93% part2
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Título del Test:
![]() 93% part2 Descripción: 20 preguntas |



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What is the back-up power supply source for the AHRU/IRU. The hot battery bus. The Maine battery bus. The central battery. Where is shows the LRRA information?. Only in the PFD. In the PFD and HUD. In the EICAS. The power for the emergency lights come from. WELS control units (WCU) batteries. Hot battery bus. Maint battery bus. A feature of the vor antenna is: It receives these 2 signals: VOR, ILS. It receives these 3 signals: VOR, ILS and GLS. Only receives the signal GLS. Where Can you control the emergency lightting system?. From p5. From p5 or master attendant switch panel (ASP). Only for master attendant switch panel (ASP). Which of the followings units procedes power to the INR (integrated radio navegation). PCM (power condition module) in to the FCE (flight control electronics). Only in the PCM (power condition module). PSM (passenger service module). The B-787 has 3 back drive actuators, which of them Ford not work in the cruiser phase?. The rudder pedal back drive actuator (BDA. The center back drive actuator (BDA. The left back drive actuator (BDA. Airplane on the ground below 50kts, which temperature sensor is used for TAT indication?. The CAC inlet temperature sensor. The Tube pitot temperature sensor. The air total temperature sensor. What is the airplane personality and module (APM) main porpuse?. The APM is used for thrust limit calculation. The APM provides mounting trays misalingment correction data. The APM provides misalingment correction data. Which are the modes of the FMF (flight management function)?. Master, hot spare and backup. Hot spare. Its a backup. Which the followings statements regarding the DME is true?. Can be tuned 5 DME ground stations at the same time. Can be tuned 3 DME ground stations at the same time. Only Can be used one tuned DME ground station at the same time. Where is the ADRF located?. This function is part of FCM. This function is part of the PFD. This function is part of The FMF. If the ACP (audio control panel) of the captain side fail, how can use the observer ACP with the captain acoustic equipment, during flight?. Using the turning control panel. Using the observer audio override selector SW in the p8. Using the left audio control Panels. Where is the thrust management function software?. In the left and right common computing resource (CCR) cabinets. In the left common computing resource (CCR) cabinets. In the right common computing resource (CCR) cabinets. The cabin attendant handset has interface with. A CZU ( cabin zone unit). Turning control panel. Passenger service module (psm). Where are the volumen control for the speakers in the flight deck. In the audio control panels. In te tuning control panels. In the P5. The frecuency of HF and VHF communications system is selected throug?. Turning control panels. Audio control panels. P8. Which the followings statement are corrected releated to the functions of thrust management function (TMF). Thrust limit calculations and the auto throttle (A/T) function (includes engine trim equalizations). Auto throttle. Thrust limit. Which are the autopilot disconnect indications?. 2 red master warning light, aural warning and EICAS warning. EICAS warning. Master warning light and EICAS warning. What happens if A/P is engaged and pitot selects VNAV And LNAV modes?. The FMF sends commands to A/P, A/T, F/D according to the select flight plan with better performance. The FMF sends commands to A/P, A/T. The FMF sends commands to A/P according to the select flight plan with better performance. |




