1.- A BATTERY FAULT LIGHT WILL ILLUMINATE WHEN: A - THE BATTERIES HAVE AUTO DISCONNECTED DUE TO LOW VOLTAGE. B - BATTERY VOLTAGE DROPS BELOW A PREDETERMINED LEVEL. C - BATTERY CHARGING CURRENT INCREASES AT AN ABNORMAL RATE.
2.- A BATTERY FAULT LIGHT WILL ILLUMINATE WHEN: A - THE BATTERIES HAVE AUTO DISCONNECTED DUE TO LOW VOLTAGE. B - BATTERY VOLTAGE DROPS BELOW A PREDETERMINED LEVEL. C - BATTERY CHARGING CURRENT INCREASES AT AN ABNORMAL RATE.
3.- AFTER IDG DISCONNECTION WHY DO YOU GET A GALLEY SHED INDICATION ON THE SD? A - IT IS A REMINDER TO PUSH THE GALLEY PUSHBUTTON TO MANUALLY SHED THE MAIN GALLEY. B - IT IS A REMINDER TO GET THE FLIGHT ATTENDANTS TO SWITCH OFF GALLEY EQUIPMENT TO DECREASE THE LOAD ON THE REMAINING GENERATOR. C - IF IT IS A REMINDER THAT THE MAIN GALLEY HAS BEEN SHED AUTOMATICALLY FOLLOWING THE LOSS OF ONE GENERATOR.
4.- AFTER LANDING, IN THE EMERGENCY ELECTRICAL CONFIGURATION: THE BATTERIES AUTOMATICALLY CONNECT TO THE DC BAT BUS WHEN SPEED DECREASES BELOW _____ KNOTS. A - 50 B - 70 C - 90 D - 100.
5.- AN AC ESS FEED SWITCH LOCATED ON THE OVERHEAD PANEL SHIFTS THE POWER SOURCE FOR THE AC ESS BUS FROM: A - AC BUS 1 TO AC BUS 2. B - AC BUS 1 TO AC GRND/FIT BUS. C - AC BUS 2 TO AC BUS 1.
6.- AN AC ESS FEED SWITCH LOCATED ON THE OVERHEAD PANEL SHIFTS THE POWER SOURCE FOR THE AC ESS BUS FROM A - AC BUS 1 TO AC BUS 2. B - AC BUS 1 TO AC GRND/FIT BUS. C - AC BUS 2 TO AC BUS 1.
7.- ARE THERE ANY LIMITATIONS ASSOCIATED WITH DISCONNECTING AN IDG? A - NEVER DISCONNECT AN IDG IN FLIGHT, OR PUSH THE IDG DISCONNECT PUSH BUTTON FOR MORE THEN 30 SECONDS. B - THERE IS NO LIMITATIONS. C - NEVER DISCONNECT AN IDG IN FLIGHT, OR PUSH THE IDG DISCONNECT PUSH BUTTON FOR MORE THEN 5 SECONDS. D - NEVER DISCONNECT AN IDG UNLESS THE ENGINE IS RUNNING NOR PUSH THE IDG DISCONNECT PUSH BUTTON FOR MORE THEN 3 SECONDS.
8.- BOTH BATTERIES ARE CHARGED BY THE EXTERNAL POWER UNIT. APPROXIMATELY HOW LONG DOES THE CHARGING PROCESS TAKE? A - 10 MINUTES. B - 20 MINUTES. C - 30 MINUTES. D - BETWEEN 30 & 45 MINUTES.
9.- CAN YOU RECONNECT AN IDG IN FLIGHT? A - YES, BUT ONLY AFTER CONTACTING MAINTENANCE CONTROL. B - YES,PUSH AND HOLD THE IDG PB UNTIL THE GEN FAULT LIGHT IS NO LONGER ILLUMINATED. C - NO. D - NONE OF THE ABOVE.
