ATR 72 – Communications

{“questions”:{“e6b69”:{“id”:”e6b69″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The VHF has the capability to automatically cutoff transmission against unintentional or continuous transmission linked with jammed Push-To-Talk (PTT) devices or equipment malfunction. After _____ of continuous transmission, a tone is heard to indicate impending cutout of transmission (TX).”,”desc”:”Five seconds later, transmission is cutoff and ‘FAIL’ indication replaces the active frequency on the VCP\/MCDU. The…… Continue Reading →

ATR 72 – Auto Flight

{“questions”:{“mzi8d”:{“id”:”mzi8d”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Altitude alert is part of the Automatic Flight Control System (AFCS).”,”desc”:”The AFCS achieves Autopilot (AP), Yaw Damper (YD), turn coordination, Flight Director (FD) function and Altitude alert.”,”hint”:””,”answers”:{“d77fs”:{“id”:”d77fs”,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”ujlod”:{“id”:”ujlod”,”image”:””,”imageId”:””,”title”:”False.”}}},”uveot”:{“id”:”uveot”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2025\/02\/ATR-72-Go-Aound-pb.jpg”,”imageId”:”6589″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”When pressing these go-around pb, the go-around mode is engaged. _____ are cancelled and the autopilot is disengaged.”,”desc”:”If LNAV is engaged when pressing the GA pb, LNAV remains engaged…… Continue Reading →

ATR 72 – Pressurization

{“questions”:{“eez80”:{“id”:”eez80″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”An overpressure relief valve and a negative pressure relief valve are fitted on both outflow valves as safety devices.”,”desc”:””,”hint”:””,”answers”:{“zll4n”:{“id”:”zll4n”,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”hcfck”:{“id”:”hcfck”,”image”:””,”imageId”:””,”title”:”False.”}}},”t4jet”:{“id”:”t4jet”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2025\/02\/Auto-and-Cab-Press.jpg”,”imageId”:”6582″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”When the pressurization system is operating in the AUTO-mode, the pneumatic outflow valve is slaved to the electropneumatic valve.”,”desc”:””,”hint”:””,”answers”:{“2e1ps”:{“id”:”2e1ps”,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”o60by”:{“id”:”o60by”,”image”:””,”imageId”:””,”title”:”False.”}}},”b40ua”:{“id”:”b40ua”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2025\/02\/ATR-72-Auto-Press-by-Smartcockpit.com_.jpg”,”imageId”:”6583″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”A DUMP function is available to send a fully open electrical signal to the electropneumatic outflow valve. DUMP function…… Continue Reading →

ATR 72 – Air Conditioning

{“questions”:{“769l1”:{“id”:”769l1″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The air intended for air conditioning and pressurization is pressurized by engines compressors and delivered through the bleed valves.”,”desc”:””,”hint”:””,”answers”:{“14jb0”:{“id”:”14jb0″,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”zg47k”:{“id”:”zg47k”,”image”:””,”imageId”:””,”title”:”False.”}}},”ct1li”:{“id”:”ct1li”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Electric and electronic equipment and the forward cargo compartment are ventilated by _____ which is then recirculated or discharged outside the aircraft.”,”desc”:””,”hint”:””,”answers”:{“481tf”:{“id”:”481tf”,”image”:””,”imageId”:””,”title”:”Cabin ambient air”,”isCorrect”:”1″},”v3w4n”:{“id”:”v3w4n”,”image”:””,”imageId”:””,”title”:”The outside air that is heated in the mixing chamber”},”tzi3n”:{“id”:”tzi3n”,”image”:””,”imageId”:””,”title”:”The mixed air manifold”}}},”it0aq”:{“id”:”it0aq”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”If one…… Continue Reading →

Pilatus PC-12 – Air Systems

{“questions”:{“5snhm”:{“id”:”5snhm”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The air cycle system cools a portion of the bleed air and then mixes it with hot bleed air to provide the correct temperature.”,”desc”:””,”hint”:””,”answers”:{“lnsn8”:{“id”:”lnsn8″,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”nd48k”:{“id”:”nd48k”,”image”:””,”imageId”:””,”title”:”False.”}}},”rl4fs”:{“id”:”rl4fs”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The PC-12 has two auxiliary electrical heaters. A cabin heater and an underfloor heater. Only the cabin heater can be used for pre-heating on the ground when external power is connected.”,”desc”:”One of…… Continue Reading →

