# N728AA: 2004 Cessna T182T

- Status: Valid registration
- Airframe: [Cessna T182T](https://openairdocs.org/model/cessna-t182t) (registry code 2072738, 4 seats)
- Engine: [Lycoming TI0-540 series](https://openairdocs.org/engine/lycoming-ti0-540-series) (registry code 41533)
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13) (Textron Aviation Inc.), [TCDS E14EA](https://openairdocs.org/tcds/E14EA) (Lycoming Engines) (OpenAirDocs)
- Serial number: T18208249
- Year built: 2004
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: August 2, 2004
- Certificate issued: October 15, 2004
- Expires: October 31, 2028
- Mode S code: A9C145
- Registered owner: [Brinckerhoff Allen D](https://openairdocs.org/faa-owner/BRINCKERHOFF%20ALLEN%20D)
- Location: [Windermere, FL](https://openairdocs.org/faa-place/FL/Windermere)
- Owner type: Individual
- Owner's area on the map: 28.4828° N, 81.5387° W: Placed by OpenAirDocs at the center of ZIP code 34786, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=728AA
- Page: https://openairdocs.org/aircraft/N728AA

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 TI0-540 model are included.

## ADs that may apply (OpenAirDocs): 64 in force

### Matched by airframe (Cessna T182T)

- [AD 2024-14-03](https://openairdocs.org/ad/2024-14-03): Autopilot System · Garmin GFC 500 Autopilot (STC SA01866WI). Effective Aug 20, 2024
- [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [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 2013-11-11](https://openairdocs.org/ad/2013-11-11): Engine Oil Pressure · Cessna 172R, 172S, 182S and 4 more. Effective Aug 1, 2013
- [AD 2008-26-10](https://openairdocs.org/ad/2008-26-10): Alternate static air source selector valve · Cessna 172, 172A, 172B and 179 more. Effective Jan 5, 2009
- [AD 2008-10-02](https://openairdocs.org/ad/2008-10-02): Part number identification placard · Cessna 172, 172R, 172RG and 64 more. Effective May 12, 2008
- [AD 2008-05-09](https://openairdocs.org/ad/2008-05-09): Crew seats · Cessna 172R, 172S, 182T and 3 more. Effective Apr 8, 2008
- [AD 2008-02-18](https://openairdocs.org/ad/2008-02-18): Pick-up collar support and nylon screws · BRS-172 parachute recovery system (Ballistic Recovery Systems STC SA01679CH or SA01999CH). Effective Feb 28, 2008
- [AD 2008-02-06](https://openairdocs.org/ad/2008-02-06): GSM 85 servo gearbox units · Cessna 182T, 206H, LC40-550FG and 11 more. Effective Feb 26, 2008
- [AD 2007-08-03](https://openairdocs.org/ad/2007-08-03): Flexible fuel hoses · Cessna 172R, 172S, 182T and 3 more. Effective May 2, 2007
- [AD 2007-05-10](https://openairdocs.org/ad/2007-05-10): Steel lock rod/bar on both crew seat back cylinder lock assemblies · Cessna 172R, 172S, 182S and 4 more. Effective Apr 11, 2007
- [AD 2006-17-04](https://openairdocs.org/ad/2006-17-04): Flexible fuel hoses located in the engine compartment · Cessna 172R, 172S, 182T and 3 more. Effective Sep 1, 2006
- [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 2005-13-10](https://openairdocs.org/ad/2005-13-10): Main electrical power junction box circuit breakers · Cessna 172R, 172S, 182T and 3 more. Effective Aug 9, 2005
- [AD 2005-05-53 R1](https://openairdocs.org/ad/2005-05-53-R1): Flight control system · Cessna 172R, 172S, 182T and 1 more. Effective Mar 21, 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 2004-15-18](https://openairdocs.org/ad/2004-15-18): Honeywell KAP 140 Autopilot Computer System · Cessna 172R, 172S, 182S and 4 more. Effective Sep 12, 2004
- [AD 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 1998

