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Pilatus PC-12/47E Quick Reference Handbook

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TO ALL OWNERS
AND OPERATORS
Pilatus Aircraft, Ltd is delighted to release the Quick Reference Handbook (QRH) for the PC-12/47E
aircraft with MSN 1720 and MSN 2001 upwards. This document is based on the latest revision of the
PC-12/47E Pilot's Operating Handbook (POH) and EASA Approved Airplane Flight Manual (Report No.
02406, ISSUE 003 REVISION 03: APR 24, 2023) and Section 9 Supplements 02415 and 02439.
The operator must be aware of the disclaimer printed on the coversheet of the present QRH.
By using this QRH, the operator declares that the conditions of the mentioned disclaimer are
understood and accepted.
This QRH (REVISION 3: APR 25, 2023) replaces the previous QRH (REVISION 2: OCT 29, 2021), which
is invalid and shall no longer be used. The QRH REVISION 2 must be returned to Pilatus, or destroyed.
This QRH is only valid for aircraft MSN 1720 and MSN 2001 upwards. The identification plate installed
on the lower left side of the rear fuselage defines the Model Designation as PC-12/47E.
One QRH is supplied with a POH. Similarly, the revision service of one QRH is included in the revision
service of the POH.
Additional QRH's and revision services can be ordered directly from your MyPilatus account or by using
the order form available at www.pilatus-aircraft.com (Menu \ Customer support \ Technical Publications
\ PC-12 \ General \ PC-12 Publications Order Form).
It is the responsibility of the operator to keep the QRH updated.
Best regards,
Pilatus Aircraft Ltd

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Summary of Contents for Pilatus PC-12/47E

  • Page 1 This QRH (REVISION 3: APR 25, 2023) replaces the previous QRH (REVISION 2: OCT 29, 2021), which is invalid and shall no longer be used. The QRH REVISION 2 must be returned to Pilatus, or destroyed. This QRH is only valid for aircraft MSN 1720 and MSN 2001 upwards. The identification plate installed on the lower left side of the rear fuselage defines the Model Designation as PC-12/47E.
  • Page 3 AIRCRAFT. IN THE EVENT OF ANY CONTRADICTIONS, THE POH SHALL PREVAIL OVER THE QRH. PILATUS WILL AT ITS SOLE DISCRETION DECIDE FROM TIME TO TIME TO ISSUE AND DISTRIBUTE REVISIONS TO THIS QRH IN ORDER TO FOLLOW UP SOME OF THE MOST IMPORTANT APPROVED POH REVISIONS.
  • Page 4 This PC-12/47E QRH Revision 03 is based on:  POH 02406 and EASA approved AFM Issue 003 Revision 03 dated APR 24, 2023  AFMS 02415 Issue 001 Revision 00 dated OCT 16, 2019  AFMS 02439 Issue 002 Revision 02 dated...
  • Page 5 Set MIC SELECT switch on the rear left panel to MASK 3. PASSENGER OXYGEN AUTO or ON selector 4. Systems MFD PAX OXY Confirm ON advisory Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 3...
  • Page 6 - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH...
  • Page 7  Fuel reserves. The pilot must consider the situation and priorities and adjust his actions accordingly. 10. Power control lever Idle 11. Landing gear Below 180 KIAS, down 12. Aircraft speed REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 5...
  • Page 8 - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH...

  • Page 9: Master Power

    Put the smoke goggles on. d. Put the normal headset back on. e. Set MIC SELECT switch on the rear left panel to MASK. 5. Crew Oxygen EMGCY Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 7...
  • Page 10 - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH...
  • Page 11 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - B. NG UNDERSPEED - ON GROUND 1. NG Check NG % indication If NG is below 64.5%: 2. PCL IDLE 3. Engine Shutdown Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 9...
  • Page 12 EEC CH B CB PULL (Ess. Bus f. EEC CH A CB PUSH, wait for 1 second (Ess. Bus g. EEC CH B CB PUSH (Ess. Bus Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 10...

