Gulfstream G650 – Powerplant

{“questions”:{“quw8o”:{“id”:”quw8o”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Maximum reverse thrust must be selected only at airplane speeds above:”,”desc”:””,”hint”:””,”answers”:{“hdnku”:{“id”:”hdnku”,”image”:””,”imageId”:””,”title”:”50 knots.”},”rfxp0″:{“id”:”rfxp0″,”image”:””,”imageId”:””,”title”:”60 knots.”,”isCorrect”:”1″},”whj4u”:{“id”:”whj4u”,”image”:””,”imageId”:””,”title”:”70 knots.”}}},”k3b9i”:{“id”:”k3b9i”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Nacelle components are interchangeable between left and right engines.”,”desc”:”Nacelle components are not interchangeable between left and right engines.”,”hint”:””,”answers”:{“925hl”:{“id”:”925hl”,”image”:””,”imageId”:””,”title”:”True.”},”18vd8″:{“id”:”18vd8″,”image”:””,”imageId”:””,”title”:”False.”,”isCorrect”:”1″}}},”3kouu”:{“id”:”3kouu”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”At what altitude must the boost pumps be operating to sustain engine operation? “,”desc”:””,”hint”:””,”answers”:{“iy7k6”:{“id”:”iy7k6″,”image”:””,”imageId”:””,”title”:”10,000 ft.”},”417n9″:{“id”:”417n9″,”image”:””,”imageId”:””,”title”:”20,000 ft.”,”isCorrect”:”1″},”p0hwq”:{“id”:”p0hwq”,”image”:””,”imageId”:””,”title”:”25,000 ft.”}}},”s5pfs”:{“id”:”s5pfs”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”What\u2019s the primary purpose of Fuel Cooled Oil Cooler…… Continue Reading →

Gulfstream G650 – Landing Gear

{“questions”:{“43kd7”:{“id”:”43kd7″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The landing gear is electrically controlled, hydraulically actuated, and electrically sequenced.”,”desc”:””,”hint”:””,”answers”:{“3f0ev”:{“id”:”3f0ev”,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”ezstn”:{“id”:”ezstn”,”image”:””,”imageId”:””,”title”:”False. “}}},”dcylo”:{“id”:”dcylo”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Landing gear position indicators and an audible warning system are incorporated to provide positive indications of the position of the landing gear. A Weight-On-Wheels (WOW) system is included in the landing gear system, to furnish ‘ground’ or ‘air’ mode reference signals to various aircraft…… Continue Reading →

Gulfstream G650 – APU

{“questions”:{“hjbd1”:{“id”:”hjbd1″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The RE220 APU is a turbine engine composed of _____ with accessory mountings for a 40 KVA generator and a Load Control Valve that provides compressor pressurized air for the aircraft pneumatic system bleed air supply manifold.”,”desc”:”The APU has a single-stage compressor section coupled on a common shaft to a two-stage turbine.”,”hint”:””,”answers”:{“5zo3p”:{“id”:”5zo3p”,”image”:””,”imageId”:””,”title”:”One compressor stage and…… Continue Reading →

Gulfstream G650 – Flight controls

{“questions”:{“l8jtc”:{“id”:”l8jtc”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The flight control system consists of the primary Flight Control System (FCS), the flap system and the horizontal stabilizer system. The primary FCS includes the components that control _____”,”desc”:”These surfaces are hydraulically actuated and electrically controlled with fly-by-wire technology. The flap actuation system includes the Flap Electronic Control Unit (FECU) and the drive system. The…… Continue Reading →

Gulfstream G650 – Fuel

{“questions”:{“klmag”:{“id”:”klmag”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The purpose of the fuel ventilation system is to protect from over and under pressurization by allowing air, fuel vapors, and fuel to move about or flow freely. “,”desc”:”The ventilation system also provides a secondary function for the fuel tank. If a fueling malfunction overfills the tank, the pressure of the increasing volume of fuel…… Continue Reading →

Gulfstream G650 – Hydraulics

{“questions”:{“rhane”:{“id”:”rhane”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”What is the purpose of Power Transfer Unit (PTU)? “,”desc”:”The PTU is used when there is pressure available in the right system and containment of the left system has not been lost, but there is no pressure available in the system. The PTU transfers hydraulic power, but not fluid, from the right to left system.…… Continue Reading →

Gulfstream G650 – Ice and Rain Protection

{“questions”:{“xog8k”:{“id”:”xog8k”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Ice protection systems on the aircraft employ either warm engine bleed air or heat generated by electrical resistance to prevent the formation of ice on critical structures and installations.”,”desc”:”There are two types of protection used on G650: electric and pneumatic.”,”hint”:””,”answers”:{“x3qe8”:{“id”:”x3qe8″,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”syxli”:{“id”:”syxli”,”image”:””,”imageId”:””,”title”:”False.”}}},”68ndm”:{“id”:”68ndm”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The wing anti-ice and engine anti-ice systems are normally activated automatically based on signals from the…… Continue Reading →

Airbus A220 – HUD

{“questions”:{“8tom8”:{“id”:”8tom8″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2024\/08\/A220-HUD-Q1.jpg”,”imageId”:”6392″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Information displayed on the HUD is focused at optical infinity. It is not necessary to refocus the eyes to see either the displayed symbols or outside the aircraft. When the head of the pilot is centered in the eye reference point, the entire display fits in the field of view: “,”desc”:””,”hint”:””,”answers”:{“h5vlo”:{“id”:”h5vlo”,”image”:””,”imageId”:””,”title”:”30 degrees vertical by 42…… Continue Reading →

