[ { "ch": "Location zone for Lower Half of Fuselage is:", "ansGr": [ { "ans": [ "100 ", "true" ] }, { "ans": [ "200 ", "false" ] }, { "ans": [ "300 ", "false" ] } ] }, { "ch": "Location zone for Left Wing is:", "ansGr": [ { "ans": [ "300 ", "false" ] }, { "ans": [ "400 ", "false" ] }, { "ans": [ "500 ", "true" ] } ] }, { "ch": "Location zone for Landing Gear and Landing Gear Doors is:", "ansGr": [ { "ans": [ "600 ", "false" ] }, { "ans": [ "700 ", "true" ] }, { "ans": [ "800 ", "false" ] } ] }, { "ch": "Dimensions of the airplane:", "ansGr": [ { "ans": [ "In some cases change with the center of gravity location and the airplane loads. ", "true" ] }, { "ans": [ "Never change. ", "false" ] }, { "ans": [ "May be measured in inches only. ", "false" ] } ] }, { "ch": "The Wings zones are numbered in the sequence that follows:", "ansGr": [ { "ans": [ "Inboard to outboard and front to back. ", "true" ] }, { "ans": [ "Outboard to inboard and front to back ", "false" ] }, { "ans": [ "Inboard to outboard and back to front. ", "false" ] } ] }, { "ch": "The Horizontal Stabilizer and Elevator zones are numbered in the sequence that follows:", "ansGr": [ { "ans": [ "Inboard to outboard and front to back. ", "true" ] }, { "ans": [ "Outboard to inboard and front to back ", "false" ] }, { "ans": [ "Inboard to outboard and back to front ", "false" ] } ] }, { "ch": "The Vertical Stabilizer and Rudder zones are numbered in the sequence that follows", "ansGr": [ { "ans": [ "Trailing edge to the leading edge the of vertical stabilizer ", "false" ] }, { "ans": [ "Leading edge to the trailing edge the of vertical stabilizer. ", "true" ] }, { "ans": [ "Inboard to outboard and front to back of vertical stabilizer ", "false" ] } ] }, { "ch": "The Fuselage zones are numbered in the sequence that follows", "ansGr": [ { "ans": [ "Back to front and away from the floorline. ", "false" ] }, { "ans": [ "Front to back and from top to the bottom. ", "false" ] }, { "ans": [ "Front to back and away from the floorline ", "true" ] } ] }, { "ch": "Fuselage station diagram gives reference to find out components, features and major fuselage structural openings in relation to:", "ansGr": [ { "ans": [ "Datum plane which is perpendicular to fuselage centerline and located 92.50 Inch forward of airplane nose ", "true" ] }, { "ans": [ "Nose of airplane ", "false" ] }, { "ans": [ "Floor of airplane passenger cabin ", "false" ] } ] }, { "ch": "Major zone 100 is", "ansGr": [ { "ans": [ "Upper half of fuselage ", "false" ] }, { "ans": [ "Lower half of fuselage ", "true" ] }, { "ans": [ "l/h and r/h wing ", "false" ] } ] }, { "ch": "NAC STA 120.00 is station used:", "ansGr": [ { "ans": [ "On engine and nacelle strut ", "true" ] }, { "ans": [ "On horizontal stabilizer ", "false" ] }, { "ans": [ "On airplane fuselage ", "false" ] } ] }, { "ch": "Access panel 191CL is:", "ansGr": [ { "ans": [ "Panel number 1CL in zone 19. ", "false" ] }, { "ans": [ "The third panel in zone 191. ", "true" ] }, { "ans": [ "An internal panel in zone 191 ", "false" ] } ] }, { "ch": "Station STA 550 is", "ansGr": [ { "ans": [ "550 inches from airplane nose ", "false" ] }, { "ans": [ "550cm from the airplane datum plane ", "false" ] }, { "ans": [ "550 inches from the airplane datum plane ", "true" ] } ] }, { "ch": "To find one access panel of airplane lower fuselage we can", "ansGr": [ { "ans": [ "Use zoning diagram of airplane ", "false" ] }, { "ans": [ "Check on airplane because access panel identification marking is on panel exterior surface ", "false" ] }, { "ans": [ "a or b ", "true" ] } ] }, { "ch": "Location zone for Powerplants and Nacelle Struts?", "ansGr": [ { "ans": [ "300 ", "false" ] }, { "ans": [ "400 ", "true" ] }, { "ans": [ "800 ", "false" ] } ] }, { "ch": "Major zone 700 is", "ansGr": [ { "ans": [ "Left Wing ", "false" ] }, { "ans": [ "Landing Gear and Landing Gear Doors ", "true" ] }, { "ans": [ "Right Wing ", "false" ] } ] }, { "ch": "Airplane B777-200ER has", "ansGr": [ { "ans": [ "3 primary jack points and 5 auxiliary jack points ", "true" ] }, { "ans": [ "5 primary jack points and 5 auxiliary jack points ", "false" ] }, { "ans": [ "3 primary jack points and 3 auxiliary jack points ", "false" ] } ] }, { "ch": "To get 3 primary jack points for airplane lifting we need", "ansGr": [ { "ans": [ "Open 3 access panels and install jack pads ", "false" ] }, { "ans": [ "Open 2 access panels only and we do not need install jack pads ", "true" ] }, { "ans": [ "Just install 3 jack pads ", "false" ] } ] }, { "ch": "For main landing gear middle wheel replacement we need", "ansGr": [ { "ans": [ "Lift airplane on fwd axle only ", "false" ] }, { "ans": [ "Lift airplane on aft axle only ", "false" ] }, { "ans": [ "Lift airplane on both fwd and aft axle ", "true" ] } ] }, { "ch": "For airplane jacking", "ansGr": [ { "ans": [ "we need install landing gear lock pins only if we jack airplane on primary jack points ", "false" ] }, { "ans": [ "we do not install landing gear lock pins only if we jack airplane on axle ", "false" ] }, { "ans": [ "we need install landing gear lock pins every time when we jack airplane ", "true" ] } ] }, { "ch": "To jack airplane nose by secondary jack point", "ansGr": [ { "ans": [ "we need open access panel for jack point ", "false" ] }, { "ans": [ "we need remove filler bolt firstly and than install specified jack adaptor ", "true" ] }, { "ans": [ "we need open access panel firstly and than install specified jack adaptor ", "false" ] } ] }, { "ch": "Before jacking airplane we make sure that", "ansGr": [ { "ans": [ "parking brake released ", "false" ] }, { "ans": [ "landing gear downlock pins installed ", "false" ] }, { "ans": [ "jacks are serviceable and leveled ", "false" ] }, { "ans": [ "all above a, b and c ", "true" ] } ] }, { "ch": "Where are stowed landing gear downlock pins when removed", "ansGr": [ { "ans": [ "in stowage box in MEC ", "true" ] }, { "ans": [ "in bag in cockpit ", "false" ] }, { "ans": [ "in IFE lower compartment ", "false" ] } ] }, { "ch": "The Airplane Is On The Jacks, It Can:", "ansGr": [ { "ans": [ "Refuel L/R tanks with limit quantity ", "false" ] }, { "ans": [ "Refuel center tanks with limit quantity ", "false" ] }, { "ans": [ "No refuel ", "true" ] } ] }, { "ch": "if the airplane was stopped or parked while it was in a turn:", "ansGr": [ { "ans": [ "Move the airplanestraight forword a minimum of 20 ft before lifting it on jacks. ", "false" ] }, { "ans": [ "Move the airplanestraight forword a minimum of 10 ft before lifting it on jacks ", "true" ] }, { "ans": [ "Move the airplanestraight forword a minimum of 5 ft before lifting it on jacks ", "false" ] } ] }, { "ch": "The location of the inclinometers are in", "ansGr": [ { "ans": [ "in the left main wheel gear well ", "false" ] }, { "ans": [ "in the right main wheel gear well ", "false" ] }, { "ans": [ "the nose wheel well ", "true" ] } ] }, { "ch": "With plumb bob installed we can check:", "ansGr": [ { "ans": [ "airplane pitch only ", "false" ] }, { "ans": [ "airplane roll only ", "false" ] }, { "ans": [ "airplane pitch and roll ", "true" ] } ] }, { "ch": "For leveling purpose, the airplane has", "ansGr": [ { "ans": [ "02 inclinometers and 01 plumb bob in nose wheel well ", "false" ] }, { "ans": [ "02 inclinometers and 01 plumb bob in right main wheel well ", "false" ] }, { "ans": [ "02 inclinometers in nose wheel well, 01 plumb bob fitting and scale in right main wheel well ", "true" ] } ] }, { "ch": "When performing airplane weighing we can use procedures of", "ansGr": [ { "ans": [ "platform scales ", "false" ] }, { "ans": [ "electronic load cells by jacking airplane at landing gear axle points ", "false" ] }, { "ans": [ "electronic load cells by jacking airplane at primary jack points ", "false" ] }, { "ans": [ "all above a, b and c ", "true" ] } ] }, { "ch": "When performing airplane weighing we make sure that", "ansGr": [ { "ans": [ "all kind of fluid is drained including engine oil and hydraulic fluid ", "false" ] }, { "ans": [ "fuel tanks drained, portable water system drained and waste tanks drained ", "true" ] }, { "ans": [ "all loose equipment items removed ", "false" ] } ] }, { "ch": "Airplane weighing is to be performed", "ansGr": [ { "ans": [ "outside but on level surface ", "false" ] }, { "ans": [ "inside opened hangar ", "false" ] }, { "ans": [ "inside closed facility that excludes all wind and drafts, permits shutdown air conditioning during weigh operation, maintains a relative constant temperature and has level surface and sufficient overhead clearance ", "true" ] } ] }, { "ch": "When performing airplane weighing we make sure that the airplane is configuration:", "ansGr": [ { "ans": [ "all doors and access panels in closed position ", "false" ] }, { "ans": [ "all landing gear wheels in specified operating pressures ", "false" ] }, { "ans": [ "horizontal stabilizer, control surfaces and spoilers in neutral positions ", "false" ] }, { "ans": [ "all above a, b and c ", "true" ] } ] }, { "ch": "After using for airplane level, plumb bob is removed and", "ansGr": [ { "ans": [ "stowed in pouch inside MEC ", "false" ] }, { "ans": [ "stowed in specified place of cockpit ", "false" ] }, { "ans": [ "returned to store ", "true" ] } ] }, { "ch": "Before towing the airplane all engine cowls to be closed and latched is:", "ansGr": [ { "ans": [ "mandatory. ", "true" ] }, { "ans": [ "not required. ", "false" ] }, { "ans": [ "optional. ", "false" ] } ] }, { "ch": "For airplane towing", "ansGr": [ { "ans": [ "all engine cowls must be closed and latched ", "true" ] }, { "ans": [ "only engine thrust cowls must be closed and latched ", "false" ] }, { "ans": [ "engine cowls may be opened and hold open rods must be in safety position ", "false" ] } ] }, { "ch": "For airplane towing due to maintenance action", "ansGr": [ { "ans": [ "all landing gear downlock pins must be installed ", "true" ] }, { "ans": [ "only nose landing gear downlock pin must be installed because tow bar is connected to nose landing gear only ", "false" ] }, { "ans": [ "all landing gear downlock pins may not be installed if APU is operating ", "false" ] } ] }, { "ch": "During towing airplane is able to turned", "ansGr": [ { "ans": [ "90 degrees maximum ", "false" ] }, { "ans": [ "60 degrees maximum ", "false" ] }, { "ans": [ "70 degrees maximum when torsion links are connected and more than 70 degrees if torsion links are disconnected ", "true" ] } ] }, { "ch": "Before removing of tow lever lock pin", "ansGr": [ { "ans": [ "we must disconnect tow bar ", "false" ] }, { "ans": [ "we make sure that nose wheels are in centering position ", "false" ] }, { "ans": [ "we must disconnect tow bar and make sure that nose wheels are in centering position ", "true" ] } ] }, { "ch": "Mechanic who stays in cockpit for airplane towing", "ansGr": [ { "ans": [ "he must be an approved mechanic ", "true" ] }, { "ans": [ "he must be older than 40 years ", "false" ] }, { "ans": [ "he is any mechanic who had B777 type qualification training ", "false" ] } ] }, { "ch": "Which fitting we can tow or push the airplane with a tow bar", "ansGr": [ { "ans": [ "A forward tow fitting on the nose and the main landing gear ", "false" ] }, { "ans": [ "An aft tow fitting if installed on the nose landing gear ", "false" ] }, { "ans": [ "A forward tow fitting on the nose and the main landing gear,an aft tow fitting if installed on the nose landing gear ", "true" ] } ] }, { "ch": "When Towed Airplane With Apu Is On,The Clearance Must Be Between The Apu Exhaust Port And The Adjacent Airplane’s Wingtip (Fuel Vent) Is:", "ansGr": [ { "ans": [ "A Minimum Clearance Of 50.0 Feet ", "true" ] }, { "ans": [ "A Minimum Clearance Of 150.0 Feet ", "false" ] }, { "ans": [ "A Minimum Clearance Of 70.0 Feet ", "false" ] } ] }, { "ch": "Most Towbarless Tow Vehicles Do Not Have A Shear Pin To Limit The Loads If The Airplane Brakes Are Used During Towing:", "ansGr": [ { "ans": [ "Damage Will Occur To The Nose Landing Gear ", "false" ] }, { "ans": [ "Damage Will Occur To The Nose Landing Gear, And The Tow Vehicle. ", "true" ] }, { "ans": [ "Damage Will Not Occur To The Nose Landing Gear ", "false" ] } ] }, { "ch": "When You Hold The Tow Lever In The Tow Position With The Lockpin:", "ansGr": [ { "ans": [ "The Nose Gear Steering Will Not Operate. ", "true" ] }, { "ans": [ "The Nose Gear Steering Will Operate Normally ", "false" ] }, { "ans": [ "The Nose Gear Steering Will Not Operate When The Hydraulic Systems Is Pressurized ", "false" ] } ] }, { "ch": "When The Landing Gear Shock Strut Is Compressed Fully:", "ansGr": [ { "ans": [ "Tow The Airplane With Limit Speed ", "false" ] }, { "ans": [ "Do Not Tow The Airplane ", "true" ] }, { "ans": [ "Tow The Airplane With Low Wind ", "false" ] } ] }, { "ch": "If Shock Strut Extension For The Nose Landing Gear Is 36 Inches At Dim \"A\":", "ansGr": [ { "ans": [ "Tow Aircaft If Shock Strut Extension For The Noselanding Gear Is Below 36 Inches To More Than 20.42 Inches At Dim \"A\" ", "true" ] }, { "ans": [ "Tow Aircaft If Shock Strut Extension For The Noselanding Gear Is More Than 36 Inches At Dim \"A\" ", "false" ] }, { "ans": [ "Can Tow Aircaft If Shock Strut Extension For The Noselanding Gear Is At Any Shock Strut Extension For The Noselanding Gear ", "false" ] } ] }, { "ch": "During Towing Aircraft:", "ansGr": [ { "ans": [ "Hold Or Turn The Tiller For The Nose Wheel Steering ", "false" ] }, { "ans": [ "Do Not Hold Or Turn The Tiller For The Nose Wheel Steering ", "true" ] }, { "ans": [ "Hold Or Turn The Tiller For The Nose Wheel Steering If Hydraulic Sysytem Depressurized ", "false" ] } ] }, { "ch": "During Towing By A Tow Bar If Apply The Airplane Brakes:", "ansGr": [ { "ans": [ "The Shear Pins To Shear In A Tow Bar ", "true" ] }, { "ans": [ "The Shear Pins To Shear In A Tow Bar On Curve Only ", "false" ] }, { "ans": [ "The Shear Pins To Shear In A Tow Bar On Straight Roads Only ", "false" ] } ] }, { "ch": "Pitot probe covers and static port covers are recommended when the airplane is parked for:", "ansGr": [ { "ans": [ "transit check. ", "false" ] }, { "ans": [ "leak and sense check. ", "false" ] }, { "ans": [ "more than a standard turnaround ", "true" ] } ] }, { "ch": "A static ground on the airplane is necessary:", "ansGr": [ { "ans": [ "when the airplane is parked or is serviced during the turnaround operation ", "false" ] }, { "ans": [ "when you do maintenance procedures ", "true" ] }, { "ans": [ "when you pressure fuel the airplane. ", "false" ] } ] }, { "ch": "Prolonged Parking means:", "ansGr": [ { "ans": [ "When an airplane is not operated for 7 days or more ", "true" ] }, { "ans": [ "When an airplane is not operated for 14 days or more, ", "false" ] }, { "ans": [ "When an airplane is not operated for 30 days or more, ", "false" ] } ] }, { "ch": "For airplane being parked more than 24hours we make sure that", "ansGr": [ { "ans": [ "landing gear downlock pins and all pitot probe covers installed ", "false" ] }, { "ans": [ "chocks installed ", "false" ] }, { "ans": [ "battery switched off and circuit breakers of hot battery bus pulled out ", "false" ] }, { "ans": [ "all above a, b and c ", "true" ] } ] }, { "ch": "When landing gear downlock pins are installed on parked airplane we make sure that", "ansGr": [ { "ans": [ "those pins are installed correctly ", "false" ] }, { "ans": [ "those pins are visible from ground by meaning of attached red flag REMOVE BEFORE FLIGHT ", "false" ] }, { "ans": [ "entry written in tech log for pins installation ", "false" ] }, { "ans": [ "all above a, b and c ", "true" ] } ] }, { "ch": "When pitot probe covers are installed on parked airplane we make sure that", "ansGr": [ { "ans": [ "those covers are in serviceable condition without damages especially fraying ", "false" ] }, { "ans": [ "those covers are visible from ground by meaning of attached red flag REMOVE BEFORE FLIGHT ", "false" ] }, { "ans": [ "entry written in tech log for covers installation ", "false" ] }, { "ans": [ "all above a, b and c ", "true" ] } ] }, { "ch": "For airplane being to be parked in high wind we make sure that", "ansGr": [ { "ans": [ "all doors, hatches and access panels closed and latched ", "false" ] }, { "ans": [ "main fuel tanks filled to a minimum 10 percent full ", "false" ] }, { "ans": [ "slat and flap in up position and stabilizer in neutral position ", "false" ] }, { "ans": [ "all above a, b and c ", "true" ] } ] }, { "ch": "For airplane parked in long time period more than 7 days we make sure that", "ansGr": [ { "ans": [ "all fuel tanks to be empty ", "false" ] }, { "ans": [ "all fuel tanks to be greater than 10% full and biocide to be put into tanks ", "false" ] }, { "ans": [ "fuel tank water drain to be repeated after 24 hours ", "false" ] }, { "ans": [ "b and c ", "true" ] } ] }, { "ch": "For airplane parked in long time period more than 7 days we make sure that", "ansGr": [ { "ans": [ "make sure shock strut serviced correctly ", "false" ] }, { "ans": [ "make sure tires serviced correctly ", "false" ] }, { "ans": [ "make sure tires turned at least 1/3 of turn each 30 days cycles ", "false" ] }, { "ans": [ "all above a, b and c ", "true" ] } ] }, { "ch": "For airplane parked in long time period more than 7 days we make sure that", "ansGr": [ { "ans": [ "the crew oxygen bottles shutoff valve to be closed and secured ", "false" ] }, { "ans": [ "all portable oxygen bottles shutoff valves to be closed ", "false" ] }, { "ans": [ "all bottle cylinders not due for hydrostatic test ", "false" ] }, { "ans": [ "all above a, b and c ", "true" ] } ] }, { "ch": "For airplane parked in long time period more than 7 days we make sure that", "ansGr": [ { "ans": [ "install protective cover for carpet in aisle ", "false" ] }, { "ans": [ "install protective cover for all seats ", "false" ] }, { "ans": [ "close all window shades ", "false" ] }, { "ans": [ "all above a, b and c ", "true" ] } ] }, { "ch": "For airplane parked in long time period more than 7 days we make sure that", "ansGr": [ { "ans": [ "ground airplane ", "false" ] }, { "ans": [ "disconnect main battery ", "false" ] }, { "ans": [ "disconnect APU battery ", "false" ] }, { "ans": [ "all above a, b and c ", "true" ] } ] }, { "ch": "For airplane parked in long time period more than 180 days we make sure that", "ansGr": [ { "ans": [ "APU is not to be removed from airplane ", "false" ] }, { "ans": [ "APU fuel system is to be preserved ", "false" ] }, { "ans": [ "APU fuel system is to be preserved and than APU is to be removed from airplane ", "true" ] } ] }, { "ch": "When airplane parking with hot brakes:", "ansGr": [ { "ans": [ "Do not let the parking brakes stay set ", "true" ] }, { "ans": [ "Let the parking brakes stay set ", "false" ] }, { "ans": [ "Let the parking brakes stay set in turn around only ", "false" ] } ] }, { "ch": "How to check of the status light on the nose landing gear if the airplane is on the ground and the parking brake is set :", "ansGr": [ { "ans": [ "Parking brake set is on., brake on is on. ", "false" ] }, { "ans": [ "Parking brake set is on., brake off is not on. ", "false" ] }, { "ans": [ "Parking brake set is on., brake on is on., brake off is not on. ", "true" ] } ] }, { "ch": "when using the parking brake for parking, the right hydraulic system must initially be fully pressurized and:", "ansGr": [ { "ans": [ "must be repressurized after every 16 hours ", "false" ] }, { "ans": [ "must be repressurized after every 8 hours ", "true" ] }, { "ans": [ "must be repressurized after every 24 hours ", "false" ] } ] }, { "ch": "Letters of marking or placard EXIT and EMERGENCY EXIT are in", "ansGr": [ { "ans": [ "red color ", "true" ] }, { "ans": [ "orange color ", "false" ] }, { "ans": [ "blue color ", "false" ] } ] }, { "ch": "On Vietnam Airlines B777 interior emergency escape path is marked by", "ansGr": [ { "ans": [ "lights installed on cabin floor ", "false" ] }, { "ans": [ "lights installed on passenger seat and walls ", "true" ] }, { "ans": [ "red shining paint on cabin floor ", "false" ] } ] }, { "ch": "Decal adjacent to one equipment gives", "ansGr": [ { "ans": [ "P/N of this equipment ", "false" ] }, { "ans": [ "Equipment number of this equipment ", "true" ] }, { "ans": [ "Name of this equipment ", "false" ] } ] }, { "ch": "Where is registration mark of Vietnam airlines B777 airplane located", "ansGr": [ { "ans": [ "on nose landing gear door ", "false" ] }, { "ans": [ "on upper surface of airplane wing ", "false" ] }, { "ans": [ "on lower surface of left wing and on aft fuselage ", "true" ] } ] }, { "ch": "Placard NO SMOKING IN LAVATORY is located", "ansGr": [ { "ans": [ "inside lavatory ", "false" ] }, { "ans": [ "outside lavatory ", "false" ] }, { "ans": [ "both a and b ", "true" ] } ] }, { "ch": "Red strip markings on aft nose landing doors are", "ansGr": [ { "ans": [ "used during airplane towing ", "true" ] }, { "ans": [ "used for airplane nose jacking ", "false" ] }, { "ans": [ "used to indicated hazard area during nose landing gear retraction and extension ", "false" ] } ] }, { "ch": "Where is located decal of instruction for forward cargo door operation", "ansGr": [ { "ans": [ "outside only ", "false" ] }, { "ans": [ "inside cargo compartment only ", "false" ] }, { "ans": [ "outside and inside ", "true" ] } ] }, { "ch": "Where is located decal of instruction for entry door operation", "ansGr": [ { "ans": [ "inside ", "false" ] }, { "ans": [ "outside ", "false" ] }, { "ans": [ "both a and b ", "true" ] } ] }, { "ch": "Marking FIRE EXT NOZ DO NOT COVER is located", "ansGr": [ { "ans": [ "inside of lavatory waste compartment ", "false" ] }, { "ans": [ "on cabin portable fire extinguisher ", "false" ] }, { "ans": [ "next to fire extinguisher nozzle inside cargo compartment ", "true" ] } ] }, { "ch": "Marking SMOKE DETECTION KEEP CLEAR is used for", "ansGr": [ { "ans": [ "lavatory smoke detector ", "false" ] }, { "ans": [ "engine fire detection system ", "false" ] }, { "ans": [ "cargo fire detection system ", "true" ] } ] }, { "ch": "Marking of outside entry passenger door PUSH IN RED FLAPS PULL OUT HANDLE ROTATE AS SHOWN BELOW PULL DOOR OUTWARD IS LOCATED :", "ansGr": [ { "ans": [ "Above the door ", "false" ] }, { "ans": [ "Below the door ", "false" ] }, { "ans": [ "On the door ", "true" ] } ] }, { "ch": "Marking REFULING/DEFULING INSTRUCTION is located:", "ansGr": [ { "ans": [ "Inside of the refueling door ", "true" ] }, { "ans": [ "Below the door ", "false" ] }, { "ans": [ "Outside of the refueling door ", "false" ] } ] }, { "ch": "In cockpit, marking EMERGENCY EQUIPMENT LOAD LIMIT 40 LB/18 KG is located:", "ansGr": [ { "ans": [ "Below the emergency equipment stowage ", "false" ] }, { "ans": [ "Inside the emergency equipment stowage ", "false" ] }, { "ans": [ "Above the emergency equipment stowage ", "true" ] } ] }, { "ch": "In cockpit, marking SPARE BULBS is located", "ansGr": [ { "ans": [ "Above the spare bulbs stowage ", "true" ] }, { "ans": [ "below the spare bulbs stowage ", "false" ] }, { "ans": [ "On the door of spare bulbs stowage ", "false" ] } ] }, { "ch": "With A.C ILF 206-209, marking MOBIL JET OIL II is located:", "ansGr": [ { "ans": [ "On the inlet of engine oil ", "false" ] }, { "ans": [ "On the body of engine oil tank ", "false" ] }, { "ans": [ "On the top of engine oil tank ", "true" ] } ] }, { "ch": "In the cargo compartments, marking CAUTION: SMOKE DETECTION EQUIPMENT, CARGO COMPARTMENT is located", "ansGr": [ { "ans": [ "On the left sidewall of FWD and AFT cargo ", "true" ] }, { "ans": [ "On the left sidewall of FWD cargo ", "false" ] }, { "ans": [ "On the left sidewall of AFT cargo ", "false" ] } ] }, { "ch": "In the cargo compartments, marking FIRE EXTINGUISHING EQUIPMENT, CARGO COMPARTMENT is located", "ansGr": [ { "ans": [ "On the right sidewall of AFT cargo ", "false" ] }, { "ans": [ "On the left sidewall of FWD cargo ", "false" ] }, { "ans": [ "On the right sidewall of FWD cargo ", "true" ] } ] }, { "ch": "Airplane refueling may be performed", "ansGr": [ { "ans": [ "with electrical power ", "false" ] }, { "ans": [ "without electrical power ", "false" ] }, { "ans": [ "with some refuel valves inop ", "false" ] }, { "ans": [ "all above a, b and c ", "true" ] } ] }, { "ch": "Where is possible to check hydraulic fluid level inside reservoir", "ansGr": [ { "ans": [ "on EICAS display ", "false" ] }, { "ans": [ "at indicator in ground service bay ", "true" ] }, { "ans": [ "by sight glasses installed on reservoir ", "false" ] }, { "ans": [ "all above a, b and c ", "false" ] } ] }, { "ch": "What is reservoir fluid level if both upper and lower sight glasses show dark", "ansGr": [ { "ans": [ "correctly filled ", "false" ] }, { "ans": [ "overfull ", "true" ] }, { "ans": [ "low ", "false" ] } ] }, { "ch": "For tire service we can use", "ansGr": [ { "ans": [ "nitrogen only ", "false" ] }, { "ans": [ "nitrogen and air ", "true" ] }, { "ans": [ "nitrogen or air only if nitrogen not available but we make sure that oxygen content in tire is not more than 5% by volume ", "false" ] } ] }, { "ch": "Accumulators can be serviced by", "ansGr": [ { "ans": [ "air ", "false" ] }, { "ans": [ "nitrogen only ", "true" ] }, { "ans": [ "hydraulic fluid ", "false" ] } ] }, { "ch": "Reservoir of the center hydraulic system is located ?", "ansGr": [ { "ans": [ "On the right wheel well ", "true" ] }, { "ans": [ "On the AFT strut fairing of right engine ", "false" ] }, { "ans": [ "On the AFT strut fairing of left engine ", "false" ] } ] }, { "ch": "Reservoir of the right hydraulic system is located?", "ansGr": [ { "ans": [ "On the AFT strut fairing of left engine ", "false" ] }, { "ans": [ "On the left wheel well ", "false" ] }, { "ans": [ "On the AFT strut fairing of right engine ", "true" ] } ] }, { "ch": "what happened if filling the reservoir to more than the full level and there is a check valve failure", "ansGr": [ { "ans": [ "The fluid can go into the ducts of the pneumatic system and the air conditioning packs ", "true" ] }, { "ans": [ "fluid trasfer to others system ", "false" ] }, { "ans": [ "stop the pump ", "false" ] } ] }, { "ch": "what happened if operating the hydraulic service cart while the handle of the reservoir fill selector valve is in the off position", "ansGr": [ { "ans": [ "The reservoir fill selector valve is in any possition ", "false" ] }, { "ans": [ "This can cause too much pressure in the reservoir fill system ", "true" ] }, { "ans": [ "no preesure fill connection ", "false" ] } ] }, { "ch": "when you fill the reservoir by the pressure service cart:", "ansGr": [ { "ans": [ "A maximum of 100 psi ", "false" ] }, { "ans": [ "A maximum of 120 psi ", "false" ] }, { "ans": [ "A maximum of 150 psi ", "true" ] } ] }, { "ch": "Where can you find the hydraulic reservoir drain valve?", "ansGr": [ { "ans": [ "Under hydraulic reservoirs ", "true" ] }, { "ans": [ "On the hydraulic Ground Service Bay ", "false" ] }, { "ans": [ "On the left wheel well ", "false" ] } ] }, { "ch": "the power door opening system (PDOS) pump is located ?", "ansGr": [ { "ans": [ "On the on the fan cowl ", "false" ] }, { "ans": [ "On the brackets on the fan cowl support assembly ", "true" ] }, { "ans": [ "On the main landing gear wheel well ", "false" ] } ] }, { "ch": "To fill the PDOS reservoir, it must be:", "ansGr": [ { "ans": [ "Thrust reversers in the close position ", "false" ] }, { "ans": [ "The fan cowl and thrust reversers in the open position ", "false" ] }, { "ans": [ "The fan cowl and thrust reversers in the close position ", "true" ] } ] }, { "ch": "How to check To PDOS reservoir oil level:", "ansGr": [ { "ans": [ "By the dipstick ", "true" ] }, { "ans": [ "By the sightglass ", "false" ] }, { "ans": [ "By overflow port ", "false" ] } ] }, { "ch": "If you disconnected connections in the PDOS system, how to bleed air from the system:", "ansGr": [ { "ans": [ "Cycle the fan cowl panels a minimum of two times ", "false" ] }, { "ans": [ "Cycle the thrust reversers a minimum of three times and Cycle the fan cowl panels a minimum of two times ", "true" ] }, { "ans": [ "Cycle the thrust reversers a minimum of three times ", "false" ] } ] }, { "ch": "How to Fill the IDG oil with oil exactly?", "ansGr": [ { "ans": [ "Until a minimum of 1.0 quart of oil comes out of the overflow drain hose. ", "true" ] }, { "ans": [ "until a minimum of 0.5 quart of oil comes out of the overflow drain