Full examen 3

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.).

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

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.

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.

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

How can be disarmed the Autotrotile function?. From CDU (Control Display Unit). From Throttle 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.

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

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 control panel (MCP). The master flight management function (FMF).

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).

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.

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 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.

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).

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 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).

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.

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.

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.

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 Thrust Management System function is part of: The flight management computer. The flight control electronics (FCE). The common core system (CCS).

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.

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 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.

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).

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.

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.

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

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

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.

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 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.

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.

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.

The inertial reference units (IRU) calculate navigation (position) data: What data do the attitude heading reference units (AHRU) need to calculate this navigation data?. GPS position. Present position. GLS position.

Where is the VOR displayed?. Navigation Displays (ND) selected in the pull-down menu. Integrated Standby Flight Display (ISD). Primary Flight Display (PFD).

Which of the following navigation systems have alternate tuning?. VOR. GLS. MKR.

Where is the setting for barometric correction (QNH/QNE), if an EFIS/DSP control panel fails?. Control Display Unit (CDU). Electronic Flight instrument System/Display Selector Panel (EFIS/DSP). Alternate EFIS/DSP control on MFD.

What are the alternative ways to disengage the autopilot?. Push the A/P disengage switch on the control wheel. Selected flap in 1 position. Mode Control Panel (MCP) disengage bar in the down position.

When does the A/P engage the yaw control and automatic control of the rudder control surface?. When the A/P engages in autoland conditions. When the A/P engages in cruise or autoland conditions. When the A/P engages in cruise conditions.

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

Where is the DME/ILS displayed?. PFDs and HUDs. PFDs and NDs. ND and HUDs.

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

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

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

The airplane is in the air. The captain puts the AIR DATA/ATT switch to the ALTN position. What is the source of this data on the captain PFD?. R FCE voted for airspeed and altitude. L FCE synthetic airspeed and L INR GPS altitude. ISFD ALTITUDE and GPS airspeed.

What does the "LAND 3" message on the Autoland Status Annunciator (ASA) indicate?. LAND 3 shows when there is no automatic landing function available in the autopilot system. LAND 3 shows when the level of redundancy is such that one fault cannot prevent the autopilot system from making an automatic landing. LAND 3 shows when the level of redundancy is such that one fault cannot cause a deviation from the flight path.

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

Where does the right INR take power from?. PCM 2 right CCR. Right 28v DC Main Bus. PCM FCE C2.

Where is the center static port located?. A. B. C.

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

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 capture antenna. Localizer track antenna.

Which of the following modes engage the A/T automatically?. Takeoff/go-around (TO/GA). Lateral navigation (LNAV). Altitude Hold (ALT HLD).

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 C1. Control column backdrive actuator through ACE C2. Control wheel backdrive actuator through ACE C2.

How does the ADRF compute aircraft speed?. From left, center and right pitot pressure and static port pressure. From left, center and right ADMs total pressure and ADMS static pressure. From left, center and right voted total pressure and voted static pressure.

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

When the airplane has power, you need to engage the autopilot on the ground for test purposes. What must you do?. Select flaps to full extent. Pressurize the hydraulic system. Select flaps up.

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

Which one is part of the integrated surveillance system (ISS)?. Radio altitude (RA). Instrument landing system (ILS). Air traffic control (ATC).

Where does the ADMs take power from?. +/- 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. +/- 13.5v Power Condition Module (PCM) in the Common Computer Resource (CCR).

What LRU supplies ILS approach deviation data to the ISF D?. Left integrated surveillance system. Left flight control electronic (FCE) C1. Left integrated navigation radio.

What does the Auto Flight Function (AFF) send its pitch, roll and yaw AP commands to?. The Flight Control Surfaces directly. The Actuator Control Electronics (ACE's). The primary flight control function (PFCF).

"ON BAT" light illuminated means: One or more of the IRU supplied from SPDU power. One or more of the IRU supplied from battery power. One or more of the IRU supplied from RPDU.

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

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. This data is a backup if the common data network (CDN) fails. This data is a backup if the FCE C2 fail.

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

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. This data is a backup if the common data network (CDN) fails. This data is a backup if the FCE C2 fail.

Where is the localizer track antenna located?. A. B. C.

Where do you select the weather radar test?. EFIS control panel. WXR TEST on TCPs. ND weather radar (WXR) pull-down menu on NDS.

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

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

Which of these functions is in the integrated navigation radio (INR)?. TAWS. Distance measuring equipment (DME). Marker beacon.

Where does the ISFD receive total pressure from?. The ISFD receives total pressure from center ADM. The ISFD receives total pressure from the common data network (CDN). The ISFD receives total pressure from the center pitot probe.

Why is the target thrust cursor magenta?. Because the flight management function (FMF) makes the thrust limit. Because the pilot makes the thrust limit by the Flight Control Unit (FCU). Because the thrust management system (TMS) makes the thrust limit.

During climb, in which modes does the A/P engage if the bank angle is greater than 5 degrees?. Pitch mode is V/S and roll mode is ALTITUDE HOLD. Pitch mode is V/S and roll mode is ATT. Pitch mode is V/S and roll mode is HDG HOLD.