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la racha amiga

COMENTARIOS ESTADÍSTICAS RÉCORDS
REALIZAR TEST
Título del Test:
la racha amiga

Descripción:
no bajar, mantener

Fecha de Creación: 2026/04/06

Categoría: Otros

Número Preguntas: 40

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the AOA units send the information of angle of attack to. FCE. CCS. ADM.

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

ISFD how does the ISFD get the heading and ground speed information ?. the ISFD itself by internal sensor. that information is supplied by the earth reference system (ERS) by a direct data bus. that information is supplied by the FCE c1.

airplane on the ground below 50 kts wich temperature sensor is used for TAT indication ?. the engine inlet temperature sensor. the CAC inlet temperature sensor. the TAT sensor.

the air data reference function is. in the air data modules. in the FCE, as softwere. in the attitude heading reference units.

how is call the unit, that makes the primary interface of the pilots and the AFF ?. MCP. CDU. EFIS/DSP.

How many backdrive units are installed in the autopilot system?. 3. 2. 1.

what function will automatically tune the VOR , ILS and DME ?. FMF IN THE CCR. DCAF IN THE CCR. AFF IN THE FCE.

which unit control the actuation of the backdrive actuator. ACE RH. ACE LH. ACE C2.

Where is shows the LRRA information ?. in EICAS display. In the PFD and HUD. in the ND.

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

which is the normal way to connect the autopilot functions ?. pushing the A/P switch on the control wheel horn. pushing the A/P switch in the MCP. autopilot engaged automatically during takeoff.

what is the airplene personality module (APM) main purpose ?. the APM connects AHRU and IRU digital information to the CDN. the APM converts digital signal into optical signal for ERS calculations. the APM provides mounting trays misaligment correction data.

where are located the FMF ?. in to CDN. in to the FCE. in to CCR.

The integrated standby flight display ISFD gets inetial data from. The earth reference system. internal inertial sensors. the GNSS system.

which units are used for the ADRF, to get information from the pitot/static probes ?. ADM. CCR. direct pneumatics lines to the FCE.

the terrain awareness and warning system (TAWS ) function includes. TCAS ans enhanced GPWS ( EGPWS). GPWS and ATC. GPWS and enhanced GPWS (EGPWS).

Which unit process the VOR function ?. INR. ISS processor units. in a softwere function in the CCR.

in the LNAV mode, where do the commands for the AFF comes from?. the master FMF. the ADRF. the pilot, heading or a track setting on the mode control panel.

the thrust management system function is part of. the CCS. the FCE. the flight management compurter.

what happens in a autopilot operations ( autopilot ON ), if the flight crew move the control wheel?. autopilot continues ON. autopilot disengaged. autopilot goes to approach/landing mode.

for flight purpose, when the A/P can be engaged ?. at 80 knots. only on cruise. when the airplane is above 200 feet ( R.A.).

The weather radar receiver transmitter modules (RTM) are. in the fwd EE bay. on the base off the antenna pedestal in the radome. in the after EE bay.

which are the modes of the FMF ?. master, hot spare and backup. primary, secundary and stanby. main, secundary and tertiary.

where does the ADM takes power?. PCM from the FCE. RPDU. PCM from the CCS.

Where is the autopilot, flight director and autothrottle mode shown?. CDU. FMA on the PFD. ND.

When does the ASA show these indications LAND 3, LAND 2 and NO AUTOLAND ?. during cruise. during take-off. during approach.

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

Which unit makes the surfaces commands in the FCE ?. FCM. ACE. PMC.

A feature of the VOR antenna is. it receives these 3 signals VOR, ILS & GLS. The VOR antenna get 12v dc from the INR receiver. the VOR antenna gets beam steering commands from the receiver.

in the ER system, what statement is true about IRU and AHRU?. The IRU and AHRU have the same performance and softwere load. the AHRU have decreased performance gyros and the same softwere load. the IRU and AHRU are completely different.

the marker beacon function is active in. right INR aptains instrument bus. left INR. firt official both INR cers instrument bus.

what are the Earth reference system components ?. they are 4 AHRU, 4 IRU and 2 APM. they are 2 AHRU, 2 IRU and 4 APM. they are 1 AHRU, 1 IRU and 2 APM.

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

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

which are the Autopilot disconect indications ?. 2 yellow master caution light, aural cautions, eicas cautions. 2 red master warning light, aural warning and Eicas warning. 2 A/P disengaged light, aural horn, and ststus MSG.

which of the following statements is true related to the TCAS/ATC antenna relays ?. allow to connect the traffic alert and collision avoidance system (TCAS) or distance mesure equipment (DME). connect either the left or right INR to the TCAS/ATC antennas. connect either the left or right ISSPU to the TCAS/ATC antennas.

what are the purpose of the GLS?. provides horizontal and vertical desviations to the autoflight system in all phases of flight. provides horizontal and vertical desviations for precision approach landing. provides lateral and longitudinal desviations to the autoflight system in all phases of flight.

the auto flight function softwere is. in the FCE. in the flight management computer. in the CCS.

VNAV is engaged which function sends thrurt target request data to the TMF?. the FMF. the PFCF. the AFF.

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