ATR-BC Exam Prep 2025 | 950 Real Exam
Questions & Verified Answers | Guaranteed
A+, Exams of Clinical Medicine
1.) When selected auto the EMER LOC XMTR will automatically activated when deceleration
exceeds;
A. 5G'S
B. 6 G's
C. 6.5 G's A. 5G'S
2.) The Radio Management System handles;
A. Radio communication and radio Navigation and TCAS
B. Radio communication and navigation and transponder function
C. Radio communication and transponder function and TCAS
D. Radio navigation, radio communication, transponder and TCAS D. Radio navigation, radio
communication, transponder and TCAS
3.)RMS information is displayed and controlled thru;
A. VCP, MCDU, MCP
B. ICP, MCDU, VCP and MCP
C. MPC, MCDU, VCP A. VCP, MCDU, MCP
4.)RMA software applications are hosted respectively inside
A. DU1 and DU4
B. DU2 and DU4
C. DU1 and DU5 B. DU2 and DU4
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,5.) lESI navigation and communication information source
A. VHF1 and XPDR1
B. V/ILS1 DME and VHF1
C. V/ILS 1 and VHF1 C. V/ILS 1 and VHF1
6.) It is used to modify communication and navigation frequency
A. Multi-purpose Control Panel - MCP
B. Multi Control panel, MCP
С. Multi-Function Control Panel С. Multi-Function Control Panel
7.) Depressing the SURV button will access these two tab on the VCP
A. XPDR and TCAS tab
B. XPDR and ISA Temp page
C. XPDR and TERR / Wx Tab A. XPDR and TCAS tab
8.) IDENT can be access by
A. Depressing SURV button to access XPDR tab on the VCP
B. Depressing NAV button to access Nav tab in VCP
C. On the MCDU communication page and thru XPDR tab on VCP C. On the MCDU
communication page and thru XPDR tab on VCP
9.) During RCAU failure, FWS is activated and FAULT light illuminates on associated failed RCAU,
what ass limitation does the failed RCAU side will experience?
A. PA and interphone capability inoperative
B. VHF transmission and PA capability can no longer be used
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,C. PA, Interphone and other VHF function can no longer be used C. PA, Interphone and other
VHF function can no longer be used
10.) ALTN pushbutton allows both crew to select alternate source in case of RCAU failure
A. CAPT affected side connects directly VHF1 and FO affected side connects to VHF2
B. FO affected side connects to VHF1 and CAPT affected side connects to VHF2
C. Both connects to VHFlin case of failure A. CAPT affected side connects directly VHF1 and
FO affected side connects to VHF2
11.) SQL function can be accessed by
A. MCDU communication page select VHF1 or VHF2 Page
B. COMM tab in VCP
C. MCDU navigation page select Nav1 or Nav2 page A. MCDU communication page select VHF1
or VHF2 Page
12. Navigation frequency display can be accessed thru
A. NAV pushbutton on the MCP and displayed in VCP NAV Tab
B. RMS pushbutton on the MCDU Navigation page
C. NAV pushbutton on MCP thru VCP NAV tab and thru RMS pushbutton on respective MCDU's
Navigation page C. NAV pushbutton on MCP thru VCP NAV tab and thru RMS pushbutton
on respective MCDU's Navigation page
13.) Auto-tuning is available and can be accessed thru
A. NAV pushbutton on MCP thru VCP NAV tab and by RMS pushbutton on respective MCDURs
Navigation page
B. NAV pushbutton on the MCP and displayed in VCP NAV Tab
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, C. RMS pushbutton on respective MCDURs and by selecting AUTO/MAN tune mode A. NAV
pushbutton on MCP thru VCP NAV tab and by RMS pushbutton on respective MCDURs
Navigation page
14.) Navigation information is displayed in PFD available in different formats,
A. In standard configuration an HSI is displayed on the PFD.
B. When pilot changes ND to system page, a mini ND is displayed on the PFD and can be
changed in 3 formats being HIS, Mini-ND mode Arc and mini-ND mode Rose.
C. In case changes in MFD other than ND, mini-ND is displayed on the PFD with available
formats in mini-ND Arc and Rose mode. C. In case changes in MFD other than ND, mini-ND
is displayed on the PFD with available formats in mini-ND Arc and Rose mode.
15.) Changes in ND page format is done thru
A. Selection of ND page (if MFD is previously other than ND) and rotating format knob on the
MCP
B. Format knob located on the EFCP Electronic Flight Control Panel
C. Selection of format knob in the EFCP, formats available are ROSE, ARC, PLAN modes C.
Selection of format knob in the EFCP, formats available are ROSE, ARC, PLAN modes
16.) Calling up the NAV/ADF bearing information on the ND displays is done thru
A. Repetitive selection of either BRG 1/BRG2 pushbutton on the MCP displays VOR1/VOR2,
ADF1/ADF2 and Bearing off.
