PC-6

ADs applicable to Swiss registred aeronautical products.

© Pilatus Aircraft Ltd.

Design holder: Pilatus Aircraft Ltd.
Model: PC-6 Series
FOCA TC/TCDS: F 56-10
Last update: 24 February 2026

• EASA 2025-0281 - AIRWORTHINESS LIMITATIONS SECTION/AMEND.

  EASA 2025-0281

  • PC-6 ALS Doc. 02334R13 extract

    PDF170.56 kB31. Oktober 2025

  • PC-6 AMM Doc. 01975R39 extract

    PDF204.29 kB31. Oktober 2025

• EASA 2021-0098 - AILERON, ELEVATOR & RUDDER HINGE BOLT INSTALLATION/IDENT;MODIF.

  EASA 2021-0098

  • PC-6 SB 55-005

    PDF1.33 MB25. Februar 2021

• EASA 2020-0278 - AIRWORTHINESS LIMITATIONS SECTION/AMEND. - SUPERSEDED BY EASA 2025-0281

  EASA 2020-0278

  PC-6 ALS DOC. 02334R10 - 30.10.2020
  PC-6 AMM Doc. 01975R30 - 30.10.2020
  PC-6 AMM Doc. 01975R30 (IAC AR) - 30.10.2020

• EASA 2020-0120 - AIRWORTHINESS LIMITATIONS SECTION/AMEND. - SUPERSEDED BY EASA 2020-0278

  EASA 2020-0120

  PC-6 ALS Doc. 02334R9 - 06.03.2020
  PC-6 AMM Doc. 01975R29 - 28.02.2020
  PC-6 AMM Doc. 01975R29 (IAC AR) - 28.02.2020

• EASA 2018-0285 - AIRWORTHINESS LIMITATIONS SECTION/AMEND. - SUPERSEDED BY EASA 2020-0120

  EASA 2018-0285

  PC-6 ALS Doc. 02334R8 - 21.11.2018
  PC-6 AMM Doc. 01975R27 - 21.11.2018
  PC-6 AMM Doc. 01975R27 (IAC AR) - 21.11.2018

• EASA 2018-0235 - FLAP ACTUATOR-PUSHROD ASSEMBLY TAPER PINS/INSP.

  EASA 2018-0235

  • PC-6 SB 27-005

    PDF360.99 kB2. Juli 2018

• EASA 2018-0222 - RUDDER SHAFT ASSEMBLY RIVET CONFIGURATION/INSP.

  EASA 2018-0222

  • PC-6 SB 27-006

    PDF244.38 kB2. Juli 2018

  • PC-6 SB 27-006R1

    PDF245.99 kB4. September 2018

• EASA 2018-0217 - HORIZONTAL STABILIZER HINGE BRACKET ASSEMBL-FRONT SPAR ATTACHMENT

  EASA 2018-0217

  • PC-6 SB 55-004

    PDF631.37 kB2. Juli 2018

• EASA 2016-0202-E - REAR FUSELAGE STABILIZER TRIM ATTACHMENT COMPONENTS/INSP.

  EASA 2016-0202-E

  • PC-6 SB 53-003R1

    PDF306.74 kB4. Oktober 2016

• EASA 2016-0183 - AILERON MASS-BALANCE COUNTERWEIGHT ATTACHMENT/INSP.

