# Pilatus PC-6/B2-H2 - Type: Aircraft model (FAA registry) - Registry code: 7090213 - Manufacturer (registry): PILATUS - Model: PC-6/B2-H2 - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 · Turbo-prop - Seats: 11 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS 7A15](https://openairdocs.org/tcds/7A15) (OpenAirDocs) - Holder: Pilatus Aircraft Ltd. - Registered aircraft: 8 - Page: https://openairdocs.org/model/pilatus-pc-6-b2-h2 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 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 2005-01-19](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 97-22-08](https://openairdocs.org/ad/97-22-08): Airplane Flight Manual (AFM) - Limitations Section - Power Levers · Pilatus PC-12, PC-6/B1-H2, PC-6/B2-H2 and 1 more. Effective Dec 5, 1997 - [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 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 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) (1) - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 ## Registered aircraft (8) - [N108MA](https://openairdocs.org/aircraft/N108MA): [Grizzly Air Service Inc](https://openairdocs.org/faa-owner/GRIZZLY%20AIR%20SERVICE%20INC), [Paris, TX](https://openairdocs.org/faa-place/TX/Paris), S/N 792 - [N156PC](https://openairdocs.org/aircraft/N156PC): [Idaho Skyworks LLC](https://openairdocs.org/faa-owner/IDAHO%20SKYWORKS%20LLC), [Walnut Creek, CA](https://openairdocs.org/faa-place/CA/Walnut%20Creek), built 1976, S/N 777 - [N19TX](https://openairdocs.org/aircraft/N19TX): [Perry James](https://openairdocs.org/faa-owner/PERRY%20JAMES), [Monroe, WA](https://openairdocs.org/faa-place/WA/Monroe), S/N 684 - [N22MA](https://openairdocs.org/aircraft/N22MA): [Miair Inc](https://openairdocs.org/faa-owner/MIAIR%20INC), [Lewes, DE](https://openairdocs.org/faa-place/DE/Lewes), S/N 785 - [N776PC](https://openairdocs.org/aircraft/N776PC): [Technical Applications & Consulting LLC](https://openairdocs.org/faa-owner/TECHNICAL%20APPLICATIONS%20%26%20CONSULTING%20LLC), [Topeka, KS](https://openairdocs.org/faa-place/KS/Topeka), S/N 775 - [N80LH](https://openairdocs.org/aircraft/N80LH): [Lochsa Aviation LLC](https://openairdocs.org/faa-owner/LOCHSA%20AVIATION%20LLC), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), built 1978, S/N 801 - [N8171K](https://openairdocs.org/aircraft/N8171K): [Perry Kathryn C](https://openairdocs.org/faa-owner/PERRY%20KATHRYN%20C), [Sultan, WA](https://openairdocs.org/faa-place/WA/Sultan), S/N 750 - [N856FA](https://openairdocs.org/aircraft/N856FA): [Plane Fun Inc Tr Trustee](https://openairdocs.org/faa-owner/PLANE%20FUN%20INC%20TR%20TRUSTEE), [Snellville, GA](https://openairdocs.org/faa-place/GA/Snellville), built 1986, S/N 856 ## NTSB investigations (2) 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 MIA06LA001](https://openairdocs.org/ntsb/MIA06LA001), Oct 3, 2005: Pilatus PC-6/B2-H2 (N7895J), Deland, FL, substantial damage. Probable cause: The pilot's incorrect setting of the stabilizer trim and his failure to maintain adequate airspeed during takeoff initial climb, which resulted in a stall. A factor contributing to the accident was… - [NTSB FTW98LA035](https://openairdocs.org/ntsb/FTW98LA035), Oct 28, 1997: Pilatus PC-6 (N19TX), Lexington, TX, substantial damage. Probable cause: the pilot's selection of an unsuitable landing area. A factor relating to the accident was: the uneven terrain (with swales) at the edge of the landing area. ## FAA accident and incident reports (3) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20141110021669I](https://openairdocs.org/incident/20141110021669I), Nov 10, 2014: Pilatus PC-6/B2-H2 (N19TX), Lebanon, ME, Substantial damage. Pilot was flying downwind and said he experienced a temporary loss of power. He immediately turned the aircraft to land in the clearing next to the runway. He… - [Accident 20051003024729A](https://openairdocs.org/incident/20051003024729A), Oct 3, 2005: Pilats PC6B2H2 (N7895J), Deland, FL, Substantial damage. (-23) According to witnesses, at approximately 1445 EDT on October 3, 2005, N7895J, a Pilatus PC-6 "porter" tailwheel turboprop skydiving aircraft piloted by… - [Accident 19971028037039A](https://openairdocs.org/incident/19971028037039A), Oct 28, 1997: Pilats PC6B1H2 (N19TX), Lexington, TX, Substantial damage. Landed near edge of new strip. Encountered