PC-12

© Bernhard Baur

ADs applicable to Swiss registred aeronautical products designed by
PILATUS AIRCRAFT Ltd.

Pertaining to Model: PC-12, PC-12/45, PC-12/47, PC-12/47E, PC-12/47G
TCDS: EASA.A.089
Last update: 02 December 2025

• EASA 2025-0271 - CENTRAL COMPUTER/PRIMUS APEX OPERATIONAL SOFTWARE/MODIF.

  EASA 2025-0271

  • PC-12 SB SB 45-030

    PDF166.60 kB29. September 2025

  • PC-12 POH TR 32

    PDF141.99 kB3. September 2025

• EASA 2025-0201 - LOSS OF AVIONICS-ENGINE INDICATIONS DURING ENGINE START/AFM AMEND.

  EASA 2025-0201 - 18.9.2025

  • PC-12 POH TR 31

    PDF141.87 kB16. Juli 2025

• EASA 2025-0182 - EMERGENCY EXIT-PASSENGER SERVICE UNIT TRIM PANEL INSTALLATION/MODIF.

  EASA 2025-0182 - 25.8.2025

  • PC-12 SB 25-059

    PDF355.05 kB2. Mai 2025

• EASA 2023-0184 - AIRWORTHINESS LIMITATION SECTION/AMEDMENT

  EASA 2023-0184

  • PC-12 AMM 02049 R46

    PDF942.90 kB2. Oktober 2023

  • PC-12 AMM 02300 R31

    PDF1.33 MB2. Oktober 2023

  • PC-12 AMM 02436 R9

    PDF2.06 MB2. Oktober 2023

• EASA 2022-0245 - NOSE & MAIN LANDING GEAR ACTUATORS/REPLMNT.

  EASA 2022-0245

  Todo: Datei nicht gefunden "32-030R2"

• EASA 2022-0212 - VAPOUR CYCLE COOLING SYSTEM-COMPRESSOR CONDENSER CABLES/INSP;MODIF.

  EASA 2022-0212

  • PC-12 SB 21-016

    PDF629.88 kB15. August 2022

• EASA 2022-0158 - NOSE & MAIN LANDING GEAR ACTUATORS/REPLMNT.

  EASA 2022-0158

  • PC-12 SB 32-030R1

    PDF1.84 MB12. September 2022

• EASA 2022-0103 - AIRWORTHINESS LIMITATION SECTION/AMEDMENT - SUPERSEDED BY 2023-0184

  EASA 2022-0103

  Todo: Dokumene fehlen
  AMM 02049 R43
  AMM 02300 R28
  AMM 02436 R6

• EASA 2021-0110-CN - CANCELLATION OF EASA AD 2021-0110

  EASA 2021-0110-CN

  • PC-12 SB 32-029R1

    PDF2.34 MB6. August 2021

• EASA 2021-0214 - AIRWORTHINESS LIMITATION SECTION/AMEDMENT

  EASA 2021-0214

  Todo: Dokumene fehlen
  AMM 02049 R41
  AMM 02300 R25
  AMM 02436 R3

• EASA 2021-0110 - CANCELLATION OF EASA AD 2021-0110

  EASA 2021-0110

  • PC-12 SB 32-029

    PDF598.86 kB8. Februar 2021

• EASA 2021-0010 - FUEL INWARD VENT VALVE/MODIF.

  EASA 2021-0010

  • PC-12 SB 28-015

    PDF2.59 MB12. Oktober 2020

• EASA 2021-0005 Correction - AIRWORTHINESS LIMITATION SECTION/AMEDMENT

  EASA 2021-0005 COR.

  AMM 02049 R40
  AMM 02300 R24
  AMM 02436 R2

• EASA 2020-0229 - FUEL TRANSFER EJECTOR/REPLMNT.

  EASA 2020-0229

  • PC-12 SB 28-014

    PDF516.37 kB12. August 2020

• EASA 2019-0231 - FLAP DRIVE SYSTEM-FLAP FAIRINGS AND FRONT INBOARD TENSION RODS/INSP.