  EASA 2016-0183

  • PC-6 SB 57-006

    PDF117.66 kB13. Mai 2016

• EASA 2014-0181 - AIRWORTHINESS LIMITATIONS SECTION/AMEND. - SUPERSEDED BY EASA 2018-0285

  EASA 2014-0181

  PC-6 ALS Doc. 02334R4 - 31.05.2014
  PC-6 AMM Doc. 01975R19 - 31.05.2014

• EASA 2013-0115-E - RIVETED STRUCTURAL PARTS/INSP;REPAIR

  EASA 2013-0115-E

  • PC-6 TM-06-000004

    PDF804.23 kB16. Mai 2013

• EASA 2012-0268 - AIRWORTHINESS LIMITATIONS SECTION/AMEND. - SUPERSEDED BY EASA 2014-0181

  EASA 2012-0268

  PC-6 ALS Doc. 02334R3 - 31.07.2012
  PC-6 AMM Doc. 01975R16 - 31.07.2012

• EASA 2011-0230 - ELEVATOR & RUDDER HINGE BOLT LOCKING/MODIF. - SUPERSEDED BY EASA 2021-0098

  EASA 2011-0230

  • PC-6 SB 55-001R1

    PDF132.99 kB25. November 2011

• EASA 2010-0176 - AIRWORTHINESS LIMITATIONS SECTION/IMPLEMENT. - SUPERSEDED BY EASA 2012-0268

  EASA 2010-0176

  PC-6 ALS Doc. 02334R1 - 14.05.2010
  PC-6 AMM Doc. 01975R12 - 14.05.2010

• EASA 2008-0171 - MOVEMENT OF BRAKE PEDALS/CHECK

  EASA 2008-0171

  • PC-6 SB 32-002R2

    PDF672.05 kB29. April 2008

• EASA 2008-0164 - MOVEMENT OF BRAKE PEDALS/CHECK - SUPERSEDED BY EASA 2008-0171

  EASA 2008-0164

  • PC-6 SB 32-002R2

    PDF672.05 kB29. April 2008

• HB-2008-242 - FLAP OPERATING MECHANISM-LEAF SPRINGS/REPET.INSP.

  HB-2008-242

  • PC-6 SB 27-002

    PDF214.98 kB2. Juli 2008

  • PC-6 SB 27-003

    PDF161.42 kB2. Juli 2008

• EASA 2008-0083 - FUSELAGE-SELF-LOCKING STOP NUTS/REPLMNT.

  EASA 2008-0083

  • PC-6 SB 53-002R2

    PDF566.39 kB24. September 2007

• EASA 2008-0070 - TAIL-WHEEL - LOCKING PLATE ATTACHMENT SCREW/REPLMNT.

  EASA 2008-0070

  • PC-6 SB 32-001

    PDF229.31 kB8. August 2006

• EASA 2007-0241R4 - UPPER WING STRUT FITTING & SPHERICAL BEARING/INSP. - SUPERSEDED BY EASA 2025-0281

  EASA 2007-0241R4

  • PC-6 SB 57-005R2

    PDF840.21 kB19. Mai 2008

• EASA 2007-0114 - UPPER WING STRUT FITTING & SPHERICAL BEARING/INSP. - SUPERSEDED BY EASA 2007-0241

  EASA 2007-0114

  • PC-6 SB 57-004

    PDF725.49 kB16. April 2007

• HB-2006-400 - WING STRUT FITTING/INSP. - SUPERSEDED BY EASA 2007-0241

  HB-2006-400

  • PC-6 SB 57-003R1

    PDF644.94 kB18. Juli 2007

• HB-2005-289 - APPLICABILITY OF ISSUED ADS/IMPLEMENT.

  HB-2005-289

  N/A

• HB-2005-263 - STABILIZER-TRIM ATTACHMENT COMPONENTS/INSP.

  HB-2005-263

  • PC-6 SB 53-001R1

    PDF502.44 kB1. Juni 2005

• HB-2005-080 - STABILIZER-TRIM ATTACHMENT COMPONENTS/INSP. - SUPERSEDED BY HB-2005-263

  HB-2005-080

  • PC-6 SB 53-001

    PDF474.64 kB16. Februar 2005

• HB-2003-092 - INTEGRAL FUEL TANK RIB ASSEMBLIES/INSP;REPAIR

  HB-2003-092

  • PC-6 SB 118

    PDF217.54 kB1. Dezember 1972

  • PC-6 SB 57-002

    PDF91.37 kB27. November 2002

• HB-2002-642 - AILERON CONTROL SYSTEM-BELLCRANK ASSEMBLIES/INSP;REPLMNT.

  HB-2002-642

  • PC-6 SB 27-001

    PDF266.28 kB5. Juni 2002

• HB-2002-314 - STABILIZER TRIM BEFORE TAKE OFF/PLACARD INSTALL;AFM REV.

