# N812AT: Piper PA-28-161 - Status: Valid registration - Airframe: [Piper PA-28-161](https://openairdocs.org/model/piper-pa-28-161) (registry code 7102803, 4 seats) - Engine: [Lycoming 0-320 series](https://openairdocs.org/engine/lycoming-0-320-series) (registry code 41508) - Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13) (Piper Aircraft Inc.), [TCDS E-274](https://openairdocs.org/tcds/E-274) (Lycoming Engines) (OpenAirDocs) - Serial number: 28-7716211 - Type: Fixed wing single engine - Engine type: Reciprocating - Airworthiness: Standard, normal, utility - Airworthiness date: May 11, 1977 - Certificate issued: January 19, 2023 - Expires: January 31, 2030 - Mode S code: AB10DC - Registered owner: [Haverlah Dennis W](https://openairdocs.org/faa-owner/HAVERLAH%20DENNIS%20W) - Location: [Cedar Park, TX](https://openairdocs.org/faa-place/TX/Cedar%20Park) - Owner type: Individual - Owner's area on the map: 30.5071° N, 97.8195° W: Placed by OpenAirDocs at the center of ZIP code 78613, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=812AT - Page: https://openairdocs.org/aircraft/N812AT 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. The registry lists only the engine series, so ADs for every Lycoming 0-320 model are included. ## ADs that may apply (OpenAirDocs): 67 in force ### Matched by airframe (Piper PA-28-161) - [AD 2024-14-03](https://openairdocs.org/ad/2024-14-03): Autopilot System · Garmin GFC 500 Autopilot (STC SA01866WI). Effective Aug 20, 2024 - [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 2020-26-16](https://openairdocs.org/ad/2020-26-16): Wing Spar · Piper PA-28-151, PA-28-161, PA-28-181 and 12 more. Effective Feb 16, 2021 - [AD 2018-07-03](https://openairdocs.org/ad/2018-07-03): Placard and Markings · Piper PA-28-140, PA-28-150, PA-28-151 and 12 more. Effective Apr 20, 2018 - [AD 2017-14-04](https://openairdocs.org/ad/2017-14-04): Engine Oil · Piper PA-28-140, PA-28-150, PA-28-151 and 22 more. Effective Aug 15, 2017 - [AD 2016-07-21](https://openairdocs.org/ad/2016-07-21): Wing Ribs/Bulkhead · Piper PA-28-161, PA-28-181 and PA-28R-201. Effective Apr 26, 2016 - [AD 2013-02-13](https://openairdocs.org/ad/2013-02-13): Stabilizer Control System · Piper PA-28-140, PA-28-150, PA-28-151 and 33 more. Effective Mar 11, 2013 - [AD 2010-26-04](https://openairdocs.org/ad/2010-26-04): Engine · Piper PA-28-161 with STC SA03303AT. Effective Feb 1, 2011 - [AD 2010-15-10](https://openairdocs.org/ad/2010-15-10): Control wheel shafts · Piper PA-28-140, PA-28-150, PA-28-151 and 33 more. Effective Aug 31, 2010 - [AD 2009-05-05](https://openairdocs.org/ad/2009-05-05): Primary Flight Displays · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 3, 2009 - [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006 - [AD 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006 - [AD 2005-19-20](https://openairdocs.org/ad/2005-19-20): Bushing screw thread expanders · Piper PA-28-160, PA-28-161, PA-28-180 and 1 more. Effective Nov 4, 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 2004-14-12](https://openairdocs.org/ad/2004-14-12): Control wheel attaching hardware · Piper PA-28-161, PA-28-181, PA-28R-201 and 8 more. Effective Aug 10, 2004 - [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001 - [AD 98-21-21 R1](https://openairdocs.org/ad/98-21-21-R1): Electric Inflatable Door Seals · Cessna 17-30, 17-30A, 17-31 and 267 more. Effective May 1, 2000 - [AD 99-26-05](https://openairdocs.org/ad/99-26-05): Induction Air Filter · Lavia Argentina PA-25, PA-25-235, PA-25-260 and 5 more. Effective Jan 13, 2000 - [AD 96-10-03](https://openairdocs.org/ad/96-10-03): Flap Handle Attach Bolt · Piper PA-28-140, PA-28-150, PA-28-151 and 28 more. Effective Jun 14, 1996 - [AD 87-08-08 R3](https://openairdocs.org/ad/87-08-08-R3): Lower spar cap · Piper PA-28-140, PA-28-150, PA-28-151 and 28 more. Effective May 22, 1989 - [AD 85-23-07](https://openairdocs.org/ad/85-23-07): Autopilot Systems · Aerostar PA-60-700P (Aerostar 700P), 172L, 172P and 37 more. Effective Jan 27, 