a swale. Right main folded due unknown weakness. Wing fuselage damage. (.23) the aircraft hit a small rut in the… ## Service difficulty reports (3) As reported by operators and repair stations, by the model named in the report. - [SDR CA140424009](https://openairdocs.org/sdr/CA140424009), Apr 13, 2014: ENGINE. MALFUNCTIONED. (CAN) ON A PARACHUTIST MISSION, THE CLIMB TO FL140 WAS NORMAL, HOWEVER, AS THE PILOT WAS MAKING A LT TURN JUST BEFORE THE DROP ZONE, AN ODOR OF FUEL WAS NOTICED - [SDR AE1](https://openairdocs.org/sdr/AE1), Dec 10, 2004: STRUCTURE. FAILED. FAILURE OF ELEVATOR ATTACH POINT AND OR HARDWARE. ACTUAL CAUSE IS UNKNOWN BECAUSE THE ELEVATOR HAS NOT BEEN LOCATED FOR RECOVERY. - [SDR 95ZZZX6074](https://openairdocs.org/sdr/95ZZZX6074), Sep 11, 1995: FORK LEG. WATER TRAPPED. FOUND 2-3 OUNCES OF WATER TRAPPED IN LANDING GEAR FORK LEG. APPLIED ONLY TO ACFT WITH PILATUS SB141, EQUIPPED FOR PARACHUTING (PARA DROP VERSION) OR OTHERWISE H ## STCs that may be installed (OpenAirDocs) (87, 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 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 SA1005EA](https://openairdocs.org/stc/SA1005EA): Installation of fuel collector tank - engine shutdown fuel discharge. PC6-AU23 Spares LLC - [STC SA1022EA](https://openairdocs.org/stc/SA1022EA): Installation of Aerosmith C-129-65 pilot's and co-pilot's seats and modified control sticks. PC6-AU23 Spares LLC - [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 SA397EA](https://openairdocs.org/stc/SA397EA): Installation of fuel collector tank vent line. 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 SA493EA](https://openairdocs.org/stc/SA493EA): Installation of Randolph Mfg. Co. Model 133 vacuum regulator. PC6-AU23 Spares LLC - [STC SA498EA](https://openairdocs.org/stc/SA498EA): Installation of Zep Aero oxygen system. PC6-AU23 Spares LLC - [STC SA526EA](https://openairdocs.org/stc/SA526EA): Installation of pilot's and co-pilot's shoulder harness. PC6-AU23 Spares LLC - [STC SA528EA](https://openairdocs.org/stc/SA528EA): Installation of KX-160 NAV/COM, 618M-1A VHF COM., T-10-R HF COMM, ARC Type 21A ADF headsets, microphones and speakers. 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 SA747EA](https://openairdocs.org/stc/SA747EA): Installation of two external fuel tanks of fifty gallons capacity each, mounted. 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 SA906EA](https://openairdocs.org/stc/SA906EA): Installation of elevator reinforcement. PC6-AU23 Spares LLC - [STC SA907EA](https://openairdocs.org/stc/SA907EA): Installation of outboard aileron reinforcement. PC6-AU23 Spares LLC - [STC SA908EA](https://openairdocs.org/stc/SA908EA): Installation of rudder reinforcement. PC6-AU23 Spares LLC - [STC SA909EA](https://openairdocs.org/stc/SA909EA): Installation of vertical stabilizer reinforcement. PC6-AU23 Spares LLC - [STC SA910EA](https://openairdocs.org/stc/SA910EA): Installation of horizontal/stabilizer reinforcement. PC6-AU23 Spares LLC - [STC SA911EA](https://openairdocs.org/stc/SA911EA): Installation of Bulkhead 12A reinforcement. PC6-AU23 Spares LLC - [STC SA945EA](https://openairdocs.org/stc/SA945EA): Installation of longitudinal out of trim warning system. PC6-AU23 Spares LLC - [STC SA986WE](https://openairdocs.org/stc/SA986WE): Removal of landing gear and installation of seaplane conversion. 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 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 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 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 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 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 SA02135SE](https://openairdocs.org/stc/SA02135SE): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data). Electronics International Inc - [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 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 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 All 87: https://openairdocs.org/model/pilatus-pc-6-b2-h2/stcs.md ## PMA parts (OpenAirDocs) (123, first 50) Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first. - [M23046-1090](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115802023520250403122904.0001): Fan Cover Assembly. Miraj Corporation · PMA PQ0870NE · Replaces 23046-1090 · Mar 24, 2025 - [RB17667ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194691205420220826132334.0001): Drive Coupling. Aircraft Component Design LLC · PMA PQ2138NE · Replaces RB17667 · Aug 23, 2022 - [01-0790906-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151251780020220706160153.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Jun 21, 2022 - [AG627000-13](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105209454020220809130915.0001): Gasket – Marker Beacon. Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · Modification part · May 10, 2022 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172518086820220809102545.0001): Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · Apr 18, 2022 - [AG844000-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152229284020220408135803.0001): Gasket – UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Feb 8, 2022 - [AG728000-52](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167607947920220408135724.0001): Gasket – Satcom Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jan 26, 2022 - [AG627000-23](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180626957320220408135702.0001): Gasket – Marker Beacon. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 15, 2021 - [AG627000-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188202971720220408140242.0001): Gasket – Marker Beacon Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021 - [AG358000-08](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132217000420220408135815.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021 - [ST-982 ST-982-1ST-982-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID323838505420211119122116.0001): Installation of S-TEC 01326 Digital Flight Control System (DFCS))Installation of S-TEC 01326 Digital Flight Control System (DFCS)Installation of S-TEC 01326 Digital Flight Control System (DFCS). S-TEC Corporation · PMA PQ0445SW · Modification part · May 19, 2021 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID866861241320210622142523.0001): AeroLEDs LLC · PMA PQ5259NM · Mar 11, 2021 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID283048585120210702175234.0001): Aspen Avionics · PMA PQ03868SW · Jan 20, 2021 - [AG358000-07](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190838665120210727195144.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 11, 2020 - [AG786000-01](https://drs.faa.gov/browse/excelExternalWindow/F240EB736CAF9B6F86258639004F7BE3.0001): Gasket - StormScope Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 8, 2020 - [AG867000-24](https://drs.faa.gov/browse/excelExternalWindow/AD6F1CD4CB9D7C2F8625863A005D9E2A.0001): Gasket - VOR Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 8, 2020 - [AG843000-79](https://drs.faa.gov/browse/excelExternalWindow/7C47B4B54B5941DF862586240047DC8E.0001): Gasket - UHF / AM / IFF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2020 - [AG477000-35](https://drs.faa.gov/browse/excelExternalWindow/CAA7A03C831CF5A78625861F004520E1.0001): Gasket - GPS ANTENNA. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 11, 2020 - [AG822000-09](https://drs.faa.gov/browse/excelExternalWindow/B363A74FB05068CA862586020044D52C.0001): Gasket - TCAS Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Oct 13, 2020 - [AG247000-05](https://drs.faa.gov/browse/excelExternalWindow/A8B3EE75D8E4BBD2862585E5006243CC.0001): Gasket - Security System Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Aug 24, 2020 - [AG843000-19](https://drs.faa.gov/browse/excelExternalWindow/6325AFC5586C8E34862585E500649009.0001): Gasket - VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Aug 24, 2020 - [L8535233](https://drs.faa.gov/browse/excelExternalWindow/EFC39C61E900ED30862586160054EC6E.0001): Oil Cooler Assy. Honeywell International Inc. Honeywell Aerospace · PMA PQ1222NM · Replaces 8535233 · Jul 26, 2020 - [9100-001-C](https://drs.faa.gov/browse/excelExternalWindow/DD343890DCD8BFDB86258569004013FB.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-D](https://drs.faa.gov/browse/excelExternalWindow/C7B6725B325949E98625856900401478.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9200-000-B](https://drs.faa.gov/browse/excelExternalWindow/BD58B0712CA0C6AA86258569004016AD.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-G](https://drs.faa.gov/browse/excelExternalWindow/ADE62C91D97E8B788625856900401557.