  • Page 13: Emergency Landing

    - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 11...
  • Page 14 - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 12...
  • Page 15 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - B. IN FLIGHT 1. Oil Check OIL T °C indication Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 13...
  • Page 16 In certain EPECS Fail conditions, the system commands flight idle and feathers the propeller. The engine continues to provide bleed air for cabin pressurization, airframe anti/de-icing and generator power. Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 14...

  • Page 17: Engine Failure In Flight

    - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 15...
  • Page 18 - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 16...
  • Page 19 - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 03: APR 25, 2023 PC-12/47E QRH PAGE 17...
  • Page 20 - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 03: APR 25, 2023 PC-12/47E QRH PAGE 18...
  • Page 21 ADAHRS B 2. Pilot PFD window Confirm ADAHRS 2 flag which indicates attitude, heading and air data same source as copilot PFD. Compare with ESIS Cont. on next page REVISION 01: DEC 18, 2020 PC-12/47E QRH PAGE 19...
  • Page 22 - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 01: DEC 18, 2020 PC-12/47E QRH PAGE 20...
  • Page 23 8. PASSENGER AUTO or ON OXYGEN selector 9. Systems MFD PAX OXY Confirm on advisory 10. Passengers Instruct to don masks 11. CPCS MODE Confirm MANUAL switch Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 21...
  • Page 24 - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 22...
  • Page 25 - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 23...
  • Page 26 - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 24...
  • Page 27 Stick shaker may activate at higher speeds than normal. If this occurs, increase speed until shaker stops. 9. Aircraft Avoid further icing conditions 10. Flap position Limited to 15° Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 25...
  • Page 28 - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 26...
  • Page 29 Put the oxygen mask on. Check 100% c. Put the normal headset back on d. Set MIC SELECT switch on the rear left panel to MASK 4. PASSENGER OXYGEN AUTO or ON selector Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 27...
  • Page 30 - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 28...
  • Page 31 - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 29...
  • Page 32 INTENTIONALLY LEFT BLANK REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 30...
  • Page 33 22 V or above 30.1 V. 1. Systems MFD - Check GEN 2 and ELECTRICAL window BAT 2 current and voltage If indications are normal: 2. BAT 2 switch Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 31...
  • Page 34 - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 32...
  • Page 35 20 seconds dwell time before inflation sequence starts, this to prevent damage to the pneumatic de-ice boots due to inflation outside of their operating envelope (-40 °C - +40 °C). REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 33...
  • Page 36 Set MIC SELECT switch on the rear left panel to MASK 7. PASSENGER OXYGEN AUTO or ON selector 8. Systems MFD PAX OXY Confirm ON advisory 9. Passengers Instruct to don masks Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 34...
  • Page 37 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 35...
  • Page 38 Put the oxygen mask on. Check 100% c. Put the normal headset back on d. Set MIC SELECT switch on the rear left panel to MASK 4. PASSENGER OXYGEN AUTO or ON selector Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 36...
  • Page 39 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 37...
  • Page 40 B. IN FLIGHT - If ∆P and CAB ALT indications are available: 1. CPCS MODE switch MANUAL for at least 1 sec, then AUTO 2. CAS Check CPCS fault remains: 3. CPCS MODE switch MANUAL Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 38...