hose. ", "false" ] }, { "ans": [ "A few drops of oil comes out of the overflow drain hose. ", "false" ] } ] }, { "ch": "what heppend if the IDG is filled with too much oil.", "ansGr": [ { "ans": [ "oil will comes into engine oil tank ", "false" ] }, { "ans": [ "oil will comes out of the overflow connector ", "false" ] }, { "ans": [ "can cause the idg to be damaged during operation. ", "true" ] } ] }, { "ch": "To check oil level of air-driven pump (ADP) assembly, what will you see if the oil level is below the sight glass", "ansGr": [ { "ans": [ "will see a reflective mirror (shiny) surface in the sight glass ", "true" ] }, { "ans": [ "will see a surface in the sight glass [3] which is not shiny. ", "false" ] }, { "ans": [ "will see the dark colour ", "false" ] } ] }, { "ch": "The maximum pressure to fill the Potable Water Tanks", "ansGr": [ { "ans": [ "More than 55 PSI ", "false" ] }, { "ans": [ "Below 55 PSI ", "true" ] }, { "ans": [ "Below 65 PSI ", "false" ] } ] }, { "ch": "Which refueling station contains Integrated Refuel Panel?", "ansGr": [ { "ans": [ "Left refueling station. ", "true" ] }, { "ans": [ "Right refueling station. ", "false" ] }, { "ans": [ "Both refueling station. ", "false" ] } ] }, { "ch": "How do you prepare to fill the Hydraulic reservoir?", "ansGr": [ { "ans": [ "Make sure that spoilers are in the down position ", "true" ] }, { "ans": [ "Make sure that parking brake is set ", "false" ] }, { "ans": [ "Make sure that Rudder is at neutral position ", "false" ] } ] }, { "ch": "Which statement is correct regarding Power door opening system (PDOS) pump oil servicing?", "ansGr": [ { "ans": [ "You must remove No.1 fairing on the strut to get access to the PDOS pump. ", "false" ] }, { "ans": [ "After the oil servicing, you must do a bleed check on the PDOS system. ", "true" ] }, { "ans": [ "The pump is installed on the fan case ", "false" ] } ] }, { "ch": "When bolt part number and nut part number use different torque value tables, to perform torque", "ansGr": [ { "ans": [ "torque value of bolt to be used ", "false" ] }, { "ans": [ "torque value of nut to be used ", "false" ] }, { "ans": [ "the lower torque value to be used ", "true" ] } ] }, { "ch": "When one torque wrench is not suitable for torque we can", "ansGr": [ { "ans": [ "use other suitable and certified torque wrench ", "false" ] }, { "ans": [ "use adapter but we need correct the toque value ", "false" ] }, { "ans": [ "a or b ", "true" ] } ] }, { "ch": "What is purpose of the index line on the sides of flexible hoses", "ansGr": [ { "ans": [ "to indicate the length of the hose ", "false" ] }, { "ans": [ "to check the hose correct alignment and make sure the hose is not twisted ", "true" ] }, { "ans": [ "to indicate the diameter of the hose ", "false" ] } ] }, { "ch": "What is correct for flexible hose installation", "ansGr": [ { "ans": [ "tighten the hose fitting by hand only ", "false" ] }, { "ans": [ "check the hose alignment and tighten the hose fitting with one wrench ", "false" ] }, { "ans": [ "tighten the hose fitting by hand firstly, check the hose alignment and tighten the hose fitting with two wrenches to prevent hose twisting ", "true" ] } ] }, { "ch": "What is correct for control cable tension check", "ansGr": [ { "ans": [ "tensionmetter applied to any position of cable to check cable tension ", "false" ] }, { "ans": [ "tensionmetter applied to cable at least 6 inches from turnbuckle or other fitting to check cable tension ", "false" ] }, { "ans": [ "let airplane minimum one hour in constant ambient temperature for airplane temperature to be stable ", "false" ] }, { "ans": [ "b and c ", "true" ] } ] }, { "ch": "What is correct for adjustment of cable tension", "ansGr": [ { "ans": [ "use cable turnbuckle ", "true" ] }, { "ans": [ "change pulley position ", "false" ] }, { "ans": [ "change cable quick stop ", "false" ] } ] }, { "ch": "Attach grounding cable to a ground and to the airplane in the following sequence:", "ansGr": [ { "ans": [ "Connect the grounding cable to an approved, identified static ground point then connect the grounding cable to approved grounding attach point on the airplane. ", "true" ] }, { "ans": [ "Connect the grounding cable to approved grounding attach point on the airplane then connect the grounding cable to an approved, identified static ground point. ", "false" ] }, { "ans": [ "a or b are correct, no need sequence when attach grounding cable to a ground and to the airplane. ", "false" ] } ] }, { "ch": "What is the precautions when using heat devices for maintenance?", "ansGr": [ { "ans": [ "Can use heat devices but inform to flight crew and ground staff before using. ", "false" ] }, { "ans": [ "Do not use heat devices in areas that are less than 100 feet from the airplane if these conditions are present: Airplane fueling, Airplane defueling, The fuel tanks are open. ", "true" ] }, { "ans": [ "Can not use heat devices for any aircraft maintenance due to heat or spark from heat devices can cause explosions and fire. ", "false" ] } ] }, { "ch": "What is/are the caution(s) when remove E/E box?", "ansGr": [ { "ans": [ "Open the applicable circuit breakers to remove electrical power. ", "false" ] }, { "ans": [ "Do not touch conductor pins or other conductors on E/E box. ", "false" ] }, { "ans": [ "Do procedure for devices that are sensitive to electrostatic discharge. ", "false" ] }, { "ans": [ "All of above ", "true" ] } ] }, { "ch": "What is NOT correct when installation of O-ring?", "ansGr": [ { "ans": [ "Lubricate the O-ring with a thin layer of the fluid used with the component or system. ", "false" ] }, { "ans": [ "Examine the old O-rings if no cuts, abrasions, deformities, and surface defects use old O-rings for installation (no need new O-rings). ", "true" ] }, { "ans": [ "Replace used O-rings with new O-rings. ", "false" ] } ] }, { "ch": "The positive pressure relief valve opens when cabin air pressure:", "ansGr": [ { "ans": [ "is higher than ambient pressure by a set value (21-32-00 p.6) ", "true" ] }, { "ans": [ "is lower than ambient pressure by a set value ", "false" ] }, { "ans": [ "is differential to the remote ambient pressure sense port by 8.95 psi ", "false" ] } ] }, { "ch": "Why should the CABIN TEMP control be set to mid range position?", "ansGr": [ { "ans": [ "To set the maximum temperature in any zone ", "false" ] }, { "ans": [ "To allow full temperature range adjustment on cabin attendant panel ", "true" ] }, { "ans": [ "To prevent cabin overheat during low altitude flight ", "false" ] } ] }, { "ch": "What does the MAN position on the FLT DECK TEMP control do?", "ansGr": [ { "ans": [ "It removes power from the trim air system. ", "false" ] }, { "ans": [ "It allows the trim air valve to be operated manually ", "true" ] }, { "ans": [ "It removes control at the cabin attendant panel. ", "false" ] } ] }, { "ch": "When does the ground crew call horn sound?", "ansGr": [ { "ans": [ "When hydraulics are pressurized. ", "false" ] }, { "ans": [ "In case of an APU fire. ", "false" ] }, { "ans": [ "Before starting engines ", "false" ] }, { "ans": [ "If the forward equipment cooling system is inoperative. ", "true" ] } ] }, { "ch": "Howmay controler doesThe air conditioning system use:", "ansGr": [ { "ans": [ "2 controlers: Cabin temperature controllers (CTCs) and Equipment cooling controllers (ECCs). ", "false" ] }, { "ans": [ "Air supply cabin pressure controllers (ASCPCs) ", "false" ] }, { "ans": [ "All above ", "true" ] } ] }, { "ch": "When the forward cargo heat valve will be close on the ground:", "ansGr": [ { "ans": [ "Smoke is detected by the E/E cooling smoke detector ", "true" ] }, { "ans": [ "Not close on ground ", "false" ] }, { "ans": [ "Fire conditions occurs in FWD cargo. ", "false" ] } ] }, { "ch": "What happens when the BULK CARGO TEMPERATURE selector is positioned to HIGH?", "ansGr": [ { "ans": [ "The compartment temperature is automatically kept at approximately 7 degrees C or 45 degrees F ", "false" ] }, { "ans": [ "The compartment temperature is automatically kept at approximately 21 degrees C or 70 degrees F ", "true" ] }, { "ans": [ "The compartment temperature is automatically kept at approximately 10 degrees C ", "false" ] } ] }, { "ch": "What is the purpose of Auto pilot flight director system?", "ansGr": [ { "ans": [ "Automatically control the airplane altitude. ", "false" ] }, { "ans": [ "Automatically control the airplane heading. ", "false" ] }, { "ans": [ "Automatically control the airplane attitude. ", "true" ] } ] }, { "ch": "What is the primary interface between pilot and auto flight director system (AFDS)?", "ansGr": [ { "ans": [ "Mode control panel (MCP) ", "true" ] }, { "ans": [ "Display control unit (CDU) ", "false" ] }, { "ans": [ "Display select panel (DSP) ", "false" ] } ] }, { "ch": "Which component causes the control wheels, control columns and rudder pedals to move during autopilot engagement?", "ansGr": [ { "ans": [ "Stepper motors ", "false" ] }, { "ans": [ "Backdrive actuators ", "true" ] }, { "ans": [ "Drive mechanism ", "false" ] } ] }, { "ch": "Where are located the autopilot disconnect switches?", "ansGr": [ { "ans": [ "On the control wheels ", "true" ] }, { "ans": [ "On the thrust levers ", "false" ] }, { "ans": [ "On the overhead panel ", "false" ] } ] }, { "ch": "Where are located the autopilot flight director computers (AFDC)?", "ansGr": [ { "ans": [ "In main equipment center ", "true" ] }, { "ans": [ "In forward equipment center ", "false" ] }, { "ans": [ "In aft equipment center ", "false" ] } ] }, { "ch": "What is the normal position of Autopilot disengage bar?", "ansGr": [ { "ans": [ "Up position ", "true" ] }, { "ans": [ "Down position ", "false" ] }, { "ans": [ "Center position ", "false" ] } ] }, { "ch": "With the autopilot engaged or disengaged, if the airplane bank angle exceeds 35 degrees, the bank angle protection (BAP) function operates. The backdrive actuators will move:", "ansGr": [ { "ans": [ "the control columns ", "false" ] }, { "ans": [ "the control wheels ", "true" ] }, { "ans": [ "the rudder pedals ", "false" ] } ] }, { "ch": "The AFDS engages all six backdrive actuators:", "ansGr": [ { "ans": [ "in autoland. ", "true" ] }, { "ans": [ "during landing phase ", "false" ] }, { "ans": [ "during take-off phase ", "false" ] } ] }, { "ch": "Which displays can show flight directors (FD) bars?", "ansGr": [ { "ans": [ "Primary flight display (PFD) ", "true" ] }, { "ans": [ "Navigation display (ND) ", "false" ] }, { "ans": [ "Autopilot display (AP) ", "false" ] } ] }, { "ch": "How the pilot engages the autopilot system?", "ansGr": [ { "ans": [ "Push an autopilot (A.P) switch on MCP ", "true" ] }, { "ans": [ "Push an autopilot (A.P) switch on control wheel ", "false" ] }, { "ans": [ "Push an autopilot (A.P) switch on thrust lever ", "false" ] } ] }, { "ch": "Which statement is not correct?", "ansGr": [ { "ans": [ "The airplane is certified for take-off with autopilot engaged ", "true" ] }, { "ans": [ "The airplane is certified for landing with autopilot engaged ", "false" ] }, { "ans": [ "The airplane is not certified for take-off with autopilot engaged ", "false" ] } ] }, { "ch": "Which autoland status cannot be seen on the PFD?", "ansGr": [ { "ans": [ "LAND 3 ", "false" ] }, { "ans": [ "LAND 2 ", "false" ] }, { "ans": [ "LAND 1 ", "true" ] } ] }, { "ch": "Which statement is correct?", "ansGr": [ { "ans": [ "Thrust management computing function (TMCF) is part of Airplane information management system (AIMS) ", "true" ] }, { "ans": [ "Thrust management computing function (TMCF) is part Auto pilot flight director system (AFDS) ", "false" ] }, { "ans": [ "Thrust management computing function (TMCF) is part Electrical load management system (EMLS). ", "false" ] } ] }, { "ch": "How many auto throttle servo motors are there?", "ansGr": [ { "ans": [ "One ", "false" ] }, { "ans": [ "Two ", "true" ] }, { "ans": [ "Three ", "false" ] } ] }, { "ch": "How can autothrottle be armed?", "ansGr": [ { "ans": [ "Push A.T ARM switch on MCP ", "true" ] }, { "ans": [ "Push A.T switch on MCP ", "false" ] }, { "ans": [ "Put thrust lever to CLB ", "false" ] } ] }, { "ch": "The HF communication system uses:", "ansGr": [ { "ans": [ "2 HF transceivers, 1 HF antenna, 2 HF couplers ", "true" ] }, { "ans": [ "2 HF transceivers, 2 HF antenna, 2 HF couplers ", "false" ] }, { "ans": [ "2 HF transceivers, 1 HF antenna, 1 HF couplers ", "false" ] } ] }, { "ch": "The HF communication transceivers position?", "ansGr": [ { "ans": [ "In the E6 rack, in AFT cargo compartment ", "true" ] }, { "ans": [ "In the MEC ", "false" ] }, { "ans": [ "In the vertical stabilizer ", "false" ] } ] }, { "ch": "Which are the HF system components in the vertical stabilizer:", "ansGr": [ { "ans": [ "2 HF communication transceivers, 2 HF antenna couplers. ", "false" ] }, { "ans": [ "2 HF communication antenna, 2 HF antenna couplers. ", "false" ] }, { "ans": [ "1 HF communication antenna, 2 HF antenna couplers. ", "true" ] } ] }, { "ch": "The VHF communication system uses:", "ansGr": [ { "ans": [ "3 VHF transceivers, 3 VHF antenna on upper fuselage ", "false" ] }, { "ans": [ "3 VHF transceivers, 3 VHF antenna on lower fuselage ", "false" ] }, { "ans": [ "3 VHF transceivers, 3 VHF antenna: 02 on upper fuselage, 01 on lower fuselage ", "true" ] } ] }, { "ch": "flight crew control the SATCOM system by:", "ansGr": [ { "ans": [ "RTPs (Radio Tuning Panel) ", "false" ] }, { "ans": [ "ACPs (Audio Control Panel) ", "false" ] }, { "ans": [ "CDUs (Control Display unit) ", "true" ] } ] }, { "ch": "communication transceivers send received audio to the SELCAL decoder.", "ansGr": [ { "ans": [ "HF communication transceivers ", "false" ] }, { "ans": [ "HF and VHF communication transceivers ", "true" ] }, { "ans": [ "VHF communication transceivers ", "false" ] } ] }, { "ch": "emergency locator transmitter (ELT) system sends emergency signals:", "ansGr": [ { "ans": [ "Automatically when it senses a large change in the airplane velocity ", "false" ] }, { "ans": [ "Manually at the flight deck with a switch on a control panel. ", "false" ] }, { "ans": [ "a or b ", "true" ] } ] }, { "ch": "are the emergency locator transmitter (ELT) and ELT antenna