# N217EB: 1996 Pilatus PC-12

- Status: Valid registration
- Airframe: [Pilatus PC-12](https://openairdocs.org/model/pilatus-pc-12) (registry code 7090550, 12 seats)
- Engine: [Pratt & Whitney PT6A series](https://openairdocs.org/engine/pratt-whitney-pt6a-series) (registry code 52032)
- Data sheets: [TCDS A78EU](https://openairdocs.org/tcds/A78EU) (Pilatus Aircraft Ltd.) (OpenAirDocs)
- Serial number: 154
- Year built: 1996
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: October 31, 1997
- Certificate issued: April 16, 2014
- Expires: April 30, 2027
- Mode S code: A1D3E9
- Registered owner: [Rapids Camp Lodge Inc](https://openairdocs.org/faa-owner/RAPIDS%20CAMP%20LODGE%20INC)
- Location: [King Salmon, AK](https://openairdocs.org/faa-place/AK/King%20Salmon)
- Owner type: Corporation
- Owner's area on the map: 59.0709° N, 155.3775° W: Placed by OpenAirDocs at the center of ZIP code 99613, within about 20 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=217EB
- Page: https://openairdocs.org/aircraft/N217EB

From the FAA registry file of October 22, 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. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included.

## ADs that may apply (OpenAirDocs): 77 in force

### Matched by airframe (Pilatus PC-12)

- [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 2024-08-07](https://openairdocs.org/ad/2024-08-07): Main Landing Gear Attach Section · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Jun 3, 2024
- [AD 2023-09-12](https://openairdocs.org/ad/2023-09-12): Air Conditioning System Wiring · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Jul 5, 2023
- [AD 2020-21-23](https://openairdocs.org/ad/2020-21-23): Stabilizers · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Dec 7, 2020
- [AD 2016-18-05](https://openairdocs.org/ad/2016-18-05): Power Plant · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Oct 6, 2016
- [AD 2016-12-01](https://openairdocs.org/ad/2016-12-01): Wings · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Jul 15, 2016
- [AD 2015-19-15](https://openairdocs.org/ad/2015-19-15): Flight Controls · Pilatus PC-12, PC-12/45 and PC-12/47E. Effective Nov 3, 2015
- [AD 2008-07-11 R1](https://openairdocs.org/ad/2008-07-11-R1): Flight Controls · Pilatus PC-12, PC-12/45 and PC-12/47. Effective Mar 25, 2013
- [AD 2009-08-11](https://openairdocs.org/ad/2009-08-11): Ice and Rain Protection · Pilatus PC-12 and PC-12/45. Effective May 26, 2009
- [AD 2009-05-07](https://openairdocs.org/ad/2009-05-07): Rear stick-pusher cable · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Mar 30, 2009
- [AD 2008-07-11](https://openairdocs.org/ad/2008-07-11): Pitch trim actuator · Pilatus PC-12, PC-12/45 and PC-12/47. Effective May 9, 2008
- [AD 2008-02-03](https://openairdocs.org/ad/2008-02-03): MLG special bolts · Pilatus PC-12, PC-12/45 and PC-12/47. Effective Feb 20, 2008
- [AD 2007-21-11](https://openairdocs.org/ad/2007-21-11): Oil pile assemblies · Pilatus PC-12, PC-12/45 and PC-12/47. Effective Nov 5, 2007
- [AD 2007-03-06](https://openairdocs.org/ad/2007-03-06): Executive seats equipped with pedestal legs · Pilatus PC-12 and PC-12/45. Effective Mar 8, 2007
- [AD 2006-16-13](https://openairdocs.org/ad/2006-16-13): Lug fittings. · Pilatus PC-12 and PC-12/45. Effective Sep 18, 2006
- [AD 2006-08-11](https://openairdocs.org/ad/2006-08-11): Crew seat bucket assemblies · Pilatus PC-12 and PC-12/45. Effective Jun 2, 2006
- [AD 2005-22-13](https://openairdocs.org/ad/2005-22-13): Left and right main landing gear (MLG) assemblies · Pilatus PC-12 and PC-12/45. Effective Dec 19, 2005
- [AD 2005-22-04](https://openairdocs.org/ad/2005-22-04): Nose landing gear (NLG), main landing gear (MLG), and MLG shock absorber  
 assemblies · Pilatus PC-12 and PC-12/45. Effective Dec 12, 2005
- [AD 2005-11-06](https://openairdocs.org/ad/2005-11-06): Pitch actuator · Pilatus PC-12 and PC-12/45. Effective Jul 18, 2005