10.- DO NOT DEPRESS THE IDG DISCONNECT SWITCH FOR MORE THAN _____ TO PREVENT DAMAGE TO THE DISCONNECT MECHANISM. A - 3 SECONDS. B - 10 SECONDS. C - 15 SECONDS.
11.- DURING A ROUTINE FLIGHT, WICH OF THE FOLLOWING WOULD RESULT AFTER THE LOSS OF GEN #2 AND THE SUBSEQUEND START OF THE APU? A - THE APU WOULD NOW POWER BOTH SIDES OF THE ELECTRICAL SYSTEM. B - ALL SYSTEMS RETURN TO NORMAL AND THE RAT MUST BE RESTORED. C - ENG GEN #1 CONTINUES TO POWER AC BUS #1 AND DOWNSTREAM SYSTEMS. THE APU POWERS AC BUS #2 AND DOWNSTREAM SYSTEMS.
12.- DURING THE FIVE SECONDS IT TAKES FOR THE RAT TO EXTEND: A - THE BATTERIES POWER BOTH BATT HOT BUSSES, ESS DC SHED, AND ESS AC SHED THROUGH THE STATIC INVERTER. B - THE BATTERIES POWER BOTH BATT HOT BUSSES, ESS DC, AND ESS AC THROUGH THE STATIC INVERTER. C - THE STATIC INVERTER POWERS BOTH BATT HOT BUSSES ESS DC, AND ESS AC THROUGH THE ESS AC SHED BUSSES. D - THE BATTERIES POWER BOTH BATT HOT BUSSES.
13.- ENGINE #1 HAS JUST BEEN STARTED AND THE APU IS INOPERATIVE. THE EXT PWR PUSH BUTTON BLUE ON LIGHT IS ILLUMINATED. WHICH OF THE STATEMENTS BELOW IS CORRECT? A - EXTERNAL POWER IS SUPPLYING AIL ELECTRICAL NEEDS. B - ENGINE GEN #1 IS SUPPLYING AC BUS #1 AND THE DOWNSTREAM SYSTEMS, AND AC BUS #2 THROUGH THE BUS TIE CONTACTORS. C - GEN #1 SUPPLIES AC BUS #1 AND (GENERALLY) THE DOWNSTREAM SYSTEMS; EXT POWER SUPPLIES AC BUS #2.
14.- FOR THE A-320 THE EMERGENCY GENERATOR SUPPLIES POWER AS LONG AS RAT IS DEPLOYED AND: A - THE LANDING GEAR IS DOWN. B - IF THE RAT STALLS OR IF THE AIRCRAFT IS ON THE GROUND WITH THE SPEED BELOW 100 KTS. C - THE LANDING GEAR IS UP.
15.- HAVING STARTING THE APU, HOW CAN YOU GET THE APU GENERATOR TO POWER THE ELECTRICAL SYSTEM? A - THE APU GENERATOR MUST BE SWITCH ON. B - BY PUSHING THE EXT PWR PUSHBUTTON THUS DISCONNECTING THE EXTERNAL POWER. C - BY PUSHING THE BUS TIE PUSHBUTTON D - YOU ARE UNABLE TO AS THE APU POWER OUTPUT IS OUTSIDE NORMAL PARAMETERS.
16.- HOW MANY TIMES CAN YOU RESET A CIRCUIT BREAKER? A - ONCE B - ONCE, IF AUTHORIZED BY THE PROCEDURES. C - TWICE. D - TWICE, IF AUTHORIZED BY THE PROCEDURES.
17.- IF BATTERIES ARE THE ONLY SOURCE OF POWER IN FLIGHT, HOW LONG WILL BATTERY POWER BE AVAILABLE? A - BETWEEN 22 AND 30 MINUTES DEPENDING ON EQUIPMENT IN USE. B - UNTIL THE APU IS STARTED. C - TWO HOURS AND 30 MINUTES DEPENDENT ON EQUIPMENT IN USE. D - 45 MINUTES DEPENDENT ON EQUIPMENT IN USE.
