Landing Gear Light Doors

ALL CABIN SIGNS COME ON AUTOMATICALLY WHEN THE CABIN ALTITUDE EXCEEDS_________ FEET, REGARDLESS OF THE RESPECTIVE SWITCH POSITION. A - 9.550. B - 10.000. C - 11.300.

AS LONG AS THE LANDING GEAR LEVER IS UP A HYDRAULIC SAFETY VALVE CLOSES TO CUT OFF THE HYDRAULIC SUPPLY TO THE GEAR WHEN THE AIRSPEED IS: A - GREATER THAN 260 KIAS. B - GREATER THAN 230 KIAS. C - LESS THAN 260 KIAS.

AUTO BRAKE MAY BE ARMED WITH THE PARKING BRAKE ON. A - TRUE. B - FALSE.

AUTO BRAKES, IF SELECTED, WILL ONLY BE ACTIVATED BY: A - THE WHEELS SPINNING UP. B - THE STRUTS BEING COMPRESSED. C - THE BRAKE PEDALS BEING DEPRESSED. D - THE GROUND SPOILER EXTENSION COMMAND.

AUTOBRAKING IS INITIATED BY. A - STRUT COMPRESSION. B - REVERSER ACTION. C - GROUND SPOILER EXTENSION COMMAND.

CAN NORMAL LANDING GEAR OPERATION BE RESTORED AFTER A GRAVITY EXTENSION IF GREEN HYDRAULIC PRESSURE IS AVAILABLE?. A - RESTORATION IS ALWAYS POSSIBLE. B - IT MAY BE POSSIBLE IF THE GRAVITY EXTENSION WAS NOT CAUSED BY A FAILURE OF THE LANDING GEAR MECHANISM. C - NO, ONLY MAINTENANCE CAN RESTORE NORMAL OPERATION.

CAN THE FLIGHT COMPARTMENT SLIDING WINDOWS BE USED AS EMERGENCY EXITS?. A - YES, IN THE COCKPIT COAT CLOSET IS A ROPE LADDER THAT CAN BE USED IN SUCH AN EVENT. B - YES, THERE ARE ESCAPE ROPES MOUNTED ABOVE EACH WINDOW BEHIND AN ACCESS PANEL. C - NO. THEY ARE NOT APPROVED EMERGENCY EXITS. D - NO, THEY ARE TOO SMALL.

CAN THE GEAR BE EXTENDED ABOVE 260 KTS IF NECESSARY?. A - NEVER. B - YES, BUT MANUALLY ONLY. C - YES, BUT THE ULTIMATE LIMIT IS 285 KT CAS.

DURING PUSHBACK, YOU START ENGINE #2. YOU OBSERVE THE NW STRG DISC MEMO HAS CHANGED TO AMBER. WHY?. A - THE NW STRG DISCONNECT MECHANISM HAS FAILED. B - THE YELLOW HYDRAULIC SYSTEM IS NOW PRESSURIZED AND THE AMBER CAPTION IS A WARNING NOT TO MOVE THE HANDWHEEL. C - THE NOSE WHEEL STEERING IS BEING RECONNECTED BY GROUND PERSONNEL. IT IS AMBER BECAUSE THE PIN IS REMOVED. D - THE MEMO HAS BECOME AMBER BECAUSE ONE ENGINE IS RUNNING.

EACH MAIN WHEEL HAS AN ANTISKID BRAKE. A - TRUE. B - FALSE.

EACH PASSENGER DOOR HAS ONE CABIN PRESSURE WARNING LIGHT THAT: A - WARNS OF RESIDUAL PRESSURE IN THE CABIN. B - SHOWS A POSSIBLE UNLOCKED DOOR. C - BOTH ARE CORRECT.

ECAM: IF YOU SEE A GREEN ARC SHOWN OVER A WHEEL INDICATION. A - IT MARKS THE HOTTEST BRAKE WITH A TEMPERATURE OF MORE THAN 100°C. B - IT INDICATES AN ABNORMAL HIGH TEMPERATURE. C - THE A/SKID SYSTEM IS AUTOMATICALLY RELEASING THE PRESSURE OF THAT BRAKE. D - THEL/G CONTROL SYSTEM HAS DETECTED A LOW TIRE PROFILE.

HOW CAN THE BRAKE ACCUMULATOR BE RE-PRESSURIZED?. A - WITH THE YELLOW ELECTRIC HYDRAULIC PUMP. B - WITH THE BLUE ELECTRIC HYDRAULIC PUMP. C - BOTH ARE CORRECT.