- [AD 2005-04-16](https://openairdocs.org/ad/2005-04-16): Windshield de-ice wiring system · Pilatus PC-12 and PC-12/45. Effective Mar 8, 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 2005-01-11](https://openairdocs.org/ad/2005-01-11): Main Landing Gear (MLG) Actuator · Pilatus PC-12 and PC-12/45. Effective Feb 22, 2005
- [AD 2004-12-11](https://openairdocs.org/ad/2004-12-11): Outboard flap flexshafts · Pilatus PC-12 and PC-12/45. Effective Jul 26, 2004
- [AD 2004-06-05](https://openairdocs.org/ad/2004-06-05): Main landing gear shock absorber · Pilatus PC-12 and PC-12/45. Effective May 6, 2004
- [AD 2004-04-01](https://openairdocs.org/ad/2004-04-01): Engine-driven pump housing · Pilatus PC-12, PC-12/45 and PC-7. Effective Mar 29, 2004
- [AD 2003-20-15](https://openairdocs.org/ad/2003-20-15): Fuel booster pump · Pilatus PC-12 and PC-12/45. Effective Oct 10, 2003
- [AD 2003-11-17](https://openairdocs.org/ad/2003-11-17): Pressure dome · Pilatus PC-12 and PC-12/45. Effective Jul 28, 2003
- [AD 2003-09-11](https://openairdocs.org/ad/2003-09-11): Pedestal Leg Assembly on Aft Facing Passenger Seats · Pilatus PC-12 and PC-12/45. Effective Jun 16, 2003
- [AD 2003-07-10](https://openairdocs.org/ad/2003-07-10): Push switch caps · Pilatus PC-12 and PC-12/45. Effective May 12, 2003
- [AD 2002-14-22](https://openairdocs.org/ad/2002-14-22): Main Landing Gear (MLG) Assembly Bolts · Pilatus PC-12 and PC-12/45. Effective Aug 29, 2002
- [AD 2002-06-10](https://openairdocs.org/ad/2002-06-10): Connector and Oxygen Tubing and Related Components in Rear Seat Bench · Pilatus PC-12 and PC-12/45. Effective May 6, 2002
- [AD 2001-25-10](https://openairdocs.org/ad/2001-25-10): Flap Control System · Pilatus PC-12 and PC-12/45. Effective Jan 25, 2002
- [AD 2001-22-15](https://openairdocs.org/ad/2001-22-15): Cargo Doors · Pilatus PC-12 and PC-12/45. Effective Dec 26, 2001
- [AD 2001-11-02](https://openairdocs.org/ad/2001-11-02): Generator · Pilatus PC-12 and PC-12/45. Effective Jul 23, 2001
- [AD 2000-26-17](https://openairdocs.org/ad/2000-26-17): Windshield Deicing System · Pilatus PC-12 and PC-12/45. Effective Feb 24, 2001
- [AD 2000-11-14](https://openairdocs.org/ad/2000-11-14): Airframe Pneumatic Deicing Boots · Pilatus PC-12 and PC-12/45. Effective Jul 17, 2000
- [AD 2000-02-31](https://openairdocs.org/ad/2000-02-31): Stick Pusher System · Pilatus PC-12 and PC-12/45. Effective Mar 27, 2000
- [AD 99-24-09](https://openairdocs.org/ad/99-24-09): Flap Inboard Attachment Fittings · Pilatus PC-12 and PC-12/45. Effective Jan 14, 2000
- [AD 99-17-01](https://openairdocs.org/ad/99-17-01): Flap Drive Shafts · Pilatus PC-12 and PC-12/45. Effective Oct 1, 1999
- [AD 99-14-03](https://openairdocs.org/ad/99-14-03): Generator Cables · Pilatus PC-12 and PC-12/45. Effective Aug 17, 1999
- [AD 99-06-17](https://openairdocs.org/ad/99-06-17): Second Generator Control Unit · Pilatus PC-12 and PC-12/45. Effective Jun 16, 1999
- [AD 99-06-05](https://openairdocs.org/ad/99-06-05): Alternate Flap System · Pilatus PC-12 and PC-12/45. Effective Apr 16, 1999
- [AD 98-21-27](https://openairdocs.org/ad/98-21-27): Passenger Seats And Seat Rail Covers · Pilatus PC-12 and PC-12/45. Effective Nov 26, 1998
- [AD 98-20-28](https://openairdocs.org/ad/98-20-28): Airplane Flight Manual (AFM) - Limitations Icing · Pilatus PC-12 and PC-12/45. Effective Nov 4, 1998
- [AD 98-11-01 R2](https://openairdocs.org/ad/98-11-01-R2): Fuel Tank Vent Valves · Pilatus PC-12 and PC-12/45. Effective Sep 22, 1998
- [AD 98-11-20](https://openairdocs.org/ad/98-11-20): Lavatory Wall and Passenger Seat Configuration · Pilatus PC-12 and PC-12/45. Effective Jul 13, 1998
- [AD 98-08-26](https://openairdocs.org/ad/98-08-26): Fuel Tank Underwing Access Panels · Pilatus PC-12 and PC-12/45. Effective May 29, 1998
- [AD 98-05-06](https://openairdocs.org/ad/98-05-06): Elevator Rivet Lengths · Pilatus PC-12. Effective May 29, 1998
- [AD 98-07-18](https://openairdocs.org/ad/98-07-18): Propeller De-icing Controller · Pilatus PC-12 and PC-12/45. Effective Apr 28, 1998
- [AD 98-04-16](https://openairdocs.org/ad/98-04-16): Aileron Tie-Rod Jam Nuts · Pilatus PC-12 and PC-12/45. Effective Apr 2, 1998

