ADs applicable to Swiss registred aeronautical products designed by
PILATUS AIRCRAFT Ltd.
Pertaining to Model: PC-6 Series
FOCA TC/TCDS: F 56-10
Last update: 09 April 2021
AD Reference |
Superseded by |
Subject |
SB Ref. |
---|---|---|---|
EASA 2021-0098 (PDF, 202 kB, 09.04.2021) | Aileron, Elevator and Rudder / Hinge Bolt Installation | 55-005 (PDF, 1 MB, 25.02.2021) | |
EASA 2020-0278 (PDF, 205 kB, 14.12.2020) | Airworthiness Limitations Section - Amendment | ALS Doc.02334R10 (PDF, 115 kB, 30.10.2020) AMM Rev.30 (PDF, 118 kB, 30.10.2020) AMM Rev.30 IAC (PDF, 124 kB, 30.10.2020) |
|
EASA 2020-0120 (PDF, 1 MB, 27.05.2020) | EASA 2020-0278 | Airworthiness Limitations Section - Amendment | ALS Doc.02334R9 (PDF, 292 kB, 06.03.2020) AMM Rev.29 (PDF, 404 kB, 28.02.2020) AMM Rev.29 IAC (PDF, 310 kB, 28.02.2020) |
EASA 2018-0285 (PDF, 1 MB, 20.12.2018) | EASA 2020-0120 | Airworthiness Limitations Section - Amendment | ALS Doc.02334R8 (PDF, 194 kB, 21.11.2018) AMM Rev.27 (PDF, 434 kB, 21.11.2018) |
EASA 2018-0235 (PDF, 494 kB, 05.11.2018) | Flap Actuator / Pushrod Assembly Taper Pins | 27-005 (PDF, 352 kB, 02.07.2018) | |
EASA 2018-0222 (PDF, 496 kB, 19.10.2018) | Rudder Shaft Assembly Rivet Configuration | 27-006 (PDF, 238 kB, 02.07.2018) 27-006R1 (PDF, 240 kB, 04.09.2018) |
|
EASA 2018-0217 (PDF, 496 kB, 10.10.2018) | Horizontal Stabilizer Hinge Bracket Assembly / Front Spar Attachment Area | 55-004 (PDF, 616 kB, 02.07.2018) | |
EASA 2016-0202-E (PDF, 390 kB, 07.10.2016) | Rear Fuselage Stabilizer-Trim Attachment Components | 53-003R1 (PDF, 299 kB, 04.10.2016) | |
EASA 2016-0183 (PDF, 314 kB, 13.09.2016) | Aileron Mass-Balance Counterweight Attachment | 57-006 (PDF, 114 kB, 13.05.2016) | |
EASA 2014-0181 (PDF, 743 kB, 31.07.2014) | EASA 2018-0285 |
Airworthiness Limitations Section - Amendment | AMM Rev.19 (PDF, 23 kB, 31.05.2014) ALS Doc. 02334 (PDF, 24 kB, 31.05.2014) |
EASA 2013-0115-E (PDF, 213 kB, 28.05.2013) | Riveted Structural Parts | TM-06-000004 (PDF, 785 kB, 16.05.2013) | |
EASA 2012-0268 (PDF, 506 kB, 20.12.2012) | EASA 2014-0181 |
Airworthiness Limitations Section - Amendment |
AMM Rev.16 (PDF, 79 kB, 31.07.2012) ALS Doc. 02334 (PDF, 843 kB, 28.02.2010) |
EASA 2011-0230 (PDF, 579 kB, 09.12.2011) | EASA 2021-0098 | Elevator and Rudder Hinge Bolt Locking |
55-001 Rev.1 (PDF, 129 kB, 25.11.2011) |
EASA 2012-0268 |
Airworthiness Limitations Section - Implementation |
AMM Rev.12 (PDF, 445 kB, 14.05.2010) ALS Doc. 02334 (PDF, 693 kB, 20.02.2010) |
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Wheels and Brakes - |
||
EASA 2008-0171 |
Wheels and Brakes - |
||
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Flap Operating Mechanism - |
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|
Fuselage - Self-locking Stop Nuts |
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LG Locking plate attachment screw |
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Wing Strut Fitting |
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EASA |
Upper Wing Strut Fitting |
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EASA 2007-0241 |
Wing Strut Fitting |
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Applicability of issued Airworthiness Directives |
N/A |
|
|
Stabilizer-Trim Attachment Components |
||
HB-2005-263 |
Stabilizer-Trim Attachment Components |
||
|
Integral Fuel-Tank Rib Assemblies |
57-002 (PDF, 89 kB, 27.11.2002) |
|
|
Bellcrank Assemblies – Bearing Housings |
||
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Stabilizer Trim Before Take Off |
||
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Horizontal Stabilizer – Trim Warning System |
||
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Aileron -Mass Balance Weights And Flettner Tabs - Configuration |
57-001 (PDF, 63 kB, 20.12.2001) |
|
|
Fuel Return Line Check-Valve Location |
179 & 135 |
|
|
Fuel Pipe Installation |
177 |
|
|
Horizontal Stabilizer Trim Actuator |
178 |
|
|
Collector Tank Vent System |
171 |
|
|
Rear Fuselage-Bulkhead 12&13 |
166R1 |
|
|
Horizontal Stabilizer Hinge Bracket |
165 |
|
|
Rudder Pedal Supports |
A-162 |
|
HB-2005-263 |
Electric Trim Actuator Bracket |
147 |
|
|
Horizontal Stabilizer |
144 |
|
|
Horizontal Stabilizer-Gusset Plates |
143 |
|
|
Vertical Stabilizer-Gusset Plates |
142 |
|
|
Flap Actuator Brackets |
140R1 |
|
|
Aileron/Flap Mount Attachment Fitting |
138R3 |
|
|
Tail Wheel Guard |
141R2 |
|
HB-84-030 |
Flap Actuator Brackets |
140 |
|
|
Flap Mounting Brackets |
139R1 |
|
HB-84-023 |
Aileron/Flap Mount Attachment Fittings |
138 |
|
|
Aileron-, Elevator-, Rudder Gust Locks |
137 |
|
|
AD Summary pre 1983 |
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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.