aircraft systems as applicable to aircraft rating/endorsement requirements: anti-icing and de-icing systems: method of de-icing aerofoils, propeller and carburettor heat or power source of de-icing/anti-icing equipment anti-icing and de-icing system limitations operation and control of anti-icing and de-icing systems likely faults that may affect anti-icing and de-icing systems emergency operating procedures for anti-icing and de-icing systems aircraft system checklists: explanation of normal system operating procedures of aircraft systems, subsystems and devices used to operate specific aircraft type including use of published scans and checklists, immediate action items, warnings, limitations automated systems: limitations of automated systems operating procedures for systems such as flight management system, auto throttle/engine control, flight director system, automated aircraft navigation systems, automated engine condition and monitoring system workload management procedures for utilising automated systems warning systems/indicators to identify automated systems failure autopilot : principles of operation of autopilot system likely faults that may affect autopilot system emergency operating procedures for autopilot system identification of power sources, voltage or pressure procedure to determine gyros are operating normally procedure to engage autopilot normal and emergency procedure to disengage autopilot limits of gyro units electrical system: use of a schematic diagram of the electrical system to explain type/s of electrical system (AC/DC) likely faults that may affect electrical system emergency operating procedures for electrical system voltage and amperage of battery number and output of generators methods of circuit protection location of fuses and circuit breakers precautions to be taken when operating electrical service instruments operated by electrics enhanced ground proximity warning system/terrain awareness and warning system (EGPWS/TAWS): identification and demonstration or explanation of function of all cockpit EGPWS/TAWS controls information terrain awareness display shows warnings given by fitted EGPWS/TAWS, including what each warning indicates is happening to aircraft in flight fuel system: use of a schematic diagram of fuel system to explain layout and normal operating procedures likely faults that may affect fuel system emergency operating procedures for fuel system operation of fuel selector panel use of cross-feed fuel-dumping procedures full fuel capacity and fuel grade normal, minimum and maximum fuel pressures heating, ventilation and pressurisation systems: normal procedures to operate and control system likely faults that may affect heating, ventilation and pressurisation system emergency procedures for operation of system precautions to be complied with hydraulic system : use of a schematic diagram of hydraulic system to explain layout and normal operating procedures likely faults that may affect hydraulic system emergency operating procedures for hydraulic system units or services operated by hydraulics type of hydraulic fluid, operating pressure and capacity of reservoir oil system: use of a schematic diagram of oil system to explain functions of oil system likely faults that may affect oil system emergency operating procedures for oil system number of tanks, capacity and oil grade oil sources of auxiliary systems such as constant speed unit (CSU), propeller feathering if fitted normal, minimum and maximum oil pressure and temperature operation of oil cooling system pitot/static system: use of a schematic diagram to explain layout and operation of pitot/static system heating source of pitot system operating procedure for pitot/static system methods of detecting pitot/static system problems procedures to rectify static system problems location of pitot and static pressure source location of static drain points pressurisation systems: pressurisation failure warning indications fitted to aircraft type flown function of bleed air with respect to an aircraft pressurisation system procedure for manual control of cabin pressurisation applicable to aircraft type flown recall of maximum pressure differential for aircraft type flown symptoms, indications and warnings that may indicate failure of pressurisation system automatic depressurisation system operation procedures after landing physiological symptoms of hypoxia physical and psychological hazards that could occur during a rapid decompression cabin altitude above which supplementary oxygen must be used by crew and passengers retractable undercarriage: method of preventing retraction of undercarriage on the ground cockpit indications for undercarriage down and locked cockpit indications for undercarriage retracted emergency procedures to extend and lock undercarriage down suction system: use of a schematic diagram of suction system to explain function of suction system source of suction pressure normal operating pressure instruments operated by suction pressure warning system to indicate suction pump failure traffic and collision avoidance systems (TCAS): surveillance and collision avoidance functions of TCAS II system limitations, selectivity and inhibits basic components of TCAS II identification and demonstration or explanation of function of cockpit controls TCAS II visual displays and symbology functions of audio alerts and annunciations appropriate crew response to multiple TCAS II events, and parallel runway approach conflicts recall of radiotelephone procedures following a TCAS II alert requirements for a written report of a TCAS II alert and to whom it must be submitted. |