[ { "ch": "What is the correct statement regarding A/C steering angle? (A)", "ansGr": [ { "ans": [ "We need to do inspection of the NLG after the steering angle is more than 95 degrees", "true" ] }, { "ans": [ "We need to do inspection of the NLG and MLG after the steering angle is more than 95 degrees", "false" ] }, { "ans": [ "It is necessary to supply Airbus with this data to get confirmation before the subsequent flight", "false" ] } ], "part": "ATA 05: TIME LIMIT", "ref": "Ref AMM 05-51-23-200-801-A" }, { "ch": "How many major zones on the A/C? (A)", "ansGr": [ { "ans": [ "6", "false" ] }, { "ans": [ "7", "false" ] }, { "ans": [ "8", "true" ] } ], "part": "ATA 06: DIMENSION AND AREAS", "ref": "Ref AMM 06-20-00 PB001" }, { "ch": "Station number is: (A, B1, B2)", "ansGr": [ { "ans": [ "The distance in millimeters of a cross section from the reference X datum", "true" ] }, { "ans": [ "The distance in millimeters of a cross section from the relating A/C axis", "false" ] }, { "ans": [ "The distance in inches of a cross section from the reference X datum", "false" ] } ], "ref": "Ref AMM 06-31-53 PB001" }, { "ch": "X datum (station 0) is located at: (A, B1, B2)", "ansGr": [ { "ans": [ "6382 millimeters from the Forward of A/C nose", "true" ] }, { "ans": [ "100 in (254cm) forward of aircraft nose", "false" ] }, { "ans": [ "The point of A/C nose", "false" ] } ], "ref": "Ref AMM 06-31-53 PB001" }, { "ch": "Access doors and panels are identified by: (A, B1, B2)", "ansGr": [ { "ans": [ "The number of the zone in which the panel is located followed by a two-letter suffix", "true" ] }, { "ans": [ "The number of the zone in which the panel is located followed by one letter suffix", "false" ] }, { "ans": [ "Two-letter followed by the number of the zone in which the panel is located", "false" ] } ], "ref": "Ref AMM 06-40-00 PB001" }, { "ch": "A/C area are divided in Zone base on: (A, B1, B2)", "ansGr": [ { "ans": [ "Major zones, major sub-zones, unit zones", "true" ] }, { "ans": [ "Major zones, major sub-zones", "false" ] }, { "ans": [ "Major zones, major sub-zones, unit zones and a two-letter suffix", "false" ] } ], "ref": "Ref AMM 06-20-00 PB001" }, { "ch": "What is Aircraft maintenance configuration before you lift the aircraft: (A, B1, B2)", "ansGr": [ { "ans": [ "Remove the wheel chocks if they are in position, set the parking brake OFF", "true" ] }, { "ans": [ "Install the wheel chocks, set the parking brake OFF", "false" ] }, { "ans": [ "We can do a loading/unloading or a fueling operation during lifting procedure", "false" ] } ], "part": "ATA 07-08: LIFTING, SHORING, LEVELING AND WEIGHING", "ref": "Ref AMM 07-11-00-581-801-A" }, { "ch": "Before you lift the aircraft make sure that: (A, B1, B2)", "ansGr": [ { "ans": [ "Passenger/crew doors, the emergency exits and the cargo doors are closed and locked or fully open and locked", "true" ] }, { "ans": [ "Passenger/crew doors, the emergency exits doors are closed and locked. Cargo doors must be closed and locked", "false" ] }, { "ans": [ "Passenger/crew doors, the emergency exits and the cargo doors are closed and locked", "false" ] } ], "ref": "Ref AMM 07-11-00-581-801-A" }, { "ch": "Aircraft maintenance configuration before you lower the aircraft: (A, B1, B2)", "ansGr": [ { "ans": [ "Landing gear lever is set to DOWN", "false" ] }, { "ans": [ "Ground lock pins are in position on the main landing gear and the nose landing gear  ", "false" ] }, { "ans": [ "Ground lock pins are in position on the main landing gear and the nose landing gear, Landing gear lever is set to DOWN, parking brake OFF", "true" ] } ], "ref": "Ref AMM 07-11-00-586-801-A" }, { "ch": "How many points are designated for lifting the aircraft for maintenance operations? (A, B1, B2)", "ansGr": [ { "ans": [ "One in the front and one under each wing", "true" ] }, { "ans": [ "One in the front, one in the rear and one under each wing", "false" ] }, { "ans": [ "One in the front, one under each MLG", "false" ] } ], "ref": "Ref AMM 07-11-00-581-801-A" }, { "ch": "Can tail safety stay be used to lift the aircraft: (A, B1, B2)", "ansGr": [ { "ans": [ "No", "true" ] }, { "ans": [ "Yes, if only with empty A/C", "false" ] }, { "ans": [ "Yes, if only with A/C is empty and in hangar", "false" ] } ], "ref": "Ref AMM 07-11-00-581-801-A" }, { "ch": "The tail safety stay is used to: (A, B1, B2)", "ansGr": [ { "ans": [ "Share load with the main jacks during jacking process", "false" ] }, { "ans": [ "Keep the aircraft stable during landing gear retraction/ extension test", "false" ] }, { "ans": [ "Keep the aircraft stable on jacks during the maintenance", "true" ] } ], "ref": "Ref AMM 07-11-00-581-801-A" }, { "ch": "The main purpose of weighing A/C is: (A, B1, B2)", "ansGr": [ { "ans": [ "Find the operating empty weight of the aircraft and to calculate the center of gravity", "true" ] }, { "ans": [ "To find the zero fuel weight", "false" ] }, { "ans": [ "Know the aircraft weight for passenger loading", "false" ] } ], "ref": "Ref AMM 08-10-00-200-801-A" }, { "ch": "When weighing the A/C to find the operating empty weight of the A/C: (A, B1, B2)", "ansGr": [ { "ans": [ "All the fire extinguishers, oxygen masks and safety belts must be removed", "false" ] }, { "ans": [ "Engine, APU, IDG oil must be checked and refilled to necessary level", "false" ] }, { "ans": [ "Engine, APU, HYD, IDG oil must be checked and refilled to necessary level", "true" ] } ], "ref": "Ref: AMM 08-10-00-200-801-A" }, { "ch": "Configuration for A/C weighing to find the operating empty weight: (A, B1, B2)", "ansGr": [ { "ans": [ "All tools and protection devices on the aircraft must be removed", "true" ] }, { "ans": [ "Empty all of Engine, APU, IDG oil", "false" ] }, { "ans": [ "Empty all of Engine, APU, HYD, IDG oil and drain fuel, water, waste tanks", "false" ] } ], "ref": "Ref: AMM 08-10-00-200-801-A" }, { "ch": "For A/C quick leveling you can use: (A, B1, B2)", "ansGr": [ { "ans": [ "A Spirit Level in the Passenger Compartment", "false" ] }, { "ans": [ "A Spirit Level in the FWD Cargo Compartment", "false" ] }, { "ans": [ "We can use any of ADIRU or spirit level in Fwd Cargo or Pax Compartment", "true" ] } ], "ref": "Ref AMM 08-21-00-200-801-A" }, { "ch": "Jacking for wheel change: (A, B1, B2)", "ansGr": [ { "ans": [ "Set the parking-brake selector switch to OFF", "false" ] }, { "ans": [ "Make sure that the CHOCK - WHEEL(S) are in position at the NLG and at the MLG (on the opposite side)", "false" ] }, { "ans": [ "Make sure that the aircraft is stable; CHOCK - WHEEL(S) are in position and parking brake OFF", "true" ] } ], "ref": "Ref AMM 07-12-00-582-802-A" }, { "ch": "Prior to towing, which statement is most correct: (A)", "ansGr": [ { "ans": [ "Do not pressurize the Blue hydraulic system if you energized the aircraft electrical circuits with the engine", "false" ] }, { "ans": [ "Make sure that the pointer of the top gauge (ACCU PRESS) is correct, must be in the green range 3000 psi", "true" ] }, { "ans": [ "Make sure that the left and right brake pressures are ON( The left and right hydraulic pressure indicators show approximately 2500psi)", "false" ] } ], "part": "ATA 09: TOWING AND TAXIING", "ref": "(Ref: AMM 09-10-00-584-802-A)" }, { "ch": "The maximum towing angle on each side of the aircraft centerline must not be more than: (A)", "ansGr": [ { "ans": [ "65 deg", "true" ] }, { "ans": [ "90 deg", "false" ] }, { "ans": [ "93 deg", "false" ] } ] }, { "ch": "How to check the towing angle limits: (A)", "ansGr": [ { "ans": [ "By visual inspection during towing operation", "false" ] }, { "ans": [ "The limits are shown by painted marks on the NLG aft doors.", "true" ] }, { "ans": [ "The towing angle exceeding limit is indicated by a red light on the nose gear", "false" ] } ], "ref": "(Ref: AMM 09-10-00-584-802-A)" }, { "ch": "Before towing, aircraft stability check is required: (A)", "ansGr": [ { "ans": [ "In wind condition", "true" ] }, { "ans": [ "Aircraft stability check is unnecessary", "false" ] }, { "ans": [ "Only in-flight operation towing condition", "false" ] } ], "ref": "(Ref: AMM 09-10-00-584-802-A)" }, { "ch": "During towing/taxing operations, the seatbelt must be fastened for/in: (A)", "ansGr": [ { "ans": [ "Everybody aboard", "false" ] }, { "ans": [ "Low speed operations", "false" ] }, { "ans": [ "Each person on the A/C is in seat and seatbelt is fastened, including low speed operations", "true" ] } ], "ref": "(Ref: AMM 09-10-00-584-802)" }, { "ch": "Installation of the landing gear safety devices is: (A)", "ansGr": [ { "ans": [ "Mandatory when you tow the aircraft to the base", "false" ] }, { "ans": [ "Mandatory when you tow the aircraft during flight operations", "false" ] }, { "ans": [ "Make sure that the safety devices are installed on the landing gears, otherwise when you tow or push the aircraft during flight operations are optional", "true" ] } ], "ref": "(Ref: AMM 09-10-00-584-802-A)" }, { "ch": "What is the correct statement: (A)", "ansGr": [ { "ans": [ "Make sure that the dimension \"H\" of the NLG is never less than 310 mm (12.2047 in.) when you tow/or push the aircraft", "false" ] }, { "ans": [ "Make sure that the dimension \"H\" of the Nose Landing Gear (NLG) is not more than 310 mm (12.20 in.)", "true" ] }, { "ans": [ "Make sure that the dimension \"H\" of the Nose Landing Gear (NLG) is not more than 300 mm (12.20 in.)", "false" ] } ], "ref": "(Ref: AMM 09-10-00-584-802)" }, { "ch": "Towing with the engine cowls opened: (A)", "ansGr": [ { "ans": [ "Is allowed only with low-speed operations", "false" ] }, { "ans": [ "Is not allowed with high-speed operations", "false" ] }, { "ans": [ "Is not allowed", "true" ] } ], "ref": "(Ref: AMM 09-10-00-584-802)" }, { "ch": "Which statement is correct? (A)", "ansGr": [ { "ans": [ "It is optional to install the landing-gear safety devices when you tow or push the aircraft during flight operations", "true" ] }, { "ans": [ "You must always install the landing-gear safety devices when you tow or push the aircraft", "false" ] }, { "ans": [ "It is mandatory to install the landing-gear safety devices when you tow or push the aircraft during high-speed operations", "false" ] } ], "ref": "(Ref: AMM 09-10-00-584-802)" }, { "ch": "During preparation for towing with towbarless tractor, you? (A)", "ansGr": [ { "ans": [ "Inform cockpit crew to release the parking brake when tractor has engaged to the NLG", "false" ] }, { "ans": [ "Inform cockpit crew to release the parking brake when tractor has lifted the NLG up", "false" ] }, { "ans": [ "Put the TRACTOR TOWBARLESS in position, lock and lift the NLG. Then, remove the MLG CHOCK - WHEEL(S) and inform cockpit crew set PARK BRK to OFF", "true" ] } ], "ref": "(Ref: AMM 09-10-00-584-814)" }, { "ch": "What indication on ECAM do you have to check prior to start towing? (A)", "ansGr": [ { "ans": [ "N/W STEER DISC", "true" ] }, { "ans": [ "N/W STEER INOP", "false" ] }, { "ans": [ "N/W STEER DISC and ANTI SKID/NWS OFF", "false" ] } ], "ref": "Ref AMM 09-10-00 PB201" }, { "ch": "What is the difference step between towing using tow bar and towbarless tractor? (A)", "ansGr": [ { "ans": [ "Deactivate of the NWS system", "false" ] }, { "ans": [ "Sequence of removing chocks", "true" ] }, { "ans": [ "Using towbarless tractor can go with higher speed", "false" ] } ], "ref": "Ref AMM 09-10-00 PB201" }, { "ch": "In towing configuration, the safety pin locks the control lever on the control box at: (A, B1, B2)", "ansGr": [ { "ans": [ "Disengaged position", "true" ] }, { "ans": [ "Normal position", "false" ] }, { "ans": [ "Stowed position", "false" ] } ], "ref": "Ref AMM 09-10-00 PB201" }, { "ch": "In the cockpit, how do you know that the parking brake is released before towing sequence? (A, B1, B2)", "ansGr": [ { "ans": [ "Check Parking brake selector in OFF, brake pressure indication on ECAM is at 0 and confirm with GND personnel", "false" ] }, { "ans": [ "Check Parking brake selector in OFF; brake pressure pointes at 0 and confirm with GND personnel", "true" ] }, { "ans": [ "Check electrical control box, paring brake light go off", "false" ] } ], "ref": "Ref AMM 09-10-00 PB201" }, { "ch": "If no APU and EXT PWR are available, what refuel method is possible? (A)", "ansGr": [ { "ans": [ "By Manual override refuel.", "false" ] }, { "ans": [ "Refuel as normal using the battery.", "false" ] }, { "ans": [ "Refuel as normal using the battery or by Manual override refuel.", "true" ] } ], "part": "ATA 12: SERVICING", "ref": "Ref AMM 12-11-38 PB301" }, { "ch": "How do you do the MMI measurement? (A)", "ansGr": [ { "ans": [ "Only use one MLI reading for each applicable tank.", "true" ] }, { "ans": [ "Use the average value of all MLI for each applicable tank.", "false" ] }, { "ans": [ "Use the average value of all MLI that can give indication for each applicable tank.", "false" ] } ], "ref": "Ref AMM 12-11-28-650-806" }, { "ch": "To reduce refuel time, can you use 04 refuel hoses at the same time? (A)", "ansGr": [ { "ans": [ "Yes, at each coupling is not more than 50 psi.", "true" ] }, { "ans": [ "Yes, as long as pressure at left side is 10 psi more than on the right one.", "false" ] }, { "ans": [ "No, you are not allowed.", "false" ] } ], "ref": "Ref AMM 12-11-38 PB301" }, { "ch": "You push (in) and hold the HI LEVEL TEST to? (A, B1, B2)", "ansGr": [ { "ans": [ "Test the HI level protection function.", "false" ] }, { "ans": [ "Test the lights and indication and Overflow protection function.", "false" ] }, { "ans": [ "All the HI level protection function, Overflow protection function, lights and indication are tested.", "true" ] } ], "ref": "Ref AMM 12-11-28-650-804" }, { "ch": "What is the indication that preselected refuel operation has completed? (A)", "ansGr": [ { "ans": [ "END light flashing.", "false" ] }, { "ans": [ "PRESELECTED value disappeared.", "false" ] }, { "ans": [ "END light comes on and does not flash.", "true" ] } ], "ref": "Ref AMM12-11-28 PB301" }, { "ch": "What test must do before MANUAL refuel? (A, B1, B2)", "ansGr": [ { "ans": [ "Light test; Overflow test.", "false" ] }, { "ans": [ "HI LEVEL test.", "false" ] }, { "ans": [ "Light test; Overflow test and HI LEVEL test.", "true" ] } ], "ref": "Ref AMM 12-11-28-650-804" }, { "ch": "How is the MANUAL refueling operation stopped? (A)", "ansGr": [ { "ans": [ "Automatically after the END light comes ON.", "false" ] }, { "ans": [ "Manually by selecting the refuel valves to SHUT.", "false" ] }, { "ans": [ "Manually by selecting the refuel valves to NORM.", "true" ] } ], "ref": "Ref AMM 12-11-28-650-80" }, { "ch": "For manual refuel. (A, B1, B2)", "ansGr": [ { "ans": [ "Always refer to Refuel Distribution Graph.", "true" ] }, { "ans": [ "Always fill the outer tanks first.", "false" ] }, { "ans": [ "You can never fill the trim tank.", "false" ] } ], "ref": "Ref AMM 12-11-28-650-804" }, { "ch": "What happen if you attempt to refuel with the T TK FEED switch on the FUEL panel 245VU set to ISOL? (A, B1, B2)", "ansGr": [ { "ans": [ "Fuel will go to trim tank.", "false" ] }, { "ans": [ "Automatic refuel progress cannot be started.", "true" ] }, { "ans": [ "Trim tank forward transfer will start.", "false" ] } ], "ref": "Ref AMM 12-11-28-650-803" }, { "ch": "What needs to be inspected on the IDG during regular inspection? (A)", "ansGr": [ { "ans": [ "Oil level must always stay in Green area, pop out pin and reset ring are not protruding.", "false" ] }, { "ans": [ "Oil level is not in the red area and pop out pin is not protruding.", "false" ] }, { "ans": [ "Oil level is correct, depend on engine is hot or cold, and pop out pin is not protruding.", "true" ] } ], "ref": "Ref AMM 24-21-00-210-820, AMM 12-13-24-610-801" }, { "ch": "What conditions are NOT necessary when you check Nitrogen Pressure on Alternate Parking Brake Accumulators? (A)", "ansGr": [ { "ans": [ "Release the pressure from the parking brake system using depressurization lever.", "false" ] }, { "ans": [ "Blue system depressurized and waited until temperature of the gas become stable.", "false" ] }, { "ans": [ "Set the PARK BRK selector switch to the ON position.", "true" ] } ], "ref": "Ref AMM 32-40-00-210-805" }, { "ch": "What needs to be observed during normal IDG oil servicing? (A)", "ansGr": [ { "ans": [ "Stop filling the IDG when oil level reaches green band.", "false" ] }, { "ans": [ "Stop filling the IDG when oil level at yellow band.", "false" ] }, { "ans": [ "Stop filling the IDG when about 0.95 l of oil has overflown.", "true" ] } ], "ref": "Ref AMM 12-13-24-612-807" }, { "ch": "Regarding IDG normal servicing procedure, you close the drain port and complete the task? (A)", "ansGr": [ { "ans": [ "When you see approximately 0,95 l of oil drain out", "true" ] }, { "ans": [ "Right after you see the oil level reach green band", "false" ] }, { "ans": [ "When only drops of oil come out of the overflow drain hose", "false" ] } ], "ref": "Ref AMM 12-13-24-612-807" }, { "ch": "How to inspect the engine starter for metallic debris? (A)", "ansGr": [ { "ans": [ "Take and inspect a sample of the starter fluid.", "false" ] }, { "ans": [ "Drain all the starter fluid to get access to the Magnetic Chip Detector.", "false" ] }, { "ans": [ "Remove the Magnetic Chip Detector for inspection without fluid drain.", "true" ] } ], "ref": "Ref AMM 12-13-80 PB301" }, { "ch": "What configuration of the aircraft to check HYD fluid levels? (A)", "ansGr": [ { "ans": [ "Cargo doors closed, Parking brake ON with brake Accumulator sufficiently charged", "true" ] }, { "ans": [ "Cargo doors closed, Parking brake OFF, brake Accumulator sufficiently charged", "false" ] }, { "ans": [ "Cargo doors open, Slat/Flap extended", "false" ] } ], "ref": "Ref AMM 29-31-00-200-801" }, { "ch": "Where can you check the HYD fluid levels? (A)", "ansGr": [ { "ans": [ "On ECAM HYD page or from HYD Ground service panel if electrical network energized", "false" ] }, { "ans": [ "At each reservoir direct reading gauge", "false" ] }, { "ans": [ "At each reservoir direct reading gauge or On ECAM HYD page/ HYD Ground service panel