18.- IF BATTERIES ARE THE ONLY SOURCE OF POWER IN FLIGHT, HOW LONG WILL BATTERY POWER BE AVAILABLE? A - BETWEEN 22 AND 30 MINUTES DEPENDING ON EQUIPMENT IN USE. B - UNTIL THE APU IS STARTED. C - TWO HOURS AND 30 MINUTES DEPENDENT ON EQUIPMENT IN USE. D - 45 MINUTES DEPENDENT ON EQUIPMENT IN USE.
19.- IF BOTH ENGINE GENERATORS ARE POWERING THE SYSTEM, AND ONE SUBSEQUENTLY FAILS. ARE ANY BUSSES UNPOWERED? A - ONLY THE AC ESS SHED BUS. B - NO, BUT SOME LOADS ARE SHED IN BOTH MAIN GALLEYS. C - YES, THOSE ASSOCIATED WITH THE FAILED GENERATOR.
20.- IF BOTH ENGINE GENERATORS ARE POWERING THE SYSTEM, AND ONE SUBSEQUENTLY FAILS. ARE ANY BUSSES UNPOWERED A - ONLY THE AC ESS SHED BUS. B - NO, BUT SOME LOADS ARE SHED IN BOTH MAIN GALLEYS. C - YES, THOSE ASSOCIATED WITH THE FAILED GENERATOR.
21.- IF DURING A NORMAL FLIGHT THE BUS TIE PUSH BUTTON IS DEPRESSED TO OFF, WHAT EFFECT WOULD THIS HAVE ON POWER TO THE BUSSES? A - NONE. B - ALL POWER WOULD BE LOST AND THE AIRCRAFT WOULD BE POWERED BY THE BATTERIES UNTIL THE RAT WAS UP TO SPEED. C - THE POWER TRANSFER WOULD SWITCH TO THE OPPOSITE BUS. D - THIS IS NOT POSSIBLE AS THE BUS TIE CONTACTORS ARE LOCKED OUT DURING FLIGHT.
22.- IF EXTERNAL POWER IS AVAILABLE AND WITHIN LIMITS: A - IT WILL AUTOMATICALLY CLOSE THE BUS TIE CONTACTORS WHEN CONNECTED BY THE GROUND CREW. B - THE GREEN AVAIL LIGHT WILL ILLUMINATE ON THE EXT PWR PUSH BUTTON. C - THE BUS TIE PUSH BUTTON ILLUMINATES. D - NONE OF THE ABOVE.
23.- IF EXTERNAL POWER IS AVAILABLE AND WITHIN LIMITS: A - IT WILL AUTOMATICALLY CLOSE THE BUS TIE CONTACTORS WHEN CONNECTED BY THE GROUND CREW. B - THE GREEN AVAIL LIGHT WILL ILLUMINATE ON THE EXT PWR PUSH BUTTON. C - THE BUS TIE PUSH BUTTON ILLUMINATES.
24.- IF NORMAL ELECTRICAL POWER IS LOST; ESSENTIAL COCKPIT LIGHTING IS MAINTAINED FOR THE: A - CAPTAIN'S INSTRUMENT PANEL. B - STANDBY COMPASS. C - RIGHT DOME LIGHT (PROVIDED THE DOME SELECTOR IS NOT OFF). D - ALL OF THE ABOVE.
25.- IF THE BATTERY VOLTAGES ARE BELOW THE MINIMUM, HOW DO YOU CHARGE THEM? A - YOU HAVE TO CALL A MECHANIC BECAUSE THE BATTERIES CAN ONLY BE CHARGED BY MAINTENANCE. B - I HAVE TO CHECK THAT THE BAT PUSHBUTTONS ARE ON AND SWITCH THE EXTERNAL POWER ON.
26.- IF THE BATTERY VOLTAGES ARE BELOW THE MINIMUM, HOW DO YOU CHARGE THEM? A - YOU HAVE TO CALL A MECHANIC BECAUSE THE BATTERIES CAN ONLY BE CHARGED BY MAINTENANCE. B - I HAVE TO CHECK THAT THE BAT PUSHBUTTONS ARE ON AND SWITCH THE EXTERNAL POWER ON.
