LOS SOBREVIVIENTES

What differences are there between the VOR/MKR receiver #1 and VOR/MKR receiver #2? ( considering the MKR). Only VOR/MKR receiver # 1 uses the MKR function. Only VOR/MKR receiver #2 uses the MKR function. Both VOR/MKR #1 and #2 receivers are used to MKR reception.

On the ND next to the VOR indication the letter "M" is shown . What does it mean?. The VOR frequency has been entered from the MCDU. The VOR frequency has been entered from the RMP. The VOR frequency was selected by the FMGC .

In normal operation, The FMGC # tunes... VOR #1, ADF #1 and ILS#1 navigation systems. VOR #2, ADF #2 and ILS#2 navigation systems. VOR #3, ADF#3 and ILS#3 navigation systems.

When are both Radio Altimeters operating?. During Take- Off only. In Approach only. Always.

Where is the VOR information shown?. In both NDs and in the DDRMI. In the captain ND and in the DDRMI. In the F/O ND and in the MCDU.

Where is the DME system information shown?. Only in the PFDs. In the PFDs, NDs and DDRMI. In the ECAM displays only.

How is a Resolution advisory , of the TCAS system, in the PFD shown?. By means of a change in the V/S indication. By means of a change in the Air Speed indication. In the overhead panel there is a flashing light.

When you test the ILS 1, where is the information displayed?. On the upper ECAM. On the capt PFD and F/O ND. On both PFDs and NDs simultaneously.

Which is the purpose of the supressor pulse, in the ATC, DME and TCAS systems ?. To permit simultaneous transmission among them. To avoid simultaneous transmission among them. To erase a datalink.

TCF and TAD are new Modes for navegation system?. FADEC. Global Position System. EGPWS.

Which component controls the weather radar antenna stabilization?. ADIRU. Transceiver. Antenna.

WR/PWS. When does the Predictive Winds hear function operate automatically?. PWS switch in AUTO, below 2300 ft, at least one engine running and ATC/TCAS in AUTO or ON position. PWS switch in AUTO, whenever a winds hear event is encountered. PWS switch in AUTO, above 2300 ft, both engines running and ATC/TCAS in AUTO or ON position.

LRRA 1 has failed with a radio altitude below 2500 ft. Which statement is right?. no Radio Altitude is displayed in Capts PFD. a flag is shown on Capts PFD. LRRA 2 is used in case of LRRA 1 failure to supply Capts PFD with Radio Altitude information.

Which VOR information is displayed on Capts ND in the Rose-NAV Mode with Selector 1 in VOR 1 a selector 2 in Off?. Deviation Bar and selected Course of VOR 1. Only the Bearing Pointer of VOR 1. Deviation Bar and Bearing Pointer of VOR 1.

The new feature of EGPWS is... the information shown is dependant on weather conditions. the information shown depends on geographical data base. the information shown depends on navigational aids.

In the GPS for navigational purposes... provides the crew and airborne system users with signals transmitted by a ground station. the radial position error increases along the route. needs at least four satellites.

The ILS and GPS functions are processed by: MMRs. VOR/MKR. GPS.

The data from the ILS receiver # 2 is displayed on... Capt PFD. Capt. ND and PFD. The F/O PFD and Captain ND.

The Alpha Floor Protection is calculated by... the SEC. the SDAC. the ELAC and FAC.

If both ELAC fail, the FAC computes... the dutch roll damping only, turn coordination is lost. the turn coordination only, the dutch roll damping is lost. the turn coordination and dutch roll damping.

Where is the Fault Isolation Detection System (FIDS) active?. In the FAC 1. In the FAC 2. In the AIDS.

The FCU SPD/Mach window display dashes lines and the white indicator light comes ON, it means... The Pilot is managing the speed by FCU. The FMGC is managing the aircraft speed. The A/Thr is managing the speed by means of throttle lever.

IF THE A/THR WAS DISENGAGED DUE TO AN EXTERNAL FAILURE: THE THRUST IN THE CORRESPONDING ENGINE IS FROZEN IN ITS LAS VALUE. THE ENGINE THRUST IS ADAPTED TO THE THRUS LEVER POSITION AUTOMATICALLY. THE ENGINE THRUST IS SET TO THE T/0 AUTOMATICALLY.

IN FLIGHT, AUTO PILOT ENGAGED, A FORCE IS APPLIED AT THE SIDE STICK OR THE RUDDER PEDALS. WHAT HAPPENS IS THAT CONDITION?. THE AUTO PILOT IS DISENGAGED AND THEA AIRPLANE FOLLOWS THE FLIGHT CONTROL ORDERS. MANUAL ASISTENCE IS ALLOWED BY THE AUTO PILOT. THE AIRPLANE STILL FOLLOW THE AUTO PILOT ORDER.

AIRPLANE IN APPROACH, ONE IDGN AND APU ARE SUPPLYING ELECTRICAL POWER, SO, AT THE AUTO PILOT…. THE CAT 3 DUAL IS NOT ACCEPTED. IT IS NOT POSSIBLE TO USE SINGLE AUTO POLOT. THE CAT 3 DUAL IS ACCEPTED.

IT AFTER THE AIRCRAFT POWER UP, THE FD ”2FD2” INDICATION APPEARS IN EACH PFD. WHAT DOES IT MEAN?. THE FMGC 1 IS INOPERATIVE. THE FMGC 2 IS INOPERATIVE. IT IS A NORMAL INDICATION.

THE FUNCTIONS OF THE FMGC ARE: AUTOPILOT, FLIGHT DIRECTOR, AUTO THRUST CONTROL AND FLIGHT MANAGEMENT. YAW DAMPER AND RUDDER TRIM. CALCULATION OF THE CHARACTERISTIC SPEED AND FLIGHT ENVELOPE MONITORING.

WHICH LRUs PERFORMED THE FLIGHT ENVELOPE FUNCTION?. THE FACs. THE FMGCs. THE FCU.

AP1 AND AP2 NOT ENGAGED, FD1 AND FD2 ENGAGED AND A/THR ACTIVE: FMGC 1 CONTROLS BOTH ENGINES. FMGC 1 CONTROLS ENGINE #1, FMGC 2 CONTROL ENGINE 2. FMGC 2 CONTROLED BOTH ENGINES.

A/THR IS ENGAGED. WHAT HAPPENS IF ONE INSTICTIVE DISCONNECT P/B IS PRESSED LONGER THAN 15 SEC?. IT INHIBITS ANY ENGAGEMENT OF THE A/THR FUNCTION EVEN ALPHA FLOOR PROTECTION (RECOVERING AL NEXT POWER UP). THE A/THR IS DISCONECTED AND......... THERE IS A SWITCH OVER TO THE....

HOW SHOULD THE ELECTRICAL CONFIGURATION BE TO GET CAT 3 DUAL?. BOTH BTCs AND 1PC2 CONTACTORS MUST BE OPEN. ONE BTC CONTACTOR MUST BE CLOSED. BOTH BTC CONTACTOR MUST BE OPEN.

TE CAT ll/lll OPERATION DEPENDS ON: THE AIRCRAFT, AIRFIELD, FLIGHT CREW AND MAINTENANCE. THE AIRFIELD ONLY. THE AIRCRAFT AND OPERATOR ONLY.

WHICH LRUs BELONGS TO THE AUTOFLIGHT SYSTEM?. 2 FMGC AND 2 FAC, 1 FCU AND BOTH MCDUs. 2 FMGC AND ELAC. ELACs AND SECs.