### Matched by engine (Lycoming TI0-540 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 2017-11-10](https://openairdocs.org/ad/2017-11-10): Engine Exhaust System · Lycoming Engines TIO-540-AJ1A. Effective Jun 28, 2017
- [AD 2015-19-07](https://openairdocs.org/ad/2015-19-07): Fuel injector fuel lines · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 187 more. Effective Nov 3, 2015
- [AD 2015-10-06](https://openairdocs.org/ad/2015-10-06): Engine exhaust pipes · Lycoming Engines TIO-540-AJ1A. Effective Jul 2, 2015
- [AD 2013-21-02](https://openairdocs.org/ad/2013-21-02): Turbochargers · Continental Motors LTSIO-360-RB, TSIO-360-MB, TSIO-360-RB and 2 more. Effective Nov 13, 2013
- [AD 2012-19-01](https://openairdocs.org/ad/2012-19-01): Crankshafts · Lycoming Engines AEIO-360-A1A, AEIO-360-A1B, AEIO-360-A1B6 and 321 more. Effective Oct 24, 2012
- [AD 71-13-01 R1](https://openairdocs.org/ad/71-13-01-R1): Rescinding an airworthiness directive · Lycoming Engines TIO-540-A1A, TIO-540-A1B, TIO-540-A1C and 13 more. Effective Mar 8, 2012
- [AD 2012-03-06](https://openairdocs.org/ad/2012-03-06): Fuel servo diaphragm · Continental Motors 6-260-A, 6-285-A, 6-285-B and 482 more. Effective Feb 24, 2012
- [AD 2011-13-03](https://openairdocs.org/ad/2011-13-03): Turbocharger Turbine · Lycoming Engines LTO-360-E1A6D, O-540-L3C5D, TIGO-541-E1A and 20 more. Effective Jul 13, 2011
- [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 2009-02-03](https://openairdocs.org/ad/2009-02-03): Fuel injection servos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 261 more. Effective Feb 9, 2009
- [AD 2008-08-17](https://openairdocs.org/ad/2008-08-17): Turbocharger turbine housing flange and the exhaust tube flange · Teledyne Continental Motors TSIOL-550-A 'Liquid-Cooled' engines (RAM Aircraft Limited Partnership STC SA7633SW or SA7633SW-D). Effective May 6, 2008
- [AD 2006-10-21](https://openairdocs.org/ad/2006-10-21): ECi connecting rods · Engine Components Reciprocating Engine Connecting Rods, AEIO-360-B1B, AEIO-360-B1D and 171 more. Effective Jun 22, 2006
- [AD 2005-19-11](https://openairdocs.org/ad/2005-19-11): Crankshafts · Lycoming Engines AEIO-360-A1B6, AEIO-360-A1E6, AEIO-540-D4A5 and 59 more. Effective Oct 21, 2005
- [AD 2005-12-06](https://openairdocs.org/ad/2005-12-06): Riveted-impulse coupling assemblies and snap-ring coupling assemblies · Lycoming Engines AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 154 more. Effective Jul 19, 2005
- [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 2004-05-24](https://openairdocs.org/ad/2004-05-24): Zinc-plated Crankshaft Gear Retaining Bolts · Lycoming Engines AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 161 more. Effective Mar 30, 2004
- [AD 2003-14-03](https://openairdocs.org/ad/2003-14-03): Rotary fuel pumps · Lycoming Engines AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 262 more. Effective Aug 14, 2003
- [AD 2002-19-03](https://openairdocs.org/ad/2002-19-03): Crankshaft · Lycoming Engines IO-540-A1A5, IO-540-AA1A5, IO-540-AA1B5 and 81 more. Effective Sep 20, 2002
- [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 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 97-01-04](https://openairdocs.org/ad/97-01-04): Cylinder assemblies · Lycoming Engines IO-540-M1B5D, LTIO-540-F2BD, LTIO-540-J2B and 10 more. Effective Apr 22, 1997
- [AD 91-21-01 R1](https://openairdocs.org/ad/91-21-01-R1): Exhaust System Flanges · Lycoming Engines TIO-540-S1AD. Effective Jun 27, 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 95-07-01](https://openairdocs.org/ad/95-07-01): Connecting Rod Bolt · Lycoming Engines AEIO-360-A1E, AEIO-360-B1G6, AEIO-360-H1A and 177 more. Effective Apr 12, 1995
- [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 91-10-04](https://openairdocs.org/ad/91-10-04): Exhaust Transition Flange Bolts · Lycoming Engines TIO-540-AE2A. Effective May 21, 1991
- [AD 91-08-07](https://openairdocs.org/ad/91-08-07): Fuel Pump · Lycoming Engines TIO-360-A1A, TIO-360-A1B, TIO-360-A3B6 and 51 more. Effective May 6, 1991
- [AD 89-15-10](https://openairdocs.org/ad/89-15-10): Nozzle Vent Manifold · Lycoming Engines TIO-540-AE2A. Effective Nov 30, 1989
- [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 84-19-03 R1](https://openairdocs.org/ad/84-19-03-R1): Cylinder Assemblies · Lycoming Engines LTIO-540-V2AD and TIO-540-V2AD. Effective Sep 20, 1984
- [AD 83-22-04](https://openairdocs.org/ad/83-22-04): Injector Fuel Diaphragm Stem · Lycoming Engines AEIO-540-L1B5D, IO-540-AA1A5, IO-540-G1B5 and 30 more. Effective Nov 4, 1983
- [AD 81-12-06 R1](https://openairdocs.org/ad/81-12-06-R1): Magnetos · Bendix Magnetos, LTIO-540-J2BD and TIO-540-J2BD. Effective Nov 12, 1981
- [AD 80-17-10](https://openairdocs.org/ad/80-17-10): Transition Wastegate Assembly · Lycoming Engines TIO-540-S1AD. Effective Aug 18, 1980
- [AD 79-04-05](https://openairdocs.org/ad/79-04-05): Regulator Diaphragm Stem Assembly · Lycoming Engines AEIO-320-D1B, AEIO-320-E1A, AEIO-320-E1B and 215 more. Effective Sep 26, 1979
- [AD 79-12-07](https://openairdocs.org/ad/79-12-07): Magnetos · Bendix Magnetos, TIO-540-F2BD, TIO-540-N2BD and 3 more. Effective Jun 19, 1979
- [AD 78-23-10](https://openairdocs.org/ad/78-23-10): Center Body Bellows Seal Assembly · Lycoming Engines AEIO-320-D1B, AEIO-320-E1A, AEIO-320-E1B and 218 more. Effective Nov 7, 1978
- [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 75-09-15](https://openairdocs.org/ad/75-09-15): Fuel Starvation To The Engine · Lycoming Engines AIO-320-A1A, AIO-320-A1B, AIO-320-A2A and 130 more. Effective Apr 30, 1975
- [AD 73-10-02](https://openairdocs.org/ad/73-10-02): Bendix Fuel Injectors · Bendix Fuel Injectors, AIO-320-A1A, AIO-320-A1B and 88 more. Effective May 16, 1973
- [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