### Matched by engine (Pratt & Whitney PT6A series)

- [AD 2024-04-51](https://openairdocs.org/ad/2024-04-51): Turbine Section · Pratt & Whitney Canada PT6A-64, PT6A-66, PT6A-66A and 17 more. Effective Mar 28, 2024
- [AD 2022-08-13](https://openairdocs.org/ad/2022-08-13): Turbine Section · Pratt & Whitney Canada PT6A-34, PT6A-34B, PT6A-34AG and 2 more. Effective May 27, 2022
- [AD 2016-05-13](https://openairdocs.org/ad/2016-05-13): Corrosion and perforation of the two-ply Cu-Be bellows in Woodward FCUs. · Pratt & Whitney Canada PT6A-60AG, PT6A-65AG, PT6A-67AF and 1 more. Effective Apr 22, 2016
- [AD 2014-17-08 R1](https://openairdocs.org/ad/2014-17-08-R1): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Jun 5, 2015
- [AD 2014-11-05](https://openairdocs.org/ad/2014-11-05): Reinforcement liner to the power turbine (PT) containment   
  ring and, for certain PT containment rings, adding scallops · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 18 more. Effective Aug 5, 2014
- [AD 2012-09-10](https://openairdocs.org/ad/2012-09-10): First stage sun gears · Pratt & Whitney Canada PT6A-110, PT6A-112, PT6A-114 and 12 more. Effective May 23, 2012
- [AD 2011-25-12](https://openairdocs.org/ad/2011-25-12): Sun gear · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 4 more. Effective Dec 28, 2011
- [AD 2011-20-51](https://openairdocs.org/ad/2011-20-51): Gears · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 4 more. Effective Nov 1, 2011
- [AD 2004-25-18](https://openairdocs.org/ad/2004-25-18): Propeller governor assemblies · Pratt & Whitney Canada PT6A-60A and PT6A-65B. Effective Jan 18, 2005
- [AD 2002-23-13](https://openairdocs.org/ad/2002-23-13): Turbine Exhaust Ducts · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 20 more. Effective Dec 31, 2002
- [AD 2001-20-01](https://openairdocs.org/ad/2001-20-01): Compressor Bleed Valve Assembly · Pratt & Whitney Canada PT6A-114A and PT6A-25C. Effective Nov 5, 2001
- [AD 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997
- [AD 95-13-08](https://openairdocs.org/ad/95-13-08): Compressor Turbine Disk · Pratt & Whitney Canada PT6A-67D. Effective Jul 12, 1995
- [AD 93-23-06](https://openairdocs.org/ad/93-23-06): Airframe Chip Detector Flag System · Pratt & Whitney Canada PT6A-50. Effective Jan 26, 1994
- [AD 92-15-11](https://openairdocs.org/ad/92-15-11): Compressor Delivery Air Line (P3) Filter Assembly · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-21 and 7 more. Effective Aug 17, 1992
- [AD 90-12-05](https://openairdocs.org/ad/90-12-05): Engine Overhaul · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 3 more. Effective May 30, 1990
- [AD 86-10-05](https://openairdocs.org/ad/86-10-05): First Stage Compressor Hub · Pratt & Whitney Canada PT6A-42. Effective Jun 5, 1986
- [AD 80-08-12](https://openairdocs.org/ad/80-08-12): Fuel Pump Drive Coupling Splines · Pratt & Whitney Canada PT6A-11, PT6A-112, PT6A-135 and 24 more. Effective Apr 18, 1980
- [AD 80-04-02](https://openairdocs.org/ad/80-04-02): Push-Pull Control Terminal · Pratt & Whitney Canada PT6A-20, PT6A-6A, PT6A-6B and 1 more. Effective Feb 8, 1980
- [AD 78-17-07](https://openairdocs.org/ad/78-17-07): Fuel Control Unit · Pratt & Whitney Canada PT6A-38, PT6A-41 and PT6A-45A. Effective Aug 31, 1978
- [AD 78-12-04](https://openairdocs.org/ad/78-12-04): No. 2 Bearing Pressure Oil Transfer Tube Assembly · Pratt & Whitney Canada PT6A-38, PT6A-41 and PT6A-45A. Effective Jun 19, 1978
- [AD 75-06-01](https://openairdocs.org/ad/75-06-01): Gearbox Deterioration · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-20B and 11 more. Effective Apr 1, 1977
- [AD 75-11-04](https://openairdocs.org/ad/75-11-04): Reduction Gearbox Engine Distress · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-20B and 8 more. Effective May 20, 1975
- [AD 70-16-01](https://openairdocs.org/ad/70-16-01): Turbo Propeller Governors · Pratt & Whitney Canada PT6A-11, PT6A-11AG, PT6A-15AG and 5 more. Effective Aug 4, 1970
- [AD 69-23-06](https://openairdocs.org/ad/69-23-06): Fuel Pumps · Pratt & Whitney Canada PT6A-20, PT6A-27, PT6A-28 and 4 more. Effective Nov 15, 1969
- [AD 68-05-03](https://openairdocs.org/ad/68-05-03): Reverse Mode · Pratt & Whitney Canada PT6A-20 and PT6A-6B. Effective Feb 28, 1968

