93%

SATCOM the diplex low noise amplifier (DLNA). lets the SATCOM system receive and transmit signals at the same time (full duplex). amplifies olny the transmitted SATCOM signal to increase output power. supplies electrical power to the SATCOM antenna and modem.

Which units process the VOR funtion. PCM ( power condition module). FCE ( fligh control electronics). INR ( integrated navignation radio).

Where does the ADM takes power. PCM ( power condition module) from the FCE ( flight control electronic). From the generator control unit (GCU). Directly from the main battery.

The auto flight funtion software is. In the flight management computer. In the air data module. In the power condition module.

Which of the followings statements regarding the AFF is true. The AFF controls the weather radar antenna. The AFF sends a signal to changes MB antenna from the Left INR to the Right INR. The AFF supplies electrical power to the INR.

When the WXR system comes on and transmits in the PWS ( predictive windshear) mode. When N1 is at least 10%. When N1 is at least 80%. When N1 is at least 60%.

Which unir are used for the ADRF to get information from the Pitot/Static probes. ADM. AGU. FCE.

SETCAL in which unit are located the "SETCAL" decoder function. In the AGUs. In the ADMs. In the CSSC.

In the ER system what statements is true about IRUs and AHRUs. The AHRUs only provide GPS pisition data. The IRUs are powered only by the APU. The AHRUs have decreased performance gyros and the same software load.

Which unit send the Pitot/Static information to the integrated standby flight director ( ISFD). Left ADMs. Center ADMs. Right ADMs.

The marker beacon funtion is active in. Air data module (ADM). Flight control electronis (FCE). Left INR ( integrated navigation radio).

Which is the central control unit in the cabin system. CSSC ( Cabin Service System Controller). CCS ( Common Core System). AGU ( Audio Gareway Unit).

Where is the AutoPilot, Flight Director and AutoThrottle mode show. ND ( navegation display). FMA ( flight mode annuncaitor) on the PFD ( primary flight display). EICAS ( engine indication and crew alerting system).

Which one of the 3 FMF software copies in the common computer resource is the master. The center FMF is always the master. The left FMF is always the master. The First FMF to power-up is the master FMF.

Which are located the FMF( flight management function). In the FCE (Flight Control Electronics). In the INR ( Integrated Navegation Radio). In to CCR ( Common Computer Resource).

How could be activeted the ELT system. Manually from ELT control panel or Automatically from G Switch. Only manually from the FMC. Automatically when the weather radar detects turbulence.

Wich functions are Integrated in the ISS (Integrated Surveillance System). SATCOM, HF, VHF, SETCAL. VOR, DME, ILS. ATC, TCAS, WXR, TAWS (GPWS).

What kind of HF antenna is used in the 787-9. It is a wire type antenna. It is a loop type antenna. It is a blade type antenna.

The AOA units send the information of angle of attack to. Power Condition Module (PCM). Flight Control Electronics (FCE). Air Data Module (ADM).

What function will automatically tune the VOR, ILS, and DME. FMC. AHRS, IRU. FMF ( in the CCRs).