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

- [AD 2005-05-53](https://openairdocs.org/ad/2005-05-53) (historical): Flight Control System · 172R, 172S, 182T and 1 more
- [AD 2003-24-13](https://openairdocs.org/ad/2003-24-13) (historical): Honeywell KAP 140 autopilot computer system · 172R, 172S, 182S and 4 more. Effective Jan 20, 2004
- [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 2012-24-09](https://openairdocs.org/ad/2012-24-09) (historical): Turbocharger turbine wheel · Continental Motors TSIO-360-MB, TSIO-360-RB, TSIO-360-SB and 1 more. Effective Dec 20, 2012
- [AD 2011-26-04](https://openairdocs.org/ad/2011-26-04) (historical): Externally mounted fuel injector fuel lines · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 186 more. Effective Jan 25, 2012
- [AD 2011-15-10](https://openairdocs.org/ad/2011-15-10) (historical): Fuel servos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 256 more. Effective Aug 16, 2011
- [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 2008-14-07](https://openairdocs.org/ad/2008-14-07) (historical): Externally mounted fuel injector fuel lines · Textron Lycoming, AVCO AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 185 more. Effective Aug 14, 2008
- [AD 2008-08-14](https://openairdocs.org/ad/2008-08-14) (historical): Fuel injection servo plugs · Superior Air Parts AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 242 more. Effective Apr 29, 2008
- [AD 2008-06-51](https://openairdocs.org/ad/2008-06-51) (historical): Fuel injection servo plugs · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 235 more
- [AD 2006-20-09](https://openairdocs.org/ad/2006-20-09) (historical): Certain crankshafts replacing · Lycoming Engines AEIO-360-A1B6, AEIO-360-A1E6, AEIO-540-D4A5 and 82 more. Effective Nov 3, 2006
- [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 2002-26-01](https://openairdocs.org/ad/2002-26-01) (historical): Fuel injector fuel lines · Textron Lycoming, AVCO IGO-480-A1B6, IGO-540-B1A, IGO-540-B1C and 178 more. Effective Jan 31, 2003
- [AD 2002-23-06](https://openairdocs.org/ad/2002-23-06) (historical): Crankshaft gear retaining bolts · Textron Lycoming, AVCO AEIO-540, AEIO-540-D4A5, AEIO-540-D4B5 and 46 more. Effective Nov 19, 2002
- [AD 2002-20-51](https://openairdocs.org/ad/2002-20-51) (historical): Crankshaft gear retaining bolts · Textron Lycoming, AVCO AEIO-540, IO-540 Series (all), LTIO-540-F2BD and 39 more
- [AD 2002-17-53](https://openairdocs.org/ad/2002-17-53) (historical): Crankshaft · Lycoming Engines LTIO-540-F2BD, LTIO-540-J2B, LTIO-540-J2BD and 36 more
- [AD 2002-04-51](https://openairdocs.org/ad/2002-04-51) (historical): Crankshaft · Lycoming Engines LTIO-540-F2BD, LTIO-540-J2B, LTIO-540-J2BD and 8 more
- [AD 98-18-12](https://openairdocs.org/ad/98-18-12) (historical): Fuel Pump · Textron Lycoming, AVCO AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 249 more. Effective Sep 28, 1998
- [AD 93-05-22](https://openairdocs.org/ad/93-05-22) (historical): Fuel Injector Fuel Lines · Lycoming Engines TIO-540-S1AD. Effective May 11, 1993
- [AD 92-12-10](https://openairdocs.org/ad/92-12-10) (historical): Lycoming Engines TIO-540-S1AD. Effective Jun 5, 1992
- [AD 71-13-01](https://openairdocs.org/ad/71-13-01) (historical): Fuel Injector Manifold To Nozzle Tube Assemblies · Lycoming Engines TIO-540-A1A, TIO-540-A1B, TIO-540-A1C and 3 more. Effective Jun 22, 1971