1986 - [AD 81-23-05](https://openairdocs.org/ad/81-23-05): Seat Springs and Battery Box · Piper PA-28-151 and PA-28-161. Effective Mar 8, 1982 - [AD 80-14-03](https://openairdocs.org/ad/80-14-03): Bendix, King or Narco Transmitters · Piper PA-28-161, PA-28-181, PA-28-201T and 16 more. Effective Jul 1, 1980 - [AD 79-26-05](https://openairdocs.org/ad/79-26-05): Oil and Fuel System Hoses · Piper PA-28-140, PA-28-150, PA-28-151 and 28 more. Effective Jan 3, 1980 - [AD 79-22-02](https://openairdocs.org/ad/79-22-02): Fuel Leakage · Piper PA-28-161, PA-28-181, PA-28-201T and 6 more. Effective Oct 26, 1979 - [AD 79-13-03](https://openairdocs.org/ad/79-13-03): Fire Hazard Prevention · Piper PA-28-161, PA-28-181, PA-28-201T and 5 more. Effective Jun 8, 1979 - [AD 79-07-02](https://openairdocs.org/ad/79-07-02): Batteries · Aircraft Parts & Development A, A-2, A-3 and 149 more. Effective Apr 3, 1979 - [AD 79-02-05](https://openairdocs.org/ad/79-02-05): Fuel Flow · Piper PA-28-161, PA-28R-201 and PA-28R-201T. Effective Jan 29, 1979 - [AD 77-23-03](https://openairdocs.org/ad/77-23-03): Rod End Bearings · Piper PA-28-140, PA-28-151, PA-28-161 and 12 more. Effective Nov 14, 1977 ### Matched by engine (Lycoming 0-320 series) - [AD 2026-04-11](https://openairdocs.org/ad/2026-04-11): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 605 more. Effective Apr 8, 2026 - [AD 2022-16-03](https://openairdocs.org/ad/2022-16-03): Engine (RECIPROCATING) · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-F and 236 more. Effective Aug 15, 2022 - [AD 2017-16-11](https://openairdocs.org/ad/2017-16-11): Reciprocating Engine Power Section · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-360-B1G6 and 93 more. Effective Aug 15, 2017 - [AD 2012-03-07](https://openairdocs.org/ad/2012-03-07): Carburetor · Lycoming Engines GO-435, GO-435-C2 (O-435-17), GO-435-C2A and 389 more. Effective Mar 27, 2012 - [AD 2010-07-08](https://openairdocs.org/ad/2010-07-08): Turbochargers · Kelly Aerospace Energy Systems HIO-360-E1AD, HIO-360-E1BD, HIO-360-F1AD and 137 more. Effective Apr 19, 2010 - [AD 2009-26-12](https://openairdocs.org/ad/2009-26-12): Cylinder assemblies · Engine Components Reciprocating Engine Cylinder Assemblies, AEIO-320-D1B, AEIO-320-D2B and 264 more. Effective Feb 4, 2010 - [AD 2007-04-19 R1](https://openairdocs.org/ad/2007-04-19-R1): SAP cylinder assemblies · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 314 more. Effective May 7, 2007 - [AD 2004-10-14](https://openairdocs.org/ad/2004-10-14): Crankshaft gear · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 642 more. Effective Jun 25, 2004 - [AD 2002-12-07](https://openairdocs.org/ad/2002-12-07): Oil Filter Converter Plate Gasket or the Converter Plate Kit · Lycoming Engines HIO-360-E1AD, HIO-360-E1BD, HIO-360-F1AD and 95 more. Effective Jul 3, 2002 - [AD 98-17-11](https://openairdocs.org/ad/98-17-11): Crankshafts · Continental Motors A-65-3, A-65-8, A75-8 and 90 more. Effective Oct 19, 1998 - [AD 98-02-08](https://openairdocs.org/ad/98-02-08): Crankshaft · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 216 more. Effective Mar 30, 1998 - [AD 98-01-06](https://openairdocs.org/ad/98-01-06): Carburetors · Continental Motors A-65-1, A-65-12, A-65-12F and 184 more. Effective Feb 13, 1998 - [AD 97-15-11](https://openairdocs.org/ad/97-15-11): Cylinder kits · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 538 more. Effective Aug 12, 1997 - [AD 96-09-10](https://openairdocs.org/ad/96-09-10): Oil pump · Lycoming Engines AEIO-320-E1A, AEIO-320-E1B, AEIO-320-E2A and 334 more. Effective Jul 15, 1996 - [AD 95-26-02](https://openairdocs.org/ad/95-26-02): Aviation Gasoline · Lycoming Engines IO-320-B1A, IO-320-B1B, IO-320-B1C and 182 more. Effective Jan 24, 1996 - [AD 93-19-04](https://openairdocs.org/ad/93-19-04): Carburetors · Continental Motors A-65-1, A-65-12, A-65-12F and 184 more. Effective Oct 18, 1993 - [AD 92-12-05](https://openairdocs.org/ad/92-12-05): Piston Pins · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 532 