787 examen 3

How can be disarmed the Autotrotile function?. From CDU (Control Display Unit). From Throtlle lever switch. From Wheel Control SW.

INR. Where is the ILS localizer track antenna located?. The ILS localizer track antenna is located at vertical fin. The ILS localizer track antenna is located behind the radome. The ILS Localizer track antenna is located below the fuselage between nose and main landing gear.

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).

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

Which sensor uses the ADRF when the groundspeed is less than 50 knots?. Engines have inlet air temperature sensors. Total air temperature (TAT) prob. Cabin air compressor (CAC) inlet temperature.

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 module (TCM). The 2 electronic engine control (EEC).

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

The purpose of the suppressor pulse (ATC, TCAS and DME) is: To prevent simultaneous transmissions. To prevent simultaneous receptions. To prevent damage to the receivers.

In the LNAV mode, Where do the commands for the AFF (Auto flight Function) come from?. The air data reference function (ADRF). The pilot, heading or a track setting on the mode contro panel (MCP). The master flight management function (FMF).

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.).

ERS. One airplane personality module (APM) has failed, and it is replaced, choose from the following: A procedure with a ramp test to programming the new APM for IRU or AHRU can be performed. 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.

The left LRRA transceiver sends RA data to: FCE left and FCE C1. FCE left, right, FCE C1 and C2. FCE right and FCE C2.

PFD and HUD shows ADR speed, if there is a speed failure: Change automatically to GPS speed. Change automatically to AOA speed. Change manually through ALT source select switch to TAT speed.

Which flight controls provides sideslip for runway alignment function?. Rudder and slats. Rudder and ailerons. Stabilizer trim and spoilers.

INR. How does the ground based augmentation system (GBAS) send correction data to the airplane?. It sends correction data on a VHF datalink broadcast (VDB) signal. It is modulated together with the ILS signal. It is mixed with the GNSS/GPS signal and send via HF system.

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

DME. When will the DME data be shown on the primary flight display (PFD)?. After tuning ILS, if airport has ILS/DME paired, the slant range will appear on PFD. The DME data is shown only when a VOR/DME is tuned, and appears on navigation display (ND). After failure of one ME interrogator, the system is degraded, by that reason slant range appears on PFD.

TAT probe analog data goes to a remote data concentrator (RDC), then is sended to: Common data network (CDN) then to air data reference función (ADRF). Air data modules (ADM) for the air data reference system (ADRS). Actuator control electronics (ACE) then to air data reference system (ADRS).

Where does the air data modules (ADM) takes power?. Power control modules in the Common Core System. Power ontrol modules in the Core Network System. Power control modules in the Flight Control Electronics.

INR. How does the INR change from ILS capture to ILS track antenna?. The autoflight function in the FCE cabinets sends a signal to the INR to change to the localizer track antenna. This is performed manually by the pilot after the ILS localizer capture to change to the localizer track antenna. During the ILS capture, this is performed automatically by the INR to change to the localizer track antenna.

Which are the Autopilot disconect indications?. 2 yellow Master Caution light, Aural cautions, Eicas caution. 2 A/P Disengaged light, Aural horn, and Status MSG. 2 red Master Warning light, Aural Warning and Eicas Warning.

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

In which component of the FCE cabinets is located the Auto Flight Function (AFF)?. FCM. PCM. ACE.

Through which unit, is the usual way to disconnect the autopilot during cruise?. Rudder Pedals. Glareshield Warning/Caution reset switch. Autopilot disconect switch on the control wheel horn.

If all FCEs fail. What happens with the inertial and air data?. All the EFIS information is lost, inertial and air data flags will be on view, no backup is possible. The left Integrated Nav Radio (INR) sends the backup and air data to the common data network. The ISFD sends backup inertial and air data to the common data network (CDN).

There are 4 flight control electronics (FCE) cabinets. How many of them have a copy of the AFF (Auto flight Function)?. 3. 2. 4.

Where is the thrust management function software?. In the left and right common computing resource (CCR) Cabinets. In the left and right Flight Control Electronic (FCE) cabinets. In the left and right Core network cabinets.

The angle of attack sensors sense the difference between the wing chord line and the direction of the airflow and send it to: AOA support function in the Common Core System (CCS). AOA support function in the flight control modules (FCM). AOA support function in the Core Network System.

When the autopilot is engaged, what moves the control wheel?. The are no flight controls feedback at autopilot engage. The wheel backdrive actuator. The Flight Control Electronic FCE C1 moves directly the flight controls.

The MCP has 2 processor lanes (A and B). Which statement is true about this?. One lane is the master, the other is the slave. Both lanes work simultaneously. One lane is for auto flight function (AFF), the other is for thrust management function (TMF).

From where the air traffic control (ATC) function receives barometric altitude data?. Air data reference function (ADRF) in the flight control electronics (FCE). Alerting and transponder control panel. Air data reference function (ADRF) in the common data network (CDN).

Which of the following statement are correct related to the functions of thrust management function (TMF)?. Autothrottle (A/T) function (includes thrust reverse trim equalization). Thrust limit calculations and Autothrottle (A/T) function (includes engine trim equalization). Thrust limit calculations and cross wind thrust compensation.

How many lanes has the mode contro panel (MCP)?. 3 lanes left, right and C1. 2 lanes A and B. 1 lanes C2.

What happens if A/P is engaged and pilot selects VNAV and LNAV modes?. The selection of those modes at the same time is not accepted by the AFDS. The AP provides control of pitch, roll and yaw. The FMF sends commands to A/P, A/T, F/D according to the selected flight plan, with better performance.

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

Which units in the control columns, control wheels and pedals rudder, provides control feedback to the crew, when the autopilot function is engaged?. Column Position transducer. Backdrive units. The control columns control does not move during autopilot operation.

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

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

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