PC12/45 SCL (QRH Rev.3)

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PC12/45 SCL (QRH Rev.3) SHORT CHECKLIST FOR COMPLETE INFORMATION REFER TO PC-12/45 POH SECTION 4 PREFLIGHT INSPECTION ENGINE STARTING Flight Control Lock removed and stowed Fuel quantity check Parking Brake Handle set/pedals push EIS system test External Power switch OFF TEST FIRE switch push (ENG FIRE and F DETECT BAT 1&2 switches OFF lights on) GEN 1&2 switches OFF TEST LAMP switch push (warning, caution, advisory AV Bus 1&2 switches OFF lights on). Overhead panel switches Non-Essential Bus AUTO LEDs lit STBY BUS switch ON Propeller area clear TEST LAMP switch push, check overhead panel Starter switch push for 2 seconds External lights OFF Oil pressure check rising Fuel pumps AUTO Ng stable between 13% and 20% IGNITION AUTO Condition lever GROUND IDLE DE-ICING OFF ITT Max 1,000°C limited to 5 sec INERT SEP OFF 800-870°C limited to 20 sec Cooling sys. OFF Ng stable above 50% Heating switch OFF Starter sequence completed PASS-WNG switches OFF Engine instruments check Circuit breakers check in Fuel Totalizer reset MSN 50-1 and UP GEN 1&2 switches ON - check CAWS - OFF MASK/Mic switch check set to MIC EXT PWR switch OFF (if external power used) EFIS CMPST switch NORM External Power Unit OFF then disconnect AHRS SLAVE INVERTER BAT or GEN check, change as required AHRS 1/AHRS 2 (if installed) SLAVE AV Bus 1&2 switches ON Landing Gear handle DN STBY BUS switch OFF ECS switch OFF Radios/avionics as required CABIN PRESS switch AUTO/GUARDED ECS switch AUTO Cabin Pressure controller set to cruise alt +500ft Temperature setting as required set rate knob to mid position Cooling or heating sys. as required Trim Interrupt switch NORM/GUARDED INERT SEP OPEN on unprepared surface Flap interrupt switch NORM/GUARDED Manual Override Lever OFF BEFORE TAXIING Power Control Lever idle detent AHRS 1/AHRS 2 check - no flags Condition Lever cut-off/feather Flaps 15° Flaps 0° A/P test button press, note lights Internal lights OFF Power Control Lever set 5 - 10 PSI Fuel Shut-off lever fully in TEST PUSHER switch push and hold Hydraulic hand pump handle stowed Power Control Lever set idle ECS Shut-off lever fully in CAWS panel check De-icing switches check, as required BEFORE STARTING ENGINE Pilot ventilation window closed and locked Preflight inspection complete External lights as required Seats adjusted and locked Parking Brake Handle release Seat belts fastened BAT 1&2 switches ON TAXIING Overhead panel voltmeter check 24 VDC Brakes check External power (if available): Connect then ON Flight instruments check EXT PWR switch ON PASS-WNG switches ON Overhead panel voltmeter check 28 VDC Landing gear 3 green lights Fuel contents check equal left/right Fuel pump LH ON, check audible, AUTO Fuel pump RH ON, check audible, AUTO OXYGEN lever ON Oxygen pressure gauge check 1850 PSI max PASS-OXY switch ON, check CAWS, set AUTO Oxygen masks check available, if required Pilot ventilation window closed and locked External lights as required PC-12/45 SCL (QRH Rev.1) REVISION 3: FEB 13, 2015 FOR FLIGHT SIMULATION PURPOSES ONLY. PILATUS LOGO AND CHECKLIST © PILATUS AIRCRAFT LTD BY AUTOGYRO 1 PC12/45 SCL (QRH Rev.3) SHORT CHECKLIST FOR COMPLETE INFORMATION REFER TO PC-12/45 POH SECTION 4 BEFORE TAKEOFF APPROACH Engine instruments check Ice Protection sys. as required Flight instruments check Altimiters set Trim set green lines and diamond Fuel quantity check Flaps 15° Landing Gear DN (below 180 KIAS) Flight controls free and correct Taxi/Landing lights as required Radios/avionics as required External lights as required CAWS panel check (no warning red lights) Flaps set conditions Probes switch ON Speed AOA centered Windshield heat as required Passengers brief/signs on External lights as required INERT SEP as required Transponder as required Runway identified FINAL HDG verified Landing Gear 3 green lights HDG Bug synchronised Flaps set as required Condition Lever FLIGHT IDLE Speed AOA centered INERT SEP as required Cabin Pressurization 0 Diff. Pressure Ice Protection sys. as required Autopilot disengaged Yaw Damper disengaged TAKEOFF EHSI check HDG LANDING ECS switch OFF Touch down main wheels first, do not flare with high pitch angle Power Control Lever set Power Control Lever IDLE or MAX reverse Engine instruments monitor, in limits Braking as required Rotate at VR, initial climb at VX or VY as req. After lift off + positive ROC: AFTER LANDING Brakes press to stop wheels Power Control Lever as required Landing Gear UP Condition Lever GROUND IDLE Yaw Damper ON Flaps UP Flaps 0° above 100 KIAS Trims set green range Taxi OFF External lights as required External lights as required Ice Protection sys. OFF or as required Yaw Damper as required Transponder STBY or check GND WX Radar as required WX Radar STBY CLIMB SHUTDOWN Ice Protection sys. as required Power Control Lever idle detent for 2 min Autopilot as required Parking brake set/pedals push Power Control Lever set as required ECS switch OFF ECS switch AUTO External lights OFF Cabin Pressurization monitor Ice Protection sys. OFF Engine instruments monitor Cooling and Heating sys. OFF Torque max 44.3 PSI PASS-WNG switches OFF ITT max 760°C, 720°C rec. STBY BUS switch ON Ng max 104% AV Bus 1&2 switches OFF Temperature setting as required GEN 1&2 switches OFF Condition lever cut off/feather CRUISE Oxygen shut-off lever OFF Altimeters set and cross-check Lighting switches OFF Cabin Pressurization monitor CAWS OIL QTY check Power Control Lever set, to cruise table (60 secs min after shutdown) refill if required Engine instruments monitor BAT 1&2 switches OFF Ice Protection sys. as required STBY BUS switch OFF Flight Control Lock installed DESCENT Wheel Chocks as required ATIS/Briefing received/performed Tie downs as required Ice Protection sys. as required Rudder/nose wheel centered Power Control Lever set to desired torque Propeller anchor installed Cabin Pressure controller set to LFE +500ft External covers installed PC-12/45 SCL (QRH Rev.1) REVISION 3: FEB 13, 2015