[ { "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": "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": "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 electric pump is automatically latched off when:", "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": [ "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": "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": [ "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": "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": "In 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 is 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 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 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-by-passing 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 HYD engine EDP pumps.", "false" ] }, { "ans": [ "It detects a current unbalance and cut-off all three phase power supply of the HYD electric pumps.", "false" ] }, { "ans": [ "It detects a current unbalance or a cut-off one or two phases three-phase power supply of the HYD 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 by-pass 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 reservoir is non-pressurized system .", "false" ] } ], "ref": "Ref: AMM 29-16-00-00 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": "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" ] } ], "ref": "D. 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": [ "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 INNER and right OUTER 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 OPEN 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 in the AUTO position and make an entry in the A/C technical", "false" ] } ], "ref": "Ref. AMM Task 30-21-00-040-807-A" }, { "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": "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 opened.", "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": "Disconnections 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": "The action required when you perform removal/installation of the FDIMU?", "ansGr": [ { "ans": [ "No specific action is required.", "false" ] }, { "ans": [ "Do the upload engine hours and cycles to the FDIMU.", "true" ] }, { "ans": [ "Removal/installation like other LRU.", "false" ] } ], "ref": "Ref. AMM 31-36-34-04 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": [ "Must 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": "In case of one SDAC, one FWC and two DMCs Inop. The EIS (Electronic Instrument System):", "ansGr": [ { "ans": [ "Still operates normally.", "true" ] }, { "ans": [ "Only Operates with ECAM and Capt. EFIS available.", "false" ] }, { "ans": [ "Only Operates with EWD, Capt. PFD and F/O ND available.", "false" ] } ], "ref": "Ref: AMM 31-60-00-00 CONF 01" }, { "ch": "The message CHECK HDG appears on the heading scale of the PFD and ND, it means:", "ansGr": [ { "ans": [ "No heading data from ADIRS.", "false" ] }, { "ans": [ "The heading data is not correct.", "false" ] }, { "ans": [ "The FWC detects a difference between the heading indications.", "true" ] } ], "ref": "Ref: AMM 31-64-00-00 CONF 00" }, { "ch": "In case ECAM DMC 2&3 are not valid (ECAM DMC 1 in normal operation), what is/are happening with the ECAM display units?", "ansGr": [ { "ans": [ "ECAM display units select inputs from ECAM DMC 1 automatically if ECAM/SWICHING Selector in AUTO or 1 position", "true" ] }, { "ans": [ "ECAM displays are lost", "false" ] }, { "ans": [ "Only EWD ECAM display available", "false" ] } ], "ref": "Ref: AMM 31-68-00-00 CONF 00" }, { "ch": "The Engine Standby Page is generated by:", "ansGr": [ { "ans": [ "FWCs", "false" ] }, { "ans": [ "SDACs", "false" ] }, { "ans": [ "EFIS parts of the DMCs", "true" ] } ], "ref": "Ref: AMM 31-65-00-00 CONF 00" }, { "ch": "Which type of the failure message when it indicated on the left side of the EWD in a frame?", "ansGr": [ { "ans": [ "Primary Failure and Secondary Failure.", "false" ] }, { "ans": [ "Primary Failure and Independent Failure.", "true" ] }, { "ans": [ "Independent Failure and Secondary Failure.", "false" ] } ], "ref": "Ref: AMM 31-51-00-00 CONF 00" }, { "ch": "When do the Captain and F/O receive the same EFIS information?", "ansGr": [ { "ans": [ "If there is only a single source for EFIS indication, two EFIS parts have failed, and this status is called “Copy Mode”", "true" ] }, { "ans": [ "If two source for EFIS indication, one EFIS part have failed, and this status is called “Copy Mode”", "false" ] }, { "ans": [ "If three EFIS parts of DMCs are in normal operation.", "false" ] } ], "ref": "Ref: AMM 31-62-00-00 CONF 00" }, { "ch": "In Emergency operation (AC bus 1&2, DC bus 1&2 are not supplied):", "ansGr": [ { "ans": [ "Captain PDF, Captain ND, ECAM are available.", "false" ] }, { "ans": [ "Captain PDF, Captain ND, EWD are available.", "true" ] }, { "ans": [ "Captain PDF, F/O PFD, ECAM are available.", "false" ] } ], "ref": "Ref: AMM 31-60-00-00 