[ { "ch": "The leak measurement solenoid valve is located between the:", "ansGr": [ { "ans": [ "High pressure filter manifold and accumulator.", "false" ] }, { "ans": [ "Engine Driven Pump (EDP) and Fire Shut-Off Valve (FSOV).", "false" ] }, { "ans": [ "Pressure transducer and pressure switches.", "true" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 117" }, { "ch": "A check of the alternate parking brake accumulator nitrogen pressure is done with the:", "ansGr": [ { "ans": [ "Accumulator fluid vented to the reservoir.", "true" ] }, { "ans": [ "Accumulator pressurized with fluid.", "false" ] }, { "ans": [ "Reservoir de-pressurized.", "false" ] } ], "ref": "Ref. AMM Task 12-14-32-614-807" }, { "ch": "The OFF legend of the GREEN/ENG 1 P/BSW goes on when:", "ansGr": [ { "ans": [ "When the green engine 1 pump P/BSW is set to OFF", "true" ] }, { "ans": [ "ENG 1 cranking stops.", "false" ] }, { "ans": [ "Eng 1 N2 is equal to zero.", "false" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 32" }, { "ch": "Extension of the RAT on ground:", "ansGr": [ { "ans": [ "Is always available by manual selection.", "true" ] }, { "ans": [ "Occurs automatically when all Engine Driven Pumps (EDPs) are at LP.", "false" ] }, { "ans": [ "Occurs automatically following a Blue reservoir low level.", "false" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 48" }, { "ch": "The green hydraulic system high pressure filter system includes:", "ansGr": [ { "ans": [ "A single HP filter on the HP manifold for all Engine Driven Pump (EDP) and electric pump supplies.", "false" ] }, { "ans": [ "One filter for both EDP supplies at the HP filter manifold, and one filter at the output of the electric pump supply.", "false" ] }, { "ans": [ "Two filters at the HP manifold.", "true" ] } ], "ref": "Ref. AMM 29-11-00 -00 CONF00" }, { "ch": "Which statement is not correct regarding hydraulic reservoir?", "ansGr": [ { "ans": [ "The reservoir is equipped with a sight glass, a low-level switch, a temperature sensor and a quantity transmitter.", "true" ] }, { "ans": [ "The reservoir is equipped with a sight glass, a low-level switch, a high-level switch, a temperature sensor and a quantity transmitter.", "false" ] }, { "ans": [ "The reservoir is equipped with a sight glass, a high-level switch, a temperature sensor and a quantity transmitter.", "false" ] } ], "ref": "Ref. AMM 29-11-00 -00 CONF00" }, { "ch": "The engine 2 hydraulic fire shut off valve can:", "ansGr": [ { "ans": [ "Shut off automatically following a blue reservoir low level.", "false" ] }, { "ans": [ "Shut off automatically following a RAT extension.", "false" ] }, { "ans": [ "Be closed by the overhead fire pushbutton.", "true" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 63" }, { "ch": "When the A/C is on the ground, a leak measurement solenoid valve can be selected shut to isolate the supply to:", "ansGr": [ { "ans": [ "The flight controls.", "false" ] }, { "ans": [ "The flaps or the slats.", "false" ] }, { "ans": [ "The primary flight controls only.", "true" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 116" }, { "ch": "The G HP filter and sampling valve are located on the:", "ansGr": [ { "ans": [ "LP manifold on the rear wall of the main landing gear bay", "false" ] }, { "ans": [ "HP manifold on the rear wall of the main landing gear bay", "true" ] }, { "ans": [ "HP manifold on the front wall of the main landing gear bay.", "false" ] } ], "ref": "Ref. AMM 29-11-00-00 CONF00" }, { "ch": "When only external power A connected, the yellow electric pump will run during cargo door opening:", "ansGr": [ { "ans": [ "If external power is AVAIL and MAINT BUS is ON.", "true" ] }, { "ans": [ "Only if external power is energized.", "false" ] }, { "ans": [ "If external power is AVAIL.", "false" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 104" }, { "ch": "On the ground during cargo door control:", "ansGr": [ { "ans": [ "Yellow leak measurement valve automatic closed.", "true" ] }, { "ans": [ "Yellow leak measurement valve automatic opened.", "false" ] }, { "ans": [ "Yellow leak measurement valve is not following cargo door control.", "false" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 104" }, { "ch": "Fluid drains into the recovery tanks by:", "ansGr": [ { "ans": [ "An electric pump.", "false" ] }, { "ans": [ "Aircraft speed", "false" ] }, { "ans": [ "Gravity", "true" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 112" }, { "ch": "Which statement is NOT correct regarding reservoir pressurizing system?", "ansGr": [ { "ans": [ "The reservoir pressurizing system is supplied in