787 PRUEBA 3

WHAT IS THE ALTERNATE WAY TO DISENGAGE THE AUTOPILOT?. MODE CONTROL PANEL (MCP) DISENGAGE BAR IN THE DOWN POSITION. SELECTED FLAP IN 1 POSITION. PUSH THE A/P DISENGAGE SWITCH ON THE CONTROL WHEEL.

THE MARKER BEACON FUNCTION IS ACTIVE IN: RIGHT INR (INTENGRATED NAVIGATION RADIO). LEFT INR (INTEGRATED NAVIGATION RADIO). BOTH INR (INTEGRATED NAVIGATION RADIO).

THE INERTIAL REFERENCE UNITS (IRU) CALCULATE NAVIGATION (POSITION) DATA. WHAT DATA DO THE ALTITUDE HEADING REFERENCE UNITS (AHRU) NEED TO CALCULATE THIS NAVIGATION DATA?. PRESENT POSITION. GLS POSITION. GPS POSITION.

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

In the thrust management function (TMF), the thrust commands go to... The 3 auto flight functions in the flight control electronics (FCE). The 2 servo motors in the thrust control modulo (TCM). The 2 electronics engine control (EEC).

When does the autoland status annunciator (ASA) shows the level redundancy?. In all phases of flight and as soon as the autopilot is engaged. In approaching flight phase above 2500 ft and approach (APP) switch on the mode control panel (MCP) is selected. In approaching flight phase below 1500 ft and approach (APP) switch on the mode control panel (MCP) is selected.

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 control wheel back drive actuator (BDA). The rudder pedal back drive actuator (BDA).

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

What function will automatically tune the VOR, ILS and DME?. DCAF (in the CCR´s). AFF(in the FCE's). FMF(in the CCR's).

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

What is the first ADRF priority for the first officer air data?. C1 FCE voted for airspeed and altitude. R FCE voted for airspeed and altitude. C2 FCE voted for airspeed and altitude.

The airplane is on approach mode. The flight crew arms approach (APP). Which is the first antenna to receive the localizer (LOC) radio signals and send them to the INR?. Localizer approach antenna. Localizer track antenna. VOR capture antenna.

Where is the Autopilot, Flight Director and autothrottle mode Shown?. ND (Navigation Display). FMA (Flight Mode Annunciator) on the PFD (Primary Flight Display). CDU (Control Display Unit).

Where does the ADMs take power from?. +/-13.5v Power Condition Module (PCM) in the Common Computer Resource (CCR). +/-13.5v DC Power Condition Module (PCM) in the Flight Control Electronics (FCE). +/-13.5v DC Power Management Modules (PMM) in the Core Network Cabinet.

Where is the thrust management function sofware located?. FCM L, R and C1. ACE C2. L and R CCR.

What are the FCEs supplied by the right radio altimeter transceiver?. FCE R and C2. FCE L and C1. FCE R only.

Why is the "TO/GA" message at the top of the column green?. Because it is the ARME D mode. Because it is STANDBY mode. Because it is ENGAGED mode.

When does the Thrust Mnagement Function (TMF) provide full go-around thrust ?. When push both "TO/GA" switch at the same time. At the first push of the "TO/GA" switch. At the second push of the "TO/GA" switch.

What are the purpose of the air data module (ADM) program pins ?. To determine ADM type (pitot or static ) and location. To get power from the power control module (PCM) in the FCE cabinets. To send the data to the air data reference function (ADRF).

Which function are integrated in to ISS (Integrated Survellance System)?. ILS, GLS, GPS (GNSS). ATC, TCAS, WXR, TAWS (GPWS). FMF, ADRF, VOR.

Where is the Auto Flight Function Software?. In the Core Network cabinet. In the Flight Control Electronic (FCE). In the Common Core System (CCS).

The weather radar receiver transmiter module (RTM) are .... FWD EE BAY. NOSE RADOME. AFT EE BAY.

What supplies alttitude data to the integrated stardby flight display (ISFD)?. It has its own Inertial sensors to calculate pitch and roll alttitude. The common data network (CDN). The left IRU.

Which one of the 3 FMF software copies in the commonm computer resource is the master ?. The first FMF to power-up is the master FMF. Master condition is based on programming pin. The FMF in the right CCR cabinet is the master.

For Flight purposes, When the A/P can be engaged?. At 80 knots. When the airplane is above 200 feet (R.A.). Only on cruise.

Where do you perform a manual tuning and selection to VOR receivers?. CDU "NAV RAD" page. Backup Navigation menu on TCPs. Alternate EFIS panel on multifunction display.

Which of these functions are in the flight control modules (FCM)?. Air data reference function (ADRF). Thrust management function (TMF). Flight Management Function (FMF).

When the autopilot director system (AFDS), prvides de better fuel economy performance?. With A/T engaged manually or automatically. With autopilot engaged in VNAV and LNAV modes. With AP engaged above 200 ft.

Which are the modes of the FMF (Flight Management Function)?. Main, Secondary and Tertiary. Master, Hot spare and Backup. Primary, Secondary and Standby.

When the airplane is in the air the autopilot is engaged and then airplane rolls right. What moves the control wheel?. Control wheel backdrive actuator through ACE C2. Control wheel backdrive actuator through ACE C1. Control column backdrive actuator through ACE C2.

What LRU supplies ILS approach deviation data to the ISFD?. Left integrated navigation radio. Left integrated surveillance system. Left flight contrai electrnonic (FCE)C1.

What does the airplane use for the TAT value the airplane is in flight?. Simple average of TAT. Weighted average of EEC elements and TAT probes. Lower average of EEC elements and CAC ice protection system (CIPS).

When does the flight Management Function (FMF) send lateral guidance commands to the Auto Flight Function (AFF)?. When the LNAV mode engages. When the HDG/TRK select mode engages. When the VNAV mode engages.

The terrain 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 traffic control (ATC). Traffic collision avoidance system (TCAS)and Enhanced GPWS (EGPWS).

Which are the Autopilot disconnect indications?. 2 yellow Master Caution light, Aural cautions, Eicas Caution. 2 red Master Warning light, Aural Waening and Eicas Warning. 2 A/P disengaged light, Aural horm, and Status MSG.

The autopilot controls the airplane in all phases of flight, except: In go-around. In climb. In takeoff.

When does the Primary Flight Control Function (PFCF) accept Auto Flight Function (AFF) commands?. Only when the PFCFs are in the SECONDARY mode. Only when the PFCFs are in NORMAL mode. When the PFCFs are in ANY mode.

When the ISFD sends backup altitude, airspeed and atitude data to the common data network (CDN). This data is a backup if the common data network (CDN) fails. This data is a backup if all FCEs fail. This data is a backup if the FCE C2 fail.