position?", "ansGr": [ { "ans": [ "ELT in Main Equipment Center (MEC). The ELT antenna is in vertical stabilizer ", "false" ] }, { "ans": [ "ELT in the passenger cabin above the cabin ceiling panels. The ELT antenna is above the Emergency Locator Transmitter on the outside of the aircraft. ", "true" ] }, { "ans": [ "ELT in Main Equipment Center (MEC). The ELT antenna is in lower fuselage. ", "false" ] } ] }, { "ch": "ELT antenna sends the emergency signals on the?", "ansGr": [ { "ans": [ "VHF and UHF frequencies ", "true" ] }, { "ans": [ "VHF and HF frequencies ", "false" ] }, { "ans": [ "Only VHF frequencies ", "false" ] } ] }, { "ch": "establish communication between cockpit and service interphone jacks, you need to:", "ansGr": [ { "ans": [ "Use Captain’s headset ", "false" ] }, { "ans": [ "Use First Officer’s headset ", "false" ] }, { "ans": [ "Put Service Interphone Switch (P5) to ON position ", "true" ] } ] }, { "ch": "are the functions of Ground Crew Call system?", "ansGr": [ { "ans": [ "To tell flight deck personnel that there is a call from the ground and/or ground personnel that there is a call from the flight deck ", "false" ] }, { "ans": [ "To tell ground personnel that the air data inertial reference unit (ADIRU)is on battery power or that there is an equipment cooling failure ", "false" ] }, { "ans": [ "Both a and b ", "true" ] } ] }, { "ch": "call the ground crew from flight deck, you use:", "ansGr": [ { "ans": [ "The left or right CDU ", "false" ] }, { "ans": [ "The center CDU ", "true" ] }, { "ans": [ "The Call button on P5 ", "false" ] } ] }, { "ch": "to call cockpit from the ground?", "ansGr": [ { "ans": [ "Push FLIGHT DECK CALL switch on P40 ", "true" ] }, { "ans": [ "Push GROUND CALL switch on P40 ", "false" ] }, { "ans": [ "Push FLIGHT DECK CALL switch on the center CDU ", "false" ] } ] }, { "ch": "what case will the ground crew call horn come on continuously?", "ansGr": [ { "ans": [ "When there is a call from the flight deck ", "false" ] }, { "ans": [ "When the ADIRU is on battery power ", "true" ] }, { "ans": [ "When there is a fire ", "false" ] } ] }, { "ch": "are the CVR (Cockpit Voice Recorder) system components location ?", "ansGr": [ { "ans": [ "The CVR panel, CVR microphone and CVR are in the E7-1 in the aft cabin above the ceiling. ", "false" ] }, { "ans": [ "The CVR panel, CVR microphone and CVR are in the flight deck. ", "false" ] }, { "ans": [ "The CVR panel and CVR microphone are in the flight deck, CVR is in E7-1 in the aft cabin above the ceiling. ", "true" ] } ] }, { "ch": "power RAT generator can supply?", "ansGr": [ { "ans": [ "20 KVA ", "false" ] }, { "ans": [ "15 KVA ", "false" ] }, { "ans": [ "7.5 KVA ", "true" ] } ] }, { "ch": "external power source automatically supplies power to ground handling bus?", "ansGr": [ { "ans": [ "Primary external power ", "true" ] }, { "ans": [ "Secondary external power ", "false" ] }, { "ans": [ "Primary and secondary external power ", "false" ] } ] }, { "ch": "statement is correct?", "ansGr": [ { "ans": [ "Backup generators are a variable-speed, variable-frequency type ", "true" ] }, { "ans": [ "Backup generators are a constant-speed, variable-frequency type ", "false" ] }, { "ans": [ "Backup generators are a variable-speed, constant-frequency type ", "false" ] } ] }, { "ch": "bus is normally supply power to hot battery and APU battery bus through their related battery chargers?", "ansGr": [ { "ans": [ "Ground service bus ", "true" ] }, { "ans": [ "Ground handling bus ", "false" ] }, { "ans": [ "Flight service bus ", "false" ] } ] }, { "ch": "power switch has 3 positions. Which position is momentary?", "ansGr": [ { "ans": [ "AUTO ", "false" ] }, { "ans": [ "OFF ", "false" ] }, { "ans": [ "BAT ", "true" ] } ] }, { "ch": "box will be shown on electrical synoptic display when power source is off or the breaker is open?", "ansGr": [ { "ans": [ "Amber box ", "false" ] }, { "ans": [ "White box ", "true" ] }, { "ans": [ "Green box ", "false" ] } ] }, { "ch": "page shows the IDG oil level?", "ansGr": [ { "ans": [ "Electrical synoptic page ", "false" ] }, { "ans": [ "Electrical maintenance page 1 ", "true" ] }, { "ans": [ "Electrical maintenance page 2 ", "false" ] } ] }, { "ch": "is/are the functions of electrical load management system (ELMS)?", "ansGr": [ { "ans": [ "Protect the electrical system ", "false" ] }, { "ans": [ "Control load switching devices ", "false" ] }, { "ans": [ "Protect the electrical system and control load switching devices ", "true" ] } ] }, { "ch": "primary sources of electrical power are:", "ansGr": [ { "ans": [ "The integrated drive generators (IDGs) ", "true" ] }, { "ans": [ "The integrated drive generators (IDGs) and the APU generator ", "false" ] }, { "ans": [ "The integrated drive generators (IDGs), the APU generator and External ground power ", "false" ] } ] }, { "ch": "APU generator is cooled by", "ansGr": [ { "ans": [ "Fuel ", "false" ] }, { "ans": [ "Oil ", "true" ] }, { "ans": [ "Air ", "false" ] } ] }, { "ch": "there are only two IDG operating, what happens if right IDG fails?", "ansGr": [ { "ans": [ "BU converter will power AC right bus ", "false" ] }, { "ans": [ "AC left bus will power AC right bus ", "true" ] }, { "ans": [ "STBY system will power AC right bus ", "false" ] } ] }, { "ch": "component control the load shedding?", "ansGr": [ { "ans": [ "BPCU ", "false" ] }, { "ans": [ "GCU ", "false" ] }, { "ans": [ "ELMS ", "true" ] } ] }, { "ch": "there too much oil in side the BUG, the indication on ELEC MAINTENANCE PAGE will be", "ansGr": [ { "ans": [ "OVERFILL ", "false" ] }, { "ans": [ "SERVICE ", "true" ] }, { "ans": [ "UNDERFILL ", "false" ] } ] }, { "ch": "Generator (BUG) Converter will automatically check the BUG", "ansGr": [ { "ans": [ "Right after engine shut down ", "false" ] }, { "ans": [ "When DC STBY self test ", "false" ] }, { "ans": [ "Right after the engine is started ", "true" ] } ] }, { "ch": "Magnetic Generators (PMGs) which supply power for Flight Control Computer Power Supply Assemblies (FCDC PSA) are located in", "ansGr": [ { "ans": [ "IDG ", "false" ] }, { "ans": [ "BUG ", "true" ] }, { "ans": [ "RAT ", "false" ] } ] }, { "ch": "component does the break power transfer between primary and secondary external powers ?", "ansGr": [ { "ans": [ "ELMS ", "false" ] }, { "ans": [ "GCU ", "false" ] }, { "ans": [ "BPCU ", "true" ] } ] }, { "ch": "statement is correct?", "ansGr": [ { "ans": [ "Backup converter get power from only one backup generator at any time ", "true" ] }, { "ans": [ "Backup converter get power from two backup generators at any time ", "false" ] }, { "ans": [ "Backup converter get power from all backup generators at any time. ", "false" ] } ] }, { "ch": "is located the RAT GCU?", "ansGr": [ { "ans": [ "Behind the RAT ", "false" ] }, { "ans": [ "Below P310 panel ", "true" ] }, { "ans": [ "Inside P310 panel ", "false" ] } ] }, { "ch": "how long main battery can supply standby system power?", "ansGr": [ { "ans": [ "At least 5 minutes ", "true" ] }, { "ans": [ "At least 10 minutes ", "false" ] }, { "ans": [ "At least 15 minutes ", "false" ] } ] }, { "ch": "PSA receives power source from hot battery bus?", "ansGr": [ { "ans": [ "Left PSA ", "true" ] }, { "ans": [ "Center PSA ", "false" ] }, { "ans": [ "Right PSA ", "false" ] } ] }, { "ch": "no power for the captain and first officer seats, which one can manually control:", "ansGr": [ { "ans": [ "The horizontal adjustment has a manual override. ", "false" ] }, { "ans": [ "The vertical adjustment has a manual override. ", "false" ] }, { "ans": [ "Both the horizontal adjustment has a manual override and The vertical adjustment has a manual override. ", "true" ] } ] }, { "ch": "to removes the slide/raft away from the airplane during ditching normally?", "ansGr": [ { "ans": [ "To pull the speed lacing release lanyard ", "true" ] }, { "ans": [ "To remove the girt bar from floor fittings ", "false" ] }, { "ans": [ "Use A hook knife is in the raft to cut the tether ", "false" ] } ] }, { "ch": "conditions to supply power The cargo handling system?", "ansGr": [ { "ans": [ "The ground handling bus has power, the cargo door is fully open ", "false" ] }, { "ans": [ "The ground handling bus has power, the cargo door is fully open, the SYSTEM POWER switch on the cargo handling control panel is in the ON position. ", "true" ] }, { "ans": [ "The ground handling bus has power, the SYSTEM POWER switch on the cargo handling control panel is in the ON position. ", "false" ] } ] }, { "ch": "you configure The cargo handling control system ?", "ansGr": [ { "ans": [ "No fixed configure ", "false" ] }, { "ans": [ "Yes by Cargo handling accessory panel ", "false" ] }, { "ans": [ "Yes by the switches on the cargo handling control panel ", "true" ] } ] }, { "ch": "statement about the Fuel temperature display is true?", "ansGr": [ { "ans": [ "Fuel temperature display turns amber when approaching the fuel freeze point entered in the FMS CDU ", "true" ] }, { "ans": [ "Fuel temperature in each fuel tank is displayed on the primary EICAS display. ", "false" ] }, { "ans": [ "Fuel temperature display turns amber during a fuel overheat condition. ", "false" ] } ] }, { "ch": "it possible to check at a door if the girt bar is attached to the floor fittings?", "ansGr": [ { "ans": [ "Yes, the girt bar indicator flags are colored black. ", "false" ] }, { "ans": [ "No, the girt bar indicator flags only indicate if the slide is usable. ", "false" ] }, { "ans": [ "Yes, the girt bar indicator flags are colored yellow. ", "true" ] }, { "ans": [ "No, the girt bar indicator is not visible. ", "false" ] } ] }, { "ch": "statement is true for Engine Overheat Detection?", "ansGr": [ { "ans": [ "Overheat detectors are different from Fire detectors ", "false" ] }, { "ans": [ "Overheat condition is detected by Engine Fire Detection Loops ", "true" ] }, { "ans": [ "Fuel control switch light comes on when there is an engine overheat ", "false" ] } ] }, { "ch": "statement is true for APU fire detection system?", "ansGr": [ { "ans": [ "Operates only in the air ", "false" ] }, { "ans": [ "Uses smoke detectors ", "false" ] }, { "ans": [ "Has two modes: Attended and Unattended ", "true" ] } ] }, { "ch": "The airplane has these fire extinguishing systems", "ansGr": [ { "ans": [ "Engine fire extinguishing, Bottles 1A and 1B fire immediately, bottle 2A fire after 20 minutes ", "true" ] }, { "ans": [ "Bottles 1A and 1B fire immediately, all bottles 2A, 2B, 2C fire after 20 minutes ", "false" ] }, { "ans": [ "Only bottles 1A and 1B fire immediately ", "false" ] } ] }, { "ch": "fire switch releases if the engine has a fire or", "ansGr": [ { "ans": [ "During fire/overheat test ", "true" ] }, { "ans": [ "Fuel control switch is in CUT OFF ", "false" ] }, { "ans": [ "BAT switch is ON ", "false" ] } ] }, { "ch": "can you find engine fire extinguisher bottles?", "ansGr": [ { "ans": [ "Forward cargo compartment ", "true" ] }, { "ans": [ "Aft cargo compartment ", "false" ] }, { "ans": [ "Main equipment center ", "false" ] } ] }, { "ch": "agent is used for engine and APU fire extinguishing?", "ansGr": [ { "ans": [ "Water ", "false" ] }, { "ans": [ "Halon ", "true" ] }, { "ans": [ "Powder ", "false" ] } ] }, { "ch": "do you check engine/APU fire bottles pressure switch circuit on the ground?", "ansGr": [ { "ans": [ "Push and hold the bottle pressure switch test button ", "true" ] }, { "ans": [ "Do a fire/overheat test ", "false" ] }, { "ans": [ "Weigh the bottle ", "false" ] } ] }, { "ch": "you shut down the APU by fire shutdown switch on P40, to start the APU again you need to.", "ansGr": [ { "ans": [ "Do a fire/overheat test ", "true" ] }, { "ans": [ "Power the airplane by external power ", "false" ] }, { "ans": [ "Cycle the BAT switch ", "false" ] } ] }, { "ch": "What is the hydrostatic test interval for fire extinguisher bottles?", "ansGr": [ { "ans": [ "7 years ", "false" ] }, { "ans": [ "6 years ", "false" ] }, { "ans": [ "10 years ", "true" ] } ] }, { "ch": "What is the purpose of cargo compartment fire extinguishing in-line pressure switch reset button?", "ansGr": [ { "ans": [ "To set switch contacts to open after it is latched closed by discharge pressure ", "true" ] }, { "ans": [ "To reset the switch after extinguisher bottle replacement ", "false" ] }, { "ans": [ "To set switch contacts to close after it is latched opened by discharge pressure ", "false" ] } ] }, { "ch": "is maximum service life of a fire extinguisher bottle squib?", "ansGr": [ { "ans": [ "5 years ", "false" ] }, { "ans": [ "10 years ", "true" ] }, { "ans": [ "15 years ", "false" ] } ] }, { "ch": "what temperature will the lavatory fire extinguisher bottle nozzles melt?", "ansGr": [ { "ans": [ "77ºC ", "true" ] }, { "ans": [ "100ºC ", "false" ] }, { "ans": [ "90ºC ", "false" ] } ] }, { "ch": "temperature indicator on the side of the waste container shows if there has been a fire. You can see the indicator without removing the container to look inside.", "ansGr": [ { "ans": [ "The indicator circles are normally white. Red circles show a fire. ", "false" ] }, { "ans": [ "The indicator circles are normally white. Orange circles show a fire. ", "false" ] }, { "ans": [ "The indicator circles are normally white. Black circles show a fire. ", "true" ] } ] }, { "ch": "fire and overheat test switch (FIRE/OVHT TEST) does a test of these systems:", "ansGr": [ { "ans": [ "Engine fire detection, APU fire detection ", "false" ] }, { "ans": [ "Engine fire detection, APU fire detection, Lower cargo compartment smoke detection ", "false" ] }, { "ans": [ "Engine fire detection, APU fire detection, Lower cargo compartment smoke detection, Wheel well fire detection. ", "true" ] } ] }, { "ch": "lavatory smoke detectors monitor the lavatories for smoke. Where are the Smoke indications show?", "ansGr": [ { "ans": [ "The Smoke indications show at the lavatory, at attendant stations and in the flight deck. ", "true" ] }, { "ans": [ "The Smoke indications show at the lavatory only ", "false" ] }, { "ans": [ "The Smoke indications show at the lavatory, in the flight deck. ", "false" ] } ] }, { "ch": "The High Lift Control System (HLCS) mode of operation", "ansGr": [ { "ans": [ "Primary, secondary ", "false" ] }, { "ans": [ "Primary, secondary, alternate ", "true" ] }, { "ans": [ "Primary, alternate ", "false" ] } ] }, { "ch": "which valve controls the amount of hydraulic flow to the flap and slat primary control valves in primary mode:", "ansGr": [ { "ans": [ "The flap/slat priority valve and limit valve ", "false" ] }, { "ans": [ "The limit valve ", "false" ] }, { "ans": [ "The flap/slat priority valve ", "true" ] } ] }, { "ch": "How to stop the flaps and slats at the commanded position in the secondary mode", "ansGr": [ { "ans": [ "The FSEUs command the relays to stop the electric motors ", "true" ] }, { "ans": [ "Sensors send directly signal to stop the electric motors ", "false" ] }, { "ans": [ "Slat skew sensors send signal to stop the electric motors ", "false" ] } ] }, { "ch": "Which component is not on the FLAP ADGE?", "ansGr": [ { "ans": [ "Hydraulic and electric motors ", "false" ] }, { "ans": [ "flap extend/retract relays. ", "false" ] }, { "ans": [ "Wing tip brake ", "true" ] } ] }, { "ch": "When do the control wheel stabilizer trim switches control stabilizer movement directly?", "ansGr": [ { "ans": [ "All the time. ", "false" ] }, { "ans": [ "Only during approaches ", "false" ] }, { "ans": [ "Only on the ground and in the Secondary and Direct flight control modes ", "true" ] } ] }, { "ch": "of these flight control surfaces move down and aft in proportion to trailing edge flaps extension?", "ansGr": [ { "ans": [ "Flaperons ", "true" ] }, { "ans": [ "Slats only ", "false" ] }, { "ans": [ "Krueger flaps and slats ", "false" ] } ] }, { "ch": "control is provided by :", "ansGr": [ { "ans": [ "Slats and spoilers only ", "false" ] }, { "ans": [ "Ailerons, flaperons and spoilers ", "true" ] }, { "ans": [ "Flaperons and slats ", "false" ] } ] }, { "ch": "happens when the stabilizer signal is not present or is invalid?", "ansGr": [ { "ans": [ "The EICAS message STAB GREENBAND displays ", "false" ] }, { "ans": [ "The green band on the indicator turns amber. ", "false" ] }, { "ans": [ "The green band and the pointer are not displayed ", "true" ] } ] }, { "ch": "purpose of the fuel vent system is", "ansGr": [ { "ans": [ "to make sure that a flame does not come inside the fuel tanks ", "false" ] }, { "ans": [ "to keep the pressure of the fuel tanks near the pressure of the outside atmosphere (28-10-00 p. 17). ", "true" ] }, { "ans": [ "to let fuel in the vent system return to the fuel tanks so the engines or APU can use it. ", "false" ] } ] }, { "ch": "To manually measure fuel quantity with the fuel measuring stick assemblies, you can get airplane attitude (pitch and roll) information", "ansGr": [ { "ans": [ "by using inclinometers (in the nose wheel well) and the leveling scale (in the right main wheel well) only ", "false" ] }, { "ans": [ "by using the pitch and roll data from the fuel quantity maintenance page 2 only ", "false" ] }, { "ans": [ "by using inclinometers (in the nose wheel well) and the leveling scale (in the right main wheel well) or the pitch and roll data from the fuel quantity maintenance page 2 (28-40-00 p. 22 & 25) ", "true" ] } ] }, { "ch": "Crossfeed Valves Actuators in fuel system is located", "ansGr": [ { "ans": [ "On the rear spar aft of the first fuel tank access door on the left wing ", "true" ] }, { "ans": [ "On the rear spar aft of the first fuel tank access door on the right wing ", "false" ] }, { "ans": [ "On the main landing gear wheel well ", "false" ] } ] }, { "ch": "The override/jettison pumps in fuel system is located", "ansGr": [ { "ans": [ "On the rear spar of the left tank ", "false" ] }, { "ans": [ "On the rear spar of the right tank ", "false" ] }, { "ans": [ "On the rear spar of the center tank ", "true" ] } ] }, { "ch": "what does control the crossfeed valves", "ansGr": [ { "ans": [ "The crossfeed valve switches on the P5 directly control the crossfeed valves ", "true" ] }, { "ans": [ "The ELMS send power to control the crossfeed valves ", "false" ] }, { "ans": [ "The AIMS send power to control the crossfeed valves ", "false" ] } ] }, { "ch": "fuel pumps are used for fuel jettison?", "ansGr": [ { "ans": [ "All fuel pumps are used for fuel jettison. ", "false" ] }, { "ans": [ "Left and right main tank jettison pumps only ", "false" ] }, { "ans": [ "Left and right main tank jettison pumps and the center tank jettison/override pumps ", "true" ] } ] }, { "ch": "statement about the fuel system limitation is most correct?", "ansGr": [ { "ans": [ "Main tanks must be scheduled to be full if center tank fuel is loaded ", "false" ] }, { "ans": [ "Fuel imbalance must not exceed 1000 pounds (500 kilograms). ", "false" ] }, { "ans": [ "Fuel crossfeet valves must be cloaed for landing ", "true" ] } ] }, { "ch": "Which of the following statements is true when the FUEL IMBALANCE message is displayed?", "ansGr": [ { "ans": [ "solid white fuel imbalance pointer is displayed beside the tank with the low quantity ", "false" ] }, { "ans": [ "solid Amber fuel imbalance pointer is displayed beside the tank with the low quantity ", "true" ] }, { "ans": [ "The fuel quantity indicator in the low tank turns amber ", "false" ] } ] }, { "ch": "of the following does not happen when the Fuel Control switch is placed to RUN with Autostart ON?", "ansGr": [ { "ans": [ "The spar fuel valve is armed. ", "true" ] }, { "ans": [ "The engine ignitor(s) is/are armed. ", "false" ] }, { "ans": [ "The EEC opens the valve and turns on the ignitor(s) when required. ", "false" ] } ] }, { "ch": "Before a normal ground start, the right center tank pump PRESS light is illuminated however, the EICAS message FUEL PUMP CENTER R is not displayed. Is this a normal indication?", "ansGr": [ { "ans": [ "Yes, center tank fuel is not used during engine start and the message is inhibited. ", "false" ] }, { "ans": [ "No, the EICAS message is never inhibited ", "false" ] }, { "ans": [ "Yes, one pump is electrically load shed and the message is inhibited. ", "true" ] } ] }, { "ch": "the RAT be stowed once it is deployed, in flight?", "ansGr": [ { "ans": [ "No only by engineers on the ground ", "true" ] }, { "ans": [ "Yes by RAT S/W ", "false" ] }, { "ans": [ "Yes At flight level below 22000ft ", "false" ] } ] }, { "ch": "RAT deploy in flight, how to stow RAT on ground?", "ansGr": [ { "ans": [ "Use the stow lever on the RAT checkout module and pressurized center hydraulic system ", "true" ] }, { "ans": [ "Use the stow lever on the RAT checkout module and pressurized right hydraulic system ", "false" ] }, { "ans": [ "Use the stow lever on the RAT checkout module ", "false" ] } ] }, { "ch": "the RAT deploy automatically if the C HYD system is low?", "ansGr": [ { "ans": [ "Yes ", "false" ] }, { "ans": [ "No, only when all 3 HYD systems has to be loss of hydraulic pressure ", "true" ] }, { "ans": [ "Yes if loss of center and left hydraulic pressure ", "false" ] } ] }, { "ch": "kind of EDP pumps?", "ansGr": [ { "ans": [ "EDP pump is an axial-piston, variable displacement, hydraulic pump assembly ", "true" ] }, { "ans": [ "EDP pump is a centrifugal pump ", "false" ] }, { "ans": [ "EDP pump is a gear pump ", "false" ] } ] }, { "ch": "overspeed shutdown system has a latching function that keeps the ADP off. How to reset", "ansGr": [ { "ans": [ "Test on MAT ", "true" ] }, { "ans": [ "Put ADP switch to OFF then ON ", "false" ] }, { "ans": [ "Test LSCU ( Logic and control unit) ", "false" ] } ] }, { "ch": "center hydraulic system pressure relief valve open when", "ansGr": [ { "ans": [ "at a pressure of 3700 3900 psid. ", "true" ] }, { "ans": [ "at a pressure of 3200 3500 psid. ", "false" ] }, { "ans": [ "at a pressure of 3500 3700 psid. ", "false" ] } ] }, { "ch": "Where is a center hydraulic system pressure relief valve?", "ansGr": [ { "ans": [ "on the keelbeam in the right wheel well. ", "true" ] }, { "ans": [ "on the left wing-to-body fairing behind the left wheel well. ", "false" ] }, { "ans": [ "on the right wing-to-body fairing behind the left wheel well. ", "false" ] } ] }, { "ch": "Where is a center hydraulic system pressure relief valve?", "ansGr": [ { "ans": [ "the right wheel well ", "false" ] }, { "ans": [ "on the forward side of the aft bulkhead of the stabilizer compartment ", "true" ] }, { "ans": [ "the right wheel well ", "false" ] } ] }, { "ch": "Hydraulic reservoir pressure “LO” shows on the hydraulic maintenance page, mean that", "ansGr": [ { "ans": [ "the pressure is 25 psia or less ", "false" ] }, { "ans": [ "the pressure is 27 psia or less ", "false" ] }, { "ans": [ "the pressure is 21 psia or less. ", "true" ] } ] }, { "ch": "what indication if a hydraulich pump temperature transducer fault is detected", "ansGr": [ { "ans": [ "Shown advisory messages ", "false" ] }, { "ans": [ "shown”Blank” on the hydraulic maintenance page ", "true" ] }, { "ans": [ "No indication ", "false" ] } ] }, { "ch": "Which slats are heated to prevent icing?", "ansGr": [ { "ans": [ "3,4,5 and 10,11,12 ", "true" ] }, { "ans": [ "All 12 slats ", "false" ] }, { "ans": [ "4,5,6 and 11,12,13 ", "false" ] } ] }, { "ch": "What control the wing anti-ice valve?", "ansGr": [ { "ans": [ "AIMS ", "false" ] }, { "ans": [ "ACIPS control card ", "true" ] }, { "ans": [ "HYDIM cards ", "false" ] } ] }, { "ch": "When WAI selector is selected to ON, does WAI system always operate?", "ansGr": [ { "ans": [ "Yes ", "false" ] }, { "ans": [ "Yes if operational mode inhibit is not active ", "true" ] }, { "ans": [ "Yes if the whole system is in good condition ", "false" ] } ] }, { "ch": "Purpose of Controller Air Cooler (CAC) is to decrease the temperature of engine bleed air that goes to.", "ansGr": [ { "ans": [ "EAI valve controller ", "true" ] }, { "ans": [ "EAI valve ", "false" ] }, { "ans": [ "Ice detectors ", "false" ] } ] }, { "ch": "How do you remove power from the flight deck window heating system for maintenance?", "ansGr": [ { "ans": [ "Select window heat switches on P5 to OFF ", "false" ] }, { "ans": [ "Select window heat switches on P5 and Backup window heat switches on P5 to OFF ", "false" ] }, { "ans": [ "Select window heat switches on P5 and Backup window heat switches on P61 to OFF ", "true" ] } ] }, { "ch": "Is there a rain repellent fluid system on B777?", "ansGr": [ { "ans": [ "Yes ", "false" ] }, { "ans": [ "No, a hydrophobic coating on each fwd window repels rain ", "true" ] }, { "ans": [ "No, rain repellent agent is dangerous ", "false" ] } ] }, { "ch": "How does the ice detected?", "ansGr": [ { "ans": [ "Ice detector probe heater cycle determine a wing or engine icing condition ", "true" ] }, { "ans": [ "Ice detector vibration frequency determine a wing or engine icing condition ", "false" ] }, { "ans": [ "Ice detector temperature probe gives indication of icing condition ", "false" ] } ] }, { "ch": "How is landscape camera window heated?", "ansGr": [ { "ans": [ "Electric heating film in the window lamination supplies heat to the window ", "true" ] }, { "ans": [ "Two heat resistors supply heat to the window ", "false" ] }, { "ans": [ "WHCU supply heat to the window ", "false" ] } ] }, { "ch": "The ice and rain protection system keeps ice from forming on these airplane components:", "ansGr": [ { "ans": [ "Wing/ Engine cowl leading edges, Air data probes, Flight deck window, Landscape camera window (if installed). ", "false" ] }, { "ans": [ "Wing/ Engine cowl leading edges, Air data probes, Flight deck window, Landscape camera window (if installed), Water and waste system lines and drains. ", "true" ] }, { "ans": [ "Wing/ Engine cowl leading edges, Flight deck window, Landscape camera window (if installed), Water and waste system lines and drains. ", "false" ] } ] }, { "ch": "is located the WAI valve access door?", "ansGr": [ { "ans": [ "Bottom of wing leading edge, inboard of engine strut. ", "false" ] }, { "ans": [ "Bottom of wing leading edge, outboard of engine strut ", "true" ] }, { "ans": [ "Bottom of wing trailing edge, inboard of engine strut ", "false" ] } ] }, { "ch": "total air temperature probe (TAT) is heated by:", "ansGr": [ { "ans": [ "Hot air from pneumatic system ", "false" ] }, { "ans": [ "Electric heater ", "true" ] }, { "ans": [ "Electric heater when A.C on ground and hot air when A.C in the air. ", "false" ] } ] }, { "ch": "valve symbols of WAI show amber circle with an amber cross through it on Air Synoptic Display:", "ansGr": [ { "ans": [ "Valve open ", "false" ] }, { "ans": [ "Valve not in commanded position ", "true" ] }, { "ans": [ "Valve position data not available ", "false" ] } ] }, { "ch": "windows have a back up heat system?", "ansGr": [ { "ans": [ "Window No.1 ", "true" ] }, { "ans": [ "Window No.2 ", "false" ] }, { "ans": [ "Window No.3 ", "false" ] } ] }, { "ch": "can you enable the landscape camera window heat?", "ansGr": [ { "ans": [ "use the window heat sw for the L fwd flight compartment. ", "true" ] }, { "ans": [ "use the window heat sw for the R fwd flight compartment. ", "false" ] }, { "ans": [ "both ", "false" ] } ] }, { "ch": "statements are true?", "ansGr": [ { "ans": [ "WAI and EAI use bleed air of pneumatic system for ice protection ", "false" ] }, { "ans": [ "WAI and EAI use bleed air of high stage bleed port on engine for ice protection ", "false" ] }, { "ans": [ "WAI use bleed air of pneumatic system and EAI use bleed air of high stage bleed port on engine for ice protection ", "true" ] } ] }, { "ch": "What is the function of ARINC signal gateway card (ASG)?", "ansGr": [ { "ans": [ "Change data format between ARINC 429 and ARINC 629 ", "true" ] }, { "ans": [ "Convert data format from ARINC 469 to ARINC 429 ", "false" ] }, { "ans": [ "Convert data format from ARINC 429 to ARINC 629 ", "false" ] } ] }, { "ch": "Which system card files have ARINC signal gateway card (ASG)?", "ansGr": [ { "ans": [ "Left system card file ", "false" ] }, { "ans": [ "Right system card files ", "false" ] }, { "ans": [ "Left and right system card files ", "true" ] } ] }, { "ch": "Which data is not shown by the clock?", "ansGr": [ { "ans": [ "Elapse time ", "false" ] }, { "ans": [ "Chronograph time ", "false" ] }, { "ans": [ "Local time ", "true" ] } ] }, { "ch": "Flight data recorder system (FDRS) is not operated on