normal operation by high pressure air, bleed from engine 1 LP compressor.", "true" ] }, { "ans": [ "The system can also be pressurized through the air-pressurization unit manifold by air a LP source from the air conditioning system.", "false" ] }, { "ans": [ "The reservoir pressurizing system is supplied in normal operation by HP air bleed from engine 1 HP compressor.", "false" ] } ], "ref": "Ref. AMM 29-14-00 -00 CONF00" }, { "ch": "The constant speed motor/generator drains into a tank located in the:", "ansGr": [ { "ans": [ "Yellow hydraulic compartment.", "false" ] }, { "ans": [ "Green hydraulic compartment.", "true" ] }, { "ans": [ "Blue hydraulic compartment.", "false" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 112" }, { "ch": "What happens if the hydraulic pressure drops?", "ansGr": [ { "ans": [ "The priority valves give priority to the heavy load users.", "false" ] }, { "ans": [ "The priority valves give priority to the essential systems.", "true" ] }, { "ans": [ "The priority valves modulate the pressure to the users.", "false" ] } ], "ref": "Ref: AMM 29-11-00-00 CONF 00" }, { "ch": "The priority valve:", "ansGr": [ { "ans": [ "Isolates the heavy load users (Constant Speed Motor/Generator, Nose Wheel Steering, Landing Gear, Slat/Flap) in the event of low hydraulic pressure.", "false" ] }, { "ans": [ "The valve is pilot-operated, and spring biased in the open position.", "false" ] }, { "ans": [ "The valve is pilot-operated, and spring biased in the closed position.", "true" ] } ], "ref": "Ref: AMM 29-11-00-00 CONF 00" }, { "ch": "Which statement is true regarding hydraulic reservoir?", "ansGr": [ { "ans": [ "They compensate for variations in fluid volume due to the operation of the user services and to the fluid temperature.", "true" ] }, { "ans": [ "They are designed to remain pressurized for at least 24 hours, at ISO temperature.", "false" ] }, { "ans": [ "Reservoirs of Green, Blue and Yellow are different types.", "false" ] } ], "ref": "Ref: AMM 29-11-00-00 CONF 00" }, { "ch": "Case drain filter of engine driven pump:", "ansGr": [ { "ans": [ "Is installed on each engine fan case. It is of the bypass type with a clogging indicator", "false" ] }, { "ans": [ "Is of the cleanable type.", "false" ] }, { "ans": [ "Is installed on each engine fan case. It is of the non-bypass type with a clogging indicator", "true" ] } ], "ref": "Ref: AMM 29-11-00-00 CONF 00" }, { "ch": "Which statement is correct regarding reservoir filling filter:", "ansGr": [ { "ans": [ "The clogging indicator is electrical, a red button comes out to show when the filter element is too dirty.", "false" ] }, { "ans": [ "The clogging indicator is mechanical, a red button comes out to show when the filter element is too dirty.", "true" ] }, { "ans": [ "There is by-pass device.", "false" ] } ], "ref": "Ref: AMM 29-16-00-00 CONF 00" }, { "ch": "The reservoir pressurizing system:", "ansGr": [ { "ans": [ "The pressurizing system ensures in each hydraulic reservoir an air pressure of 4.5 bars absolute in flight and on ground so as to avoid cavitations of the pumps on the ground and throughout the whole flight envelope.", "true" ] }, { "ans": [ "It cannot keep the reservoir sufficiently air-tight if failure of the pressurization system or after an engine shutdown.", "false" ] }, { "ans": [ "The reservoir is a non-pressurized system .", "false" ] } ], "ref": "Ref: AMM 29-10-00-00 CONF 00" }, { "ch": "What hydraulic pump can only be controlled manually?", "ansGr": [ { "ans": [ "Green electrical pump.", "false" ] }, { "ans": [ "Blue electrical pump.", "true" ] }, { "ans": [ "Yellow electrical pump.", "false" ] } ], "ref": "Ref: AMM 29-22-00-00 CONF 00" }, { "ch": "Which of the following components operates only on GND?", "ansGr": [ { "ans": [ "Blue electrical pump.", "false" ] }, { "ans": [ "Yellow electrical pump.", "false" ] }, { "ans": [ "Leak measurement valve.", "true" ] } ], "ref": "Ref: AMM 29-19-00-00 CONF 00" }, { "ch": "RAT can be extended on ground from?", "ansGr": [ { "ans": [ "OVHD HYD panel.", "true" ] }, { "ans": [ "OVHD ELEC panel.", "false" ] }, { "ans": [ "OVHD EMER ELEC panel.", "false" ] } ], "ref": "Ref: AMM 29-24-00-00 CONF 00" }, { "ch": "Each wiper is controlled:", "ansGr": [ { "ans": [ "by WHC computer.", "false" ] }, { "ans": [ "By a P/B.", "false" ] }, { "ans": [ "By a two-position rotary selector.", "true" ] } ], "ref": "Ref: Airbus TTM ATA 30 Page 40" }, { "ch": "The rain repellent system is inhibited:", "ansGr": [ { "ans": [ "On ground when the engines are running.", "false" ] }, { "ans": [ "During take-off and landing.", "false" ] }, { "ans": [ "On ground when engines are shut down", "true" ] } ], "ref": "Ref: Airbus TTM ATA 30 Page 42" }, { "ch": "The water ice protection system is controlled:", "ansGr": [ { "ans": [ "Automatically.", "true" ] }, { "ans": [ "By a P/B in the cockpit.", "false" ] }, { "ans": [ "By a P/B on the Flight Attendant Panel (FAP).", "false" ] } ], "ref": "Ref. AMM 30-73-00-00 CONF 00" }, { "ch": "Escape slide locking mechanism are electrically heated:", "ansGr": [ { "ans": [ "At first engine start-up.", "false" ] }, { "ans": [ "At door closed and armed.", "false" ] }, { "ans": [ "When door is closed, armed and the temperature sensor reads less than 12°C", "true" ] } ], "ref": "Ref: Airbus TTM ATA 30 Page 54" }, { "ch": "Escape slide locking mechanisms are electrically heated are controlled:", "ansGr": [ { "ans": [ "By a P/B in the cockpit.", "false" ] }, { "ans": [ "By a P/B on the Flight Attendant Panel (FAP).", "false" ] }, { "ans": [ "Automatically by IPCUs in case of icing conditions.", "true" ] } ], "ref": "Ref. AMM 30-46-00-00 CONF 00" }, { "ch": "The two-water ice protection control units (IPCUs) are located:", "ansGr": [ { "ans": [ "In the avionics bay.", "false" ] }, { "ans": [ "One in the Fwd and the other in the aft cargo compartment.", "false" ] }, { "ans": [ "One in the avionics bay and the other in the aft cargo compartment.", "true" ] } ], "ref": "Ref. AMM 30-73-00-00 CONF 00" }, { "ch": "The ice protection control unit status can be check on the:", "ansGr": [ { "ans": [ "EWD of the ECAM.", "false" ] }, { "ans": [ "Cabin Intercommunication Data System (CIDS) or FAP", "true" ] }, { "ans": [ "Primary Flight Display (PFD).", "false" ] } ], "ref": "Ref. AMM 30-73-00-00 CONF 00" }, { "ch": "How many wing anti-ice valves are on each wing.", "ansGr": [ { "ans": [ "Two, one for slat 4 and one for slat 5,6 and 7.", "true" ] }, { "ans": [ "Two, one for slat 4, 5 and one for slat 6 and 7.", "false" ] }, { "ans": [ "Three, one for slat 4, one for slat 5 and one for slat 6 , 7.", "false" ] } ], "ref": "Ref. AMM 30-11-00-00 CONF 00" }, { "ch": "How can you display SD (System Display) image in case of the SD unit fault or set to off?", "ansGr": [ { "ans": [ "The SD image is automatically displayed on upper ECAM.", "false" ] }, { "ans": [ "The SD image is automatically displayed on F/O ND.", "false" ] }, { "ans": [ "You can display SD image on upper ECAM by manual using ECAM control panel or use ECAM/ND Transfer switch to display SD image on Capt ND or F/O ND.", "true" ] } ], "ref": "Ref AMM 31-68-00-00 CONF 00" }, { "ch": "The ECAM MAINTENANCE STATUS message", "ansGr": [ { "ans": [ "Can be left unrectified until the next C check.", "false" ] }, { "ans": [ "Has to be rectified before dispatched.", "false" ] }, { "ans": [ "Is always “GO” item without any restriction.", "true" ] } ], "ref": "Ref: TSM Introduction" }, { "ch": "Class 1 faults displayed on the PFR are:", "ansGr": [ { "ans": [ "NO GO items.", "false" ] }, { "ans": [ "Is always “GO” item without any restriction.", "false" ] }, { "ans": [ "The maintenance class indication enables the maintenance teams to establish a priority in trouble shooting actions .", "true" ] } ], "ref": "Ref: TSM Introduction" }, { "ch": "Class 1 and 2 faults be found?", "ansGr": [ { "ans": [ "On ECAM upper page.", "false" ] }, { "ans": [ "On the STS page.", "false" ] }, { "ans": [ "In the PFR.", "true" ] } ], "ref": "Ref: TSM Introduction" }, { "ch": "Changeover valve is used to isolate leak on?", "ansGr": [ { "ans": [ "NLG shock absorber", "false" ] }, { "ans": [ "MLG shock absorber", "false" ] }, { "ans": [ "Both NLG & MLG shock absorbers", "true" ] } ], "ref": "Ref. AMM 32-11-13-860-801/ 32-21-13 860-801" }, { "ch": "To have a brake INOP, MEL requires the Green and Blue brake systems associated with operative brakes are operative, it means?", "ansGr": [ { "ans": [ "All the Green hydraulic pumps are operative.", "false" ] }, { "ans": [ "All the Blue hydraulic pumps are operative.", "false" ] }, { "ans": [ "Make sure that the Normal and the Alternate brakes for the other wheels are serviceable.", "true" ] } ], "ref": "Ref. AMM 32-42-00-040-801" }, { "ch": "How is the brake unit attached to the MLG axle?", "ansGr": [ { "ans": [ "By the brake rod and torque pin", "true" ] }, { "ans": [ "By 2 bolts located around the brake unit", "false" ] }, { "ans": [ "By 3 bolts located around the brake unit.", "false" ] } ], "ref": "Ref. AMM 32-42-27-400-801" }, { "ch": "How do you set the parking brake during main wheel replacement?", "ansGr": [ { "ans": [ "Brake ON; jack axle; brake OFF; remove/install wheel; torque