[ { "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": "If a hydraulic pipe has been replaced in the suction line from the reservoir to the EDP or electric pump, bleeding is performed in accordance with:", "ansGr": [ { "ans": [ "The \"Upstream of the engine or electric pump\" procedures as appropriate to the maintenance carried out.", "true" ] }, { "ans": [ "The \"Upstream of the engine\" procedure regardless of the maintenance activity.", "false" ] }, { "ans": [ "The \"Downstream of the engine or electric pump\" procedures as appropriate to the maintenance carried out.", "false" ] } ], "ref": "Ref: AMM Task 29-00-00-870-804A" }, { "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": "After checking the manual extension of the RAT and before retracting it:", "ansGr": [ { "ans": [ "Pressurize the blue hydraulic system.", "false" ] }, { "ans": [ "Check the retraction interlock by turning the blades away from the index position.", "true" ] }, { "ans": [ "Pressurize the yellow system.", "false" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 162" }, { "ch": "When checking the RAT gearbox oil level is correct:", "ansGr": [ { "ans": [ "No oil must be visible in the sight glass.", "false" ] }, { "ans": [ "The oil level should be above the middle of the sight glass.", "false" ] }, { "ans": [ "Check the oil level on the middle of the sight glass.", "true" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 180" }, { "ch": "The MCDU test function for the hydraulic system monitoring unit (HSMU) will:", "ansGr": [ { "ans": [ "Perform a test of the reservoir (fluid) overheat channel.", "true" ] }, { "ans": [ "Check the electrical pump overheat detection system only.", "false" ] }, { "ans": [ "Check the Engine Driven Pump (EDP) auto-depressurization mode only.", "false" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 26" }, { "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 green and blue reservoir low level.", "false" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 48" }, { "ch": "The green electric pump is automatically latched off following an electric pump:", "ansGr": [ { "ans": [ "Overheat.", "false" ] }, { "ans": [ "Phase unbalance detected by HSMU.", "true" ] }, { "ans": [ "Phase unbalance detected by RCCB.", "false" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 46" }, { "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 29-11/12/13-00-00 CONF00" }, { "ch": "The engine 2 hydraulic fire shut off valve can:", "ansGr": [ { "ans": [ "Shut automatically following a blue reservoir low level.", "false" ] }, { "ans": [ "Shut 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 electric pump 115VAC power supply is monitored by the:", "ansGr": [ { "ans": [ "Hydraulic System Monitoring Unit (HSMU).", "false" ] }, { "ans": [ "Current Unbalance Detection Unit (CUDU).", "true" ] }, { "ans": [ "High/low voltage monitoring unit.", "false" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 46" }, { "ch": "The G HP filter and sampling valve are located on the:", "ansGr": [ { "ans": [ "HP manifold.", "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": "Which statement is NOT correct regarding leak measurement valve?", "ansGr": [ { "ans": [ "Leak measurement valve is a two position, three-way, solenoid-operated type.", "false" ] }, { "ans": [ "The valve is normally open. it is closed when the solenoid is energized. in this case there is a leakage flow.", "false" ] }, { "ans": [ "The valve is normally open. It is closed when the solenoid is de-energized. in this case there is a leakage flow", "true" ] } ], "ref": "Ref AMM 29-19-00-00 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": [ "The Yellow leak measurement valve automatic closed.", "true" ] }, { "ans": [ "The Yellow leak measurement valve automatic opened.", "false" ] }, { "ans": [ "The 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": "The