27.- IF THE SOURCE OF POWER FOR THE ESS AC BUS IS LOST, DOES ANOTHER SOURCE OF POWER AUTOMATICALLY POWER THE BUS? A - YES, TRANSFER IS AUTOMATIC. B - YES, ONLY IF AUTO WAS SELECTED ON THE AC ESS FEED PUSH BUTTON. C - NO, THIS MUST BE DONE BY THE CREW.
28.- IN CRUISE, YOU HAVE SUDDENLY A MASTER WARNING AND CAUTION COMES ON WITH ELEC EMER CONFIG AND APP OFF. YOU NOTICE A RED FAULT LIGHT ON THE RAT & EMER GEN PUSHBUTTON. WHAT DO YOU THINK OF THIS INDICATION? A - THE EMER GEN IS NOT YET SUPPLYING THE SYSTEM. B - THE RAT HAS FAILED. YOU WILL HAVE TO TURN THE BATTERIES TO OFF. C - THE FAULT LIGHT IS ALWAYS ON WHEN ARE IN SLEC EMER CONFIG. D - THE RAT HAS FAILED. YOU HAVE TO TRY TO RECONNECT BOTH IDC/S.
29.- IS IT POSIBLE TO DETERMINE THE SOURCE OF POWER FOR AIRCRAFT BUSSES? A - IT IS INDICATED ON THE ELECTRICAL SCHEMATIC OVERHEAD. B - NO. C - ONLY WHEN OPERATING IN THE EMERGENCY ELECTRICAL CONFIGURATION. D - YES, PRESS THE ECAM ELEC PUSH BUTTON AND VIEW THE ELECTRICAL SHEMATIC ON THE ECAM.
30.- IS IT POSSIBLE TO PARALLEL GENERATORS? A - OF COURSE YES. B - ONLY WITH THE RAT DEPLOYED. C - THE ELECTRICAL SYSTEM WILL NOT ALLOW "PARALLELING" OF GENERATORS. D - ONLY ONE ENGINE GENERATOR MAY BE PARALLELED WITH THE APU.
31.- ON THE COCKPIT OVERHEAD PANEL, THERE IS A THREE POSITIONS EMERGENCY EXIT LIGHT SWITCH. WHAT LIGHTS ARE ASSOCIATED WITH THIS SWITCH. A - EXIT SIGNS, EMERGENCY LIGTHS, AND ESCAPE PATH LIGHTING. B - EXIT SIGNS, EMERGENCY LIGHTS, MAIN PANEL FLOOD LIGHTS, AND ESCAPE PATH LIGHTING. C - EXIT SIGNS, EMERGENCY LIGHTS, DOME LIGHTS, MAIN PANEL FLOOD LIGHTS, AND THE STANDBY COMPASS LIGHTS.
32.- THE A-320 HAS _______ BATTERIES IN ITS MAIN ELECTRICAL SYSTEM. A - 1 B - 2 C - 3.
33.- THE AC ESSENTIAL BUS IS POWERED BY THE BATTERY AT SPEED ABOVE 50 KT. A - TRUE. B - FALSE.
34.- THE BAT FAULT LIGHT WILL ILLUMINATE WHEN: A - BATTERY VOLTAGE IS LOW. B - CHARGING CURRENT INCREASES AT AN ABNORMAL RATE. C - CHARGING CURRENT DECREASES AT AN ABNORMAL RATE.
35.- THE BATTERY BUS IS NORMALLY POWERED BY: A - DC BUS 2. B - DC BUS 1 AND DC BUS 2. C - DC BUS 1 THROUGH A DC TIE CONTROL RELAY. D - DC BUS 2 THROUGH A DC TIE CONTROL RELAY.