axle nut; brake OFF; lower jack.", "false" ] }, { "ans": [ "Brake ON; jack the axle; remove/install wheel; brake OFF; torque axle nut; lower the jack.", "false" ] }, { "ans": [ "Brake OFF; jack axle; brake ON; remove/install wheel; brake OFF; torque axle nut; lower jack.", "true" ] } ], "ref": "Ref. AMM 32-41-11-04 CONF 00" }, { "ch": "For wheel replacement, can you lift the two axles of the bogie beam of the same MLG at the same time?", "ansGr": [ { "ans": [ "Yes, keep the bogie beam level position to prevent extension of the pitch trimmer.", "true" ] }, { "ans": [ "Yes, the AFT jack must always be higher than the FWD to prevent too much load on the aft axle.", "false" ] }, { "ans": [ "No, you are not allowed.", "false" ] } ], "ref": "Ref. AMM 07-12-00-582-802" }, { "ch": "What is permissible during jacking for main LDG wheel change?", "ansGr": [ { "ans": [ "Cargo, PAX loading.", "false" ] }, { "ans": [ "Gate docking.", "false" ] }, { "ans": [ "Put CHOCK - WHEELs are in position at the LDG wheels on the side where you do not remove the wheels.", "true" ] } ], "ref": "Ref. AMM 07-12-00-582-802" }, { "ch": "The Parking brake is effective?", "ansGr": [ { "ans": [ "When selected ON; at least one BATT at AUTO; BRK ACC has pressure.", "false" ] }, { "ans": [ "When selected ON; Both BATT at AUTO; BRK ACC has pressure.", "false" ] }, { "ans": [ "When selected ON; BRK ACC has pressure.", "true" ] } ], "ref": "Ref. AMM 32-45-00-00 CONF 00 ``" }, { "ch": "What do you do if you see the Red Light on the Electric Box at NLG comes on during towing?", "ansGr": [ { "ans": [ "Parking brake is ON, you cannot tow the aircraft.", "false" ] }, { "ans": [ "No further towing allowed due to excess angular travel on the NLG steering .", "true" ] }, { "ans": [ "Parking brake pressure is low, you are not allowed to tow aircraft.", "false" ] } ], "ref": "Ref. AMM 32-53-00-00 CONF 00" }, { "ch": "What you do if you found the aircraft had rolled out with main wheel # 3 deflated?", "ansGr": [ { "ans": [ "Re-inflate wheel #3 to normal pressure range and monitor for 24 hours.", "false" ] }, { "ans": [ "Replace wheel #3 before A/C departure.", "false" ] }, { "ans": [ "Replace wheel #3 and the adjacent wheel.", "true" ] } ], "ref": "Ref. AMM 32-41-00-220-802" }, { "ch": "Wheels mixability precaution is applied for ?", "ansGr": [ { "ans": [ "Only radial tires can be installed on the NLG wheels.", "true" ] }, { "ans": [ "Radial and bias tires can be installed on the NLG wheels.", "false" ] }, { "ans": [ "Mixability allowed only for new tires.", "false" ] } ], "ref": "Ref. AMM 32-41-00-200-802" }, { "ch": "Excessive shoulders wear of the tire is the indication of:", "ansGr": [ { "ans": [ "Too much operation on wet runway.", "false" ] }, { "ans": [ "Underinflated.", "true" ] }, { "ans": [ "Overinflated.", "false" ] } ], "ref": "Ref. AMM 32-41-00-210-803" }, { "ch": "When shall you remove the wheel?", "ansGr": [ { "ans": [ "Only if the tire is worn to the base of all grooves all around its circumference.", "false" ] }, { "ans": [ "You can see any reinforcing material.", "true" ] }, { "ans": [ "Its adjacent wheel pressure is 15% underinflated.", "false" ] } ], "ref": "Ref. AMM 32-41-00-210-803, AMM 32-41-00-220-802" }, { "ch": "When installing the main wheel, you torque:", "ansGr": [ { "ans": [ "Twice with the same torque value.", "false" ] }, { "ans": [ "Twice, the first one with lower value than the second.", "false" ] }, { "ans": [ "Twice, the first one with higher value than the second.", "true" ] } ], "ref": "Ref. AMM 32-41-11-400-801" }, { "ch": "What statement is NOT true: Brake unit is considered defective when?", "ansGr": [ { "ans": [ "Leakage found on any piston.", "false" ] }, { "ans": [ "There is no brake-wear indicator pin installed.", "false" ] }, { "ans": [ "A wear pin is missing.", "true" ] } ], "ref": "Ref. AMM 32-40-00-200-801" }, { "ch": "What you do if you found one wear indicator pin on a brake unit is missing?", "ansGr": [ { "ans": [ "This brake is serviceable if other indicator is still in limit.", "true" ] }, { "ans": [ "Aircraft can be dispatched like it is. Not any action required.", "false" ] }, { "ans": [ "The brake is no longer serviceable. It needs to be deactivated.", "false" ] } ], "ref": "Ref. AMM 32-40-00-200-801" }, { "ch": "When TORQUE the axle nut during installation of the main wheel?", "ansGr": [ { "ans": [ "You turn the wheel in the direction of the axle nut rotation.", "true" ] }, { "ans": [ "You turn the wheel counterclockwise.", "false" ] }, { "ans": [ "You turn the wheel clockwise.", "false" ] } ], "ref": "Ref. AMM 