ground?", "ansGr": [ { "ans": [ "When the engine is not running. ", "true" ] }, { "ans": [ "When the engine is starting. ", "false" ] }, { "ans": [ "When the engine is running. ", "false" ] } ] }, { "ch": "Which color flight data recorder (FDR) is?", "ansGr": [ { "ans": [ "Black ", "false" ] }, { "ans": [ "Red ", "false" ] }, { "ans": [ "Orange ", "true" ] } ] }, { "ch": "Which data is sent to the printer with highest priority?", "ansGr": [ { "ans": [ "Flight deck communication function (FDCF) data ", "true" ] }, { "ans": [ "Central maintenance computing function (CMCF) data ", "false" ] }, { "ans": [ "Airplane condition monitoring function (ACMF) data ", "false" ] } ] }, { "ch": "How does the user interface with Aircraft condition monitoring system?", "ansGr": [ { "ans": [ "Through maintenance access terminal ", "true" ] }, { "ans": [ "Through multifunction display ", "false" ] }, { "ans": [ "Through control display unit ", "false" ] } ] }, { "ch": "Quick access recorder (QAR records data on?", "ansGr": [ { "ans": [ "Memory card ", "false" ] }, { "ans": [ "Floppy disk ", "false" ] }, { "ans": [ "Optical disk ", "true" ] } ] }, { "ch": "What does AIMS stand for?", "ansGr": [ { "ans": [ "Airplane interface monitoring system ", "false" ] }, { "ans": [ "Airplane information monitoring system ", "true" ] }, { "ans": [ "Airplane information management system ", "false" ] } ] }, { "ch": "How many Input/Outputs module (IOM) does each AIMS cabinet have?", "ansGr": [ { "ans": [ "Two ", "false" ] }, { "ans": [ "Three ", "false" ] }, { "ans": [ "Four ", "true" ] } ] }, { "ch": "How do you determine the AIMS block point installed on the airplane?", "ansGr": [ { "ans": [ "Perform a ground test ", "false" ] }, { "ans": [ "Perform a LRU identification. ", "false" ] }, { "ans": [ "Perform a configuration check. ", "true" ] } ] }, { "ch": "Which system provides stall warning alert?", "ansGr": [ { "ans": [ "Airplane information management system (AIMS) ", "false" ] }, { "ans": [ "Flight data recording system (FDRS) ", "false" ] }, { "ans": [ "Warning electronic system (WES) ", "true" ] } ] }, { "ch": "Which display unit does not receive information from AIMS cabinets?", "ansGr": [ { "ans": [ "Primary flight display ", "false" ] }, { "ans": [ "Navigation display ", "false" ] }, { "ans": [ "Integrating display. ", "true" ] } ] }, { "ch": "Display select panel (DSP) controls the format on which display units?", "ansGr": [ { "ans": [ "The two inboard and the center upper display units ", "false" ] }, { "ans": [ "The two outboard and the center lower display units ", "false" ] }, { "ans": [ "The two inboard and the center lower display units ", "true" ] } ] }, { "ch": "Which display shows Gear door information?", "ansGr": [ { "ans": [ "Door synoptic ", "false" ] }, { "ans": [ "Gear synoptic ", "true" ] }, { "ans": [ "Hydraulic synoptic ", "false" ] } ] }, { "ch": "How do you open nose landing gear door for ground maintenance", "ansGr": [ { "ans": [ "Use gear door control switch on P40 panel ", "false" ] }, { "ans": [ "Use gear door control switch on P56 panel ", "true" ] }, { "ans": [ "Use gear door control switch on P28 panel ", "false" ] } ] }, { "ch": "Red light in landing gear compartment indicated that", "ansGr": [ { "ans": [ "Landing gear door is fully opened ", "false" ] }, { "ans": [ "Landing gear door is fully closed ", "false" ] }, { "ans": [ "It is unsafe condition ", "true" ] } ] }, { "ch": "What is the indication of landing gear position on upper EICAS display when airplane is in cruise with all landing gears up", "ansGr": [ { "ans": [ "No indication ", "true" ] }, { "ans": [ "One UP white box ", "false" ] }, { "ans": [ "Three UP white box ", "false" ] } ] }, { "ch": "What happen to streering tillers when you push rudder pedal to move the rudder", "ansGr": [ { "ans": [ "Always move ", "false" ] }, { "ans": [ "Never move ", "false" ] }, { "ans": [ "Move if nose landing gear extended ", "true" ] } ] }, { "ch": "How many sensors do tail strike system have", "ansGr": [ { "ans": [ "No sensor becaused it is open/short circuit ", "true" ] }, { "ans": [ "1 sensor ", "false" ] }, { "ans": [ "2 sensors ", "false" ] } ] }, { "ch": "On EICAS, at landing gear position display area there is only one box with DOWN inside. It means", "ansGr": [ { "ans": [ "One main landing gear is extended and locked ", "false" ] }, { "ans": [ "Only nose landing gear is extended and locked ", "false" ] }, { "ans": [ "All landing gears are extended and locked ", "true" ] } ] }, { "ch": "What does the GEAR DOOR (Advisory) indicate?", "ansGr": [ { "ans": [ "The one or more landing gear doors are not closed 40 seconds after landing gear lever movement. ", "true" ] }, { "ans": [ "The one landing gear doors are not closed 40 seconds after landing gear lever movement only ", "false" ] }, { "ans": [ "Both landing gear doors are not closed 40 seconds after landing gear lever movement only ", "false" ] } ] }, { "ch": "When does RTO automatically apply maximum brake pressure?", "ansGr": [ { "ans": [ "When the thrust levers are retarded to idle above 85 knots ", "true" ] }, { "ans": [ "When a thrust lever is retarded to idle. ", "false" ] }, { "ans": [ "When the speedbrake lever reaches the UP position. ", "false" ] } ] }, { "ch": "Where is located master dim and test card file:", "ansGr": [ { "ans": [ "In main equipment center ", "false" ] }, { "ans": [ "In coat storage area in flight deck ", "true" ] }, { "ans": [ "In P61 maintenance panel ", "false" ] } ] }, { "ch": "Power for indirect ceiling lights and sidewall lights is from:", "ansGr": [ { "ans": [ "Ground handling bus ", "false" ] }, { "ans": [ "Ground service bus ", "true" ] }, { "ans": [ "Standby bus ", "false" ] } ] }, { "ch": "Fasten seatbelt lights are controlled from:", "ansGr": [ { "ans": [ "CSCP ", "false" ] }, { "ans": [ "CACP ", "false" ] }, { "ans": [ "Cockpit ", "true" ] } ] }, { "ch": "Where is located the lavatory call reset switch", "ansGr": [ { "ans": [ "At flight attendant panel ", "false" ] }, { "ans": [ "Behind mirror inside lavatory ", "false" ] }, { "ans": [ "Above lavatory door on external wall of lavatory ", "true" ] } ] }, { "ch": "When does lavatory light go to dim mode", "ansGr": [ { "ans": [ "Airplane is on ground and lavatory door is locked ", "false" ] }, { "ans": [ "Airplane is in the air and lavatory door is locked ", "false" ] }, { "ans": [ "Airplane is in the air and lavatory door is not locked ", "true" ] } ] }, { "ch": "Where are located the emergency light power supplies", "ansGr": [ { "ans": [ "Behind air grills ", "false" ] }, { "ans": [ "Beside passenger entry doors ", "false" ] }, { "ans": [ "Above passenger entry doors ", "true" ] } ] }, { "ch": "What happen if you push emergency light test switch on attendant panel at door 1L", "ansGr": [ { "ans": [ "All interior emergency lights will come on for 1 minute ", "false" ] }, { "ans": [ "All exterior emergency lights will come on for 1 minute ", "false" ] }, { "ans": [ "All interior and exterior emergency lights will come on for 1 minute ", "true" ] } ] }, { "ch": "Advisory message EMER LIGHTS is not shown if emergency light switch on P5 panel is set to", "ansGr": [ { "ans": [ "ON ", "false" ] }, { "ans": [ "OFF ", "false" ] }, { "ans": [ "ARM ", "true" ] } ] }, { "ch": "Which color is navigation light on forward of left wing tip", "ansGr": [ { "ans": [ "Red ", "true" ] }, { "ans": [ "Green ", "false" ] }, { "ans": [ "White ", "false" ] } ] }, { "ch": "The beacons and strobes are redundant systems.The two beacon lights flash at the same time and:", "ansGr": [ { "ans": [ "Three strobe lights also flash at the same time and at the same time as the beacon lights. ", "false" ] }, { "ans": [ "Three strobe lights also flash at the same time, but not at the same time as the beacon lights. ", "true" ] }, { "ans": [ "Three strobe lights do not flash at the same time ", "false" ] } ] }, { "ch": "Where is located the spare lamp box?", "ansGr": [ { "ans": [ "In left side of flight deck above coat storage area ", "true" ] }, { "ans": [ "In right side of flight deck above MAT ", "false" ] }, { "ans": [ "In main equipment center ", "false" ] } ] }, { "ch": "Where is located the floor light control switch in cockpit", "ansGr": [ { "ans": [ "P5 panel ", "false" ] }, { "ans": [ "P61 panel ", "false" ] }, { "ans": [ "P8 panel ", "true" ] } ] }, { "ch": "How do you make dome and flood light come fully bright:", "ansGr": [ { "ans": [ "Push OVRD switch ", "false" ] }, { "ans": [ "Push STORM switch ", "true" ] }, { "ans": [ "Push BRIGHT switch ", "false" ] } ] }, { "ch": "Which power supply for the Cargo Loading Lights?", "ansGr": [ { "ans": [ "Ground handling bus ", "true" ] }, { "ans": [ "Ground service bus ", "false" ] }, { "ans": [ "Main AC bus ", "false" ] } ] }, { "ch": "What statement true relate to the anti-collision lights?", "ansGr": [ { "ans": [ "Do not touch the power supply for three minutes after you remove the power ", "false" ] }, { "ans": [ "Do not touch the lamp with your bare hands. ", "false" ] }, { "ans": [ "Both are correct ", "true" ] } ] }, { "ch": "What air pressure(s) used by ADIRU and SAARU to calculate airspeed", "ansGr": [ { "ans": [ "Static air pressure ", "false" ] }, { "ans": [ "Pitot air pressure ", "false" ] }, { "ans": [ "Both pitot and static air pressures ", "true" ] } ] }, { "ch": "The piot-static system get static air pressure from", "ansGr": [ { "ans": [ "Flush static port on the fuselage ", "true" ] }, { "ans": [ "Static port on pitot probe ", "false" ] }, { "ans": [ "Static port on engine cowls ", "false" ] } ] }, { "ch": "What statement is not true", "ansGr": [ { "ans": [ "ADM & SADM are interchangeble ", "true" ] }, { "ans": [ "Pitot ADM & static ADM are interchangeble ", "false" ] }, { "ans": [ "Pitot SADM & static SADM are interchangeble ", "false" ] } ] }, { "ch": "What is indicated on standby airspeed indicator when aircraft on ground and not moving", "ansGr": [ { "ans": [ "0 knots ", "false" ] }, { "ans": [ "30 knots ", "true" ] }, { "ans": [ "50 knots ", "false" ] } ] }, { "ch": "When pitot probe is low power heated", "ansGr": [ { "ans": [ "Airplane is onground with an engine running ", "true" ] }, { "ans": [ "Computed airspeed is more than 50 knots ", "false" ] }, { "ans": [ "Airplane is in the air ", "false" ] } ] }, { "ch": "When ADIRU loses primary power, the ground crew call horn will come on if", "ansGr": [ { "ans": [ "Airplane on ground with battery switch OFF and ADIRU switch ON ", "true" ] }, { "ans": [ "Airplane on ground with battery switch ON and ADIRU switch ON ", "false" ] }, { "ans": [ "Airplane on ground with battery switch ON and ADIRU switch OFF ", "false" ] } ] }, { "ch": "From which power supply assembly SAARU get the power", "ansGr": [ { "ans": [ "Left power supply assembly ", "false" ] }, { "ans": [ "Center power supply assembly ", "true" ] }, { "ans": [ "Right power supply assembly ", "false" ] } ] }, { "ch": "TAT probe is heated", "ansGr": [ { "ans": [ "When airplane is on the ground ", "false" ] }, { "ans": [ "When airplane is in the air ", "true" ] }, { "ans": [ "Only in icing conditions ", "false" ] } ] }, { "ch": "What time is provided by GPS system", "ansGr": [ { "ans": [ "UTC time ", "true" ] }, { "ans": [ "Local time ", "false" ] }, { "ans": [ "Both UTC and local time ", "false" ] } ] }, { "ch": "Which guidance to the runway provided by ILS in normal mode", "ansGr": [ { "ans": [ "Vertical guidance ", "false" ] }, { "ans": [ "Lateral guidance ", "false" ] }, { "ans": [ "Both are correct ", "true" ] } ] }, { "ch": "What kind of distance is provide by DME", "ansGr": [ { "ans": [ "Vertical distance ", "false" ] }, { "ans": [ "Horizontal distance ", "false" ] }, { "ans": [ "Slant range distance ", "true" ] } ] }, { "ch": "On weather radar display, which color indicated turbulance", "ansGr": [ { "ans": [ "Yellow ", "false" ] }, { "ans": [ "Red ", "false" ] }, { "ans": [ "Magenta ", "true" ] } ] }, { "ch": "Windshear symbol on ND display are", "ansGr": [ { "ans": [ "Red and yellow bars ", "false" ] }, { "ans": [ "Red and black bars ", "true" ] }, { "ans": [ "Yellow and black bars ", "false" ] } ] }, { "ch": "Which page is used to check the effectivity date of navigation data base", "ansGr": [ { "ans": [ "Ident page ", "true" ] }, { "ans": [ "Nav data page ", "false" ] }, { "ans": [ "Maint page ", "false" ] } ] }, { "ch": "Center pitot probe is located on", "ansGr": [ { "ans": [ "Left side of aircraft ", "false" ] }, { "ans": [ "Right side of aircraft ", "true" ] }, { "ans": [ "Bottom of aircraft ", "false" ] } ] }, { "ch": "Where is located the left GPS antenna", "ansGr": [ { "ans": [ "On the top of aircraft ", "true" ] }, { "ans": [ "On the bottom of aircraft ", "false" ] }, { "ans": [ "On vertical stabilizer ", "false" ] } ] }, { "ch": "Where can you check the crew oxygen pressure", "ansGr": [ { "ans": [ "At cylinder gage ", "false" ] }, { "ans": [ "At status page ", "false" ] }, { "ans": [ "Both are correct ", "true" ] } ] }, { "ch": "How many crew oxygen masks are installed on B777", "ansGr": [ { "ans": [ "2 ", "false" ] }, { "ans": [ "4 ", "true" ] }, { "ans": [ "6 ", "false" ] } ] }, { "ch": "What oxygen is supply for crew in crew rest area in case of decompression", "ansGr": [ { "ans": [ "Oxygen from crew oxygen cylinder ", "false" ] }, { "ans": [ "Oxygen from portable oxygen bottle ", "false" ] }, { "ans": [ "Oxygen from chemical oxygen generator ", "true" ] } ] }, { "ch": "The oxygen overboard discharged disk is", "ansGr": [ { "ans": [ "Green color ", "true" ] }, { "ans": [ "Blue color ", "false" ] }, { "ans": [ "Red color ", "false" ] } ] }, { "ch": "The Crew oxygen bleed valve is located", "ansGr": [ { "ans": [ "The valve is on the lower, left side of the MEC. ", "true" ] }, { "ans": [ "The valve is on the upper, left side of the MEC. ", "false" ] }, { "ans": [ "The valve is on the lower, right side of the MEC. ", "false" ] } ] }, { "ch": "What happened when flight crew oxygen cylinder pressure gets above safe cylinder limits?", "ansGr": [ { "ans": [ "An overpressure valve will open ", "false" ] }, { "ans": [ "The thermal relief frangible disc in the fitting breaks to release oxygen ", "true" ] }, { "ans": [ "An shutoff valve will open ", "false" ] } ] }, { "ch": "Portable oxygen equipment gives the oxygen flow to the Oxygen mask when:", "ansGr": [ { "ans": [ "You connect the mask hose to the regulator ", "false" ] }, { "ans": [ "Connect the mask and open the regulator valve ", "false" ] }, { "ans": [ "Connect the mask and open the shutoff valve. ", "true" ] } ] }, { "ch": "In the passenger oxygen system: The chemical reaction that generates oxygen starts", "ansGr": [ { "ans": [ "when you pull down on the mask. ", "true" ] }, { "ans": [ "When you push the passenger oxygen switch to drop the masks manually. ", "false" ] }, { "ans": [ "When the masks drop automatically ", "false" ] } ] }, { "ch": "An advisory message shows “ CREW OXYGEN LOW”", "ansGr": [ { "ans": [ "if the bottle pressure goes below 600psi. ", "false" ] }, { "ans": [ "if the bottle pressure goes below 400 psi. ", "false" ] }, { "ans": [ "if the bottle pressure goes below 500 psi. ", "true" ] } ] }, { "ch": "How many high pressure ground connection are installed on B777", "ansGr": [ { "ans": [ "2 connections ", "false" ] }, { "ans": [ "3 connections ", "true" ] }, { "ans": [ "4 connections ", "false" ] } ] }, { "ch": "Engine bleed air is used for", "ansGr": [ { "ans": [ "FWD cargo heat, packs, trim air ", "false" ] }, { "ans": [ "Pack and APU & engine starting ", "true" ] }, { "ans": [ "All above ", "false" ] } ] }, { "ch": "does the backup mode latches the PRSOV closed", "ansGr": [ { "ans": [ "Engine strut duct leak ", "false" ] }, { "ans": [ "Engine bleed overtemperature,Engine strut duct leak,Engine bleed overpressure ", "true" ] }, { "ans": [ "Engine bleed overpressure,Engine strut duct leak ", "false" ] } ] }, { "ch": "happen if the engine bleed switch is set to the out (OFF) position", "ansGr": [ { "ans": [ "the primary mode commands the HPSOV and the PRSOV to close and the FAMV to open. ", "true" ] }, { "ans": [ "The HPSOV and the PRSOV to close ", "false" ] }, { "ans": [ "Only the FAMV to close. ", "false" ] } ] }, { "ch": "is true for external air source connect to the main pneumatic distribution system", "ansGr": [ { "ans": [ "Apply electrical power before apply pneumatic power and vice versa ", "true" ] }, { "ans": [ "Apply pneumatic power before apply pneumatic power and vice versa ", "false" ] }, { "ans": [ "Apply any of them ", "false" ] } ] }, { "ch": "What is true for external air source connect to the pneumatic distribution system", "ansGr": [ { "ans": [ "Do not supply external air source greater than 60 PSI and/or 232C (450F) ", "false" ] }, { "ans": [ "Do not supply external air source greater than 50 PSI and/or 232C (450F) ", "true" ] }, { "ans": [ "Do not supply external air source greater than 70 PSI and/or 232C (450F) ", "false" ] } ] }, { "ch": "L ENG and the R ENG switches have an annunciator light that comes on when:", "ansGr": [ { "ans": [ "the pressure regulation and shutoff valve (PRSOV) is set to OFF ", "true" ] }, { "ans": [ "the fan air modulating valve(FAMV) is set to OFF ", "false" ] }, { "ans": [ "the pressure regulation and shutoff valve (PRSOV) is set to ON ", "false" ] } ] }, { "ch": "How to make sure the actual engine bleed valve (PRSOV) position", "ansGr": [ { "ans": [ "shown on the air synoptic display ", "false" ] }, { "ans": [ "Shown on the maintenance page ", "false" ] }, { "ans": [ "do a check the position indicator on the valve. ", "true" ] } ] }, { "ch": "After application of de-icing fluids to the exterior of the airplane, how long should you wait before restoring normal Engine and APU bleed air operation?", "ansGr": [ { "ans": [ "5 minutes ", "false" ] }, { "ans": [ "Approximately 1 minute ", "true" ] }, { "ans": [ "Normal bleed air operation is allowed during de-icing procedures. ", "false" ] } ] }, { "ch": "How many potable water tanks are installed on B777", "ansGr": [ { "ans": [ "One ", "false" ] }, { "ans": [ "Two ", "false" ] }, { "ans": [ "Three ", "true" ] } ] }, { "ch": "Where can you check the water level remained in the tanks", "ansGr": [ { "ans": [ "CSCP at door 1L ", "true" ] }, { "ans": [ "CACP at door 2L ", "false" ] }, { "ans": [ "CACP at door 4L ", "false" ] } ] }, { "ch": "Where can you fill the water tanks", "ansGr": [ { "ans": [ "At aft potable water service panel ", "true" ] }, { "ans": [ "At mid potable water service panel ", "false" ] }, { "ans": [ "At forward potable water service panel ", "false" ] } ] }, { "ch": "Lavatory water heater is located", "ansGr": [ { "ans": [ "Next to water tank ", "false" ] }, { "ans": [ "Below sink ", "true" ] }, { "ans": [ "Behind mirror ", "false" ] } ] }, { "ch": "Where can you find water isolation/drain valve handle", "ansGr": [ { "ans": [ "Above door 1L ", "false" ] }, { "ans": [ "Above door 2L ", "true" ] }, { "ans": [ "Above door 4L ", "false" ] } ] }, { "ch": "The lavatory sink and galley drain water system is called", "ansGr": [ { "ans": [ "Brown water drain system ", "false" ] }, { "ans": [ "Gray water drain system ", "true" ] }, { "ans": [ "Blue water drain system ", "false" ] } ] }, { "ch": "How many potable water tank are there on VNA B777?", "ansGr": [ { "ans": [ "3 ", "true" ] }, { "ans": [ "2 ", "false" ] }, { "ans": [ "1 ", "false" ] } ] }, { "ch": "Where can you find potable water system isolation/drain valve in passenger cabin?", "ansGr": [ { "ans": [ "Above the ceiling aft of door 4 left ", "false" ] }, { "ans": [ "Above the ceiling fwd of door 4 left ", "false" ] }, { "ans": [ "Above the ceiling aft of door 2 left ", "true" ] } ] }, { "ch": "Where can you find water shutoff valve in the lavatory?", "ansGr": [ { "ans": [ "Under the water sink ", "false" ] }, { "ans": [ "Behind the mirror ", "true" ] }, { "ans": [ "Behind the waste bin ", "false" ] } ] }, { "ch": "Which of the following statements is true", "ansGr": [ { "ans": [ "The fill/overflow valve lets water flow overboard when tanks are full ", "true" ] }, { "ans": [ "The fill/overflow valve opens to turn on air compressor ", "false" ] }, { "ans": [ "The fill/overflow valve lets air flow into the tanks ", "false" ] } ] }, { "ch": "Where can you find potable water system drain valves?", "ansGr": [ { "ans": [ "In the forward and aft drain panels ", "false" ] }, { "ans": [ "In the cargo compartments ", "true" ] }, { "ans": [ "In the forward most and aft most lavatory ", "false" ] } ] }, { "ch": "The potable water isolation valves isolate the overhead water distribution lines to", "ansGr": [ { "ans": [ "Forward and mid lavatories and galleys ", "true" ] }, { "ans": [ "Forward lavatories and galleys ", "false" ] }, { "ans": [ "Mid lavatories and galleys ", "false" ] } ] }, { "ch": "What do you do to prevent cabin pressure go out through the vacuum system if the flush valve fails in open position", "ansGr": [ { "ans": [ "Push manual handle to close the valve ", "false" ] }, { "ans": [ "Pull manual handle to close the valve ", "true" ] }, { "ans": [ "Disconnect electric connector to flush control handle ", "false" ] } ] }, { "ch": "How do you keep the flush valve in open position for maintenance?", "ansGr": [ { "ans": [ "Remove power to the flush control module ", "false" ] }, { "ans": [ "Push manual handle ", "false" ] }, { "ans": [ "Push maintenance switch on the flush control module one time ", "true" ] } ] }, { "ch": "When do the vacuum blowers operate?", "ansGr": [ { "ans": [ "Below 16000ft ", "true" ] }, { "ans": [ "Above 16000ft ", "false" ] }, { "ans": [ "Any time flush switch is activated ", "false" ] } ] }, { "ch": "What air is used to pressurize potable water tank?", "ansGr": [ { "ans": [ "Air from compressor only ", "false" ] }, { "ans": [ "Air from pneumatic system or from compressor ", "true" ] }, { "ans": [ "No air is required ", "false" ] } ] }, { "ch": "Where is the vacuum blowers located?", "ansGr": [ { "ans": [ "At the forward of the forward waste tank. ", "true" ] }, { "ans": [ "At the after of the forward waste tank. ", "false" ] }, { "ans": [ "Under of the forward waste tank. ", "false" ] } ] }, { "ch": "is the air compressor located?", "ansGr": [ { "ans": [ "On the waste tank ", "false" ] }, { "ans": [ "On the water tank ", "false" ] }, { "ans": [ "The compressor is on the right side of the bulk cargo compartment ", "true" ] } ] }, { "ch": "To prevents the water tank pressurization system", "ansGr": [ { "ans": [ "The pressure relief valve prevents pressure of more than 60 psig ", "true" ] }, { "ans": [ "The pressure relief valve prevents pressure of more than 50 psig ", "false" ] }, { "ans": [ "The pressure relief valve prevents pressure of more than 65 psig ", "false" ] } ] }, { "ch": "When does The air compressor operate?", "ansGr": [ { "ans": [ "The motor starts when water tank pressure is less than 35 psig. The motor stops when water tank pressure is 45 psig. ", "true" ] }, { "ans": [ "The motor starts when water tank pressure is less than 45 psig ", "false" ] }, { "ans": [ "The motor starts when water tank pressure is 45 psig. ", "false" ] } ] }, { "ch": "Which is not a CMCS primary function?", "ansGr": [ { "ans": [ "Condition monitoring ", "true" ] }, { "ans": [ "Testing ", "false" ] }, { "ans": [ "Data load ", "false" ] } ] }, { "ch": "Which component is used to show CMCS data?", "ansGr": [ { "ans": [ "Maintenance access terminal (MAT) ", "true" ] }, { "ans": [ "Multifunction display (MFD) ", "false" ] }, { "ans": [ "Control display unit (CDU) ", "false" ] } ] }, { "ch": "How many CMCF can operate at a time?", "ansGr": [ { "ans": [ "One ", "true" ] }, { "ans": [ "Two ", "false" ] }, { "ans": [ "Three ", "false" ] } ] }, { "ch": "Where is located the PMAT receptacle?", "ansGr": [ { "ans": [ "On P18 panel in the flight deck ", "true" ] }, { "ans": [ "In the bulk cargo ", "false" ] }, { "ans": [ "On the refuel panel. ", "false" ] } ] }, { "ch": "Where is located the GROUND TEST switch?", "ansGr": [ { "ans": [ "On the P5 overhead panel ", "false" ] }, { "ans": [ "On the P61 overhead panel ", "true" ] }, { "ans": [ "On the P18 MAT/second observer panel ", "false" ] } ] }, { "ch": "Which CPM has CMCF software?", "ansGr": [ { "ans": [ "CPM/ Basic ", "false" ] }, { "ans": [ "CPM/ ACMF ", "false" ] }, { "ans": [ "CPM/Comm ", "true" ] } ] }, { "ch": "How does CMCF calculate the last leg?", "ansGr": [ { "ans": [ "Last leg = leg 0 ", "false" ] }, { "ans": [ "Last leg = leg 1 ", "true" ] }, { "ans": [ "Last leg = leg 1 ", "false" ] } ] }, { "ch": "How many recent flight legs can CMCF store?", "ansGr": [ { "ans": [ "10 flight legs ", "false" ] }, { "ans": [ "50 flight legs ", "false" ] }, { "ans": [ "100 flight legs ", "true" ] } ] }, { "ch": "What is one of the CMCS main menu selection?", "ansGr": [ { "ans": [ "Line maintenance ", "true" ] }, { "ans": [ "Base maintenance ", "false" ] }, { "ans": [ "Ground maintenance ", "false" ] } ] }, { "ch": "What is the normal cursor symbol on the display?", "ansGr": [ { "ans": [ "A plus (+) symbol ", "true" ] }, { "ans": [ "A wristwatch symbol ", "false" ] }, { "ans": [ "An I-beam symbol ", "false" ] } ] }, { "ch": "The APU inlet door is located at", "ansGr": [ { "ans": [ "Upper right side of tail cone ", "true" ] }, { "ans": [ "Upper left side of tail cone ", "false" ] }, { "ans": [ "Bottom of tail cone ", "false" ] } ] }, { "ch": "Which is normal APU shut down", "ansGr": [ { "ans": [ "Shut down using APU switch on P5 panel ", "true" ] }, { "ans": [ "Shut down using APU shutdown switch on P40 panel ", "false" ] }, { "ans": [ "Shut down using APU fire handle on P5 panel ", "false" ] } ] }, { "ch": "How many chip collectors used on the APU", "ansGr": [ { "ans": [ "1 chip collectors on the APU ", "false" ] }, { "ans": [ "3 chip collectors on the APU ", "false" ] }, { "ans": [ "5 chip collectors on the APU ", "true" ] } ] }, { "ch": "The purpose of the APU lubrication system is to lubricate and cool these components:", "ansGr": [ { "ans": [ "APU bearings, APU gearbox, Electric starter (ES) and APU generator. ", "false" ] }, { "ans": [ "APU gearbox, Air turbine starter (ATS), APU bearings and APU generator. ", "true" ] }, { "ans": [ "APU generator, Air turbine starter (ATS), APU bearings and IGV actuator bearings. ", "false" ] } ] }, { "ch": "Which computer controls APU system functions and is an interface with other airplane systems:", "ansGr": [ { "ans": [ "EEC. ", "false" ] }, { "ans": [ "ECB. ", "false" ] }, { "ans": [ "APUC. ", "true" ] } ] }, { "ch": "APU ignition system consists of:", "ansGr": [ { "ans": [ "01 ignition unit, 01 igniter and the ignition lead. ", "false" ] }, { "ans": [ "01 ignition unit, 02 igniters and the ignition leads. ", "true" ] }, { "ans": [ "02 ignition units, 02 igniters and the ignition leads. ", "false" ] } ] }, { "ch": "APU is started with the electric starter motor:", "ansGr": [ { "ans": [ "You can try three APU starts in a 60 minute period. ", "true" ] }, { "ans": [ "You can try four APU starts in a 60 minute period. ", "false" ] }, { "ans": [ "No limitation. ", "false" ] } ] }, { "ch": "What is the purpose of APU vent doors?", "ansGr": [ { "ans": [ "Permit outside air to go into the APU compartment for the compartment cooling. ", "false" ] }, { "ans": [ "To equalize pressure. ", "true" ] }, { "ans": [ "Permit APU compartment air to move through the oil cooler to cool the APU oil. ", "false" ] } ] }, { "ch": "What is the purpose of APU air supply system-inlet guide vanes?", "ansGr": [ { "ans": [ "To control the air flow to the load compressor. ", "true" ] }, { "ans": [ "To control the air flow to the APU two-stage centrifugal compressor. ", "false" ] }, { "ans": [ "To control the air flow to the load compressor and the air flow to the APU two-stage centrifugal compressor. ", "false" ] } ] }, { "ch": "The APU air supply system-inlet guide vanes actuator is operated:", "ansGr": [ { "ans": [ "Electrically. ", "false" ] }, { "ans": [ "Pneumatically. ", "false" ] }, { "ans": [ "Hydraulically. ", "true" ] } ] }, { "ch": "What is the purpose of the APU surge bleed system-surge control valve?", "ansGr": [ { "ans": [ "To release pneumatic pressure from the APU two-stage centrifugal compressor to prevent compressor surge. ", "false" ] }, { "ans": [ "To release pneumatic pressure from the load compressor to