# Pilatus PC-6/B-H2

- Type: Aircraft model (FAA registry)
- Registry code: 7090210
- Manufacturer (registry): PILATUS
- Model: PC-6/B-H2
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Turbo-prop
- 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: 0
- Page: https://openairdocs.org/model/pilatus-pc-6-b-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 2005-18-20](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 69-05-05](https://openairdocs.org/ad/69-05-05): Power Lever Travel · Pilatus PC-6/B-H2 and PC-6/B1-H2. Effective Mar 12, 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 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

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

None registered with this model now.

## 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 ANC73FAG57](https://openairdocs.org/ntsb/ANC73FAG57), Nov 8, 1972: Pilatus PC6BH2 (N2854T), Anchorage, AK, substantial damage
- [NTSB ANC72AA010](https://openairdocs.org/ntsb/ANC72AA010), Aug 16, 1971: Pilatus PC6-H2 (N2854T), Akiak, AK, substantial damage
- [NTSB ANC68A0047](https://openairdocs.org/ntsb/ANC68A0047), May 17, 1968: Pilatus PC6-H2 (N2851T), Venetie, AK, substantial damage
- [NTSB ANC67A0041](https://openairdocs.org/ntsb/ANC67A0041), Oct 28, 1966: Pilatus PC6BH2 (N2854T), Kotzebue, AK, substantial damage
- [NTSB ANC66A0014](https://openairdocs.org/ntsb/ANC66A0014), Oct 1, 1965: Pilatus Por PC6BH2 (N2851T), Selawik, AK, substantial damage

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (3)

As reported by operators and repair stations, by the model named in the report.

- [SDR CA040730011](https://openairdocs.org/sdr/CA040730011), Jul 29, 2004: BEARING. LOOSE. (CAN) DURING 100 HR INSPECTION - LT IB AILERON CONTROL BELLCRANK WAS FOUND TO HAVE LOOSE FITTING BEARING. ALLOWING AILERON CONTROL ROD TO FLOAT UP AND DOWN, CON
- [SDR CA040730010](https://openairdocs.org/sdr/CA040730010), Jul 29, 2004: BEARING. LOOSE. (CAN) DURING 100 HR INSPECTION, RT AILERON OUTER PUSHROD WAS FOUND TO HAVE A LOOSE BEARING, ALLOWING ROD END TO FLOAT SIDEWAYS ON BEARING. BEARING REMOVED, ROD 
- [SDR AU971374](https://openairdocs.org/sdr/AU971374), Sep 24, 1997: BOLT. BROKEN. (AUS) COMPRESSOR TURBINE VANE BOLTS (3OFF) HAD THE BOLT HEADS SEPARATE AND BECOME TRAPPED BETWEEN THE VANE AND TURBINE DISC CAUSING DAMAGE TO THE DISC IN THE AR

## STCs that may be installed (OpenAirDocs) (102, 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 SA614EA](https://openairdocs.org/stc/SA614EA): Installation of UACL engine Model PT6A-27 with Hartzell propeller Model HC-B3TN-3D/T10178C(H) on aircraft configured with cockpit doors. PC6-AU23 Spares, LLC
- [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 SA747EA](https://openairdocs.org/stc/SA747EA): Installation of two external fuel tanks of fifty gallons capacity each, mounted. PC6-AU23 Spares LLC
- [STC SA753EA](https://openairdocs.org/stc/SA753EA): Installation of dual ARC 21A ADF's, and ARC 131B VHF's and one SA14RA HF avionics equipment. PC6-AU23 Spares LLC
- [STC SA755EA](https://openairdocs.org/stc/SA755EA): Installation of polyurethane Reticulated Foam in the aircraft's integral and collector fuel tanks in addition to check valves in the fuel lines between the integral tanks and the collector and sediment tanks. 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 SA937EA](https://openairdocs.org/stc/SA937EA): Cabin Floor, Special Installation - Structural Provisions. PC6-AU23 Spares LLC
- [STC SA938EA](https://openairdocs.org/stc/SA938EA): Wing Flap and Aileron Reinforcement. PC6-AU23 Spares LLC
- [STC SA939EA](https://openairdocs.org/stc/SA939EA): Substitution of AN Hardware in lieu of Metric Hardware. PC6-AU23 Spares LLC
- [STC SA940EA](https://openairdocs.org/stc/SA940EA): Left Wing Reinforcement. PC6-AU23 Spares LLC
- [STC SA941EA](https://openairdocs.org/stc/SA941EA): Wing Hard Point Modification. PC6-AU23 Spares LLC
- [STC SA945EA](https://openairdocs.org/stc/SA945EA): Installation of longitudinal out of trim warning system. PC6-AU23 Spares LLC
- [STC SA946EA](https://openairdocs.org/stc/SA946EA): Relocation of wing landing light between left wing rib stations 11 and 12 to left wing rib stations21 and 22. PC6-AU23 Spares LLC
- [STC SA961EA](https://openairdocs.org/stc/SA961EA): Installation of battery over- temperature 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