32-41-11-400-801" }, { "ch": "During wheel installation, after applying the required final torque value, if the axle nut slots still do not align with the bolt holes in the axle, what do you do?", "ansGr": [ { "ans": [ "Remove this wheel and install another wheel.", "false" ] }, { "ans": [ "Remove and reinstall the wheel until you get them aligned.", "false" ] }, { "ans": [ "Slightly tighten axle nut until you get them aligned.", "true" ] } ], "ref": "Ref. AMM 32-41-11-400-801" }, { "ch": "Landing gear safety pins shall be installed on landing gears:", "ansGr": [ { "ans": [ "During landing gears Retraction/ Extension test on ground.", "false" ] }, { "ans": [ "During A/C maintenance operation or parking on ground .", "true" ] }, { "ans": [ "Only during A/C towing.", "false" ] } ], "ref": "Ref. AMM 10-11/12/20" }, { "ch": "You open the LDG doors on GND with:", "ansGr": [ { "ans": [ "Green reservoir and the Green hydraulic system depressurized.", "false" ] }, { "ans": [ "Green reservoir and the Green hydraulic system pressurized.", "false" ] }, { "ans": [ "Door’s opening do not depend on pressurization of Green system and RSVR.", "true" ] } ], "ref": "Ref. AMM 32-12-00, AMM 32-22-00" }, { "ch": "The brake triple indicator needles are not moving during?", "ansGr": [ { "ans": [ "Normal brake.", "true" ] }, { "ans": [ "Alternate brake.", "false" ] }, { "ans": [ "Parking brake", "false" ] } ], "ref": "Ref. AMM 32-43-00-00 CONF 00, AMM 32-44-00-00 CONF 00" }, { "ch": "When you bleed the brake system at the brake unit", "ansGr": [ { "ans": [ "Push the pedals as moderately as possible.", "true" ] }, { "ans": [ "Push the pedals as quickly as possible.", "false" ] }, { "ans": [ "Do not use the pedals brake. Use the parking brake only.", "false" ] } ], "ref": "Ref. AMM 32-42-00-870-801" }, { "ch": "What do you NOT have to do before installing the main wheel brake?", "ansGr": [ { "ans": [ "Remove the axle sleeves.", "true" ] }, { "ans": [ "Grease the axle sleeves.", "false" ] }, { "ans": [ "Make sure that the Guide Cone – Brake is removed.", "false" ] } ], "ref": "Ref AMM TASK 32-42-27-400-801-A" }, { "ch": "During the main wheel brake replacement, the brake torque pin?", "ansGr": [ { "ans": [ "Can be NDT checked before re-use if new part is not available.", "false" ] }, { "ans": [ "Can be re-installed with a new brake.", "false" ] }, { "ans": [ "Need to be attached with the removed brake unit and sent back to the store.", "true" ] } ], "ref": "Ref. AMM 32-42-27-400-801" }, { "ch": "What is correct regarding greasing during replacement of brake unit?", "ansGr": [ { "ans": [ "Apply as much as possible the high temperature type of grease to all surface’s contacts.", "false" ] }, { "ans": [ "Axle sleeves need to be removed for greasing.", "true" ] }, { "ans": [ "No need to apply the high temperature type of grease to all surface’s contacts.", "false" ] } ], "ref": "Ref. AMM 32-42-27-400-801" }, { "ch": "When cockpit door is opened and the engine is running, the forward LH entrance light intensity is:", "ansGr": [ { "ans": [ "Dimmed to 50%", "false" ] }, { "ans": [ "Dimmed to 10%", "true" ] }, { "ans": [ "Normal", "false" ] } ], "ref": "Ref. AMM 33-21-00-00 CONF 00" }, { "ch": "In abnormal configuration such as either rapid cabin decompression or a total CIDS failure, the cabin lights:", "ansGr": [ { "ans": [ "Up to 100%", "true" ] }, { "ans": [ "Up to 50%", "false" ] }, { "ans": [ "Up to 10%", "false" ] } ], "ref": "Ref. AMM 33-21-00-00 CONF 00" }, { "ch": "You turn ON the engine scan lights when the MID PAX L/H or R/H DOOR opens, the corresponding engine scan light is still ON.", "ansGr": [ { "ans": [ "It is abnormal, you must do the trouble shooting.", "true" ] }, { "ans": [ "L/H Engine scan light always ON", "false" ] }, { "ans": [ "R/H Engine scan light always ON.", "false" ] } ], "ref": "Ref. AMM 33-49-00-00 CONF 00" }, { "ch": "What is the difference between the STORM and BRT position of dome light switch 5LE?", "ansGr": [ { "ans": [ "When the switch in the BRT positions the doom light has 90% brightness.", "false" ] }, { "ans": [ "When the switch in the STORM positions the doom light has 90% brightness.", "false" ] }, { "ans": [ "The brightness of the dome lights are the same when the switch is in the STORM position or in the BRT position.", "true" ] } ], "ref": "Ref. AMM 33-12-00-00-CONF 00 Figure 33-12-00-15000" }, { "ch": "In STORM condition, with interior dome light switch in STORM position, what is the brightness of Storm lighting?", "ansGr": [ { "ans": [ "Full brightness and not depend on the position of rheostat", "true" ] }, { "ans": [ "80% brightness", "false" ] }, { "ans": [ "10% brightness", "false" ] } ], "ref": "Ref. AMM 33-12-00-00-CONF 00" }, { "ch": "When lavatory doors are closed and locked:", "ansGr": [ { "ans": [ "The fluorescent lights come on 50% light intensity and the mirror lights are OFF.", "false" ] }, { "ans": [ "The fluorescent lights come on 50% light intensity and the mirror lights are ON.", "false" ] }, { "ans": [ "The fluorescent lights come on 100% light intensity and the mirror lights are ON.", "true" ] } ], "ref": "Ref. AMM 33-24-00-00-CONF 00" }, { "ch": "When do the landing lights come on?", "ansGr": [ { "ans": [ "The landing lights switch is in ON position .", "true" ] }, { "ans": [ "The nose landing gear down lock and landing light switch is in ON position.", "false" ] }, { "ans": [ "The flaps are extended, and the landing light switch is in ON position.", "false" ] } ], "ref": "Ref. AMM 33-42-00-00-CONF 00" }, { "ch": "The condition for the runway turn off lights come ON is :", "ansGr": [ { "ans": [ "The runway turn off switch is set to ON position and MLG down locked.", "false" ] }, { "ans": [ "The runway turn off switch is set to ON position and NLG down locked", "true" ] }, { "ans": [ "The runway turn off switch is set to ON position and NLG retracted.", "false" ] } ], "ref": "Ref. AMM 33-43-00-00-CONF 00" }, { "ch": "If the power from the DC essential bus bar is not available, how long can EPSU supply the power to emergency lights:", "ansGr": [ { "ans": [ "Maximum 15 minutes", "false" ] }, { "ans": [ "Maximum 30 minutes", "false" ] }, { "ans": [ "Minimum 10 minutes", "true" ] } ], "ref": "Ref. AMM 33-51-00-00 CONF 00" }, { "ch": "When strobe lights selector is set to ON position, strobe lights will flash:", "ansGr": [ { "ans": [ "If shock absorber is not compressed", "false" ] }, { "ans": [ "Always", "true" ] }, { "ans": [ "If shock absorber is extended", "false" ] } ], "ref": "Ref: Airbus TTM ATA 33 Page 56" }, { "ch": "The cabin lighting is controlled from:", "ansGr": [ { "ans": [ "From P/B in cockpit.", "false" ] }, { "ans": [ "The CIDS FAP and several AAPs", "true" ] }, { "ans": [ "Any attendant station.", "false" ] } ], "ref": "Ref. AMM 33-21-00-00 CONF 00" }, { "ch": "Emergency lights are supplied from the EPSU batteries when:", "ansGr": [ { "ans": [ "The EMER light switch is in the ON position and the DC Essential Bus is supplied.", "false" ] }, { "ans": [ "The EMER light switch is in the ARM or ON position and the DC Essential Bus fails.", "true" ] }, { "ans": [ "The EMER P/B on the Forward Attendant Panel is pressed.", "false" ] } ], "ref": "Ref. AMM 33-51-00-00 CONF 00" }, { "ch": "If both FMGECs have failed, the third RMP:", "ansGr": [ { "ans": [ "Automatically operate in RADIO NAV backup tuning mode.", "false" ] }, { "ans": [ "Operates only in RADIO NAV backup mode.", "false" ] }, { "ans": [ "Does not operate in RADIO NAV backup mode.", "true" ] } ], "ref": "Ref. Airbus TTM ATA 34 Page 10" }, { "ch": "ILS 1 DATA is displayed on the:", "ansGr": [ { "ans": [ "CAPT ND and F/O PFD.", "false" ] }, { "ans": [ "CAPT PFD and F/O ND.", "true" ] }, { "ans": [ "CAPT and F/O ND", "false" ] } ], "ref": "Ref. AMM 34-36-00-00 CONF 00" }, { "ch": "The function of 2 GPS antennas is:", "ansGr": [ { "ans": [ "One for transmitting, the other for receiving.", "false" ] }, { "ans": [ "Receiving only.", "true" ] }, { "ans": [ "Each antenna can be used to transmit or receive.", "false" ] } ], "ref": "Ref. AMM 34-36-00-00 CONF 00" }, { "ch": "Standby Pitot and Standby Static Probe supply total and static pressure:", "ansGr": [ { "ans": [ "Directly to ADR3", "false" ] }, { "ans": [ "To IR3 via ADM", "false" ] }, { "ans": [ "Directly to ISIS and to ADR3 via ADM", "true" ] } ], "ref": "Ref. AMM figure 34-10-00-11100" }, { "ch": "The Multi-Mode Receiver (MMR) system is composed of an Instrument Landing System (ILS) and:", "ansGr": [ { "ans": [ "A Global Positioning System (GPS).", "true" ] }, { "ans": [ "A Radio Altimeter (RA).", "false" ] }, { "ans": [ "A GPS and RA", "false" ] } ], "ref": "Ref. to AMM 34-36-00-00 CONF 01" }, { "ch": "If RA1 fails:", "ansGr": [ { "ans": [ "RA 2 provides data to the EGPWC.", "false" ] }, { "ans": [ "FMGEC1 provides data to the EGPWC.", "false" ] }, { "ans": [ "The EGPWC no longer receives radio altitude data.", "true" ] } ], "ref": "Ref MEL 34-40-04A Operational Procedures" }, { "ch": "During maintenance operations, in order to prevent automatic activation of the Predictive Windshear System (PWS):", "ansGr": [ { "ans": [ "The Weather Radar SYS switch must be set to OFF and the PWS switch set to OFF", "true" ] }, { "ans": [ "The Weather Radar SYS switch must be set to OFF and the PWS switch set to AUTO.", "false" ] }, { "ans": [ "The WX/TURB selector must be set to WX, and the PWS switch must be set to STANDBY.", "false" ] } ], "ref": "Ref. AMM 34-41-00-00 CONF 01" }, { "ch": "Radio Height is displayed on the PFD:", "ansGr": [ { "ans": [ "Less than or equal to 2500 ft", "true" ] }, { "ans": [ "When the LOC or APPR p/b is pressed", "false" ] }, { "ans": [ "When a Decision Height is selected", "false" ] } ], "ref": "Ref. AMM 34-42-00-00 CONF 00" }, { "ch": "Alignment of the IRS system is done:", "ansGr": [ { "ans": [ "With IR rotary selectors set at ATT.", "false" ] }, { "ans": [ "With ADIRS pushbutton switches at ON position.", "false" ] }, { "ans": [ "With ADIRS rotary selectors set at NAV and the A/C in static condition.", "true" ] } ], "ref": "Ref. AMM 34-10-00-860-802" }, { "ch": "When working on gaseous oxygen system, you must:", "ansGr": [ { "ans": [ "Stop all refueling, all repairs on fuel and hydraulic systems, all procedures that use flammable material such as cleaning and de-icing materials.", "true" ] }, { "ans": [ "Do not operate VHF system and carry out maintenance on VHF system,", "false" ] }, { "ans": [ "Do not operate RAs system and carry out maintenance on RAs system,", "false" ] } ], "ref": "Ref. AMM 35-00-00-860-801" }, { "ch": "The CKPT OXY indication in amber on ECAM DOOR/OXY page when:", "ansGr": [ { "ans": [ "The CREW SUPPLY P/BSW is ON, and oxygen high pressure is more than 400 PSI,", "false" ] }, { "ans": [ "There is detection high pressure in high pressure system or regulated low pressure,", "false" ] }, { "ans": [ "The CREW SUPPLY P/BSW is OFF, or oxygen high pressure is less than 300 PSI or regulated low pressure.", "true" ] } ], "ref": "Ref. AMM 35-13-00-00 CONF 00" }, { "ch": "Numerical value (in PSI) for oxygen high pressure indicates in cross amber when:", "ansGr": [ { "ans": [ "Pressure is less than 400 PSI,", "false" ] }, { "ans": [ "Pressure is less than 1500 PSI,", "false" ] }, { "ans": [ "Oxygen high pressure information is not available.", "true" ] } ], "ref": "Ref. AMM 35-13-00-00 CONF 00" }, { "ch": "When visual inspection PBE in cockpit you found 01 PBE vacuum sealed bag is inflated:", "ansGr": [ { "ans": [ "This is serviceable one, if date of overhaul is not due,", "false" ] }, { "ans": [ "You must replace it with a new one.", "false" ] }, { "ans": [ "You can defer defect refer MEL if spare not available.", "true" ] } ], "ref": "Ref. AMM 35-31-00-00 CONF 00 and MEL 35-30-02A" }, { "ch": "Before remove the crew oxygen cylinder, you must do:", "ansGr": [ { "ans": [ "Close the ON/OFF valve and bleed the oxygen system.", "true" ] }, { "ans": [ "Open the ON/OFF valve and bleed the oxygen system,", "false" ] }, { "ans": [ "Make sure indication of crew oxygen system are available on ECAM DOOR/OXY page.", "false" ] } ], "ref": "Ref. AMM 35-11-41-000-801-A" }, { "ch": "When the CREW SUPPLY push button is pushed in and oxygen high pressure equal or more than 600psi. Indication of oxy high pressure on ECAM DOOR/OXY page is:", "ansGr": [ { "ans": [ "CKPT OXY label in white, oxy high-pressure value in green, unit of pressure in blue.", "true" ] }, { "ans": [ "OXY label and oxy high pressure in green, unit of oxy high pressure in blue,", "false" ] }, { "ans": [ "CKPT OXY label in green, oxy high pressure in blue and unit of oxy high pressure in white.", "false" ] } ], "ref": "Ref. AMM 35-13-00-00 CONF 00: Control and Indicating" }, { "ch": "The passenger emergency-oxygen is stored in oxygen containers, and which have:", "ansGr": [ { "ans": [ "The high-pressure oxygen cylinder and continuous-flow oxygen masks with the flexible supply hoses,", "false" ] }, { "ans": [ "One supply valve to supply oxygen to passengers,", "false" ] }, { "ans": [ "The chemical emergency oxygen-generators and the continuous-flow oxygen masks with the flexible supply hoses.", "true" ] } ], "ref": "Ref. AMM 35-20-00 PB001: Passenger oxygen storage" }, { "ch": "In automatic mode, the cross-bleed valve:", "ansGr": [ { "ans": [ "Opens when the system is using APU Bleed air and closes if the system detects an air leak of APU duct (except during engine start).", "true" ] }, { "ans": [ "Closes when the system is using APU Bleed air and if the system detects an air leak (except in flight).", "false" ] }, { "ans": [ "Opens when the system is using APU Bleed air and closes if the system detects an air leak (except on ground).", "false" ] } ], "ref": "Ref. AMM 36-12-00-00 CONF 00" }, { "ch": "When selected, APU bleed air:", "ansGr": [ { "ans": [ "  