## Information bulletins (advisory) (17 in force)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-12-41](https://openairdocs.org/saib/CE-12-41): Flight Controls  Loose Glide Screw. Issued Aug 9, 2012
- [SAIB CE-12-15](https://openairdocs.org/saib/CE-12-15): DC Power Distribution System - Avionics Master Switch. Issued Jan 30, 2012
- [SAIB CE-10-40R1](https://openairdocs.org/saib/CE-10-40R1): Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanes. Issued Jul 30, 2010
- [SAIB CE-09-12](https://openairdocs.org/saib/CE-09-12): Navigation: CRS/BARO Knob Interference in some G1000/G900X/G950 Installations. Issued Feb 11, 2009
- [SAIB CE-09-10](https://openairdocs.org/saib/CE-09-10): Availability of Secondary Seat Stops for Pilot and Copilot Seats. Issued Feb 5, 2009
- [SAIB CE-09-01](https://openairdocs.org/saib/CE-09-01): Equipment - Emergency. Issued Oct 21, 2008
- [SAIB CE-08-02](https://openairdocs.org/saib/CE-08-02): Flight Controls. Issued Nov 2, 2007
- [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-08-26R3](https://openairdocs.org/saib/NE-08-26R3): Magneto/Distributor. Issued Mar 31, 2011
- [SAIB NE-09-04](https://openairdocs.org/saib/NE-09-04): Fuel Control/Reciprocating Engines. Issued Jan 10, 2009
- [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-03-12](https://openairdocs.org/saib/NE-03-12): . Issued Dec 30, 2002
- [SAIB NE-01-37](https://openairdocs.org/saib/NE-01-37): . Issued Aug 16, 2001
- [SAIB CE-19-01](https://openairdocs.org/saib/CE-19-01) (historical): Engine Oil and Airplane Hour Meter; Pressure Switch Failure. Issued Feb 12, 2019
- [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

## NTSB investigations

None matched to N728AA.

## FAA accident and incident reports

None matched to N728AA.

## Reports on N728AA not matched to an aircraft (1)

They name N728AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19921218055209I](https://openairdocs.org/incident/19921218055209I), Dec 18, 1992: Boeing 727227 (N728AA), Rochester, NY. Experienced right gear warning light on rollout. Landing gear was pinned fefore taxiing to gate.