HOW DO YOU MANUALLY EXTEND THE LANDING GEAR?. A - LIFT THE RED HANDLE AND TURN ANTICLOCKWISE 4 TURNS. B - LIFT THE RED HANDLE AND TURN ANTICLOCKWISE A MINIMUM OF 2 TURNS. C - LIFT THE RED HANDLE AND TURN CLOCKWISE A MINIMUM OF 4 TURNS. D - LIFT THE RED HANDLE AND TURN CLOCKWISE A 3 TUNS.

HOW IS CREW OXYGEN PROVIDE?. A - FROM A SINGLE BOTTLE. B - THERE IS ONE BOTTLE PER CREW MEMBER EXCEPT FOR JUMP SEATS. C - OXYGEN GENERATOR. D - ONE OXYGEN BOTTLE WITH AN OXYGEN GENERATOR.

HOW IS IT DETERMINED THAT THE COCKPIT SLIDING WINDOW IS CLOSED AND LOCKED?. A - THE RED RING BELOW THE RELEASE BUTTON SHOULD NOT BE IN VIEW. B - THE RED RING BELOW THE RELEASE BUTTON SHOULD BE IN VIEW. C - THE LOCKING PIN WAS PLACED IN THE FORWARD POSITION WHEN THE WINDOW WAS CLOSED. D - THE PIN IS ENGAGED.

HOW MANY CABIN ENTRANCE, OVERWING EMERGENCY EXITS AND CARGO DOORS ARE ON THE A320?. A - FOUR CABIN, TWO OVERWINGS, AND TWO CARGO, PLUS THE BULK CARGO. B - FOUR CABIN, FOUR OVERWINGS , AN TWO CARGO, PLUS THE BULK CARGO. C - TWO CABIN, FOUR OVERWINGS, AND THREE CARGO, PLUS THE BULK CARGO.

HOW MANY TURNS ARE REQUIRED ON THE GRAVITY EXTENSION HAND CRANK TO EXTEND THE LANDING GEAR?. A-2. B-3. C-5. D-6.

IF DOOR HANDLE IS LIFTED AND THE WHITE INDICATOR ILLUMINATES, WHAT DOES THIS MEAN?. A - THE ESCAPE SLIDE IS ARMED AND IF YOU GO ON LIFTING THE HANDLE, DOOR OPENS AND SLIDE WILL DEPLOY. B - PNEUMATIC ASSISTANCE OF THE DOOR HAS FAILED. C - THE ESCAPE SLIDE IS IN DISARMED CONFIGURATION. D - THE CABIN IS STILL PRESSURIZED.

IF NORMAL ELECTRICAL POWER IS LOST, ESSENTTIAL 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 OFF THE ABOVE.

IF THE ACCUMULATOR ON THE ALTERNATE BRAKE SYSTEM IS YOUR ONLY SOURCE PRESSURE, WHICH OF THE FOLLOWING WILL BE AVAILABLE?. A - AUTO BRAKES AND ANTISKID. B - ANTISKID. C - SEVEN APPLICATIONS OF THE BRAKE PEDALS. D - THREE APPLICATIONS OF THE BRAKE PEDALS.

IF THE BRAKE SYSTEM AUTOMATICALLY TRANSITIONS TO ALTERNATE BRAKES WITH THE A/SKID & N/W STRG SWITCH IN THE ON POSITION, WHICH OF THE FOLLOWING WILL BE AVAILABLE?. A - AUTO BRAKES AND ANTI-SKID. B - ONLY AUTO BRAKES. C - BRAKES, AUTO BRAKES, ANTI-SKID. D - ANTI-SKID.

IF THE BSCU DETECTS A BRAKE SYSTEM MALFUNCTION IN FLIGHT WITH THE A/SKID & N/W STRG SWITCH IN THE ON POSITION. A - THE CREW WILL BE NOTIFIED WITH AN ECAM MESSAGE AFTER TOUCHDOWN IF THE BRAKE SYSTEM DOES MALFUNCITION. B - THE CREW WILL BE NOTIFIED WITH AN ECAM MESSAGE. C - THE CREW MUST MANUALLY SELECT ALTERNATE BRAKES. D - ALL OF THE ABOVE.

