787 examen (3)

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

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

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

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 LIN GPS altitude. ISFD ALTITUDE and GPS airspeed.

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

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).

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

When the ISFD sends backup attitude, airspeed and altitude 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.

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

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

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

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

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

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

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

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

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

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

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

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

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.

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 capture antenna. Localizer approach antenna. Localizer track antenna.

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

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

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

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

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.

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

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. GPS position. GLS position.

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

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

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

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

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

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

When does the Thrust Management 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 does the "LAND 3" message on the Autoland Status Annunciator (ASA) indicate?. LAND 3 shows when the level of redundancy is such that one fault cannot cause a deviation from the flight path. 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.

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

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 HDG HOLD. Pitch mode is V/S and roll mode is ATT.