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 →

Airbus A220 – Hydraulics

{“questions”:{“xa3d4”:{“id”:”xa3d4″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The hydraulic power is supplied by three independent systems. Each system delivers a nominal pressure of _____”,”desc”:””,”hint”:””,”answers”:{“3j522”:{“id”:”3j522″,”image”:””,”imageId”:””,”title”:”3000 psi.”,”isCorrect”:”1″},”0ju28″:{“id”:”0ju28″,”image”:””,”imageId”:””,”title”:”2500 psi.”},”ak5nv”:{“id”:”ak5nv”,”image”:””,”imageId”:””,”title”:”3500 psi.”}}},”x41yo”:{“id”:”x41yo”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Each hydraulic system uses a reservoir to store hydraulic fluid and to supply it to the components. The systems are equipped with a main pump and a backup pump to supply pressure. There is limited fluid…… Continue Reading →

Airbus A220 – Fuel

{“questions”:{“pkhf9”:{“id”:”pkhf9″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Fuel inerting system uses Nitrogen-Enriched Air (NEA) to reduce the risk of fuel fumes igniting in the fuel tanks.”,”desc”:”The Fuel Tank Inerting System (FTIS) generates Nitrogen-Enriched Air (NEA) and distributes it into the air space in the fuel tanks to provide non-flammable air in the tanks.”,”hint”:””,”answers”:{“5wpk0”:{“id”:”5wpk0″,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”4mbew”:{“id”:”4mbew”,”image”:””,”imageId”:””,”title”:”False.”}}},”r7s3j”:{“id”:”r7s3j”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”A collector tank is installed in _____ to ensure a…… Continue Reading →

Airbus A220 – Flight controls

{“questions”:{“nz85n”:{“id”:”nz85n”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The Primary Flight Control System (PFCS) has two ailerons, two elevators, and a rudder. The secondary flight controls include:”,”desc”:”The high-lift flight system has leading edge slats and trailing edge flaps. The primary and secondary control surfaces are hydraulically actuated. An electrically actuated horizontal stabilizer supplies longitudinal (pitch) trim.\r\n“,”hint”:””,”answers”:{“6vio7”:{“id”:”6vio7″,”image”:””,”imageId”:””,”title”:”Eight Multifunction Spoilers (MFS) (four per wing), two…… Continue Reading →

Airbus A220 – Fire and Overheat Protection

{“questions”:{“dd652”:{“id”:”dd652″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The engine fire protection system includes:”,”desc”:””,”hint”:””,”answers”:{“za9e1”:{“id”:”za9e1″,”image”:””,”imageId”:””,”title”:”Dual fire detection loops, EICAS and aural alerting, and two fire-extinguishing bottles.”,”isCorrect”:”1″},”mhlzv”:{“id”:”mhlzv”,”image”:””,”imageId”:””,”title”:”Dual fire detection loops, EICAS and aural alerting, smoke detectors, and two fire-extinguishing bottles.”},”lyf6m”:{“id”:”lyf6m”,”image”:””,”imageId”:””,”title”:”A fire detection loop, EICAS and aural alerting, and two fire-extinguishing bottles.”}}},”k1sa1″:{“id”:”k1sa1″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The engine Fire Detection Extinguishing (FIDEX) system has dual fire detection loops, which are temperature-sensitive…… Continue Reading →

Airbus A220 – Electronic Display

{“questions”:{“e1x9p”:{“id”:”e1x9p”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”To select and control a display, and to enter data, each pilot can use the:”,”desc”:””,”hint”:””,”answers”:{“illje”:{“id”:”illje”,”image”:””,”imageId”:””,”title”:”Control Tuning Panel (CTP), or Multifunction Keyboard Panels (MKP), or Cursor Control Panel (CCP).”,”isCorrect”:”1″},”86ydt”:{“id”:”86ydt”,”image”:””,”imageId”:””,”title”:”Control Tuning Panel (CTP), or Multifunction Keyboard Panels (MKP).”},”6f4xw”:{“id”:”6f4xw”,”image”:””,”imageId”:””,”title”:”Multifunction Keyboard Panels (MKP), or Cursor Control Panel (CCP).”}}},”zqp4m”:{“id”:”zqp4m”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The information displayed on the DUs is grouped into:”,”desc”:””,”hint”:””,”answers”:{“n0uls”:{“id”:”n0uls”,”image”:””,”imageId”:””,”title”:”Two specific areas: Primary…… Continue Reading →