  • Page 41: Manual Control

    - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 39...
  • Page 42 Continue flight and monitor system. Avoid low power settings if possible If captions stay in failure status: 6. Aircraft Depart icing conditions to positive SAT atmosphere, if possible Cont. on next page REVISION 03: APR 25, 2023 PC-12/47E QRH PAGE 40...
  • Page 43 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 41...
  • Page 44 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 42...
  • Page 45 Set MIC SELECT switch on the rear left panel to MASK 12. PASSENGER OXYGEN ON. Check contents. selector Calculate Oxygen duration. 13. Systems MFD PAX OXY Confirm on advisory Cont. on next page REVISION 01: DEC 18, 2020 PC-12/47E QRH PAGE 43...
  • Page 46 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 44...
  • Page 47 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 45...
  • Page 48 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 46...
  • Page 49 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - B. IN FLIGHT 1. Aircraft Check and monitor engine parameters. Possible degraded engine response. Prepare for uncommanded change in engine power 2. Autothrottle Disconnect (if active) Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 47...
  • Page 50 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 48...
  • Page 51 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 49...
  • Page 52 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 50...
  • Page 53 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 51...
  • Page 54 INTENTIONALLY LEFT BLANK REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 52...
  • Page 55 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 53...
  • Page 56 INTENTIONALLY LEFT BLANK REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 54...
  • Page 57 5 segments for landing. Use flaps up to keep approach speed high. If no fuel leak is suspected: 7. FUEL PUMP CB (on fuller side) Reset (Essential bus J1 or Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 55...
  • Page 58 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 56...
  • Page 59 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 57...
  • Page 60 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 58...
  • Page 61 When the system switches FUEL PUMPs automatically to ON at lower engine power, this is a result of degraded ejector pump performance. Fuel Pressure Low persists: 13. FUEL PUMP switches Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 59...
  • Page 62 (on affected side) (Essential bus J1 or 3. FUEL PUMP switch (on affected side) After 10 seconds: 4. FUEL PUMP switch AUTO (on affected side) 5. Fuel state Monitor Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 60...
  • Page 63 If a prompt landing is not possible, keep high IAS to nearest airfield and consider burning off fuel until the fuel imbalance is not greater than 5 segments for landing. Use flaps up to keep approach speed high. REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 61...
  • Page 64 4. Aircraft Descend to warmer air if necessary If indicated fuel temperature remains low (less than 12 °C): 5. CAS window Check for fuel filter faults Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 62...
  • Page 65 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 63...
  • Page 66 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 64...
  • Page 67 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 01: DEC 18, 2020 PC-12/47E QRH PAGE 65...
  • Page 68 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 66...
  • Page 69 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 67...
  • Page 70 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 68...
  • Page 71 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 69...
  • Page 72 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 70...
  • Page 73 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 71...
  • Page 74 - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 72...
  • Page 75 If failure remains: 2. Display Reversion Control Panel Set LOWER MFD control knob to OFF/REV 3. Display Reversion Control Panel Set CO-PILOTS PFD control knob to AGM1 Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 73...
  • Page 76 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 74...
  • Page 77 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 75...
  • Page 78 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 76...
  • Page 79 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - B. IN FLIGHT 1. Pusher Test Carry out Pusher If Shaker 1 and 2 active and extinguished: 2. Aircraft No further action required Cont. on next page REVISION 03: APR 25, 2023 PC-12/47E QRH PAGE 77...
  • Page 80 Cycle from CLOSED to OPEN 4. PROP DE-ICE CB Check. Do not reset unless tripped (LH Power Junction Box) 5. INERT SEP CB Check. Do not reset unless tripped (Essential bus Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 78...
  • Page 81 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 79...
  • Page 82 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 80...
  • Page 83 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 81...
  • Page 84 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 82...
  • Page 85 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 83...
  • Page 86 INTENTIONALLY LEFT BLANK REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 84...
  • Page 87 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 02: OCT 29, 2021 PC-12/47E QRH PAGE 85...
  • Page 88 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 86...
  • Page 89 Reset the AFCS as follows: Open the A/P SERVO (Avionic 1 Bus Z2) and A/P SERVO ENABLE (Avionic 1 Bus Y2) CBs for 2 secs, then close. Check CAS. Only one reset attempt per flight. REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 87...
  • Page 90 * These messages require maintenance action if they cannot be cleared before flight, or dispatch the aircraft under the provisos of an approved and permissible PC-12 aircraft MEL. During flight, continue with remaining operational equipment and report on landing. REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 88...
  • Page 91 * These messages require maintenance action if they cannot be cleared before flight, or dispatch the aircraft under the provisos of an approved and permissible PC-12 aircraft MEL. During flight, continue with remaining operational equipment and report on landing. REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 89...
  • Page 92 * These messages require maintenance action if they cannot be cleared before flight, or dispatch the aircraft under the provisos of an approved and permissible PC-12 aircraft MEL. During flight, continue with remaining operational equipment and report on landing. REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 90...
  • Page 93 * These messages require maintenance action if they cannot be cleared before flight, or dispatch the aircraft under the provisos of an approved and permissible PC-12 aircraft MEL. During flight, continue with remaining operational equipment and report on landing. REVISION 02: OCT 29, 2021 PC-12/47E QRH PAGE 91...
  • Page 94 * These messages require maintenance action if they cannot be cleared before flight, or dispatch the aircraft under the provisos of an approved and permissible PC-12 aircraft MEL. During flight, continue with remaining operational equipment and report on landing. REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 92...
  • Page 95 Reset the AFCS as follows: Open the A/P SERVO (Avionic 1 Bus Z2) and A/P SERVO ENABLE (Avionic 1 Bus Y2) CBs for 2 secs, then close. Check CAS. Only one reset attempt per flight. REVISION 02: OCT 29, 2021 PC-12/47E QRH PAGE 93...
  • Page 96 INTENTIONALLY LEFT BLANK REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 94...
  • Page 97 * These messages require maintenance action if they cannot be cleared before flight, or dispatch the aircraft under the provisos of an approved and permissible PC-12 aircraft MEL. During flight, continue with remaining operational equipment and report on landing. REVISION 03: APR 25, 2023 PC-12/47E QRH PAGE 95...
  • Page 98 * These messages require maintenance action if they cannot be cleared before flight, or dispatch the aircraft under the provisos of an approved and permissible PC-12 aircraft MEL. During flight, continue with remaining operational equipment and report on landing. REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 96...
  • Page 99 * These messages require maintenance action if they cannot be cleared before flight, or dispatch the aircraft under the provisos of an approved and permissible PC-12 aircraft MEL. During flight, continue with remaining operational equipment and report on landing. REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 97...
  • Page 100 INTENTIONALLY LEFT BLANK REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 98...
  • Page 101 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 03: APR 25, 2023 PC-12/47E QRH PAGE 99...
  • Page 102 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 100...

