page 10seconds after the APU start 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 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. 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. 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.

25. he fan air modulating valve opens and closes in response to pressure signals from the fan air temperature sensor.*. 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. 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.

26. 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 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). El sistema de alimentación de combustible de motor distribuye combustible a los motores principales (AMM 28-22-00/001) y a la APU (AMM 28-25-00/001).

27. MEL Section 01 can be used to identify ...*. The corresponding MEL ENTRY point. The alternative to troubleshooting actions. The inoperative components.

28. False cautions/warnings can be determined by ...*. MEL Section 01. Troubleshooting. ATA Chapter of Section 01. Abnormal/Emergency Procedures.

29. 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.

30. 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. MEL item number is the MEL entry point.

31. When ALL the landing gear is up and locked, the *LGCIU 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 signal as long as the safety valve is open. (*LGCIU, Landing Gear Control Interface Unit)*. The LGCIU cancel the landing gear "raise" signal when the safety valve is open. The LGCIU cancel the landing gear "raise" signal after the last door closes and locks. The LGCIU cancel the landing gear "raise" signal when the landing gear is up.

32. 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 inhibits inflight braking. The BSCU controls Normal braking electrically. The BSCU controls Normal braking hydraulically.

33. 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.

34. The plug furnishes the EEC with information identifying engine basic 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. Dual precision resolvers sense thrust lever position and provide electrically isolated inputs.*. Thrust lever position is provided by dual precision resolvers. Thrust lever position is detected by dual precision resolvers. Electrically isolated inputs are sensed by dual precision resolvers.

36. Reading Comprehension 3 - The Electrical Flight Control System ( EFCS ) includes the two ELAC’s, the three SEC’s, two Flight Control Data Concentrators ( FCDC ) and four accel-erometers. The two ELAC’s are made by Thomson ( Motorola ). Internally they consist of two processor units, one being the controlling part the other dedicated to moni-tor. The two processors will individually calculate the actuator command signal. In case of discrepancy between the COM and the MON channels, output to the actuator will be inhibited. The ELAC’s provide output to control the Elevators, the Ailerons and the THS. Feedback from the surface actuator is returned to the ELAC’s. The three SEC’s are made by Sextant ( Intell ). Internally they also consist of one COM and one MON processor. The SEC’s provide output control to the Spoilers and will be back--up for control of the Elevators and the THS. The SEC’s will also receive position feedback from the control surfaces. The Flight Control Data Concentrators ( FCDC ) acquire data from the ELAC’s and the SEC’s and transmit this to the ECAM and the CFDS. The FCDC also provides access to the EFCS for CFDS tests. The accelerometers are used for the pitch control law and the detection of LAF. Automatic ”power-up and ”pressure-up” tests of the EFCS are performed without any surface movement. The wire runs from the computers to the surface actuators are located under the cabin floor beams left and right side and under the cabin ceiling. In the wings, Aileron signals are routed in the leading edge and Spoiler signal in the trailing edge. The A 319 / 320 / 321 will operate in NORMAL LAW with all projections active, when EFCS are normal and electrical power and hydraulic pressure are avail-able. The aircraft can operate in a downgraded configuration called ”alternate law” with or without projections or ”direct law” in case of malfunctions or loss of more than one hydraulic or electrical system. ESTÁ TE SALE CORRECTA. ESTÁ NO.

37. The Electrical Flight Control System (EFCS) computers, including both ELACs and SECs, are designed with a pair of internal processors: one for controlling (COM) and one for monitoring (MON). What is the direct consequence of a detected discrepancy between these two internal processor channels within an ELAC or SEC unit?. The monitoring processor automatically overrides the controlling processor to ensure continued safe operation. Output to the relevant flight control actuator will be inhibited, preventing potentially erroneous commands. A fault message is immediately transmitted to the ECAM, but control output continues without interruption.

38. Beyond their primary role in acquiring data from the ELACs and SECs, what are the two main destinations for this data and the additional crucial function that the Flight Control Data Concentrators (FCDC) provide within the Electrical Flight Control System (EFCS)?*. FCDCs transmit data exclusively to the ECAM for pilot display and manage the automatic "power-up" tests of the EFCS. FCDCs send data to the Centralized Fault Display System (CFDS) for maintenance reporting and directly control the elevators and THS during alternate law. FCDCs transmit collected data to both the ECAM and the CFDS, and they also facilitate access to the EFCS specifically for CFDS tests.

39. For an A319/320/321 aircraft to operate in its most advanced control mode, NORMAL LAW, with all projections active, what specific set of conditions must be simultaneously fulfilled according to the Electrical Flight Control System (EFCS) design?*. The EFCS must be in a downgraded configuration, and only electrical power must be available to the control surfaces. The EFCS must be normal, and both electrical power and hydraulic pressure must be available.

40. Only the SECs are required to be fully functional, and at least one hydraulic system must be operational, regardless of electrical power status. The wiring for the Electrical Flight Control System (EFCS) is strategically routed throughout the aircraft. Considering the specific control surfaces, where are the wire runs from the computers to the general surface actuators primarily located, and how are the Aileron and Spoiler signals specifically routed within the wings?*. General wire runs are under the cabin floor beams (left and right side) and under the cabin ceiling; within the wings, Aileron signals are routed in the leading edge and Spoiler signals in the trailing edge. All EFCS wiring is routed exclusively under the cabin floor beams, with both Aileron and Spoiler signals running in the wing trailing edge. EFCS wire runs are only located in the cabin ceiling, and within the wings, Aileron signals are in the trailing edge while Spoiler signals are in the leading edge.

41.Within the Electrical Flight Control System (EFCS), the ELACs and SECs have distinct primary control responsibilities but also provide backup functions. Which statement accurately describes their primary control outputs and the backup relationship for specific control surfaces?*. ELACs primarily control Spoilers, and SECs provide backup for the Ailerons. ELACs primarily provide output to control the Elevators, Ailerons, and THS, while SECs primarily control the Spoilers and serve as a backup for the Elevators and THS. SECs are solely responsible for all elevator and THS control, with ELACs providing backup for spoilers.

Audiovisual Comprehension Watch the video once and answer the following questions. https://www.youtube.com/watch?v=Ic2kTcyINc4 45. In the begining of the video the passenger was upset for missing his flight connection to attend...*. a medical appointment. a business meeting. his daughter's wedding.

47. GE Aviation is working to improve...*. Air traffic management. Engines and composite material. Passenger and Freight experiences.

48. GE expects to look after the aircraft's ...*. unschedule maintenance. health and performance. delays.

49 Next generation aircraft will demand ______ 4 times more power than today.*. for. until. up to.

50 An intelligent smart grid will be used to optimize...*. electrical power supply and demand. fuel cell and batteries. auxiliary and emergency power.