Diferencias

WHAT CONTROLS THE AUDIO TO AND FROM THE FLIGHT CREW?. AUDIO ACCESSORY UNIT (AAU). REMOTE ELECTRONIC UNIT (REU). AUDIO MANAGEMENT UNIT (AMU).

HOW MANY ATTENDANT HANDSETS ARE FITTED?. FOUR. SIX. EIGHT.

WHICH ELECTRICAL BUS BAR PROVIDES POWER TO THE AUDIO MANAGEMENT UNIT FOR CAB/SERVICE INTERPHONE OPERATION?. STANDBY DC BUS. BATTERY BUS. LEFT DC BUS.

WHAT SUPPLIES THE ALARM SIGNAL TO THE IRS WARNING RELAY TO SOUND THE GROUND CREW CALL HOR. CABIN TEMPERATURE CONTROLLER. ELECTRONIC CONTROL CARD. EQUIPMENT COOLING INDICATOR CARD.

WHAT IS THE PA GAIN INCREASE IN DECIBELS FOR AIRCRAFT DECOMPRESSION?. 3. 6. 9.

HOW IS THE ALTERNATE PSS CONTROLLER SELECTED FOR OPERATION?. AUTOMATICALLY ON PRIMARY CONTROLLER FAIL. MANUAL SELECTION ON THE PASSENGER SERVICES CONTROLLER. MANUAL SELECTION ON THE CABIN COFIGURATION/TEST MODULE.

WHICH AC ELECTRICAL BUS BAR PROVIDES POWER FOR THE LEFT OUTBOARD OVERHEAD ELECTRONICS UNITS IN ZONE 3?. LEFT. LETF TRANSFER. LEFT UTILITY.

WHAT PROVIDES THE CONTROL FOR THE CABIN CHIMES?. PASSENGER SERVICES CONTROLLER. OVERHEAD ELECTRONICS UNIT. LOCAL AREA CONTROLLER.

WHAT PROVIDES CONTROL FOR THE READING LIGHTS?. PASSENGER SERVICES CONTROLLER. OVERHEAD ELECTRONICS UNIT. LOCAL AREA CONTROLLER.

TO WHICH STATIC PORT IS THE DIFFERENTIAL PRESSURE SENSOR CONNECTED TO?. ALTERNATE. CAPTAINS S1. FIRST OFFICER S2.

WHAT PROVIDES POWER FOR THE OPERATION OF THE AIR DATA MODULES?. ADC TRANSFORMER. ADIRU. INERTIAL REFERENCE MODE PANEL (IRMP).

WHAT SETS THE SOURCE DESTINATION IDENTIFIER (SDI) FOR THE ADM?. PROGRAM PINS. SOFTWARE DATALOAD. INTERNAL ADDRESSING.

WHAT PROVIDES THE BARO CORRECTION DATA FROM THE LEFT EFIS CONTROL PANEL TO THE LEFT ADIRU?. CENTER CDU. LEFT CDU. LEFT DISPLAY PROCESSOR CONTROLLER (DPC).

FOR THE RIGHT ATC TRANSPONDER, WITH THE F/O AIR DATA INSTRUMENT SOURCE SELECT SWITCH IN ¨R¨, WHICH ADIRU CAN PROVIDE AIR DATA?. LEFT AND RIGHT. LEFT AND CENTRE. RIGHT AND CENTRE.

WHAT PROVIDES THE TAKE-OFF THRUST SIGNAL IN TO THE WEATHER RADAR?. DATA CONCENTRATOR UNITS (DCU). DISPLAY PROCESSOR COMPUTER (DPC). ENGINE ELECTRONIC CONTROL (ECC).

IF THE AUTOPILOT IS ENGAGED WITH LOC OR G/S CAPTURED, HOW CAN THE ILS RECEIVERS TUNING BE RESET?. DIRECTLY FROM THE FMC NAVIGATION TUNING DISPLAY. AFTER THE AUTOPILOT HAS BEEN DISENGAGED AND F/Ds TURNED OFF. AFTER HEADING FLCH HAS BEEN SELECTED.

WHICH ADIRU PROVIDE DATA TO THE LEFT MMR FOR GPS OPERATION?. LEFT AND CENTRE. LEFT AND RIGHT. CENTRE AND RIGHT.