  • Page 103: Emergency Off

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  • Page 104 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 01: DEC 18, 2020 PC-12/47E QRH PAGE 102...

  • Page 105: Air Start

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  • Page 106 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 104...
  • Page 107 5. EEC CH B CB PULL (Essential Bus 6. EEC CH A CB PUSH, wait for 1 sec. (Essential Bus 7. EEC CH B CB PUSH (Essential Bus Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 105...
  • Page 108 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 106...
  • Page 109 13. VENT FANS 14. Fire extinguisher Use if required As soon as time permits and source is known to be electrical: 15. Associated electrical Off (CBs) equipment Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 107...

  • Page 110: Master Power Switch

    - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 108...
  • Page 111 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 109...
  • Page 112 After 5 mins battery can be switched ON again. If indication still positive, switch battery OFF. NOTE Engine Oil Level Engine Oil Temp During extended glide period and/or may appear - disregard for air start. Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 110...
  • Page 113 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 111...

  • Page 114: Maximum Rate Descent

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  • Page 115 Set to ON If landing site allows: 10. Landing gear DOWN If landing site not suitable for gear down landing: 11. Landing gear Keep UP 12. Flaps 40° Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 113...
  • Page 116 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 114...
  • Page 117 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Landing without Elevator Control 1. Passengers Brief 2. Landing gear DOWN 3. Flaps 40° Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 115...
  • Page 118 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 116...
  • Page 119 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 117...
  • Page 120 INTENTIONALLY LEFT BLANK REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 118...
  • Page 121 Select DN If 3 green lights not illuminated within 30 seconds: Emergency Extension 3. Aircraft Refer to (next page) If 3 green lights illuminated: 4. Aircraft Land as soon as practical REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 119...
  • Page 122 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 120...
  • Page 123 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 121...
  • Page 124 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 03: APR 25, 2023 PC-12/47E QRH PAGE 122...