Pilatus PC-12 – Electrical

{“questions”:{“5hi02”:{“id”:”5hi02″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”When the engine is running, Generator 1 is the primary power source for the Channel 1 Power Line, and the Essential and Avionic 1 Buses. The Standby Bus is powered from the Avionic 1 Bus.”,”desc”:”If the Avionic 1 Bus is switched OFF, the Standby Bus is powered from the Hot Bat Bus provided the STBY…… Continue Reading →

Pilatus PC-12 – Fuel

{“questions”:{“bdk4t”:{“id”:”bdk4t”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Electric booster pumps provide pressure during the engine start sequence, as a standby function when the normal system cannot maintain adequate pressure and are used to balance the fuel level in each wing.\r\n”,”desc”:””,”hint”:””,”answers”:{“qwg87”:{“id”:”qwg87″,”image”:””,”imageId”:””,”title”:”True.\r\n”,”isCorrect”:”1″},”y1yvq”:{“id”:”y1yvq”,”image”:””,”imageId”:””,”title”:”False.”}}},”r2gau”:{“id”:”r2gau”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Fuel symmetry is maintained automatically by the Fuel Control and Monitoring Unit (FCMU).”,”desc”:””,”hint”:””,”answers”:{“n8tgq”:{“id”:”n8tgq”,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”pkljt”:{“id”:”pkljt”,”image”:””,”imageId”:””,”title”:”False.”}}},”r3dly”:{“id”:”r3dly”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The transfer and delivery of fuel is achieved using a motive…… Continue Reading →

Pilatus PC-12 – Engine

{“questions”:{“d24fe”:{“id”:”d24fe”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2025\/02\/Pilatus-PC-12-Nose-Gear-by-Smartcockpit.com_.jpg”,”imageId”:”6544″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The airplane is equipped with a four or five blade, variable pitch, full feathering propeller which is driven by the engine power turbine through the reduction gearbox. Propeller pitch is adjusted by engine oil pressure regulated through the Propeller Governor\/Constant Speed Unit (CSU).”,”desc”:”The blade angle is set by controlling the pressure of the oil supplied…… Continue Reading →

Pilatus PC-12 – Engine

{“questions”:{“a0kqr”:{“id”:”a0kqr”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2025\/02\/Pilatus-PC-12_Flyingmag.jpg”,”imageId”:”6559″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”When the POWER CONTROL lever (PCL) is at the idle detent, the gas generator is at idle and the propeller is at maximum pitch. A lifting action to raise the PCL over the detent is required to move the PCL into the ground operating range.”,”desc”:”When the PCL is at the idle detent, the gas generator…… Continue Reading →

Pilatus PC-12 – Landing gear

{“questions”:{“9ceov”:{“id”:”9ceov”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2025\/02\/Pilatus-PC-12-Landing-Gear-by-Smartcockpit.com_.jpg”,”imageId”:”6542″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The landing gear is a conventional tricycle configuration that is extended and retracted using hydraulic pressure produced by an electrically powered hydraulic pump. Landing gear extension and retraction is the only function of the hydraulic system.”,”desc”:””,”hint”:””,”answers”:{“yvvks”:{“id”:”yvvks”,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”79fvf”:{“id”:”79fvf”,”image”:””,”imageId”:””,”title”:”False.”}}},”jgu64″:{“id”:”jgu64″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”A nitrogen charged accumulator is used to:”,”desc”:””,”hint”:””,”answers”:{“keb1b”:{“id”:”keb1b”,”image”:””,”imageId”:””,”title”:”Maintain hydraulic pressure and hold the landing gear in the retracted position in normal…… Continue Reading →

Pilatus PC-12 – Flight controls

{“questions”:{“mitn8”:{“id”:”mitn8″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2025\/02\/PC-12-In-Flight2-by-Smartcockpit.com_.jpg”,”imageId”:”6534″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The flight control system is conventional using push-pull rods and carbon steel cables. Electric trim systems are provided for the aileron, rudder, and elevator. All trim systems can be disconnected in the event of a runaway condition.”,”desc”:”The aileron, horizontal stabilizer and rudder trim are electrically operated. Aileron and horizontal stabilizer trim operation is controlled by…… Continue Reading →