prevent compressor surge. ", "true" ] }, { "ans": [ "To release pneumatic pressure from the APU two-stage centrifugal compressor and from the load compressor to prevent compressor surge. ", "false" ] } ] }, { "ch": "The APU surge bleed system-surge control valve actuator is operated:", "ansGr": [ { "ans": [ "Electrically. ", "false" ] }, { "ans": [ "Pneumatically. ", "false" ] }, { "ans": [ "Hydraulically. ", "true" ] } ] }, { "ch": "Which passenger entry doors are plug type door", "ansGr": [ { "ans": [ "All doors ", "true" ] }, { "ans": [ "Left side doors ", "false" ] }, { "ans": [ "Right side doors ", "false" ] } ] }, { "ch": "What should you do first when close passenger entry door", "ansGr": [ { "ans": [ "Release hold open device ", "true" ] }, { "ans": [ "Disarm the door ", "false" ] }, { "ans": [ "Pull the door in ", "false" ] } ] }, { "ch": "Flight lock mechanism is used to", "ansGr": [ { "ans": [ "Lock the door when airplane in the air ", "false" ] }, { "ans": [ "Lock the door when airplane is parked ", "false" ] }, { "ans": [ "Lock the door when airspeed above 80 knots ", "true" ] } ] }, { "ch": "Two positions of passenger door mode handle are", "ansGr": [ { "ans": [ "ARMED and DISARMED ", "false" ] }, { "ans": [ "AUTO and MANUAL ", "true" ] }, { "ans": [ "LOCKED and UNLOCKED ", "false" ] } ] }, { "ch": "Which cargo door on VNA owned aircraft is large size", "ansGr": [ { "ans": [ "Forward ", "true" ] }, { "ans": [ "Aft ", "false" ] }, { "ans": [ "Both forward and aft ", "false" ] } ] }, { "ch": "You open and close forward and aft cargo doors using", "ansGr": [ { "ans": [ "Electric power ", "true" ] }, { "ans": [ "Hydraulic power ", "false" ] }, { "ans": [ "Pneumatic power ", "false" ] } ] }, { "ch": "When closing the forward cargo door, which light should be on before you can use lock handle to lock the door", "ansGr": [ { "ans": [ "DOOR CLOSED light ", "false" ] }, { "ans": [ "DOOR IN light ", "false" ] }, { "ans": [ "DOOR LATCHED light ", "true" ] } ] }, { "ch": "What should you do before opening the forward cargo door using internal switch", "ansGr": [ { "ans": [ "Unlock the door using internal release lever ", "false" ] }, { "ans": [ "Unlock the door using external catch release handle ", "false" ] }, { "ans": [ "Both are correct ", "true" ] } ] }, { "ch": "How many vent doors are installed on forward cargo door", "ansGr": [ { "ans": [ "1 ", "true" ] }, { "ans": [ "2 ", "false" ] }, { "ans": [ "4 ", "false" ] } ] }, { "ch": "Bulk cargo door is open and close using", "ansGr": [ { "ans": [ "Electric motor ", "false" ] }, { "ans": [ "Hydraulic motor ", "false" ] }, { "ans": [ "Counter balance mechanism ", "true" ] } ] }, { "ch": "the Door Select Lever is in the red armed position, which of the following is correct?", "ansGr": [ { "ans": [ "The slide bar is attached to the floor fittings and the door is selected for pneumatic emergency operation ", "true" ] }, { "ans": [ "The slide bar is not attached to the floor fittings and the door is selected for normal operation ", "false" ] }, { "ans": [ "The slide bar is attached to the floor fittings and the door is selected for counterbalance emergency opening ", "false" ] } ] }, { "ch": "The light on the EPAS battery pack blinks a continuous green color. It shows:", "ansGr": [ { "ans": [ "The mode select handle is in the MANUAL position. ", "false" ] }, { "ans": [ "The mode select handle is in the AUTO position. ", "false" ] }, { "ans": [ "The battery pack capacitor is charged and ready to fire. ", "true" ] } ] }, { "ch": "When operating a cargo door electrically, some caution should be observed:", "ansGr": [ { "ans": [ "Do not operate the door electrically more than 2 full open/ close cycles within 5 minutes. ", "true" ] }, { "ans": [ "Do not operate the door electrically more than 3 full open/ close cycles within 5 minutes. ", "false" ] }, { "ans": [ "Do not operate the door electrically more than 3 full open/ close cycles within 10 minutes. ", "false" ] } ] }, { "ch": "When lifting and lowering a cargo door manually, some caution should be observed:", "ansGr": [ { "ans": [ "Do not operate the manual drive at a speed faster than 750 RPM. ", "false" ] }, { "ans": [ "Do not apply a torque of more than 110 pound-inches. ", "true" ] }, { "ans": [ "Do not operate the manual drive at a speed faster than 1000 RPM. ", "false" ] } ] }, { "ch": "Looking through each witness port along the bottom edge of the cargo door, if each indication arrow points to the target, it means:", "ansGr": [ { "ans": [ "The door is locked. ", "false" ] }, { "ans": [ "The door is latched. ", "true" ] }, { "ans": [ "The door is closed. ", "false" ] } ] }, { "ch": "Looking through each witness port along the bottom edge of the cargo door, if all of the yellow circles are seen, it means:", "ansGr": [ { "ans": [ "The door is locked. ", "true" ] }, { "ans": [ "The door is latched. ", "false" ] }, { "ans": [ "The door is closed. ", "false" ] } ] }, { "ch": "Which door is a non-plug type of door?", "ansGr": [ { "ans": [ "The passenger/ crew entry door. ", "false" ] }, { "ans": [ "The cargo door. ", "true" ] }, { "ans": [ "The bulk cargo door. ", "false" ] } ] }, { "ch": "The purpose of the breakaway panel installed on the flight compartment door?", "ansGr": [ { "ans": [ "For flight crew to escape in case of a hard landing. ", "true" ] }, { "ans": [ "Will open aft in the event of a decompression in the passenger cabin. ", "false" ] }, { "ans": [ "Will open inward in case of a rapid decompression in the flight compartment. ", "false" ] } ] }, { "ch": "If a passenger/ crew entry door is not locked, the cabin system control panel (CSCP)-the cabin door status screen shows:", "ansGr": [ { "ans": [ "NOT LOCKED in red color. ", "true" ] }, { "ans": [ "NOT LOCKED in amber color. ", "false" ] }, { "ans": [ "NOT LOCKED in green color. ", "false" ] } ] }, { "ch": "How many pressure bulkheads are there in the fuselage?", "ansGr": [ { "ans": [ "3 ", "false" ] }, { "ans": [ "4 ", "false" ] }, { "ans": [ "2 ", "true" ] } ] }, { "ch": "When you open the radome, it is", "ansGr": [ { "ans": [ "Detached from the fuselage ", "false" ] }, { "ans": [ "Held by a hinge ", "true" ] }, { "ans": [ "Opened upward ", "false" ] } ] }, { "ch": "Wing-to-body fairing is made of", "ansGr": [ { "ans": [ "Steel ", "false" ] }, { "ans": [ "Alluminum ", "false" ] }, { "ans": [ "Composite ", "true" ] } ] }, { "ch": "When you open the nose radome, wind velocity must be", "ansGr": [ { "ans": [ "Less than 65kts ", "true" ] }, { "ans": [ "Less than 45kts ", "false" ] }, { "ans": [ "Less than 80kts ", "false" ] } ] }, { "ch": "The fuselage is put together in sections. How many sections are there?", "ansGr": [ { "ans": [ "6. ", "true" ] }, { "ans": [ "7. ", "false" ] }, { "ans": [ "8. ", "false" ] } ] }, { "ch": "The fuselage is put together in sections. What are they?", "ansGr": [ { "ans": [ "41/42/43/45/46/48. ", "false" ] }, { "ans": [ "41/43/45/46/47/48. ", "false" ] }, { "ans": [ "41/43/44/46/47/48. ", "true" ] } ] }, { "ch": "Wing structure and skin are made of", "ansGr": [ { "ans": [ "Aluminum ", "true" ] }, { "ans": [ "Steel ", "false" ] }, { "ans": [ "Composite ", "false" ] } ] }, { "ch": "Vortex generators are installed on", "ansGr": [ { "ans": [ "Wing tip ", "false" ] }, { "ans": [ "Wing lower surface ", "false" ] }, { "ans": [ "Wing upper surface ", "true" ] } ] }, { "ch": "Where are located the wing dry bays?", "ansGr": [ { "ans": [ "Outboard of each main tank. ", "false" ] }, { "ans": [ "Above each engine strut. ", "true" ] }, { "ans": [ "In the center wing section. ", "false" ] } ] }, { "ch": "Wing dry bay access door is located:", "ansGr": [ { "ans": [ "On the bottom of the wing. ", "true" ] }, { "ans": [ "On the top of the wing. ", "false" ] }, { "ans": [ "On the engine pylon. ", "false" ] } ] }, { "ch": "Can you reuse gaskets and preformed packing seals", "ansGr": [ { "ans": [ "No ", "true" ] }, { "ans": [ "Yes, B1 CRS decision ", "false" ] }, { "ans": [ "Yes, Forman decision ", "false" ] } ] }, { "ch": "How can you bend an originally bent tube?", "ansGr": [ { "ans": [ "In any direction ", "false" ] }, { "ans": [ "In reverse direction ", "false" ] }, { "ans": [ "In the same direction ", "true" ] } ] }, { "ch": "Number of twists of lockwire per inch are", "ansGr": [ { "ans": [ "7-9 ", "false" ] }, { "ans": [ "12-15 ", "false" ] }, { "ans": [ "9-12 ", "true" ] } ] }, { "ch": "Maximum length of lockwire between points that are in tension is", "ansGr": [ { "ans": [ "3 in ", "false" ] }, { "ans": [ "6 in ", "true" ] }, { "ans": [ "7 in ", "false" ] } ] }, { "ch": "You are allowed to lockwire maximum", "ansGr": [ { "ans": [ "4 parts in a series ", "false" ] }, { "ans": [ "3 parts in a series ", "true" ] }, { "ans": [ "5 parts in a series ", "false" ] } ] }, { "ch": "Can you reuse gaskets, packings, and rubber parts after removal?", "ansGr": [ { "ans": [ "No. ", "true" ] }, { "ans": [ "Yes, B1 CRS decision ", "false" ] }, { "ans": [ "Yes, Forman decision ", "false" ] } ] }, { "ch": "The maximum distance between tension points that safety wire can go is:", "ansGr": [ { "ans": [ "3 inch ", "false" ] }, { "ans": [ "6 inch ", "true" ] }, { "ans": [ "7 inch ", "false" ] } ] }, { "ch": "With one continuous length of safety wire, do not safety together more than:", "ansGr": [ { "ans": [ "4 units in a series ", "true" ] }, { "ans": [ "3 units in a series ", "false" ] }, { "ans": [ "5 units in a series ", "false" ] } ] }, { "ch": "Number of twists of lockwire (with 0.51 mm diameter) per inch are:", "ansGr": [ { "ans": [ "7-9 ", "false" ] }, { "ans": [ "12-15 ", "false" ] }, { "ans": [ "9-13 ", "true" ] } ] }, { "ch": "Number of twists of lockwire (with 0.864 mm diameter) per inch are:", "ansGr": [ { "ans": [ "7-10 ", "true" ] }, { "ans": [ "5-8 ", "false" ] }, { "ans": [ "9-13 ", "false" ] } ] }, { "ch": "Lower Lobe Attendant Rest Heaters operates at", "ansGr": [ { "ans": [ "the airplane is below 25000 feet. ", "true" ] }, { "ans": [ "the airplane is below 33000 feet. ", "false" ] }, { "ans": [ "the airplane is above 33000 feet. ", "false" ] } ] }, { "ch": "When do Operational Test Lower Lobe Attendant Rest Heaters, it must:", "ansGr": [ { "ans": [ "Put the ADIRU switch on the P5 overhead panel in the OFF position ", "false" ] }, { "ans": [ "Put the ADIRU switch on the P5 overhead panel in the OFF position and Put the air/ground system in the air mode ", "true" ] }, { "ans": [ "Put the air/ground system in the air mode ", "false" ] } ] }, { "ch": "What is (are) corrects when do The HF communication systtems test?", "ansGr": [ { "ans": [ "Do not transmit with the HF communication system while you refuel or defuel the airplane an explosion can cause injuries to personnel and damage to equipment ", "false" ] }, { "ans": [ "Make sure personnel stay a minimum of 6 feet away from stabilizer when the HF system transmits the RF energy from HF communication atenna can causes injuries to personnel ", "false" ] }, { "ans": [ "Both a and b ", "true" ] } ] }, { "ch": "When do cleaning touch screen of CSCP ( Cabin System Control Panel) or CACP ( Cabin Attendant Control Panel), what is the correct procedue?", "ansGr": [ { "ans": [ "Deactivate touchscreen by selections PANEL LOCKOUT from MAIN MENU on CSCP or CACP then do a clean ", "true" ] }, { "ans": [ "Pull out circuit breaker of touchscreen then do clean ", "false" ] }, { "ans": [ "Use a clean, soft, natural- bristle brush to brush directly on touchscreen no need pull out circuit breaker or deactivation of touchscreen. ", "false" ] } ] }, { "ch": "What is recommended when you transfer power sources on the airplane?", "ansGr": [ { "ans": [ "Battery switch is in the ON position (latched) ", "true" ] }, { "ans": [ "Battery switch is in the OFF position (unlatched) ", "false" ] }, { "ans": [ "APU is running. ", "false" ] } ] }, { "ch": "Which light on P30 panel should be OFF after SECONDARY external power was supplied to the aircraft network?", "ansGr": [ { "ans": [ "SECONDARY POWER CONNECTED light ", "false" ] }, { "ans": [ "SECONDARY POWER NOT IN USE light ", "true" ] }, { "ans": [ "AVAIL light ", "false" ] } ] }, { "ch": "During APU operating, the igniter plugs is:", "ansGr": [ { "ans": [ "turns ON the plugs if below 50 percent RPM. ", "false" ] }, { "ans": [ "turns ON the plugs if below 7 percent RPM ", "false" ] }, { "ans": [ "turns the igniter plugs on if below 95 percent RPM ", "true" ] } ] }, { "ch": "How many starter motors are there in the APU start system? (A, B1, B2)", "ansGr": [ { "ans": [ "1 ", "false" ] }, { "ans": [ "2 ", "true" ] }, { "ans": [ "3 ", "false" ] } ] }, { "ch": "The B777 fuselage is: (A, B1, B2)", "ansGr": [ { "ans": [ "A monocoque structure. ", "false" ] }, { "ans": [ "A semi-monocoque structure. ", "true" ] }, { "ans": [ "A truss structure. ", "false" ] } ] }, { "ch": "The pylon attaches to the wing and contains the strut. What is the purpose of the strut? (A, B1, B2)", "ansGr": [ { "ans": [ "To support the engine. ", "true" ] }, { "ans": [ "To provide smooth aerodynamic surface to the airflow. ", "false" ] }, { "ans": [ "To provide access doors and panels to get access to components inside the pylon. ", "false" ] } ] }, { "ch": "Which passenger entry doors are plug type door", "ansGr": [ { "ans": [ "All doors ", "true" ] }, { "ans": [ "Left side doors ", "false" ] }, { "ans": [ "Right side doors ", "false" ] } ] }, { "ch": "In the cargo compartments, marking CAUTION: SMOKE DETECTION EQUIPMENT, CARGO COMPARTMENT is located", "ansGr": [ { "ans": [ "On the left sidewall of FWD and AFT cargo ", "true" ] }, { "ans": [ "On the left sidewall of FWD cargo ", "false" ] }, { "ans": [ "On the left sidewall of AFT cargo ", "false" ] } ] }, { "ch": "Pitot probe covers and static port covers are recommended when the airplane is parked for:", "ansGr": [ { "ans": [ "transit check. ", "false" ] }, { "ans": [ "leak and sense check. ", "false" ] }, { "ans": [ "more than a standard turnaround ", "true" ] } ] }, { "ch": "The maximum pressure to fill the Potable Water Tanks", "ansGr": [ { "ans": [ "More than 55 PSI ", "false" ] }, { "ans": [ "Below 55 PSI ", "true" ] }, { "ans": [ "Below 65 PSI ", "false" ] } ] } ]