  EASA 2019-0231

  • PC-12 SB 27-026

    PDF1.13 MB10. Juli 2019

• EASA 2019-0129 - HORIZONTAL STABILIZER REAR ATTACHMENT BOLTS/REPLMNT.

  EASA 2019-0129

  • PC-12 SB 55-004

    PDF3.36 MB29. März 2019

• EASA 2019-0032 - MAIN LANDING GEAR SPRING PACK ASSEMBLIES/REPLMNT.

  EASA 2019-0032

  • PC-12 SB 32-027

    PDF148.01 kB7. Januar 2019

• EASA 2017-0024 - PRIMUS APEX BUILD 10 OR 10.9/AFM AMEND.

  EASA 2017-0024

  • PC-12 POH TR 38

    PDF22.31 kB8. Februar 2017

• EASA 2016-0083 - AIRWORTHINESS LIMITATION SECTION/AMEDMENT

  EASA 2016-0083

  AMM_R14

  • PC-12 AMM 02300 R31

    PDF1.33 MB2. Oktober 2023

  • PC-12 SL 186

    PDF365.53 kB27. April 2016

• EASA 2016-0081 - ENGINE MOUNTING FRAME-SWAGED TUBE ENDS/INSP.

  EASA 2016-0081

  • PC-12 SB 71-009R2

    PDF1.41 MB18. März 2016

• EASA 2016-0037 - WING-TO-FUSELAGE ATTACHMENT TORLON PLATES/INSP.

  EASA 2016-0037

  • PC-12 SB 57-007

    PDF211.18 kB29. September 2015

• EASA 2015-0111 - AILERON CONTROL SYSTEM-UNIVERSAL JOINTS/REPLMNT.

  EASA 2015-0111

  • PC-12 SB 27-022

    PDF587.59 kB17. März 2015

• EASA 2014-0170 - AIRWORTHINESS LIMITATION SECTION/AMEDMENT

  EASA 2014-0170

  AMM_R28

  AMM_R11

• EASA 2013-0114 - ELECTRONIC STANDBY INSTRUMENT SYSTEM-POWER RETURN WIRES/MODIF.

  EASA 2013-0114

  • PC-12 SB 34-038

    PDF503.86 kB26. Mai 2013

• EASA 2013-0031 - AIRWORTHINESS LIMITATION SECTION/AMEDMENT

  EASA 2013-0031

  AMM_R26

  • PC-12 AMM 02436 R9

    PDF2.06 MB2. Oktober 2023

• EASA 2012-0099 - AIRWORTHINESS LIMITATION SECTION/AMEDMENT

  EASA 2012-0099

  AMM_R25

  AMM_R8

• EASA 2010-0093 - POWER CONTROL LEVER REVERSE THRUST LATCH/INSP.

  EASA 2010-0093

  • PC-12 POH TR 12-PCL

    PDF9.82 kB15. Oktober 2009

  • PC-12 SB 76-002R1

    PDF642.12 kB7. Juli 2011

• EASA 2009-0249 - ADAHRS-ROLL ATTITUDE OFFSET/SOFTWARE MODIF.OR REPLMNT.

  EASA 2009-0249

  • Honeywell SB KSG 7200-34-09

    PDF2.55 MB24. September 2009

  • PC-12 SB 34-022

    PDF121.88 kB5. Oktober 2009

• EASA 2009-0086 - NOSE LANDING GEAR-RH UPPER DRAG LINK/INSP;LIFE LIMIT.

  EASA 2009-0086

  AMM_TR

  AMM_R1

• EASA 2009-0080-E - ADAHRS-ROLL ATTITUDE OFFSET/POH TEMP.REV.

  EASA 2009-0080-E

  • PC-12 POH TR 11

    PDF45.62 kB3. Februar 2004

  • PC-12 POH TR 11

    PDF12.70 kB18. März 2009

• EASA 2009-0060 - NOSE WHEEL STEERING TORQUE TUBE/REPLMNT;AMM REV.