## 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 N728AA not matched to an aircraft (72, newest 50)

They name N728AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR AALA20012071](https://openairdocs.org/sdr/AALA20012071), Nov 26, 2001: LIGHT. INOPERATIVE. DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT VENTRAL AFT STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL
- [SDR AALA20011978](https://openairdocs.org/sdr/AALA20011978), Nov 2, 2001: BATTERY. CORRODED. ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONNECTION. SYSTEM GROUND CHECKED NO
- [SDR AALA20011149A](https://openairdocs.org/sdr/AALA20011149A), May 22, 2001: SPAR. CORRODED. TUL - FOUND RIGHT WING FORWARD SPAR CORRODED AT LOWER CHORD 8 INCHES INBOARD OF DEFUEL VALVE BELOW NR 4 L/E FLAP ACT MOUNT. CUT OUT DAMAGED MATERIAL AND INSTALL
- [SDR AALA20011147](https://openairdocs.org/sdr/AALA20011147), May 22, 2001: SPLICE. CRACKED. TUL - FOUND STRINGER SPLICE CRACKED. REMOVED AND REPLACED STRINGER SPLICE. (M)
- [SDR AALA2001148](https://openairdocs.org/sdr/AALA2001148), May 22, 2001: WEB. CORRODED. TUL - FOUND LEFT HORIZONTAL WALKWAY CORRODED 9 INCHES BY 3 INCHES UNDERSIDE BETWEEN STATION 303 TO 312. REMOVED CORRODED AREA OF WALKWAY. INSTALLED DOUBLER PER 
- [SDR AALA20011149](https://openairdocs.org/sdr/AALA20011149), May 22, 2001: STRAP. CORRODED. TUL - FOUND CORROSION 4 INCHES BY 12 INCHES, ON BUTT SPLICE STRAP AT STATION 680, BETWEEN 28L AND 28R. REMOVED CORRODED STRAP AND INSTALLED NEW STRAP. (M)
- [SDR AALA20011152](https://openairdocs.org/sdr/AALA20011152), May 22, 2001: SKIN. CORRODED. TUL - FOUND FASTENER HEAD DISHED FUSE SKIN STATION 680 STRINGER 28R AND SKIN CORRODED. CUT OUT CORRODED AREA INSTALLED FILLER AND DOUBLER PER SRM 53-30-3. (M)
- [SDR AALA20011150](https://openairdocs.org/sdr/AALA20011150), May 22, 2001: BRACKET. TUL - FOUND THROTTLE CONTROL DRUM MOUNT BRACKET CRACKED UPPER END, NR 3 ENGINE. REPAIRED CRACK IN CONTROL DRUM MOUNT BRACKET PER ESO 11697 DATED 5-21-01 AND SRM
- [SDR AALA20011151](https://openairdocs.org/sdr/AALA20011151), May 21, 2001: PAN. CORRODED. TUL - FOUND CORROSION 2 INCHES BY 8 INCHES ON LOWER SIDE OF LAVATORY FLOOR PAN AND DOUBLER STATION 1164-1178 AT LBL 24-28. CUT OUT DAMAGED AREA INSTALLED FILLER
- [SDR AALA20011153](https://openairdocs.org/sdr/AALA20011153), May 18, 2001: SKIN. CRACKED. TUL - FOUND CRACK IN FUSELAGE SKIN AT STATION 720A AND 19 BL 0. INSTALLED DOUBLER PER 53-30-03 PART 1 PAGE 5-8. (M)
- [SDR AALA20010973](https://openairdocs.org/sdr/AALA20010973), May 10, 2001: LIGHT. INOPERATIVE. DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE. REPLACED AFT AIRSTAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND C
- [SDR AALA20010524](https://openairdocs.org/sdr/AALA20010524), Mar 16, 2001: LIGHT. DEFECTIVE. DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR DIM. REPLACED EMERGENCY EXIT LIGHT AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20000813](https://openairdocs.org/sdr/AALA20000813), May 20, 2000: LIGHT. INOPERATIVE. MIA - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY LIGHT BY REAR EXIT DOES NOT ILLUMINATE DURING TEST. REPLACED OVERHEAD EMERGENCY LIGHT BY REAR EXIT. SYSTE
- [SDR AALA2000818](https://openairdocs.org/sdr/AALA2000818), May 16, 2000: FRAME. CRACKED. TUL - FOUND STATIO 720D BELL FRAME CRACKED AT INBOARD UPPER RADIUS OF CUTOUT FOR STRINGER 26L. STOP DRILLED CRACK INSTALLED TYPICAL WEB REPAIR PER SRM 51-40-2. 
- [SDR AALA2000817](https://openairdocs.org/sdr/AALA2000817), May 16, 2000: FRAME. CRACKED. TUL - FOUND BELL FRAME CRACKED UPPER FORWARD RADIUS STATION 720D ABOVE STRINGER 26 RT. INSTALLED DOUBLER PER SRM 51-40-3 FROM 7075-T6 .071 INCH USING 3 ROW OF .
- [SDR AALA2000816](https://openairdocs.org/sdr/AALA2000816), May 16, 2000: SKIN. CORRODED. TUL - FOUND SKIN LAP 26R CORRODED ON OUTBOARD SIDE OF STRINGER 26R STATION 720C-D. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AFTER REMOVAL OF CORRODED 