### Historical (superseded or no longer in force)

- [AD 2023-12-17](https://openairdocs.org/ad/2023-12-17) (historical): Horizontal Stabilizer, Spar/Rib · Pilatus PC-12, PC-12/47, PC-12/45 and 1 more. Effective Aug 7, 2023
- [AD 2022-19-03](https://openairdocs.org/ad/2022-19-03) (historical): Rudder Actuator, Main Landing Gear, Main Landing Gear Attach Section · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Oct 27, 2022
- [AD 2016-26-08](https://openairdocs.org/ad/2016-26-08) (historical): Time Limits · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Feb 9, 2017
- [AD 2014-22-01](https://openairdocs.org/ad/2014-22-01) (historical): Time Limits · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Dec 18, 2014
- [AD 2012-26-16](https://openairdocs.org/ad/2012-26-16) (historical): Time Limits · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Mar 26, 2013
- [AD 2009-14-13](https://openairdocs.org/ad/2009-14-13) (historical): Landing gear · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Aug 19, 2009
- [AD 2008-06-17](https://openairdocs.org/ad/2008-06-17) (historical): Rear stick-pusher · Pilatus PC-12, PC-12/45 and PC-12/47. Effective Apr 2, 2008
- [AD 2003-14-07](https://openairdocs.org/ad/2003-14-07) (historical): Nose landing gear (NLG) · Pilatus PC-12 and PC-12/45. Effective Sep 5, 2003
- [AD 2002-01-09](https://openairdocs.org/ad/2002-01-09) (historical): Gasket Material and Relief Valve Attachment Screws · Pilatus PC-12, PC-12/45 and PC-7. Effective Feb 28, 2002
- [AD 2000-21-14](https://openairdocs.org/ad/2000-21-14) (historical): Torque Oil-pressure Tubes and Py Pressure Pipe · Pilatus PC-12 and PC-12/45. Effective Dec 15, 2000
- [AD 99-19-32](https://openairdocs.org/ad/99-19-32) (historical): Actuator Internal Gear Systems · Pilatus PC-12 and PC-12/45. Effective Nov 8, 1999
- [AD 99-17-08](https://openairdocs.org/ad/99-17-08) (historical): Generator · Pilatus PC-12 and PC-12/45. Effective Oct 4, 1999
- [AD 98-11-01 R1](https://openairdocs.org/ad/98-11-01-R1) (historical): Fuel Tank Vent Valves · Pilatus PC-12 and PC-12/45. Effective Sep 22, 1998
- [AD 98-13-08](https://openairdocs.org/ad/98-13-08) (historical): Generator Cables · Pilatus PC-12. Effective Jul 31, 1998
- [AD 98-11-01](https://openairdocs.org/ad/98-11-01) (historical): Fuel Tank Vent Valves · Pilatus PC-12 and PC-12/45. Effective Jun 7, 1998
- [AD 97-23-04](https://openairdocs.org/ad/97-23-04) (historical): Fuel Tank Vent Valves · Pilatus PC-12 and PC-12/45. Effective Dec 1, 1997
- [AD 2014-17-08](https://openairdocs.org/ad/2014-17-08) (historical): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Oct 8, 2014
- [AD 88-24-02](https://openairdocs.org/ad/88-24-02) (historical): Airframe Chip Detector Flag System · Pratt & Whitney Canada PT6A-50