IF THE LANDING GEAR WAS GRAVITY EXTENDED USING THE HAND CRANK ON THE CENTER PEDESTAL, LANDING GEAR POSITION MUST BE VERIFIED THROUGH. A - THE LANDING GEAR VIEWERS. B - THE LANDING GEAR INDICATIONS DEPICTED ON THE ECAM AND, IF AVAILABLE, THE CENTER PANEL LDG GEAR INDICATOR PANEL LIGHTS. C - BOTH ARE CORRECT.

IF THE LANDING GEAR WAS GRAVITY EXTENDED USING THE HAND CRANK ON THE CENTER PEDESTAL, WHAT OTHER SYSTEMS WILL BE INOPERATIVE?. A - NOSE WHEEL STEERING AND AUTO BRAKING. B - NOSE WHEEL STEERING ONLY. C - ANTI-SKID AND AUTO BRAKING. D - NOSE WHEEEL STEERING AND ANTI-SKID.

LANDING GEAR OPERATION IS INHIBITED AT SPEEDS: A - BELOW 100 KNOTS. B - ABOVE 260 +/- 5 KNOTS. C - BELOW 100 KNOTS AND ABOVE 260 KNOTS. D - ABOVE 250 KNOTS.

NOSE WHEELS AND MAIN WHEELS HAVE FUSIBLE PLUGS THAT PREVENT THE TIRES FROM BUSTING IF THEY OVERHEAT. A - TRUE. B - FALSE.

ON THE COCKPIT OVERHEAD PANEL THERE IS A THREE POSITION EMERGENCY EXIT LT SWITCH. WHAT LIGHTS ARE ASSOCIATED WITH THIS SWITCH?. A - EXIT SIGNS, EMERGENCY LIGHTS, AND FLOOR PATH LIGHTS. B - EXIT SIGNS, EMERGENCY LIGHTS, MAIN PANEL FLOOD LIGHTS, AND FLOOR PATH LIGHTS. C - EXIT SIGNS, EMERGENCY LITHTS, DOME LIGHTS, MAIN PANEL FLOOD LIGHTS, AND THE STANDBY COMPASS LIGHT. D - EXIT SIGNS, AND THE STANDBY COMPASS LIGHT.

ON THE ECAM DOOR/OXY PAGE, THE SLIDE INDICATION APPEARS ____ WHEN THE SLIDE IS NOT DISARMED. A - WHITE. B - AMBER. C - GREEN. D - RED.

ON THE E/WD, YOU NOTICE THE NW STRG DISC MEMO. WHAT DOES IT MEAN?. A - THE NOSE WHEEL STEERING HAS BEEN DISCONNNECTED BY GROUND PERSONNEL. B - A FAILURE IN THE NOSE WHEEL STEERING SYSTEM HAS BEEN DETECTED. C - THERE IS A DISCREPANCY BETWEEN THE TWO NOSE WHEEL STEERING HANDWHEEL POSITIONS. D - THE NOSE WHEEL STERRING COMPUTER HAS FINISHED ITS SELF TEST.

OPENING AN EMERGENCY OVERWING EXIT WILL: A - INFLATE THE SLIDE AT THE LEADING EDGE OF THE WING. B - AUTOMATICALLY INFLATE THE DOUBLE LANE SLIDE OFF THE TRAILING EDGE OF THE WING. C - ONLY ARM THE OVERWING SLIDE.

THE A-320 CARGO DOORS CAN BE OPERATED BY EITHER AN ___ OR A ____TO PRESSURIZE THE _____ HYDRAULIC SYSTEM. A - ELECTRIC PUMP, HAND PUMP, GREEN. B - MECHANICAL PUMP, HAND PUMP, YELLOW. C - ELECTRIC PUMP, HAND PUMP, YELLOW.

THE ALTERNATE BRAKE SYSTEM HAS THE SAME CAPABILITIES AS NORMAL BRAKES EXCEPT: A - ANTI-SKID IS INOPERATIVE. B - AUTOBRAKES ARE INOPERATIVE. C - BOTH A AND B.

THE ANTISKID DEACTIVATES WHEN GROUND SPEED IS LESS THAN _____. A - 10 KTS. B - 20 KTS. C - 25 KTS. D - 30 KTS.

THE AUTOBRAKE WILL ARM IF AT LEAST ONE ADIRS IS FUNCTIONNING. A - TRUE. B - FALSE.