36.- THE DC BAT BUS IS NORMALLY POWERED BY: A - THE A-320 HAS ______ BATTERIES IN ITS MAIN ELECTRICAL SYSTEM. B - DC BUS 2. C - BATTERIES. D - DC BUS 1.
37.- THE ENGINE GENERATORS AND APU GENERATOR ARE RATED AT _______ KVA. A - 50 B - 90 C - 45.
38.- THE GALLEY FAULT LIGHT ILLUMINATES WHEN ANY GENERATOR IS EXCEEDING 80% OF ITS RATED OUTPUT. A - TRUE. B - FALSE.
39.- THE IDG FAULT LIGHT INDICATES: A - AN IDG OIL OVERHEATS. B - IDG LOW OIL PRESSURE. C - IDG HAS BEEN DISCONNECTED. D - EITHER A OR B.
40.- THE NORMAL PRIORITY FOR SUPPLYING ELECTRICAL POWER TO THE AC BUSSES IS: A - EXTERNAL POWER, ENGINE GENERATORS, APU. B - APU, EXTERNAL POWER, ENGINE GENERATORS. C - ENGINE GENERATORS, EXTERNAL POWER, APU.
41.- THE NUMBER 1 AC BUS CHANNEL NORMALLY SUPPLIES POWER TO _____ AND TO THE _____ BUS. A - TR2/AC ESS SHED/DC ESS SHED. B - TR1/AC ESS SHED / DC ESS. C - TR1/AC ESS / AC ESS SHED. D - TR1 /AC ESS / DC ESS SHED.
42.- THE NUMBER 1 AC BUS CHANNEL NORMALLY SUPPLIES POWER TO _____ AND TO THE _____ BUS. A - TR1, DC 1 B - TR1, AC ESS. C - NONE OF ABOVE.
43.- THE PURPOSE OF THE AUTO BUS TIE IS TO ALLOW EITHER ENGINE-DRIVEN IDG TO AUTOMATICALLY POWER BOTH MAIN AC BUSES IN THE EVENT OF A GENERATOR LOSS UNTIL EITHER GROUND POWER OR THE APU GENERATOR IS ACTIVATED. A - TRUE B - FALSE.
44.- THE RAT IS CONNECTED DIRECTLY (MECHANICALLY) TO THE EMERGENCY GENERATOR. A - TRUE. B - FALSE.
45.- WHAT COCKPIT LIGHTING IS AVAILABLE DURING AN EMERGENCY ELECTRICAL SITUATION? A - EMERGENCY PATH LIGHTING ONLY. B - RIGHT SIDE DOME LIGHT, MAIN PANEL FLOOD LIGHTS (LEFT TWO COLUMNS ONLY), AND THE STANDBY COMPASS LIGHT. C - LOCATED ON NORMAL CIRCUIT BREAKER PANELS. D - RIGHT SIDE DOME LIGHT, MAIN PANEL FLOOD LIGHTS, AND THE STANDBY COMPASS LIGHT.
46.- WHAT DOES THE BLUE EXT PWR ON LIGHT MEAN? A - EXTERNAL POWER IS PLUGGED IN AND PARAMETERS ARE NORMAL. B - EXTERNAL POWER IS SUPPLYING THE AIRCRAFT S ELECTRICAL SYSTEM. C - THERE IS A FAULT WITH THE EXTERNAL POWER.
47.- WHAT IS THE FUNCTION OF APU GEN PUSH BUTTON LOCATED ON THE OVERHEAD ELECTRICAL PANEL? A - PUSH THIS BUTTON TO AUTOMATICALLY START THE APU B - WHEN SELECTED TO OFF THE APU GENERATOR FIELD IS DE-ENERGIZED. C - BOTH ARE CORRECT.
48.- WHAT IS THE FUNCTION OF THE GEN 1 LINE PUSH BUTTON? A - WHEN SELECTED OFF THE AVIONICS COMPARTMENT ISOLATION VALVES CLOSE. B - WHEN SELECTED OFF THE #1 GENERATOR POWERS ALL AC BUSES. C - WHEN SELECTED OFF GENERATOR #1 IS REMOVED FROM ALL BUSSES BUT CONTINUES TO POWER ONE FUEL PUMP IN EACH WING.