more. Effective Jul 10, 1992 - [AD 90-04-06 R1](https://openairdocs.org/ad/90-04-06-R1): Propeller Governor External Oil Line · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 427 more. Effective May 28, 1991 - [AD 87-10-06 R1](https://openairdocs.org/ad/87-10-06-R1): Rocker Arm Assembly · Lycoming Engines IO-360-B4, IVO-360-A1A, O-340-A1A and 243 more. Effective Sep 1, 1989 - [AD 80-04-03 R2](https://openairdocs.org/ad/80-04-03-R2): Hydraulic Lifter · Lycoming Engines LO-360-E1A6D, LTO-360-E1A6D, O-320-H1AD and 7 more. Effective Apr 25, 1988 - [AD 81-16-05](https://openairdocs.org/ad/81-16-05): Magnetos · Lycoming Engines AEIO-320-E1B, AEIO-320-E2B, AEIO-360-B1G6 and 234 more. Effective Aug 6, 1981 - [AD 80-14-07](https://openairdocs.org/ad/80-14-07): Upper Exhaust Valve Spring Seats · Lycoming Engines LO-360-E1A6D, O-320-H1AD, O-320-H1BD and 5 more. Effective Jul 7, 1980 - [AD 79-10-03 R2](https://openairdocs.org/ad/79-10-03-R2): Engine Mounting Bracket Attaching Bolts · Lycoming Engines LO-360-E1A6D, O-320-H2AD and O-360-E1A6D. Effective Jul 1, 1980 - [AD 80-06-05](https://openairdocs.org/ad/80-06-05): Magnetos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 254 more. Effective Mar 28, 1980 - [AD 78-12-09](https://openairdocs.org/ad/78-12-09): Crankshaft Gear Assembly · Lycoming Engines O-320-H1AD, O-320-H1BD, O-320-H2AD and 3 more. Effective Feb 20, 1979 - [AD 77-07-07](https://openairdocs.org/ad/77-07-07): Oil Level Gage · Lycoming Engines O-320-H2AD. Effective Feb 20, 1979 - [AD 77-20-07](https://openairdocs.org/ad/77-20-07): Loose Rocker Arm Retaining Studs and Hydraulic Tappets · Lycoming Engines O-320-H1AD, O-320-H1BD, O-320-H2AD and 3 more. Effective Aug 31, 1978 - [AD 78-12-08](https://openairdocs.org/ad/78-12-08): Oil Pump Body · Lycoming Engines O-320-H1AD, O-320-H1BD, O-320-H2AD and 3 more. Effective Jun 20, 1978 - [AD 75-08-09](https://openairdocs.org/ad/75-08-09): Oil Pump Drive Shaft · Lycoming Engines AEIO-360-A1B, AEIO-360-A1B6, AEIO-360-A1C and 365 more. Effective Aug 18, 1977 - [AD 73-23-01](https://openairdocs.org/ad/73-23-01): Piston Pin Assembly · Lycoming Engines AIO-360-A1A, AIO-360-A1B, AIO-360-A2A and 215 more. Effective Jan 13, 1977 - [AD 69-24-03](https://openairdocs.org/ad/69-24-03): Carburetors · Continental Motors A-65-1, A-65-12, A-65-12F and 321 more. Effective Nov 29, 1969 - [AD 66-06-03](https://openairdocs.org/ad/66-06-03): Connecting Rod Assemblies · Lycoming Engines GO-435-C2 (O-435-17), GO-435-C2A, GO-435-C2A2 and 317 more. Effective Jan 16, 1969 - [AD 63-23-02](https://openairdocs.org/ad/63-23-02): Exhaust Valves · Lycoming Engines O-320-A1A, O-320-A1B, O-320-A2A and 25 more. Effective Aug 6, 1968 - [AD 67-01-04](https://openairdocs.org/ad/67-01-04): Oil Filters · Full flow oil filter (Superior Flow STC SA401SW or 2 others). Effective Jan 2, 1967 - [AD 66-20-04](https://openairdocs.org/ad/66-20-04): Oil Filter Adapter Gasket · Lycoming Engines IO-320-A1A, IO-320-A2A, IO-320-B1A and 121 more. Effective Aug 27, 1966 - [AD 64-16-05](https://openairdocs.org/ad/64-16-05): AC Pumps · Lycoming Engines HIO-360-B1A, HIO-360-B1B, IO-320-B1A and 86 more. Effective Jul 10, 1964 - [AD 59-10-07](https://openairdocs.org/ad/59-10-07): Cylinder Baffle Clamps · Lycoming Engines GO-480-A1A, GO-480-B, GO-480-B1A6 and 58 more - [AD 55-02-02](https://openairdocs.org/ad/55-02-02): Gasket · Lycoming Engines O-320-A1A and O-320-A2A ### Historical (superseded or no longer in force) - [AD 2018-02-05](https://openairdocs.org/ad/2018-02-05) (historical): Placard and Markings · Piper PA-28-140, PA-28-150, PA-28-151 and 12 more. Effective Feb 7, 2018 - [AD 2015-20-13](https://openairdocs.org/ad/2015-20-13) (historical): Wing Ribs/Bulkhead · Piper PA-28-161, PA-28-181 and PA-28R-201. Effective Oct 29, 2015 - [AD 2008-06-28 R1](https://openairdocs.org/ad/2008-06-28-R1) (historical): Primary Flight Displays (PFDs) · Avidyne Primary Flight Displays, 441, LC41-550FG and 22 more. Effective Apr 10, 2008 - [AD 2008-06-28](https://openairdocs.org/ad/2008-06-28) (historical): Primary