787b

1.- Where are located the FMF ( flight management function). IN TO CCR ( common computer resource ). s.

2.- In the ER system what statement is true about IRUs and AHRUs?. The AHRUs have decreased performance gyros and the same software load. a.

3.-The frequency of the HF and VHF communication system in selected through: Tuning control panel (TCP). a.

4.- The auto flight function software is: : In the flight control electronic (FCE). a.

5.- When the WXR system comes on and transmits in the PWS( predictive windshear ) mode: When N1 is at least 60%. a.

6.-Where is the ADRF located?. this function is part of FCM. n.

7.-What is the back-up power supply source for the AHRU/IRU. The hot battery bus. b.

8.-How could be activated the ELT system?. manually from ELT control panel or automatically from G switch. d.

9.- Where does the ADM (air data module) takes power?. PCM( power control module) from the FCE (flight control electronics). d.

10.- The power for the emergency lights comes from. Wels control unit (WCU) Batteries. d.

11.-What happens if A/P is engaged and pilot selects VNAV and LNAV modes?. The FMF sends commands to A/P, A/T, F/D according to the selected flight plan, with better performance. d.

12.- The cabin attendant Handset has interface with…. A cabin zone unit (CZU). d.

13.- The marker beacon function is active in: Left INR (integrated navigation radio). d.

14.- Which of the following statement are correct related to the functions of thrust management function (TMF)?. Thrust limit calculation and autothrotte (A/T) function (includes engine trim equalization). s.

15.-What is the airplane personality module (APM) main purpose?. The APM provides mounting trays misalignment correction data. s.

16.- The b787 has 3 back drive actuator, which of them does not work in the cruise phase?. The rudder pedal back drive actuator (BDA). s.

17.- Which units process the VOR function?. : INR (integrated navigation radio). s.

18.- SELCAL.. In which unit are located the “SELCAL” decoder function?. In the AGUs. s.

19.- Which on the 3 FMF software copies in the common computer resource is the master?. The first FMF to power-up is the master FMF. s.

20.- Which of the pollowing statements regarding the AFF is true?. The AFF sends a signal to the INR to change localizer signal input from the VOR antena to the ILS antenna. s.

21.- Which to the following statements regarding the DME is tru. Can be tuned 5 DME ground stations at the same time. s.

22.- SATCOM. The diplexer low noise amplifier (DLNA). Lets the SATCOM system receive and transmit signals at the same time (Full duplex). s.

23.- Which is the central control unit in the cabin system?. CSSC (cabin service system controller). s.

*24.- Where is the autopilot, Flight Director and autothrottle mode shown?. FMA (flight mode annunciator)on the PFD( primary flight display). s.

25.-Which functions are integrated in the ISS( integrated surveillance system)?. ATC, TCAS, WXR, TAWS (GPWS). s.

26.- Which unit are used for the ADRF, to get information from the pitot/static probec?. ADM. s.

27.- Where are the volume control for the speakers in the flight deck?. In the audio control panels. s.

28.- Where is shows the LRRA information?. In the PFD and HUD. s.

29.- Which are the autopilot disconnect indications?. 2 red master warning light, aural warning and eicas warning. s.

30.- Where can you control the emergency lighting system?. From P5 or master attendant switch panel (ASP). s.

31.- What kind of HF antenna is used in the 787-9?. It is a wire type antenna. s.

32.- Airplane on the ground below 50 kts. Which temperature sensor is used for TAT indication?. The CAC inlet temperature sensor. s.

*33.- Where is the trust management function software?. In the left and right common computing resource (CCR) cabinets. s.

34.- What function will automatically tune the VOR, ILS and DME. FMF (in the CCRs.). s.

35.- Which of the following units provides power to the INR (integrated navigation radio)?. PCM (power condition module) in to the FCE( flight control electronics). s.

36.- Which unit send the pilot/static information to the integrated standby flight director (ISFD). Center ADMs. s.

37.- Which are the model of the FMF (flight management function)?. Master, Hot spare and backup. a.

38.- A feature of the VOR antenna is: It receives these 3 signals VOR,ILS & GLS. a.

39.- The AOA units send the information af angle of attack to: flight control electronic (FCE). a.

40. wich-of the following statements regarding the AFF is true?. the AFF sends a signal to the INR to change localizer signal input from VOR antena to the ILS antenna. a.

41. If the ACP (audio control panel) of the Captain side fall, how can use the observer ACP with the Captain acoustc equipment, during flight?. Using the oserver audio override selector SW in the PS. a.