49.- WHAT IS THE MEANING OF THE GREEN AVAIL LIGHT? A - EXTERNAL POWER IS PLUGGED IN AND PARAMETERS ARE NORMAL. YOU MUST PUSH THE EXTERNAL POWER TO CONNECT IT. B - EXTERNAL POWER IS AVAILABLE TO THE BATTERIES ONLY. C - THE EXTERNAL POWER PANEL DOOR HAS BEEN OPENED. D - EXTERNAL POWER IS SUPPLYING THE AIRCRAFT SYSTEMS.
50.- WHAT IS THE MINIMUM VOLTAGE WHEN CONSULTING A BATTERY CHECK? A - 28 VOLTS. B - LESS THAN 60 AMPS IN 10 SECONDS. C - GREATER THAN 25 VOLTS.
51.- WHAT IS THE PRIORITY OF ELECTRICAL SOURCES? A - EXTERNAL POWER, GEN #1 AND #2, APU. B - APU, EXTERNAL POWER (IF SELECTED), GEN #1 AND #2. C - APU, GEN #2 OR #1, EXTERNAL POWER (IF SELECTED D - GEN #1 OR #2, EXTERNAL POWER (IF SELECTED), APU.
52.- WHAT IS THE SIGNIFICANCE OF THE CIRCUIT BREAKERS ON THE OVERHEAD PANEL? A - THEY ARE NOT MONITORED BY ECAM B - CANNOT BE RESET. C - THEY MAY BE OPERATIONAL IN THE EMERGENCY ELECTRICAL CONFIGURATION.
53.- WHAT IS THE SIGNIFICANCE OF THE CIRCUIT BREAKERS ON THE OVERHEAD PANEL? A - THEY ARE NOT MONITORED BY ECAM. B - CANNOT BE RESET. C - THEY MAY BE OPERATIONAL IN THE EMERGENCY ELECTRICAL CONFIGURATION.
54.- WHAT WOULD CAUSE THE GALLEY FAULT LIGHT TO ILLUMINATE? A - THE FLIGHT ATTENDANTS HAVE ALL THE COFFEE MAKERS AND OVENS ON AT ONCE. B - THE MAIN GALLEY HAS SHED. C - THE LOAD ON ANY GENERATOR IS ABOVE 100% OF ITS RATED OUTPUT. D - THE AFT GALLEY HAS SHED.
55.- WHEN ARE THE ESSENTIAL SHEED BUSES POWERED BY HIS BATTERY? A - NEVER. THE PURPOSE OF THE SHED BUSES IS TO REDUCE THE LOAD ON THE BATTERIES. B - IN CASE OF DOUBLE GENERATOR FAILURE. C - AFTER EVERY IDG CONNECTION.
56.- WHEN DOES THE RAT AUTOMATICALLY DEPLOY? A - WITH THE LOSS OF TWO HYDRAULIC SYSTEMS. B - ELECTRICAL POWER TO BOTH AC BUS #1 & #2 IS LOST AND THE AIRCRAFT SPEED IS ABOVE 100 KNOTS. C - BOTH ARE CORRECT.
57.- WHEN DOES THE RAT AUTOMATICALLY DEPLOY? A - WITH THE LOSS OF TWO HYDRAULIC SYSTEMS. B - ELECTRICAL POWER TO BOTH AC BUS #1 & #2 IS LOST AND THE AIRCRAFT SPEED IS ABOVE 100 KNOTS. C - BOTH ARE CORRECT.
58.- WHEN NO OTHER POWER IS AVAILABLE IN FLIGHT, THE STATIC INVERTER CONVERTS POWER TO AC POWER FOR THE ____ BUS, AND _____ POWERS THE _____ BUS. A - BAT1 DC /AC ESS BUS /BAT2 /DC ESS. B - BAT1 DC / AC ESS SHED /BAT2 /DC ESS SHED. C - BAT1 DC / AC ESS BUS /BAT2 /DC ESS SHED.