  EASA 2009-0060

  • PC-12 SB 32-021

    PDF188.26 kB21. November 2008

• EASA 2009-0040 - STICK PUSHER SERVO CABLE/INSP.

  EASA 2009-0040

  • PC-12 SB 27-020R1

    PDF309.46 kB30. Januar 2009

• EASA 2009-0028-E - ADAHRS INCORRECT INFORMATION/POH TEMP.REV.

  EASA 2009-0028-E

  • PC-12 POH TR 9

    PDF237.65 kB30. Januar 2009

• EASA 2009-0007 - OVERBOARD VENT FOR AIRFOIL DE-ICE SYSTEM PRESS. REGULATOR/INST.

  EASA 2009-0007

  • PC-12 SB 30-011

    PDF279.61 kB9. Juli 2008

• EASA 2008-0163 - AIRWORTHINESS LIMITATION/AMEDMENT

  EASA 2008-0163

  AMM

• EASA 2008-0047 - ELEVATOR CONTROL STICK-PUSHER SERVO-CABLE/INSP.

  EASA 2008-0047

  • PC-12 SB 27-018

    PDF261.94 kB27. November 2007

• EASA 2007-0235 Correction - TORQUE OIL PRESSURE PIPE & HOSE ASSEMBLIES/INSP;REPLMNT.

  EASA 2007-0235 Correction

  • PC-12 SB 71-007

    PDF1.05 MB21. August 2007

• HB-2007-382 - MAIN LANDING GEAR SPECIAL BOLTS/IDENT;REPLMNT.

  HB-2007-382

  • PC-12 SB 32-020R1

    PDF771.67 kB22. November 2007

• HB-2006-444 - EXECUTIVE SEAT LEGS/IDENT;REPLMNT.

  HB-2006-444

  • PC-12 SB 25-032

    PDF134.96 kB2. Oktober 2006

  • Decrane SB 05147

    PDF315.12 kB26. Juni 2006

• HB-2006-223 - CENTER FUSELAGE FRAME 21/INSP.

  HB-2006-223

  • PC-12 SB 53-004

    PDF388.96 kB10. Juni 2006

• HB-2005-470 - CREW SEATS-BACKREST TUBES/LIFE LIMITATIONS

  HB-2005-470

  • PC-12 MM TR 04-13

    PDF29.34 kB15. Juni 2005

• HB-2005-288 - MAIN LANDING GEAR SPECIAL BOLT ASSEMBLY/INSP.

  HB-2005-288

  • PC-12 SB 32-018

    PDF374.92 kB2. Mai 2005

• HB-2005-168 - LANDING GEAR COMPONENTS/INSP.

  HB-2005-168

  • PC-12 SB 32-016

    PDF561.74 kB11. März 2004

  • PC-21 SB 32-016

    PDF1.79 MB14. September 2018

• HB-2005-128 - PITCH ACTUATOR/REPLMNT.

  HB-2005-128

  • PC-12 SB 22-004

    PDF128.16 kB21. Dezember 2004

• HB-2005-079 - WINDSHIELD DEICE SYSTEM WIRING/INSP.

  HB-2005-079

  • PC-12 SB 30-009

    PDF111.24 kB25. Juli 2005

• HB-2004-330 - MAIN LANDING GEAR ACTUATOR/REPLMNT.

  HB-2004-330

  • PC-12 SB 32-017

    PDF107.04 kB3. August 2004

• HB-2004-329 - CREW SEATS-BUCKET ASSEMBLY TUBES/INSP. - SUPERSEDED BY HB-2005-470

  HB-2004-329

  • PC-12 SB 25-031

    PDF410.19 kB21. Juli 2004

• HB-2004-182 - PASSENGER OXYGEN SYSTEM-OXYGEN PIPES/INSP;MODIF.

  HB-2004-182

  • PC-12 SB 35-004

    PDF262.17 kB19. Dezember 2003

• HB-2004-101 - GENERATOR CONTROL UNIT/REPLMNT.