B. Selection on either BRG 1/BRG2 pushbutton on the EFCP cycles the display for VOR1/VOR2,
ADF/ADF2 and bearing off
C. Bearing information may be manually called up thru MCDU Navigation page. B. Selection
on either BRG 1/BRG2 pushbutton on the EFCP cycles the display for VOR1/VOR2, ADF/ADF2
and bearing off
17.) IESI navigation information source
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Questions & Verified Answers | Guaranteed
A+, Exams of Clinical Medicine
1.) When selected auto the EMER LOC XMTR will automatically activated when deceleration
exceeds;
A. 5G'S
B. 6 G's
C. 6.5 G's A. 5G'S
2.) The Radio Management System handles;
A. Radio communication and radio Navigation and TCAS
B. Radio communication and navigation and transponder function
C. Radio communication and transponder function and TCAS
D. Radio navigation, radio communication, transponder and TCAS D. Radio navigation, radio
communication, transponder and TCAS
3.)RMS information is displayed and controlled thru;
A. VCP, MCDU, MCP
B. ICP, MCDU, VCP and MCP
C. MPC, MCDU, VCP A. VCP, MCDU, MCP
4.)RMA software applications are hosted respectively inside
A. DU1 and DU4
B. DU2 and DU4
C. DU1 and DU5 B. DU2 and DU4
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,5.) lESI navigation and communication information source
A. VHF1 and XPDR1
B. V/ILS1 DME and VHF1
C. V/ILS 1 and VHF1 C. V/ILS 1 and VHF1
6.) It is used to modify communication and navigation frequency
A. Multi-purpose Control Panel - MCP
B. Multi Control panel, MCP
С. Multi-Function Control Panel С. Multi-Function Control Panel
7.) Depressing the SURV button will access these two tab on the VCP
A. XPDR and TCAS tab
B. XPDR and ISA Temp page
C. XPDR and TERR / Wx Tab A. XPDR and TCAS tab
8.) IDENT can be access by
A. Depressing SURV button to access XPDR tab on the VCP
B. Depressing NAV button to access Nav tab in VCP
C. On the MCDU communication page and thru XPDR tab on VCP C. On the MCDU
communication page and thru XPDR tab on VCP
9.) During RCAU failure, FWS is activated and FAULT light illuminates on associated failed RCAU,
what ass limitation does the failed RCAU side will experience?
A. PA and interphone capability inoperative
B. VHF transmission and PA capability can no longer be used
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,C. PA, Interphone and other VHF function can no longer be used C. PA, Interphone and other
VHF function can no longer be used
10.) ALTN pushbutton allows both crew to select alternate source in case of RCAU failure
A. CAPT affected side connects directly VHF1 and FO affected side connects to VHF2
B. FO affected side connects to VHF1 and CAPT affected side connects to VHF2
C. Both connects to VHFlin case of failure A. CAPT affected side connects directly VHF1 and
FO affected side connects to VHF2
11.) SQL function can be accessed by
A. MCDU communication page select VHF1 or VHF2 Page
B. COMM tab in VCP
C. MCDU navigation page select Nav1 or Nav2 page A. MCDU communication page select VHF1
or VHF2 Page
12. Navigation frequency display can be accessed thru
A. NAV pushbutton on the MCP and displayed in VCP NAV Tab
B. RMS pushbutton on the MCDU Navigation page
C. NAV pushbutton on MCP thru VCP NAV tab and thru RMS pushbutton on respective MCDU's
Navigation page C. NAV pushbutton on MCP thru VCP NAV tab and thru RMS pushbutton
on respective MCDU's Navigation page
13.) Auto-tuning is available and can be accessed thru
A. NAV pushbutton on MCP thru VCP NAV tab and by RMS pushbutton on respective MCDURs
Navigation page
B. NAV pushbutton on the MCP and displayed in VCP NAV Tab
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, C. RMS pushbutton on respective MCDURs and by selecting AUTO/MAN tune mode A. NAV
pushbutton on MCP thru VCP NAV tab and by RMS pushbutton on respective MCDURs
Navigation page
14.) Navigation information is displayed in PFD available in different formats,
A. In standard configuration an HSI is displayed on the PFD.
B. When pilot changes ND to system page, a mini ND is displayed on the PFD and can be
changed in 3 formats being HIS, Mini-ND mode Arc and mini-ND mode Rose.
C. In case changes in MFD other than ND, mini-ND is displayed on the PFD with available
formats in mini-ND Arc and Rose mode. C. In case changes in MFD other than ND, mini-ND
is displayed on the PFD with available formats in mini-ND Arc and Rose mode.
15.) Changes in ND page format is done thru
A. Selection of ND page (if MFD is previously other than ND) and rotating format knob on the
MCP
B. Format knob located on the EFCP Electronic Flight Control Panel
C. Selection of format knob in the EFCP, formats available are ROSE, ARC, PLAN modes C.
Selection of format knob in the EFCP, formats available are ROSE, ARC, PLAN modes
16.) Calling up the NAV/ADF bearing information on the ND displays is done thru
A. Repetitive selection of either BRG 1/BRG2 pushbutton on the MCP displays VOR1/VOR2,
ADF1/ADF2 and Bearing off.
B. Selection on either BRG 1/BRG2 pushbutton on the EFCP cycles the display for VOR1/VOR2,
ADF/ADF2 and bearing off
C. Bearing information may be manually called up thru MCDU Navigation page. B. Selection
on either BRG 1/BRG2 pushbutton on the EFCP cycles the display for VOR1/VOR2, ADF/ADF2
and bearing off
17.) IESI navigation information source
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