exam 2 787

The AOA units send the information of angle of attack to: Flight Control Electronic - FCE. Common Core System - CCS. Air Data Module - ADM.

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

How does the ISFD get the heading and ground speed information?. The ISFD itself by internal sensors. That information is supplied by the earth reference system ERS by a direct data bus. That information is supplied by the flight control electronic FCE C1.

Airplane on the ground below 50 kts, whitch temperature sensor used for TAT indication?. The engine inlet temperature sensor. The CAC inlet temperature sensor. The TAT sensor.

The air data reference function es: In the air data modules. In the flight control electronic FCE, as software. In the altitude heading reference unit.

How is call the unit, that makes the primary interface of the pilots and the AFF ( Auto flight Function)?. MCP. EFIS/DSP. CDU.

HOW MANY BACKDRIVE UNITS ARE INTALLED IN THE AUTOPILOT SYSTEM?. 3. 2. 1.

WHAT FUNCTION WILL AUTOMATICALLY TUNE THE VOR,ILS AND DME?. FMF (IN THE CCR´S). DCAF (IN THE CCR´S). AFF (IN THE FCE´S).

WHICH UNITS CONTROLS THE ACTUATION OF THE BACKDRIVE ACTUATOR?. ACE RH. ACE LH. ACE C2.

WHRE IS SHOWS THE LRRA INFORMATION?. IN EICAS DISPLAY. IN THE PFD AND HUD. IN THE ND.

WHITCH ONE OF THE 3 FMF SOFTWARE COPIES IN THE COMMON COMPUTER RESOURCE IS THE MASTER?. MASTER CONDITION IS BASED ON PROGRAMMING PIN. THE FIRST FMF TO POWER-UP IS THE MASTER FMF. THE FMF IN THE FLIFHT CCR CABINET IS THE MASTER.

WHICH IS THE NORMAL WAY TO CONNECT THE AUTOPILOT FUNCTIONS?. PUSHING THE A/P SWITCH ON THE CONTROL WHEEL HORN. PUSHING THE A/P SWITCH IN THE MCP. AUTOPILOT ENGAGED AUTOMATICALLY DURING TAKEOFF.

WHAT IS THE AIRPLANE PERSONALITY MODULE (APM) MAIN PURPOSE?. THE APM CONECT AHRU AND IRU DIGITAL INFORMATION TO THE CDN. THE APM CONVERTS DIGITAL SIGNAL INTO OPTICAL SIGNAL FOR ERS CALCULATIONS. THE APM PROVIDES MOUNTING TRAYS MISALIGNMENT CORRECTION DATA.

WHERE ARE LOCATED THE FMF (FLIGHT MANAGEMENT FUNCTION)?. IN TO CDN. IN TO THE FCE. IN TO CCR.

THE INTEGRATED STANDBY FLIGHT DISPLAY (ISFD) GETS INERTIAL DATA FROM?. THE EARTH REFERENCE SYSTEM. INTERNAL INERTIAL SENSORS. THE GNSS SYSTEM.

WHICH UNIT ARE USED FOR THE ADRF, TO GET INFORMATION FROM THE PITOT/STATIC PROBES?. DIRECT PNEUMATICS LINES TO THE FCE. ADM. CCR.

THE TERRAIN AWARENESS AND WARNING SYSTEM (TAWS) FUNCTION INLCUDES: TRAFFIC COLLISION AVOINDANCE SYSTEM (TCAS) AND ENHANCED GPWS (EGPWS). BASIC GROUND PROXIMITY WARNING SYSTEM (GPWS) AND AIR TRAFFIC CONTROL (ATC). BASIC GROUND PROXIMITY WARNING SYSTEM (GPWS) AND ENHANCED GPWS (EGPWS).

WHICH UNITS PROCESS THE VOR FUCTION?. INR (Integrated Navigation Radio). ISS Processor units. in a software function in the CCR.

IN THE LNAV MODE, WHERE DO THE COMMANDS FOR THE AFF (AUTO FLIGHT FUNCTION) COME FROM?. THE MASTER FLIGHT MANAGEMENT FUNCTION (FMF). THE AIR DATA REFERENCE FUNCTION (ADRF). THE PILOT, HEADING OR A TRACK SETTING ON THE MODE CONTROL PANEL (MCP).