with electrical network energized.", "true" ] } ], "ref": "Ref AMM 29-31-00-200-801" }, { "ch": "Engine Starter oil gravity replenishment completed when? (A)", "ansGr": [ { "ans": [ "Oil comes out at drain port or overflow port.", "false" ] }, { "ans": [ "Oil level reach the 3/4 mark on the sign glass.", "false" ] }, { "ans": [ "Oil flows out at fill port.", "true" ] } ], "ref": "Ref AMM 12-13-80-612-802" }, { "ch": "Before doing the hydraulic fluid reservoir filling? (A)", "ansGr": [ { "ans": [ "The related reservoirs air pressurize system must be depressurized.", "false" ] }, { "ans": [ "Check that no related RSVR LO AIR PR message on ECAM.", "true" ] }, { "ans": [ "Check that no related SYS LO PR message on ECAM.", "false" ] } ], "ref": "Ref AMM 12-12-29 PB301" }, { "ch": "HP pneumatic GND cart can be used for? (A, B1, B2)", "ansGr": [ { "ans": [ "Start the Engine, pressurize the water system and hydraulic RSVR and ACC.", "false" ] }, { "ans": [ "Running the packs if APU bleed and LP GND cart are not available.", "true" ] }, { "ans": [ "Eng anti ice testing and pressurize the HYD ACCU", "false" ] } ], "ref": "Ref AMM 12-33-21-618-801- 01" }, { "ch": "Is it allowed to simultaneously supply Pack and LP GROUND cart during long stops in a hot airfield? (A, B1, B2)", "ansGr": [ { "ans": [ "Yes, if only one pack supplies.", "false" ] }, { "ans": [ "No, system damage may result.", "true" ] }, { "ans": [ "No, it is not possible.", "false" ] } ], "ref": "Ref AMM 12-33-21-618-801" }, { "ch": "Regarding air pressurizing of Hydraulic Reservoir, what statement is correct? (A)", "ansGr": [ { "ans": [ "You normally pressurize one system reservoir at a time.", "false" ] }, { "ans": [ "Reservoir ground pressurizing port can be found at any hydraulic system servicing panel", "false" ] }, { "ans": [ "You may pressurize all three Hyd system reservoirs at the same time.", "true" ] } ], "ref": "Ref AMM 29-14-00 PB201" }, { "ch": "Regarding air pressurizing of Hydraulic Reservoir, what statement is correct? (A)", "ansGr": [ { "ans": [ "You stop fill the reservoir with air until 50 psi is shown on the reservoir pressure gages", "true" ] }, { "ans": [ "Reservoir ground pressurizing connector can be found at any hydraulic system servicing panel", "false" ] }, { "ans": [ "Reservoir air pressure will automatically be depressurized after all engines and APU shut down", "false" ] } ], "ref": "Ref AMM 29-14-00 PB201" }, { "ch": "Regarding Depressurization of the Hydraulic Reservoirs: (A)", "ansGr": [ { "ans": [ "You depressurize all system reservoir at the same time", "false" ] }, { "ans": [ "You depressurize the Hydraulic Reservoir before filling with fluid", "false" ] }, { "ans": [ "You can only depressurize each Hydraulic system reservoir at a time.", "true" ] } ], "ref": "Ref AMM 29-14-00 PB201" }, { "ch": "What are the Special Precautions to apply Insecticide Agent in Cargo Compartments during Turn-Around? (A, B1, B2)", "ansGr": [ { "ans": [ "Smoke warning may occur", "true" ] }, { "ans": [ "Cargo Ventilation controller must be selected OFF before applying insecticide agent", "false" ] }, { "ans": [ "Recirculation system must be OFF before applying insecticide agent", "false" ] } ], "ref": "Ref AMM 12-21-12-670-805" }, { "ch": "In the AMM tasks, “CAUTION” is meant: (A, B1, B2)", "ansGr": [ { "ans": [ "Calls attention to use of materials, processes, methods, procedures or limits which must be followed precisely to avoid injury of death to persons", "false" ] }, { "ans": [ "Calls attention to methods and procedures which be followed to avoid damage to equipment", "true" ] }, { "ans": [ "Calls attention to methods which make the job easier or provide supplementary or explanatory information", "false" ] } ], "part": "ATA 20: STANDARD PRACTICES & DOCUMENTATION", "ref": "Ref: ESPM/ introduction/ 3. Definitions" }, { "ch": "AMM gives: (A, B1, B2)", "ansGr": [ { "ans": [ "Information required for trouble shooting is contained in the manual", "false" ] }, { "ans": [ "The information required to service, repair, replace, adjust, inspect and check equipment’s and systems of the A/C normally performed on the ramp or in the maintenance hangar", "true" ] }, { "ans": [ "Schematic diagrams of the electrical installation with sufficient data for A/C fault isolation", "false" ] } ], "ref": "Ref: ESPM/ introduction/ interfaces with other manuals" }, { "ch": "Removal/Installation of O-rings on Straight plug-in of hydraulic system Components:(A)", "ansGr": [ { "ans": [ "You can use pointed/sharp or metal tools to remove the O-ring.", "false" ] }, { "ans": [ "Put the O-ring fully into Phosphate Ester hydraulic fluid for a maximum of 15 minutes before installing.", "true" ] }, { "ans": [ "You can re-use the O-rings when you checked it in good condition", "false" ] } ], "ref": "Ref: AMM 20-29-00-911-801" }, { "ch": "Tightening Torques for Standard Threaded Fasteners: (A, B1, B2)", "ansGr": [ { "ans": [ "Recommends that you use a torque wrench that has a torque value in the range of 30% to 80% of the full range.", "true" ] }, { "ans": [ "You can use a torque wrench to loosen a fastener.", "false" ] }, { "ans": [ "You use a self-locking nut and self-sealing nut again.", "false" ] } ], "ref": "Ref: AMM 20-21-11-911-801" }, { "ch": "Safetying with Lockwire: (A)", "ansGr": [ { "ans": [ "The lockwire is installed to put tension on the wire when the parts become loose.", "true" ] }, { "ans": [ "It is permitted to use a lockwire to lock the control cable turnbuckles.", "false" ] }, { "ans": [ "The length of this twisted part (pigtail) must be 35 mm maximum.", "false" ] } ], "ref": "Ref: AMM 20-11-11-911-803" }, { "ch": "Safetying with a Cotter Pin:(A)", "ansGr": [ { "ans": [ "It is permitted to use cotter pins more than one time.", "false" ] }, { "ans": [ "For the castellated nuts or the slotted nuts, adjust the torque value (between the minimum/maximum values) to align the castellations or the slots is permitted.", "true" ] }, { "ans": [ "You can only engage the cotter pin in the hole with the plane of its head perpendicular to the bolt/screw axis.", "false" ] } ], "ref": "Ref: 20-11-11-911-805" }, { "ch": "Handling Precautions for Electrostatic Discharge Sensitive Devices: (A, B1, B2)", "ansGr": [ { "ans": [ "It is not necessary to prevent electrostatic discharge damage, because of the A/C components have sufficient built-in protection.", "false" ] }, { "ans": [ "It is necessary to wear wrist straps for the Installation/replacement of OBRMs.", "true" ] }, { "ans": [ "We must wear wrist straps while replacing the LRUs.", "false" ] } ], "ref": "Ref: AMM 20-15-00-912-801" }, { "ch": "During maintenance in Storm Conditions: (A)", "ansGr": [ { "ans": [ "You can do ground servicing operations external to the aircraft (refueling...) with A/C and Tanker are bonded and the A/C is grounded.", "false" ] }, { "ans": [ "Not touch metal parts, equipment or connections to the aircraft.", "true" ] }, { "ans": [ "We can do connecting headset communication if the A/C is grounded.", "false" ] } ], "ref": "Ref: AMM 20-17-00-910-801" }, { "ch": "Why must we do the paint marking line after Standard or Specific tightening torque application? (A, B1, B2)", "ansGr": [ { "ans": [ "To identify a tightened union.", "false" ] }, { "ans": [ "To show the loosened union.", "false" ] }, { "ans": [ "To identify a tightened union and may show the possible loosened union during inspection.", "true" ] } ], "ref": "Ref: AMM 20-23-22-910-801" }, { "ch": "Why do we need to do the bonding procedure during the installation of the equipment or the part assembly (access doors, fairings, antenna, fittings or pipes etc.)? (A, B1, B2)", "ansGr": [ { "ans": [ "To prevent lighting strikes.", "false" ] }, { "ans": [ "To make sure that there is an electrical continuity between electrically conductive parts (Two structural Parts or A system point and the structure).", "true" ] }, { "ans": [ "To make sure there is a low voltage between two conductive parts", "false" ] } ], "ref": "Ref: AMM 20-28-00-912-810" }, { "ch": "What is the function of each pack controller? (A)", "ansGr": [ { "ans": [ "To control the corresponding pack and the flow control valve", "true" ] }, { "ans": [ "To control the trim air valve", "false" ] }, { "ans": [ "To optimize the zone temperature selecting", "false" ] } ], "part": "ATA 21: AIR CONDITIONING", "ref": "Ref P20-22-ATA21-T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "How is pack outlet temperature regulated? (A)", "ansGr": [ { "ans": [ "By modulating the ram air doors along with bypass valve", "false" ] }, { "ans": [ "By modulating the ram air doors along with heat exchangers", "false" ] }, { "ans": [ "By modulating the ram air doors along with temperature control valve", "true" ] } ], "ref": "Ref P22-ATA21-T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "What are the controllers related to the temperature control system? (A)", "ansGr": [ { "ans": [ "Zone controller and pack controllers", "true" ] }, { "ans": [ "AEVC and Vent controller", "false" ] }, { "ans": [ "RPCU and zone controller", "false" ] } ], "ref": "Ref AMM 21-53-00-00 pb001" }, { "ch": "What is the function of the Trim Air Valves? (A)", "ansGr": [ { "ans": [ "To regulate the hot air pressure", "false" ] }, { "ans": [ "To optimize the zone temperature by adding hot air", "true" ] }, { "ans": [ "To modulate pack discharge temperature", "false" ] } ], "ref": "Ref P54-ATA21-T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "What is the main purpose of the anti-icing valve? (A, B1, B2)", "ansGr": [ { "ans": [ "Prevents ice formation across the primary heat exchanger", "false" ] }, { "ans": [ "Prevents ice formation across the pack condenser", "true" ] }, { "ans": [ "Condenses humidity of air into water particles", "false" ] } ], "ref": "Ref P34- ATA21-T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "What is the purpose of the reheater? (A, B1, B2)", "ansGr": [ { "ans": [ "To reheat the air leaving the turbine", "false" ] }, { "ans": [ "To revaporise the remaining water particles not extracted by the water extractor", "true" ] }, { "ans": [ "Prevents ice formation across the pack condenser", "false" ] } ], "ref": "Ref P22-24 - ATA21-T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "The turbo fan of the air conditioning bay: (A)", "ansGr": [ { "ans": [ "Operates as long as the A/C is energized", "false" ] }, { "ans": [ "Operates on ground only", "true" ] }, { "ans": [ "Operates on ground and in flight", "false" ] } ], "ref": "Ref P139 ATA21-T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "Which is the controller related to the Air Conditioning Bay ventilation system? (A)", "ansGr": [ { "ans": [ "AEVC", "true" ] }, { "ans": [ "Zone controller", "false" ] }, { "ans": [ "Pack controllers", "false" ] } ], "ref": "Ref P139 ATA21-T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "What is the function of EMER RAM AIR INLET?: (A)", "ansGr": [ { "ans": [ "During flight, if both packs fail. Or in case of smoke in the cabin, a ram air inlet may be opened allowing ambient air to enter the mixing unit.", "true" ] }, { "ans": [ "After the aircraft is making emergency landing on water", "false" ] }, { "ans": [ "Opens automatically when the DITCHING pushbutton is set to ON", "false" ] } ], "ref": "Ref P50 ATA21-T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "The purpose of the safety valves is to avoid: (A)", "ansGr": [ { "ans": [ "Excessive negative differential pressure", "false" ] }, { "ans": [ "Both excessive positive differential pressure and excessive negative differential pressure", "true" ] }, { "ans": [ "Of residual cabin pressure by automatically control the outflow valves fully open on ground", "false" ] } ], "ref": "Ref P110 ATA21-T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "Which statement is correct regarding illumination of the amber aft isolation valve ‘FAULT’ light? (A, B1, B2)", "ansGr": [ { "ans": [ "Automatically closes the aft cargo compartment isolation valves", "false" ] }, { "ans": [ "Means that either the inlet or outlet isolation valve(s) disagrees with the switch position", "true" ] }, { "ans": [ "Indicates that the extract fan has stopped", "false" ] } ], "ref": "Ref FCOM 1.21.50" }, { "ch": "When do the isolation valves closed?: (A, B1, B2)", "ansGr": [ { "ans": [ "In case of extract fan failed", "false" ] }, { "ans": [ "In case of aft cargo smoke warning", "true" ] }, { "ans": [ "In case of AEVC failed", "false" ] } ], "ref": "Ref P94 ATA21-T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "How can you switching the cabin pressurization controller?: (A, B1, B2)", "ansGr": [ { "ans": [ "Cycle the LDG ELEV AUTO knob out of the AUTO position then back to AUTO", "false" ] }, { "ans": [ "Cycle the CABIN PRESS MODE SEL pushbutton to the MAN position then back to AUTO", "true" ] }, { "ans": [ "Cycle the cabin pressurization MAN V/S CTL switch", "false" ] } ], "ref": "Ref FCOM 1.21.20" }, { "ch": "What is the consequence if a decompression panel in the cargo is failure? (A, B1, B2)", "ansGr": [ { "ans": [ "Cargo compartment shall be empty or no flammable materials cargo loaded", "true" ] }, { "ans": [ "No live stock allowed", "false" ] }, { "ans": [ "Cabin pressurization system warning “EXCEESS CAB ALT” may occurs", "false" ] } ], "ref": "Ref. MEL 25-50-01A" }, { "ch": "What is the position of the avionic ventilation vavles when OVRD is selected on the EXTRACT pushbutton?: (A, B1, B2)", "ansGr": [ { "ans": [ "Underfloor valve open, overboard valve partially open", "false" ] }, { "ans": [ "Underfloor valve closed, overboard valve open", "false" ] }, { "ans": [ "Underfloor valve closed, overboard valve partially opeN", "true" ] } ], "ref": "Ref P121 ATA21-T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "What is the position of the avionic ventilation vavles in flight/ or at least 1 engine running in AUTO mode?: (A, B1, B2)", "ansGr": [ { "ans": [ "Underfloor valve open, overboard valve partially open", "false" ] }, { "ans": [ "Underfloor valve open, overboard valve closed", "true" ] }, { "ans": [ "Underfloor valve open, overboard valve open", "false" ] } ], "ref": "Ref P121 ATA21-T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "When does the emergency ram air inlet flap open?: (A)", "ansGr": [ { "ans": [ "The ram air p/b is selected ON and ditching p/b selected OFF.", "true" ] }, { "ans": [ "The ditching p/b is selected ON and delta P inferior a 1 psi", "false" ] }, { "ans": [ "When both Out Flow Valves are openned manually", "false" ] } ], "ref": "Ref P50 ATA21-T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "Which motor(s) is(are) controlled from the cabin pressure panel?: (A)", "ansGr": [ { "ans": [ "Motor 1", "false" ] }, { "ans": [ "Motor 3", "true" ] }, { "ans": [ "Motor 3 and Motor 1", "false" ] } ], "ref": "Ref P110 ATA21-T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "What is the normal position of the outflow valves when aircraft stop on GND? (A)", "ansGr": [ { "ans": [ "Both open", "true" ] }, { "ans": [ "Either FWD or AFT valve open", "false" ] }, { "ans": [ "Closed or open depend on the outside temperature", "false" ] } ], "ref": "Ref AMM 21-31-00 PB001 and Ref P110 ATA21-T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "Auto flight system built around: (A)", "ansGr": [ { "ans": [ "1 FMGEC, 3 MCDU, FCU", "false" ] }, { "ans": [ "2 FMGEC, 2 MCDU, FCU", "false" ] }, { "ans": [ "2 FMGECs, 3 MCDUs, FCU", "true" ] } ], "part": "ATA 22: AUTO FLIGHT", "ref": "Ref (AMM 22-00-00 PB001)" }, { "ch": "During auto flight operation, the side sticks and thrust levels: (A)", "ansGr": [ { "ans": [ "Do not move automatically", "true" ] }, { "ans": [ "Move automatically during aircraft roll banking", "false" ] }, { "ans": [ "Automatically set to TOGA thrust target", "false" ] } ], "ref": "Ref (AMM 22-00-00 PB001)" }, { "ch": "The FIDS is active in: (A)", "ansGr": [ { "ans": [ "FMGEC installed on the side 1 only", "true" ] }, { "ans": [ "FMGEC installed on the side 2 only", "false" ] }, { "ans": [ "FMGEC 1 or 2 change over each flight.", "false" ] } ], "ref": "Ref (AMM 22-00-00 PB001)" }, { "ch": "Can we engage AP on ground? (A)", "ansGr": [ { "ans": [ "No, we can not", "false" ] }, { "ans": [ "Yes, we can if both engines stopped", "true" ] }, { "ans": [ "Yes, we can if both engines are running", "false" ] } ], "ref": "Ref (AMM 22-11-00 PB001)" }, { "ch": "Which computer contains navigation databases? (A)", "ansGr": [ { "ans": [ "MCDU", "false" ] }, { "ans": [ "FMGEC", "true" ] }, { "ans": [ "T2CAS", "false" ] } ], "ref": "Ref (AMM 22-70-00 PB001)" }, { "ch": "If very high frequency 2 (VHF 2) is selected on radio management panel 3 (RMP 3): (A)", "ansGr": [ { "ans": [ "Nothing happens.", "false" ] }, { "ans": [ "The SELector light comes on, on RMP 3 and RMP 2.", "true" ] }, { "ans": [ "The SELector light comes on, on three RMPs.", "false" ] } ], "part": "ATA 23: COMMUNICATIONS", "ref": "Ref AMM 23-81-00 PB001" }, { "ch": "Any communication transceiver frequency selection can be performed from: (A)", "ansGr": [ { "ans": [ "Any Radio Management Panel (RMP).", "true" ] }, { "ans": [ "RMP 1 and RMP 2 only.", "false" ] }, { "ans": [ "Any Audio Control Panel (ACP)", "false" ] } ], "ref": "(Ref AMM 23-81-00PB001)" }, { "ch": "When aircraft on ground to communicate on the service interphone from the cockpit to any service interphone jack by using a cockpit handmike: (A)", "ansGr": [ { "ans": [ "Select INT on the Audio Control Panel (ACP) and press the SVCE INT OVRD switch on the overhead maintenance panel.", "false" ] }, { "ans": [ "Press the CAB key and push to release CAB knob on the related ACP.", "true" ] }, { "ans": [ "Select the INT transmission key on the ACP and activate the INT reception knob.", "false" ] } ], "ref": "(Ref AMM 23-44-00-860-801-A)" }, { "ch": "Decoder/encoder units (DEU) type A and B are used for: ( A)", "ansGr": [ { "ans": [ "Cabin Intercommunication Data System (CIDS) control.", "false" ] }, { "ans": [ "Cockpit and avionics bay systems