bing bong

Each common computing resource (CCR) contains: A.- One PCMs. B.- Four ACSs, two FOXs, ten GPMs, one PCM. C.- Two ACSs, two FOXs, eight GPMs, two PCMs.

2.- How many power conditioning modules (PCM) has each CCR?. A.- One PCM only. B.- Four PCMs. C.- Two PCMs.

3.- What is the purpose of the 2 nose gear pressure transducers information?. A.- The DCAF uses the data to verify the calculated stabilizer. B.- The FMF uses the data to verify the calculated stabilizer green band position. C.- The TMF uses the data to verify the calculated stabilizer green band position.

4.- How many GPM can you dispatch in defective condition?. A.- Two GPMs. B.- One GPM only, provided it is in GPM slot 8 left or 8 right. C.- One GPM only, provided it is in GPM slot 1R.

5.- Which of the folowing system is connected to the open data network (ODN)?. A.- Flight compartment printer. B.- Terminal Wireless lan unit (TWLU) module. C.- Cabin services system controller (CSSC).

6.- The fiber optic translator (FOX) is used to: A.- Send data between GPM. B.- Transfer data between LH and RH CCR trought CDN. C.- Send data to graphic generator.

COMMON DATA NETWORK CDN. ACS. FOX. ARS.

- Where does the L CCR takes power?. A.- Primary power from the 28 VDC HOT BAT BUS. B.- Primary power from the 28 VDC F/O INSTR BUS. C.- Primary power from the 28 VDC CAPT INSTR BUS.

Where does the central maintenence computing function (CMCF) menus shown is?. A.- Navigation displays (NDs). B.- Primary flight displays (PFDs). C.- Multifunction displays (MFDs), Electronic flight bags (EFBs) and maintenance laptop (ML).

9.- Electronic flight bag is used to: A.- Control the head upper display (HUD). B.- Replace some paper materials (MEL, QRH, etc.). C.- Show primary flight display data.

If one power conditioning module (PCM) fails: A.- 50% of CCR components are unpowered. B.- Only the GPMs and GG’s remain whith power. C.- The other PCM continues to supply to all CCR cabinet module.

In CCR, where is the fan and the valve assembly located?. A.- On the lower parto of the CCR. B.- On the front fase of the CCR. C.- On the back parto f the CCR. The CCS starts in inhibitedmo.

The CCS starts in inhibitedmode if: A.- CCR is reset and the airplane is in the air. B.- CCR is reset during airplane on ground fuel control switch on cutoff position. C.- External power is disconnected.

Where are the loadable software airplane parts storage (LSAP) stored for loading to airplane system. A.- On the controller server module (CSM) server. B.- On the common computing resource (CCR) cabinet left only. C.- On the crew information system – maintenance system (CIS/MS) server.

In which common core system (CCS) components are the hosted software applications for the airplane system. A.- Power conditioning modules (PCM). B.- General processor modules (GPM). C.- Graphics generator (GG) modules.

The power conditioning module (PCM) senses a voltaje less tan 18 VDC on the Captain’s or first officer’s instrument bus, what does the PCM do?. A.- The PCM tells the cards in the CCR that threshold of voltaje is still Good to continue working. B.- The PCM switches the source to the hot battery bus (HBB) for 11 seconds. C.- The corresponding termal circuit bracker (TCB) will pop out.

What is the airplane condition monitoring function (ACMF) purpose?. A.- Engine performance, airplane systems performance and trend análysis of maintenace data. B.- Ramp and transit troubleshooting. C.- Short term and transit troubleshooting.

Wich of the following components belong to the common computing resource (CCR) cabinets: A.- ARINC 664 network remote switches (ARS). . B.- ARINC 664 network cabinet switches (ACS). C.- Network interface module (NIM).

What is the purpose of the fiber optic translator (FOX) modules?. A.- Convert signals from electrical to optical signals and viceversa. B.- Send and receive ARINC 664 electrical signal data to and from the general processor modules (GPM). C.- Supply power to all the modules in the cabinet.

How many displays show data if the one grapics generator fails?. A.- Four displays show data (four HDD) only). B.- All remaining displays show data. C.- Six displays show data (five HDD and one HUD).