THE BRAKES PRESSURE INDICATION ON TRIPLE PRESSURE INDICATOR READS WHICH SYSTEM PRESSURE?. A - YELLOW. B - BLUE. C - GREEN.

THE CARGO DOORS ARE POWERED BY: A - THE BLUE ELECTRIC PUMP. B - THE YELLOW HYDRAULIC SYSTEM BEFORE ENGINE START AND THE GREEN HYDRAULIC SYSTEM AFTER ENGINE START. C - THE YELLOW HYDRAULIC SYSTEM. D - THE BLUE HYDRAULIC SYSTEM BEFORE ENGINE START AND THE GREEN HYDRAULIC SYSTEM AFTER ENGINE START.

THE COCKPIT DOOR: A - CAN ONLY BE OPEN INTO THE COCKPIT. B - CAN ONLY OPEN INTO THE CABIN. C - NORMALLY OPENS INTO THE COCKPIT BUT CAN BE FORCED IN EITHER DIRECTION. D - SLIDES IN EITHER DIRECTION.

THE COCKPIT WINDOWS CAN BE OPENED BOTH FROM INSIDE AND OUTSIDE. A - TRUE. B - FALSE. C - FROM INSIDE ONLY.

THE ECAM WILL DISPLAY A DOOR NOT LOCKED IN: A - AMBER. B - RED. C - GREEN.

THE FORWARD AND AFT CARGO DOORS CAN BE OPENED FROM: A - THE INSIDE AND THE OUTSIDE. B - THE OUTSIDE ONLY.

THE GEAR DOORS REMAIN OPEN AFTER A MANUAL EXTENSION. A - TRUE. B - FALSE.

THE GREEN DECEL LIGHT ON THE AUTOBRAKE SWITCH ILLUMINATES WHEN THE ACTUAL AIRPLANE DECELERATION CORRESPONDS TO ________% OF THE SELECTED RATE. A - 80. B - 95. C - 100.

THE HALON FIRE EXTINGUISHER SHOULD BE USED ON WHAT TYPE FIRES?. A - ELECTRICAL FIRES ONLY. B - ELECTRICAL AND BURNING METALS. C - ELECTRICAL AND FLAMMABLE LIQUID FIRES. D - ELECTRICAL AND ORDINARY COMBUSTIBLES.

THE.............. HYDRAULIC SYSTEM PROVIDES POWER FOR GEAR EXTENSION/RETRACTION. A - YELLOW. B - BLUE. C - GREEN.

THE MAXIMUN DEGREE OF NOSE WHEEL STEERING AVAILABLE WHEN USING THE STEERING HANDWHEEL IS ________. A - +/- 60. B - +/- 75. C - +/- 95.

THE NORMAL BRAKE SYSTEM USES ________ HYDRAULIC PRESSURE AND THE ALTERNATE BRAKES USE_______ SYSTEM PRESSURE, WITH_____ BACKUP. A - GREEN, BLUE, AN ELECTRICAL. B - GREEN, YELLOW, AN ACCUMULATOR. C - GREEN, YELLOW, AN ELECTRICAL.

THE PARKING BRAKE ACCUMULATOR IS DESIGNED TO MAINTAIN THE PARKING PRESSURE FOR AT LEAST _____. A - 6 HOURS. B - 12 HOURS. C - 18 HOURS. D - 24 HOURS.

THE PBE PROVIDES A BREATHABLE ATMOSPHERE FOR APPROXIMATELY ____ MINUTES. A - 10. B - 15. C - 16. D - 18.

THERE ARE TWO TRIANGLES FOR EACH GEAR ON THE ECAM WHEEL PAGE. WHAT DO THEY REPRESENT?. A - EACH TRIANGLE REPRESENTS ONE WHEEL ON THE GEAR. B - EACH TRIANGLE REPRESENTS THE POSITION DETECTED BY ONE OF THE TWO COMPUTERS SYSTEMS. C - EACH TRIANGLE REPRESENTS ONE OF THE BRAKING SYSTEMS AVAILABLE FOR THAT GEAR. D - THE FRONT TRIANGLE INDICATES THE POSITION OF THAT GEAR AND THE BACK TRIANGLE INDICATES THE STATUS OF THE BRAKES FOR THAT GEAR.

THERE IS NO OTHER WAY OF DEPLOYING THE OVERWING ESCAPE SLIDE IF IT FAILS TO DEPLOY AUTOMATICALLY ON OPENING THE EMERGENCY EXIT. A - TRUE. B - FALSE.

