B787 2exam

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 PITOS/TAATIC SIGNALS FOR ISFD COME FROM?. THEY COME FROM THE CENTER PITOT/TATIC SYSTEM. THEY COME FROM THE LEFT PITOT/TATIC SYSTEM. THEY COME FROM THE RIGHT PITOT/TATIC SYSTEM.

ISFD. HOW DOES THE ISFD GET THE HEADING AND GROUND SPEED INFORMATION?. THAT INFORMATIION IS SUPPLIED BY THE FLIGHT CONTROL ELECTRONICS (FEC) C1. THE ISFD IT SELF BY INTERNAL SENSORS. THAT INFORMATION IS SUPPLIED BY THE EARTH REFERENCE SYSTEM.

AIRPLANE ON THE GROUND BELOW 50 KTS, WHICH TEMPERATURE SENSOR IS USED FOR TAT INFORMATION?. THE CAC INLET AIR TEMPERATURE SENSOR. THE ENGINE INLET TEMPERATURE SENSOR. THE TAT SENSOR.

THE AIR DATA REFERENCE FUNCTION IS: IN THE FLIGHT CONTROL ELECTRONICS (FCE) AS A SOFTWARE. IN THE AIR DATA MODULES. IN THE ATTITUDE HEADING REFERENCE UNITS.

HOW IS CALL THE UNIT, THAT MAKES THE PRIMARY INTERFACE OF THE PILOTS AND THE AFF (AUTO FLIGTHTM FUNCTION)?. MCP. EFIS/DSP. CDU.

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

WHAT FUNCTION AUTOMATICALLY TUNE THE VOR, ILS AND DME?. FMF (IN THE CCRs). DCAF (IN THE CCRs). AFF (IN THE FCEs).

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

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

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

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

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

WHERE ARE LOCATED THE FMF (FLIGHT MANAGEMENT FUNCTION)?. IN TO CCR (COMMON COMPUTER RESOURCE). IN TO CDN (COMMON DATA NETWORK). IN TO FCE (FLIGHT CONTROL ELECTRONIC).

THE INTEGRATED STAND BY FLIGHT DISPLAY (ISFD) GETS INERTIAL DAATA FROM: INTERNAL INERTIAL SENSOR. THE EARTH REFERENCE SYSTEM. THE GNSS SYSTEM.

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

THE TERRIN AWARENESS AND WARNING SYSTEM (TAWS) FUNCTION INCLUDES: BASIC GROUND PROXIMITY WARNING SYSTEM (GPWS) AND ENHANCED GPWS (EGPWS). BASIC GROUND PROXIMITY WARNING SYSTEM (GPWS) AND AIR TRAFIC CONTROL (ATC). TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS) AND ENHANCED GPWS (EGPWS).

WHICH UNITS PROCESS THE VOR FUNCTION?. INR (INTEGRATED NAVIGATION RADIO). ISS PROCESSOR UNIT. IN A SOFTWARE FUNCTION IN THE CCR.

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

THE THRUST MANAGEMENT SYSTEM FUNCTION IS A PART OF: THE COMMUN CORE SYSTEM (CCS). THE FLIGHT CONTROL ELECTRONICS (FCE). THE FLIGHT MANGEMENT COMPUTER (FMC).

WHAT HAPPENDS IN A AUTOPILOT OPERATIONS (AUTOPILOT ON), IF THE FLIGHT CREW MOVE THE CONTROL WHEEL?. AUTOPILOT DISENGANGED. AUTOPILOT CONTINUES ON. AUTOPILOT GOES TO APPROACH/LANDING MODE.

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

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

WHICH ARE THE MODES OF THE FMF (FLIGHT MANAGEMENT FUNTION )?. MASTER, HOT SPARE AND BACK UP. PRIMARY, SECUNDARY AND STAND BY. MAIN, SECUNDARY AND TERTIARY.

WHERE DOES THE ADM (AIR DATA MODULE) TAKES POWER?. PCM (POWER CONTITION MODULE) FROM THE FCE (FLIGHT CONTROL ELECTRONIC). RPDU (REMOTE POWER DISTRIBUTION UNIT). PCM (POWER CONDITION MODULE) FROM THE CCS (COMMON CORE SYSTEM).

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

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

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

WHICH UNIT MAKES THE SURFACES COMMANDS IN THE FCE (FLIGHT CONTROL ELECTRONICS)?. ACE. FCM. PCM.

