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9. Where are the pitot/static signals for ISFD come from? . They come from the right pitot/static system. . They come from the left pitot/static system. . They come from the center pitot/static system. .

10. What function will automatically tune the VOR, ILS and DME? . FMF (in the CCR's). . AFF (in the FCE's). . DCAF (in the CCR's). .

ERS. One airplane personality module (APM) has failed, and it is replaced, choose from the following: The related IRU or AHRU sends the stored misalignment data to the new APM. The new APM brings the misalignment data for-8 or -9 configuration. A procedure with a ramp test to programming the new APM for IRU or AHRU can be performed.

12. What is the first ADRF priority for the first officer air data?  C1 FCE voted for airspeed and altitude.  R FCE voted for airspeed and altitude.  C2 FCE voted for airspeed and altitude. . C1 FCE voted for airspeed and altitude. . R FCE voted for airspeed and altitude. . C2 FCE voted for airspeed and altitude. .

13. The airplane is on approach mode. The flight crew arms approach (APP). Which is the first antenna to receive the localizer (LOC) radio signals and send them to the INR? . VOR capture antenna. Localizer track antenna. . Localizer approach antenna.

14. Where is the Autopilot, Flight Director and autothrottle mode Shown? . ND (Navigation Display). . FMA (Flight Mode Annunciator) on the PFD (Primary Flight Display). . CDU (Control Display Unit). .

15. Where does the ADMs take power from? . +/-13,5v DC Power Management Module (PMM) in the Core Network Cabinet. . +/-13,5v DC Power Condition Module (PCM) in the Flight Control Electronics (FCE). . +/-13,5v Power Condition Module (PCM) in the Common Computer Resource (CCR).

16. Where is the thrust management function software located? . FCM L, R and C1. . ACE C2. . L and R CCR. .

17. What are the FCEs supplied by the right radio altimeter transceiver? . FCE R and C2. . FCE L and C1. . FCE R only. .

18. Why is the "TO/GA" message at the top of the column green? (Incluye imagen de referencia) . Because it is the ARME D mode. Because it is in STANDBY mode. . Because it is the ENGAGED mode. .

19. When does the Thrust Management Function (TMF) provide full go-around thrust? . When push both "TO/GA" switch at the same time. . At the first push of the "TO/GA" switch. . At the second push of the "TO/GA" switch. .

20. What are the purpose of the air data modules (ADM) program pins? . To determine ADM type (pitot or static) and location. . To get power from the power control modules (PCM) in the FCE cabinets. . To send the data to the air data reference function (ADRF). .

21. Which function are integrated in to the ISS (Integrated Surveillance System)? . ILS, GLS, GPS (GNSS). . ATC, TCAS, WXR, TAWS (GPWS). . FMF, ADRF, VOR. .

22. Where is the Auto Flight Function software? . In the Core Network Cabinet. . In the Flight Control Electronic (FCE). In the Common Core System (CCS). .

23. The weather radar receiver transmitter modules (RTM) are. FWD EE BAY. . NOSE RADOME. . AFT EE BAY. .

24. What supplies attitude data to the integrated standby flight display (ISFD)? . It has its own inertial sensors to calculate pitch and roll attitude. . cdn.

40. When the ISFD sends backup attitude, airspeed and altitude data to the common data network (CDN). . This data is a backup if the common data network (CDN) fails. . This data is a backup if all FCEs fail. . This data is a backup if the FCE C2 fail. . The left IRU.

25. Which one of the 3 FMF software copies in the common computer resource is the master? . The first FMF to power-up is the master FMF. . Master condition is based on programming pin. . The FMF in the right CCR cabinet is the master. .

26. For flight purposes, When the A/P can be engaged? . At 80 knots. . When the airplane is above 200 feet (R.A.). . Only on cruise. .

27. Where do you perform a manual tuning and course selection to VOR receivers? . CDU "NAV RAD" page. . Backup Navigation menu on TCPs. . Alternate EFIS panel on multifunction displays. .

28. Which of these functions are in the flight control modules (FCM)? . Air data reference function (ADRF). . Thrust management function (TMF). . Flight Management Function (FMF).

29. When the autopilot flight director system (AFDS), provides de better fuel economy performance? . With A/P engaged above 200 ft. . With autopilot engaged in VNAV and LNAV modes. . With A/T engaged manually or automatically. .

30. Which are the modes of the FMF (Flight Management Function)? . Main, Secondary and Tertiary. . Master, Hot spare and Backup. . Primary, Secondary and Standby. .

31. When the airplane is on the air and the autopilot is engaged and the airplane rolls right. What moves the control wheel? . Control wheel backdrive actuator through ACE C1. Control wheel backdrive actuator through ACE C2. . Control column backdrive actuator through ACE C2. .

32. What LRIU supplies ILS approach deviation data to the ISFD? . Left integrated navigation radio. . Left integrated surveillance system. . Left flight control electronics (FCE) C1. .

33. What does the airplane use for the TAT value when the airplane is in flight? . Simple average of TAT. . Weighted average of EEC elements and TAT probes. . ower average of EEC elements and CAI ice protection system (CIPS). .

34. When does the Flight Management Function (FMF) send lateral guidance commands to the Auto Flight Function (AFF)? . When the HDG/TRK select mode engages.When the VNAV mode engages. . When the LNAV mode engages. .

35. The terrain awareness and warning system (TAWS) function includes: . Basic ground proximity warning system (GPWS) and Enhanced GPWS (EGPWS). Basic ground proximity warning system (GPWS) and air traffic control (ATC). . Traffic collision avoidance system (TCAS) and Enhanced GPWS (EGPWS). .

36. Which are the AutoPilot disconnect indications? . 2 yellow Master Caution light, Aural cautions, Eicas Caution. . 2 red Master Warning light, Aural Warning and Eicas Warning. . 2 A/P Disengaged light, Aural horn, and Status MSG. .

37. The autopilot controls the airplane attitude in all phases of flight, except: . In takeoff. . In climb. . In go-around. .

38. When does the Primary Flight Control Function (PFCF) accept Auto-Flight Function (AFF) commands? . Only when the PFCFs are in SECONDARY mode. . Only when the PFCFs are in NORMAL mode. . When the PFCFs are in ANY mode.