# Pilatus PC-6 - Type: Aircraft model (FAA registry) - Registry code: 7090102 - Manufacturer (registry): PILATUS - Model: PC-6 - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 · Reciprocating - Seats: 8 - Weight class: Up to 12,499 lb - Cruise speed: 102 mph - Certification: Type certificated - Data sheet: [TCDS 7A15](https://openairdocs.org/tcds/7A15) (OpenAirDocs) - Holder: Pilatus Aircraft Ltd. - Registered aircraft: 1 - Page: https://openairdocs.org/model/pilatus-pc-6 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022 - [AD 2021-24-22](https://openairdocs.org/ad/2021-24-22): Flight Control System, Aileron Control System, Rudder Control System, Elevator Control System · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Jan 25, 2022 - [AD 2021-11-08](https://openairdocs.org/ad/2021-11-08): Time Limits/Maintenance Checks · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Jul 12, 2021 - [AD 2020-16-02](https://openairdocs.org/ad/2020-16-02): Stabilizers · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Sep 9, 2020 - [AD 2020-11-06](https://openairdocs.org/ad/2020-11-06): Flight Controls · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Jun 30, 2020 - [AD 2019-10-07](https://openairdocs.org/ad/2019-10-07): Stabilizers · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Jul 10, 2019 - [AD 2017-04-03](https://openairdocs.org/ad/2017-04-03): Wings · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Apr 7, 2017 - [AD 2016-22-12](https://openairdocs.org/ad/2016-22-12): Fuselage · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Nov 4, 2016 - [AD 2009-18-03 R1](https://openairdocs.org/ad/2009-18-03-R1): Wings · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Feb 16, 2011 - [AD 2008-23-03](https://openairdocs.org/ad/2008-23-03): Brake pedals · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Dec 11, 2008 - [AD 2008-16-19](https://openairdocs.org/ad/2008-16-19): Self-locking stop nuts · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Sep 17, 2008 - [AD 2008-16-03](https://openairdocs.org/ad/2008-16-03): Leaf springs · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Aug 11, 2008 - [AD 2008-13-18](https://openairdocs.org/ad/2008-13-18): Tail landing gear · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Jul 30, 2008 - [AD 2007-26-11](https://openairdocs.org/ad/2007-26-11): High-pressure oxygen cylinder · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 45 more. Effective Jan 28, 2008 - [AD 2006-15-03](https://openairdocs.org/ad/2006-15-03): Integral fuel tank wing ribs · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Aug 23, 2006 - [AD 2006-15-02](https://openairdocs.org/ad/2006-15-02): Aileron control bellcrank assemblies · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Aug 23, 2006 - [AD 2006-13-12](https://openairdocs.org/ad/2006-13-12): Fuel starvation during maximum climb · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Aug 7, 2006 - [AD 2006-13-11](https://openairdocs.org/ad/2006-13-11): Aileron assembly · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Aug 7, 2006 - [AD 68-17-03 R1](https://openairdocs.org/ad/68-17-03-R1): Rudder end rib · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Aug 3, 2006 - [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005 - [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005 - [AD 2001-02-04](https://openairdocs.org/ad/2001-02-04): Stabilizer Trim Actuator · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Mar 13, 2001 - [AD 96-22-13](https://openairdocs.org/ad/96-22-13): Hinge Brackets On Horizontal Stabilizer · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Dec 27, 1996 - [AD 90-19-01](https://openairdocs.org/ad/90-19-01): Rudder Pedal Support · Pilatus PC-6, PC-6-H1, PC-6-H2 and 11 more. Effective Oct 15, 1990 - [AD 85-16-09](https://openairdocs.org/ad/85-16-09): Vertical/Horizontal Stabilizer · Pilatus PC-6, PC-6-H1, PC-6-H2 and 11 more. Effective Aug 31, 1985 - [AD 