Supply bleed air only if the ENG BLEED pb's are selected OFF.", "false" ] }, { "ans": [ "  Has priority over engine bleed air.", "true" ] }, { "ans": [ "  Does not have priority over engine bleed air.", "false" ] } ], "ref": "Ref. Airbus TTM ATA 36 page 6" }, { "ch": "Each engine bleed system is designed to:", "ansGr": [ { "ans": [ "Regulate bleed air pressure only.", "false" ] }, { "ans": [ "Regulate bleed air temperature only.", "false" ] }, { "ans": [ "Regulate bleed air pressure and bleed air temperature.", "true" ] } ], "ref": "Ref. AMM 36-11-00-00 CONF 00" }, { "ch": "When engine anti-ice and wing anti-ice are in use, and a BMC detects a bleed leak:", "ansGr": [ { "ans": [ "Only the engine anti-ice on the associated side will be lost.", "false" ] }, { "ans": [ " The wing and engine anti-ice on the associated side will be lost.", "false" ] }, { "ans": [ " The wing anti-ice on the associated side will be lost, and the engine anti-ice on the associated side will continue to function.", "true" ] } ], "ref": "Ref. AMM 30-11-00-00 CONF 00, AMM 30-21-00-00 CONF 22" }, { "ch": "Air leakage detection is based on:", "ansGr": [ { "ans": [ "Double looped sensing units in Pylon, Wings, mid Fuselage and APU ducts.", "false" ] }, { "ans": [ "Single loop for Pylon and double loops for Wings, mid Fuselage and APU ducts.", "true" ] }, { "ans": [ "Single loop for Pylon, APU and double loops for Wings and mid Fuselage ducts.", "false" ] } ], "ref": "Ref. AMM 36-22-00-00 CONF 00 System Description" }, { "ch": "If one BMC fails, the remaining BMC takes over the monitoring of the Bleed system:", "ansGr": [ { "ans": [ "Wing/pack, APU and Pylon leak detection monitoring.", "false" ] }, { "ans": [ "Wing/pack and Pylon leak detection monitoring.", "false" ] }, { "ans": [ "Wing/pack and APU leak detection monitoring", "true" ] } ], "ref": "Ref. Airbus TTM ATA 36 page 42" }, { "ch": "On ECAM bleed page: when is the GND symbol displayed?", "ansGr": [ { "ans": [ "  Whenever the aircraft is on the ground.", "true" ] }, { "ans": [ "  All the time.", "false" ] }, { "ans": [ "  Only when a ground air supply is connected.", "false" ] } ], "ref": "Ref. Airbus TTM ATA 36 page 60" }, { "ch": "In case of PRV (Pressure Regulating Valve) is controlled to close:", "ansGr": [ { "ans": [ "The HPV (High Pressure Valve) is also controlled to close pneumatically.", "false" ] }, { "ans": [ "The HPV (High Pressure Valve) is also controlled to close electrically.", "true" ] }, { "ans": [ "The HPV (High Pressure Valve) close/open state is independent from PRV position.", "false" ] } ], "ref": "Ref. AMM 36-11-00-00 CONF 22 Control and Indicating" }, { "ch": "The pressure regulation of the engine bleed air is performed by:", "ansGr": [ { "ans": [ "The Pressure Regulating Valve (PRV), which is controlled by the Thermostat Solenoid (ThS).", "true" ] }, { "ans": [ "The Fan Air Valve (FAV), which is controlled by the Control Thermostat (ThC).", "false" ] }, { "ans": [ "The Overpressure valve, which is controlled by the Control Thermostat (ThC).", "false" ] } ], "ref": "Ref. Airbus TTM ATA 36 page 22" }, { "ch": "If one BMC fails:", "ansGr": [ { "ans": [ "The dedicated wing and pylon leak detection is lost.", "false" ] }, { "ans": [ "The corresponding pylon leak detection is lost only.", "true" ] }, { "ans": [ "The dedicated pylon and APU leak detection is lost.", "false" ] } ], "ref": "Ref. Airbus TTM ATA 36 page 42" }, { "ch": "When start the right engine using ground air supply:", "ansGr": [ { "ans": [ "The cross-bleed selector must be left in close position.", "false" ] }, { "ans": [ "The cross-bleed selector must be left in auto position.", "false" ] }, { "ans": [ "The cross-bleed selector must be left in open position.", "true" ] } ], "ref": "Ref. AMM 36-12-00-00 CONF 00" }, { "ch": "In normal condition, if both engine and APU bleed sources are selected ON, what will supply to the packs?", "ansGr": [ { "ans": [ "APU Bleed only.", "true" ] }, { "ans": [ "Engine bleed 1 for Pack1 and Engine bleed 2 for Pack 2.", "false" ] }, { "ans": [ "Wrong configuration, no bleed can supply the packs.", "false" ] } ], "ref": "Ref. AMM 36-12-00-00 CONF 00" }, { "ch": "From Cockpit can you check the HP pneumatic GND cart is connected to the A/C?", "ansGr": [ { "ans": [ "No, it does not indicate that external pneumatic supply is connected or even that the access door is open", "true" ] }, { "ans": [ "Yes, check the “GND” indication on the ECAM BLEED page.", "false" ] }, { "ans": [ "Yes, check the “GND” indication on the control panel.", "false" ] } ], "ref": "Ref. Airbus TTM ATA 23 page 34" } ]