HOW MANY DME CHANNELS CAN THE FMC SUPPLY TO TUNE THE DME?. 2. 3. 5.

WHICH FLIGHT CONTROL COMPUTERS (FCC) CONNECT TO THE LEFT YSM?. RIGHT AND CENTER. LEFT AND RIGHT. CENTER AND LEFT.

HOW IS DATA FROM THE ENGINE ELECTRONIC CONTROL (EEC)ROUTED TO THRUST MANAGEMENT COMPUTER (TCM)?. DIRECT FROM THE EEC. THROUGH A DCU. THROUGH A DPC.

WHERE IS THE AUDIO MANAGEMENT UNIT LOCATED?. E2 RACK. E3 RACK. E4 RACK.

WHAT EICAS LEVEL IS A CABIN INTERPHONE MESSAGE?. LEVEL C. LEVEL E. LEVEL S.

WHERE IS THE PRE-RECORDED ANNOUNCEMENT REPRODUCER LOCATED?. E5 RACK. E2 RACK. E1 RACK.

WHAT PROVIDES CONTROL FOR THE MASTER CALL LIGHTS?. PASSENGER SERVICES CONTROLLER. OVERHEAD ELECTRONICS UNIT. LOCAL AREA CONTROLLER.

WHICH AC ELECTRICAL BUS BAR PROVIDES POWER FOR PASSENGER SERVICES CONTROLLER?. LEFT. LEFT TRANSFER. LEFT UTILITY.

WHAT DATA BUS PROTOCOL IS USED BY THE PASSENGER SERVICE CONTROLLER TO COMMUNICATED WITH THE LOCAL AREA CONTROLLERS?. ARINC 429. 10 BASE T. RS-485.

HOW MANY OVERHEAD ELECTRONICS UNITS IN A COLUMN CAN BE SUPPORTED?. 30. 25. 20.

WHICH ADIRU CAN RECEIVE POWER FROM THE STANDBY BUS DURING AUTOLAND?. RIGHT. CENTER. LEFT.

WHAT IS THE POWER REQUIREMENT FOR AN AIR DATA MODULE?. +-13V DC. +-15V AC. +-26 AC.

WHICH AIR DATA SOURCE CAN THE CAPTAINS LFDS SYSTEM USE AS A BACKUP?. LEFT. CENTER. RIGHT.

FOR THE TCAS COMPUTER, WHICH ADIRU CAN PROVIDE DATA?. LEFT AND RIGHT. LEFT AND CENTER. RIGHT AND CENTER.

FOR THE LEFT VOR, WHEN MANUALLY TUNED, WHAT DIRECTLY PROVIDES THE TUNING DATA?. RIGHT CDU. LEFT CDU. LEFT FMC.

WHICH ELECTRICAL BUS BAR PROVIDES POWER FOR THE OPERATION OF THE LEFT FMC SOURCE SELECT RELAYS?. STANDBY DC. DC R BUS. DC L BUS.

WHICH OF THE FOLLOWING STORES THE FMCS FAULT DATA WHICH IS RECORDED DURING FLIGHT?. DISPALY PROCESSOR COMPUTER (DPC). FLIGHT MANAGEMENT COMPUTER (FMC). MAINTENANCE CONTROL DISPLAY PANEL (MCDP).

WHICH OF THE AUTOPILOT DISCRETE WARNINGS GO TO THE WARNING ELECTRONIC UNIT?. A/P WARN 1 (BAT) AND A/P WARN 2. A/P WARN 1 (BAT) AND A/P WARN 2 (BAT). A/P WARN 2 AND A/P WARN 2 (BAT).

FOR THE FUSELAGE EXTENSION PLUGS, WHAT IS THE SIZE OF THE AFT PLUG?. 253 INCHES. 205 INCHES. 281 INCHES.

FOR AXLE JACKING OF THE AIRCRAFT, WHAT IS THE MAXIMUM WEIGHT FOR THE MAIN GEAR?. 90,000 POUNDS. 85,000 POUNDS. 80,000 POUNDS.

ATA 31 HOW MANY SYSTEM SYNOPTIC PAGES ARE AVAILABLE?. TWO. THREE. FOUR.

