TEST BORRADO, QUIZÁS LE INTERESE:
ATR72-1
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Título del Test:
ATR72-1 Descripción: ATR72-1 PRrimera 50 preguntas Autor: atr42 OTROS TESTS DEL AUTOR Fecha de Creación: 23/01/2014 Categoría: Test de conducir Número Preguntas: 50 |
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1- The oxygen syst of the ATR has been designed to supply cockpit crew members and observer, the cabin crew and :' a) 25% of passengers during 30 min b) 50% of passengers during 30 min c) 100% of passengers during 30 min. 2.It is possible to charge the oxygen cylinder : a. On the aircraft aircraft b. On workshop c. A and b are correct. 3. The PW127F engine is installed on: a. ATR 72-212A b. ATR 42-400 c. ATR 42-500. 4. The power plant control system consist of: : a. The power lever (PL) b. The condition lever (CL) c. A and b are correct. 5. The CL positions are the following: a. MAX REV,GI, FI,T.O,MAX PWR b. FUEL SO, FTR,AUTO, OVRD c. A and b are correct. The fuel cooled oil cooler provides cooling of the RGB lubricating oil by using: a. Air as cooling source b. Oil as cooling source c. Fuel as cooling source. 7. The EEC controls a stepper motor located in : a. AFU b. HMU c. RGB. 8. The fuel manifold has : a. 14 fuel nozzles b. 16 fuel nozzles c. 10 fuel nozzles. 9. In hotel mode the airflow is inverted. What component opens the oil cooler flaps: a. The thermal actuator b. The oil cooler c. A and b are correct. 10. Controlled by the EEC , if the EEC fail, this components shows dashes: a. Torque indicator b. NH indicator c. NP indicator. 11. The HBV is controlled in manual mode by differential press in case of: a. Loss of EEC b. EEC push button release out c. A and b are correct. 12. The torque sensors are located on RGB casting at: a. 4 and 8 o’clock, looking forward b. 12 and 8 o’clock, looking forward b. 12 and 8 o’clock, looking forward. 13. 2 identical sensors (NH1,NH2) are located on: a. Reduction gear box b. Accessory gear box c. Non are correct. 14. An IGN blue light on MEMO panel illuminates in case of: a. Automatic relight b. Manual ignition c. Both are correct. 15. When the engine start selector is set to any start position, what component check the start and battery contactors position: a. GCU b. BPCU c. MFC. 16. Illuminates blue when the propeller brake is fully released and extinguished when propeller brake is fully locked: a. PROP BRK light b. Ready light c. Non are correct. 17. Max torque computed depending the PWR MGT selection is achieved by: a. EEC b. AFU c. FDAU. 18. Actual torque signal (pointer) is displayed from the: a. EEC b. AFU c. FDAU. 19. Actual torque signal (digital counter) is displayed from the: a. EEC b. AFU c. FDAU. 20. Propeller pump test sw with 2 stable positions enables to test the feathering pump a. On flight b. On flight and on ground c. Only on ground for safety. 21. The AFCS ensures 3 functions: a. AP,FD & YD b. AP,FD & AT c. AP,AT & YD. 22. The main components of the AFCS are: a. 2 ADC, 3 servo actuators, 1 ADU (advisory display unit) b. 2 SBU, 1 ADU,1 computer (AFCS) c. 1 Computer AFCS, 3 servo actuators, 1 ADU, 1 control panel. 23. Autopilot engagement automatically engages : a. YD b. GA c. Both YD & GA. 24. Yaw damper is used also for: a. Pilot in manual mode b. Autopilot in turn coordination c. A & b are correct. 25. Autopilot disengagement logic is controlled by: a. AFCS computer b. ADU c. MFC. 26. Both SGU receive analog signal coming from NAV sensor (VOR,ILS,MKR), this data is sent to the AFCS computer through: a. Arinc 429 b. ASCB c. Rs 422. 27. Autotrim is powered by: a. MFC b. AFCS computer c. ADC. 28. Sound level preset and are not adjustable: a. TCAS, CCAS,GPWS b. PA,VHF comm system c. Nav aids, ADF. 29. The heart of all electronic cockpit communications is: a. Remote control audio unit (RCAU) b. CVR c. ACP. 30. CVR has a memory capacity of : a. 30 min b. 60 min c. 120 min. 31. The CVR system is of latest standard and is known as : a. CVR enhanced b. CVR uprated c. SSCVR. 32. The audio level for pass cabin loudspeaker is increased by 6dB as soon as: a. The last engine is started b. One engine is started c. The two engine are started and stabilized. 33- CVR stop recording: a) 10 min after first engine shut down b) 10 min brake applied c) 10 min after last engine shut down. 34- The CVR is located : a) In the aft unpressurized area b) In the aft ceiling att panel c) In the 85 Vu. 35- The ELT is able to transmit distress signal on: a) 121.5Mhz, 280.3Mhz, 406.025Mhz b) 121.5Mhz, 406.025Mhz, 243Ghz c) 121,5Mhz, 406.025Mhz, 243Mhz. 36- The erase of the CVR is made when: a) WOW + Parking brake applied + erase push button depressed b) WOW + parking brake off + erase push button depressed c) WOW + Parking brake applied + erase push button not depressed. 37- The electrical system consist of 3 subsystem separated: a) DCW, ACW, AC b) ACW,AC,DC c) AC,CC,ACW. 38- Ac constant frequency is provided by : a) Inverters(dc to ac) b) TRUs c) Ac generators. 39- TRUs Transforms: a) Acw into dc for emergency purposes b) dc into dc for emergency purposes c) cc into ac for emergency purposes. 40- Starter generators as starter, it rotates the HP compressor. The cut out point is: a) 25% NH b) 45% NH c) 61.5% NH. 41- Starter generators as generator, it is driven by the HP compressor. The on line point is: a) 25% NH b) 45% NH c) 61.5% NH. 42- Provides control for its own generator and starter operation: a) BPCU b) GCU c) TRU. 43- Provide controls for batterys own operation and transfer contactors controls: a) BPCU b) GCUs c) MFCs. 44- Amber arrow in the TRU push button indicate: a) TRU is in operation b) TRU faulty c) TRU off. 45- Opened position is forward door. operations can be performed manually from inside or outside of the airplane a) Cargo door b) Service door c) Pax door. 46- This door gives access to the unpressurized area of the aircraft: a) Forward compartment door b) Cockpit communication door c) Aft avionic compartment door. 47- When you are doing the light test the MFC turns on : a) All lights b) Almost all lights c) Some lights. 48- The power supply for flushing motor is a) 28vdc service bus b) 26vac main bus c) 115vac main bus. 49- The pack valves are : a) Pneumatically operated and electrically controlled b) electrically operated and electrically controlled c) Pneumatically operated and pneumatically controlled. 50- A turbo fan provides cooling air on ground or flight when the aircraft speed is lower than: a) 150 k/h b) 150 m/h c) 150 kts. |
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