purpose of the manual selector valve is to:", "ansGr": [ { "ans": [ "Cut off hydraulic power to isolate the flight controls.", "false" ] }, { "ans": [ "Give priority to the primary flight controls in flight only.", "false" ] }, { "ans": [ "This four-position valve is used for the selection of the reservoir to be filled", "true" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 06" }, { "ch": "To carry out the leak test it is necessary to pressurize the system with:", "ansGr": [ { "ans": [ "An Engine-Driven Pump (EDP).", "false" ] }, { "ans": [ "An electric pump provides a minimum of 2,850 psi.", "false" ] }, { "ans": [ "A ground service cart.", "true" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 116" }, { "ch": "When flight above 100 Kts, when the guarded leak measurement switch is released:", "ansGr": [ { "ans": [ "The leak measurement valve closes.", "false" ] }, { "ans": [ "The leak measurement valve position has not changed.", "true" ] }, { "ans": [ "The manual selector valves close.", "false" ] } ], "ref": "Ref: Airbus TTM ATA 29 Page 54" }, { "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.", "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 type .", "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": "The current unbalance detector units (CUDU) are used to:", "ansGr": [ { "ans": [ "It detects a current balance or a cut-off one or two phases three-phase power supply of the electric pumps.", "false" ] }, { "ans": [ "It detects a current unbalance and cuts off all three-phase power supply of the electric pumps.", "false" ] }, { "ans": [ "It detects a current unbalance or a cut-off one or two phases three-phase power supply of the electric pumps.", "true" ] } ], "ref": "Ref: AMM 29-21-00-00 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 a bypass device.", "false" ] } ], "ref": "Ref: AMM 29-16-00-00 CONF 00" }, { "ch": "The purpose of 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 pressurizing system ensures in each hydraulic reservoir an air pressure of 5.5 bars absolute in flight and on ground so as to avoid cavitations of the pumps on the ground and throughout the whole flight envelope.", "false" ] } ], "ref": "Ref: AMM 29-16-00-00 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 from?", "ansGr": [ { "ans": [ "HYD control panel.", "true" ] }, { "ans": [ "ELEC control panel.", "false" ] }, { "ans": [ "AIRCON control panel.", "false" ] } ], "ref": "Ref: AMM 29-24-00-00 CONF 00" }, { "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": "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" ] } ] }, { "ch": "Escape slide locking mechanism are electrically heated:", "ansGr": [ { "ans": [ "At first engine start-up.", "false" ] }, { "ans": [ "At door closed and armed.", "false" ] }, { "ans": [ "In case of icing conditions.", "true" ] } ], "ref": "Ref. AMM 30-46-00-00 CONF 00" }, { "ch": "On the ice & rain protection system, the bite sensor, which interfaces directly with the central maintenance system, is the:", "ansGr": [ { "ans": [ "Pitot probe.", "false" ] }, { "ans": [ "Ice detector.", "true" ] }, { "ans": [ "Total Air Temperature (TAT) sensor.", "false" ] } ], "ref": "Ref. AMM 30-81-00-00 CONF 00" }, { "ch": "Left and right wing anti-ice valves are:", "ansGr": [ { "ans": [ "Identical and have the same locking procedure.", "true" ] }, { "ans": [ "Different but have the same locking procedure.", "false" ] }, { "ans": [ "Identical but have different locking procedure.", "false" ] } ], "ref": "Ref. AMM Task 30-11-00-040-801-A" }, { "ch": "After deactivation of the engine air-intake anti-ice valve in the closed locked position, you have to:", "ansGr": [ { "ans": [ "Deactivate the engine air-intake ANTI ICE P/B SW in the OFF position and make an entry in the A/C technical log.", "false" ] }, { "ans": [ "Deactivate the engine air-intake ANTI ICE P/B SW in the ON position and make