ELECTRICAL BUS PROVIDES POWER FOR RED ANTI COLLISION LIGHT?. AC GROUND SERVICE BUS. X.

HOW MANY SAMPLING AIR BLOWERS FITTED ON FWD CARGO SMOKE DETECTION?. 4. 1. 2.

SECONDARY EXT POWER CONNECT TO?. LEFT AC BUS. RIGHT AC BUS. CENTER DC BUS.

WHAT COORDINATES NO-BREAK POWER TRANSFER?. BPCU. CPCU. ECC.

LEFT QTY SENSOR CONNECT TO?. HYDRAULIC MONITOR UNIT. X.

ATA 29 WHAT CONTROLS THE SPEED OF THE AIR DRIVEN UNIT?. LOGIC SPEED CONTROL UNIT. ELECTRONIC CONTROL CARD. LEFT DATA CONCENTRATOR UNIT.

HOW MANY SPOILER CONTROL MODULES IN LEFT CSEU?. 3. 2. 1.

MANUAL TRIM DONE AT SAME TIME FCC?. MANUAL TRIM HAS PRIORITY. X.

PACK FLOW SENSOR CONNECT TO?. CTC. X.

ATA 32 WHAT CONTROLS THE AUTO-OFF RELAYS FOR THE UP SOLENOIDS IN THE SELECTOR/BYPASS VALVE?. PROXIMITY ELECTRONIC SENSING UNIT (PSEU). DISPLAY PROCESSING COMPUTERS (DPC). DATA CONCENTRATOR UNITS (DCU).

WHICH DATA PROTOCOL IS USED FOR MAJOR LFDS COMPONENTS?. ARINC 429. 10 BASE T. ARINC 663.

WHAT CONTROLS THE OPERATION OF ALTERNATE VENTILATION SYSTEM?. CTC. ASCTU. A SWITCH ON P5.

WHICH ELECTRICAL BUS BAR PROVIDES POWER FOR THE LEFT OUTBOARD DISPLAY UNIT?. LEFT DC BUS. CAPTAINS DC DISPLAY BUS. STANDBY DC BUS.

WHICH DISPLAY UNIT HAS A REMOTE LIGHT SENSOR INPUT?. OUTBOARD DU. INBOARD DU. UPPER CENTER DU.

WHICH OF THE FOLLOWING PROVIDES THE ¨ WINDSHEAR AHEAD¨ AUDIO TO THE WARNING ELECTRONICS UNIT?. WEATHER RADAR. GROUNG PROXIMITY WARNING SYSTEM. TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM.

WHICH DISPLAY PROCESSOR COMPUTER IS AN ACTIVE BACKUP?. LEFT. CENTER. RIGHT.

SELECT THE CORRECT STATEMENT FOR THE PANEL DATA CONCENTRATOR UNITS (PDCU). THEY CONNECT TO THE DPCs BASE T DATA BUS. THEY CONNECT TO THE DPCs BY TWO DATA BUSES. THEY MONITOR LFDS SWITCH SELECTIONS.

HOW MANY PROGRAM SWITCH MODULE INPUTS ARE USED BY EACH DISPLAY PROCESSOR COMPUTER TO SET POSITION AND AIRFRAME TYPE?. TWO. THREE. SIX.

11- which air/ground sensing input is used by the weu?. SYSTEM 1 FROM THE NOSE WHEEL. SYSTEM 1 FROM TRUCK TALT. SYSTEM 1 FROM MAIN GEAR COMPRESSED.

ATA 24 12- TO WHICH BUS BAR DOES THE SECONDARY EXTERNAL POWER CONNECT DIRECTLY TO?. LEFT AC BUS. TIE BUS. RIGHT AC BUS.

ATA 24 13- WHAT COORDINATES THE NO-BREAK POWER TRANSFERS?. L/R GENERATOR CONTROL UNITS (GCU). APU GCU. BUS POWER CONTROL UNIT (BPCU).

ATA 29 14- WHERE DOES THE LEFT RESERVOIR QUALITY SENSOR CONNECT TO ELECTRICALLY FOR THE LFDS?. TO A DATA CONCENTRATOR UNIT. DIRECT TO THE LEFT DPC. TO A HYDRAULIC MONITOR UNIT.