  • Page 125: Fuel System

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  • Page 126 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 124...
  • Page 127 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 125...
  • Page 128 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 126...

  • Page 129: Wheel Brake

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  • Page 130 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 128...
  • Page 131 105 KIAS (flap position limit 15°) D. Balked Landing (Go Around): After failure of: Pneumatic Deice Boots (flap position limit 0°) (TO/Pwr, flaps 0°, LG down, Pusher Ice Mode) 130 KIAS REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 129...
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  • Page 133 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 131...
  • Page 134 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 03: APR 25, 2023 PC-12/47E QRH PAGE 132...
  • Page 135 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 03: APR 25, 2023 PC-12/47E QRH PAGE 133...
  • Page 136 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 03: APR 25, 2023 PC-12/47E QRH PAGE 134...
  • Page 137 The total landing distance will be longer by up to 71%. Refer to the POH Section 5, Performance, for the exact landing distance calculation. 10. Aircraft Land as soon as practical Cont. on next page REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 135...
  • Page 138 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 136...

  • Page 139: Stuck Mic

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  • Page 140 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 138...
  • Page 141 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 139...
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  • Page 143: Before Taxiing

    PC-12/47E SHORT CHECKLIST MSN 1720, 2001 and up FOR COMPLETE INFORMATION REFER TO PC-12/47E POH 02406 SECTION 4 COCKPIT PREPARATION Oxygen pressure gage check 1850 PSI max Flight control lock removed+stowed PAX OXYGEN selector AUTO. Set switch to EMERG COM 1 switch...
  • Page 144 PC-12/47E SHORT CHECKLIST MSN 1720, 2001 and up FOR COMPLETE INFORMATION REFER TO PC-12/47E POH 02406 SECTION 4 LINE UP CHECK APPROACH Probes switch Altimeter Windshield heat as required Ice protection system as required INERT SEP as required INERT SEP...
  • Page 145 REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 143...
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  • Page 152 REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 150...
  • Page 153 1300 1400 1500 1600 1700 1800 1015 1900 1070 2000 1125 2100 1180 2200 1000 1240 2300 1045 1295 2400 1090 1350 2500 1135 1405 2600 1180 1465 2700 1225 1520 REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 151...
  • Page 154 INTENTIONALLY LEFT BLANK REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 152...
  • Page 155 Conversion CPFD Copilot Primary Flight Display CPCS Cabin Pressurization Control System CSIO Custom Input Output Control CTLR Controller Acronyms Meaning Database DEOS Digital Engine Operating System Distance Measuring Equipment Dead Reckoning REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 153...
  • Page 156 Indicated Airspeed Instrument Meteorological Condition INAV Integrated Navigation INERT SEP Inertial Separator Inhib Inhibit Inop Inoperative INTR Interrupt IOAT Indicated Outside Air Temperature Interstage Turbine Temperature Input/Output KIAS Knots Indicated Airspeed REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 154...
  • Page 157 Phase of Flight Pilot Operating Handbook PPFD Pilot Primary Flight Display PPOS Present Position Primary PROP Propeller Pounds per Square Inch Power P&WC EMM Pratt & Whitney Canada Engine Maintenance Manual REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 155...
  • Page 158 Very High Frequency Visual Meteorological Condition VNAV Vertical Navigation VHF Omni-directional Radio range Vertical Speed Indicator WARN Warning Weight On Wheel Waypoint WSHLD Windshield Weather Radar XPDR or XPNDR Transponder Yaw Damper REVISION 00: MAR 11, 2020 PC-12/47E QRH PAGE 156...

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