THE SLIDE ARMED LIGHT ILLUMINATES WHITE ON THE PASSENGER CABIN ENTRY DOORS WHEN: A - THE DOOR IS NOT ARMED. B - THE DOOR IS ARMED. C - THE CONTROL HANDLE IS OPERATED WITH THE SLIDE ARMED.

THE STEERING HANDWHEELS, WHICH ARE INTERCONNECTED, CAN STEER THE NOSE WHEEL UP TO:_____ IN EITHER DIRECTION. A - 55°. B - 65°. C - 75°. D - 90°.

THE STROBE LIGHT SELECTOR IS SET TO AUTO. IN THIS POSITION, WHEN DO THE STROBE LIGHTS STOP FLASHING?. A - WHEN THE AIRCRAFT TOUCHES DOWN. B - WHEN THE FIRST REVERSER IS DEPLOYED. C - WHEN THE LANDING LIGHTS ARE SWITCHED OFF. D - WHEN THE LAST ENGINE HAS BEEN SHUT DOWN.

WHAT ARE THE INDICATIONS THAT THE PBE OXYGEN SUPPLY HAS DEPLETED?. A - THE HOOD COLLAPSES TO THE POINT THAT IT TOUCHES YOUR FACE OR BY A FLASHING RED LIGHT IN ADDITION TO THE FLASHING GREEN LIGHT. B - THE SOUND OF THE OXYEN FLOW STOPS AND FLASHING RED AND GREEN LIGHTS APPEAR. C - NO 02 SUPPLY INDICATIONS & LIGHTS ONLY INDICATE TIME. D - ALL OF THE ABOVE.

WHAT COCKPIT LIGHTING IS AVAILABLE DURING AN EMERGENCY ELECTRICAL CONFIGURATION (EEC)?. A - ALL LIGHTS ARE FULLY FUNCTIONAL. B - DOME LIGHTS, MAIN PANEL FLOOD LIGHTS, AND THE STANDBY COMPASS LIGHT. C - DOME LIGHT (RIGHT SIDE ONLY), MAIN PANEL FLOOD LIGHTS, AND THE STANDBY COMPASS LIGHT. D - DOME LIGHT (RIGHT SIDE ONLY), MAIN PANEL FLOOD LIGHTS (LEFT TWO COLUMNS ONLY), AND THE STANDBY COMPASS LIGHT.

WHAT DOES EACH TURN OF THE GRAVITY GEAR EXTENSION HANDLE DO?. A - OPEN GEAR DOOR, UNLOCK GEAR, DROP GEAR. B - OPEN GEAR DOORS, DROP GEAR, SHUT DOORS. C - SHUTOFF HYDRAULIC PRESSURE, OPEN DOORS, UNLOCKS GEAR. D - OPEN GEAR DOORS, SHUTOFFS HYDRAULICS, UNLOCK GEAR, DROP GEAR.

WHAT DOES HORN SHUTOFF ON THE EVAC PANEL DO?. A - CANCELS THE EVAC ALERT. B - SILENCES EVAC SIGNALS THROUGHOUT THE CABIN AND COCKPIT. C - SILENCES HORN IN COCKPIT. D - NONE OF THE ABOVE.

WHAT DOES ILLUMINATION OF THE RED CABIN PRESSURE LIGHT REPRESENT ON THE MAIN CABIN DOOR?. A - THIS INDICATES THAT THE EVACUATION SLIDE IS ARMED. B - THIS INDICATES THAR THE AIRCRAFT CABIN IS STILL PRESSURIZED AND THE CABIN DOOR SHOULD NOT BE OPENED. C - BOTH ARE CORRECT.

WHAT DOES ILLUMINATION OF THE WHITE SLIDE ARMED LIGHT REPRESENT ON THE MAIN CABIN DOOR?. A - THIS INDICATES THAT THE SLIDE HAS PROPERLY INFLATED AND IS SAFE FOR USE. B - THIS INDICATES THAT THE SLIDE IS ARMED AND THE SLIDE WILL INFLATE IF THE DOOR IS OPENED FROM INSIDE THE AIRCRAFT. C - THIS INDICATES THAT THE MAIN CABIN DOOR HAS NOT BEEN PROPERLY CLOSED. D - THIS INDICATES THAT THE MAIN CABIN DOOR HAS NOT BEEN PROPERLY CLOSED BUT THE SLIDE IS PROPERLY ARMED.