  HB-2002-314

  • PC-6 TR-TRIM1

    TR-TRIM1

    PDF93.66 kB26. August 1999

  • PC-6 TR-TRIM3

    PDF87.97 kB14. Juni 2002

• HB-2002-134 - HORIZONTAL STABILIZER-TRIM WARNING SYSTEM/INSTALL.

  HB-2002-134

  • PC-6 SB 180R1

    PDF919.33 kB27. September 2001

• HB-2002-001 - MASS BALANCE WEIGHTS & FLETTNER TABS CONFIGURATION/IDENT.

  HB-2002-001

  • PC-6 SB 57-001

    PDF64.78 kB20. Dezember 2001

  • PC-6 SB 62B

    PDF145.73 kB1. Mai 1967

• HB-2000-336 - FUEL RETURN LINE CHECK-VALVE LOCATION/INSP.

  HB-2000-336

  PC-6 SB 179
  PC-6 SB 135

• HB-2000-041 - FUEL PIPE INSTALLATION IN THE FUSELAGE/MODIF.

  HB-2000-041

  PC-6 SB 177

• HB-99-507 - HORIZONTAL STABILIZER TRIM ACTUATOR/INSP.

  HB-99-507

  PC-6 SB 178

• HB-95-451 - COLLECTOR TANK VENT SYSTEM/AFM TEMP.REV;MODIF.

  HB-95-451

  PC-6 SB 171

• HB-94-087R1 - REAR FUSELAGE-BULKHEAD 12 & 13/REINFORCEMENT

  HB-94-087R1

  PC-6 SB 166R1

• HB-94-086 - HORIZONTAL STABILIZER HINGE BRACKET/REPET.INSP.

  HB-94-086

  PC-6 SB 165

• HB-89-301 - RUDDER PEDAL SUPPORTS/REPET.INSP.

  HB-89-301

  PC-6 SB A-162

• HB-86-042 - ELECTRICAL TRIM ACTUATOR ATTACHMENT BRACKET/INSP. - SUPERSEDED BY HB-2005-263

  HB-86-042

  PC-6 SB 147

• HB-84-182 - HORIZONTAL STABLIZER/INSP.

  HB-84-182

  PC-6 SB 144

• HB-84-181 - HORIZONTAL STABILIZER-GUSSET PLATES/REPLMNT.

  HB-84-181

  PC-6 SB 143

• HB-84-180 - VERTICAL STABILIZER-GUSSET PLATES/REPLMNT.

  HB-84-180

  PC-6 SB 142

• HB-84-030 - FLAP ACTUATOR BRACKETS/INSP;REPLMNT.

  HB-84-030

  PC-6 SB 140R1

• HB-84-023 - AILERON & FLAP MOUNT ATTACHMENT FITTINGS/INSP.

  HB-84-023

  PC-6 SB 138R3

• HB-84-007 - TAIL WHEEL GUARD/INSTALL.

  HB-84-007

  PC-6 SB 141R2

• HB-84-006 - FLAP ACTUATOR BRACKETS/INSP;REPLMNT. - SUPERSEDED BY HB-84-030

  HB-84-006

  PC-6 SB 140

• HB-84-005 - FLAP MOUNTING BRACKETS/INSP;REPLMNT.

  HB-84-005

  PC-6 SB 139R1

• HB-83-018 - AILERON/FLAP MOUNT ATTACHMENT FITTINGS/REPLMT. - SUPERSEDED BY HB-84-023

  HB-83-018

  PC-6 SB 138

• HB-83-017 - AILERON-,ELEVATOR,-RUDDER GUST LOCKS/MOD;REPLMNT.

  HB-83-017

  PC-6 SB 137

• TM-L Nr.:80-627-6 - AD SUMMARY PRE 1983 TM-L NR.: 80.627-6

  TM-L Nr.: 80.627-6

ADs pre 1983:

Airworthiness Directives issued prior to 1983 are not published as individual issues. However you may download (7.38 MB) the PC-6 AD-Summary TM-L Nr.: 80.627-6 with all PC-6 ADs issued prior to 31 December 1982 in the above mentioned list.