flight display · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 10, 2008 - [AD 95-26-13](https://openairdocs.org/ad/95-26-13) (historical): Inspect Oil Cooler Hoses · Piper PA-28-140, PA-28-150, PA-28-151 and 22 more. Effective Feb 5, 1996 - [AD 2024-21-02](https://openairdocs.org/ad/2024-21-02) (historical): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 548 more. Effective Dec 5, 2024 - [AD 2008-19-05](https://openairdocs.org/ad/2008-19-05) (historical): Parallel Valve'' reciprocating engines · Engine Components Reciprocating Engine Cylinder Assemblies, AEIO-320-D1B, AEIO-320-D2B and 262 more. Effective Oct 20, 2008 - [AD 2005-26-10](https://openairdocs.org/ad/2005-26-10) (historical): ECi cylinder assemblies. · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 413 more. Effective Jan 31, 2006 - [AD 2000-18-53](https://openairdocs.org/ad/2000-18-53) (historical): Oil Filter Converter Plate Gaskets · Textron Lycoming, AVCO AEIO-540, IO-360-A1B6D, IO-360-A1D6D and 73 more - [AD 81-18-04 R2](https://openairdocs.org/ad/81-18-04-R2) (historical): Engine Oil Pump Driven Impeller and Shaft · Textron Lycoming, AVCO AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 376 more. Effective Jun 7, 1982 ## Information bulletins (advisory) (26 in force) - [SAIB 2022-20](https://openairdocs.org/saib/2022-20): Wing Spar. Issued Oct 19, 2022 - [SAIB AIR-21-10](https://openairdocs.org/saib/AIR-21-10): Wing, Attach Fittings (JASC 5740). Issued Jun 29, 2021 - [SAIB AIR-21-07](https://openairdocs.org/saib/AIR-21-07): WING SPAR, Verification of Correct Washers used with Wing Spar Attach Bolts. Issued Mar 30, 2021 - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 - [SAIB CE-11-12R1](https://openairdocs.org/saib/CE-11-12R1): Wings - PA-28, PA-32, PA-34, and PA-44 Rear Spar Corrosion at Fuselage Attach Fitting. Issued Dec 2, 2015 - [SAIB CE-14-23](https://openairdocs.org/saib/CE-14-23): Powerplant; Air Intake. Issued Aug 6, 2014 - [SAIB CE-11-42](https://openairdocs.org/saib/CE-11-42): Flight Controls: Control Cable/Pulley Inspections. Issued Jun 29, 2011 - [SAIB CE-11-14](https://openairdocs.org/saib/CE-11-14): Stabilizers- Vertical Stabilizer on Piper PA-28, PA-32, PA-34 Forward Attach Point Corrosion. Issued Jan 5, 2011 - [SAIB CE-11-13](https://openairdocs.org/saib/CE-11-13): Wings - Piper PA-28, PA-32, PA-34 Forward Spar Corrosion. Issued Jan 5, 2011 - [SAIB CE-11-11](https://openairdocs.org/saib/CE-11-11): Wings - Piper PA-28, PA-32, and PA-34 Aileron Hinge Fitting Corrosion. Issued Jan 5, 2011 - [SAIB CE-11-10](https://openairdocs.org/saib/CE-11-10): Piper PA-28, PA-32, PA-34, and PA-44 Corrosion on Flap Hinges, Brackets, and Ribs. Issued Jan 5, 2011 - [SAIB CE-11-01](https://openairdocs.org/saib/CE-11-01): Stabilizers -Horizontal Stabilator Turnbuckle. Issued Oct 4, 2010 - [SAIB CE-09-23](https://openairdocs.org/saib/CE-09-23): Fuel: Piper PA-28, PA-32, PA-34. Issued Apr 7, 2009 - [SAIB CE-09-17](https://openairdocs.org/saib/CE-09-17): Fuel: Piper PA-28 Series Aircraft Fuel Vent and Supply Hose Condition. Issued Mar 10, 2009 - [SAIB CE-08-13](https://openairdocs.org/saib/CE-08-13): Electrical Power. Issued Feb 27, 2008 - [SAIB CE-07-08](https://openairdocs.org/saib/CE-07-08): Avidyne Primary Flight display (PFD). Issued Oct 31, 2006 - [SAIB CE-01-30](https://openairdocs.org/saib/CE-01-30): . Issued Jul 11, 2001 - [SAIB NE-06-31R6](https://openairdocs.org/saib/NE-06-31R6): Engine Lubricating Oils. Issued Sep 26, 2022 - [SAIB NE-19-08](https://openairdocs.org/saib/NE-19-08): Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve Cylinders. Issued May 2, 2019 - [SAIB NE-08-32R1](https://openairdocs.org/saib/NE-08-32R1): Propeller Governor Idler Gear Shaft Set Screw. Issued May 13, 2016 - [SAIB NE-14-13](https://openairdocs.org/saib/NE-14-13): Reciprocating Engine - Cylinder Mounting Studs. Issued Mar 24, 2014 - [SAIB NE-13-06](https://openairdocs.org/saib/NE-13-06): Pushrod Shroud Spring Retainers, Engine Components Part No. AEL14995, for