WHAT HAPPENS TO THE COCKPIT DOOR WITH ELECTRICAL POWER FAILURE?. A - IT OPERATES NORMALLY ON HOT BAT BUS. B - IT AUTOMATICALLY UNLOCKS. C - IT AUTOMATICALLY LOCKS FROM OUTSIDE BUT STAYS UNLOCK FROM INSIDE.

WHAT HAPPENS TO THE OTHER BRAKE MODES WHEN PARKING BRAKES ARE APPLIED?. A - THERE IS NO CHANGE. B - ALL OTHER BRAKING MODES AND ANTISKID ARE DEACTIVATED. C - ANTISKID MODE ONLY IS DEACTIVATED.

WHAT IS CREW OXYGEN MINUMUM PRESSURE, WHERE CAN IT BE READ?. A - 850 PSI, ECAM DOOR/OXY PAGE. B - 950 PSI, GAUGE ON THE BOTTLE. C - 1000 PSI, GAUGE ON THE BOTTLE. D - 1500 PSI , ECAM DOOR/OXY PAGE.

WHAT IS INDICATED BY THE AUTOBRAKE DECEL LIGHTS?. A - AIRPLANE DECELERATION IS 25% OF SELECTED RATE. B - AIRPLANE DECELERATON IS 50% OF SELECTED RATE. C - AIRPLANE DECELERATION IS 100% OF SELECTED RATE. D - AIRPLANE DECELERATION IS 80% OF SELECTED RATE.

WHAT IS REQUIRED TO ARM THE AUTO BRAKES?. A - GREEN HYDRAULIC PRESSURE AVAILABLE, ANTI-SKID, NO FAILURES IN THE BRAKING SYSTEM. B - LANDING GEAR LEVER SELECTED DOWN AND SELECTION OF AN AUTOBRAKING RATE. C - BOTH ARE CORRECT.

WHAT SYSTEM PRESSURE DOES THE ACCU PRESS AND BRAKES PRESSURE INDICATOR INDICATE?. A - YELLOW BRAKE ACCUMULATOR AND YELLOW BRAKE SYSTEM PRESSURE TO THE LEFT AND RIGHT BRAKES. B - YELLOW BRAKE ACCUMULATOR AND GREEN BRAKE SYSTEM PRESSURE TO THE LEFT AND RIGHT BRAKES. C - YELLOW BRAKE ACCUMULATOR AND GREEN OR YELLOW BRAKE SYSTEM PRESSURE TO THE LEFT AND RIGHT BRAKES. D - BLUE BRAKE ACCUMULATOR AND GREEN BRAKE SYSTEM PRESSURE TO THE LEFT AND RIGHT BRAKES.

WHEN OPENED IN AN EMERGENCY, THE PASSENGER ENTRY DOORS: A - THEY ARE PNEUMATICALLY ASSISTED INTO THE OPEN POSITION. B - WILL NEED TWO CABIN CREW TO PUSH THEM OPEN. C - ARE ASSISTED TO THE OPEN POSITION BY SLIDE INFLATION. D - ARE ELECTRICALLY ASSISTED INTO THE OPEN POSITION.

WHEN THE CARGO DOOR SWITCH FOR THE YELLOW HYDRAULIC PUMP IS IN USE, THE FLIGHT CONTROLS ARE: A - FULLY OPERATIONAL. B - INHIBITED. C - HYDRAULICALLY LOCKED BY PRESSURE FROM THE ELECTRIC PUMP. D - ONLY OPERATED BY THE GREEN SYSTEM.

WHEN THE DOOR ARMING LEVER IS IN THE ARMED POSITION, OPENING THE DOOR FROM THE OUTSIDE WILL: A - AUTOMATICALLY DEPLOY AND INFLATE THE EVACUATION SLIDE. B - DISARM THE DOOR. C - THE POWER ASSIST WILL RAPIDLY OPEN THE DOOR.

WHEN THE ELECTRIC PUMP IS OPERATING THE FWD OR AFT CARGO DOORS, THE ONLY OTHER YELLOW SYSTEM DEVICES THAT CAN OPERATE ARE BRAKING AND ENGINE 2 REVERSE. A - TRUE. B - FALSE.