- [SDR AALA2000815](https://openairdocs.org/sdr/AALA2000815), May 16, 2000: DOOR FRAME. CORRODED. TUL - FOUND LOWER CARGO DOOR FRAME CORRODED AT STATION 950E AFT SIDE OF BELL FRAME. FABRICATED AND INSTALLED FRAME REPAIR AND STRAP PER SRM 51-00-3. (M)
- [SDR AALA2000819](https://openairdocs.org/sdr/AALA2000819), May 15, 2000: STIFFENER. CORRODED. TUL - FOUND CORROSION ON VERTICAL STIFFENER AT GROUND WIRES JUST OUTBOARD OF NR 5 LEADING EDGE FLAP ACTUATOR. REMOVED AND REPLACED FRONT SPAR VERT STIFFENER SRM
- [SDR AALA20000548](https://openairdocs.org/sdr/AALA20000548), Mar 26, 2000: WIRE. BROKEN. DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE LIGHTS BETWEEN FIRST CLASS AND COACH INOPERATIVE. REPAIRED BROKEN WIRE BETWEEN FIRST CLASS AND COACH. 
- [SDR AALA20000448](https://openairdocs.org/sdr/AALA20000448), Mar 10, 2000: ACCESSORY UNIT. MALFUNCTIONED. MIA - FLT 1880 - AFTER TAKEOFF, LEFT GEAR WARNING LIGHT (RED) REMAINED ILLUMINATED. RECYCLED TWICE AND REMAINED ILLUMINATED. RETURNED AND LANDED MIA WITHOUT INC
- [SDR AALA991676](https://openairdocs.org/sdr/AALA991676), Nov 8, 1999: ENGINE. MALFUNCTIONED. CCS - FLT 2140 - EN ROUTE CCS/MIA - NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED DURING CLIMB. WOULD NOT EXTINGUISH. AIRCRAFT RETURNED TO CCS AND LANDED WITHOUT
- [SDR AALA991002](https://openairdocs.org/sdr/AALA991002), Jul 8, 1999: FRAME. CRACKED. TUL - HFEC INDICATES CRACK IN NR 2 CARGO DOOR FORWARD FUSELAGE FRAME WEB INBOARD OF LOWER STOP FITTING. STOP DRILLED CRACK, HFEC AROUND STOP DRILL, NO FURTHER C
- [SDR AALA991005](https://openairdocs.org/sdr/AALA991005), Jul 6, 1999: STRINGER. CORRODED. TUL - FOUND STRINGER 28L CORRODED AT PRODUCTION SPLICE, BS 675. REMOVED CORROSION DAMAGED PORTION OF STRINGER 28L AND INSTALLED STRINGER REPAIR SPLICE PER SRM 5
- [SDR AALA991003](https://openairdocs.org/sdr/AALA991003), Jul 6, 1999: SKIN. CRACKED. TUL - FOUND CRACK IN FUSELAGE SKIN AT RIVET LOCATED BS 251.9 AND STRINGER 22L. REMOVED RIVET, CONFIRMED CRACK WITH HFEC. REMOVED 1 INCH DIAMETER AREA OF SKIN TO
- [SDR AALA991004](https://openairdocs.org/sdr/AALA991004), Jun 28, 1999: FRAME. CRACKED. TUL - FRAME CRACKED ON WEB AT STRINGER CUTOUT STATION 480, STRINGER 27R. INSTALLED WEB REPAIR PER SRM 51-40-2. (M)
- [SDR AALA990669](https://openairdocs.org/sdr/AALA990669), May 5, 1999: LAMP. DEFECTIVE. MCO - FLT 478 - AFTER TAKEOFF, RIGHT MAIN GEAR RED UNSAFE LIGHT ILLUMINATED INTERMITTENTLY. LANDED MCO WITHOUT INCIDENT. RELAMPED RIGHT MAIN GEAR INDICATION MOD
- [SDR AALA990042](https://openairdocs.org/sdr/AALA990042), Jan 8, 1999: AIR DISTR. SMOKE. KIN - FLT 1504 - EN ROUTE KIN-MIA, FLIGHT ATTENDANT NOTICED SMOKE IN AFT AIRCRAFT AND AFT GALLEY AREA. SMOKE SMELLED ELECTRICAL, TURNED OFF OVENS 3 AND 4, CIRCU
- [SDR AALA981261](https://openairdocs.org/sdr/AALA981261), Jun 19, 1998: STRINGER. CORRODED. TUL - FOUND HEAVY CORROSION ON STRINGER 27L AT STATION 560. INSTALLED NEW STRINGER SECTION AND 2 DOUBLERS PER SRM. (M)
- [SDR AALA981260](https://openairdocs.org/sdr/AALA981260), Jun 19, 1998: FRAME. DENTED. TUL - FOUND BELL FRAME DENTED STATION 660 BETWEEN STRINGER 24R AND 25R. INSTALLED DOUBLER PER SRM 53-10-4 PAGE 5. (M)
- [SDR AALA981259](https://openairdocs.org/sdr/AALA981259), Jun 19, 1998: ANGLE. CORRODED. TUL - FOUND CORROSION ON TOP OF CREASE ANGLE RBL 55, FS 360 TO 445. REMOVED AND REPLACED WITH NEW CREASE ANGLE PER SRM 51-10-1. (M)
- [SDR AALA981249](https://openairdocs.org/sdr/AALA981249), Jun 19, 1998: SKIN. CORRODED. TUL - CORROSION ALONG DOME NUT. STA 720B TO STA 720C. CUT OUT CORROSION AND INSTALLED FLUSH REPAIR PER 53-30-3. TST: 68,331. CYCLES: 45,099. (X)
- [SDR AALA981246](https://openairdocs.org/sdr/AALA981246), Jun 19, 1998: STRINGER. CRACKED. TUL - STR 15L CRACKED JUST AFT OF ICE LIGHT. REPAIRED PER SRM 53-10-3 FIG 5. FINISHED INSTALLING FASTENERS. TST: 68,331. CYCLES: 45,099. (X)
- [SDR AALA981244](https://openairdocs.org/sdr/AALA981244), Jun 19, 1998: FRAME. DENTED. TUL - FOUND BELL FRAME HAS 3 DEEP DENTS ON TOP OF FRAME BETWEEN STRINGER 22L AND 25L AT STATION 500 FWD WEB OF FRAME DISTORTED. INSTALLED BELL FRAME REPAIR PER 