59.- WHEN WILL THE RAT & EMER GEN RED FAULT LIGHT MOMENTARY ILLUMINATES? A - WHEN THE EMER GEN IS NOT SUPPLYING ELECTRICAL POWER, AC BUSSES # 1 &. #2 ARE UNPOWERED AND THE NOSE GEAR IS UP. B - WHEN THE RAT IS DEPLOYED USING HYDRAULIC RAT MAN ON PUSH BUTTON. C - BOTH ARE CORRECT.
60.- WHICH BUSSES WILL BE POWERED AFTER THE RAT IS EXTENDED AND THE EMER GEN BEGINS PRODUCING POWER? A - BATT HOT BUSSES, ESS DC, ESS DC SHED, ESS AC AND ESS AC SHED. B - THE STATIC INVERTER WOULD POWER BOTH HOT THE STATIC INVERTER WOULD POWER BOTH HOT BATT BUSSES, ESS DC AND ESS AC THROUGH THE ESS AC SHED BUSSES. C - THE BATTERIES WOULD POWER BOTH HOT BATT BUSSES, ESS DC AND ESS AC THROUGH THE STATIC INVERTER. D - ESS DC, ESS DC SHED, ESS AC AND ESS AC SHED.
61.- WHICH COMMUNICATION AND NAVIGATION RADIOS ARE OPERATIONAL IN THE EMERGENCY ELECTRICAL CONFIGURATION WITH THE EMER GEN POWERING THE SYSTEM? A - ACP 1 AND 2, VHF 1, HF, RMP 1, VOR 1, AND ILS 1. B - VHF L, RMP L, VOR L. C - RMP #1 &. #2, VHF #1, HF (IF EQUIPPED), ACP #1, VOR#1 AND ILS #1:. D - ALL RADIOS ARE LOST.
62.- WHICH FLIGHT CONTROL COMPUTERS ARE OPERATIONAL IN THE EMERGENCY ELECTRICAL POWER CONFIGURATION (GEAR DOWN AND BATTERIES POWERING THE SYSTEM)? A - ALL ARE OPERATIONAL. B - ELAC 1, SEC 1 AND FAC 1. C - ELAC 1 AND 2, SEC 1 AND 2 FAC 1. D - ELAC 1 AND SEC 1.
63.- WHICH FLIGHT CONTROL COMPUTERS ARE OPERATIONAL IN THE EMERGENCY ELECTRICAL POWER CONFIGURATION (GEAR DOWN AND BATTERIES POWERING THE SYSTEM)? A - ALL ARE OPERATIONAL. B - ELAC 1, SEC 1 AND FAC 1. C - ELAC 1 AND 2, SEC 1 AND 2 FAC 1. D - ELAC 1 AND SEC 1.
64.- WHICH FLIGHT CONTROL COMPUTER WILL BE INOPERATIVE WITH GEAR EXTENSION WHILE IN THE EMERGENCY ELECTRICAL CONFIGURATION? A - FAC 1 AND ELAC 1 B - SEC 1 C - SEC 1 AND ELAC 1 D - FAC 1.
65.- WHICH OF THE FOLLOWING AC BUSSES CAN BE POWERED BY THE EMERGENCY GENERATOR? A - AC BUS 1. B - AC BUS 2. C - AC ESS BUS / AC ESS SHED BUS.
66.- WHICH OF THE FOLLOWING AC BUSSES THE EMERGENCY GENERATOR CAN POWER? A - AC BUS 1. B - AC BUS 2. C - AC ESS BUS.
67.- WHICH RADIOS ARE INOPERATIVE WITH GEAR EXTENSION WHILE IN THE EMERGENCY ELECTRICAL CONFIGURATION? A - DME 1 AND TRANSPONDER 1. B - DME 1, DDRM1, AND TRANSPONDER 1. C - DME, AND TRANSPONDER. D - ILS 2 DME, AND ADF.
