# N4795P: Pilatus PC-6

- Status: Valid registration
- Airframe: [Pilatus PC-6](https://openairdocs.org/model/pilatus-pc-6) (registry code 7090102, 8 seats)
- Data sheets: [TCDS 7A15](https://openairdocs.org/tcds/7A15) (Pilatus Aircraft Ltd.) (OpenAirDocs)
- Serial number: 341
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: March 23, 1984
- Certificate issued: June 21, 2019
- Expires: June 30, 2029
- Mode S code: A5E59E
- Registered owner: [Miair Inc](https://openairdocs.org/faa-owner/MIAIR%20INC)
- Location: [Lewes, DE](https://openairdocs.org/faa-place/DE/Lewes)
- Owner type: Corporation
- Owner's area on the map: 38.7287° N, 75.1685° W: Placed by OpenAirDocs at the center of ZIP code 19958, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=4795P
- Page: https://openairdocs.org/aircraft/N4795P

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 43 in force

### Matched by airframe (Pilatus PC-6)

- [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) (5 in force)

- [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 ACE-96-08](https://openairdocs.org/saib/ACE-96-08): . Issued Nov 8, 1996
- [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

## NTSB investigations

None matched to N4795P.

## FAA accident and incident reports

None matched to N4795P.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## STCs that may be installed (OpenAirDocs) (88, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Pilatus PC-6)

- [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/aircraft/N4795P/stcs.md

## Earlier aircraft with N4795P

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N4795P before.

- [Cancelled 1962-11-21](https://openairdocs.org/deregistered/N4795P-1962-11-21): Piper PA-23-250, S/N 27-354. Exported to Australia. Owner: [Cutright Ralph W](https://openairdocs.org/faa-owner/CUTRIGHT%20RALPH%20W), [Santa Monica, CA](https://openairdocs.org/faa-place/CA/Santa%20Monica)

## Related

- Other Pilatus PC-6 aircraft: https://openairdocs.org/model/pilatus-pc-6/aircraft.md

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