  HB-2004-101

  • PC-12 SB 24-022

    PDF107.58 kB13. Juni 2003

  • PC-12 SB 24-010R1

    PDF2.64 MB6. Oktober 2003

  • PC-12 SB 24-019R1

    PDF1.27 MB6. Juni 2003

• HB-2004-068 - INBOARD & OUTBOARD FLAP FLEXIBLE SHAFTS/REPLMNT.

  HB-2004-068

  • PC-12 SB 27-015RA

    PDF430.41 kB13. November 2003

• HB-2004-048 - OERATIONAL LIMITATIONS-AUTOPILOT & FLAP SELECTION/POH REV. - SUPERSEDED BY HB-2005-128

  HB-2004-048

  • PC-12 POH TR 11

    PDF45.62 kB3. Februar 2004

  • PC-12 POH TR 40

    PDF46.41 kB3. Februar 2004

• HB-2003-522 - MAIN LANDING GEAR-SHOCK-ABSORBER ATTACHMENT BOLTS/REPLMNT.

  HB-2003-522

  • PC-12 SB 32-015

    PDF233.38 kB12. September 2003

• HB-2003-301 - FUEL BOOSTER PUMP WIRING/INSP;MODIF.

  HB-2003-301

  • PC-12 SB 28-011R1

    PDF223.69 kB11. Juli 2003

• HB-2003-251 - ENGINE DRIVEN FUEL PUMP/INSP;REPLMNT.

  HB-2003-251

  • PC-12 SB 28-009

    PDF240.17 kB10. August 2001

  • PC-12 SB 28-010

    PDF42.09 kB16. September 2002

• HB-2002-659 - OVERHEAD PANEL-SWITCH CAPS/REPLMNT.

  HB-2002-659

  • PC-12 SB 31-003

    PDF282.59 kB27. September 2002

• HB-2002-658 - PAX SEATS-PART NUMBER & PEDESTAL LEG ASSEMBLY/IDENT.

  HB-2002-658

  25-025

• HB-2002-609 - OPERATIONAL LIMITATION PLACARD/INSP.

  HB-2002-609

  11-003

• HB-2002-608 - REAR PRESSURE BULKHEAD/INSP;REPAIR

  HB-2002-608

  53-003R1

• HB-2002-271 - NOSE LANDING GEAR DRAG LINK RIGHTHAND PART/LIFE LIMIT. - SUPERSEDED BY EASA 2009-0086

  HB-2002-271

  ---

• HB-2001-636 - FIREWALL INSULATION/ADHESIVE TAPE APPL.

  HB-2001-636

  25-023

• HB-2001-603 - MAIN LANDING GEAR-SPECIAL BOLTS/REPLMNT.

  HB-2001-603

  32-012

• HB-2001-500 - ENGINE DRIVEN FUEL PUMP-RELIEF VALVE BODY SCEWS/INSP. - SUPERSEDED BY HB-2003-251

  HB-2001-500

  • PC-12 SB 28-009

    PDF240.17 kB10. August 2001

• HB-2001-389R1 - CARGO DOOR END FRAME LIGHTENING HOLES-REINFORCING PLATES/INSTALL.

  HB-2001-389R1

  52-004R1

• HB-2001-070 - FLAP CONTROL WIRING/MODIF.

  HB-2001-070

  27-011R1

• HB-2001-005 - FLAP SYSTEM LIMITATION/AFM-POH TEMP.REV. - SUPERSEDED BY HB-2001-070

  HB-2001-005

  ---

• HB-2001-001 - PASSENGER OXYGEN SYSTEM-REAR BENCH SEAT/MODIF.

  HB-2001-001

  35-002

• HB-2000-444 - FLAP CONTROL AND WARNING UNIT/REPLMNT.

  HB-2000-444

  27-012

• HB-2000-443 - FLAP SYSTEM/MODIF.

  HB-2000-443

  27-008R2

• HB-2000-393 - WINDSHIELD DE-ICE SYSTEM-WIRES AND CIRCUIT BRAKERS/MODIF.