an entry in the A/C technical log.", "true" ] }, { "ans": [ "Deactivate the engine air-intake ANTI ICE P/B SW on ANTI ICE valve and make an entry in the A/C technical log.", "false" ] } ], "ref": "Ref. AMM Task 30-21-00-040-801-A" }, { "ch": "The two-water ice protection control units (IPCUs) are located:", "ansGr": [ { "ans": [ "In the avionics bay.", "false" ] }, { "ans": [ "One in the cockpit 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": "In flight when the crew selects the wing anti-ice system ON, the configuration of the system is:", "ansGr": [ { "ans": [ "Solenoids energized and valves open.", "true" ] }, { "ans": [ "Solenoids energized and valves closed.", "false" ] }, { "ans": [ "Solenoids de-energized and valves closed.", "false" ] } ], "ref": "Ref. AMM 30-11-00-00 CONF 00" }, { "ch": "When the flight crew selects engine anti-icing ON, the configuration of the engine anti-ice system is:", "ansGr": [ { "ans": [ "Solenoid energized and valve open.", "false" ] }, { "ans": [ "Solenoid de-energized and valve open", "true" ] }, { "ans": [ "Solenoid energized and valve close.", "false" ] } ], "ref": "Ref. AMM 30-21-00-00 CONF 22" }, { "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": "Disconnection of power supply to which computer will activate probe heat system?", "ansGr": [ { "ans": [ "PHC(s) and EIVMU(s).", "false" ] }, { "ans": [ "LGCIU(s) and EIVMU(s).", "false" ] }, { "ans": [ "Either PHC(s), EIVMU (s), LGCIU(s).", "true" ] } ], "ref": "Ref. Airbus TTM ATA 30 Page 27" }, { "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": [ "GO IF items.", "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": "In the case of one SDAC, one FWC and two DMCs inop. The EIS (Electronic Instrument System):", "ansGr": [ { "ans": [ "Still operates normally.", "true" ] }, { "ans": [ "Operates with ECAM and Capt. EFIS available.", "false" ] }, { "ans": [ "Operates with EWD, Capt. PFD and F/O ND available.", "false" ] } ], "ref": "Ref: AMM 31-60-00-00 CONF 01" }, { "ch": "Which is the main function of the Clock?", "ansGr": [ { "ans": [ "Provides UTC to the FMGEC 1 & 2, the FDIU and the CMC", "true" ] }, { "ans": [ "Provides GMT to the FMGEC 1 and 2, the FDIU and the CMC1 and 2.", "false" ] }, { "ans": [ "Provides UTC which is indicated on lower ECAM DU.", "false" ] } ], "ref": "Ref: AMM 31-21-00-00 CONF 00" }, { "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": "MLG changeover valve can be?", "ansGr": [ { "ans": [ "Activated one time only.", "false" ] }, { "ans": [ "Activated and reactivated for 3 time maximum with no limitation.", "false" ] }, { "ans": [ "Activated and reactivated for 3 time maximum after certain period of time interval.", "true" ] } ], "ref": "Ref. AMM 32-11-13-860-801" }, { "ch": "Energize the MLG secondary seal to confirmed hydraulic leak:", "ansGr": [ { "ans": [ "Re-energize primary seal not more than seven days.", "true" ] }, { "ans": [ "Re-energize primary seal more than seven days.", "false" ] }, { "ans": [ "Do not re-energize the primary seal.", "false" ] } ], "ref": "Ref. AMM 32-11-13-860-801" }, { "ch": "How you confirm the leak of MLG gland seal?", "ansGr": [ { "ans": [ "Visual check on the chrome surface of the slide member for the film of hydraulic leak.", "true" ] }, { "ans": [ "Check for leaks at the drain hole on the pitch trimmer attachment lug.", "false" ] }, { "ans": [ "Check the hydraulic fluid content in the MLG shock absorber.", "false" ] } ], "ref": "Ref. AMM 32-11-13-860-801" }, { "ch": "To reset the LDG normal extension system after a free fall extension during flight, you do?", "ansGr": [ { "ans": [ "Select the RESET on the free fall selector.", "false" ] }, { "ans": [ "Select the RESET on the free fall selector with Green system pressurized.", "true" ] }, { "ans": [ "Use the LDG door ground control system with Green system pressurized to retract the doors.", "false" ] } ], "ref": "Ref. AMM 