All 95: https://openairdocs.org/aircraft/N217EB/ads.md

## Information bulletins (advisory) (15 in force)

- [SAIB CE-17-13](https://openairdocs.org/saib/CE-17-13): Engine Oil Pressure; Torque Transducer Oil Pressure Pipe P-Clamp Installation. Issued May 19, 2017
- [SAIB CE-16-12](https://openairdocs.org/saib/CE-16-12): AUTO FLIGHT - Autopilot. Issued Jan 25, 2016
- [SAIB CE-05-08](https://openairdocs.org/saib/CE-05-08): . Issued Oct 25, 2004
- [SAIB CE-04-70](https://openairdocs.org/saib/CE-04-70): . Issued Jul 8, 2004
- [SAIB CE-04-62](https://openairdocs.org/saib/CE-04-62): . Issued Apr 12, 2004
- [SAIB CE-04-60](https://openairdocs.org/saib/CE-04-60): . Issued Mar 30, 2004
- [SAIB CE-04-52](https://openairdocs.org/saib/CE-04-52): . Issued Feb 13, 2004
- [SAIB CE-03-19](https://openairdocs.org/saib/CE-03-19): . Issued Jan 22, 2003
- [SAIB CE-02-15](https://openairdocs.org/saib/CE-02-15): . Issued Feb 13, 2002
- [SAIB ACE-96-08](https://openairdocs.org/saib/ACE-96-08): . Issued Nov 8, 1996
- [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015
- [SAIB NE-12-04](https://openairdocs.org/saib/NE-12-04): Turbine/ Turboprop Engine: Reduction Gearbox. Issued Nov 1, 2011
- [SAIB NE-10-47](https://openairdocs.org/saib/NE-10-47): Turbine Engine Compressor Section. Issued Aug 30, 2010
- [SAIB NE-06-34](https://openairdocs.org/saib/NE-06-34): . Issued Mar 21, 2006
- [SAIB CE-03-24](https://openairdocs.org/saib/CE-03-24): . Issued Feb 19, 2003

## NTSB investigations

None matched to N217EB.

## FAA accident and incident reports

None matched to N217EB.

## 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) (203, 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-12)

