ata 34

The 4 __________ (FCE) cabinets provide manual and automatic control of the airplane pitch, roll and yaw axes. The FCE cabinets also provide manual and automatic control of the speedbrakes and leading and trailing edge high lift surfaces. a. Flight Computer Equipment. b. Flight Control Electronics. c. Flight Control Equipment.

Which of the following groups compose the B787 communication systems: a. Flight Interphone System, VHF Comm., DME, HF, SELCAL, SATCOM, Data Communication Management, ELT, Service Interphone, Flight Deck Entry Video. b. Flight Interphone System, VHF Comm., HF, SELCAL, SATCOM, Data Communication Management, ELT, Service Interphone, ADF, Flight Deck Entry Video. c. Flight Interphone System, VHF Comm., HF, SELCAL, SATCOM, Data Communication Management, ELT, Service Interphone, Flight Deck Entry Video.

Which computer processes and manage the B787 Pitot-Static Systems: a. Fight Computer Equipment - FCE. b. Flight Control Electronics - FCE. c. Air Data Computers – ADC.

The B787 __________ ERS calculates aircraft parameters such us heading, velocity and position. a. Earth Reference System. b. Elevation Reference System. c. Estimated Reference System.

The GPS, ILS, VOR and Marker Beacon system information is received and processed by the following component: a. Aircraft Receiver Radio – ARR. b. Integrated Navigation Radio – INR. c. Common Core System – CCS.

The ATC, TCAS, Weather Radar WXR, Terrain Awareness System –TAWS system information is received and processed by the following system: a. Integrated Surveillance System - ISS. b. Aircraft Surveillance System - ASS. c. Common Core System – CCS.

If GNSS (GPS) data is available, it is not necessary to enter an inertial position on the CDU POS INIT page. True. False.

The integrated standby flight display (ISFD) gets inertial data from: internal inertial sensors. the earth reference system.

The weather radar receiver transmitter modules (RTM) are: on the base of the antenna pedestal in the radome. in the forward EE bay.