32-33-00-710-809" }, { "ch": "To have BRAKES Pressure Indicator INOP, MEL requires checking ALTN brake system, how you do that?", "ansGr": [ { "ans": [ "Pressurize the Yellow system and push pedals or set parking brake", "false" ] }, { "ans": [ "Pressurize the Blue system and push pedals", "false" ] }, { "ans": [ "Pressurize the Blue system and push pedals with A/SKID & N/W STRG ON", "true" ] } ], "ref": "Ref. AMM 32-44-00-040-801, AMM 32-43-00-710-801-A" }, { "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 can 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.", "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 nose wheels.", "false" ] }, { "ans": [ "Mixability allowed only for new tires.", "false" ] } ], "ref": "Ref. AMM 32-41-00-200-802" }, { "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": [ "Wear pin is longer than a certain value.", "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 another indicator is still in limit.", "true" ] }, { "ans": [ "Aircraft can be dispatched like it is. No action is 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 in the rolling direction of AFT to FWD.", "false" ] } ], "ref": "Ref. AMM 32-41-11-400-801" }, { "ch": "During wheel installation, after apply the required final torque value, if the axle nut slots still do not align with the bolt holes in the axle, what 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 alligned.", "true" ] } ], "ref": "Ref. AMM 32-41-11-400-801" }, { "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": [ "Doors 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": "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 apply the high temperature type of grease to all surfaces contacts.", "false" ] } ], "ref": "Ref. AMM 32-42-27-400-801" }, { "ch": "Which unit gives the landing gear DOWN LOCKED information to LDG control panel?", "ansGr": [ { "ans": [ "LGCIU 1 only", "true" ] }, { "ans": [ "Either LGCIU in turn", "false" ] }, { "ans": [ "Both LGCIUs simultaneously.", "false" ] } ], "ref": "Ref. AMM 32-31-00-00 CONF 00" }, { "ch": "With parking brake applied and brake pedals pressed, the pedals brake.", "ansGr": [ { "ans": [ "Will always be deactivated.", "true" ] }, { "ans": [ "Will be activated if Blue pressure drops while Green pressure is available.", "false" ] }, { "ans": [ "Both parking brake and pedals brake will be activated at the same time.", "false" ] } ], "ref": "Ref. AMM 32-45-00-00 CONF 00" }, { "ch": "You use the manual depressurization lever located on the hydraulic parking brake manifold to?", "ansGr": [ { "ans": [ "Depressurize the air pressure charged in the accumulator.", "false" ] }, { "ans": [ "Depressurize the Blue hydraulic system.", "false" ] }, { "ans": [ "Release the pressure from the parking brake system.", "true" ] } ], "ref": "Ref. AMM 32-45-00-864-801" }, { "ch": "To Removal of the NLG Leg Assy:", "ansGr": [ { "ans": [ "Lift the aircraft with 3 jacks only.", "false" ] }, { "ans": [ "Lift the aircraft with 4 jacks only.", "false" ] }, { "ans": [ "Can lift the aircraft with only FWD jack.", "true" ] } ], "ref": "Ref. AMM 32-21-00-000-801 and AMM 07-11-00-851-802" }, { "ch": "Which reservoir must be depressurized before removing the NLG?", "ansGr": [ { "ans": [ "Depressurize the reservoir of the Green hydraulic system.", "true" ] }, { "ans": [ "Depressurize the nose-gear shock absorber.", "false" ] }, { "ans": [ "Depressurize the nose-wheel steering accumulator.", "false" ] } ], "ref": "Ref. AMM 32-21-00-000-801  " }, { "ch": "When disconnection of the Upper Drag Stay at its Attachment with the Lower Drag Stay, you need:", "ansGr": [ { "ans": [ "Push the nose gear leg to the front to prevent damage to the component of nose landing gear doors.", "true" ] }, { "ans": [ "Push the nose gear leg to the aft to prevent damage to the component of nose landing gear doors.", "false" ] }, { "ans": [ "Keep NLG stable at vertical position.", "false" ] } ], "ref": "Ref. AMM 32-21-00-000-801" }, { "ch": "When engage the trunnion pins of NLG into the bearings?", "ansGr": [ { "ans": [ "You must install only one washer on each side.", "true" ] }, { "ans": [ "You can install one or more washers on each side.", "false" ] }, { "ans": [ "You can install one or more washers on one side.", "false" ] } ], "ref": "Ref. AMM 32-21-00-400-801" }, { "ch": "Which position of the flaps is corrected when removing the MLG leg assembly?", "ansGr": [ { "ans": [ "The flaps are fully extended.", "true" ] }, { "ans": [ "The flaps are in 2nd position.", "false" ] }, { "ans": [ "The flaps are fully retracted.", "false" ] } ], "ref": "Ref. AMM 32-11-11-000-801" }, { "ch": "When doing remove of the MLG Leg Assembly, which pintle pin must be removed first?", "ansGr": [ { "ans": [ "Removal of the Rear Pintle Pin first and then Removal of the Forward Pintle Pin", "true" ] }, { "ans": [ "Removal of the Forward Pintle Pin first and then Removal of the Rear Pintle Pin", "false" ] }, { "ans": [ "No specific sequence must be followed.", "false" ] } ], "ref": "Ref. AMM 32-11-11-000-801" }, { "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": "What is the signal from engine transmits to CISD to dim forward LH entrance illumination to 10% when cockpit door is opened, and the engine is running?", "ansGr": [ { "ans": [ "The oil pressure signal", "true" ] }, { "ans": [ "The N1 signal", "false" ] }, { "ans": [ "The N2 signal", "false" ] } ], "ref": "Ref. AMM 33-21-00-00 CONF 00 Figure 33-21-00-16550" }, { "ch": "In case NAV light system uses source from the towing tractor supply, which NAV light system will operate?", "ansGr": [ { "ans": [ "NAV light system 1 or system 2", "false" ] }, { "ans": [ "NAV light system 2", "false" ] }, { "ans": [ "NAV light system 1", "true" ] } ], "ref": "Ref. AMM 33-41-00-00 CONF 00 Figure 33-41-00-14400" }, { "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": [ "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 flood lighting?", "ansGr": [ { "ans": [ "Full brightness and not dependent 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": "The NAV lights include:", "ansGr": [ { "ans": [ "28V lamps with red lens on the left-hand wing, 28V lamps with green lens on the right-hand wing and 12V lamps on the rearward", "true" ] }, { "ans": [ "12V lamps with red lens on the left-hand wing, 12V lamps with green lens on the right-hand wing and 12V lamps on the rearward", "false" ] }, { "ans": [ "28V lamps with red lens on the left-hand wing, 28V lamps with green lens on the right-hand wing and 28V lamps on the rearward", "false" ] } ], "ref": "Ref. AMM 33-41-00-00 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": "When you set the switch taxi take off light to the", "ansGr": [ { "ans": [ "O position:", "false" ] }, { "ans": [ "Only 600W lamps beam come ON.", "false" ] }, { "ans": [ "Only 400W lamps beam come ON.", "false" ] }, { "ans": [ "Both 600W lamps beam and 400W lamps beam come ON (only has GND signal from LGCIU1,2 when NLG down locked)", "true" ] } ], "ref": "Ref. AMM 33-46-00-00 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": "Two tests of the cabin emergency lighting system from the MCDU are:", "ansGr": [ { "ans": [ "System test and battery capacity test", "true" ] }, { "ans": [ "Operation test and Function test", "false" ] }, { "ans": [ "System test and Function test", "false" ] } ], "ref": "Ref. AMM 33-51-00-00 CONF 00" }, { "ch": "The cabin lighting is controlled from:", "ansGr": [ { "ans": [ "The Circuit Breaker panel 2000 VU.", "false" ] }, { "ans": [ "The CIDS FAP and several AAPs", "true" ] }, { "ans": [ "Any attendant station.", "false" ] } ], "ref": "Ref. AMM 33-21-00-00 CONF 00" }, { "ch": "The overhead exit marking and exit location signs come on automatically when:", "ansGr": [ { "ans": [ "The switch FASTEN SEAT BELT in the ON position and landing gear is extended.", "false" ] }, { "ans": [ "The switch EMER EXIT LT is in AUTO position and landing gear is extended.", "false" ] }, { "ans": [ "The switch NO SMOKING is in AUTO position and landing gear is extended.", "true" ] } ], "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 Wind shear 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": "Vertical Speed (V/S) is computed by:", "ansGr": [ { "ans": [ "ADR", "false" ] }, { "ans": [ "IR and ADR if IR fault", "true" ] }, { "ans": [ "Either ADR or IR", "false" ] } ], "ref": "Ref. AMM 34-13-00-00 CONF 03" }, { "ch": "In the ATT mode, IR supplying:", "ansGr": [ { "ans": [ "Attitude, heading, angular rates and accelerations", "false" ] }, { "ans": [ "Attitude only", "false" ] }, { "ans": [ "Attitude and heading", "true" ] } ], "ref": "Ref. AMM 34-14-00-00 CONF 03" }, { "ch": "The airspeed indication on the PFD starts at:", "ansGr": [ { "ans": [ "80 knots.", "false" ] }, { "ans": [ "60 knots.", "false" ] }, { "ans": [ "30 knots.", "true" ] } ], "ref": "Ref AMM 34-13-00-00 CONF 03" }, { "ch": "Radio Height is displayed on the PFD:", "ansGr": [ { "ans": [ "Below 2500 feet.", "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": "In case of loss of AIR DATA parameters on CAPT or F/O PFD and ND, the affected displays can be manually selected over to ADR 3 by the:", "ansGr": [ { "ans": [ "ECAM/ND transfer selector", "false" ] }, { "ans": [ "AIR DATA selector", "true" ] }, { "ans": [ "ATT HDG selector", "false" ] } ], "ref": "Ref AMM 34-13-00-00 CONF 03" }, { "ch": "Which statement is correct regarding the rapid realign?", "ansGr": [ { "ans": [ "The OFF/NAV/ATT selector switches from NAV to OFF and back to NAV within 5 seconds. The align completes in 30 seconds.", "true" ] }, { "ans": [ "You can only do rapid realign if the ground speed is more than 20 knots.", "false" ] }, { "ans": [ "Realign is initialized with existing attitude, heading angles and velocities.", "false" ] } ], "ref": "Ref AMM 34-14-00-00 CONF 03" }, { "ch": "The ON BAT indicator in ADIRS Mode Selector Unit comes on when?", "ansGr": [ { "ans": [ "One or more ADIRUs are supplied by batteries.", "true" ] }, { "ans": [ "You align ADIRUs with only batteries supplied.", "false" ] }, { "ans": [ "Battery is not able to supply the ADIRUs.", "false" ] } ], "ref": "Ref AMM 34-14-00-00 CONF 03" }, { "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 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 HF system and carry out maintenance on HF system,", "false" ] } ], "ref": "Ref. AMM 35-00-00-860-801" }, { "ch": "Indicating of flight crew oxygen system on ECAM DOOR/OXY page is sent through:", "ansGr": [ { "ans": [ "DMC1, DMC2 and DMC3.", "false" ] }, { "ans": [ "FWC1 and FWC2.", "false" ] }, { "ans": [ "SDAC1 and SDAC2.", "true" ] } ], "ref": "Ref. AMM 35-10-00-00 CONF 00" }, { "ch": "When you do leakage test of the LP oxygen for the crew, you can:", "ansGr": [ { "ans": [ "Test with the nitrogen source,", "false" ] }, { "ans": [ "Test with the Oxygen Cylinder source,", "false" ] }, { "ans": [ "Test with the nitrogen source or the Oxygen Cylinder source.", "true" ] } ], "ref": "Ref. AMM: 35-10-00-790-801 A/A01" }, { "ch": "The CKPT OXY indication in amber on ECAM DOOR/OXY page when", "ansGr": [ { "ans": [ "The CREW SUPPLY P/BSW is OFF and oxygen high pressure is less than 400 PSI.", "false" ] }, { "ans": [ "There is detection low 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 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" }, { "ch": "For passenger oxygen system. To avoid the full release of all the oxygen masks during do functional test of the automatic Mask release, you must:", "ansGr": [ { "ans": [ "Pull out the test push buttons and turn them 90 degrees to the TEST position on all of the emergency oxygen containers.", "true" ] }, { "ans": [ "Pull out the door stops and turn them 180 degrees to the TEST position on all of the emergency oxygen containers.", "false" ] }, { "ans": [ "Apply high speed tape around all of the emergency containers.", "false" ] } ], "ref": "Ref. AMM 35-21-00-720-801-A" }, { "ch": "For passenger oxygen system. When you do operational test of a circuit of the emergency oxygen containers, you must:", "ansGr": [ { "ans": [ "Open, safety and tag all the passenger oxygen control/actuator circuit breakers", "false" ] }, { "ans": [ "Close all the passenger oxygen control/actuator circuit breakers,", "false" ] }, { "ans": [ "Open, safety and tag all the passenger oxygen control/actuator circuit breakers except the circuit breaker of the area being checked.", "true" ] } ], "ref": "Ref. AMM 35-21-00-710-805-A" }, { "ch": "The functional test of regulator can be done by:", "ansGr": [ { "ans": [ "Pressing the TEST/EMERGENCY knob", "true" ] }, { "ans": [ "Pressing the PRESS TO TEST AND RESET push button,", "false" ] }, { "ans": [ "Push and release CREW SUPPLY push button,", "false" ] } ], "ref": "Ref. AMM 35-12-00-00 CONF 00 Operation of the Regulation" }, { "ch": "Before remove the crew oxygen cylinder, you must do:", "ansGr": [ { "ans": [ "Close the ON/OFF valve and bleed the oxygen system.", "true" ] }, { "ans": [ "Make sure there is no leak in 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 CREW SUPPLY P/B is pushed in and oxygen high pressure equal or more than 300psi. 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": "When you replace crew oxygen cylinder/valve Assy you must:", "ansGr": [ { "ans": [ "Replaced conical seal on the HP oxygen-overpressure hose by new one.", "true" ] }, { "ans": [ "Replaced rubber O-ring seal on the HP oxygen-overpressure hose by new one,", "false" ] }, { "ans": [ "Replaced seals on the HP oxygen-overpressure and LP oxygen-overpressure hoses with new ones.", "false" ] } ], "ref": "Ref. AMM 35-11-41-400-801" }, { "ch": "To inspect oxygen pressure for flight crew. The reference temperature is calculated by:", "ansGr": [ { "ans": [ "Average outside air temperature (OAT) and cabin temperature.", "true" ] }, { "ans": [ "Average of outside air temperature (OAT) and avionic compartment temperature,", "false" ] }, { "ans": [ "Overage of outside air temperature (OAT) and cockpit temperature,", "false" ] } ], "ref": "Ref Airbus ATA 35 TTM page 93" }, { "ch": "What functions are ensured by pressure regulator/transmitter?", "ansGr": [ { "ans": [ "Reduce the LP delivered by the oxygen cylinder in HP compatible with the distribution equipment,", "false" ] }, { "ans": [ "Reduce the LP delivered by the oxygen cylinder in LP compatible with the distribution equipment,", "false" ] }, { "ans": [ "Reduce the HP delivered by the oxygen cylinder in LP compatible with the distribution equipment,", "true" ] } ], "ref": "Ref. AMM 35-11-00-00 CONF 00: Pressure regulator/transmitter" }, { "ch": "When you do detail inspection/check of mask full face/quick donning, you do:", "ansGr": [ { "ans": [ "Check the correct position of mask lock.", "false" ] }, { "ans": [ "Make sure that the doors of the oxygen-mask stowage box open and close correctly.", "false" ] }, { "ans": [ "Check of the correct position of mask lock and correct torque of the retaining screw", "true" ] } ], "ref": "Ref. AMM 35-12-41-200-804" }, { "ch": "The passenger emergency-oxygen is stored in oxygen containers, and which have:", "ansGr": [ { "ans": [ "The chemical emergency oxygen-generators,", "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": [ "Normally opens when the system is using APU bleed air and closes if the system detects an air leak (except in flight).", "false" ] }, { "ans": [ "Normally opens when the system is using APU bleed air and closes automatically 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": [ "  Will 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": "If