Airbus A220 – Electrical

{“questions”:{“45e9p”:{“id”:”45e9p”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2024\/06\/A220-Electrical-Q1.jpg”,”imageId”:”6342″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The electrical control and distribution system is divided into three Electrical Power Centers (EPCs) that are managed by the Bus Power Control Units (BPCUs) and an Emergency Power Control (EMPC).”,”desc”:””,”hint”:””,”answers”:{“b5anl”:{“id”:”b5anl”,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”z2msg”:{“id”:”z2msg”,”image”:””,”imageId”:””,”title”:”False.”}}},”3atgy”:{“id”:”3atgy”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Three Transformer Rectifier Units (TRUs) and _____ supply the required DC power.”,”desc”:””,”hint”:””,”answers”:{“lx0bh”:{“id”:”lx0bh”,”image”:””,”imageId”:””,”title”:”Two Nickel Cadmium (NiCad) batteries.”,”isCorrect”:”1″},”dy1vi”:{“id”:”dy1vi”,”image”:””,”imageId”:””,”title”:”Three Nickel Cadmium (NiCad) batteries.”},”4dqab”:{“id”:”4dqab”,”image”:””,”imageId”:””,”title”:”Two lithium batteries.”}}},”p2v4w”:{“id”:”p2v4w”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Three dedicated Permanent Magnet Alternator\/Generators…… Continue Reading →

Airbus A220 – APU

{“questions”:{“st1bg”:{“id”:”st1bg”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2024\/06\/A220-APU-Q1.jpg”,”imageId”:”6338″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The APU is self-governing, with automatic start sequencing and automatic protective shutdown:”,”desc”:””,”hint”:””,”answers”:{“27qsg”:{“id”:”27qsg”,”image”:””,”imageId”:””,”title”:”On the ground and in flight.”,”isCorrect”:”1″},”sujry”:{“id”:”sujry”,”image”:””,”imageId”:””,”title”:”On the ground only.”},”2wmbs”:{“id”:”2wmbs”,”image”:””,”imageId”:””,”title”:”In flight only.”}}},”unwfc”:{“id”:”unwfc”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The APU is monitored and controlled by an Electronic Control Unit (ECU) and certified for unattended operation on the ground.”,”desc”:””,”hint”:””,”answers”:{“0m93p”:{“id”:”0m93p”,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”wamx9″:{“id”:”wamx9″,”image”:””,”imageId”:””,”title”:”False.”}}},”sgtsj”:{“id”:”sgtsj”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The APU controls are on the APU panel, and on the external service panel. In…… Continue Reading →

Airbus A220 – Automatic Flight

{“questions”:{“yo633”:{“id”:”yo633″,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”The Flight Director (FD) sends pitch and roll commands to the AP system to control the primary flight control surfaces, and displays information on the Primary Flight Display (PFD) for the Flight Path Vector (FPV).”,”desc”:””,”hint”:””,”answers”:{“ik0yt”:{“id”:”ik0yt”,”image”:””,”imageId”:””,”title”:”True.”,”isCorrect”:”1″},”0cp2q”:{“id”:”0cp2q”,”image”:””,”imageId”:””,”title”:”False.”}}},”fdubr”:{“id”:”fdubr”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:””,”imageId”:””,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”On the coupled PFD, if the Autopilot (AP) is engaged:”,”desc”:””,”hint”:””,”answers”:{“kt90t”:{“id”:”kt90t”,”image”:””,”imageId”:””,”title”:”Selection of the FD switch has no effect.”,”isCorrect”:”1″},”k4fsx”:{“id”:”k4fsx”,”image”:””,”imageId”:””,”title”:”Either FD switch can be…… Continue Reading →

Airbus A220 – Air Systems

{“questions”:{“8867s”:{“id”:”8867s”,”mediaType”:”image”,”answerType”:”text”,”imageCredit”:””,”image”:”https:\/\/www.smartcockpit.com\/wp-content\/uploads\/2024\/06\/A220-Air-Systems-Q1.jpg”,”imageId”:”6319″,”video”:””,”imagePlaceholder”:””,”imagePlaceholderId”:””,”title”:”Without external bleed air connected and while on BATT power only, it is possible that the EXT AIR symbol is displayed (green) on the AIR synoptic page while the L and R bleed pressure readouts can vary between 9 PSI and 16 PSI (instead of 0 PSI). This is because:”,”desc”:””,”hint”:””,”answers”:{“1n96c”:{“id”:”1n96c”,”image”:””,”imageId”:””,”title”:”Data from the Air Data System…… Continue Reading →