  HB-2000-393

  30-006

• HB-2000-008 - WINDSHIELD HEATER OPERATION/AFM TEMP.REV. - SUPERSEDED BY HB-2000-393

  HB-2000-008

  ---

• HB-2000-007 - POWERPLANT-CHAFING OF PIPE ASSEMBLIES/INSP.

  HB-2000-007

  71-004

• HB-1999-542 - ELECTRICAL POWER-SUPPRESSION FILTER/REPLMNT.

  HB-1999-542

  24-014

• HB-1999-406 - STICK PUSHER SERVO AND CAPSTAN/REPLMNT.

  HB-1999-406

  22-003

• HB-1999-353 - FLAP INBOARD ATTACHMENT FITTINGS/MODIF.

  HB-1999-353

  57-004

• HB-1999-348 - WINDSHIELD HEAT WIRING/MODIF.

  HB-1999-348

  30-005

• HB-1999-347 - HEATED WINDSHIELD WIRING/OPS PROHIBITION - SUPERSEDED BY HB-1999-348

  HB-1999-347

  30-005

• HB-1999-241 - FLAPS DRIVE SHAFTS/REPLMNT.

  HB-1999-241

  27-003

• HB-1999-143 - ELECTRICAL POWER-GENERATOR 2 EXITATION/MODIF.

  HB-1999-143

  24-012

• HB-1999-142 - «LIMITED SERVICE-LIFE» FLAP SCREW ACTUATORS/REPLMNT.

  HB-1999-142

  27-007

• HB-1998-537 - ELECTRICAL POWER-CUT-OUT RELAY/INSTALL.

  HB-1998-537

  24-009

• HB-1998-460 - FLAP ACTUATORS/OPS LIMIT;REPET.INSP.

  HB-1998-460

  27-005

• HB-1998-426 - STANDBY MAGNETIC COMPASS SWING/REVISED PROCEDURE

  HB-1998-426

  34-006

• HB-1998-352 - ALTERNATE FLAP SYSTEM/MODIF;POH+AMM REV.

  HB-1998-352

  27-004

• HB-1998-179 - CORPORATE COMMUTER CABIN LAYOUT/HIC MODIF.

  HB-1998-179

  25-006

• HB-1998-126 - FUEL STORAGE-VENT VALVE SYSTEM/MODIF.

  HB-1998-126

  28-005

• HB-1998-086 - FUEL FILLER CAPS/MODIF. - SUPERSEDED BY HB-1998-126

  HB-1998-086

  28-004

• HB-1997-432A - FUEL TANK INWARD VENT VALVES/REPLMNT. - SUPERSEDED BY HB-1998-126

  HB-1997-432A

  28-003R1

• HB-1997-249A - EXECUTIVE CABIN LAYOUT/MODIF.

  HB-1997-249A

  25-003R1

• HB-1997-174 - AILERON TIE-ROD ASSEMBLY/MODIF.

  HB-1997-174

  27-001

• HB-1997-002 - DICONNECT NON ESSENTIAL BUS & NAV CONVERTER KN 40/INSP.

  HB-1997-002

  24-003R1

• HB-1997-001 - MAGNETIC COMPASS DEVIATION/MODIF;POH-,MM REV.

  HB-1997-001

  24-002R1

• HB-1996-535A - ELEVATOR/INSP;REPAIR

  HB-1996-535A

  55-001

• HB-1996-416 - PROPELLER DE-ICING CONTROLLER/REPLMNT.

  HB-1996-416

  30-002

• HB-1996-335 - DISCONNECT NON ESSENTIAL BUS & NAV CONVERTER KN 40/INSP. - SUPERSEDED BY HB-1997-002

  HB-1996-335

  24-003

• HB-1996-140 - MAGNETIC COMPASS DEVIATION/MODIF;POH REV. - SUPERSEDED BY HB-1997-001

  HB-1996-140

  30-001

• HB-1996-139 - HYDRAULIC HANDPUMP INSTALLATION/POH REV;MODIF.

  HB-1996-139

  29-001