68.- WHICH VOLTAGE REQUIRES RECHARGING OR REPLACING THE BATTERIES? A - 20 VOLTS. B - 24 VOLTS OR LESS. C - 25 VOLTS OR LESSD 26 VOLTS OR LESS.
69.- WHILE OPERATING ON EMERGENCY ELECTRICAL POWER WITH THE LANDING GEAR LOWERED WICH OF THE FOLLOWING CONTROL LAWS IS IN EFFECT? A - BACKUP. B - DIRECT. C - ALTERNATE D - BACKUP OR ALTERNATE.
70.- WHILE OPERATING ON EMERGENCY ELECTRICAL POWER (EMER GEN POWERING THE SYSTEM) WHAT SHOULD THE CREW ACCOMPLISH PRIOR TO LOWERING THE LANDING GEAR? A - CHECK TO SEE THAT THE FMGC HAS AUTO TUNED THE APPROPRIATE NAV FACILITY FOR THE APPROACH TO BE ACCOMPLISHED. B - DEPRESS THE GUARDED RMP NAV PUSH BUTTON AND TUNE THE APPROPRIATE NAV FACILITY AND COURSE FOR THE APPROACH TO BE ACCOMPLISHED. C - BOTH ARE CORRECT.
71.- WHILE OPERATING ON EMERGENCY ELECTRICAL POWER (EMER GEN POWERING THE SYSTEM, FAC #1 RESET) WHICH OF THE FOLLOWING CONTROL LAWS ARE IN EFFECT? A - MANUAL B - ALTERNATE. C - BACKUP D - MANUAL AND BACKUP.
72.- WHILE OPERATING ON EMERGENCY ELECTRICAL POWER (EMER GEN POWERING THE SYSTEM) HOW IS IT POSSIBLE TO PROPERLY COMPLETE THE ECAM CHECKLIST WITH ONLY AN UPPER DISPLAY? A - DEPRESS AND HOLD THE SPECIFIC ECAM PAGE PUSH BUTTON ON THE ECAM CONTROL PANEL B - TRANSFER OCCURS AUTOMATICALLY. C - THIS IS NOT POSSIBLE. USE THE COCKPIT OPERATING MANUAL.
73.- WHILE OPERATING ON EMERGENCY ELECTRICAL POWER WITH THE LANDING GEAR LOWERED WITCH OF THE FOLLOWING CONTROL LAWS IS IN EFFECT? A - BACKUP. B - DIRECT. C - ALTERNATE. D - MANUAL AND BACKUP.
74.- WHILE OPERATING ON EMERGENCY ELECTRICAL POWER WITH THE LANDING GEAR LOWERED WITCH OF THE FOLLOWING STATEMENTS IS CORRECT? A - IF THE APU IS NOT OPERATING IT SHOULD BE STARTED AT THIS TIME. B - THE APU WILL NOT START UNTIL THE AIRCRAFT HAS COME TO A COMPLETE STOP AND ALL POWER HAS BEEN REMOVED FOR 15 SECONDS. C - ON THE GROUND AT 100 KNOTS, THE DC BATTERY BUS AUTOMATICALLY RECONNECTS TO THE BATTERIES ALLOWING APU START. D - AT 70 KNOTS ESS AC IS DISCONNECTED FROM THE BATTERIES.
75.- YOU ENTER A DARK COCKPIT, WHAT ACTION IS NECESSARY BEFORE CHECKING THE BATTERY VOLTAGES? A - YOU HAVE TO CHECK THAT THE EXTERNAL POWER IS ON. B - YOU HAVE TO ENSURE THAT AT LEAST ONE BATTERY IS ON. C - YOU HAVE TO ENSURE THAT BOTH BATTERIES ARE ON. D - YOU HAVE TO VERIFY THAT BOTH BATTERIES ARE OFF.
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