interface.", "false" ] }, { "ans": [ "CIDS Directors and cabin systems interface.", "true" ] } ], "ref": "(Ref AMM 23-73-00 PB001)" }, { "ch": "The solid state cockpit voice recorder (SSCVR) records: ( A)", "ansGr": [ { "ans": [ "Communications between cockpit and ground.", "false" ] }, { "ans": [ "All cockpit crew conversations and ambient noise.", "true" ] }, { "ans": [ "No other page comes on automatically (warning, advisory...) or is manually selected on the ECAM Control Panel (ECP).", "false" ] } ], "ref": "(Ref AMM 23-71-00 PB 001 )" }, { "ch": "Radio management panel 1 (RMP 1) is allocated to: ( A)", "ansGr": [ { "ans": [ "VHF Data Radio 1 (VDR 1).", "true" ] }, { "ans": [ "VDR 1and HF Data Radio 1 (HFDR 1).", "false" ] }, { "ans": [ "VDR 1 and VDR3 in case VDR 1 fail.", "false" ] } ], "ref": "(Ref AMM 23-81-00 PB001)" }, { "ch": "In normal operation, VHF data radio (VDR) transceiver frequency control is performed by: (A, B1, B2)", "ansGr": [ { "ans": [ "Any Audio control panels (ACPs)", "false" ] }, { "ans": [ "RMPs and the Air Traffic Service Unit (ATSU) for all VDRs.", "false" ] }, { "ans": [ "RMPs for all VDRs, and the ATSU for VDR3.", "true" ] } ], "ref": "(Ref AMM 23- 81- 00 PB001)" }, { "ch": "In reception, with a failure of the capt channel, the manual emergency mode is to set the audio switching selector to the: (A,B1, B2)", "ansGr": [ { "ans": [ "CAPT ON 3 position.", "true" ] }, { "ans": [ "F/O ON 3 position", "false" ] }, { "ans": [ "NORM position.", "false" ] } ], "ref": "Ref AMM 23-51-00 PB001 and P52 ATA 23 T1+T2 A330 RR Trent 700" }, { "ch": "The passenger address (PA) is broadcast announcements for passengers from: (A)", "ansGr": [ { "ans": [ "Cockpit to all passenger loudspeakers.", "false" ] }, { "ans": [ "Cockpit, the attendant stations to all passenger loudspeakers.", "true" ] }, { "ans": [ "The attendant stations to all passenger loudspeakers", "false" ] } ], "ref": "Ref AMM 23-73-00 PB001" }, { "ch": "The service interphone system allows communication between: (A)", "ansGr": [ { "ans": [ "Flight crew and service interphone jacks.", "false" ] }, { "ans": [ "Flight attendant stations and service interphone jacks.", "false" ] }, { "ans": [ "The cockpit, the cabin crew stations and the service interphone jacks located around and in the aircraft.", "true" ] } ], "ref": "Ref AMM 23-44-00 PB001 and P100 ATA 23 T1+T2 A330 RR Trent 700" }, { "ch": "The INT/RAD switch on the ACP is used for establishing call from? (A,B2)", "ansGr": [ { "ans": [ "Handset.", "false" ] }, { "ans": [ "Boomset.", "true" ] }, { "ans": [ "Side-stick PTT handgrips.", "false" ] } ], "ref": "Ref AMM 23-51-00-00 CONF 00 - AUDIO MANAGEMENT SYSTEM (AMS)" }, { "ch": "Reset the CIDS by pulling 2 C/Bs on the reset panel? (A, B2)", "ansGr": [ { "ans": [ "Whole cabin lights will be turn OFF", "false" ] }, { "ans": [ "The CIDS will do a power up test", "true" ] }, { "ans": [ "CIDS will stay powered, only cabin lighting control system to be reset.", "false" ] } ], "ref": "Ref AMM 23-73-00-710-814-A" }, { "ch": "Aircraft on ground, in order to communicate between cockpit and APU position, you must: (A)", "ansGr": [ { "ans": [ "Select the INT on the audio control panel and press the “SERV INT” pushbutton.", "false" ] }, { "ans": [ "Press “CAB” transmission key and release “CAB” receiving knob.", "true" ] }, { "ans": [ "Press “CAB” transmission key and “SERV INT” pushbutton.", "false" ] } ], "ref": "Ref AMM 23-44-00-860-801-A" }, { "ch": "The Cabin AREA CALL PANEL indicates: (A, B1, B2)", "ansGr": [ { "ans": [ "The call started from the ground, cockpit, PAX and also lavatory smoke alert.", "false" ] }, { "ans": [ "The call started from interphone call, PAX, EVAC signaling and lavatory smoke alert.", "true" ] }, { "ans": [ "The call started from interphone call, PAX and lavatory smoke alert.", "false" ] } ], "ref": "Ref AMM 23-73-00 PB00" }, { "ch": "To supply the service bus only, we must connect aircraft with external power source: (A)", "ansGr": [ { "ans": [ "External power A", "true" ] }, { "ans": [ "External power B", "false" ] }, { "ans": [ "Both external powers A and B at the same time", "false" ] } ], "part": "ATA 24 ELECTRICAL POWER", "ref": "Ref P26 - ATA 24 - T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "Which push button has AUTO position? (A)", "ansGr": [ { "ans": [ "Ext power A", "false" ] }, { "ans": [ "Ext power B", "true" ] }, { "ans": [ "APU GEN", "false" ] } ], "ref": "Ref FCOM 24-20 (ELEC control panel)" }, { "ch": "To perform grounding aircraft, we must: (A)", "ansGr": [ { "ans": [ "Connect the ground cable to the ground point before connecting it to aircraft.", "true" ] }, { "ans": [ "Connect the ground cable to the aircraft and then connect it to the ground point.", "false" ] }, { "ans": [ "Not necessary following the sequence.", "false" ] } ], "ref": "Ref AMM TASK 12-34-24-860-801-A Warning" }, { "ch": "To make the bonding of the aircraft before the defuel/refuel operation, we must:(A)", "ansGr": [ { "ans": [ "Connect the bonding cable from the fuel tanker to the ground point.", "false" ] }, { "ans": [ "Connect the bonding cable from the fuel tanker to the ground point of the aircraft.", "true" ] }, { "ans": [ "Connect bonding cable between two fuel tankers.", "false" ] } ], "ref": "Ref AMM TASK 12-34-24-860-801" }, { "ch": "For servicing IDG oil, what is correct level for IDG oil after an engine dry motoring – cold oil condition? (A)", "ansGr": [ { "ans": [ "Oil level is within the green band", "true" ] }, { "ans": [ "Oil level is above the green band", "false" ] }, { "ans": [ "Oil level is within the yellow band", "false" ] } ], "ref": "Ref AMM TASK 12-13-24-612-812-A" }, { "ch": "For servicing IDG oil, what is correct level for IDG oil after an engine starts – hot oil condition? (A)", "ansGr": [ { "ans": [ "The oil level is within the green band.", "false" ] }, { "ans": [ "The oil level is above the green band but within the yellow band.", "false" ] }, { "ans": [ "The oil level is within the yellow band.", "true" ] } ], "ref": "Ref AMM TASK 12-13-24-612-812-A" }, { "ch": "Filling of the IDG with oil, when will you disconnect the pressure fill hose? (A)", "ansGr": [ { "ans": [ "When the quantity of oil collected minimum of 0.95 l (0.2510 USgal) from the overflow port.", "true" ] }, { "ans": [ "When only drops of oil come out the overflow hose after oil collected more than minimum of requirement.", "false" ] }, { "ans": [ "When we see drops of oil come out of the overflow hose.", "false" ] } ], "ref": "Ref AMM TASK 12-13-24-612-812-A" }, { "ch": "APU BCL fault, which is correct sentence? (A)", "ansGr": [ { "ans": [ "APU cannot start.", "true" ] }, { "ans": [ "APU can start by external power.", "false" ] }, { "ans": [ "APU can start with APU BAT pushed.", "false" ] } ], "ref": "Ref P140 - ATA 24 - T1+T2 Mechanical and Avionics A330 RR TRENT 700; And ASM 24-00-01 SCH 01 P 0005; ASM 49-42-01 SCH 01 P 0004" }, { "ch": "Normally DC ESS bus supplied by: (A)", "ansGr": [ { "ans": [ "TR 1 through DC BUS 1", "false" ] }, { "ans": [ "ESS TR through AC ESS bus", "true" ] }, { "ans": [ "TR 2 through DC BUS 2", "false" ] } ], "ref": "Ref P138 - ATA 24 - T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "In case of emergency generator running on ground, which bus bar will be cut? (A)", "ansGr": [ { "ans": [ "AC ESS", "false" ] }, { "ans": [ "AC ESS and DC ESS", "false" ] }, { "ans": [ "AC ESS SHED and DC ESS SHED.", "true" ] } ], "ref": "Ref AMM task 24-24-00-710-801-A" }, { "ch": "The Operational Test of the AC Emergency Generation System is for: (A)", "ansGr": [ { "ans": [ "Make sure that aircraft electrical networks are supplied through CSM/G.", "false" ] }, { "ans": [ "Make sure that the essential busbars are supplied through the CSM/G.", "true" ] }, { "ans": [ "Make sure that AC essential busbars are supplied through the CSM/G & Shedd-able buses are shed", "false" ] } ], "ref": "Ref AMM 24-24-00-710-801-A" }, { "ch": "Press and hold the EMER GEN TEST P/B switch causes? (A)", "ansGr": [ { "ans": [ "Start the test of Emergency Generator.", "false" ] }, { "ans": [ "RAT extension if no AC normal bus available.", "false" ] }, { "ans": [ "Nothing happens", "true" ] } ], "ref": "Ref AMM 24-24-00-710-801- A" }, { "ch": "What work is always required after main Batteries replacement? (A)", "ansGr": [ { "ans": [ "Recycling of the BAT pushbutton switch and adjusting the Clock.", "false" ] }, { "ans": [ "Upload PDIMU memory (ENG and APU HRS & CYC).", "false" ] }, { "ans": [ "Operational test of the BCL", "true" ] } ], "ref": "Ref AMM 24-38-51 PB401" }, { "ch": "What of the following conditions is necessary for test of CSM/G? (A)", "ansGr": [ { "ans": [ "All Leak Measurement Valves are PUSHED.", "false" ] }, { "ans": [ "Slat/Flap retracted.", "true" ] }, { "ans": [ "Green and Blue hydraulic pumps are OFF.", "false" ] } ], "ref": "Ref AMM 24-24-00-710-801-A" }, { "ch": "How do you switch on only the Maintenance buses? (A)", "ansGr": [ { "ans": [ "EXT PWR energized A/C network; MAINT BUS switch is in ON position.", "false" ] }, { "ans": [ "EXT PWR A/AVAIL; MAINT BUS switch is in ON position.", "true" ] }, { "ans": [ "EXT PWR B/AVAIL; MAINT BUS switch is in ON position.", "false" ] } ], "ref": "Ref AMM 24-42-00-861-801-A" }, { "ch": "Battery voltage check is carried out with. (A)", "ansGr": [ { "ans": [ "BAT P/B AUTO.", "false" ] }, { "ans": [ "BAT P/B OFF.", "true" ] }, { "ans": [ "EXT power connected.", "false" ] } ], "ref": "Ref ASM 24-37-01 SCH 01 P 0001" }, { "ch": "What is the function of NBPT (A, B2):", "ansGr": [ { "ans": [ "To prevent busbar power interruption due to electrical power supply source transfer on ground in emergency.", "false" ] }, { "ans": [ "To prevent busbar power interruption due to electrical power supply source transfer in flight in normal.", "false" ] }, { "ans": [ "To prevent busbar power interruption due to electrical power supply source transfer on ground in normal.", "true" ] } ], "ref": "Ref: AMM 24-00-00-00 conf 00 - electrical power - description and operation" }, { "ch": "Where is APU battery located (A, B1, B2):", "ansGr": [ { "ans": [ "In avionic bay.", "false" ] }, { "ans": [ "In the sidewall panel 162rw of the bulk cargo compartment.", "true" ] }, { "ans": [ "In the APU compartment.", "false" ] } ], "ref": "Ref AMM task 24-38-52-000/400-801-a" }, { "ch": "The APU Bat is used (A, B1, B2)", "ansGr": [ { "ans": [ "To supply the DC BAT BUS in case of BAT 1 and BAT 2 failure", "false" ] }, { "ans": [ "To start the APU", "true" ] }, { "ans": [ "To supply APU auto fire extinguishing power sources", "false" ] } ], "ref": "Ref AMM 24-38-00-00 conf 00 - dc generation - batteries - description and operation" }, { "ch": "The AC power source supply priority for AC BUS 1 is as follows: (A, B1, B2)", "ansGr": [ { "ans": [ "GEN 1 / EXT A / APU GEN/ EXT B / GEN 2", "false" ] }, { "ans": [ "GEN 2 / APU GEN / EXT B / EXT A / GEN 1", "false" ] }, { "ans": [ "GEN 1 / APU GEN / EXT B / EXT A / GEN 2", "true" ] } ], "ref": "Ref AMM 24-22-00-00 conf 00 - ac main generation - description and operation" }, { "ch": "The AC power source supply priority for AC BUS 2 is as follows: (A, B1, B2)", "ansGr": [ { "ans": [ "GEN 1 / EXT A / APU GEN/ EXT B / GEN 2", "false" ] }, { "ans": [ "GEN 2 / EXT A / APU GEN / EXT B / GEN 1.", "true" ] }, { "ans": [ "GEN 1 / APU GEN / EXT B / EXT A / GEN 2", "false" ] } ], "ref": "Ref Amm 24-22-00-00 conf 00 - ac main generation - description and operation" }, { "ch": "Floor lighting is located under the seat pan of: (A, B1, B2)", "ansGr": [ { "ans": [ "Captain and First Officer seats only", "true" ] }, { "ans": [ "Captain, First Officer seats and Third Occupant Seat", "false" ] }, { "ans": [ "Captain, First Officer seats and Fourth Occupant Seat", "false" ] } ], "part": "ATA 25: EQUIPMENT/FURNISHINGS", "ref": "Ref: AMM 25-11-00 PB001" }, { "ch": "Third Occupant Seat has: (A)", "ansGr": [ { "ans": [ "Only mechanical controls", "true" ] }, { "ans": [ "Mechanical controls and electrical controls.", "false" ] }, { "ans": [ "Only electrical controls.", "false" ] } ], "ref": "Ref: AMM 25-11-00 PB001" }, { "ch": "The side stick armrests (Captain and F/O) are:(A)", "ansGr": [ { "ans": [ "Symmetrical for the Captain and First Officer", "true" ] }, { "ans": [ "Asymmetrical for the Captain and First Officer.", "false" ] }, { "ans": [ "Interchangeable for the Captain and First Officer.", "false" ] } ], "ref": "Ref: AMM 25-11-00 PB 001" }, { "ch": "When you adjust Captain and First Officer seats (electrical controls), when the seat reaches its limit position: (A, B1, B2)", "ansGr": [ { "ans": [ "The electrical stop cuts off power supply to the gear motor.", "true" ] }, { "ans": [ "The gear motor runs until you release the control switch.", "false" ] }, { "ans": [ "The gear motor runs and locks the seat on the rack.", "false" ] } ], "ref": "Ref: AMM 25-11-00 PB001" }, { "ch": "To deactivate a Defective Cabin Attendant Seat: (A, B1, B2)", "ansGr": [ { "ans": [ "Safety the affected seat in its stowed position and put a WARNING NOTICE, if not remove it.", "true" ] }, { "ans": [ "You have to remove it.", "false" ] }, { "ans": [ "Safety the affected seat in its stowed position.", "false" ] } ], "ref": "Ref: AMM 25-22-00-040-801" }, { "ch": "Each PSU (Passenger Service Unit) contains: (A, B1, B2)", "ansGr": [ { "ans": [ "A reading light panel, a cabin attendance call/reset, a loudspeaker, a information light sign.", "true" ] }, { "ans": [ "A reading light panel and PAX air conditioning tube.", "false" ] }, { "ans": [ "A lighted sign NO SMOKING and FASTEN SEAT BELT.", "false" ] } ], "ref": "Ref: AMM 25-25-00 PB 001" }, { "ch": "The wet unit galley is used to: (A)", "ansGr": [ { "ans": [ "Store and prepare food and drink. It is provided with electrically operated equipment and provisions for potable and waste water.", "true" ] }, { "ans": [ "Store food, drinks and equipment only.", "false" ] }, { "ans": [ "Store food, drinks and equipment only and has a crew rest.", "false" ] } ], "ref": "Ref: AMM 25-31-00" }, { "ch": "The air chiller units supply cold air to: (A)", "ansGr": [ { "ans": [ "Trolleys or the trolley compartment in the connected galleys.", "true" ] }, { "ans": [ "Trolleys and galleys.", "false" ] }, { "ans": [ "All wet and dry galleys.", "false" ] } ], "ref": "Ref: AMM 25-34-00 PB 001" }, { "ch": "To deactivate the Galley-Waste-Compartment Flapper-Door: (A, B1, B2)", "ansGr": [ { "ans": [ "Make sure that no waste can be put into the waste compartment and make logbook entry.", "true" ] }, { "ans": [ "Make sure that the flapper-door cannot be opened.", "false" ] }, { "ans": [ "Put a WARNING NOTICE in position to tell people not to use the galley-waste-compartment and seal with the aluminum foil tape.", "false" ] } ], "ref": "Ref: AMM 25-35-00-040-801" }, { "ch": "To deactivate of the defective Toilet Waste-Compartment Flapper-Door: (A, B1, B2)", "ansGr": [ { "ans": [ "Seal the opening of the waste chute with self-adhesive tape and put a WARNING NOTICE.", "false" ] }, { "ans": [ "Put a WARNING NOTICE in position to tell people do not use the waste compartment.", "false" ] }, { "ans": [ "Make sure the waste container is empty, seal the opening of the waste chute with self-adhesive aluminum foil tape and put a WARNING NOTICE.", "true" ] } ], "ref": "Ref: AMM 25-40-00-040-801" }, { "ch": "Lavatory Door(s) can be: (A)", "ansGr": [ { "ans": [ "Unlocked and opened from the outside of the lavatory.", "true" ] }, { "ans": [ "Unlocked and opened from the inside of the lavatory only.", "false" ] }, { "ans": [ "Locked from the inside of the lavatory only.", "false" ] } ], "ref": "Ref: AMM 25-45-00 PB 001" }, { "ch": "You can control the FWD and AFT cargo loading systems from: (A)", "ansGr": [ { "ans": [ "Separate control panels.", "true" ] }, { "ans": [ "FWD control panel near to the FWD cargo compartment door.", "false" ] }, { "ans": [ "AFT control panel near to the AFT cargo compartment door.", "false" ] } ], "ref": "Ref: AMM 25-50-00 PB 001" }, { "ch": "Which cargo compartment has semiautomatic cargo-loading system: (A)", "ansGr": [ { "ans": [ "FWD Cargo Compartment and AFT Cargo Compartment.", "true" ] }, { "ans": [ "FWD Cargo Compartment and BULK Cargo Compartment.", "false" ] }, { "ans": [ "AFT Cargo Compartment and BULK Cargo Compartment", "false" ] } ], "ref": "Ref: AMM 25-50-00 PB 001" }, { "ch": "When you open a door with the emergency control-handle set in the ARMED position, indications are given: (A, B1, B2)", "ansGr": [ { "ans": [ "At the applicable door, on the Forward Attendant Panel (FAP) and on the display units of the ECAM system.", "true" ] }, { "ans": [ "On the Forward Attendant Panel (FAP), at the applicable door.", "false" ] }, { "ans": [ "On the display units of the ECAM system, at the applicable door.", "false" ] } ], "ref": "Ref: AMM 25-62-00 PB 001" }, { "ch": "The inflation reservoirs pressure is monitored and low pressure indications are shown on: (A)", "ansGr": [ { "ans": [ "On FAP thru the CIDS.", "true" ] }, { "ans": [ "The display units of the ECAM system.", "false" ] }, { "ans": [ "The MCDU-CIDS page.", "false" ] } ], "ref": "Ref: AMM 25-62-00 PB 001" }, { "ch": "When you set the emergency control handle to the ARMED position: (A, B1, B2)", "ansGr": [ { "ans": [ "The girt bar connects the girt of the pack assembly to the door frame structure.", "true" ] }, { "ans": [ "The girt bar disconnects the girt of the pack assembly from the door frame structure.", "false" ] }, { "ans": [ "The emergency operation cylinder pushes the door to the fully open position", "false" ] } ], "ref": "Ref: AMM 25-62-00 PB 001" }, { "ch": "The cabin escape facilities (slide/raft) are installed on: (A)", "ansGr": [ { "ans": [ "All passenger doors", "false" ] }, { "ans": [ "All emergency exit doors.", "false" ] }, { "ans": [ "All passenger doors and all emergency exit doors.", "true" ] } ], "ref": "Ref: AMM 25-62-00 PB 001" }, { "ch": "The door escape facilities have interfaces with: (A, B1, B2)", "ansGr": [ { "ans": [ "The CIDS, the cabin emergency-lighting system.", "false" ] }, { "ans": [ "The cabin emergency-lighting system, Door and Escape-Slide Control System (DSCS) and CIDS.", "true" ] }, { "ans": [ "Door and Escape-Slide Control System (DSCS), the cabin emergency-lighting system.", "false" ] } ], "ref": "Ref: AMM 25-62-00 PB 001" }, { "ch": "The CHECK SLIDE PRESSURE message? (A, B1, B2)", "ansGr": [ { "ans": [ "Means that the door cylinder is low pressure.", "false" ] }, { "ans": [ "Shown if safety pin installed on slide bottle.", "true" ] }, { "ans": [ "Slide bottle pressure is out of normal range (MIN/MAX)", "false" ] } ], "ref": "Ref AMM 25-62-41-400-801, AMM 25-62-42-400-801" }, { "ch": "The LAV waste bin extinguisher pressure can be checked? (A)", "ansGr": [ { "ans": [ "Through the Flight Attendant Panel (FAP).", "false" ] }, { "ans": [ "On the bottle pressure sight gage.", "true" ] }, { "ans": [ "Using the red disk indicator fitted on the bottle.", "false" ] } ], "ref": "Ref AMM 26-25-00-280-803" }, { "ch": "What precaution for working on the PAX door escape slide raft? (A, B1, B2)", "ansGr": [ { "ans": [ "The door-damper and emergency-operation cylinder is DISARMED, Slide inflation reservoir is safetied.", "false" ] }, { "ans": [ "Door emergency control-handle is set to the DISARMED position, Door-damper and emergency-operation cylinder is DISARMED; Slide inflation reservoir is safetied.", "true" ] }, { "ans": [ "Slide inflation reservoir is safetied, Door emergency control-handle is set to the DISARMED position", "false" ] } ], "ref": "Ref AMM 25-62-41 PB401, AMM 25-62-42-PB401" }, { "ch": "To prevent inadvertent activation of the fixed ELT, what should be noted: (A, B1, B2)", "ansGr": [ { "ans": [ "Make sure AUTO-OFF-MAN/RESET switch is in OFF prior installation.", "true" ] }, { "ans": [ "Make sure AUTO-OFF-MAN/RESET switch is in AUTO prior installation.", "false" ] }, { "ans": [ "Make sure AUTO-OFF-MAN/RESET switch is in MAN/RESET prior installation.", "false" ] } ], "ref": "Ref AMM 25-65-35 PB401" }, { "ch": "The Fourth Occupant seat (A, B1, B2)", "ansGr": [ { "ans": [ "Is NOT adjustable.", "false" ] }, { "ans": [ "Has only mechanical control for in horizontal and vertical travel.", "true" ] }, { "ans": [ "Is identical to the third occupant seat", "false" ] } ], "ref": "Ref AMM 25-11-00-00 CONF 00 - COCKPIT SEATS - DESCRIPTION AND OPERATION" }, { "ch": "The YZ-latches must be lowered manually: (B1, B2)", "ansGr": [ { "ans": [ "During loading operation,", "false" ] }, { "ans": [ "During unloading operation,", "false" ] }, { "ans": [ "During both operations.", "true" ] } ], "ref": "Ref AMM 25-51-00-00 CONF 00 - LOWER DECK CARGO LOADING SYSTEM (CLS) - DESCRIPTION AND OPERATION" }, { "ch": "With the APU fire detection loop A INOP, the MEL requires: (A, B1, B2)", "ansGr": [ { "ans": [ "To monitor APU condition continuously in the CKPT during its GND operation.", "false" ] }, { "ans": [ "Not to operate the APU on GND.", "false" ] }, { "ans": [ "APU fire is made before each APU start.", "true" ] } ], "part": "ATA 26: FIRE PROTECTION", "ref": "Ref. MEL 26-13-01" }, { "ch": "To do the operational test of the APU Fire-Extinguishing System: (A, B1, B2)", "ansGr": [ { "ans": [ "The APU MASTER SW P/B must be pushed to ON.", "true" ] }, { "ans": [ "Do not need to push ON APU MASTER SW.", "false" ] }, { "ans": [ "Only push and hold the TEST P/B.", "false" ] } ], "ref": "Ref. AMM 26-22-00-710-801" }, { "ch": "What is the warning while you do operational test of the APU Fire-Extinguishing System? (A)", "ansGr": [ { "ans": [ "Do not release the APU fire TEST P/B.", "false" ] }, { "ans": [ "Do not push and hold the fire TEST P/B.", "false" ] }, { "ans": [ "Do not push the AGENT pushbutton switch while the APU fire p/b switch is released", "true" ] } ], "ref": "Ref. AMM 26-22-00-710-801-A" }, { "ch": "What are warnings if a smoke detection in the Avionics Compartment is confirmed by the SDCU? (A, B1, B2)", "ansGr": [ { "ans": [ "Warning on the FIRE panel, the MASTER WARN light, message on the EWD and the CRC.", "false" ] }, { "ans": [ "Warning on the VENTILATION control panel, the MASTER WARN light, message on the EWD and the CRC.", "true" ] }, { "ans": [ "the MASTER WARN light, message on the EWD and the CRC.", "false" ] } ], "ref": "Ref. AMM 26-00-00 PB 001" }, { "ch": "How do you make sure a Waste-Bin Fire- Extinguishing Bottle is serviceable? (A, B1, B2)", "ansGr": [ { "ans": [ "The gauge needle is in the green area.", "true" ] }, { "ans": [ "The gauge needle is on the outer side, to the right of the green area.", "false" ] }, { "ans": [ "The gauge needle is on the outer side, to the left of the green area.", "false" ] } ], "ref": "Ref AMM 26-25-00 PB 601" }, { "ch": "How does the APU fire Extinguishing can be operated? (A, B1, B2)", "ansGr": [ { "ans": [ "It can be operated manually only on the ground, from the cockpit.", "false" ] }, { "ans": [ "From the EXT panel or from refuel/defuel station: push the APU EMERG P/B.", "false" ] }, { "ans": [ "In flight or on the ground, the crew can operate the system manually from the cockpit.", "true" ] } ], "ref": "Ref. AMM 26-22-00 PB001" }, { "ch": "You do the APU fire test prior to start the APU with no EXT PWR available? (A)", "ansGr": [ { "ans": [ "The red fire lights in APU fire P/B will not come on.", "false" ] }, { "ans": [ "The red fire lights in APU fire P/B will come on in half only.", "false" ] }, { "ans": [ "The red fire lights in APU fire P/B will come on in half only, and the SQUIB/DISCH legends in the AGENT P/B Sw comes on.", "true" ] } ], "ref": "Ref. AMM 49-00-00-860-801" }, { "ch": "What do you do to prevent the APU fire bottle from being discharged during APU fire test? :(A)", "ansGr": [ { "ans": [ "Keep the Master S/W OFF, Batteries OFF.", "false" ] }, { "ans": [ "Pull C/B L40 on 121VU.", "false" ] }, { "ans": [ "Simulation of flight configuration from MCDU.", "true" ] } ], "ref": "Ref. AMM 49-00-00-860-801" }, { "ch": "What if the APU fire bottle red disk found missing? (A)", "ansGr": [ { "ans": [ "APU has a fire, and the fire bottle has been emptied automatically.", "false" ] }, { "ans": [ "The fire bottle has been emptied manually.", "false" ] }, { "ans": [ "The bottle has been emptied as result of overpressure.", "true" ] } ], "ref": "Ref. Airbus TTM ATA 26" }, { "ch": "THE APU AUTOMATIC EXTINGUISHING ON GROUND IS CONTROL BY: (A, B1, B2)?", "ansGr": [ { "ans": [ "APU FDU", "false" ] }, { "ans": [ "AFECU", "true" ] }, { "ans": [ "SDCU", "false" ] } ], "ref": "Ref: AMM 26-22-00-00 CONF 00 - APU FIRE EXTINGUISHING - DESCRIPTION AND OPERATION" }, { "ch": "HOW MANY FIRE EXTINGUISHING BOTTLE PROVIDE FOR CARGO COMPARTMENTS (A, B1, B2)?", "ansGr": [ { "ans": [ "One", "false" ] }, { "ans": [ "Two", "true" ] }, { "ans": [ "Three", "false" ] } ], "ref": "Ref AMM 26-23-00-00 CONF 00 - LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING FWD, AFT AND BULK - DESCRIPTION AND OPERATION" }, { "ch": "How can the aircraft be controlled in mechanical backup? (A)", "ansGr": [ { "ans": [ "Pitch Trim is achieved using the Horizontal Stabilizer manual trim wheels, lateral control is by rudder trim selector", "false" ] }, { "ans": [ "Pitch Trim is achieved using the Horizontal Stabilizer manual trim wheels, lateral control is by Rudder pedals", "true" ] }, { "ans": [ "Pitch Trim is achieved using the Horizontal Stabilizer manual trim wheels, lateral control is by BYDU", "false" ] } ], "part": "ATA 27: FLIGHT CONTROLS", "ref": "Ref. AMM 27-90-00 PB001" }, { "ch": "Which statement is correct regarding the Aileron Droop function? (A, B1, B2)", "ansGr": [ { "ans": [ "The inboard ailerons are deflected downwards 10o when the slats and flaps are extended", "false" ] }, { "ans": [ "The outboard ailerons are deflected downwards 10o when the slats and flaps are extended", "false" ] }, { "ans": [ "All ailerons are deflected downwards 10o when the flaps are extended", "true" ] } ], "ref": "Ref. AMM 27-90-00 PB001" }, { "ch": "Which statement is correct regarding the Speed Brake Function? :(A, B1, B2)", "ansGr": [ { "ans": [ "The Speed Brake Function is automatic (commanded from FMGEC)", "false" ] }, { "ans": [ "The Speed Brake Function is ensured by spoilers 1 to 6", "true" ] }, { "ans": [ "The Speed Brake Function has priority order over roll order", "false" ] } ], "ref": "Ref. Page 66 ATA27 - T1+T2 Mechanical and Avionics A330 RR TRENT 700." }, { "ch": "In high speed configuration the roll control is performed by :(A, B1, B2)", "ansGr": [ { "ans": [ "The inboard ailerons and the roll spoilers 2 to 6", "true" ] }, { "ans": [ "The outboard ailerons and the roll spoilers 2 to 6", "false" ] }, { "ans": [ "The inboard and outboard ailerons only", "false" ] } ], "ref": "Ref. Page 10 ATA27 - T1+T2 Mechanical and Avionics A330 RR TRENT 700." }, { "ch": "Each ruder servo control can operates in: (A, B1, B2)", "ansGr": [ { "ans": [ "Two modes: active or damping mode", "true" ] }, { "ans": [ "Three modes: active or damping or centering mode", "false" ] }, { "ans": [ "Three modes: active or damping or bypass mode", "false" ] } ], "ref": "Ref. AMM 27-24-00 PB001" }, { "ch": "In the case of control valve jamming, FCDCs initiate the warning when: (A, B1, B2)", "ansGr": [ { "ans": [ "The related ruder servo control is not pressurized", "false" ] }, { "ans": [ "The related ruder servo control is pressurized", "true" ] }, { "ans": [ "Immediately", "false" ] } ], "ref": "Ref. Lufthansa technical training ATA 27-23 page 183" }, { "ch": "Which statement is correct if one SFCC is inoperative? (A)", "ansGr": [ { "ans": [ "Flaps and Slats operate at half normal speed", "true" ] }, { "ans": [ "Flaps and slats both operate at normal speed.", "false" ] }, { "ans": [ "Slats operate normally, but the flaps operate at half speed", "false" ] } ], "ref": "Ref. Page 112 ATA27 - T1+T2 Mechanical and Avionics A330 RR TRENT 700" }, { "ch": "In the event of a complete electrical failure of the flight control computers the Back-Up Yaw Damper Unit (BYDU) provides: (A, B1, B2)", "ansGr": [ { "ans": [ "The turn co-ordination function", "false" ] }, { "ans": [ "The Dutch roll damping function", "true" ] }, { "ans": [ "The rudder trim function", "false" ] } ], "ref": "Ref. Lufthansa technical training ATA 27-26 page 196" }, { "ch": "In case of fuel tank unbalance: (A, B1, B2)", "ansGr": [ { "ans": [ "The fuel quantity indications can be pulsing", "true" ] }, { "ans": [ "The concerned fuel quantity indications become amber", "false" ] }, { "ans": [ "The last two digits are dashed with two horizontal amber lines", "false" ] } ], "part": "ATA 28: FUEL" }, { "ch": "The center tank vent pipe is connected to the: (A)", "ansGr": [ { "ans": [ "LH vent surge tank", "true" ] }, { "ans": [ "RH vent surge tank", "false" ] }, { "ans": [ "LH wing tank", "false" ] } ] }, { "ch": "The P/Bs on the fuel control panel controls the: (A)", "ansGr": [ { "ans": [ "Cross-feed valve, the main pumps, the stand-by pumps and the LP valves.", "false" ] }, { "ans": [ "Cross-feed valve, the main pumps and the stand-by pumps and CTR tank pumps (optional).", "true" ] }, { "ans": [ "Main pumps, the stand-by pumps, cross feed valve, T-tank isolation valve", "false" ] } ] }, { "ch": "In case of an APU fire, the: (A, B1, B2)", "ansGr": [ { "ans": [ "Engine and APU fuel pumps are stopped.", "false" ] }, { "ans": [ "Cross feed valve is closed.", "false" ] }, { "ans": [ "APU Low Pressure valve is closed.", "true" ] } ], "ref": "Ref. AMM 28-29-00 PB001" }, { "ch": "The auxiliary forward transfer valve controls the fuel flow between the (A, B1, B2)", "ansGr": [ { "ans": [ "Inner and center tanks.", "false" ] }, { "ans": [ "Outer and inner tanks.", "false" ] }, { "ans": [ "Trim and center tanks or inner tank.", "true" ] } ], "ref": "Ref. AMM 28-27-00 PB001" }, { "ch": "On the fuel control panel, the \"RH CTR TANK XFR\" P/BSW enables: (A)", "ansGr": [ { "ans": [ "Opening of the LH inner tank transfer valve.", "false" ] }, { "ans": [ "Operation of the RH inner tank transfer valve.", "false" ] }, { "ans": [ "Operation of the fuel transfer pump of the related right center tank.", "true" ] } ], "ref": "Ref. AMM 28-25-00 PB301" }, { "ch": "The TRIM TK FEED switch enables: (A)", "ansGr": [ { "ans": [ "Manual pressurized fuel FWD transfer to the center tank.", "false" ] }, { "ans": [ "Manual pressurized fuel aft transfer to the trim tank.", "false" ] }, { "ans": [ "Isolation/ open of the trim transfer pipe.", "true" ] } ], "ref": "Ref Page 528-529 ATA 28 T1+T2 A330 RR Trent 700 or FCOM DSC.28.20" }, { "ch": "Pressure defuel procedure, the defuel configuration is: (A, B1, B2)", "ansGr": [ { "ans": [ "MODE SELECT to DEFUEL, TRANSF VALVE to OPEN and fuel pumps turned on.", "true" ] }, { "ans": [ "Inlet valves close, isolation valves open and fuel pumps turned on.", "false" ] }, { "ans": [ "Inlet valves open, isolation valve open and fuel pumps turned off.", "false" ] } ], "ref": "Ref. AMM 28-25-00-650-801 And Page626 ATA 28 T1+T2 A330 RR Trent 700" }, { "ch": "It is possible to drain accumulated water in: (A)", "ansGr": [ { "ans": [ "All tanks.", "true" ] }, { "ans": [ "Wing tanks only.", "false" ] }, { "ans": [ "All tanks except the trim vent surge tank.", "false" ] } ], "ref": "Ref: AMM 12-32-28 PB301" }, { "ch": "At the refuel defuel area, put the NO SMOKING safety notice not less than: (A)", "ansGr": [ { "ans": [ "60 m.", "false" ] }, { "ans": [ "30 m.", "false" ] }, { "ans": [ "15 m.", "true" ] } ], "ref": "Ref: AMM 12-11-28-650-801" }, { "ch": "The distance of refueling/defueling safety zone and the fueling and venting points on the A/C is not less than: (A)", "ansGr": [ { "ans": [ "3 m.", "true" ] }, { "ans": [ "6 m.", "false" ] }, { "ans": [ "15 m.", "false" ] } ], "ref": "Ref: AMM 12-11-28-650-801" }, { "ch": "When excessive differential pressure in vent surge tank causes the overpressure protector to break open fuel is: (A)", "ansGr": [ { "ans": [ "Sucked back by a dedicated jet pump.", "false" ] }, { "ans": [ "Send overboard.", "true" ] }, { "ans": [ "Drained back into the inner tank through the drainpipe.", "false" ] } ], "ref": "Ref: AMM 28-12-00 PB001" }, { "ch": "Which information FCMS get from the ADIRS: (A, B1, B2)", "ansGr": [ { "ans": [ "Acceleration and pitch and roll angles.", "false" ] }, { "ans": [ "Fuel data, attitude and acceleration.", "false" ] }, { "ans": [ "Attitude, acceleration and pitch and roll angles.", "true" ] } ], "ref": "Ref: AMM 28-42-00 PB001 & AMM 12-11-28-860-801" }, { "ch": "Each engine LP valve is controlled open or shut by the: (A, B1, B2)", "ansGr": [ { "ans": [ "Fuel Control and Monitoring Computers (FCMCs).", "false" ] }, { "ans": [ "Corresponding ENG MASTER or ENG FIRE P/BSW.", "true" ] }, { "ans": [ "FCMCs or the corresponding ENG FIRE P/BSW.", "false" ] } ], "ref": "Ref Page 440-445 ATA 28 T1+T2 A330 RR Trent 700" }, { "ch": "When the center tank is empty, the FCMC will (Optional): (A, B1, B2)", "ansGr": [ { "ans": [ "De-energize both center tank pumps and close both inner tank inlet valves.", "true" ] }, { "ans": [ "De-energize both center tank pumps and close both inner tank transfer valves.", "false" ] }, { "ans": [ "Open the inner tank inlet valves.", "false" ] } ], "ref": "Ref: Page 470 ATA 28 T1+T2 A330 RR Trent 700" }, { "ch": "Fuel transfer from the outer to inner tank by: (A)", "ansGr": [ { "ans": [ "Gravity.", "true" ] }, { "ans": [ "Fuel pump pressure.", "false" ] }, { "ans": [ "Fuel pump pressure or a jet pump.", "false" ] } ], "ref": "Ref. AMM 28-26-00 PB001 and Page 476 ATA 28 T1+T2 A330 RR Trent 700" }, { "ch": "The FCMC controls the: (A, B1, B2)", "ansGr": [ { "ans": [ "Inner tank transfer valves only.", "false" ] }, { "ans": [ "Outer tank inlet valves only.", "false" ] }, { "ans": [ "Inner tank inlet valves, outer tank inlet valves and inner tank transfer valves.", "true" ] } ], "ref": "Ref AMM 28-26-00 PB001" }, { "ch": "When the T TK MODE P/BSW is set to FWD, FCMS: (A, B1, B2)", "ansGr": [ { "ans": [ "Still available to control A/C CG and the forward transfer starts with high-level protection.", "false" ] }, { "ans": [ "Stop control A/C CG and the forward transfer starts with high-level protection.", "false" ] }, { "ans": [ "Stop control A/C CG and the forward transfer starts with not active high-level protection", "true" ] } ], "ref": "Ref. AMM 28-27-00 PB001 and Page 526 ATA 28 T1+T2 A330 RR Trent 700" }, { "ch": "Suction defuel: (A, B1, B2)", "ansGr": [ { "ans": [ "On the R/D panel, the MODE SELECT switch must be set to REFUEL and the necessary pump P/Bs are pushed.", "false" ] }, { "ans": [ "On the R/D panel, the necessary REFUEL/DEFUEL VALVE switches set to OPEN, and the MODE SELECT switch must be set to DEFUEL.", "true" ] }, { "ans": [ "On the R/D panel, the MODE SELECT switch must be set to DEFUEL and the necessary pump P/Bs are pushed.", "false" ] } ], "ref": "Ref. AMM 28-25-00 PB301" }, { "ch": "During refueling, the END Light (Green) flashing: (A, B1, B2)", "ansGr": [ { "ans": [ "The related fuel inlet valve closed when the fuel tank got the set fuel load.", "false" ] }, { "ans": [ "A tank high level sensor has a failure, or a surge tank overflow sensor becomes wet.", "true" ] }, { "ans": [ "The refueling completed, preselected fuel equal the actual fuel quantity.", "false" ] } ], "ref": "Ref: AMM 28-42-00 PB001 And AMM 28-25-00 PB001" }, { "ch": "During ground transfer (A, B1, B2)", "ansGr": [ { "ans": [ "The MODE SELECT to REFUEL, Transfer Valves open, the necessary REFUEL valve OPEN, XFeed valve open", "false" ] }, { "ans": [ "The MODE SELECT to REFUEL, Transfer Valves open, the necessary REFUEL valve OPEN, XFeed valve open and fuel pump is selected ON.", "true" ] }, { "ans": [ "The MODE SELECT to REFUEL, the necessary REFUEL valve OPEN, XFeed valve open and fuel pump is selected ON.", "false" ] } ], "ref": "Ref AMM 28-25-00 PB001" }, { "ch": "Steps to be performed for bleeding of the APU fuel line using FUEL VENT PUSH p/b: (A, B1, B2)", "ansGr": [ { "ans": [ "Do the ground fuel transfer to the