Akademik Dersler - İçerik

KNOWS; PRIMARY FLIGHT DISPLAY (PFD). • Monitor specialties, • Different formats of the monitor, • Informations gained via monitor, • Dısplay mulfunctıons • Annunciators of primary flıght dısplay and its meanıngs. KNOWS; MULTIFUNCTION DISPLAY (MFD) • Specialites of the monitor, • Different formats of the monitor, • Informations gained via monitor, • Dısplay mulfunctıons • Annunciators of multifunction display and its meanings
KNOWS; AIR DATA COMPUTER VE ATTITUDE HEADING REFERANCE SYSTEM • Working principles, • Procedures should be done during mulfunctions,
KNOWS; DISPLAY CONTROL PANEL (DCP) • Panel specialities, • Functions of the panel, • Connections of DCP with PFD and MFD, • Enterance of the refe speeds, • Enterance of the barometric pressure , • Tuning of the NAV Source and Bearing Source, • Usage of WX radar
KNOWS; RADIO TUNING UNIT (RTU) • COM-1, COM-2, NAV-1, NAV-2, ATC-1, ATC-2, ADF devices; • Turning on, • Turning OFF, • Enterace of information, • Usage of system with its full performance, • Usage of CDU panel as a primary device in case of emergency,
KNOWS; AUDIO PANEL • Choosing of microphone, Listening of COM-1, COM-2, NAV-1, NAV-2 and ADF, MARKER signals,
KNOWS; REVERSIONARY PANEL • Prop synronizer, • Tuning of Compas gyro deviations manuelly, • TCAS system TEST, Vertical range tuning, • ATC (Transponder) Turning ON/OFF, Choosing device, • Knows; During PILOT DISPLAY mulfunction monitoring informations from the other monitor, • Choosing AHRS (NORMAL-1-2) • Choosing ADC(NORMAL-1-2) • Choosing Communication and Navigation Radio (RTU - CDU or BOTH) via TUNE , • Entering EMERGENCY FREQUENCY from the COM-1. • Tuning over RMT TUNE device iot change informations simultaneously at the same time with CDU - RTU - FMS devices • Communicating via COMM-1 device without turning on battery via GROUND COM prefernce
KNOWS; COCKPIT VOICE RECORDER (CVR) • Working principles, • Testing, • Erasing the data, • Checking the recorded data,
KNOWS; CURSOR CONTROL PANEL (CCP), KNOWS; TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS I)
KNOWS; WEATHER RADAR (WX RADAR), KNOWS; TERRAIN AWERENESS AND WARNING SYSTEM (TAWS+)
KNOWS; FLIGHT MANAGEMENT SYSTEM (FMS) • Working principles, • Systems connected with,
KNOWS; FLIGHT GUIDANCE COMPUTER (FGC) • Working principles, • Systems connected with, • Monitor of FGC,
KNOWS; FLIGHT GUIDANCE PANEL (FGP) • Working principle • How it shown it PFD, • Pilot (left) Flight Director (FD) usage, • Pilot (left) COURSE knob usagei, • Vertical Speed (VS) knob usage, • Vertical Navigation (VNAV) konb usaege. • VI wheel (UP-DOWN) usage, • Flight Level Change (FLC) knob usage, • SPEED knob usage, • Navigation (NAV) knob usage, • BANK knob usage, • Heading (HDG) knob usage, • Approach (APPR) knob usage, • Altitude (ALT) knob usage, • ALT wheel (Pre select Altitude) usage, • Yaw Damper (YD) knob usage, • CPL knob usage, • Auto Pilot (AP) knob usage, • YD/AP DISC (DISCONNECT) knob usage • Copilot (right) Flight Director (FD) usage, • Copilot (right) COURSE knob usage,
KNOWS; DISPLAY DONTROL UNIT (CDU) • Checking of the validity avionic data of the aircraft, • Planing the route, • Calling the preplanned route from the memory, • Entering the configuraiton of the aircarft, • Entering the SID, • Entering the approach and landing type, • Renewal or replaning the current flight plan, • MFD view of the flight which planned in CDU ,
KNOWS; CDU ROUTE DISIGN