Read Pilatus_PC-12.cdr text version

Aircraft Operating Manuals

Pilatus PC-12

Aircraft Operating Manuals

Aircraft Operating Manuals Pilatus PC-12 CHECK LIST 1/5

Preflight Flight Control Lock ........................... REMOVED AND PLACED IN STOWAGE POINT Parking Brake Handle ..................................................... SET/PUSH BRAKE PEDALS External Power Switch ........................................................................................... OFF Battery 1 and 2 Switches ....................................................................................... OFF Generator 1 and 2 Switches ................................................................................... OFF AV Bus 1 and 2 Switches ....................................................................................... OFF Non-Essential Bus ............................................................................................... AUTO STBY BUS Switch .................................................................................................. ON TEST LAMP Switch .............. PUSH, CHECK OVERHEAD PANEL INDICATORS ON EXTERNAL LIGTHS Switches ............................................................................... OFF FUEL PUMPS Switches ...................................................................................... AUTO IGNITION Switch ................................................................................................. AUTO DE-ICING Switches ................................................................................................ OFF COOLING SYS Switch ........................................................................................... OFF HEATING Switches ................................................................................................. OFF Landing Gear Handle .......................................................................................... DOWN ECS Switch ............................................................................................................. OFF CABIN PRESS Switch ....................................................................... AUTO/GUARDED Cabin Pressure Controller ............................ SET TO CRUISE ALTITUDE + 500 FEET Manual Override Lever ........................................................................................... OFF Power Control Lever................................................................................ IDLE DETENT Condition Lever ............................................................................. CUT-OFF/FEATHER Flap Lever .................................................................................................................... 0º Cockpit/Instruments/Cabin Light Switches ............................................................. OFF

Before Starting Preflight Inspections ................................................................................... COMPLETE Battery 1 and 2 Switches .......................................................................................... ON Overhead Panel Voltmeter ................................................ CHECK (23 VDC MINIMUN) Landing Gear 3 Greens ..................................................................................... CHECK Fuel Contents ........................................... CHECK EQUAL LEFT AND RIGHT LEVELS FUEL PUMP LH Switch ON and AUTO ................ CHECK FOR AUDIBLE OPERATON FUEL PUMP RH Switch ON and AUTO ............... CHECK FOR AUDIBLE OPERATON OXYGEN Lever ......................................................................................................... ON External Lights ....................................................................................... AS REQUIRED

Aircraft Operating Manuals Pilatus PC-12 CHECK LIST 2/5

Engine Starting Fuel Quantity ....................................................................................................... CHECK EIS System ............................................................................................................. TEST TEST FIRE Switch ............................. PUSH (ENG FIRE AND F DETECT LIGHTS ON) TEST LAMP Switch .............. PUSH (WARNING, CAUTION, ADVYSORY LIGHTS ON) Propeller Area ...................................................................................................... CLEAR STARTER Switch .................................................................... PUSH FOR 2 SECONDS (A) Oil Pressure ................................................................................. CHECK RISING (B) Ng ................................................................... STABLE BETWEEN 9% AND 14% Condition Lever ...................................................................................... GROUND IDLE Starter Sequence ...................................................................................... COMPLETED Engine Instruments ............................................................................................. CHECK Fuel Totalizer ....................................................................................................... RESET Generator 1 Switch ..................................................... ON (CHECK CAWS GEN 1 OFF) Generator 2 Switch ..................................................... ON (CHECK CAWS GEN 2 OFF) INVERTER BAT or GEN ............................ CHECK FUNCTION/CHANGE SELECTION AV Bus 1 and 2 Switches ........................................................................................... ON STBY BUS Switch .................................................................................................... OFF Radios/Avionics ...................................................................................... AS REQUIRED ESC Switch ............................................................................................................ AUTO Temperature Setting ............................................................................ .. AS REQUIRED Cooling or Heating System ..................................................................... AS REQUIRED Inertial Separator ....................................................................................................OPEN Before Taxiing AHRS 1/AHRS 2 ............................................................................ CHECK (NO FLAGS) Flap Lever ................................................................................................................... 15º Autopilot Test Button ................................................................. PRESS MOMENTARILY CAWS Panel .................................................... CHECK (NO RED WARNINGS LIGHTS) DE-ICING PROBES Switch ............................. PUSH TO ON AND CHECK CAWS AOA DE-ICE, PITOT 1, PITOT 2, STATIC CAUTIONS OFF DE.ICING LH WSH Switch ...... PUSH TO ON AND CHECK CAWS WSHLD HEAT OFF DE-ICING RH WSH Switch ...... PUSH TO ON AND CHECK CAWS WSHLD HEAT OFF EXTERNAL LIGHTS Switches ................................................................ AS REQUIRED Parking Brake Handle ..................................................................................... RELEASE