CONF 00" }, { "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": "What is the difference between Alpha Call Up and Label Call Up?", "ansGr": [ { "ans": [ "Alpha Call Up to read various parameters directly; Label Call Up to read selected digital data words, the readouts have to be decoded then.", "true" ] }, { "ans": [ "Alpha Call Up to read selected digital data words, the readouts have to be decoded then. Label Call Up to read various parameters directly.", "false" ] }, { "ans": [ "Alpha Call Up and Label Call Up are a means to read parameters directly, but in different ways.", "false" ] } ], "ref": "Ref. Airbus TTM ATA 31 Page 62 & 64" }, { "ch": "What is/are the function(s) of the FDIU (Flight Data Interface Unit)?", "ansGr": [ { "ans": [ "FDIU collects various basic A/C system parameters, builds up reports then transmits them to DFDR (Digital Flight Data Recorder) for recording.", "true" ] }, { "ans": [ "FDIU receives all parameters from all A/C systems then makes reports for sending via ACARS or print.", "false" ] }, { "ans": [ "FDIU collects various basic A/C system parameters, converts then transmits to FDR.", "false" ] } ], "ref": "Ref: AMM 31-33-00-00 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 & MLGs 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 3 times maximum with no limitation.", "false" ] }, { "ans": [ "Activated and reactivated 3 times maximum after certain period of time interval.", "true" ] } ], "ref": "Ref. AMM 32-11-13-860-801" }, { "ch": "Energize the MLG secondary seal to confirm 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 leak 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 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; 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 nose 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": "You will have to 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 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": [ "To prevent possible gears and doors operation on ground.", "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": [ "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-install to new brake", "false" ] }, { "ans": [ "Need to be attached with the removed brake unit and sent back to 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 applies 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": "Interface between the external power supply and navigation light during towing?", "ansGr": [ { "ans": [ "From electrical box-oversteer warning 8GH.", "true" ] }, { "ans": [ "From electrical de-activation box 5GC.", "false" ] }, { "ans": [ "External power receptacle A or B", "false" ] } ], "ref": "Ref. AMM 32-51-00-00 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 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": "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 CIDS 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 happens when you put the switch of dome light to STORM position and the switch 29LE on left rear panel in the cockpit to OFF position?", "ansGr": [ { "ans": [ "The dome lights still on", "true" ] }, { "ans": [ "The dome light off", "false" ] }, { "ans": [ "The dome light dim to 10%", "false" ] } ], "ref": "Ref. AMM 33-12-00-00-CONF 00 Figure 33-12-00-15000" }, { "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 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": "Why does the brightness of the dome lights decrease when we turn the switch 5LE to DIM position?", "ansGr": [ { "ans": [ "Because the lamps are supplied in parallel by group of two", "false" ] }, { "ans": [ "Because the lamps are supplied in series by group of two", "true" ] }, { "ans": [ "Because of only a haft of lamps illuminate", "false" ] } ], "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": "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": "When do the landing lights come on?", "ansGr": [ { "ans": [ "The landing lights switch is in ON position", "true" ] }, { "ans": [ "Nose landing gear down lock and landing light switch is in ON position", "false" ] }, { "ans": [ "The flaps are extended, and 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": "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 or 2 when NLG down locked)", "true" ] } ], "ref": "Ref. AMM 33-46-00-00 CONF 00" }, { "ch": "The logo lights illuminate when:", "ansGr": [ { "ans": [ "The NAV and LOGO light switch is in position 1 or 2", "false" ] }, { "ans": [ "The NAV and LOGO light switch is in position 1 or 2 and flap extend or ground signal take from LGCIU 1", "false" ] }, { "ans": [ "The NAV and LOGO light switch is in position 1 or 2 and flap extend or ground signal take from LGCIU 2", "true" ] } ], "ref": "Ref. AMM 33-47-00-00 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": [ "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": "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": "Position of ADMs in relation with pitot and static probes:", "ansGr": [ { "ans": [ "Near and above the level of the probes for self-draining when aircraft on ground.", "true" ] }, { "ans": [ "Above the level of pitot probes and below the level of static probes.", "false" ] }, { "ans": [ "Always below the level of relating probes.", "false" ] } ], "ref": "Ref. AMM 34-11-00-00 CONF 00" }, { "ch": "Which information is computed by ADR?", "ansGr": [ { "ans": [ "ATT, CAS, M, SAT/TAT", "false" ] }, { "ans": [ "ALT, CAS, M", "false" ] }, { "ans": [ "ALT, CAS/TAS, M, Baro V/S, SAT/TAT", "true" ] } ], "ref": "Ref. AMM 34-13-00-00 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 transmitting or receiving", "false" ] } ], "ref": "Ref. AMM 34-36-00-00 CONF 00" }, { "ch": "On installation of ATC, TCAS, RA, DME antennas, the electrical bonding of antenna is made:", "ansGr": [ { "ans": [ "Through the attachment screws.", "true" ] }, { "ans": [ "Through a bonding cable.", "false" ] }, { "ans": [ "No bonding is required for antennas.", "false" ] } ], "ref": "Ref. AMM 34-42/43/51/52-11-400-801" }, { "ch": "A second qualified CRS is required to do a visual inspection of the quick disconnect coupling connection when replacing:", "ansGr": [ { "ans": [ "More than 1 pitot probe, pitot probe 3 or ADM.", "true" ] }, { "ans": [ "The pitot and static probe system 1or 2.", "false" ] }, { "ans": [ "More than 1 static probe.", "false" ] } ], "ref": "Ref. AMM 34-11-15/17-400-801" }, { "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": "The ATC/TCAS Control Unit control the:", "ansGr": [ { "ans": [ "ATC transponders and TCAS computer directly.", "false" ] }, { "ans": [ "ATC transponders directly and the TCAS computer through the ATC transponders.", "true" ] }, { "ans": [ "TCAS computer directly and the ATC transponders through the TCAS computer.", "false" ] } ], "ref": "Ref. Airbus TTM ATA 34 Page 124" }, { "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": "What is TRUE regarding Marker beacon system", "ansGr": [ { "ans": [ "Marker beacon system has its own receiver", "false" ] }, { "ans": [ "There is only one Marker beacon system whose receiver is a part of VOR/MRK receiver 1 active.", "true" ] }, { "ans": [ "There is only one Marker beacon system whose receiver is a part of VOR/MRK receiver 2 active.", "false" ] } ], "ref": "Ref. to AMM 34-55-00-00 CONF 00" }, { "ch": "If MSG “NAV LS TUNING DISAGREE” is shown on UPPER ECAM, what is the first action that should be done?", "ansGr": [ { "ans": [ "Do a reset MMR1 then MMR2", "false" ] }, { "ans": [ "Do a reset FCDC1 then FCDC2.", "false" ] }, { "ans": [ "Do the LAND CAT III Capability test.", "true" ] } ], "ref": "Ref. TSM 34-36-00-810-895-A" }, { "ch": "No Weather Radar image on NDs, what circumstance should be reviewed first before doing the test of Weather Radar?", "ansGr": [ { "ans": [ "Type of ND DU (CRT or LCD)", "false" ] }, { "ans": [ "Fault of Avionic Ventilation system", "true" ] }, { "ans": [ "Fault of Weather Radar transceiver.", "false" ] } ], "ref": "Ref. TSM 34-41-00-810-847-A" }, { "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": "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": "What is displayed on PFD if the inertial V/S is not available?", "ansGr": [ { "ans": [ "A red V/S flag comes on", "false" ] }, { "ans": [ "The Baro V/S data from ADR", "false" ] }, { "ans": [ "Automatic replace by Baro V/S.", "true" ] } ], "ref": "Ref. AMM 34-13-00-00 CONF 03" }, { "ch": "An altitude discrepancy between two PFDs is detected by:", "ansGr": [ { "ans": [ "DMCs", "false" ] }, { "ans": [ "ADIRS", "false" ] }, { "ans": [ "FWCs", "true" ] } ], "ref": "Ref. AMM 34-13-00-00 CONF 03" }, { "ch": "The DME and ATC antennas are identical and:", "ansGr": [ { "ans": [ "Interchangeable", "true" ] }, { "ans": [ "Switchable", "false" ] }, { "ans": [ "Not interchangeable", "false" ] } ], "ref": "Ref. IPC 34-51/52-11-01" }, { "ch": "When A/C on ground and the ATC mode selector is in AUTO position:", "ansGr": [ { "ans": [ "Selected ATC transponder operates with all its functions", "false" ] }, { "ans": [ "Selected ATC transponder does not operate", "false" ] }, { "ans": [ "The selected transponder operates only mode S", "true" ] } ], "ref": "Ref. AMM 34-52-00-00 CONF 00" }, { "ch": "The message “GPS PRIMARY” is displayed:", "ansGr": [ { "ans": [ "At the bottom of the image in all the ND modes (except engine standby modes) when the GPS is not used for navigation", "false" ] }, { "ans": [ "At the bottom of the image in all the ND modes (except engine standby modes) when the GPS becomes primary", "true" ] }, { "ans": [ "At the bottom of the image in all the ND modes (except engine standby modes) when the GPS approach is selected in the flight plan", "false" ] } ], "ref": "Ref AMM 34-36-00-00 CONF 01" }, { "ch": "Residual ground speed can be checked on:", "ansGr": [ { "ans": [ "PFDs or MCDU", "false" ] }, { "ans": [ "NDs or MCDU", "true" ] }, { "ans": [ "PFDs or NDs.", "false" ] } ], "ref": "Ref TSM 34-10-00-810-984" }, { "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": "Message