Embraer Phenom 300 – Oxygen

{“questions”:{“0k405”:{“id”:”0k405″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2025\/02\/Oxygen-Mask.jpg”,”imageId”:”6528″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Mask stowage box and crew mask (B\/E Aerospace) – A bright yellow star illuminates, indicating that oxygen is _____”,”desc”:””,”hint”:””,”answers”:{“k36lz”:{“id”:”k36lz”,”image”:””,”imageId”:””,”title”:”Flowing through the mask.”,”isCorrect”:”1″},”0ul6n”:{“id”:”0ul6n”,”image”:””,”imageId”:””,”title”:”Available.”},”bnk3l”:{“id”:”bnk3l”,”image”:””,”imageId”:””,”title”:”Open and available.”}}},”zmapw”:{“id”:”zmapw”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2025\/02\/Oxygen-Mask.jpg”,”imageId”:”6528″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Mask stowage box and crew mask (B\/E Aerospace) – The OXY ON flag appears whenever _____”,”desc”:””,”hint”:””,”answers”:{“23qjk”:{“id”:”23qjk”,”image”:””,”imageId”:””,”title”:”TEST\/RESET button is pressed.”,”isCorrect”:”1″},”0iy1c”:{“id”:”0iy1c”,”image”:””,”imageId”:””,”title”:”Oxygen is available and is flowing through the mask.”},”d4l7x”:{“id”:”d4l7x”,”image”:””,”imageId”:””,”title”:”The Auto Dilution Valve is activated.”}}},”jerjn”:{“id”:”jerjn”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2025\/02\/Oxygen-Mask.jpg”,”imageId”:”6528″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Mask…… Continue Reading →

Embraer Phenom 300 – Automatic flight

{“questions”:{“o5rjs”:{“id”:”o5rjs”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2025\/01\/Lateral-Guidance-Control-Embraer-300-by-Smartcockpit.com_.jpg”,”imageId”:”6523″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”When the APR mode is intercepted, the lateral mode (ROL, HDG, VAPP, BC or FMS) is automatically deactivated.”,”desc”:””,”hint”:””,”answers”:{“qa0rb”:{“id”:”qa0rb”,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”yg50u”:{“id”:”yg50u”,”image”:””,”imageId”:””,”title”:”False.”}}},”cl1f5″:{“id”:”cl1f5″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2025\/01\/Lateral-Guidance-Control-Embraer-300-by-Smartcockpit.com_.jpg”,”imageId”:”6523″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The BANK button enables and disables the low bank mode that is _____”,”desc”:””,”hint”:””,”answers”:{“fv0zf”:{“id”:”fv0zf”,”image”:””,”imageId”:””,”title”:”Plus or minus 10 degrees.”},”pxb76″:{“id”:”pxb76″,”image”:””,”imageId”:””,”title”:”Plus or minus 15 degrees.”,”isCorrect”:”1″},”xv6hr”:{“id”:”xv6hr”,”image”:””,”imageId”:””,”title”:”Plus or minus 20 degrees.”}}},”eyyqc”:{“id”:”eyyqc”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2025\/01\/Vertical-Guidance-Control-Embraer-300-by-Smartcockpit.com_.jpg”,”imageId”:”6524″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Rotating the thumb wheel selector will make the VS mode to automatically become effective…… Continue Reading →

Embraer Phenom 300 – Electrical

{“questions”:{“0rdk1”:{“id”:”0rdk1″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”In certain conditions, batteries 1 and 2 are used to backup all buses except the SHED BUS. Battery 2 also supplies the CENTRAL BUS, during engine starting.”,”desc”:”When connected to the CENTRAL BUS, the DC external power source may be used to provide power for engine starting, in parallel with Battery 2.”,”hint”:””,”answers”:{“kszxn”:{“id”:”kszxn”,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”csj0i”:{“id”:”csj0i”,”image”:””,”imageId”:””,”title”:”False.”}}},”tv16s”:{“id”:”tv16s”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”During normal operation, BATT 1…… Continue Reading →

Embraer Phenom 300 – Ice and Rain Protection

{“questions”:{“7ft9r”:{“id”:”7ft9r”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The Wing and Horizontal Stabilizer Anti-Icing System (WHSAIS) prevents the ice formation and remove the ice formed on the wing and the horizontal-stabilizer leading edges. The Pneumatic System supplies bleed air at controlled temperature and pressure to the WHSAIS.”,”desc”:””,”hint”:””,”answers”:{“p193r”:{“id”:”p193r”,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”aghek”:{“id”:”aghek”,”image”:””,”imageId”:””,”title”:”False.”}}},”lwc75″:{“id”:”lwc75″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”In order to avoid leading edge overheating, the Wing and Horizontal Stabilizer Anti-Icing System (WHSAIS) is inhibited…… Continue Reading →