Aircraft Operating Manuals Pilatus PC-12 CHECK LIST 3/5

Taxiing Brakes ................................................................................................................. CHECK Flight Instruments ................................................................................................ CHECK Before Takeoff Checklist Takeoff Power Setting ............................................................................... CALCULATED Fuel Quantity ....................................................................................................... CHECK Engine Instruments .............................................................................................. CHECK Flight Instruments ................................................................................................ CHECK Trim .................................................................................................. SET GREEN LINES Flap ............................................................................................................................. 15º Flight Controls ............................................................................. FREE AND CORRECT CAWS Panel .......................................................CHECK (NO WARNING RED LIGHTS) Radios/Avionics ....................................................................................... AS REQUIRED De-Ice Probes Switch ................................................................................................. ON Windshield Heat ....................................................................................... AS REQUIRED External Light Switches ............................................................................ AS REQUIRED Transponder .............................................................................................. ON ALTITUDE Condition Lever .......................................................................................... FLIGHT IDLE DE-ICING Switches ................................................................................. AS REQUIRED Takeoff EHSI ........................................................................................................... CHECK HDG ESC Switch ............................................................................................................... OFF Power Control Lever ................................................................................................. SET Engine Instruments............................................................................................................ A) Torque ..................................................................................................... MONITOR B) ITT .......................................................................................................... MONITOR C) Ng ........................................................................................................... MONITOR D) Oil Temp/Pressure .................................................................................. MONITOR Rotate at Vr, Initial Climb at Vx or Vy ....................................................... AS REQUIRED Brakes ................................................................. PRESS TO STOP WHELL ROTATION

Aircraft Operating Manuals Pilatus PC-12 CHECK LIST 4/5

After Lift-Off and Positive Rate of Climb: Landing Gear Handle .................................................................................................. UP Flaps ................................................................................................ 0º ABOVE 100 KIAS Taxi Light ................................................................................................................... OFF External Lights ......................................................................................... AS REQUIRED Yaw Damper ............................................................................................ AS REQUIRED Climb Ice Protection System .............................................................................. AS REQUIRED Autopilot ................................................................................................... AS REQUIRED Power Control Lever .................................................................................................. SET ECS Switch ............................................................................................................ AUTO Engine Instruments ............................................................................................................ A) Torque ..................................................................................................... MONITOR B) ITT ........................................................................................................... MONITOR C) Ng ........................................................................................................... MONITOR D) Oil Temp/Pressure .................................................................................. MONITOR Temperature Setting ................................................................................. AS REQUIRED Inertial Separator ............................................................................................... CLOSED Cruise Altimeters .......................................................................................... SET 29.92 (1013.2) AHRS ................................................................................................................... CHECK Cabin Pressurization ....................................................................................... MONITOR Power Control Lever ................................................................................................. SET Engine Instruments ......................................................................................... MONITOR Ice Protection System .............................................................................. AS REQUIRED Descend Ice Protection System .............................................................................. AS REQUIRED Power Control Lever ........................................................... SET TO DESIRED TORQUE Cabin Pressure Controller ............................... SET TO FIELD ELEVATION + 500 FEET Windshield Heat ....................................................................................... AS REQUIRED

Aircraft Operating Manuals Pilatus PC-12 CHECK LIST 5/5

Before Landing Ice Protection System .............................................................................. AS REQUIRED Altimeter .................................................................................................................... SET Fuel Quantity ....................................................................................................... CHECK Landing Gear ........................................................................ DOWN (BELOW 177 KIAS) Landing Lights ......................................................................................... AS REQUIRED External Lights ......................................................................................... AS REQUIRED Flaps (Normal) ......................................................................... SET 15º (MAX 163 KIAS) Speed ................................................................................................... AOA CENTERED Passengers ............................................................................................................ BRIEF Inertial Separator ......................... ON (IF OPERATING ON UNPREPARED SURFACE) Final Check Landing Gear ................................................................................................. 3 GREENS Flaps (Normal) .................................................................... SET 40º (BELOW 130 KIAS) Speed ................................................................................................... AOA CENTERED Pressurization ................................................................................... 0 DIFF PRESSURE Autopilot .................................................................................................... DISENGAGED Yaw Damper ............................................................................................. DISENGAGED

Aircraft Operating Manuals Pilatus PC-12 PERFORMANCE 1/5

Stall Speeds - Flight Idle Power Example: (Standard Units) Notes: Stall is defined by Pusher Activation. Landing Gear position has no effect. Weight Flaps Angle of Bank Stall Speed - KIAS

REFERENCE LINE 140

7800 lb 40º 45º 69

120 STALL SPEED - KMOTS CALIBRATED

100 FLAPS 0 80 FLAPS 15 FLAPS 30 FLAPS 40 60

40 11000 10000 9000 8000 WEIGT - LB 7000 6000 0 20 40 60

ANGLE OF BANK - DEG

Aircraft Operating Manuals Pilatus PC-12 PERFORMANCE 2/5

Aircraft Operating Manuals Pilatus PC-12 PERFORMANCE 3/5

Aircraft Operating Manuals Pilatus PC-12 PERFORMANCE 4/5

Aircraft Operating Manuals Pilatus PC-12 PERFORMANCE 5/5

Aircraft Operating Manuals Pilatus PC-12 WEIGHT AND BALANCE ½

Aircraft Operating Manuals Pilatus PC-12 WEIGHT AND BALANCE 2/2

Information

Pilatus_PC-12.cdr

13 pages

Find more like this

Report File (DMCA)

Our content is added by our users. We aim to remove reported files within 1 working day. Please use this link to notify us:

Report this file as copyright or inappropriate

316579


You might also be interested in

BETA
44886B001
02959602
Microsoft Word - FIST 4-1A-Jan21-09.DOC