3OING N1 2 PART

how de CMCFs operate. both CMCF operates at the same time. only one CMCF oparates at a time alternating between them on each flight. only one CMCF operate at time the other CMCF is a backup.

how many copies of DCAF sorfware are there on the B787. there are only 1 copy of the DCAF software. there are 4 copies of the DCAF softwere. there are 2 copies of the DCAF softwere.

the CCS provides. improved reliability, decreased cost and weight. decreased cost only. better airplane aerodynamic performance.

what is the airplane condition monitoring function (ACMF) purpose. short term and transit troubleshooting. ramp and transit troubleshooting. engine performance airplane systems performance and trend analysis of maintenance data.

what program do you use to loard the loadable softwere airplane part ( LSAP) from file server module to airplane system. ODLF. OSM. CMCF.

what happens if you press the common core system ( ccs ) guarded RESET switches. this action allows reset only the left CCR. this action allows to do a ccr reset after 11 s providing a normal gpm shutdown. this action removes ccr power and 30s providing a normal shutdown of gpm.

the main difference between uninhibited and inhibited mode is. in inhibited mode the gpm do not do a full pbit. both modes are the same. in uninhibited mode the gpm do not do a full pbit.

to perform maintenance taks and test in the airplane the system thet is used is. CMCF. ODLF. ACMF.

when does the ccs start automatically in uninhibited mode. airplane on ground and external power available or battery is selected to on. every time battery is selected to on. in flight whenever ccr reset switch is pressed.

how many gg does the pds have. 8 gg. 4 gg. 2n gg.

which of the following applications provides cb indication and control emulation on ml. eicas maintenance page plug-in ( EMPPI ). ACMF ON MCDF. OSM.

the GG has. six output buses but only two buses can be active at a time. two output buses but only two buses can be active at a time. five output buses but only two buses can be active at a time.

at initial power up where is the eicas displayed. on the inboard side of capt inboard hdd. on the outboard side of capt inboard hdd. on the inboard side of firt officer inboard hdd.

the gpm are used to. contain recorded airplane data during last flight. communications between RDC and ARS. contain the softwere applications programs.

in primary display system hud projector is cooled by. internal fan. cold air from left CAC. it does not have a cooling system.

on the b787 stall warning is. a softwere partition within the flight cointrol electronics cabinet (FCF). a softwere partition within the flight management fuction ( FMF ). a softwere partition within the displat and crew alerting function ( DCAF).

which of the following LRU energize the auxiliary fan and airflow valv to activate the auxiliary function. GPM. ACS. PCM.

full power up built in test (PBIT) of the GPM takes. up to three minutes. one minutes on gruond and theree minutes in flight. the GPM start immediately.

what can i do if an EFIS/DSP control panel fails completely. activate the alternate (EFIS/DSP) function on maintenance laptop. activate the alternate (EFIS/DSP) function on electronic flight bag. activate the alternate (EFIS/DSP) function on multi-function display.

to alert the flight crew when airplane is near a stall condition, how many DCAF functions should be detected at least. 1 of 4. 4 of 4. 2 of 4.

how many ethernet ports are there for wired connections?. one in flight deck and two in forward electronics equipment ( EE ) bay. two in flight deck. one in flight deck and one in each electronics equipment ( EE ) bay.

ya verificadas las respuestas. si. si.