Lycoming Engines 320, 360, and 540 Series Engines. Issued Nov 21, 2012 - [SAIB NE-08-26R3](https://openairdocs.org/saib/NE-08-26R3): Magneto/Distributor. Issued Mar 31, 2011 - [SAIB NE-06-32R1](https://openairdocs.org/saib/NE-06-32R1): Reciprocating Engine - Crankshaft. Issued Sep 10, 2008 - [SAIB NE-03-18](https://openairdocs.org/saib/NE-03-18): . Issued Jan 22, 2003 - [SAIB NE-00-22](https://openairdocs.org/saib/NE-00-22): . Issued May 23, 2000 - [SAIB CE-11-12](https://openairdocs.org/saib/CE-11-12) (historical): PA-28, PA-32, PA-34, and PA-44 Rear Spar Corrosion at Fuselage Attach Fitting. Issued Jan 5, 2011 - [SAIB NE-06-31R5](https://openairdocs.org/saib/NE-06-31R5) (historical): Engine Lubricating Oils. Issued Oct 19, 2011 - [SAIB NE-06-31R4](https://openairdocs.org/saib/NE-06-31R4) (historical): Engine Lubricating Oils. Issued Jul 6, 2011 - [SAIB NE-06-31R3](https://openairdocs.org/saib/NE-06-31R3) (historical): Engine Lubricating Oils. Issued Jul 22, 2009 - [SAIB NE-06-31R2](https://openairdocs.org/saib/NE-06-31R2) (historical): Engine Lubricating Oils. Issued Apr 29, 2009 - [SAIB NE-08-26R1](https://openairdocs.org/saib/NE-08-26R1) (historical): Dual Magnetos. Issued Jul 8, 2008 - [SAIB NE-08-32](https://openairdocs.org/saib/NE-08-32) (historical): Propeller Governor Set Screw. Issued Jul 3, 2008 - [SAIB NE-06-31R1](https://openairdocs.org/saib/NE-06-31R1) (historical): . Issued Apr 18, 2006 - [SAIB NE-06-31](https://openairdocs.org/saib/NE-06-31) (historical): . Issued Feb 27, 2006 ## NTSB investigations None matched to N812AT. ## FAA accident and incident reports None matched to N812AT. ## 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. ## Service difficulty reports on N812AT not matched to an aircraft (41) They name N812AT, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR AT9900757](https://openairdocs.org/sdr/AT9900757), Oct 19, 1999: JAMB. CRACKED. FOUND SERVICE DOOR JAMB, LOWER AFT CORNER CRACKED .700 ALONG OUTER SKIN. FABRICATED AND INSTALLED 2 DOUBLER AND FILLERS IAW EO 09-5310-29-E1472. - [SDR AT9900754](https://openairdocs.org/sdr/AT9900754), Oct 18, 1999: FLOORBEAM. CORRODED. FOUND FLOORBEAM AT BS 996 RBL 35-RBL49 WAS CORRODED. FABRICATED FLOORBEAM AND INSTALLED IAW DC9 SRM 53-05 FIGURE 108, MM 27-20-0, 20-17-0. - [SDR AT9900744](https://openairdocs.org/sdr/AT9900744), Oct 15, 1999: FLOORBEAM. CORRODED. FOUND FLOORBEAM UPPER ATTACH ANGLE HAD EXFOLIATION CORROSION AT BS 980 RBL 35-RBL 49. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 53-05 FIGUR - [SDR AT9900741](https://openairdocs.org/sdr/AT9900741), Oct 15, 1999: SKIN. CRACKED. FOUND FORWARD SERVICE DOOR JAMB LOWER AFT CORNER OF SKIN CRACKED OUT OF LIMITS. FABRICATED 2 DOUBLERS, FILLERS, TRIMMED FILLER TO FIT, BACK DRILLED AND PRIMED R - [SDR AT9900745](https://openairdocs.org/sdr/AT9900745), Oct 10, 1999: PANEL. GOUGED. FOUND LEFT WING PANEL GOUGED BEYOND LIMITS. FABRICATED PANEL REPAIR IAW EO 99-1288. - [SDR AT9900713](https://openairdocs.org/sdr/AT9900713), Oct 6, 1999: ANGLE. CRACKED. FOUND RIGHT PYLON WEB LOWER SUPORT ANGLE FOUND 3 CRACK, PYLON STATION 105 3 BELOW PYLON REFERANCE PLANE, 5 OUTBOARD FUSELAGE SKIN. REMOVED SUPPORT ANGLE, FABRIC - [SDR AT9900753](https://openairdocs.org/sdr/AT9900753), Oct 4, 1999: BALANCE WT. CORRODED. FOUND RIGHT ELEVATOR BALANCE WEIGHT WAS CORRODED. REMOVED AND REPLACED RIGHT ELEVATOR BALANCE WEIGHT IAW DC9 SRM 55-01 PG 3, 51-30-1. - [SDR AT9900694](https://openairdocs.org/sdr/AT9900694), Oct 3, 1999: SUPPORT. CORRODED. FOUND IN CABIN FORWARD SECTION AT RIGHT FLOOR SUPPORT 10 FROM SERVICE DOOR WAS CORRODED, BS 160-200. REMOVED CORRODED FLOOR SUPPORT, FABRICATED AND INSTALLED RE - [SDR AT9900714](https://openairdocs.org/sdr/AT9900714), Oct 1, 1999: WINDOW FRAME. CORRODED. FOUND UPPER CORNER OF WINDOW FRAME WAS CRACKED AT BS 699R. REMOVED WINDOW FRAME, INSTALLED NEW WINDOW FRAME IAW DC9 SRM 51-30-5, 53-04 FIGURE 34. - [SDR AT9900746](https://openairdocs.org/sdr/AT9900746), Sep 29, 1999: ANGEL. CORRODED. FOUND CAP L ANGEL CORRODED AND CRACKED 4AT BS 965-BL24R. REMOVED CAP ANGEL AND REPLACED, FABRICATED AND INSTALLED 8 TRACKED ANGLE REPAIR IAW TIMCO RES 07186 AND - [SDR AT9900706](https://openairdocs.org/sdr/AT9900706), Sep 29, 1999: ANGLE. CORRODED. FOUND AFT AIRSTAIR, FIFTH STEP FROM THE BOTTOM AT SUPPORT ANGLE, WAS CORRODED. REMOVED CORRODED ANGLE, FABRICATED, TREADED, PRIMED, AND INSTALLED NEW ATTACH ANG - [SDR AT9900688](https://openairdocs.org/sdr/AT9900688), Sep 29, 1999: ANGLE. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND SUPPORT ANGLE FOR AFT VENTRAL STAIRS AND 3RD STEP CORRODED. REMOVED, FABRICATED, AND INSTALLED SU - [SDR AT9900708](https://openairdocs.org/sdr/AT9900708), Sep 28, 1999: SUPPORT. CORRODED. FOUND FLOOR SUPPORT AT BS 200-218 WAS CORRODED, ABOUT 14 FROM CENTER LINE. REMOVED FLOOR SUPPORT, FABRICATED, TREATED, PRIMED AND INSTALLED NEW FLOOR SUPPORT IA - [SDR AT9900707](https://openairdocs.org/sdr/AT9900707), Sep 28, 1999: STEP. CORRODED. FOUND AFT AIRSTAIR NR 3 WAS CORRODED. REMOVED AND REPLACED STEP IAW DC9 SRM 51-10-3, 53-01, 53-30-1. - [SDR AT9900692](https://openairdocs.org/sdr/AT9900692), Sep 28, 1999: SUPPORT. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND FLOOR SUPPORT AT LBL 50 BS 160-200 WAS CORRODED. REMOVED, FABRICATED, AND INSTALLED FLOOR SUPPORT - [SDR AT9900690](https://openairdocs.org/sdr/AT9900690), Sep 28, 1999: SUPORT. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND FLOOR SUPPORT CORRODED AT BS 205, RBL 0-40. REMOVED, FABRICATED, AND INSTALLED FLOOR SUPPORT IAW - [SDR AT9900752](https://openairdocs.org/sdr/AT9900752), Sep 27, 1999: SUPPORT. CORRODED. FOUND CABIN FLOOR SUPPORT BS 200 BL 0-BL 42L WAS CORRODED BEYOND LIMITS. REMOVED CORRODED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED REPAIR FLOOR SUPPOR - [SDR AT9900711](https://openairdocs.org/sdr/AT9900711), Sep 24, 1999: STEP. CORRODED. FOUND AFT AIRSTAIR, FOURTH STEP FROM THE BOTTOM, WEB ON INBOARD AND OUTBOARD SIDE OF STEP WAS CORRODED. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR FILLE - [SDR AT9900765](https://openairdocs.org/sdr/AT9900765), Sep 23, 1999: LONGERON. CRACKED. FOUND LONGERONS 3 AND 4 AT BS 148-178 CRACKED. REMOVED CRACKED SECTIONS, TRIMMED TO FIT AND INSTALLED NEW SECTIONS OF LONGERONS 3 AND 4 WITH SPLICES IAW DC9 SRM - [SDR AT9900680](https://openairdocs.org/sdr/AT9900680), Sep 23, 1999: SUPPORT. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND CORRODED FLOOR SUPPORT AND ATTACHMENT HARDWARE AT BS 157-218. REMOVED AND REPLACED FLOOR SUPPORT - [SDR AT9900751](https://openairdocs.org/sdr/AT9900751), Sep 22, 1999: ROD ASSY. CORRODED. FOUND FORWARD AIRSTAIRS AND LOWER ROD ASSEMBLY WERE CORRODED. REMOVED AND REPLACED THE LOWER ROD ASSEMBLY OF FORWARD AIRSTAIRS, AND RIGGED IAW DC9 MM 20-10-0, 5 - [SDR AT9900764](https://openairdocs.org/sdr/AT9900764), Sep 14, 1999: LONGERON. CRACKED. LONGERON AT BS 680-699 L6R WAS FOUND CRACKED. CUT OUT CRACKED SECTION, FABRICATED LONGERON REPAIR AND SPLICE IAW DC9 SRM 53-02 FIGURE18, 51-10-3, 51-10-4, 51-30 - [SDR AT9900767](https://openairdocs.org/sdr/AT9900767), Sep 13, 1999: SUPPORT. CORRODED. FOUND RIGHT OUTBOARD FLOOR SUPPORT ABOUT 10 FROM SERVICE DOOR AT BS 160-200 WAS CORRODED. REMOVED FLOOR SUPPORT, FABRICATED, AND INSTALLED NEW FLOOR SUPPORT IAW - [SDR AT9900719](https://openairdocs.org/sdr/AT9900719), Sep 13, 1999: SEAT TRACK. GOUGED. FOUND LEFT OUTBOARD SEAT TRACK WAS GOUGED AT BS 908. REMOVED AND REPLACED TRACK IAW DC9 SRM 53-05 FIGURE 4F 53-20-1, 51-10-3, 51-10-4. - [SDR AT9900717](https://openairdocs.org/sdr/AT9900717), Sep 13, 1999: BEAM. CRACKED. FOUND L-1 DOOR NR 4 BEAM WAS CRACKED AT THE AFT END. INSTALLED NEW FITTING, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-3, 52-01 FIGURE 1, 51-30-2 - [SDR AT9900693](https://openairdocs.org/sdr/AT9900693), Sep 13, 1999: STOP. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND RIGHT INBOARD ELEVATOR TRAVEL STOP WAS CORRODED. REMOVED AND REPLACED ELEVATOR TRAVEL STOP AND CA - [SDR AT9900691](https://openairdocs.org/sdr/AT9900691), Sep 13, 1999: SUPPORT. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND PASSENGER ENTRY WAY FLOOR SUPPORT WAS CORRODED AT BS 200. REMOVED, FABRICATED, AND INSTALLED FLOO - [SDR AT9900795](https://openairdocs.org/sdr/AT9900795), Sep 12, 1999: CONTROL COLUMN. CORRODED. FOUND FIRST OFFICERS CONTROL COLUMN ON THE AFT LOWER SIDE BELOW THE MACH TRIM INDICATOR WAS CORRODED. TRIMMED OUT CRACK, MECHANICALLY REMOVED CORROSION. FABRICA - [SDR AT9900768](https://openairdocs.org/sdr/AT9900768), Sep 12, 1999: RIB. GOUGED. FOUND RIGHT WING 5TH SLAT TRACK WAS CHAFING INTO XRS 241 LEADING EDGE RIB. BLENDED GOUGED AREA, TREATED AND PRIMED. REMOVED AND REPLACED ROLLER BEARING IAW TIMC - [SDR AT9900762](https://openairdocs.org/sdr/AT9900762), Sep 12, 1999: RIB. CRACKED. FOUND RIGHT WING LEADING EDGE HAD TWO CRACKED REPAIR FRAMES/RIBS AT BS 383. FABRICATED AND INSTALLED REPAIR ANGLES/FRAMES/RIBS IAW DC9 SRM 51-30-1, 51-30-2, 51- - [SDR AT9900718](https://openairdocs.org/sdr/AT9900718), Sep 12, 1999: SKIN. CRACKED. FOUND RIGHT ELEVATOR CRACKED IN THE SECONDARY SKIN AT THE RIVET OF THE OUTBOARD TRIM ATTACH POINT. STOP DRILLED HOLE NDT REVEALED CRACK CONTINUED. FABRICATED AN - [SDR AT9900710](https://openairdocs.org/sdr/AT9900710), Sep 12, 1999: SKIN. CORRODED. FOUND RIGHT OUTBOARD ELEVATOR UPPER TRAILING EDGE AT THE TIP WAS CORRODED. CUT OUT CORROSION. FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IAW DC9 SRM 51- - [SDR AT9900766](https://openairdocs.org/sdr/AT9900766), Sep 11, 1999: PANEL. DELAMINATED. FOUND LEFT WING UPPER TRAILING EDGE PANEL INBOARD OF THE AILERON AT XRS 383 WAS DELAMINATED. CUT OUT DELAMINATED HONEYCOMB CORE, BONDED NEW CORE, DOUBLERS AND S - [SDR AT9900742](https://openairdocs.org/sdr/AT9900742), Sep 11, 1999: LONGERON. CORRODED. FOUND A BULGE AT BS 598, LB 0, GAINED ACCESS AND FOUND CORROSION AT LONGERON 30. REMOVED LONGERON 30 LEFT AND RIGHT HAND WEB ASSEMBLY, INSTALLED NEW LONGERON, F - [SDR AT9900709](https://openairdocs.org/sdr/AT9900709), Sep 11, 1999: SKIN. DENTED. FOUND A DENT OUT OF LIMITS AT BS 445.3 BELOW L 19R. CUT OUT DENT, FABRICATED AND INSTALLED REPAIR IAW TIMCO EO 99-1281 REV DATED 10/01/99. - [SDR AT9900763](https://openairdocs.org/sdr/AT9900763), Sep 6, 1999: STRINGER. CRACKED. FOUND LEFT SIDE CABIN AT BS 756 STRINGER 2L WAS CRACKED AT ATTACH POINT. CUT OUT CRACKED SECTION, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICES IAW DC9 SR - [SDR AT9900761](https://openairdocs.org/sdr/AT9900761), Aug 12, 1999: RIB. CRACKED. FOUND RIGHT WING LEADING EDGE HAD THREE CRACKED REPAIR FRAMES/RIBS AT BS 445. REMOVED, FABRICATED AND INSTALLED REPAIR ANGLES IAW DC9 SRM 51-30-5, 57-01 FIGURE - [SDR AT9900461R1](https://openairdocs.org/sdr/AT9900461R1), Jun 22, 1999: SWITCH. DEFECTIVE. DURING APPROACH, NOTED SMOKE AFTER TURNING ON LEFT AND RIGHT WING LANDING LIGHTS, SMOKE STOP AFTER TURNING LIGHTS OFF. REMOVED AND REPLACED RIGHT WING LANDING L - [SDR AT9900461](https://openairdocs.org/sdr/AT9900461), Jun 22, 1999: SWITCH. FAILED. DURING APPROACH, NOTED SMOKE AFTER TURNING ON LEFT AND RIGHT WING LANDING LIGHTS, SMOKE STOPPED AFTER TURNING LIGHTS OFF. RIGHT WING LANDING LIGHT SWITCH WAS FO - [SDR AT9900131](https://openairdocs.org/sdr/AT9900131), Feb 18, 1999: SLIDE. LOOSE. GALLEY DOOR SLIDE CAME OUT OF BIN. RESECURED GALLEY DOOR EVACUATION SLIDE IAW MM 25-62-0. - [SDR AT9900114](https://openairdocs.org/sdr/AT9900114), Feb 12, 1999: BULB. FAILED. DURING A B CHECK, FOUND THE TAIL CONE EMERGENCY EXIT INOPERATIVE. RELAMPED TAIL CONE EMERGENCY EXIT LIGHT IAW MM 33-53-0, OPS CHECKED NORMAL. ## STCs that may be installed (OpenAirDocs) (408, 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 (Piper PA-28-161) - [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 SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation - [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies - [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 SA01134DE](https://openairdocs.org/stc/SA01134DE): Installation of EarthX ETX680-24-TSO Lithium Battery. EarthX Inc - [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels 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 SA02661LA](https://openairdocs.org/stc/SA02661LA): Installation to enlarge the existing main landing gear over-wing access hole in the upper wing skin. M2 Aviation Soultions LLC - [STC SA01147WI](https://openairdocs.org/stc/SA01147WI): Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. Concorde Battery Corporation - [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies - [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc - [STC SA01866WI](https://openairdocs.org/stc/SA01866WI): Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection. Garmin International Inc - [STC SA04075CH](https://openairdocs.org/stc/SA04075CH): Installation of Dynon EFIS-D10A EAA sales kit part number 102778-000. Dynon Avionics Inc - [STC SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. Alcor LLC - [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC. Lists PA-28 Series - [STC SA316SO](https://openairdocs.org/stc/SA316SO): Carburetor ice detector. LegacySTC.com. Lists PA-28 Series - [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 SA00037WI](https://openairdocs.org/stc/SA00037WI): Installation of B & C Specialty Products BC100-1 battery. B & C Specialty Products Inc - [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd - [STC SA01120SE](https://openairdocs.org/stc/SA01120SE): Installation of Door Steward. Mountain View Aviation LLC - [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC - [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc - [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft. Michelin North America Inc - [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc - [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine - [STC SA04400NY](https://openairdocs.org/stc/SA04400NY): Installation of the Integrated Back-up Battery System (IBBS). TCW Technologies LLC - [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International Inc - [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC - [STC SA00060AT](https://openairdocs.org/stc/SA00060AT): Installation of flap gap seals. Whelen Aerospace Technologies. Lists PA-28 Series - [STC SA01038AT](https://openairdocs.org/stc/SA01038AT): Installation of composite construction wingtips with Hoernr chordwise section with a clear plexiglass nose enclosure for aircraft lighting. (PA-28, -28R, -32, -32R, -34 series MODELS WITH CONSTANT-CHORD WINGS). Whelen Aerospace Technologies. Lists PA-28 Series - [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation - [STC SA04586CH](https://openairdocs.org/stc/SA04586CH): Installation of Electroair Back Up Battery Panel System Control. Electroair Aquisition Corp - [STC SA2156CE](https://openairdocs.org/stc/SA2156CE): Installation of flap and aileron gap seals. Curry Aviation LLC - [STC SA2230CE](https://openairdocs.org/stc/SA2230CE): Installation of replacement stabilator tips. Curry Aviation LLC - [STC SA00954WI](https://openairdocs.org/stc/SA00954WI): Installation of Concorde RG Series Batteries in Piper Single Engine Airplanes. Aero-Mach Wilco LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc - [STC SA01982AT](https://openairdocs.org/stc/SA01982AT): Installation of new composite wingtip with recognition light. Whelen Aerospace Technologies - [STC SA00028AT](https://openairdocs.org/stc/SA00028AT): Installation of 'speed splitter' flap bracket fairings. Whelen Aerospace Technologies. Lists PA-28 Series - [STC SA04231CH](https://openairdocs.org/stc/SA04231CH): Installation and activation of a TruTrak Vizion autopilot system. Honeywell International Inc - [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). 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 All 408: https://openairdocs.org/aircraft/N812AT/stcs.md ## Related - Other Piper PA-28-161 aircraft: https://openairdocs.org/model/piper-pa-28-161/aircraft.md - The Lycoming 0-320 series engine: https://openairdocs.org/engine/lycoming-0-320-series.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.