77-20-06](https://openairdocs.org/ad/77-20-06): Wing Strut Corrosion · Pilatus PC-6, PC-6-H1, PC-6-H2 and 11 more. Effective Nov 3, 1977 - [AD 77-13-06](https://openairdocs.org/ad/77-13-06): Landing Flaps · Pilatus PC-6, PC-6-H1, PC-6-H2 and 11 more. Effective Jul 25, 1977 - [AD 76-01-09](https://openairdocs.org/ad/76-01-09): Elevator Attach Brackets · Pilatus PC-6, PC-6-H1, PC-6-H2 and 11 more. Effective Feb 6, 1976 - [AD 75-27-07](https://openairdocs.org/ad/75-27-07): Rudder Bars · Pilatus PC-6, PC-6-H1, PC-6-H2 and 11 more. Effective Jan 21, 1976 - [AD 75-27-06](https://openairdocs.org/ad/75-27-06): Fuel Leak Fittings · Pilatus PC-6, PC-6-H1, PC-6-H2 and 11 more. Effective Jan 19, 1976 - [AD 69-20-01](https://openairdocs.org/ad/69-20-01): Rudder Trim Control Cable · Pilatus PC-6, PC-6-H1, PC-6-H2 and 9 more. Effective Oct 27, 1969 - [AD 69-19-01](https://openairdocs.org/ad/69-19-01): Pivot Bolt Rotation · Pilatus PC-6, PC-6-H1, PC-6-H2 and 9 more. Effective Sep 20, 1969 - [AD 69-07-02](https://openairdocs.org/ad/69-07-02): Aileron Balance Unit · Pilatus PC-6, PC-6-H1, PC-6-H2 and 9 more. Effective Apr 1, 1969 - [AD 69-04-04](https://openairdocs.org/ad/69-04-04): Aileron Balance Bolt · Pilatus PC-6, PC-6-H1, PC-6-H2 and 9 more. Effective Feb 14, 1969 - [AD 68-10-06](https://openairdocs.org/ad/68-10-06): Horizontal Stabilizer · Pilatus PC-6, PC-6-H1, PC-6-H2 and 9 more. Effective Jun 10, 1968 - [AD 67-32-04](https://openairdocs.org/ad/67-32-04): Stabilizer Cable Trim Control Clamps · Pilatus PC-6, PC-6-H1, PC-6-H2 and 9 more. Effective Dec 17, 1967 - [AD 67-21-02](https://openairdocs.org/ad/67-21-02): Elevator Attachment Bracket · Pilatus PC-6, PC-6-H1, PC-6-H2 and 9 more. Effective Aug 13, 1967 - [AD 67-13-03](https://openairdocs.org/ad/67-13-03): Rudder Control Lever Rivets · Pilatus PC-6, PC-6-H1, PC-6-H2 and 6 more. Effective May 4, 1967 - [AD 67-12-05](https://openairdocs.org/ad/67-12-05): Pulley Fairleads · Pilatus PC-6, PC-6-H1, PC-6-H2 and 6 more. Effective May 4, 1967 - [AD 66-28-05](https://openairdocs.org/ad/66-28-05): Rudder Pedal Support · Pilatus PC-6, PC-6-H1, PC-6-H2 and 6 more. Effective Nov 19, 1966 - [AD 71-23-01](https://openairdocs.org/ad/71-23-01): Safety of Aileron Cable Turnbuckles · Pilatus PC-6, PC-6-H1, PC-6-H2 and 9 more - [AD 66-01-03](https://openairdocs.org/ad/66-01-03): Fuel Valve · Pilatus PC-6, PC-6-H1, PC-6-H2 and 6 more Historical (superseded or no longer in force): - [AD 2014-25-04](https://openairdocs.org/ad/2014-25-04) (historical): Time Limits · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Jan 16, 2015 - [AD 2013-11-08](https://openairdocs.org/ad/2013-11-08) (historical): Time Limits · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Jul 29, 2013 - [AD 2012-06-16](https://openairdocs.org/ad/2012-06-16) (historical): Stabilizer · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective May 4, 2012 - [AD 2011-01-14](https://openairdocs.org/ad/2011-01-14) (historical): Time Limits · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Mar 8, 2011 - [AD 2009-18-03](https://openairdocs.org/ad/2009-18-03) (historical): Wings · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Oct 1, 2009 - [AD 2007-19-14](https://openairdocs.org/ad/2007-19-14) (historical): Upper wing strut fittings · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Sep 26, 2007 - [AD 2007-15-09](https://openairdocs.org/ad/2007-15-09) (historical): Wing strut fittings · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Sep 4, 2007 - [AD 2007-03-08](https://openairdocs.org/ad/2007-03-08) (historical): Bottom skin of hte wing · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Mar 8, 2007 - [AD 2005-17-01](https://openairdocs.org/ad/2005-17-01) (historical): Stabilizer-trim attachment and structural components · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Sep 29, 2005 - [AD 2003-13-04](https://openairdocs.org/ad/2003-13-04) (historical): Integral Fuel Tank Wing Ribs · Pilatus PC-6. Effective Aug 15, 2003 - [AD 2003-09-01](https://openairdocs.org/ad/2003-09-01) (historical): Aileron Control Bellcrank Assemblies · Pilatus PC-6. Effective Jun 17, 2003 - [AD 2002-21-08](https://openairdocs.org/ad/2002-21-08) (historical): Aileron assembly · Pilatus PC-6. Effective Dec 6, 2002 - [AD 98-12-01](https://openairdocs.org/ad/98-12-01) (historical): Fuel Venting System · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Jul 13, 1998 - [AD 68-17-03](https://openairdocs.org/ad/68-17-03) (historical): Cracks in Rudder End Rib · Pilatus PC-6, PC-6-H1, PC-6-H2 and 12 more. Effective Aug 19, 1968 ## Information bulletins (advisory) (7) - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 - [SAIB SW-07-13](https://openairdocs.org/saib/SW-07-13): Oxygen Reserve Cylinder. Issued Dec 11, 2006 - [SAIB CE-02-37R1](https://openairdocs.org/saib/CE-02-37R1): . Issued Feb 28, 2006 - [SAIB CE-02-29R1](https://openairdocs.org/saib/CE-02-29R1): . Issued Feb 28, 2006 - [SAIB CE-02-37](https://openairdocs.org/saib/CE-02-37) (historical): . Issued Jul 9, 2002 - [SAIB CE-02-29](https://openairdocs.org/saib/CE-02-29) (historical): . Issued May 30, 2002 - [SAIB ACE-96-08](https://openairdocs.org/saib/ACE-96-08): . Issued Nov 8, 1996 ## Registered aircraft (1) - [N4795P](https://openairdocs.org/aircraft/N4795P): [Miair Inc](https://openairdocs.org/faa-owner/MIAIR%20INC), [Lewes, DE](https://openairdocs.org/faa-place/DE/Lewes), S/N 341 ## NTSB investigations (5) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB OAK72DJY06](https://openairdocs.org/ntsb/OAK72DJY06), Apr 24, 1972: Pilatus PC6CH2 (N391R), Nyot Mo, Laos, destroyed, 4 fatal - [NTSB OAK72DJY18](https://openairdocs.org/ntsb/OAK72DJY18), Mar 21, 1972: Pilatus PC6-H2 (N391R), Song Lai, Laos, substantial damage - [NTSB OAK70O0002](https://openairdocs.org/ntsb/OAK70O0002), Dec 31, 1969: Pilatus PC-6 (N391R), Saigon, VM, substantial damage - [NTSB ANC70A0013](https://openairdocs.org/ntsb/ANC70A0013), Aug 12, 1969: Pilatus PC-6H2 (N2853T), Chevak, AK, substantial damage - [NTSB OAK69O0003](https://openairdocs.org/ntsb/OAK69O0003), May 9, 1968: Pilatus PC-6C (N357F), Phu Sang Lao, Laos, substantial damage ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (9) As reported by operators and repair stations, by the model named in the report. - [SDR EVGR202610220001](https://openairdocs.org/sdr/EVGR202610220001), Sep 30, 2026: RUDDER BAR. CRACKED. A MECHANIC WAS COMPLETING OUR COMPANY REQUIRED FINAL INSPECTION PRIOR TO RELEASING THE AIRCRAFT BACK TO SERVICE. ONE OF THOSE INSPECTION ITEMS, WAS TO CHECK THE - [SDR EVGR2024012300001](https://openairdocs.org/sdr/EVGR2024012300001), Jan 17, 2024: JETTISON HANDLE. BACKED OUT. THE AIRCRAFT HAD LANDED AND AS THE PILOTS BROUGHT THE POWER LEVER INTO BETA/REVERSE, THE LEFT SIDE PILOT DOOR FELL OFF. IT FELL FORWARD OVER THE MLG STRUT. THE - [SDR 2023FA0000660](https://openairdocs.org/sdr/2023FA0000660), Oct 23, 2023: UNKNOWN. UNKNOWN. TCDS 7A15, PILATUS ENGINE BUILD SPEC FOR PWC IS 877 & 624. THIS REQUIRES A FINE ENGINE INLET SCREEN, DUE TO NO INERTIA PARTICAL SEPARATOR INSTALLED ON THE ENGIN - [SDR CA071016018](https://openairdocs.org/sdr/CA071016018), Sep 27, 2007: TURBINE BLADES. FRACTURED. (CAN) DURING AIRCRAFT STALL RECOVERY TRAINING, THE ENGINE FLAMED OUT. SUBSEQUENT RE-LIGHT ATTEMPTS WERE UNSUCCESSFUL. INSPECTION REVEALED FRACTURED COMPRESSOR T - [SDR CA050824017](https://openairdocs.org/sdr/CA050824017), Aug 19, 2005: ENGINE. LACK OF LUBE. (CAN) IN CLIMB, ENGINE TORQUE WAS REPORTED TO FLUCTUATE FOLLOWED BY WHITE SMOKE EMANATING FROM THE EXHAUST. THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPE - [SDR CA050824008](https://openairdocs.org/sdr/CA050824008), Aug 6, 2005: BLADES. DAMAGED. (CAN) DURING CLIMB, THE ENGINE EXHIBITED A SQUEALING NOISE ACCOMPANIED BY AN UNCOMMANDED POWER REDUCTION. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIV - [SDR CA050329007](https://openairdocs.org/sdr/CA050329007), Mar 13, 2005: DRIVE ASSY. MALFUNCTIONED. (CAN) FRENCH AUTHORITIES HAVE REPORTED AN INFLT SHUTDOWN WITH INDICATIONS OF A FUEL PUMP DRIVE MALFUNCTION. - [SDR AUS20010407](https://openairdocs.org/sdr/AUS20010407), Apr 30, 2001: LINE. CONTAMINATED. (AUS) ENGINE FAILED DUE TO LACK OF FUEL. INVESTIGATION FOUND AIR IN THE FUEL LINE BETWEEN THE FUEL HEATER AND THE FCU. SUSPECT CAUSED BYPOOR VENTING OF THE FUEL - [SDR AU010223](https://openairdocs.org/sdr/AU010223), Mar 4, 2001: GOVERNOR. FAILED. (AUS) PROPELLER REVERSE GOVERNOR IDLER GEAR BEARING COLLAPSED. METALCONTAMINATION OF ENGINE. ## STCs that may be installed (OpenAirDocs) (88, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc - [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc - [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc - [STC SA307EA](https://openairdocs.org/stc/SA307EA): Removal of either or both of the right hand cabin door and/or opening of the fuselage bottom hatch in flight. PC6-AU23 Spares LLC - [STC SA433EA](https://openairdocs.org/stc/SA433EA): Installation of dual brake valves. PC6-AU23 Spares LLC - [STC SA465EA](https://openairdocs.org/stc/SA465EA): Installation of UAT-1 Transponder, MBT-R Marker Beacon, KN-60 DME, KX-160 and KX-160-1 Nav/Comm, KR-80ADF, Headset Microphone and Speaker. PC6-AU23 Spares LLC - [STC SA743EA](https://openairdocs.org/stc/SA743EA): Installation of a sliding door on the left side of fuselage. PC6-AU23 Spares LLC - [STC SA830EA](https://openairdocs.org/stc/SA830EA): Installation of fiberglass protective boot on leading edge of horizontal stabilizer. PC6-AU23 Spares LLC - [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine - [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc - [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc - [STC SA02254AK](https://openairdocs.org/stc/SA02254AK): Installation of "Single Screen", "2 or 3 Screen", "Dual Screen", or "4 or 6 screen". Genesys Aerosystems Inc - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA01015SE](https://openairdocs.org/stc/SA01015SE): Installation of eligible Alaska Bushwheel, Inc. wheels and TSO-C62d tires. ABI LLC - [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King) - [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc - [STC SA04403CH](https://openairdocs.org/stc/SA04403CH): EMS conversion in accordance with Spectrum Aeromed Master Drawing List 6056DL, Revision 1, dated March 14, 2019, or later FAA approved revisions. Spectrum Aeromed LLC dba Spectrum Aeromed - [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies - [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine - [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation - [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine - [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC - [STC SA04364AT](https://openairdocs.org/stc/SA04364AT): Introduction of alternative cargo tie down fittings for Pilatus PC-6 series aircraft. JAARS Inc - [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA00352BO PAGE 2](https://openairdocs.org/stc/SA00352BO%20PAGE%202): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA02119SE PAGE 2](https://openairdocs.org/stc/SA02119SE%20PAGE%202): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc - [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics - [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA02442AK PAGE 2](https://openairdocs.org/stc/SA02442AK%20PAGE%202): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc - [STC SA02402SE PAGE 2](https://openairdocs.org/stc/SA02402SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc - [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc - [STC SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000. Avidyne Corporation All 88: https://openairdocs.org/model/pilatus-pc-6/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Pilatus PC-6 PORTER](https://openairdocs.org/model/pilatus-pc-6-porter): 0 registered aircraft, registry code 7090112 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.