A CLASS 3 FAILURE:

AMONG THE FOLLOWING, THE STEP NOT APPLICABLE TO THE STORAGE PROCEDURE FOR LESS THAN 6 MONTHS, IS:

AT THE MAIN LANDING GEAR STATION, THE LOCATION FOR THE RAM AIR TURBINE (RAT) SAFETY DEVICE INSTALLATION IS ON THE:

DMC 1 NORMALLY PROCESSES:

EFIS AND ECAM DISPLAY UNITS (CRT'S) ARE:

ELECTROSTATIC DISCHARGE SENSITIVE EQUIPMENT ARE IDENTIFIED BY:

ELECTROSTATIC ELECTRICITY IS BUILD UP BY:

IF BATTERY VOLTAGE IS BELOW 25 VOLTS, THE NECESSARY CHARGING CYCLE IS:

IF ENGINE REVERSER COWLS HAVE BEEN OPENED FOR MAINTENANCE ACTION THE:

IF THE AIRCRAFT POINTS INTO THE WIND AND WIND SPEED IS BETWEEN 50 AND 70 KTS, MOOR THE AIRCRAFT AT THE:

IN NORMAL OPERATION, IF SOME LIGHTS ARE ILLUMINATED, THESE LIGHTS COULD BE:

IN THE CENTRALIZED FAULT DISPLAY SYSTEM, FAILURE DETECTION IS PERFORMED BY THE:

JACKING OPERATION IS LIMITED IF THE WIND VELOCITY EXCEEDS VALUES DEPENDING ON THE AIRCRAFT:

LEVELING THE AIRCRAFT WITH THE ATTITUDE MONITOR CONSISTS IN:

THE A321 IS THE A320 MODIFIED WITH: