Akademik Dersler - İçerik

APPLIES EMERGENCY AIRSPEEDS ENGINE FAILURE EMERGENCY ENGINE SHUTDOWN
APPLIES ENGINE FIRE ON GROUND ENGINE FAILURE DURING TAKEOFF (AT OR BELOW V1) - TAKEOFF ABORTED ENGINE FAILURE DURING TAKEOFF (AT OR ABOVE V1) - TAKEOFF CONTINUED
APPLIES ENGINE FAILURE IN FLIGHT BELOW AIR MINIMUM CONTROL SPEED (VMCA) OIL PRESSURE LOW
APPLIES FUEL SYSTEM BOOST PUMP and AUTO CROSSFEED FAILURE 2ND ENGINE FLAMEOUT SMOKE AND FUME ELIMINATION
APPLIES WINDSHIELD ELECTRICAL FAULT ELECTRICAL SMOKE OR FIRE ENVIRONMENTAL SYSTEM SMOKE OR FUMES
APPLIES CABIN DOOR UNLOCKED EMERGENCY DESCENT GLIDE
KNOWS ELECTRICAL DUAL GENERATOR FAILURE LOAD MANAGEMENT WITH DUAL GENERATOR FAILURE LOAD MANAGEMENT TABLE
APPLIES FLIGHT CONTROLS UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION UNSCHEDULED RUDDER BOOST ACTIVATION
APPLIES ENVIRONMENTAL SYSTEMS USE OF OXYGEN PRESSURIZATION LOSS HIGH DIFFERENTIAL PRESSURE
APPLIES EMERGENCY EXIT SPINS AVIONICS AUTOPILOT MALFUNCTION ALTITUDE LOSSES
KNOWS AUTOPILOT FAILURES AUTOPILOT MISTRIM AUTOPILOT TRIM FAIL
APPLIES AUTOPILOT MANUAL DISENGAGEMENT AUTOPILOT AUTOMATIC DISENGAGEMENT ELECTRIC PITCH TRIM INOPERATIVE
KNOWS FLIGHT DISPLAY FAILURE FLAGS TERRAIN AWARENESS WARNING SYSTEM + (TAWS+)
APPLIES SINGLE ADC FAILURE DUAL ADC FAILURE SINGLE AHRS FAILURE DUAL AHRS FAILURE