trim tank", "false" ] }, { "ans": [ "Push the APU Master SW to ON", "false" ] }, { "ans": [ "Do the ground fuel transfer to the trim tank and then push the FUEL VENT p/b to release the remaining air.", "true" ] } ], "ref": "Ref AMM Task 28-22-00-870-801" }, { "ch": "To make sure that overboard vent lines are not blocked before refueling. (A)", "ansGr": [ { "ans": [ "White X marks remained on surge tanks", "false" ] }, { "ans": [ "White X marks disappeared on surge tanks.", "false" ] }, { "ans": [ "No obstruction on the NACAs intake.", "true" ] } ], "ref": "Ref: Page 392 ATA 28 T1+T2 A330 RR Trent 700" }, { "ch": "Fuel that comes out from the “CTR TK VENTING/DRAINING” drain mast is the indication of: (A, B1, B2)", "ansGr": [ { "ans": [ "Fuel overflow in the Center tank.", "false" ] }, { "ans": [ "Fuel leak in center wing box.", "true" ] }, { "ans": [ "Normal fuel leak. No maintenance action required.", "false" ] } ], "ref": "Ref. Page 392 ATA 28 T1+T2 A330 RR Trent 700" }, { "ch": "THE PURPOSE OF THE TRIM TRANSFER SYSTEM IS TO: (A, B1, B2)", "ansGr": [ { "ans": [ "Burn the fuel from the trim tank.", "false" ] }, { "ans": [ "Control the center of gravity (CG) position.", "true" ] }, { "ans": [ "Control all transfers for engine feed.", "false" ] } ], "ref": "Ref AMM 28-27-00-00 CONF 00 - TRIM TANK TRANSFER SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "The leak measurement solenoid valve is located between the: (A, B1, B2)", "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" ] } ], "part": "ATA 29: HYDRAULIC POWER", "ref": "Ref AMM 29-19-00-00 CONF 00 - GROUND INTERNAL LEAK TEST SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "The two check valves of the air pressure unit are used to: (A, B1, B2)", "ansGr": [ { "ans": [ "Avoid back pressure.", "false" ] }, { "ans": [ "Keep the line pressurized in case of pipe rupture.", "false" ] }, { "ans": [ "Avoid back pressure and keep the line pressurized in case of pipe rupture.", "true" ] } ], "ref": "Ref AMM 29-14-00-00 CONF 00 - HYDRAULIC RESERVOIR PRESSURIZING SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "A check of the alternate parking brake accumulator nitrogen pressure is done with the: (A, B1, B2)", "ansGr": [ { "ans": [ "Accumulator fluid vented to the reservoir.", "true" ] }, { "ans": [ "Accumulator pressurized with fluid.", "false" ] }, { "ans": [ "Reservoir de-pressurized.", "false" ] } ], "ref": "Ref AMM TASK 32-40-00-210-805-A" }, { "ch": "The OFF legend of the GREEN/ENG 1 P/BSW goes off when: (A)", "ansGr": [ { "ans": [ "Pushing on the GREEN/ENG 1 P/BSW.", "true" ] }, { "ans": [ "ENG 1 cranking stops.", "false" ] }, { "ans": [ "Eng 1 N2 is equal to zero.", "false" ] } ], "ref": "Ref AMM 29-11-00-00 CONF 00 - GREEN MAIN HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "Extension of the RAT on ground: (A, B1, B2)", "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 AMM 29-24-00-00 CONF 00 - GREEN AUXILIARY HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "The green hydraulic system high pressure filter system includes: (A, B1, B2)", "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 CONF 00 - GREEN MAIN HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "Which statement is not correct regarding hydraulic reservoir? (A)", "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 TASK 29-11-41-000-801-A" }, { "ch": "The engine 2 hydraulic fire shut off valve can: (A, B1, B2)", "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 AMM 29-13-00-00 CONF 00 - YELLOW MAIN HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "When the A/C is on the ground, a leak measurement solenoid valve can be selected shut to isolate the supply to: (A, B1, B2)", "ansGr": [ { "ans": [ "The flight controls.", "false" ] }, { "ans": [ "The flaps or the slats.", "false" ] }, { "ans": [ "The primary flight controls only.", "true" ] } ], "ref": "Ref AMM 29-19-00-00 CONF 00 - GROUND INTERNAL LEAK TEST SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "The G HP filter and sampling valve are located on the: (A, B1, B2)", "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 29-11-00-00 CONF 00 - GREEN MAIN HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "The yellow electric pump will run during cargo door opening: (A)", "ansGr": [ { "ans": [ "If external power is connected and available.", "true" ] }, { "ans": [ "Only if external power is connected and selected ON.", "false" ] }, { "ans": [ "Only if the yellow electric pump has been selected ON at the hydraulic panel.", "false" ] } ], "ref": "Ref AMM 29-23-00-00 CONF 00 - YELLOW AUXILIARY HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "On the ground during cargo door control: (A)", "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 AMM 29-23-00-00 CONF 00 - YELLOW AUXILIARY HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "Fluid drains into the recovery tanks by: (A)", "ansGr": [ { "ans": [ "An electric pump.", "false" ] }, { "ans": [ "Aircraft speed", "false" ] }, { "ans": [ "Gravity", "true" ] } ], "ref": "Ref AMM 29-17-00-00 CONF 00 - SEAL DRAIN SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "Which statement is correct regarding reservoir pressurizing system? (A)", "ansGr": [ { "ans": [ "The reservoir pressurizing system is supplied in normal operation by high pressure air, bled from engine 1 LP compressor.", "false" ] }, { "ans": [ "The system can also be pressurized through the air-pressurization unit manifold, using air from aircraft bleed air system.", "false" ] }, { "ans": [ "The reservoir pressurizing system is supplied in normal operation by high pressure air, bled from engine 1 LP compressor. The system can also be pressurized through the air-pressurization unit manifold, using air from aircraft bleed air system.", "true" ] } ], "ref": "Ref AMM 29-14-00-00 CONF 00" }, { "ch": "The constant speed motor/generator drains into a tank located in the: (A)", "ansGr": [ { "ans": [ "Yellow hydraulic compartment.", "false" ] }, { "ans": [ "Green hydraulic compartment.", "true" ] }, { "ans": [ "Blue hydraulic compartment.", "false" ] } ], "ref": "Ref AMM 29-17-00-00 CONF 00 - SEAL DRAIN SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "What happens if the hydraulic pressure drops? (A, B1, B2)", "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 - GREEN MAIN HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "Which statement is correct? (A, B1, B2)", "ansGr": [ { "ans": [ "The LP filter, which is installed in the return line below the reservoir, is fitted with a by-pass system and clogging indicator.", "false" ] }, { "ans": [ "Located on the HP manifold, the HP filter is of the non-by-pass type with a clogging indicator.", "false" ] }, { "ans": [ "The LP filter, which is installed in the return line below the reservoir, is fitted with a bypass system and clogging indicator, located on the HP manifold, the HP filter is of the non-by-pass type with a clogging indicator.", "true" ] } ], "ref": "Ref 29-12-00-00 CONF 00 - BLUE MAIN HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "The priority valve: (A, B1, B2)", "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 - GREEN MAIN HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "Which statement is true regarding hydraulic reservoir? (A, B1, B2)", "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": [ "They compensate for variations in fluid volume due to the operation of the user services and to the fluid temperature. They are designed to remain pressurized for at least 24 hours, at ISO temperature", "false" ] } ], "ref": "Ref AMM 29-14-00-00 CONF 00" }, { "ch": "Case drain filter of engine driven pump: (A, B1, B2)", "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 - GREEN MAIN HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "Which statement is correct regarding reservoir filling filter: (A, B1, B2)", "ansGr": [ { "ans": [ "With a bypass device, the filter element is of the replaceable type. It cannot be cleaned.", "false" ] }, { "ans": [ "The clogging indicator is mechanical, a red button comes out to show when the filter element is too dirty.", "true" ] }, { "ans": [ "With a bypass device, the filter element is of the replaceable type. It cannot be cleaned. The clogging indicator is mechanical, a red button comes out to show when the filter element is too dirty.", "false" ] } ], "ref": "Ref AMM 29-16-00-00 CONF 00 - HYDRAULIC RESERVOIR FILLING - DESCRIPTION AND OPERATION" }, { "ch": "The purpose of reservoir pressurizing system: (A, B1, B2)", "ansGr": [ { "ans": [ "The pressurizing system ensures in each hydraulic reservoir an air pressure of 4.5 bars absolute in flight and on ground to avoid cavitations of the pumps on the ground and throughout the whole flight envelope.", "false" ] }, { "ans": [ "It keeps the reservoir sufficiently air-tight in the event of failure of the pressurization system or after an engine shutdown.", "false" ] }, { "ans": [ "The pressurizing system ensures in each hydraulic reservoir an air pressure of 4.5 bars absolute in flight and on ground to avoid cavitations of the pumps on the ground and throughout the whole flight envelope. It keeps the reservoir sufficiently air-tight in the event of failure of the pressurization system or after an engine shutdown.", "true" ] } ], "ref": "Ref 29-14-00-00 CONF 00 - HYDRAULIC RESERVOIR PRESSURIZING SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "You select the leak management valves to? (A, B1, B2)", "ansGr": [ { "ans": [ "Stop the leak of hydraulic to minimize the risk of fire.", "false" ] }, { "ans": [ "Stop movement of the high lift devices during maintenance.", "false" ] }, { "ans": [ "Measure the ground internal leak test system.", "true" ] } ], "ref": "Ref AMM 29-19-00-00 CONF 00 - GROUND INTERNAL LEAK TEST SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "What hydraulic pump can only be controlled manually? (A)", "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 - BLUE AUXILIARY HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "Which of the following components operates only on GND? (A)", "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 - GROUND INTERNAL LEAK TEST SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "RAT can be extended from. (A)", "ansGr": [ { "ans": [ "HYD control panel.", "true" ] }, { "ans": [ "ELEC control panel.", "false" ] }, { "ans": [ "Both HYD control panel and ELEC control panel.", "false" ] } ], "ref": "Ref AMM 29-24-00-00 CONF 00 - GREEN AUXILIARY HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "Hydraulic system Safety Precautions: (A, B1, B2)", "ansGr": [ { "ans": [ "Ensure proper clearance of flight control surfaces and landing gear/ doors during hydraulic system operations.", "false" ] }, { "ans": [ "Do not mix different specifications of hydraulic fluid in the aircraft hydraulic or landing gear systems.", "false" ] }, { "ans": [ "Hydraulic system safety involves maintaining proper clearance for moving components and use the correct type of hydraulic fluid.", "true" ] } ], "ref": "Ref AMM TASK 29-11-41-000-801-A" }, { "ch": "How is the Green system normally pressurized? (A, B1, B2)", "ansGr": [ { "ans": [ "By one electric pump.", "false" ] }, { "ans": [ "By one engine pump and one electric pump.", "false" ] }, { "ans": [ "By two engine pumps.", "true" ] } ], "ref": "Ref AMM 29-11-00-00 CONF 00 - GREEN MAIN HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "The hand pump, which is used for operating the cargo door is located on: (A, B1, B2)", "ansGr": [ { "ans": [ "The Green ground service panel.", "false" ] }, { "ans": [ "The Blue ground service panel.", "false" ] }, { "ans": [ "The Yellow ground service panel.", "true" ] } ], "ref": "Ref AMM 29-23-00-00 CONF 00 - YELLOW AUXILIARY HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "Which hydraulic system supplies the Constant Speed Motor/Generator (CSM/G)? (A, B1, B2)", "ansGr": [ { "ans": [ "Blue system.", "false" ] }, { "ans": [ "Yellow system.", "false" ] }, { "ans": [ "Green system.", "true" ] } ], "ref": "Ref AMM 29-24-00-00 CONF 00 - GREEN AUXILIARY HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "The telescopic lever for operate the cargo door hand pump can be found at (A, B1, B2)", "ansGr": [ { "ans": [ "The Blue ground service panel.", "false" ] }, { "ans": [ "The Green ground service panel.", "true" ] }, { "ans": [ "The Yellow ground service panel.", "false" ] } ] }, { "ch": "The Ram Air Turbine (RAT) is a variable pitch, two blade unit located in (A, B1, B2)", "ansGr": [ { "ans": [ "In the LH belly fairing.", "false" ] }, { "ans": [ "The number 4 flap track fairing on the right wing.", "true" ] }, { "ans": [ "The number 4 flap track fairing on the left wing.", "false" ] } ], "ref": "Ref AMM 29-24-00-00 CONF 00 - GREEN AUXILIARY HYDRAULIC POWER - DESCRIPTION AND OPERATION" }, { "ch": "Each wiper is controlled: (A)", "ansGr": [ { "ans": [ "By a two-position rotary selector.", "false" ] }, { "ans": [ "By a P/B.", "false" ] }, { "ans": [ "By a three-position rotary selector.", "true" ] } ], "part": "ATA 30: ICE & RAIN PROTECTION", "ref": "Ref AMM 30-45-00-00 CONF 01 - WINDSHIELD RAIN PROTECTION - DESCRIPTION AND OPERATION" }, { "ch": "The rain repellent system is inhibited: (A)", "ansGr": [ { "ans": [ "On ground when the engines are shut down.", "false" ] }, { "ans": [ "During take-off and landing.", "false" ] }, { "ans": [ "On ground.", "true" ] } ], "ref": "Ref AMM 30-45-00-00 CONF 01 - WINDSHIELD RAIN PROTECTION - DESCRIPTION AND OPERATION" }, { "ch": "The water ice protection system is controlled: (A, B1, B2)", "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 - POTABLE WATER ICE PROTECTION - DESCRIPTION AND OPERATION" }, { "ch": "Escape slide locking mechanism are electrically heated: (A)", "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 - ESCAPE SLIDE LOCKING MECHANISM ICE PROTECTION - DESCRIPTION AND OPERATION" }, { "ch": "The two water ice protection control units (IPCUs) are located: (A, B1, B2)", "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 - POTABLE WATER ICE PROTECTION - DESCRIPTION AND OPERATION" }, { "ch": "How many wing anti-ice valve on each wing: (A )", "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 - WING ICE PROTECTION - DESCRIPTION AND OPERATION" }, { "ch": "How can you display SD (System Display) image in case of the SD unit fault or set to off? (A)", "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" ] } ], "part": "ATA 31: INDICATING/RECORDING SYSTEMS", "ref": "Ref AMM 31-67-00-00 CONF 00 - SYSTEM DISPLAY (SD) - DESCRIPTION AND OPERATION" }, { "ch": "The STATUS message: (A)", "ansGr": [ { "ans": [ "Can be left unrectified until the next C check.", "false" ] }, { "ans": [ "Has to be rectified before dispatched.", "false" ] }, { "ans": [ "Is “GO” item.", "true" ] } ], "ref": "Ref AMM 31-51-00-00 CONF 00 - FLIGHT WARNING SYSTEM (FWS) OPERATIONAL USE - DESCRIPTION AND OPERATION" }, { "ch": "Class 1 faults displayed on the PFR are: (A)", "ansGr": [ { "ans": [ "NO GO items.", "false" ] }, { "ans": [ "GO IF items.", "false" ] }, { "ans": [ "NO Go or Go If Items.", "true" ] } ], "ref": "Ref AMM 31-51-00-00 CONF 00 - FLIGHT WARNING SYSTEM (FWS) OPERATIONAL USE - DESCRIPTION AND OPERATION" }, { "ch": "Classification of a fault can be found. (A)", "ansGr": [ { "ans": [ "On ECAM upper page.", "false" ] }, { "ans": [ "On the STS page.", "false" ] }, { "ans": [ "In the PFR.", "true" ] } ], "ref": "Ref AMM 31-51-00-00 CONF 00 - FLIGHT WARNING SYSTEM (FWS) OPERATIONAL USE - DESCRIPTION AND OPERATION" }, { "ch": "What happening when we trip a circuit breaker (A,B2):", "ansGr": [ { "ans": [ "There is message “C/B TRIPPED” on Upper ECAM Display.", "false" ] }, { "ans": [ "The tripped circuit breaker will be indicated in C/B Page.", "true" ] }, { "ans": [ "The tripped circuit breaker will be indicated in C/B Page if it is a green C/B.", "false" ] } ], "ref": "Ref AMM 31-67-24-00 CONF 00 - SD - ELEC AC, ELEC DC & C/B PAGES - DESCRIPTION AND OPERATION" }, { "ch": "What is the function of ENG detent of mode selector switch on EFIS Control Panel (A,B2):", "ansGr": [ { "ans": [ "To indicate Engine Warning Display (EWD) on ND.", "false" ] }, { "ans": [ "To indicate Engine Standby Page on ND instead of NAV Page after failure of all the ECAM parts of the DMCs of the EIS.", "true" ] }, { "ans": [ "To indicate Engine Warning Display (EWD) on PFD.", "false" ] } ], "ref": "Ref AMM 31-65-00-00 CONF 00 - NAVIGATION DISPLAY (ND) - DESCRIPTION AND OPERATION" }, { "ch": "IF THERE IS NO C/B OPEN, ON THE ECAM C/B PAGE (A, B1, B2)", "ansGr": [ { "ans": [ "Message “NOT AVAIL” comes on", "false" ] }, { "ans": [ "A message “NORMAL” appear in green", "true" ] }, { "ans": [ "No message longer appears.", "false" ] } ], "ref": "Ref AMM 31-67-24-00 CONF 00 - SD - ELEC AC, ELEC DC & C/B PAGES - DESCRIPTION AND OPERATION" }, { "ch": "Changeover valve is used to isolate leak on. (A)", "ansGr": [ { "ans": [ "NLG shock absorber", "false" ] }, { "ans": [ "MLG shock absorber", "false" ] }, { "ans": [ "Both NLG & MLG shock absorbers", "true" ] } ], "part": "ATA 32: LANDING GEAR", "ref": "Ref 32-31-00-00 CONF 00 - NORMAL EXTENSION AND RETRACTION - DESCRIPTION AND OPERATION" }, { "ch": "To have a brake INOP, MEL requires the Green and Blue brake systems associated with operative brakes are operative, it means? (A, B1, B2)", "ansGr": [ { "ans": [ "All the Green hydraulic pumps are operative", "false" ] }, { "ans": [ "All the Blue hydraulic pumps are operative", "false" ] }, { "ans": [ "The green and blue brake systems associated with the operative brakes are operative. The tachometers associated with the operative brakes are operative. The affected brake is deactivated or removed. The Flight Manual performance penalties are applied", "true" ] } ], "ref": "Ref Mel 32-41-01" }, { "ch": "How is the brake unit attached to the MLG axle? (A)", "ansGr": [ { "ans": [ "By the brake rod and torque pin", "true" ] }, { "ans": [ "By bolts located around the brake unit", "false" ] }, { "ans": [ "By