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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.

3. The Marker Beacon function is active in: Right INR (Integrated 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 attitude 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 stering commands from the recalver. It receives these 3 signals: VOR, ILS & GLS. The VOR antenna get 12v de from the INR receiver.

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

When does the autoland status annunciator (ASA) shows the level of redundancy?. Inal phases of fight and as soon as the autopilot is engaged. In approaching flight phase above 2500 i 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 pitol/static system. They come from the center pitolistatic system.

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

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

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

13. 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).

15. 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 Module (PMM) in the Core Network Cabinet.

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

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

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

When does the Thrust Management Function (TMF) provide full go-around thrust?. When push both "TO/GA" switch at the sarne 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 modules (ADM) program pins?. To determine ADM type (pitot or static) and location. To get power from the power control modules (PCM) in the FCE cabinets. To send the data to the air data reference function (ADRF).

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

Where is the Auto FIght Function software's. ih the Core-Network Cabinet. in te Fight Control Electronic (FCE). the Common Core System (CCS).

The weather radar recoiver tranemitter modules (RTM) are.... FWDee bay. NOSE RADOME. AFTEE BAY.

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

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 programming pin. The FMF in the right CCR cabinet is the master.

For flight purposes, When the AP can be engaged?. At 80 knots. When the airplane is above 200 feet (R.A.). Only on cuise.

Where do you perform a manual tuning and course selection to VOR recelvers?. CDU "NAV RAD" page. Backup Navigation menu on TCPs. Alternate EFIS panei on multitunction displays.

28. Which of these functions are in the fight contrai modules (FCM)?. Air data reference function (ADRF). Thrust management function (TMF). FIght Management Function (FMF).

When the autopilot flight director system (AFDS), provides de better fuel economy performance?. With AT engaged manually or automatically. With autopilot engaped in VNAV and LNAV modes. With AP engagea 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 and the autopilot is engaged and the 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 electronic (FCE) C1.

33. What does the airplane use for the TAT value when 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 red Master Warning light, Aural Warning and Eicas Warning. .

The autopilot controls the airplane attitude in all phases of flight, except: In takeoff. .

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

Where is shows the LRRA information?. C (En la imagen, el círculo rojo "C" señala la zona del radio altímetro en el PFD). .

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