chaparritas

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

what are the alternative ways to disengage the autopilot ?. MCP disengage bar in the down position. puch the A/P disengage sw on the control wheel. selected flap in 1 position.

when does the PFCF accept AAF commands. when the PFCF are in any mode. only when the PFCF are in the secondary mode. only when the PFCF are in the normal mode.

the airplane is in the air. the captain puts the AIR DATA/ATT sw 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 are the FCE supplied by the right radio altimeter transceiver ?. FCE L and C1. FCE R and C2. FCE R only.

what does the AFF send its pitch, roll and yaw AP commands to ?. the flight control surfaces directly. the ACE. the PFCF.

what supplies attitude data to ISFD?. the CDN. it has its own inertial sensors to calculate pitch and roll attitude. the left IRU.

when the ISFD sendsnbackup attitude, airspeed and altitude data to the CDN. this data is a backup if the CDN fails. This data is a backup if all FCE fails. this data is a backup if the FCE C2 fails.

which one is part of the integrated surveillance system. ATC. ILS. RA.

Where do you performance a manual tuning and course selection to VOR reseivers. alternate EFIS panel on MD. backup navegation menu on TCP. CDU nav RAT page.

ON BAT light iluminated means. one or more of the IRU supplies from SPDU power. one or more of the IRU supplies from RPDU. one or more of the IRU supplies from BATTERY power.

when the airplane is in the air and the autopilot is engaged and the airplane roll right.what moved 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 HUD. PFD and HUD. PFD and ND.

when the airplane has power,you need to engage the autopilot on the ground for test purposes.what must you do?. select flap up. pressurize the hydraulic system. select flap 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 managment function software located ?. ACE C2. L and R CCR. FCM L,R and C1.

which of the following navigation system have alternate tuning?. GLS. VOR. MKR.

Where does the ADM take power from?. +/-13.5v DC PCM in the FCE. +/-13.5v PCM in the CCR. +/-13.5v DC PMM in the CNC.

What LRU supplies ILS aproach deviation data to the ISFD. LH integrated surveillance system. LH integrated navigation radio. LH FCE C1.

where is the localizer track antenna located. C. B. A.

why is the target thrust cursor magenta?. because the FMF makes the thrust limit. because the pilot makes the thrust limit by the FCU. because the thrust managment system makes the thrust limit.

the airplane is on approach mode.the flight crew arms approach.which is the first antenna to receive the localizer radio signals and send them to the INR?. Localizer capture antenna. Localizer approach antenna. Localizer track antenna.

where is the vor displayed?. PFD. ND selected in the pull-down menu. ISFD.

how does the ADRF compute aircraft speed. From left,center and right ADM total pressure and ADM 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 the functions is in the integrated navigation radio. marker beacon. DME. TAWS.

what does the airplane use the TAT value when the airplane is in flight?. lower average of EEC element and CAC ice protection system. simple average of TAT. weighted average of EEC elements and TAT probes.

what is 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 CDN.

The IRU calculate navigation (position) data.what data do the AHRU need to calculate this navigation data?. present position. GPS position. GLSposition.

where do you select the weather radar test. WXR TEST on TCP. ND WXR pull-down menu on ND. EFIS control panel.

which of these functions are in the FCM?. TMF. ADRF. FMF.

Where is the AFF software. in the FCE. in the CCS. in the CNC.

Where is the setting for marometric correction(QNH,QNE),if an EFIS/DSP. Alternate EFIS/DSP control on MFD. EFIS/DSP. CDU.