- [SDR AALA981241](https://openairdocs.org/sdr/AALA981241), Jun 19, 1998: STRINGER. CORRODED. TUL - FOUND STRINGER 28R OUTBOARD LEG CORRODED AT STATION 720C. INSTALLED A FILLER AND STRAP WITH SEALANT AND HI-LOKS PER ESO 11697, DATED 6/3/98. (M)
- [SDR AALA981240](https://openairdocs.org/sdr/AALA981240), Jun 19, 1998: FLOORBEAM. CORRODED. TUL - HEAVY CORROSION ON TOP OF FLOORBEAM RBL 55 TO 62, STATION 460. TOP CAP OF FLOORBEAM RBL 55 TO 62. REMOVED FLOORBEAM, REPAIR PERFORMED PER 53-10-8 PAGE 9A.
- [SDR AALA981239](https://openairdocs.org/sdr/AALA981239), Jun 19, 1998: STRINGER. CORRODED. TUL - FOUND STRINGER 19R AT FS 474 HEAVILY CORRODED. CUTOUT CORRODED AREA AND INSTALLED REPAIR PER SRM 53-10-34 AND 51-10-2. (M)
- [SDR AALA981238](https://openairdocs.org/sdr/AALA981238), Jun 19, 1998: STRINGER. CRACKED. TUL - FOUND STRINGER 15R CRACKED JUST FWD OF ICE LIGHT. FINISHED DRILLING PARTS, ALODINED, PRIMED SEALED PARTS AND INSTALLED PER SRM 53-10-3 FIG 5, PAGE 12. (M)
- [SDR AALA981236](https://openairdocs.org/sdr/AALA981236), Jun 19, 1998: FRAME. DENTED. TUL - BELTFRAME DENTED AT STATION 700 BETWEEN STRINGER 24L AND 23L, FORWARD WEB OF FRAME DISTORTED. INSTALLED DOUBLER OVER DAMAGE CUTOUT ON BELTFRAME AT STATION
- [SDR AALA981235](https://openairdocs.org/sdr/AALA981235), Jun 19, 1998: SPLICE. GOUGED. TUL - BELL FRAME SPLICE HAS DEEP GOUGE AT STATION 700 BETWEEN STRINGER 25R AND STRINGER 21R. REMOVED AND REPLACED SPLICE PER SRM 53-10-4. (M)
- [SDR AALA981234](https://openairdocs.org/sdr/AALA981234), Jun 19, 1998: FRAME. DENTED. TUL - BELL FRAME DENTED AT STATION 680 BETWEEN STRINGER 24R AND STRINGER 23R. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-4. (M)
- [SDR AALA981233](https://openairdocs.org/sdr/AALA981233), Jun 19, 1998: FRAME. DENTED. TUL - BELL FRAME DENT AND FORWARD WEB DISTORTED AT STATION 700, BETWEEN STRINGER23R AND 24R. CUT OUT DAMAGED INSTALLED FRAME REPAIR PER 53-10-4. (M)
- [SDR AALA981232](https://openairdocs.org/sdr/AALA981232), Jun 19, 1998: FRAME. DENTED. TUL - FOUND BELL FRAME DENTED STATION 620 BETWEEN STRINGER 25L AND 24L. REPAIRED BELL FRAME PER SRM 53-10-4. (M)
- [SDR AALA981231](https://openairdocs.org/sdr/AALA981231), Jun 19, 1998: FRAME. CRACKED. TUL - STATION 380 BELL FRAME CRACKED AT HORIZONTAL DOOR FRAME STIFFENER ATTACH POINT HI-LOK, STRINGER 20R. INSTALLED DOUBLER AND FILLER AND FASTENERS PER SRM 53
- [SDR AALA981230](https://openairdocs.org/sdr/AALA981230), Jun 19, 1998: BULKHEAD. CRACKED. TUL - STATION 1183 BULKHEAD CRACKED LBL 35, WL 188 BELOW LEFT CENTER DUCT CUTOUT. REPAIRED BULKHEAD PER BOEING SB 727-53-0217, DOUBLER/TRIPLER WITH HI-LOKS. (M)
- [SDR AALA981229](https://openairdocs.org/sdr/AALA981229), Jun 19, 1998: SKIN. CORRODED. TUL - FOUND CORROSION BULGING BETWEEN EXT SKIN AND LAV SVC PAN AT AFT LAV PANEL ACCESS DOOR. REMOVED LAV PAN, REMOVED CORROSION PER 51-10-6. REPLACED PAN SUPPOR
- [SDR AALA981228](https://openairdocs.org/sdr/AALA981228), Jun 19, 1998: BULKHEAD. CRACKED. TUL - LEFT WING TIP BULKHEAD CRACKED, UPPER FLANGE AT 3 RIVETS, OUTBOARD SIDE PANEL VENT BOX. REPAIRED LT BULKHEAD UPPER FLAGNE CRACKS AT 3 RIVETS PER SRM 51-40
- [SDR AALA981227](https://openairdocs.org/sdr/AALA981227), Jun 19, 1998: FRAME. CRACKED. TUL - BELL FRAME CRACKED UNDER UPPER FLANGE AT FS STATION 500 BETWEEN STRINGER 21R AND 22R. INSTALLED DOUBLER AND FILLR PER SRM 51-40-3. (M)
- [SDR AALA981226](https://openairdocs.org/sdr/AALA981226), Jun 19, 1998: FRAME. DENTED. BELL FRAME DENTED AND FWD WEB DISTORTED AT STATION FS 500 BETWEEN STRINGER 24R AND 25R. INSTALLED DOUBLER AND FILLER PER SRM 51-40-3 FIG 1 SHT 3. (M)
- [SDR AALA981225](https://openairdocs.org/sdr/AALA981225), Jun 19, 1998: BEAM. CORRODED. FOUND CORROSION ON BOTTOM AND INSIDE OF DELTA BEAM FS 740 TO FS 780, LBL 7 TO RBL 7. REMOVED CORROSION, TREATED AND PRIMED PER ESO 11697. (M)
- [SDR AALA981224](https://openairdocs.org/sdr/AALA981224), Jun 19, 1998: HOUSING. CORRODED. TUL - FOUND CORROSION AROUND FASTENERS ON ICE LIGHT HOUSING, STATION 720B TO 720C BETWEEN STRINGER 14R AND STRINGER 16R. INSTALLED NEW ICE LIGHT HOUSING AND SEA