the torque pin and bolts located around the brake unit.", "false" ] } ], "ref": "Ref AMM TASK 32-42-27-000/400-801-A" }, { "ch": "How do you set the parking brake during main wheel replacement? (A)", "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 TASK 32-41-11-000/400-801-A" }, { "ch": "For wheel replacement, can you lift the two axles of the bogie beam of the same MLG at the same time? (A)", "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 TASK 32-41-11-000/400-801-A" }, { "ch": "What is permissible during jacking for main LDG wheel change? (A)", "ansGr": [ { "ans": [ "Cargo, PAX loading.", "false" ] }, { "ans": [ "Gate docking.", "false" ] }, { "ans": [ "Install the safety devices on the landing gear", "true" ] } ], "ref": "Ref AMM TASK 32-41-11-000/400-801-A" }, { "ch": "The Parking brake is effective? (A, B1, B2)", "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 TASK 32-41-11-000/400-801-A" }, { "ch": "What do you do if you see the red light on the Electric Box at NLG comes on during towing? (A)", "ansGr": [ { "ans": [ "Parking brake is ON, you cannot tow the aircraft.", "false" ] }, { "ans": [ "Not further towing allowed.", "true" ] }, { "ans": [ "Parking brake pressure is low, you are not allowed to tow aircraft.", "false" ] } ], "ref": "Ref AMM TASK 09-10-00-584-802-A" }, { "ch": "What you do if you found the aircraft had rolled out with main wheel # 3 deflated? (A)", "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 TASK 09-10-00-584-807-A" }, { "ch": "Wheels mixability precaution is applied for? (A)", "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 TASK 32-41-00-200-802-A" }, { "ch": "Excessive shoulders wear of the tire is the indication of: (A)", "ansGr": [ { "ans": [ "Too much operation on wet runway.", "false" ] }, { "ans": [ "Underinflated.", "true" ] }, { "ans": [ "Overinflated.", "false" ] } ], "ref": "Ref AMM TASK 32-41-00-210-803-A" }, { "ch": "You will have to remove the wheel? (A)", "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 TASK 32-41-00-210-803-A" }, { "ch": "When installing the main wheel, you torque? (A)", "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 TASK 32-41-11-000/400-801-A" }, { "ch": "When remove the wheel, do you need to deflate the tire? (A)", "ansGr": [ { "ans": [ "No need if you remove for access or inspections only.", "true" ] }, { "ans": [ "Only if you find the wheel tie bolt is missing, broken or loosen.", "false" ] }, { "ans": [ "Only if the tire is damaged that it may exploded.", "false" ] } ], "ref": "Ref AMM TASK 32-41-11-000/400-801-A" }, { "ch": "What do you NOT have to do before installing the main wheel? (A)", "ansGr": [ { "ans": [ "Check tire mixability.", "false" ] }, { "ans": [ "Inspect the brake unit.", "false" ] }, { "ans": [ "Remove the Guide Cone - Wheel.", "true" ] } ], "ref": "Ref AMM TASK 32-41-11-000/400-801-A" }, { "ch": "The Axe Thread Protector is used during: (A)", "ansGr": [ { "ans": [ "Wheel removal.", "false" ] }, { "ans": [ "Wheel installation.", "false" ] }, { "ans": [ "Wheel removal and installation.", "true" ] } ], "ref": "Ref AMM TASK 32-41-11-000/400-801-A" }, { "ch": "What statement is NOT true: Brake unit is considered defective when? (A)", "ansGr": [ { "ans": [ "Leakage found on any piston.", "false" ] }, { "ans": [ "Wearing pin is longer than a certain value.", "false" ] }, { "ans": [ "A wear pin is missing.", "true" ] } ], "ref": "Ref AMM TASK 32-42-00-200-801-A" }, { "ch": "What you do if you found one wear indicator pin on a brake unit is missing? (A)", "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 TASK 32-42-00-200-801-A" }, { "ch": "When TORQUE the axle nut during installation of the main wheel? (A)", "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 TASK 32-41-11-000/400-801-A" }, { "ch": "During wheel installation, after applying the required final torque value, if the axle nut slots still do not align with the bolt holes in the axle, what do you do? (A)", "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 TASK 32-41-11-000/400-801-A" }, { "ch": "Landing gear safety pins shall be installed on landing gears: (A)", "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 TASK 32-41-11-000/400-801-A" }, { "ch": "You open the LDG doors on GND with? (A, B1, B2)", "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 TASK 32-22-00-010-801-A" }, { "ch": "The brake triple indicator needles are not moving during. (A)", "ansGr": [ { "ans": [ "Normal brake.", "true" ] }, { "ans": [ "Alternate brake.", "false" ] }, { "ans": [ "Parking brake.", "false" ] } ], "ref": "Ref AMM 32-42-00-00 CONF 00 - NORMAL BRAKING - DESCRIPTION AND OPERATION" }, { "ch": "When you bleed the brake system at the brake unit ? (A)", "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 TASK 32-42-27-000/400-801-A" }, { "ch": "What do you NOT have to do before installing the main wheel brake? (A)", "ansGr": [ { "ans": [ "Remove the axle sleeves.", "true" ] }, { "ans": [ "Grease the axle sleeves.", "false" ] }, { "ans": [ "Make sure that the Guide Cone – Brake is removed.", "false" ] } ], "ref": "Ref AMM TASK 32-42-27-000/400-801-A" }, { "ch": "During the main wheel brake replacement, the brake torque pin? (A)", "ansGr": [ { "ans": [ "Need to be NDT checked for crack before use if new part is not available", "false" ] }, { "ans": [ "Need to be attached with the removed brake unit and sent back to store", "false" ] }, { "ans": [ "Need to be NDT checked for crack before use if new part is not available and to be attached with removed brake unit and set back to store.", "true" ] } ], "ref": "Ref AMM TASK 32-42-27-000/400-801-A" }, { "ch": "What is correct regarding greasing during replacement of brake unit? (A)", "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": [ "Apply grease on Axle sleeves only.", "false" ] } ], "ref": "Ref AMM TASK 32-42-27-000/400-801-A" }, { "ch": "The Red warning light on Electric Box 8GH comes on when:", "ansGr": [ { "ans": [ "An excess angular 93-degree travel of the NLG steering during towing operations.", "true" ] }, { "ans": [ "An excess angular 90-degree travel of the NLG steering during towing operations.", "false" ] }, { "ans": [ "To indicate Parking brake applying.", "false" ] } ], "ref": "Ref AMM 32-53-00-00 CONF 00 - NOSE LANDING GEAR - STEERING ANGLE PROTECTION - DESCRIPTION AND OPERATION" }, { "ch": "Which hydraulic system powers the nose wheel steering? (A, B1, B2)", "ansGr": [ { "ans": [ "Green system.", "true" ] }, { "ans": [ "Blue system.", "false" ] }, { "ans": [ "Yellow system.", "false" ] } ], "ref": "Ref AMM 32-50-00-00 CONF 00 - STEERING - DESCRIPTION AND OPERATION" }, { "ch": "When cockpit door is opened and the engine is running, the forward LH entrance light intensity is: (A)", "ansGr": [ { "ans": [ "Dimmed to 50%", "false" ] }, { "ans": [ "Dimmed to 10%", "true" ] }, { "ans": [ "Normal", "false" ] } ], "part": "ATA 33: LIGHTS", "ref": "Ref AMM 33-21-00-00 CONF 00 - GENERAL ILLUMINATION - DESCRIPTION AND OPERATION" }, { "ch": "In abnormal configuration such as either rapid cabin decompression or a total CIDS failure, the cabin lights: (A)", "ansGr": [ { "ans": [ "Up to 100%", "true" ] }, { "ans": [ "Up to 50%", "false" ] }, { "ans": [ "Up to 10%", "false" ] } ], "ref": "Ref AMM 33-25-00-00 CONF 00 - PASSENGER AND CABIN ATTENDANT LIGHTS - DESCRIPTION AND OPERATION" }, { "ch": "You turn ON the engine scan lights when the MID PAX L/H or R/H DOOR opened, the corresponding engine scan light still ON: (A)", "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 - WING AND ENGINE SCAN LIGHTING - DESCRIPTION AND OPERATION" }, { "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? (A)", "ansGr": [ { "ans": [ "The dome lights still on", "true" ] }, { "ans": [ "The doom light off", "false" ] }, { "ans": [ "The doom light dim to 10%", "false" ] } ], "ref": "Ref AMM 33-12-00-00 CONF 00 - GENERAL ILLUMINATION - DESCRIPTION AND OPERATION" }, { "ch": "What is the difference between the STORM and BRT position of dome light switch 5LE? (A)", "ansGr": [ { "ans": [ "When the switch is in the BRT position, the doom light has 90% brightness.", "false" ] }, { "ans": [ "When the switch is in the STORM position, the doom light has 90% brightness.", "false" ] }, { "ans": [ "The brightness of the dome lights are the same when the switch is in the STORM position or in the BRT position.", "true" ] } ], "ref": "Ref AMM 33-12-00-00 CONF 00 - GENERAL ILLUMINATION - DESCRIPTION AND OPERATION" }, { "ch": "In storm conditions, with interior dome light switch in STORM position, what is the brightness of flood lighting? (A)", "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 - GENERAL ILLUMINATION - DESCRIPTION AND OPERATION" }, { "ch": "When lavatory doors are closed and locked: (A)", "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 - LAVATORY LIGHTING - DESCRIPTION AND OPERATION" }, { "ch": "When do the landing lights come on? (A)", "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 - LANDING LIGHTS - DESCRIPTION AND OPERATION" }, { "ch": "The condition for the Runway Turn Off lights come ON is: (A)", "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 - RUNWAY TURNOFF LIGHTS - DESCRIPTION AND OPERATION" }, { "ch": "Where can you control the CAB Emergency lighting? (A)", "ansGr": [ { "ans": [ "From the Switch in the cockpit.", "false" ] }, { "ans": [ "From the EMER push button on the FAP.", "false" ] }, { "ans": [ "From the Switch in the cockpit and the EMER P/B on the FAP.", "true" ] } ], "ref": "Ref AMM 33-51-00-00 CONF 00 - CABIN EMERGENCY LIGHTING - DESCRIPTION AND OPERATION" }, { "ch": "If the power from the DC essential bus bar is not available, how long can EPSU supply the power to emergency lights: (A , B1, B2)", "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 - CABIN EMERGENCY LIGHTING - DESCRIPTION AND OPERATION" }, { "ch": "When strobe lights selector is set to ON position, strobe lights will flash: (A)", "ansGr": [ { "ans": [ "If shock absorber is not compressed", "false" ] }, { "ans": [ "Always", "true" ] }, { "ans": [ "If shock absorber is extended", "false" ] } ], "ref": "Ref AMM 33-48-00-00 CONF 00 - ANTI-COLLISION/STROBE LIGHTING - DESCRIPTION AND OPERATION" }, { "ch": "The whole cabin lighting is controlled from: (A)", "ansGr": [ { "ans": [ "The Circuit Breaker panel 2000 VU.", "false" ] }, { "ans": [ "The CIDS FAP only.", "true" ] }, { "ans": [ "Any attendant station", "false" ] } ], "ref": "Ref AMM 33-25-00-00 CONF 00 - PASSENGER AND CABIN ATTENDANT LIGHTS - DESCRIPTION AND OPERATION" }, { "ch": "Emergency lights are supplied from the EPSU batteries when: (A,B2)", "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 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 - CABIN EMERGENCY LIGHTING - DESCRIPTION AND OPERATION" }, { "ch": "If the both FMGECs have failed, the third RMP: (A, B1, B2)", "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" ] } ], "part": "ATA 34: NAVIGATION", "ref": "Ref AMM 34-53-00-00 CONF 01 - ADF - DESCRIPTION AND OPERATION" }, { "ch": "ILS 1 DATA is displayed on the: (A, B1, B2)", "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 01 - INSTRUMENT LANDING SYSTEM (ILS) (MULTI MODE RECEIVER (MMR) - INCLUDING GPS OR THE DIGITAL GLOBAL POSITIONING SYSTEM (DGPS) FUNCTION) - DESCRIPTION AND OPERATION" }, { "ch": "The function of 2 GPS antennas are: (A, B1, B2)", "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 01 - INSTRUMENT LANDING SYSTEM (ILS) (MULTI MODE RECEIVER (MMR) - INCLUDING GPS OR THE DIGITAL GLOBAL POSITIONING SYSTEM (DGPS) FUNCTION) - DESCRIPTION AND OPERATION" }, { "ch": "The Multi-Mode Receiver (MMR) system is composed of an Instrument Landing System (ILS) and: (A, B1, B2)", "ansGr": [ { "ans": [ "A Global Positioning System (GPS).", "true" ] }, { "ans": [ "A Radio Altimeter (RA).", "false" ] }, { "ans": [ "A GPS and RA", "false" ] } ], "ref": "Ref AMM 34-36-00-00 CONF 01 - INSTRUMENT LANDING SYSTEM (ILS) (MULTI MODE RECEIVER (MMR) - INCLUDING GPS OR THE DIGITAL GLOBAL POSITIONING SYSTEM (DGPS) FUNCTION) - DESCRIPTION AND OPERATION" }, { "ch": "Radio Height is displayed on the PFD: (A, B1, B2)", "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 - RADIO ALTIMETER (RA) - DESCRIPTION AND OPERATION" }, { "ch": "The flight crew oxygen system give protection for flight crew members in case of: (A)", "ansGr": [ { "ans": [ "Loss of cabin pressure altitude.", "false" ] }, { "ans": [ "Smoke or toxic gas release.", "false" ] }, { "ans": [ "Loss of cabin pressure altitude, smoke or toxic gas release.", "true" ] } ], "part": "ATA 35: OXYGEN", "ref": "Ref AMM 35-10-00-00 CONF 00 - CREW OXYGEN - DESCRIPTION AND OPERATION" }, { "ch": "The flight crew system consists of: (A)", "ansGr": [ { "ans": [ "The oxygen storage,", "false" ] }, { "ans": [ "The oxygen distribution, control and indicating", "false" ] }, { "ans": [ "The oxygen storage and oxygen distribution, control and indicating.", "true" ] } ], "ref": "Ref AMM 35-10-00-00 CONF 00 - CREW OXYGEN - DESCRIPTION AND OPERATION" }, { "ch": "When working on gaseous oxygen system, you must: (A, B1, B2)", "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 TASK 35-00-00-860-801-A" }, { "ch": "The CKPT OXY indication in amber on ECAM DOOR/OXY page when: (A)", "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 400 PSI or regulated low pressure.", "true" ] } ], "ref": "Ref AMM 35-10-00-00 CONF 00 - CREW OXYGEN - DESCRIPTION AND OPERATION" }, { "ch": "Numerical value (in PSI) for oxygen high pressure indicates in cross amber when: (A, B1, B2)", "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 35-10-00-00 CONF 00 - CREW OXYGEN - DESCRIPTION AND OPERATION" }, { "ch": "When visual inspection PBE in cockpit you found vacuum sealed bag is inflated: (A)", "ansGr": [ { "ans": [ "This is serviceable one, if date of overhaul is not due,", "false" ] }, { "ans": [ "You must replace it by new one.", "false" ] }, { "ans": [ "You can defer defect refer MEL if spare not available", "true" ] } ], "ref": "Ref AMM 35-32-00-00 CONF 00 - CABIN ATTENDANTS PORTABLE DEVICES - DESCRIPTION AND OPERATION" }, { "ch": "Before remove the crew oxygen cylinder, you must do: (A, B1, B2)", "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 TASK 35-11-41-750-801-A" }, { "ch": "When the CREW SUPPLY push button is pushed in and oxygen high pressure equal or more than 600psi . Indication of oxy high pressure on ECAM DOOR/OXY page is: (A, B1, B2)", "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 35-10-00-00 CONF 00 - CREW OXYGEN - DESCRIPTION AND OPERATION" }, { "ch": "The passenger emergency-oxygen is stored in oxygen containers, and which have: (A)", "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 35-20-00-00 CONF 00 - PASSENGER OXYGEN - DESCRIPTION AND OPERATION" }, { "ch": "In automatic mode, the cross bleed valve: (A, B1, B2)", "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" ] } ], "part": "ATA 36: PNEUMATIC SYSTEM", "ref": "Ref AMM 36-12-00-00 CONF 00 - APU BLEED AIR SUPPLY AND CROSSBLEED SYSTEMS - DESCRIPTION AND OPERATION" }, { "ch": "When selected, APU bleed air: (A)", "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 AMM 36-12-00-00 CONF 00 - APU BLEED AIR SUPPLY AND CROSSBLEED SYSTEMS - DESCRIPTION AND OPERATION" }, { "ch": "Each engine bleed system is designed to: (A)", "ansGr": [ { "ans": [ "Select one of the two compressor stages of the engine HP compressor in agreement with the supplied Pressure", "false" ] }, { "ans": [ " Regulate bleed air pressure to prevent overpressure, regulate bleed air temperature to prevent overtemperature", "false" ] }, { "ans": [ "  Select one of the two compressor stages of the engine HP compressor in agreement with the supplied Pressure and regulate bleed air pressure to prevent overpressure, regulate bleed air temperature to prevent overtemperature", "true" ] } ] }, { "ch": "When engine anti-ice and wing anti-ice are in use, and a BMC detects a bleed leak: (A, B1, B2)", "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 36-11-00-00 CONF 22 - ENGINE BLEED AIR SUPPLY SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "Air leakage detection is based on: (A, B1, B2)", "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 01 - LEAK DETECTION HF - DESCRIPTION AND OPERATION" }, { "ch": "If one BMC fails, the remaining BMC takes over the monitoring of the bleed system to issue the following ECAM warnings: (A, B1, B2)", "ansGr": [ { "ans": [ "  Overpressure detection, Over temperature detection", "false" ] }, { "ans": [ "  Leak on pylon detection, wing leak detection", "false" ] }, { "ans": [ "  Overpressure detection, over temperature detection, leak on pylon detection, wing leak detection.", "true" ] } ], "ref": "Ref AMM 36-22-00-00 CONF 01 - LEAK DETECTION HF - DESCRIPTION AND OPERATION" }, { "ch": "On ECAM bleed page: when is the GND symbol displayed? (A)", "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 AMM 36-13-00-00 CONF 00 - GROUND COMPRESSED AIR SUPPLY SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "In case of PRV (Pressure Regulating Valve) is controlled to close: (A, B1, B2)", "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 36-10-00-00 CONF 00 - DISTRIBUTION - DESCRIPTION AND OPERATION" }, { "ch": "The pressure regulation of the engine bleed air is performed by (A, B1, B2)", "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 AMM 36-10-00-00 CONF 00 - DISTRIBUTION - DESCRIPTION AND OPERATION" }, { "ch": "When start the right engine using ground air supply:(A, B1, B2)", "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 - APU BLEED AIR SUPPLY AND CROSSBLEED SYSTEMS - DESCRIPTION AND OPERATION" }, { "ch": "In normal condition, if both engine and APU bleed sources are selected ON, what will supply to the packs? (A )", "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 - APU BLEED AIR SUPPLY AND CROSSBLEED SYSTEMS - DESCRIPTION AND OPERATION" }, { "ch": "From the Cockpit, how can you know that the HP pneumatic GND cart is connected to the A/C?: (A, B1, B2)", "ansGr": [ { "ans": [ "The only way is to confirm with GND staff.", "true" ] }, { "ans": [ "Check the “GND” indication on the ECAM BLEED page.", "false" ] }, { "ans": [ "Check the “GND” indication on the control panel.", "false" ] } ], "ref": "Ref AMM 36-13-00-00 CONF 00 - GROUND COMPRESSED AIR SUPPLY SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "The potable water system can be serviced: (A, B1, B2)", "ansGr": [ { "ans": [ "With electrical power.", "false" ] }, { "ans": [ "Without electrical power.", "false" ] }, { "ans": [ "With electrical power and without electrical power.", "true" ] } ], "part": "ATA 38: WATER/WASTE", "ref": "Ref AMM 12-15-38-613-801-A & AMM 12-15-38-613-802-A" }, { "ch": "In flight, the portable water system is pressurized by. (A, B1, B2)", "ansGr": [ { "ans": [ "The pressurized air comes from the bleed air system.", "true" ] }, { "ans": [ "The ground air pressure supply system or a compressor is installed (optional).", "false" ] }, { "ans": [ "Air compressor.", "false" ] } ], "ref": "Ref AMM 38-10-00-614-801-A" }, { "ch": "Waste water from the lavatories and galleys is: (A, B1, B2)", "ansGr": [ { "ans": [ "Drained overboard via two heated drain masts.", "true" ] }, { "ans": [ "Drained to the waste tank.", "false" ] }, { "ans": [ "Used for rinsing the toilet.", "false" ] } ], "ref": "Ref AMM 38-32-00-00 CONF 00 - WASTE WATER DRAIN - DESCRIPTION AND OPERATION" }, { "ch": "How can a leak in a lavatory be isolated? (A, B1, B2)", "ansGr": [ { "ans": [ "By depressurizing the water tank.", "false" ] }, { "ans": [ "By setting the manual water shut-off valve of the lavatory to the closed position.", "true" ] }, { "ans": [ "The Vacuum System Controller will open the filling line drain valve automatically.", "false" ] } ], "ref": "Ref AMM 38-31-00-040-801-A" }, { "ch": "How many water service and drain panels are fitted on the aircraft? (A, B1, B2)", "ansGr": [ { "ans": [ "One.", "false" ] }, { "ans": [ "Two.", "false" ] }, { "ans": [ "Three.", "true" ] } ], "ref": "Ref AMM 38-10-00-00 CONF 00 - POTABLE - DESCRIPTION AND OPERATION" }, { "ch": "Which service panels are used to drain the water system? (A, B1, B2)", "ansGr": [ { "ans": [ "Forward and Aft water drain panels", "false" ] }, { "ans": [ "Portable water service panel.", "false" ] }, { "ans": [ "Forward and aft water drain panels, portable water service panel.", "true" ] } ], "ref": "Ref AMM 38-10-00-00 CONF 00 - POTABLE - DESCRIPTION AND OPERATION" }, { "ch": "Can preselection keys are used to preselect the water quantity during refilling (A, B1, B2)", "ansGr": [ { "ans": [ "No, preselection of water quantity is only available when the water service panel door is closed", "true" ] }, { "ans": [ "No, in this case you must select the water quantity only at the water service panel", "false" ] }, { "ans": [ "Yes, it doesn’t matter", "false" ] } ], "ref": "Ref AMM 38-10-00-00 CONF 00 - POTABLE - DESCRIPTION AND OPERATION" }, { "ch": "When the water quantity has reached the preselected level, control unit automatic: (A, B1, B2)", "ansGr": [ { "ans": [ "Closes the fill/drain/overflow valve in the corresponding tank.", "true" ] }, { "ans": [ "Closes the shut off valve in the corresponding tank.", "false" ] }, { "ans": [ "Open the fill/drain/overflow valve in the corresponding tank.", "false" ] } ], "ref": "Ref AMM 38-10-00-00 CONF 00 - POTABLE - DESCRIPTION AND OPERATION" }, { "ch": "The pressurization of the potable water tanks is achieved by: (A, B1, B2)", "ansGr": [ { "ans": [ "The aircraft pneumatic system only.", "false" ] }, { "ans": [ "The compressor only.", "false" ] }, { "ans": [ "The aircraft pneumatic system or a ground air pressure supply.", "true" ] } ], "ref": "Ref AMM 38-10-00-00 CONF 00 - POTABLE - DESCRIPTION AND OPERATION" }, { "ch": "From which sources are the water tanks normally pressurized in flight? (A, B1, B2)", "ansGr": [ { "ans": [ "The aircraft pneumatic system.", "true" ] }, { "ans": [ "An optional electrical compressor.", "false" ] }, { "ans": [ "The water service panel.", "false" ] } ], "ref": "Ref AMM 38-10-00-00 CONF 00 - POTABLE - DESCRIPTION AND OPERATION" }, { "ch": "Water heater is automatically switch off in case of: (A, B1, B2)", "ansGr": [ { "ans": [ "Low level quantity in the heater", "false" ] }, { "ans": [ "Low inlet line pressure", "false" ] }, { "ans": [ "Low level quantity in the heater and low inlet line pressure.", "true" ] } ], "ref": "Ref AMM 38-31-00-00 CONF 00 - TOILET SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "Waste water disposal is achieved in flight. (A, B1, B2)", "ansGr": [ { "ans": [ "By gravity.", "false" ] }, { "ans": [ "By differential pressure.", "false" ] }, { "ans": [ "By differential pressure and gravity action.", "true" ] } ], "ref": "Ref AMM 38-32-00-00 CONF 00 - WASTE WATER DRAIN - DESCRIPTION AND OPERATION" }, { "ch": "Waste water disposal is achieved on ground. (A, B1, B2)", "ansGr": [ { "ans": [ "By gravity.", "true" ] }, { "ans": [ "By differential pressure.", "false" ] }, { "ans": [ "By differential pressure and gravity action.", "false" ] } ], "ref": "Ref AMM 38-32-00-00 CONF 00 - WASTE WATER DRAIN - DESCRIPTION AND OPERATION" }, { "ch": "The waste water Drain Masts are electrically heated (A, B1, B2)", "ansGr": [ { "ans": [ "On ground only.", "false" ] }, { "ans": [ "In flight only.", "false" ] }, { "ans": [ "On ground and in flight.", "true" ] } ], "ref": "Ref AMM 38-32-00-00 CONF 00 - WASTE WATER DRAIN - DESCRIPTION AND OPERATION" }, { "ch": "How is the complete toilet system monitored? (A, B1, B2)", "ansGr": [ { "ans": [ "By a Vacuum System Controller.", "true" ] }, { "ans": [ "By a Vacuum Generator.", "false" ] }, { "ans": [ "By a Flush Control Unit.", "false" ] } ], "ref": "Ref AMM 38-31-00-00 CONF 00 - TOILET SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "For flushing of the toilet systems, which source water come from (A, B1, B2)", "ansGr": [ { "ans": [ "Waste water of the lavatories and galleys", "false" ] }, { "ans": [ "Potable water system.", "true" ] }, { "ans": [ "Waste water of lavatories and portable system.", "false" ] } ], "ref": "Ref AMM 38-31-00-00 CONF 00 - TOILET SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "Toilet operation is sequenced by (A, B1, B2)", "ansGr": [ { "ans": [ "A Flush Control Unit.", "true" ] }, { "ans": [ "A Vacuum System Controller.", "false" ] }, { "ans": [ "A Vacuum Generator.", "false" ] } ], "ref": "Ref AMM 38-31-00-00 CONF 00 - TOILET SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "When does the vacuum generator run? (A, B1, B2)", "ansGr": [ { "ans": [ "On ground only.", "false" ] }, { "ans": [ "On ground and at low altitude", "true" ] }, { "ans": [ "In flight only.", "false" ] } ], "ref": "Ref AMM 38-31-00-00 CONF 00 - TOILET SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "The vacuum generators generate the necessary vacuum: (A, B1, B2)", "ansGr": [ { "ans": [ "To drain the waste tanks.", "false" ] }, { "ans": [ "When the differential pressure between cabin and atmosphere is insufficient.", "true" ] }, { "ans": [ "All the time.", "false" ] } ], "ref": "Ref AMM 38-31-00-00 CONF 00 - TOILET SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "How is the waste material transported to the Waste Holding tank? (A, B1, B2)", "ansGr": [ { "ans": [ "By the vacuum created inside the tank.", "true" ] }, { "ans": [ "By water flushing and gravity effect.", "false" ] }, { "ans": [ "By water pressure action.", "false" ] } ], "ref": "Ref AMM 38-31-00-00 CONF 00 - TOILET SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "To rinse the toilet bowl and facilitate evacuation of waste during the Flush Cycle, the system uses (A, B1, B2).", "ansGr": [ { "ans": [ "Waste water from galley.", "false" ] }, { "ans": [ "Waste water from lavatory.", "false" ] }, { "ans": [ "Fresh water from the potable water system.", "true" ] } ], "ref": "Ref AMM 38-31-00-00 CONF 00 - TOILET SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "Can you work on the toilet waste system and the portable system at the same time? (A, B1.B2)", "ansGr": [ { "ans": [ "Yes, the two systems are independent.", "false" ] }, { "ans": [ "No, it can cause the contamination to the portable water system", "true" ] }, { "ans": [ "Yes, water from portable water system will flow to waste system", "false" ] } ], "ref": "Ref AMM 38-31-00-00 CONF 00 - TOILET SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "Can you set the water quantity at FAP 120 RH at any time ? (A, B1.B2)", "ansGr": [ { "ans": [ "Only when PWSP access door 164 AR is closed", "false" ] }, { "ans": [ "Only when PWSP access door 164 AR is opened", "false" ] }, { "ans": [ "Only when A/C is energized and PWSP access door 164AR is closed.", "true" ] } ], "ref": "Ref AMM 38-13-00-00 CONF 00 - QUANTITY INDICATING - DESCRIPTION AND OPERATION" }, { "ch": "When you push preselection key on FAP 120RH, (A, B1, B2)", "ansGr": [ { "ans": [ "The preselection value for two portable water tanks is made at the same time.", "true" ] }, { "ans": [ "The first time is for tank 1 and the second time is for tank 2.", "false" ] }, { "ans": [ "The first time is for tank 2 and the second time is for tank 1.", "false" ] } ], "ref": "Ref AMM 38-13-00-00 CONF 00 - QUANTITY INDICATING - DESCRIPTION AND OPERATION" }, { "ch": "When water from faucet in LAV cannot stop, what should you do? (A, B1, B2)", "ansGr": [ { "ans": [ "You can disconnect the water line from the faucet and INOP the LAV.", "false" ] }, { "ans": [ "Let the water flow because it flows small water.", "false" ] }, { "ans": [ "Close the SOV and deactivate the LAV.", "true" ] } ], "ref": "Ref AMM 38-31-00-040-801-A" }, { "ch": "When water form faucet in LAV cannot stop and we close the SOV (A, B1, B2)", "ansGr": [ { "ans": [ "Water flows from faucet stop so we can use toilet in that LAV normally.", "false" ] }, { "ans": [ "All the water supply to that LAV stops and the LAV is considered inoperative.", "true" ] }, { "ans": [ "Water stops flowing to faucet and still supply to toilet line.", "false" ] } ], "ref": "Ref AMM 38-31-00-040-801-A" }, { "ch": "What is aircraft configuration to refill the water tanks? (A, B1, B2)", "ansGr": [ { "ans": [ "You cannot refill the water tanks if A/C have no electrical", "false" ] }, { "ans": [ "You can only refill the water tanks when A/C is energized", "false" ] }, { "ans": [ "It does not matter if the aircraft is energized or not.", "true" ] } ], "ref": "Ref AMM 12-15-38-613-801-A" }, { "ch": "The drains masts of waste water can be (A, B1, B2)", "ansGr": [ { "ans": [ "Electrically heated only on ground.", "false" ] }, { "ans": [ "Electrically heated only in flight.", "false" ] }, { "ans": [ "Not heated when A/C energized.", "true" ] } ], "ref": "Ref AMM 38-32-00-00 CONF 00 - WASTE WATER DRAIN - DESCRIPTION AND OPERATION" }, { "ch": "The water tanks are pressurized can using (A, B1, B2)", "ansGr": [ { "ans": [ "Only A/C pneumatic system", "false" ] }, { "ans": [ "Only Electrical compressor", "false" ] }, { "ans": [ "Ground air supply, A/C pneumatic system and electrical compressor.", "true" ] } ], "ref": "Ref AMM 38-11-00-00 CONF 00 - WATER STORAGE - DESCRIPTION AND OPERATION" }, { "ch": "Electrical compressor for water tanks does not operate when (A, B1, B2)", "ansGr": [ { "ans": [ "Water service door is opened", "true" ] }, { "ans": [ "Water service door is closed", "false" ] }, { "ans": [ "AFT drain panel is opened", "false" ] } ], "ref": "Ref AMM 38-11-00-00 CONF 00 - WATER STORAGE - DESCRIPTION AND OPERATION" }, { "ch": "Water drain mast is heating by (A, B1, B2)", "ansGr": [ { "ans": [ "Electricity.", "true" ] }, { "ans": [ "Pneumaticity.", "false" ] }, { "ans": [ "Electricity and pneumaticity.", "false" ] } ], "ref": "Ref AMM 38-14-00-00 CONF 00 - WATER DRAINING - DESCRIPTION AND OPERATION" }, { "ch": "Where you can check water quantity (A, B1, B2)", "ansGr": [ { "ans": [ "Only on the FAP", "false" ] }, { "ans": [ "Direct on the gauge of water tank and on the FAP", "false" ] }, { "ans": [ "On the FAP and on the portable water service panel (optionally)", "true" ] } ], "ref": "Ref AMM 38-13-00-00 CONF 00 - QUANTITY INDICATING - DESCRIPTION AND OPERATION" }, { "ch": "When does the vacuum generator operate? (A, B1, B2)", "ansGr": [ { "ans": [ "Aircraft is on ground and up to 16000 ± 700 ft.", "true" ] }, { "ans": [ "Aircraft is on ground and up to 18000 ± 700 ft.", "false" ] }, { "ans": [ "Aircraft is on ground and up to 20000± 700 ft.", "false" ] } ], "ref": "Ref AMM 38-31-00-00 CONF 00 - TOILET SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "What is the device inhibiting operation of vacuum generators during servicing (A, B1, B2)", "ansGr": [ { "ans": [ "Flush Control Unit.", "false" ] }, { "ans": [ "Vacuum system controller.", "true" ] }, { "ans": [ "Waste service door switch.", "false" ] } ], "ref": "Ref AMM 38-31-00-00 CONF 00 - TOILET SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "Before removal of the waste level transmitter (11MG, 111MG), you must (A, B1, B2)", "ansGr": [ { "ans": [ "Make sure the toilet is operative.", "false" ] }, { "ans": [ "Make sure the waste tanks are empty by draining the waste holding tanks.", "true" ] }, { "ans": [ "Make sure the waste tanks are empty by see waste tank empty on the fap.", "false" ] } ], "ref": "Ref AMM 38-31-00-00 CONF 00 - TOILET SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "The potable water Manual shut off valve located in the LAV is to? (A, B1, B2)", "ansGr": [ { "ans": [ "Stop water supply to related Galley and LAV.", "false" ] }, { "ans": [ "Stop water supply to related toilet and faucet.", "true" ] }, { "ans": [ "Stop water supply to related Galley and LAV, to related toilet and faucet.", "false" ] } ], "ref": "Ref AMM 38-31-00-040-801-A" }, { "ch": "The CMS (CENTRAL MAINTENANCE SYSTEM) is composed of:(A, B1, B2)", "ansGr": [ { "ans": [ "Two CMCs and two FWCs (Flight Warning Computer).", "false" ] }, { "ans": [ "Two CMCs and all aircraft system BITEs.", "true" ] }, { "ans": [ "Two FWC", "false" ] } ], "part": "ATA 45: OMS", "ref": "Ref: Vacbi A330-ATA 45 – CMS Presentation." }, { "ch": "The CMCS centralize and memorize warnings generated by:(A, B1, B2)", "ansGr": [ { "ans": [ "Flight Warning Computers (FWCs)", "false" ] }, { "ans": [ "All failure messages produced by the BITE function integrated in the A/C computers.", "false" ] }, { "ans": [ "Flight Warning Computers (FWCs) and all failure messages produced by the BITE function integrated in the A/C computers", "true" ] } ], "ref": "Ref: Vacbi A330-ATA 45 – CMS Presentation." }, { "ch": "How many MCDU can be used to access the cms system simultaneously? (A, B1, B2)", "ansGr": [ { "ans": [ "One only", "false" ] }, { "ans": [ "Two", "true" ] }, { "ans": [ "Three.", "false" ] } ], "ref": "Ref: Vacbi A330 - ATA 45 – CMS Architecture" }, { "ch": "Which type of systems can memorize failures that occurred during the last 64 flights? (A, B1, B2)", "ansGr": [ { "ans": [ "Type 1", "true" ] }, { "ans": [ "Type 2", "false" ] }, { "ans": [ "Type 3", "false" ] } ], "ref": "Ref: Vacbi A330 - ATA 45 – CMS Function." }, { "ch": "Which type of systems can only memorize failures from the last flight? (A, B1, B2)", "ansGr": [ { "ans": [ "Type 1", "false" ] }, { "ans": [ "Type 2", "true" ] }, { "ans": [ "Type 3", "false" ] } ], "ref": "Ref: Vacbi A330 - ATA 45 - CMS Function." }, { "ch": "The class failures have an operational consequence on the current flight is (A, B1, B2)", "ansGr": [ { "ans": [ "Class 1", "true" ] }, { "ans": [ "Class 2", "false" ] }, { "ans": [ "Class 3", "false" ] } ], "ref": "Ref : Vacbi A330 - ATA 45 – CMS-Failure Classification." }, { "ch": "Which function is used to enable access to a system bite? (A, B1, B2)", "ansGr": [ { "ans": [ "POST FLIGHT REPORT", "false" ] }, { "ans": [ "REPORT PROGRAMMING?", "false" ] }, { "ans": [ "SYSTEM REPORT/ TEST", "true" ] } ], "ref": "Ref AMM 45-10-00-00 CONF 00 - CENTRAL MAINTENANCE SYSTEM (CMS) - DESCRIPTION AND OPERATION" }, { "ch": "What happens to the post flt reports when you install a cmc coming from another A/C? (A, B1, B2)", "ansGr": [ { "ans": [ "THE “FIRST A/C INSTALLATION” MSG WILL BE DISPLAYED", "false" ] }, { "ans": [ "THE PREVIOUS POST FLT REPORTS WILL BE DISPLAYED", "false" ] }, { "ans": [ "THE PREVIOUS POST FLT REPORTS WILL NOT BE DISPLAYED", "true" ] } ], "ref": "Ref AMM 45-13-00-00 CONF 00 - CENTRAL MAINTENANCE COMPUTER (CMC) - DESCRIPTION AND OPERATION" }, { "ch": "Which item displays only the internal failures of any class? (A, B1, B2)", "ansGr": [ { "ans": [ "GROUND REPORT", "true" ] }, { "ans": [ "GROUND SCANNING", "false" ] }, { "ans": [ "LAST LEG REPORT", "false" ] } ], "ref": "Ref AMM 45-10-00-00 CONF 00 - CENTRAL MAINTENANCE SYSTEM (CMS) - DESCRIPTION AND OPERATION" }, { "ch": "An ATC message is indicated in the cockpit by means of… (A, B1, B2)", "ansGr": [ { "ans": [ "…two ATC message lights.", "true" ] }, { "ans": [ "…two master caution lights.", "false" ] }, { "ans": [ "…a buzzer only.", "false" ] } ], "part": "ATA 46: INFORMATION", "ref": "Ref AMM 46-21-00-00 CONF 00 - AIR TRAFFIC AND INFORMATION MANAGEMENT SYSTEM (ATIMS) - COMPONENTS AND INTERFACES - DESCRIPTION AND OPERATION" }, { "ch": "How can the DCDUs (Data link Communication Display Units) be tested? (A, B1, B2)", "ansGr": [ { "ans": [ "By a test button on the DCDUs.", "false" ] }, { "ans": [ "By the system test from the CMS/ATIMS menu.", "true" ] }, { "ans": [ "The annunciator light test triggers the DCDU test.", "false" ] } ], "ref": "Ref AMM 46-21-00-00 CONF 00 - AIR TRAFFIC AND INFORMATION MANAGEMENT SYSTEM (ATIMS) - COMPONENTS AND INTERFACES - DESCRIPTION AND OPERATION" }, { "ch": "In case of a message from the ATC station, the aural alert is generated… (A, B1, B2)", "ansGr": [ { "ans": [ "…by the Flight Warning Computer.", "true" ] }, { "ans": [ "…by the Air Traffic Services Unit.", "false" ] }, { "ans": [ "…by the Audio Management Unit.", "false" ] } ], "ref": "Ref AMM 46-21-00-00 CONF 00 - AIR TRAFFIC AND INFORMATION MANAGEMENT SYSTEM (ATIMS) - COMPONENTS AND