Communications

When selected auto the EMER LOC XMTR will automatically activated when deceleration exceeds;. 5G's. 6G's. 6.5 G's.

The Radio Management System handles;. Radio communication and radio Navigation and TCAS. Radio communication and navigation and transponder function. Radio communication and transponder function and TCAS. Radio navigation, radio communication, transponder and TCAS.

RMS information is displayed and controlled thru;. VCP, MCDU, MCP. ICP, MCDU, VCP and MCP. MPC, MCDU, VCP.

RMA software applications are hosted respectively inside. DU1 and DU4. DU2 and DU4. DU1 and DU5.

IESI navigation and communication information source. VHF1 and XPDR1. V/ILS1 DME and VHF1. V/ILS 1 and VHF1.

It is used to modify communication and navigation frequency. Multi-purpose Control Panel - MCP. Multi Control panel, MCP. Multi-Function Control Panel.

Depressing the SURV button will access these two tab on the VCP. XPDR and TCAS tab. XPDR and ISA Temp page. XPDR and TERR / Wx Tab.

IDENT can be access by. Depressing SURV button to access XPDR tab on the VCP. Depressing NAV button to access Nav tab in VCP. On the MCDU communication page and thru XPDR tab on VCP.

During RCAU failure, FWS is activated and FAULT light illuminates on associated failed RCAU, what associated limitation does the failed RCAU side will experience?. PA and interphone capability inoperative. VHF transmission and PA capability can no longer be used. PA, Interphone and other VHF function can no longer be used.

ALTN pushbutton allows both crew to select alternate source in case of RCAU failure. CAPT affected side connects directly VHF1 and FO affected side connects to VHF2. FO affected side connects to VHF1 and CAPT affected side connects to VHF2. Both connects to VHF1in case of failure.

SQL function can be accessed by. MCDU communication page select VHF1 or VHF2 Page. COMM tab in VCP. MCDU navigation page select Nav1 or Nav2 page.

RAD/INT SELECTOR ON neutral position (on Audio control panel). Is it possible to communicate between flight deck crews using headset. YES by depressing PTT on control wheel but it will also be transmitted to ATC. YES by selecting PTT to forward position and it will not be transmitted to ATC. NO it is not possible.

Which is recommended procedures regarding position of RAD/ INT selector while using oxygen mask. Put it on INT position and you won•t hear breathing noise. Put it on Neutral position but you need to depress PTT on control wheel to communicate with other flight desk crew. Put it on Neutral position but you need to put PTT forward position to communicate with other flight deck crew to avoid breathing noise.

To make emergency to call cabin attendant from cockpit. Press the EMER CALL BUTTON ON overhead panel once. Press Normal call button ON overhead panel five times. Press Normal call button on overhead panel three times. There is no way to make EMER call from flight deck. Only cabin crew can make EMER call to flight deck.

If you press voice only key in audio control panel, voice only light illuminates Amber on audio control panel which is used to. Inhibit squelch function. Inhibit Nav receiver identification audio. Inhibit PA system. Inhibit ACARS message.

When fault is encountered in audio SEL PB, By releasing the affected PB(ALT) affected station can be directly connected to VHF1 OR VHF2 depending on station affected. Only PA can't be used anymore on affected side. Only interphone function side. Other VHF can't be used any longer on affected side. PA, Interphone and other VHF can•t be used any longer on affected side.

Which is true regarding EMER LOC XMTER. When IN auto position, transmission is made automatically when deceleration exceeds 5gs. TEST must not be performed in manual mode. Mechanical horn will be generated when A/C is on ground electrically supplied when emergency beacon is triggered for more than 30 sec. All of the above.

TCAS _TA' triggers when the intruder is. Within 6 NM and plus minus 1200 feet. With 12 NM and plus minus 600 feet. Within 2o to 48 sec from collision area. 3 min from collision area.

which is true regarding TCAS. All aural alerts are inhibited below 1100 feet AGL when A/C is climbing. All aural alerts are inhibited below 900 feet AGL when A/C is descending. Both a and b are correct. Both a and b are incorrect.

RA _increase climb' on TCAS is inhibited in. ICING condition regardless of aircraft configuration and altitude. ICING condition depending in A/C configuration and altitude. NEVER.

How many RMS are in ATR 72-600. 1. 2. 3. 4.

In ATR 72-600, RMS radio management system handles. Radio communication, radio navigation but not TCAS/XPONDER. Radio communication ,TCAS/XPONDER but not radio navigation. Radio communication, radio navigation and TCAS/XPONDER. Radio communication only.

In ATR 72-600 IESI displays. VHF1 frequency. VHF 2 frequency. VHF 1 OR VHF2 depending on pilots selection. NO VHF frequencies are displayed.

In ATR 72-600 EMERGENCY XPDR code 7700 can be set. By using MCP. By using MCDU ( type 7700 on scratch pad and insert on communication page). By pressing EMER using LSK XPNDER page in MCDU. ALL OF THE ABOVE.

In ATR 72-600, VHF EMITTING amber message triggers on EWD with MC+SC when. VHF is emitting for more than 30 sec. VHF is emitting for more than 29 sec. VHF is emitting for more than 25 sec. VHF is emitting for more than 20 sec.

In ATR 72-600 which caution is generated when XPDR fault is detected. MC+ SCT + XPDR ON EWD. MC,SC,XPDER ON EWD, Amber display on VCP PAGE. b and AMBER FAIL OR communication page of MCDU. There will be no caution message generated.