TEST BORRADO, QUIZÁS LE INTERESE: TMA DE LU
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Título del Test:
TMA DE LU Descripción: EXAMEN TMA 1 Autor:
Fecha de Creación: 21/11/2024 Categoría: Idiomas Número Preguntas: 11 |
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WHAT IS INDICATED TO THE CAPTIAN WHEM A PRIMARY FAILURE IS OCCURRING IN THE AIRCRAFT? A PRIMARY FAILURE IS DISPLAYED WITH A TITLEU NDERLINE A PRIMARY FAILURE IS DISPALYED WITH AN ASTERIK A PRIMARY FAILURE IS DISPLAYED WITH A BOX AROUND THE FAILURE. WHAT ARE THE FUNCTIONS OF THE ECAM SYSTEM? DATA ACQUISITION AND CONCENTRATION, DATA WARNING COMPUTATION AND WARNING ANNOUNCEMENT AND DATA DISPLAY SDAC, FWC AND DMC? DATA ACQUISITION AND CONCENTRATION, DATA WARNING COMPUTATION AND WARNING ANNOUNCEMENT AND DATA DISPLAY SDAC, CFDIU AND DMC DATA ACQUISITION AND CONCENTRATION, DATA WARNING COMPUTATION ANDWARNING ANNOUCEMENT AND DATA DISPLAY SDAC, FWC ADN BSCU. WHICH TYPE OF WARNING GENERATES THE ALERT 3 AND 2? ALERT 2 MASTER WARNING + CRC, ALERT 3 MASTER CAUTION + SC ALERT 3 MASTER WARNING + CRC, ALERT 2 MASTER CAUTION + SC ALERT 1 MASTER WARNING + CRC, ALERT 2 MASTER CAUTION + SC. WICH STATEMENT IS CORRECT ABOUT THE POST FLIGHT REPORT (PFR)? THE POST FLIGHT REPORT (PFR) IS THE SUM OF THE last leg report AND OF THE last leg ecam report. THE PFR CAN ONLY BE PRINTED 0N GROUND. THE POST FLIGHT REPORT (PFR) IS THE SUM OF THE last leg report AND OF THE current leg ecam report. THE PFR CAN ONLY BE PRINTED 0N GROUND. THE POST FLIGHT REPORT (PFR) IS THE SUM OF THE current leg report AND OF THE last leg ecam report. THE PFR CAN ONLY BE PRINTED 0N GROUND. what class of failures has operational consequences and needs to be refer to the minimum equipment lis (MEL): "GO", "GO IF" or "NO GO"? class 2 class 1 class 3. when is the ADV indication presented? appears in single display configuration on the lower memo area when a parameter drifts from its normal value. appears in single display configuration on the status page area when a parameter drifts from its normal value. appears in normal display configuration on the lower memo area when parameter drifts from its normla value. IN NORMAL OPERTAION , WHICH DISPLAYS ARE CONTROLLED BY THE DMC 1? CAPTIAN PFD AND ND, E/W DISPLAY AND SD ARE CONTROLLED BY DMC 1, IN CASE OF FAIL ARE TRANSFERRED AUTOMATICALLY TO DMC 2 AND A MANUAL SWITCHING HAS TO BE DONE TO DMC 3 CAPTIAN PFD AND ND, E/W DISPLAY AND SD ARE CONTROLLED BY DMC 1, IN CASE OF FAIL ARE TRANSFERRED AUTOMATICALLY TO DMC 3 AND A MANUAL SWITCHING HAS TO BE DONE TO DMC 2 CAPTIAN PFD AND ND, E/W DISPLAY AND SD ARE CONTROLLED BY DMC 1, IN CASE OF FAIL ARE TRANSFERRED MANUALLY TO DMC 2 AND A MANUAL SWITCHING HAS TO BE DONE TO DMC 3. when the type 2 systems are considered in flight? from 30 secunds after touch down up to lift off. from 30 secunds after touch down up to lift off. from 30 secunds after lift off up to touch down. which inputs are directly sen to DMC to elaborate information on the systems pages? engines , air conditioning, navigation. engines, fuel, navigation. engines, fuel, doors status . what are the functions of the ECAM system? data acquisition and concentration, data warning computation and warning announcement and data display SDAC, FWC, and DMC. data acquisition and concentration, data warning computation and warning announcement and data display SDAC,CFDIU, and DMC. data acquisition and concentration, data warning computation and warning announcement and data display SDAC, FWC, and BSCU. what indicates the STS reminder on the E/W display? status memo messages in present on the E/W display info. a parameter has drifted on the STS page. status messages (info) is present on the SD STS. |
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