All 102: https://openairdocs.org/model/pilatus-pc-6-b-h2/stcs.md

## PMA parts (OpenAirDocs) (122, 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.

- [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
- [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
- [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
- [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
- [M05-374094](https://drs.faa.gov/browse/excelExternalWindow/04A248CF6B40096C862580E40064D09B.0001): Washer, Non Metallic. Miraj Corporation · PMA PQ0870NE · Replaces Safran/Goodrich 05-374094 · Mar 6, 2017
- [01-0771833-20](https://drs.faa.gov/browse/excelExternalWindow/C4A392C20DA3333A86257FCC006EBC03.0001): LED Landing Light. Whelen Engineering Co Inc · PMA PQ0610NE · Modification part · Apr 20, 2016
- [01-0771833-25](https://drs.faa.gov/browse/excelExternalWindow/618915409FDEC97186257FCC006EBC05.0001): LED Taxi Light. Whelen Engineering Co Inc · PMA PQ0610NE · Modification part · Apr 20, 2016
- [01-0771833-15](https://drs.faa.gov/browse/excelExternalWindow/466B93ACC46B636486257FCC006EBC01.0001): LED Taxi Light. Whelen Engineering Co Inc · PMA PQ0610NE · Modification part · Apr 20, 2016
- [01-0771833-10](https://drs.faa.gov/browse/excelExternalWindow/3073DD83C9E2984D86257FCC006EBBFD.0001): LED Landing Light. Whelen Engineering Co Inc · PMA PQ0610NE · Modification part · Apr 20, 2016
- [01-0790750-20](https://drs.faa.gov/browse/excelExternalWindow/2D8AB0D7C6000CA786257FCA00724738.0001): LED Landing Light. Whelen Engineering Co Inc · PMA PQ0610NE · Modification part · Apr 20, 2016
- [01-0790750-10](https://drs.faa.gov/browse/excelExternalWindow/0ABFC613100772D586257FCA00724733.0001): LED Landing Light. Whelen Engineering Co Inc · PMA PQ0610NE · Modification part · Apr 20, 2016
- [9230-17003-01](https://drs.faa.gov/browse/excelExternalWindow/9DD900830DCF6B3D86257EBD005F60D4.0001): L-3 Detachable Configuration Module. Acron Aviation Inc. · PMA PQ2024CE · Modification part · Aug 16, 2015
- [9060-17250-01](https://drs.faa.gov/browse/excelExternalWindow/8511FE654B6B00B686257EBD005F5E3F.0001): L-3 Kit Installation NGT-1000/ NGT-2000/ NGT-2500. Acron Aviation Inc. · PMA PQ2024CE · Modification part · Aug 16, 2015
- [9060-17500-02 (right angle RF)](https://drs.faa.gov/browse/excelExternalWindow/76DD7CDEA34E5E2786257EBD005F5FFE.0001): L-3 Kit Installation NGT-9000R Panel Mount. Acron Aviation Inc. · PMA PQ2024CE · Modification part · Aug 16, 2015

All of them: https://openairdocs.org/model/pilatus-pc-6-b-h2/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Pilatus PC-6-BH2](https://openairdocs.org/model/pilatus-pc-6-bh2): 0 registered aircraft, registry code 7090201

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