CHECK HDG detected by which computer?", "ansGr": [ { "ans": [ "SDACs", "false" ] }, { "ans": [ "FWCs", "true" ] }, { "ans": [ "ADIRUs", "false" ] } ], "ref": "Ref. AMM 34-14-00-00 CONF 03" }, { "ch": "Message CHECK ATT detected by which computer?", "ansGr": [ { "ans": [ "SDACs", "false" ] }, { "ans": [ "FWCs", "true" ] }, { "ans": [ "ADIRUs", "false" ] } ], "ref": "Ref. AMM 34-14-00-00 CONF 03" }, { "ch": "In which EFIS modes on ND are TCAS targets displayed?", "ansGr": [ { "ans": [ "All modes", "false" ] }, { "ans": [ "All ROSE modes or ARC mode.", "true" ] }, { "ans": [ "All ROSE modes except ROSE LS, and ARC mode.", "false" ] } ], "ref": "Ref. AMM 34-43-10-00 CONF 00" }, { "ch": "If the Terrain Awareness Display (TAD) function of the EGPWS generates a caution/warning message with the TERR ON ND selected OFF, which of the following statements is correct?", "ansGr": [ { "ans": [ "An aural \"Terrain Ahead, Pull Up\" will be heard and you should select the TERR ON ND pushbutton ON unless the weather display is required", "false" ] }, { "ans": [ "Terrain is automatically displayed on the ND and the ON light of the TERR ON ND pushbutton comes on.", "true" ] }, { "ans": [ "With the TERR ON ND pushbutton selected OFF, the terrain function of the EGPWS is inhibited.", "false" ] } ], "ref": "Ref. AMM 34-72-20-00 CONF 00" }, { "ch": "Which statement is correct regarding the Predictive Windshear system aural alerts?", "ansGr": [ { "ans": [ "They are inhibited by TCAS, GPWS and other FWC aural alerts.", "false" ] }, { "ans": [ "They are inhibited by windshear detected by FMGEC and stall warning aural messages.", "true" ] }, { "ans": [ "They have priority over windshear detected by FMGC and stall warning aural messages", "false" ] } ], "ref": "Ref. AMM 34-72-00-00 CONF 00" }, { "ch": "What will be displayed on the ND when the weather radar is ON, and the TERR ON ND switch is also ON?", "ansGr": [ { "ans": [ "Weather Radar information.", "false" ] }, { "ans": [ "Terrain information.", "true" ] }, { "ans": [ "Both weather and terrain information", "false" ] } ], "ref": "Ref. Airbus TTM ATA 34 Page 85" }, { "ch": "What actions are required if after a 3-hour flight the POSITION MONITOR page indicates that the Radial Position Error for a particular IRS is 18 nm?", "ansGr": [ { "ans": [ "No action is required unless GS > 15 kt", "false" ] }, { "ans": [ "The Aircraft can be dispatched if it is the first time and an entry is recorded in the Maintenance Log identifying the associated IRS.", "false" ] }, { "ans": [ "The ADIRU must be replaced.", "true" ] } ], "ref": "Ref TSM 34-10-00-810-994" }, { "ch": "In order to access BACKUP NAV mode on the MCDU MENU, it is necessary to have the FM source selected switch in position:", "ansGr": [ { "ans": [ "BOTH ON 1", "false" ] }, { "ans": [ "BOTH ON 2", "false" ] }, { "ans": [ "NORM position", "true" ] } ], "ref": "Ref AMM 22-70-00-00 CONF 01" }, { "ch": "Barometric settings to the ADIRU's are made:", "ansGr": [ { "ans": [ "On the Barometric setting knobs on the FCU", "true" ] }, { "ans": [ "Via the MCDU", "false" ] }, { "ans": [ "On the ADIRS switching panel", "false" ] } ], "ref": "Ref. Airbus TTM ATA 34 Page 4 and 46" }, { "ch": "VOR data can be displayed on:", "ansGr": [ { "ans": [ "Both NDs", "true" ] }, { "ans": [ "Both PFDs", "false" ] }, { "ans": [ "Both PFDs and NDs", "false" ] } ], "ref": "Ref AMM 34-55-00-00 CONF 00" }, { "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": "The AOA sensor provides:", "ansGr": [ { "ans": [ "A single signal to the Air Data Inertial Reference Unit (ADIRU) and receives a self-test signal from it", "false" ] }, { "ans": [ "Two independent signals through two independent sensing elements", "false" ] }, { "ans": [ "A primary and a backup signal to each ADIRU", "true" ] } ], "ref": "Ref. Airbus TTM ATA 34 Page 12" }, { "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": [ "The 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 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 VHFs system and carry out maintenance on VHFs 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": "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 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 1 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": "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 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 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 300 psi. 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 high-pressure oxygen cylinder and continuous-flow oxygen masks with 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 (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": [ "  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 always ensure 200°C outlet air", "false" ] }, { "ans": [ "To always ensure 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 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" } ]