WHEN THE LANDING GEAR IS GRAVITY EXTENDED, WILL NOSE WHEEL STEERING BE AVAILABLE?. A - ONLY IF THE A/SKID & N/W STRG SWITCH IS SELECTED ON. B - NO. C - LIMITED NOSE WHEEL STEERING IS AVAILABLE ONLY THROUGH THE CAPTIAN'S RUDDER PEDALS.

WHEN THE SLIDE ARMING LIVER, ON THE EMERGENCY OPENING SYSTEM, IS IN THE ARMED POSITION, WHERE IS THE SLIDE CONNECTED?. A - TO THE BRACKETS ON THE UNDERSIDE OF THE FUSELAGE. B - TO THE BRAKETS ON THE ABOVE THE DOOR. C - TO THE FLOOR BRACKETS ON BOTH SIDES OF THE DOOR. D - ALL OF THE ABOVE.

WHEN USING THE ALTERNATE BRAKE SYSTEM ON ACCUMULATOR PRESSURE ONLY, THE ACCUMULATOR SUPPLIES: A - PARTIAL BRAKES. B - AT LEAST SEVEN FULL BRAKE APPLICATIONS. C - ALTERNATE BRAKES WITH ANTISKID.

WHERE DOES THE DOOR AND SLIDE CONTROL SYSTEM (DSCS) GENERATE WARNINGS?. A - ON ECAM. B - ON THE DOORS. C - BOTH ARE CORRECT.

WHICH HYDRAULIC SYSTEM(S) SUPPLY PRESSURE TO THE LANDING GEAR SYSTEM?. A - GREEN. B - BLUE. C - YELLOW AND BLUE. D - GREEN AND BLUE.

WHICH HYDRAULIC SYSTEM SUPPLIES PRESSURE TO THE NOSE WHEEL STEERING?. A - GREEN. B - BLUE. C - YELLOW AND BLUE. D - GREEN AND BLUE.

WHICH SITUATION WILL AUTOMATICALLY ILLUMINATE THE ESCAPE PATH LIGHTING?. A - THE LOSS OF POWER TO THE DC ESS SHED BUS AND THE LOSS OF POWER TO THE AC BUS #1. B - THE LOSS OF POWER TO THE AC ESS SHED BUS AND THE LOSS OF POWER TO THE AC BUS #1. C - THE LOSS OF POWER TO THE AC ESS SHED AND THE LOSS OF POWER TO THE DC ESS SHED. D - THE LOSS OF POWER TO THE AC ESS SHED.

WITH THE A/SKID & N/W STRG SWITCH IN THE ON POSITION, IF THE BSCU DETECTS A BRAKE SYSTEM MALFUNCTION AND/OR NORMAL BRAKING IS NOT AVAILABLE: A - THE CREW WILL BE NOTIFIED WITH AN ECAM MESSAGE ONLY IF AFTER TOUCHDOWN THE BRAKE SYSTEM DOES ACTUALLY MALFUNCTION. B - TRANSITION TO THE ALTERNATE BRAKE SYSTEM IS AUTOMATIC.

WITH THE EMER EXIT LT SELECTOR IN THE ARM POSITION. IF AC BUS #1 IS UNPOWERED: A - THE ESCAPE PATH MARKINGS WILL AUTOMATICALLY ILLUMINATE. B - THE EMERGENCY LIGHTS AND EXIT SIGNS WILL ILLUMINATE AUTOMATICALLY. C - BOTH ARE CORRECT.

YOU HAVE JUST SET THE PARKING BRAKE HANDLE TO ON. IS IT STILL POSSIBLE TO CHECK THE MAIN BRAKE SYSTEM USING THE TOE BRAKES?. A - YES. AS SOON AS YOU PRESS THE BRAKE PEDALS THE BRAKES INDICATOR WILL READ MAIN SYSTEM PRESSURE. B - NO. IT IS NOT POSSIBLE TO PRESS HARD ENOUGH TO OBTAIN AN ACCURATE READING. C - NO. WHEN THE PARK BRK IS SET, THE OTHER BRAKING MODES ARE DEACTIVATED.

YOU WANT TO OPEN THE CABIN DOOR, WHILE LIFTING THE CONTROL HANDLE THE WHITE LIGHT ILLUMINATES. WHAT DOES IT MEAN?. A - THERE IS RESIDUAL PRESSURE IN THE CABIN. B - THE RAMP IS NOT CORRECTLY POSITIONED. C - THE SLIDE IS STILL ARMED. D - SOMEBODY IS TRYING TO OPEN THE DOOR FROM AOUTSIDE.