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-E](https://drs.faa.gov/browse/excelExternalWindow/A37F050253EE808A86258569004014BA.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9200-000-A](https://drs.faa.gov/browse/excelExternalWindow/8E10EF4D973C1D6D8625856900401662.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-A](https://drs.faa.gov/browse/excelExternalWindow/62DC748A2B9B1D9386258569004012FD.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-F](https://drs.faa.gov/browse/excelExternalWindow/3746AAB4CC0D6883862585690040151B.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-B](https://drs.faa.gov/browse/excelExternalWindow/32446D71EB78157686258569004013B2.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-H](https://drs.faa.gov/browse/excelExternalWindow/1AEB415100FB45D8862585690040159F.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [01-0771833-20](https://drs.faa.gov/browse/excelExternalWindow/FFF505DF238D9E3E86258557004EB967.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019 - [01-0771833-25](https://drs.faa.gov/browse/excelExternalWindow/D17366A21258BFC186258557004EB9A2.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019 - [01-0771833-10](https://drs.faa.gov/browse/excelExternalWindow/D0F0E113B870DF1C86258557004EB8E0.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019 - [01-0771833-15](https://drs.faa.gov/browse/excelExternalWindow/CB6A5B42DF6A574686258557004EB925.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019 - [01-0790750-10](https://drs.faa.gov/browse/excelExternalWindow/8FBCEA35A3837D6386258557004EB9D7.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019 - [01-0790750-20](https://drs.faa.gov/browse/excelExternalWindow/5919E033D600DA3386258557004EBA0C.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019 - [MCG-1901](https://drs.faa.gov/browse/excelExternalWindow/8FF1F05D77C8510E862584740061230C.0001): Dampener Hub. Miraj Corporation · PMA PQ0870NE · Replaces 23032-1901 · Feb 24, 2019 - [M23032-2711](https://drs.faa.gov/browse/excelExternalWindow/4AF3A478C94705EA862582CF006DC0C8.0001): Dampener Plate. Miraj Corporation · PMA PQ0870NE · Replaces 23032-2711 · Jun 17, 2018 - [87-05208-001](https://drs.faa.gov/browse/excelExternalWindow/C4B8A8A2B2422B728625822E007853B6.0001): Assembly, Light, PAR 46 Landing. Astronics Luminescent Systems Inc · PMA PQ0786NE · Replaces 01-0790750-20 · Jan 23, 2018 - [SK1413](https://drs.faa.gov/browse/excelExternalWindow/4BBE2CFFF8FF4C6F862582D300747451.0001): Radome Boot. Skandia, Inc. · PMA PQ2665CE · Modification part · Dec 18, 2017 - [M2002-5HL](https://drs.faa.gov/browse/excelExternalWindow/238474E2270AA01686258228007537BE.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces Safran/Goodrich 23081-1850 30300-1380 · Dec 12, 2017 - [PC-6 001-20](https://drs.faa.gov/browse/excelExternalWindow/D08CD1ADBDD337F2862581B500746E6B.0001): Cargo Tie Down. JAARS Inc · PMA PQ4133CE · Modification part · Sep 23, 2017 - [87-05207-002](https://drs.faa.gov/browse/excelExternalWindow/4BE4BA39295AB01E862581760058C64D.0001): Assembly, Light, PAR 36 Taxi. Astronics Luminescent Systems Inc · PMA PQ0786NE · Replaces 01-0771833-25 · Aug 1, 2017 - [87-05207-001](https://drs.faa.gov/browse/excelExternalWindow/4ACD6BDF5990D9C7862581760058C571.0001): Assembly, Light, PAR 36 Landing. Astronics Luminescent Systems Inc · PMA PQ0786NE · Replaces 01-0771833-20 · Aug 1, 2017 - [R20696-1](https://drs.faa.gov/browse/excelExternalWindow/E555491D6AE1CE2A862580D600749E2D.0001): Bushing. Hutchinson Aerospace & Industry Inc · PMA PQ0524NM · Replaces R20696-1 · Feb 13, 2017 - [R20697-1](https://drs.faa.gov/browse/excelExternalWindow/E3D0AC8228127348862580D600749E30.0001): Bushing. Hutchinson Aerospace & Industry Inc · PMA PQ0524NM · Replaces R20697-1 · Feb 13, 2017 - [R20702-2](https://drs.faa.gov/browse/excelExternalWindow/B67AA76AA4E497BF862580D600749E33.0001): Gasket. Hutchinson Aerospace & Industry Inc · PMA PQ0524NM · Replaces R20702-2 · Feb 13, 2017 - [R20695-2](https://drs.faa.gov/browse/excelExternalWindow/6B0E240B915AC4D2862580D600749E2E.0001): Tube - Bumper. Hutchinson Aerospace & Industry Inc · PMA PQ0524NM · Replaces R20695-2 · Feb 13, 2017 All of them: https://openairdocs.org/model/pilatus-pc-6-b2-h2/pma.md --- 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.