THE THRUST MANAGEMENT SYSTEM FUNCTION IS PART OF: THE COMMON CORE SYSTEM (CCS). THE FLIGHT CONTROL ELECTRONICS (FCE). THE FLIGHT MANAGEMENT COMPUTER.

WHAT HAPPENS IN A AUTIPILOT OPERATIONS (AUTOPILOT ON), IF THE FLIGHT CREW MORE THE CONTROL WHEEL?. AUTOPILOT CONTINUES ON. AUTOPILOT DISENGAGED. AUTOPILOT GOES TO APPROACH.

FOR FLIGHT PURPOSES, WHEN THE A/P CAN BE ENGAGED?. AT 80 KNOTS. ONLY ON CRUISE. WHEN THE AIRPLANE IS ABOVE 200 FEET (R.A).

THE WEATHER RADAR RECEIVER TRANSMITTER MODULES (RTM) ARE: IN THE FORWARD EE BAY. ON THE BASE OF THE ANTENNA PEDESTAL IN THE RADOME. IN THE AFTER EE BAY.

WHICH ARE THE MODES OF THE FMF ( FLIGHT MANAGEMENT FUNCTION). MASTER, HOT SPARE AND BACKUP. PRIMARY, SECUNDARY AND STANBY. MAIN, SECUNDARY AND.

WHERE DOES THE ADM (AIR DATA MODULE) TAKES POWER?. PCM FROM THE FCE. RPDU. PCM FROM THE CCS.

WHERE IS THE AUTOPILOT, FLIGHT DIRECTOR AND AUTOTHROTTLE MODE SHOWN?. CDU ( CONTROL DISPLAY UNIT). FMA (FLIGHT MODE ANUNCIATOR) ON THE PFD. ND (NAVEGATION DISPLAY).

WHEN DOES THE ASA SHOW THESE INDICATIONS: LAND 3, LAND 2, AND NO AUTOLAND?. DURING CRUISE. DURING TAKE-OFF. DURING APPROACH.

WHICH FUNCTION ARE INTEGRATED IN TO THE ISS (INTEGRATED SURVEILLANCE SYSTEM). ATC, TCAS, WXR, TAWS (GPWS). ILS, GLS, GPS (GNSS). FMF, ADRF, VOR.

WHICH UNIT MAKES THE SURFACES COMMANDS IN THE FCE?. FMC. ACE. PMC.

A FEATURE OF THE VOR ANTENNA IS: IT RECIVES THESE 3 SIGNALS: VOR,ILS & GLS. THE VOR ANTENNA GET 12V DC FROM THE INR RECEIVER. THE VOR ANTENNA GETS BEAM STEERING COMMANDS FROM THE RECEIVER.

IN THE ER SYSTEM, WHAT STATEMENT IS TRUE ABOUT IRUs AND AHRUs?. The IRUs and AHRUs have the same performance and software load. The AHRUs have decreased performance gyros and the same software load. The IRUs and AHRUs are completely different.

The marker Beacon function is active in: Right INR (Integrated navegation radio) Captains Intrument Bus. Left INR. First OFFICER both INR cers. Intrument bus.

What are the Earth Reference System components?. They are 4 AHRU, 4 IRU and 4 APM. They are 2 AHRU, 2 IRU and 4 APM. They are 1 AHRU, 1 IRU and 2 APM.

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

The B-787 has 3 back drive actuators, which of them does not work in the cruise phase?. The control column back drive actuator (BDA). The rudder epdal back drive actuator (BDA). The control wheel back drive actuator (BDA).

Which are the autopilot disconect 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.

Which of the following statements is true related to the TCAS/ATC antenna relays?. Allow to connect the traffic alert and collision avoidance system TCAS or distance mesure equiqment (DME). Connect either the left or right integrated navigation system INR to the TCAS/ATC antennas. Connect either the left or right integrated surveillance system processor unit (ISSPU) to the TCAS/ATC antennas.

What are the purpose of the gobal navigation satellite system (GLS)?. Provides horizontal and vertical deviations to the autoflight system in all phases of flight. Provides horizontal and vertical deviations for precision approach landing. Provides lateral and longitudinal deviations to the autoflight system in all phases of flight.

The auto flight function software is. In the flight control electronic (FCE). In the flight management computer. In the common core system (CCS).

VNAV is engaged, Which function sends thrust target request data to the TMF?. The flight management function (FMF). The primary flight control function (PFCF). The autoflight function (AFF).