What is the core network function that allows you to find and delete loadable software airplane part (L) from the crew information system-maintenance system (CIS/MS) file server module (FSM)?. A.- The on board data loading function (ODLF). B.- The central maintenance computing function (CMCF). . C.- The onboard storage management function (OSMF).

The hosted applications are: A.- Programs to optimize fuel consumption during flight only. B.- Programs to control autoflight function only. C.- Programs to calculate data for many airplane system and functions.

In what components is the CMCF menú displayed?. A.- On maintenance laptop (ML), electronic flight bag (EFB) and multifunction display (MFD). B.- On maintenance laptop (ML) and electronic flight bag (EFB). C.- On multifunction display (MFD) and electronic flight bag (EFB).

For the most central maintenance computing function (CMCF) operations, where does the ground test (GND TEST) P5 switch position selection is?. A.- ENABLE. B.- DATA LOAD / ENABLE. C.- NORMAL.

24.- WHICH OF THE FOLLOWING SYSTEM IS CONNECTED TO THE ISOLATED DATA NETWORK (IDN)?. A.- SATELLITE COMMUNICATIONS (SATCOM) SYSTEM. B.- MAINTENANCE LAPTOP ETHERNET PORTS. C.- XXXXXXXX MODULE.

The ARS, communicate whith the other components of the CCS using: A.- ARINC 664 Buses and Fiber optic. B.- Fiber optic only. C.- Only ARINC 664 buses.

The remote data concentrators (RDC) have: A.- ARINC 429 connections. B.- A and B are correct. C.- Controller área network (CAN) bus connections.

The ACS, communicate with other components of the CCS using: A.- Fiber optic only. B.- Only ARINC 664 buses. C.- ARINC 664 Buses and Fiber optic.

Where is the electronic flight bag (EFB) software and data stored?. A.- In a hard drive inside the EFB display unit. B.- In a hard drive inside the EFB electronic unit (EU). C.- In GPM 7.

What is the function of the recorder independent power supply (RIPS). A.- Is to give power to the forward flight recorder for 10 minutes when aircraft power is not available. B.- Is to give power to the forward flight recorder for 2 hours when aircraft power is not available. C.- . Is to give power to the forward flight recorder for 30 minutes when aircraft power is not available.

The grapics generator (GG) transmits data to: A.- Head down display (HDD) only. B.- Remote data concentrator (RDC). C.- Head down display (HDD) and head up display (HUD).

To perform maintenance tasks and tests in the airplane, the system that is used is: A.- CMCF (Central Maintenance Computing Function). B.- ACMF trough MFD. C.- ODLF trough EFB.

You use the common computing resources (CCR) reset switches: A.- If there is a los off light deck displays. B.- When a PCM is changed. C.- If I need to delete a message.

The CCS has: A.- Two CCRs, six ARSs and twenty one RDCs. B.- One CCR, six ARSs and twenty one RDCs. C.- Two CCRs, four ARSs and then RDCs.

The wired connection connects the maintenance laptop (ML)directly to: A.- Isolated data network (IDN). B.- Open data network (ODN). C.- Common core system (CCS).

How does the CCS send and receive airplane data?. A.- Trough a common data network (CDN). B.- By remote data concentrator (RDC). C.- Through Wireless connection in forward and aft E&E compartment.

What is the remote data concentrator main purpose?. A.- The RDC main purpose is to calcule data and give orders to many system. B.- The RDC main purpose is to change airplane systems data from analog, discrete, arinc 429, CAN bus data to ARINC 664 format. C.- The RDC main purpose is to convert fiber optic signal into electrical ARINC 664 signal.

The maintenance laptop-to-airplane connections are: A.- Wired and Wireless. B.- Bluetooth. C.- ARINC429 high speed full.

Each HUD has a “Desiccant” to: A.- Remove spurious data. B.- Prevent moisture droplets in the lense. C.- Prevent overheating in the projector.

The power conditioning module (PCM) changes 28 Vdc to: A.- =+12,5 Vdc to GPM and +28 Vdc to other components in CCR. B.- =+12,5 Vdc to cooling components and *28 Vdc to modules in CCR. C.- =+12,5 Vdc used by all modules in CCR and +28 Vdc to cooling fan and control valve motor.

What components does the head up display (HUD) have?. A.- Proyector and combiner. B.- Projector only. C.- Projector, combiner and display.