A FEATURE OF THE VOR ANTENNA IS: IT RECEIVES THESE 3 SIGNAL: VOR, ILS AND GLS. THE VOR ANTENNA GET 12 VDC 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 AHRUs HAVE DECREASED PERFORMANCE GYROS AND THE SAME SOFTWARE LOAD. THE IRUs AND AHRUs HAVE THE SAME PERFORMANCE AND SOFTWARE LOAD. THE IRUs AND AHRUS ARE COMPLETELY DIFFERENT.

THE MARKER BEACON FUNCTION IS ACTIVE IN: LEFT INR (INTEGRATED NAVIGATION RADIO). FIRST OFFICER BOTH INR (INTEGRATED NAVIGATION RADIO) INSTRUMENT BUS. RIGHT INR (INTEGRATED NAVIGATION RADIO) CAPTAIN INSTRUMEN BUS.

WHAT ARE THE EARTH REFERENCE SYSTEM COMPONENTS?. THEY ARE 2 AHRU, 2 IRU AND 4 APM. THEY ARE 4 AHRU, 4 IRU AND 4 APM. THEY ARE 1 AHRU, 1 IRU AND 2 APM.

ERS. ONE AIRPLANE PERSONALITY MODULE (APM) HAS FAILED. AND ITS REPLACED, CHOOSE FROM THE FOLLOWING: THE RELATED IRU OR AHRU SENDS THE STORED MISALIGNMENT DATA TO THE NEW APM. THE NEW APM BRINGS THE MISALIGMENT DATA FOR -8 OR -9 CONFIGURATION. A PROCEDURE WITH A RAMP TEST TO PROGRAMMING THE NEW APM FOR IRU OR AHRU CAN BE PERFORMED.

THE B-787 HAS 3 BACK DRIVE ACTUATORS, WHICH OF THEM DOES NOT WORK IN THE CRUISE PHASE. THE RUDDER PEDAL BACK DRIVE ACTUATOR (BDA). THE CONTROL COLUMN BACK DRIVE ACTUATOR (BDA). THE CONTROL WHEEL BACK DRIVE ACTUATOR (BDA).

WHICH ARE THE AUTOPILOT DISCONECT INDICATIONS?. 2 RED MASTER WARNING LIGHT, AURAL WARNING AND EICAS WARNING. 2 YELLOW MASTER CAUTION LIGHT, AURAL CAUTION AND EICAS CAUTION. 2 A/P DISENGAGED LIGHT, AURAL HORN AND STATUS MSG.

WHICH OF THE FOLLOWING STATEMENTS IS TRUE RELATED TO THE TCAS/ATC ANTENNA RELAYS. CONNECT EITHER THE LEFT OR RIGHT INTEGRATED SURVILLANCE SYSTEM PROCESSOR UNIT (ISSPU) TO THE TCAS/ATC ANTENNAS. ALLOW TO CONNECT THE TRAFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) OR DISTANCE MESURE EQUIPMENT (DME). CONNECT EITHER THE LEFT OR RIGHT INTEGRATED NAVIGATION SYSTEM (INR) TO THE TCAS/ATC ANTENNAS.

WHAT ARE THERE THE PURPOSE OF THE GLOBAL NAVIGATION SATELLITE SYSTEM (GLS). PROVIDES HORIZONTAL AND VERTICAL DEVIATIONS FOR PRECISION APPROACH LANDING. PROVIDES HORIZONTAL AND VERTICAL DEVIATIONS TO THE AUTOFLIGHT SYSTEM IN ALL PHASES OF FLIGHT. PROVIDES LATERAL AND LONGITUDINAL DEVIATIONS TO THE AUTOFLIGHT SYSTEM IN ALL PHASES OF FLIGHT.

THE AUTOFLIGHT FUNTION SOFTWARE IS: IN THE FLIGHT CONTROL ELECTRONICS (FCE). IN THE FLIGHT MANAGEMENT COMPUTER. IN THE COMMON CORE SYSTEM (CCS).

VNAV IS ENGAGED. WHICH FUNTION SENDS THRUST TARGET REQUEST DATA TO THE TMF?. THE FLIGHT MANAGMENT FUNTION (FMF). THE PRIMARY FLIGHT CONTROL FUNCTION (PFCF). THE AUTOLFLIGHT FUNCTION (AFF).