All 72: https://openairdocs.org/aircraft/N728AA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (337, 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 (Cessna T182T)

- [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 SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc
- [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 SA04439NY](https://openairdocs.org/stc/SA04439NY): Installation of an X cam Pod. J & C Engineering Services LTD
- [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 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 SA02266AK](https://openairdocs.org/stc/SA02266AK): Replacement of Rudder and Elevator Hinge Bearings with P. Ponk Aviation Bearing p/n PPA-1401. McFarlane Aviation LLC
- [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. Alcor LLC
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [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 SA02006CH](https://openairdocs.org/stc/SA02006CH): Installation of air conditioning system. Kelly Aerospace Thermal Systems LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA01105DE](https://openairdocs.org/stc/SA01105DE): Installation of the Persistent Systems MPU5 Wave Radio System. Persistent Systems
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc
- [STC SA02576AK](https://openairdocs.org/stc/SA02576AK): Installation of Cleveland and ABI, LLC Wheel and Brake Kits. ABI LLC
- [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 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 SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA3-44](https://openairdocs.org/stc/SA3-44): Installation of model AWB-2500A(aircraft skis) main and AWN-1200 nose wheel-skis. ee Dodge Aircraft Services. Lists 182 Series
- [STC SA00673DE](https://openairdocs.org/stc/SA00673DE): Installation of B&C Specialty Standby Alternator System. Freedom Aviation Inc
- [STC SA01552WI](https://openairdocs.org/stc/SA01552WI): Installation of Supplemental Audio System, including #2 GMA 1347 Audio Panel. Yingling Aircraft Inc
- [STC SA04586CH](https://openairdocs.org/stc/SA04586CH): Installation of Electroair Back Up Battery Panel System Control. Electroair Aquisition Corp
- [STC SA950CE](https://openairdocs.org/stc/SA950CE): Installation STOL kits (wing leading edge cuffs, drooped tips, stall fences and aileron gap seals). Curry Aviation LLC
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA01830WI](https://openairdocs.org/stc/SA01830WI): G1000 Integrated Avionics System hardware and software updates including optional Flight Stream 510. Textron Aviation Inc
- [STC SA00753WI](https://openairdocs.org/stc/SA00753WI): Installation of the Concorde VRSLA (RG-24-15, RG-24-16, RG-35AXC and RG-35A) batteries. Aero-Mach Wilco LLC
- [STC SA01827WI](https://openairdocs.org/stc/SA01827WI): Installation of LED Position Lights. Aero-Mach Wilco LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [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 SA00026IB](https://openairdocs.org/stc/SA00026IB): Validation for the Installation of Beringer Wheels, axles, brake and master-cylinders. Beringer Aero
- [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 SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA02553AK](https://openairdocs.org/stc/SA02553AK): Fabrication and installation of a Tail Wheel Anti-Shimmy Dampener. Keller Engineering Group LLC
- [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King)

All 337: https://openairdocs.org/aircraft/N728AA/stcs.md

## Related

- Other Cessna T182T aircraft: https://openairdocs.org/model/cessna-t182t/aircraft.md
- The Lycoming TI0-540 series engine: https://openairdocs.org/engine/lycoming-ti0-540-series.md

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