INTERFACES - DESCRIPTION AND OPERATION" }, { "ch": "What is the purpose of the ATC COMM Pushbutton on the MCDU?", "ansGr": [ { "ans": [ "To establish ATC communication.", "false" ] }, { "ans": [ "To access the ATC communication log.", "false" ] }, { "ans": [ "To access the ATSU ATC menu.", "true" ] } ], "ref": "Ref AMM 46-21-00-00 CONF 00 - AIR TRAFFIC AND INFORMATION MANAGEMENT SYSTEM (ATIMS) - COMPONENTS AND INTERFACES - DESCRIPTION AND OPERATION" }, { "ch": "The uploading of the ATSU (AIR TRAFFIC SERVICE UNIT) software package is possible: (A, B1, B2)", "ansGr": [ { "ans": [ "In flight and on ground.", "false" ] }, { "ans": [ "On ground only, through the Data Loader.", "true" ] }, { "ans": [ "In flight and on ground for the uploading of all AOC (Airline Operational Control) applications.", "false" ] } ] }, { "ch": "The \"ATC MSG\" indicator lights are used for: (A, B1, B2)", "ansGr": [ { "ans": [ "Crew awareness for message transmission.", "false" ] }, { "ans": [ "Crew awareness for frequency tuning prior to message reception.", "false" ] }, { "ans": [ "Crew awareness for message reception.", "true" ] } ], "ref": "Ref AMM 46-21-00-00 CONF 00 - AIR TRAFFIC AND INFORMATION MANAGEMENT SYSTEM (ATIMS) - COMPONENTS AND INTERFACES - DESCRIPTION AND OPERATION" }, { "ch": "Where is the RAT door installed? (A, B1, B2)", "ansGr": [ { "ans": [ "RH Belly fairing", "false" ] }, { "ans": [ "RH Flap track fairing No.4", "true" ] }, { "ans": [ "LH Belly fairing", "false" ] } ], "part": "ATA 51-57", "ref": "Ref TTM ATA 51 Pg10" }, { "ch": "How many emergency exits are installed? (A, B1, B2)", "ansGr": [ { "ans": [ "1", "false" ] }, { "ans": [ "2", "true" ] }, { "ans": [ "3", "false" ] } ], "ref": "Ref TTM ATA 51 Pg2" }, { "ch": "There are two triangular openings to enable the access for maintenance in: (A, B1, B2)", "ansGr": [ { "ans": [ "The rear spar", "true" ] }, { "ans": [ "The front spar", "false" ] }, { "ans": [ "From aft cargo lining", "false" ] } ], "ref": "Ref TTM ATA 51 Pg102" }, { "ch": "The wing leading edge is fitted with seven slats. Which slats are de-iced? (A, B1, B2)", "ansGr": [ { "ans": [ "Slat 3 to 7", "false" ] }, { "ans": [ "Slat 4 to 7", "true" ] }, { "ans": [ "Slat 5 to 7", "false" ] } ], "ref": "Ref TTM ATA 51 Pg120" }, { "ch": "The Trailing Edge (TE) movable surfaces are: (A, B1, B2)", "ansGr": [ { "ans": [ "The inboard and outboard flaps, the two ailerons, and the 6 spoilers.", "true" ] }, { "ans": [ "The inboard and outboard flaps, the two ailerons, and the 5 spoilers.", "false" ] }, { "ans": [ "The inboard and outboard flaps, the two ailerons, and the 7 spoilers.", "false" ] } ], "ref": "Ref TTM ATA 51 Pg 134" }, { "ch": "The passenger/crew doors are opened (A, B1, B2)", "ansGr": [ { "ans": [ "Outwards and forwards, parallel to the fuselage.", "true" ] }, { "ans": [ "Outwards and upwards from the fuselage.", "false" ] }, { "ans": [ "Inwards and upwards.", "false" ] } ], "part": "ATA 52: DOORS", "ref": "Ref AMM 52-11-00-00 CONF 00 - FWD PASSENGER/CREW DOOR - DESCRIPTION AND OPERATION" }, { "ch": "The door seal around the door is inflated through holes when (A, B1, B2)", "ansGr": [ { "ans": [ "Aircraft in flight only", "false" ] }, { "ans": [ "The cabin is depressurized.", "false" ] }, { "ans": [ "The cabin pressure is available.", "true" ] } ], "ref": "Ref AMM 52-11-00-00 CONF 00 - FWD PASSENGER/CREW DOOR - DESCRIPTION AND OPERATION" }, { "ch": "Which component maintains the door parallel to the fuselage? (A, B1, B2)", "ansGr": [ { "ans": [ "Two guide arms", "true" ] }, { "ans": [ "By the support arm.", "false" ] }, { "ans": [ "The guide rollers.", "false" ] } ], "ref": "Ref AMM 52-11-00-00 CONF 00 - FWD PASSENGER/CREW DOOR - DESCRIPTION AND OPERATION" }, { "ch": "The door does not move when in the fully opened position by (A, B1, B2).", "ansGr": [ { "ans": [ "The rubber door buffer", "false" ] }, { "ans": [ "The door stay mechanism.", "true" ] }, { "ans": [ "Two locking hooks located on the upper edge", "false" ] } ], "ref": "Ref AMM 52-11-00-00 CONF 00 - FWD PASSENGER/CREW DOOR - DESCRIPTION AND OPERATION" }, { "ch": "In \"ARMED\" mode, the arming mechanical linkage (A, B1, B2)", "ansGr": [ { "ans": [ "Fixes the girt bar to the floor structure.", "true" ] }, { "ans": [ "Secures the girt bar to the door.", "false" ] }, { "ans": [ "Let the girt bar move freely between the door and the door floor.", "false" ] } ], "ref": "Ref AMM 52-11-00-00 CONF 00 - FWD PASSENGER/CREW DOOR - DESCRIPTION AND OPERATION" }, { "ch": "The red flashing light located below the viewing prism window: (A, B1, B2)", "ansGr": [ { "ans": [ "Indicates the ARMED configuration of the evacuation system.", "false" ] }, { "ans": [ "Warns the operator that the cabin is still pressurized.", "true" ] }, { "ans": [ "Indicates the LOCKED condition of the door.", "false" ] } ], "ref": "Ref AMM 52-71-00-00 CONF 00 - DOOR AND ESCAPE SLIDE CONTROL SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "The white light located below the viewing prism window: (A, B1, B2)", "ansGr": [ { "ans": [ "Indicates the ARMED configuration of the evacuation system.", "true" ] }, { "ans": [ "Warns the operator that the cabin is still pressurized.", "false" ] }, { "ans": [ "Indicates the LOCKED condition of the door.", "false" ] } ], "ref": "Ref AMM 52-71-00-00 CONF 00 - DOOR AND ESCAPE SLIDE CONTROL SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "When does the damper and emergency cylinder work as a damper? (A, B1, B2)", "ansGr": [ { "ans": [ "When the arming lever is in \"DISARMED\" position.", "true" ] }, { "ans": [ "When the door is fully closed.", "false" ] }, { "ans": [ "When the arming lever is in \"ARMED\" position.", "false" ] } ], "ref": "Ref AMM 52-71-00-00 CONF 00 - DOOR AND ESCAPE SLIDE CONTROL SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "The gear box allows (A, B1, B2)", "ansGr": [ { "ans": [ "The outer handle does not move when the inner handle is operated.", "true" ] }, { "ans": [ "The inner handle does not move when the outer handle is operated.", "false" ] }, { "ans": [ "The outer handle moves simultaneously when the inner handle is operated.", "false" ] } ], "ref": "Ref AMM 52-11-00-00 CONF 00 - FWD PASSENGER/CREW DOOR - DESCRIPTION AND OPERATION" }, { "ch": "When will the safety lock pin be installed on the arming lever? (A, B1, B2)", "ansGr": [ { "ans": [ "When arming level in ARMED position.", "true" ] }, { "ans": [ "When arming level in DISARMED position.", "false" ] }, { "ans": [ "When arming level in ARMED position and DISARMED position.", "false" ] } ], "ref": "Ref AMM 52-71-00-00 CONF 00 - DOOR AND ESCAPE SLIDE CONTROL SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "What happens when you open the door from outside in ARMED mode? (A, B1, B2)", "ansGr": [ { "ans": [ "The system is automatically disarmed.", "true" ] }, { "ans": [ "The white light comes on.", "false" ] }, { "ans": [ "The escape slide deploys.", "false" ] } ], "ref": "Ref AMM 52-71-00-00 CONF 00 - DOOR AND ESCAPE SLIDE CONTROL SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "Each passenger door is equipped with: (A, B1, B2)", "ansGr": [ { "ans": [ "One mechanical indicator.", "false" ] }, { "ans": [ "Two electrical indicators.", "false" ] }, { "ans": [ "Two mechanical indicators.", "true" ] } ], "ref": "Ref AMM 52-11-00-00 CONF 00 - FWD PASSENGER/CREW DOOR - DESCRIPTION AND OPERATION" }, { "ch": "How many emergencies exit door are installed on the A330 aircraft (A, B1, B2)", "ansGr": [ { "ans": [ "Two.", "true" ] }, { "ans": [ "Four.", "false" ] }, { "ans": [ "Six.", "false" ] } ], "ref": "Ref AMM 52-20-00-00 CONF 00 - EMERGENCY EXIT - DESCRIPTION AND OPERATION" }, { "ch": "The FWD and AFT cargo door: (A, B1, B2)", "ansGr": [ { "ans": [ "Are identical in design and in operation, but not in size.", "true" ] }, { "ans": [ "Are identical in size and in operation, but not in design.", "false" ] }, { "ans": [ "Are identical only in operation.", "false" ] } ], "ref": "Ref AMM 52-30-00-00 CONF 00 - CARGO - DESCRIPTION AND OPERATION" }, { "ch": "The pump handle is: (A, B1, B2)", "ansGr": [ { "ans": [ "Used for closing only, even with or without electric pump.", "false" ] }, { "ans": [ "Used for assisting the hydraulic system.", "false" ] }, { "ans": [ "Located in the green hydraulic ground service panel.", "true" ] } ], "ref": "Ref AMM 52-30-00-00 CONF 00 - CARGO - DESCRIPTION AND OPERATION" }, { "ch": "The FWD and AFT cargo doors are opened (A, B1, B2)", "ansGr": [ { "ans": [ "Outwards and forwards, parallel to the fuselage.", "false" ] }, { "ans": [ "Outwards and upwards from the fuselage.", "true" ] }, { "ans": [ "Inwards and upwards.", "false" ] } ], "ref": "Ref AMM 52-30-00-00 CONF 00 - CARGO - DESCRIPTION AND OPERATION" }, { "ch": "What does the red flag indicator show? (A, B1, B2)", "ansGr": [ { "ans": [ "The hooks are not correctly fully latched.", "false" ] }, { "ans": [ "The latching handle has been operated.", "false" ] }, { "ans": [ "The corresponding hook is not locked.", "true" ] } ], "ref": "Ref AMM 52-32-00-00 CONF 00 - AFT CARGO COMPARTMENT DOOR - DESCRIPTION AND OPERATION" }, { "ch": "What does the green light fitted near the manual selector valve indicate? (A, B1, B2)", "ansGr": [ { "ans": [ "The yellow hydraulic pressure is available to operate the door.", "false" ] }, { "ans": [ "The door is fully opened & locked.", "true" ] }, { "ans": [ "The door is correctly unlatched & unlocked.", "false" ] } ], "ref": "Ref AMM 52-32-00-00 CONF 00 - AFT CARGO COMPARTMENT DOOR - DESCRIPTION AND OPERATION" }, { "ch": "In the cargo door, behind the flapper door, a red light flashes when (A, B1, B2)", "ansGr": [ { "ans": [ "There is a residual pressure in the cabin.", "true" ] }, { "ans": [ "The hooks are not locked.", "false" ] }, { "ans": [ "The door is unlatched", "false" ] } ], "ref": "Ref AMM 52-32-00-00 CONF 00 - AFT CARGO COMPARTMENT DOOR - DESCRIPTION AND OPERATION" }, { "ch": "The power to operate the cargo door actuation system is supplied by (A, B1, B2)", "ansGr": [ { "ans": [ "The Green hydraulic system.", "false" ] }, { "ans": [ "The Blue hydraulic system.", "false" ] }, { "ans": [ "The Yellow hydraulic system.", "true" ] } ], "ref": "Ref AMM 52-32-00-00 CONF 00 - AFT CARGO COMPARTMENT DOOR - DESCRIPTION AND OPERATION" }, { "ch": "The latching handle operates (A, B1, B2)", "ansGr": [ { "ans": [ "The hooks which secure the door to the door frame.", "true" ] }, { "ans": [ "The latching shaft to secure the hooks in the latched position.", "false" ] }, { "ans": [ "A locking shaft which secures the latching shaft when the hooks are closed.", "false" ] } ], "ref": "Ref AMM 52-32-00-00 CONF 00 - AFT CARGO COMPARTMENT DOOR - DESCRIPTION AND OPERATION" }, { "ch": "Locking handle operates (A, B1, B2)", "ansGr": [ { "ans": [ "A locking shaft which secures the latching shaft when the hooks are closed.", "true" ] }, { "ans": [ "The hooks which secure the door to the door frame.", "false" ] }, { "ans": [ "The latching shaft to release or lock the hooks.", "false" ] } ], "ref": "Ref AMM 52-32-00-00 CONF 00 - AFT CARGO COMPARTMENT DOOR - DESCRIPTION AND OPERATION" }, { "ch": "Can we operate the cargo door without the electrical power (A, B1, B2)", "ansGr": [ { "ans": [ "Yes, by using the hand pump", "true" ] }, { "ans": [ "Yes, by using the mechanical driven device", "false" ] }, { "ans": [ "No, the yellow electrical pump is the only way to operate the cargo door.", "false" ] } ], "ref": "Ref AMM 52-32-00-00 CONF 00 - AFT CARGO COMPARTMENT DOOR - DESCRIPTION AND OPERATION" }, { "ch": "How many people are required for manually operate the cargo door (A, B1, B2)", "ansGr": [ { "ans": [ "One", "false" ] }, { "ans": [ "Two", "true" ] }, { "ans": [ "Three", "false" ] } ], "ref": "Ref AMM 52-32-00-00 CONF 00 - AFT CARGO COMPARTMENT DOOR - DESCRIPTION AND OPERATION" }, { "ch": "For cargo door operation (A, B1, B2)", "ansGr": [ { "ans": [ "The door sill latches (of the cargo loading system) must be in LATCHED position", "true" ] }, { "ans": [ "The door sill latches (of the cargo loading system) must be in UNLATCHED position", "false" ] }, { "ans": [ "The door sill latches position is not affected.", "false" ] } ], "ref": "Ref AMM 52-32-00-00 CONF 00 - AFT CARGO COMPARTMENT DOOR - DESCRIPTION AND OPERATION" }, { "ch": "During normal operation of the cargo door (A, B1, B2)", "ansGr": [ { "ans": [ "The Yellow system leak measurement isolation valve is automatically controlled shut", "false" ] }, { "ans": [ "The Yellow system motor valve block of the Flap PCU is latched off.", "false" ] }, { "ans": [ "The Yellow system leak measurement isolation valve is automatically controlled shut and the Yellow system motor valve block of the Flap PCU is latched off.", "true" ] } ], "ref": "Ref AMM 52-32-00-0 CONF 00 - AFT CARGO COMPARTMENT DOOR - DESCRIPTION AND OPERATION" }, { "ch": "The Bulk cargo door is opened (A, B1, B2)", "ansGr": [ { "ans": [ "Outwards and forwards, parallel to the fuselage.", "false" ] }, { "ans": [ "Outwards and upwards from the fuselage.", "false" ] }, { "ans": [ "Inwards and upwards.", "true" ] } ], "ref": "Ref AMM 52-33-00-00 CONF 00 - BULK CARGO COMPARTMENT DOOR - DESCRIPTION AND OPERATION" }, { "ch": "The bulk cargo door latch assembly located on (A, B1, B2)", "ansGr": [ { "ans": [ "The lower edge.", "true" ] }, { "ans": [ "The upper edge.", "false" ] }, { "ans": [ "Both sides.", "false" ] } ], "ref": "Ref AMM 52-33-00-00 CONF 00 - BULK CARGO COMPARTMENT DOOR - DESCRIPTION AND OPERATION" }, { "ch": "The Bulk cargo door can operate from (A, B1, B2)", "ansGr": [ { "ans": [ "Outside only.", "false" ] }, { "ans": [ "Inside only.", "false" ] }, { "ans": [ "Outside and inside", "true" ] } ], "ref": "Ref AMM 52-33-00-00 CONF 00 - BULK CARGO COMPARTMENT DOOR - DESCRIPTION AND OPERATION" }, { "ch": "The Door & Slide Control System consists of: (A, B1, B2)", "ansGr": [ { "ans": [ "Proximity switches and a proximity Switch Control Unit,", "false" ] }, { "ans": [ "A pressure switch and an Autonomous Standby Power Supply Unit.", "false" ] }, { "ans": [ "Proximity switches and a proximity Switch Control Unit and a pressure switch and an Autonomous Standby Power Supply Unit.", "true" ] } ] }, { "ch": "The functions of the DSCS are: (A, B1, B2)", "ansGr": [ { "ans": [ "Door and Escape Slide Indicating and Warning, Residual Cabin Pressure Detection and Indicating,", "false" ] }, { "ans": [ "Cargo Doors Electrical Control and Indicating.", "false" ] }, { "ans": [ "Door and Escape Slide Indicating and Warning, Residual Cabin Pressure Detection and Indicating and Cargo Doors Electrical Control and Indicating.", "true" ] } ], "ref": "Ref AMM 52-71-00-00 CONF 00 - DOOR AND ESCAPE SLIDE CONTROL SYSTEM - DESCRIPTION AND OPERATION" }, { "ch": "The door operation starts as soon as: (A, B1, B2)", "ansGr": [ { "ans": [ "The door is unlatched, and the selector is set to the open or closed position.", "false" ] }, { "ans": [ "The cargo loading sill latches are raised,", "false" ] }, { "ans": [ "The door is unlatched, and the selector is set to the open or close position and the cargo loading sill latches are raised,", "true" ] } ], "ref": "Ref AMM 52-32-00-00 CONF 00 - AFT CARGO COMPARTMENT DOOR - DESCRIPTION AND OPERATION" }, { "ch": "The cockpit door is: (A, B1, B2)", "ansGr": [ { "ans": [ "An armored and bulletproof door made with one mechanical latch electrically released.", "false" ] }, { "ans": [ "An armored and bulletproof door made with three mechanical latches electrically released.", "true" ] }, { "ans": [ "An armored and bulletproof door made with three mechanical latches mechanically released.", "false" ] } ], "ref": "Ref AMM 52-51-00-00 CONF 00 - PASSENGER COMPARTMENT FIXED PARTITION INTERIOR DOORS - DESCRIPTION AND OPERATION" }, { "ch": "The cockpit door is locked: (A, B1, B2)", "ansGr": [ { "ans": [ "Automatically when it is closed, and the aircraft is powered.", "true" ] }, { "ans": [ "Automatically when the aircraft is in flight.", "false" ] }, { "ans": [ "Manually by the crew only.", "false" ] } ], "ref": "Ref AMM 52-51-00-00 CONF 00 - PASSENGER COMPARTMENT FIXED PARTITION INTERIOR DOORS - DESCRIPTION AND OPERATION" }, { "ch": "In normal mode, incase of no response from the pilots, at a request to entry in the cockpit by the cabin attendant crew: (A, B1, B2)", "ansGr": [ { "ans": [ "The cockpit door remains closed.", "true" ] }, { "ans": [ "The cockpit door opens automatically after a defined time.", "false" ] }, { "ans": [ "The cockpit door can be opened by the cabin attendant crew.", "false" ] } ], "ref": "Ref AMM 52-51-00-00 CONF 00 - PASSENGER COMPARTMENT FIXED PARTITION INTERIOR DOORS - DESCRIPTION AND OPERATION" }, { "ch": "When the emergency mode is activated from the keypad with the cockpit door toggle switch in norm neutral position: (A, B1, B2)", "ansGr": [ { "ans": [ "All the latches remain locked, and access is not possible from the cabin.", "false" ] }, { "ans": [ "All the latches are unlocked, and access is possible from the cabin.", "false" ] }, { "ans": [ "All the latches will unlock automatically after a preset time delay.", "true" ] } ], "ref": "Ref AMM 52-51-00-00 CONF 00 - PASSENGER COMPARTMENT FIXED PARTITION INTERIOR DOORS - DESCRIPTION AND OPERATION" }, { "ch": "A locked cockpit door: (A, B1, B2)", "ansGr": [ { "ans": [ "Can be always opened from the cabin side.", "false" ] }, { "ans": [ "Can be always opened from the cockpit side.", "true" ] }, { "ans": [ "Cannot be opened from the cockpit side.", "false" ] } ], "ref": "Ref AMM 52-51-00-00 CONF 00 - PASSENGER COMPARTMENT FIXED PARTITION INTERIOR DOORS - DESCRIPTION AND OPERATION" }, { "ch": "You can access the avionics compartments from: (A, B1, B2)", "ansGr": [ { "ans": [ "The cockpit and the outside.", "false" ] }, { "ans": [ "The cockpit, the outside and the cabin.", "false" ] }, { "ans": [ "The cockpit, the outside, and the forward cargo compartment.", "true" ] } ], "ref": "Ref AMM 52-51-00-00 CONF 00 - PASSENGER COMPARTMENT FIXED PARTITION INTERIOR DOORS - DESCRIPTION AND OPERATION" } ]