Gulfstream G650 – Air Conditioning and Pressurization

{“questions”:{“lvg9c”:{“id”:”lvg9c”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The airflow leaving the aircraft is regulated by a _____ that opens and closes in response to automatic or manual commands to maintain the desired cabin altitude level.”,”desc”:”The TROV is located on the right side of the fuselage.”,”hint”:””,”answers”:{“rycx1”:{“id”:”rycx1″,”image”:””,”imageId”:””,”title”:”Thrust Recovery Outflow Valve (TROV).”,”isCorrect”:”1″},”qa4xh”:{“id”:”qa4xh”,”image”:””,”imageId”:””,”title”:”Regulated Outflow Valve (ROV).”},”4zgv1″:{“id”:”4zgv1″,”image”:””,”imageId”:””,”title”:”Automatic Outflow Valve (AOV).”}}},”905ck”:{“id”:”905ck”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The Airflow Control System is a combination of…… Continue Reading →

Gulfstream G550 – Powerplant

{“questions”:{“kvbpu”:{“id”:”kvbpu”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The BR 710 configuration is:”,”desc”:”The HP rotating group consists of a ten-stage HP compressor and a two-stage HP turbine. Engine control is achieved by the full authority digital engine control system (FADEC).”,”hint”:””,”answers”:{“6bha4”:{“id”:”6bha4″,”image”:””,”imageId”:””,”title”:”Ten-stage HP compressor, two-stage LP turbine”,”isCorrect”:”1″},”j0gqm”:{“id”:”j0gqm”,”image”:””,”imageId”:””,”title”:”7-stage HP compressor, two-stage HP turbine”},”0c0gp”:{“id”:”0c0gp”,”image”:””,”imageId”:””,”title”:”Single fan, 10-stage HP compressor and single LP and HP turbines”}}},”statg”:{“id”:”statg”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”A green IGN message…… Continue Reading →

Airbus A320 – Powerplant

{“questions”:{“ldukc”:{“id”:”ldukc”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Thrust reverser system – When deployed, the synchronized electric actuators move the translating sleeves aft, which causes the blocker doors to rotate.”,”desc”:”The actuators are hydraulically operated.”,”hint”:””,”answers”:{“yyku5”:{“id”:”yyku5″,”image”:””,”imageId”:””,”title”:”True.”},”xafsn”:{“id”:”xafsn”,”image”:””,”imageId”:””,”title”:”False.”,”isCorrect”:”1″}}},”6g63m”:{“id”:”6g63m”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The Electronic Engine Control (EEC) is powered by the Permanent Magnet Alternator\/Generator (PMAG), which is driven by the Main Gearbox (MGB). N2 has to be greater than _____ to ensure…… Continue Reading →

Airbus A320 – Navigation

{“questions”:{“wyyrq”:{“id”:”wyyrq”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The Inertial Reference Units (IRUs) enter the Stationary Alignment (SA) mode on ground with no excessive aircraft movement. Aircraft speed must be less than _____.”,”desc”:””,”hint”:””,”answers”:{“2f72s”:{“id”:”2f72s”,”image”:””,”imageId”:””,”title”:”30 kt.”,”isCorrect”:”1″},”iaksj”:{“id”:”iaksj”,”image”:””,”imageId”:””,”title”:”10 kt.”},”juozh”:{“id”:”juozh”,”image”:””,”imageId”:””,”title”:”5 kt.”}}},”4z965″:{“id”:”4z965″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”After successful alignment, the Inertial Reference Units (IRUs) transfers to navigation mode. The time required for an Stationary Alignment (SA) mode is dependent on the aircraft latitude. Alignment…… Continue Reading →

Airbus A320 – Landing gear

{“questions”:{“nz5nw”:{“id”:”nz5nw”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The landing gear system has two main landing gear assemblies and one nose landing gear assembly. Each assembly is equipped with two tires. The landing gear is extended and retracted by hydraulic actuators and pressure from:”,”desc”:””,”hint”:””,”answers”:{“fkj8h”:{“id”:”fkj8h”,”image”:””,”imageId”:””,”title”:”Hydraulic System No. 1 (HYD 1).”,”isCorrect”:”1″},”zby0f”:{“id”:”zby0f”,”image”:””,”imageId”:””,”title”:”Hydraulic System No. 2 (HYD 2).”},”q106j”:{“id”:”q106j”,”image”:””,”imageId”:””,”title”:”Hydraulic Systems No. 1 and No.2 (HYD 1 + HYD2).”}}},”3vabx”:{“id”:”3vabx”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The…… Continue Reading →

Airbus A320 – Ice and rain protection

{“questions”:{“agypm”:{“id”:”agypm”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Ice and rain protection is provided for the engine cowls, flight deck windshields\/side windows, and Air Data System (ADS) probes and sensors and also:”,”desc”:”The leading edge, inboard, and outboard slats of the engine do not require anti-icing. Ice accumulation is not considered significant in these areas, even in adverse icing conditions. For the same reason,…… Continue Reading →

Airbus A320 – Indicating and Recording

{“questions”:{“kkjo5”:{“id”:”kkjo5″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”On a bottom of the STATUS page, what does the upper arrow mean?”,”desc”:””,”hint”:””,”answers”:{“e699e”:{“id”:”e699e”,”image”:””,”imageId”:””,”title”:”It is a reminder to land as soon as possible. “},”u0wfj”:{“id”:”u0wfj”,”image”:””,”imageId”:””,”title”:”It indicates that there is a system page behind. “},”mn173”:{“id”:”mn173″,”image”:””,”imageId”:””,”title”:”It means that there is more information to be seen.”,”isCorrect”:”1″}}},”7e0oh”:{“id”:”7e0oh”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”When should the EMER CANC push button be used?”,”desc”:””,”hint”:””,”answers”:{“bo49t”:{“id”:”bo49t”,”image”:””,”imageId”:””,”title”:”At the completion of an ECAM procedure…… Continue Reading →