- [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 SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [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 SA02742NY](https://openairdocs.org/stc/SA02742NY): Installation of MT-Propeller Entwicklung GmbH model MTV-27-1-N-C-F-R(P)/CFR260-65. MT- Propeller Entwicklung GmbH
- [STC SA04763NY](https://openairdocs.org/stc/SA04763NY): Installation of of Gogo Galileo HDX. Pro Star Aviation LLC
- [STC SA03275CH](https://openairdocs.org/stc/SA03275CH): Installation of an antiskid brake system. Lee Air Inc
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc
- [STC SA04841NY](https://openairdocs.org/stc/SA04841NY): Installation of replacement LED recognition lights, LED wingtip lights, LED beacon lights, LED taxi lights, and LED landing lights. Whelen Aerospace Technologies
- [STC SA04278NY](https://openairdocs.org/stc/SA04278NY): Installation of the GPS/Iridium Antenna Provisions. SKYTRAC Systems Ltd
- [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 SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc
- [STC SA01527CH](https://openairdocs.org/stc/SA01527CH): Installation of a Honeywell KMH 880 Multi-Hazard Awareness System or a Honeywell KTA 870 Traffic Advisory System. Amphenol Cable and Interconnect Technologies Inc
- [STC SA04220NY](https://openairdocs.org/stc/SA04220NY): Installation of Retractable Camera Mount System. Trine Aerospace & Defense
- [STC SA02558SE](https://openairdocs.org/stc/SA02558SE): Installation of a Light Emitting Diode (LED) Landing and Taxi Light. AeroLED's Holdings LLC
- [STC SA04051CH](https://openairdocs.org/stc/SA04051CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC SA00028MC](https://openairdocs.org/stc/SA00028MC): Installation of non-essential antenna and radome. Sierra Nevada Company LLC
- [STC SA03316CH](https://openairdocs.org/stc/SA03316CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development Inc
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [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 SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA03097AT](https://openairdocs.org/stc/SA03097AT): Installation of Cabin Interior Light Emitting Diode (LED) Reading and Wash Lights and Air Gaspers. Woven Electronics, LLC
- [STC SA01044DE](https://openairdocs.org/stc/SA01044DE): This STC approves the Finnoff Aviation Products installation of the TB44 advanced lithium-ion battery manufactured by True Blue Power in the make and model listed above (Single Battery Configuration). Finnoff Aviation Products
- [STC SA01376CH](https://openairdocs.org/stc/SA01376CH): Installation of Parker Hannifin Wheel/Brake Assembly P/N 40-424/30-244 (conversion kit no. 199-241). KAMAN Corporation Aircraft Wheel and Brake LLC
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc
- [STC ST03660AT](https://openairdocs.org/stc/ST03660AT): Installation of a Flight Components/EMTEQ LED Position (Navigation) Lights. Woven Electronics LLC
- [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 SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. 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 SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA02075SE](https://openairdocs.org/stc/SA02075SE): Installation of a Mid-Continent MD835( ) Lithium Ion Battery. Mid-Continent Instrument Co. Inc
- [STC SA00272LA](https://openairdocs.org/stc/SA00272LA): Installation of a Patient Loading Utility System (PLUS). LifePort LLC
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC SA02427AK](https://openairdocs.org/stc/SA02427AK): Installation of the Max-Viz® Enhanced Vision System (EVS) Model-1500 on Pilatus PC-12 aircraft equipped with a fixed-mounted or panel-mounted Multi-Function Display (MFD) with the ability to display video imagery. PECO Inc
- [STC SA01116WI-D](https://openairdocs.org/stc/SA01116WI-D): Installation of a Honeywell AM-250 Altimeter. Honeywell International Inc
- [STC SA00886WI-D](https://openairdocs.org/stc/SA00886WI-D): Installation of Honeywell KGP 560 General Aviation Enhanced Ground Proximity Warning System (GA-EGPWS) with optional KMD 550/850 Multi-Function Display. Honeywell International Inc
- [STC SA01524WI-D](https://openairdocs.org/stc/SA01524WI-D): Models PC-12, PC-12/45 and PC-12/47 - Installation of the alternate part number EFS 40/50 SG 465 Symbol Generator. Honeywell International Inc
- [STC SA00393BO](https://openairdocs.org/stc/SA00393BO): Installation of the Pratt & Whitney Engine Services FAST System. Pratt & Whitney Engine Services Inc
- [STC SA01855WI](https://openairdocs.org/stc/SA01855WI): Installation of the Send Solutions Airtext Router in 14 CFR Part 23 Aircraft. 3S Certification LLC
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc
- [STC SA02677LA](https://openairdocs.org/stc/SA02677LA): Modification to upgrade the existing Mode S Transponder system by installing the ACSS NXT-700 Transponder with ADS-B Out and optionally install the ACSS NXG-900 GPS as the position source for ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA02678LA](https://openairdocs.org/stc/SA02678LA): Modification to upgrade the existing Mode S Transponder system by installing the ACSS NXT-600 Transponder with ADS-B Out and optionally install the ACSS NXG-900 GPS as the position source for ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [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 SA02651SE](https://openairdocs.org/stc/SA02651SE): Installation of ram air cowling. American Aviation Inc
- [STC SA00658SE](https://openairdocs.org/stc/SA00658SE): Installation of a fuselage mounted emergency medical stowage box. LifePort LLC

All 203: https://openairdocs.org/aircraft/N217EB/stcs.md

## Earlier aircraft with N217EB

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N217EB before.

- [Cancelled 1993-09-01](https://openairdocs.org/deregistered/N217EB-1993-09-01): Embraer EMB-110P1, S/N 110445. Exported to Sweden. Owner: [First Security Bk Of Utah Trustee](https://openairdocs.org/faa-owner/FIRST%20SECURITY%20BK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)

## Related

- Other Pilatus PC-12 aircraft: https://openairdocs.org/model/pilatus-pc-12/aircraft.md
- The Pratt & Whitney PT6A series engine: https://openairdocs.org/engine/pratt-whitney-pt6a-series.md

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