the pylon loop is inoperative", "ansGr": [ { "ans": [ "The overheat detection in the corresponding pylon is not affected.", "false" ] }, { "ans": [ "The overheat detection in the corresponding pylon is lost.", "true" ] }, { "ans": [ "The overheat detection in the corresponding pylon is transferred to the opposite BMC.", "false" ] } ], "ref": "Ref. AMM 36-22-00-00 CONF 00" }, { "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 overpressure (the PRV does not operate correctly), the engine bleed system protection is ensured by:", "ansGr": [ { "ans": [ "Pneumatically controlled Overpressure Valve.", "true" ] }, { "ans": [ "Pneumatically operated, electrically controlled Overpressure Valve.", "false" ] }, { "ans": [ "Pneumatically controlled Fan Air Valve.", "false" ] } ], "ref": "Ref. Airbus TTM ATA 36 page 12" }, { "ch": "On the engine bleed system, the auto switching between HP and IP source is:", "ansGr": [ { "ans": [ "Automatically achieved by internal EEC logic", "false" ] }, { "ans": [ "Electrically controlled by BMC", "false" ] }, { "ans": [ "Pneumatically achieved.", "true" ] } ], "ref": "Ref. Airbus TTM ATA 36 page 12" }, { "ch": "The temperature regulation of the engine bleed air is performed by:", "ansGr": [ { "ans": [ "The Fan Air Valve (FAV).", "true" ] }, { "ans": [ "The Bleed Valve.", "false" ] }, { "ans": [ "The HP bleed valve.", "false" ] } ], "ref": "Ref. Airbus TTM ATA 36 page 30" }, { "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": "The engine bleed air temperature is regulated by the Fan Air Valve (FAV) controlled by the Control Thermostat (ThC):", "ansGr": [ { "ans": [ "To ensure always 200°C outlet air", "false" ] }, { "ans": [ "To ensure always 150°C outlet air", "false" ] }, { "ans": [ "To ensure 150°C or 200°C outlet air depending on A/C configuration (Pack temperature demand, Wing Anti-ice use)", "true" ] } ], "ref": "Ref. Airbus TTM ATA 36 page 12" }, { "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 the HPV, PRV deactivated", "ansGr": [ { "ans": [ "The locking pin secured the valve shaft in closed position", "true" ] }, { "ans": [ "The locking pin ensures the motive pressure of the valve opening chamber to vent outboard (to vent the opening pressure)", "false" ] }, { "ans": [ "The locking pin ensures the valve shaft in unlocks position.", "false" ] } ], "ref": "Ref. Airbus TTM ATA 36 page 56" }, { "ch": "The test port of the HPV, PRV is used to:", "ansGr": [ { "ans": [ "Check leak of the sense lines and assembly", "false" ] }, { "ans": [ "Simulate the operation of the valves", "true" ] }, { "ans": [ "Check leak of the valve and assembly", "false" ] } ], "ref": "Ref. AMM 36-11-51-720-810, AMM 36-11-52-720-809" }, { "ch": "The cross-bleed valve is:", "ansGr": [ { "ans": [ "Solenoid controlled and pneumatically operated", "false" ] }, { "ans": [ "Electrically controlled, operated by two electrical motors.", "true" ] }, { "ans": [ "Electrically controlled, operated by one electrical motor.", "false" ] } ], "ref": "Ref. AMM 36-12-00-00 CONF 00" }, { "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": "The ENG bleed ‘FAULT’ comes on ECAM when", "ansGr": [ { "ans": [ "One corresponding wing loop is inoperative", "false" ] }, { "ans": [ "Overpressure or over temperature occurs", "true" ] }, { "ans": [ "Low pressure or over temperature occurs", "false" ] } ], "ref": "Ref. Airbus TTM ATA 23 page 34" }, { "ch": "Failure of which component does NOT cause the associated bleed system to be inoperative?", "ansGr": [ { "ans": [ "FAV", "false" ] }, { "ans": [ "PRV", "false" ] }, { "ans": [ "HPV", "true" ] } ], "ref": "Ref. MEL 36-11-07B/07C, AMM 36-11-00-040-812" }, { "ch": "In normal condition, if both engine and APU bleed sources are selected ON, what will supply to the packs?", "ansGr": [ { "ans": [ "APU bleeds 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" } ]