# N313AA: 2013 Cessna 172S

- Status: Valid registration
- Airframe: [Cessna 172S](https://openairdocs.org/model/cessna-172s) (registry code 2072439, 4 seats)
- Engine: [Lycoming IO-360-L2A](https://openairdocs.org/engine/lycoming-io-360-l2a) (registry code 41597)
- Data sheets: [TCDS 3A12](https://openairdocs.org/tcds/3A12) (Textron Aviation Inc.), [TCDS 1E10](https://openairdocs.org/tcds/1E10) (Lycoming Engines) (OpenAirDocs)
- Serial number: 172S11286
- Year built: 2013
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal, utility
- Airworthiness date: March 22, 2013
- Certificate issued: June 23, 2023
- Expires: June 30, 2030
- Mode S code: A351F7
- Registered owner: [Aviator Air Operations LLC](https://openairdocs.org/faa-owner/AVIATOR%20AIR%20OPERATIONS%20LLC)
- Location: [Grand Prairie, TX](https://openairdocs.org/faa-place/TX/Grand%20Prairie)
- Owner type: LLC
- Owner's area on the map: 32.6647° N, 97.0295° W: Placed by OpenAirDocs at the center of ZIP code 75052, 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=313AA
- Page: https://openairdocs.org/aircraft/N313AA

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

## ADs that may apply (OpenAirDocs): 56 in force

### Matched by airframe (Cessna 172S)

- [AD 2024-14-03](https://openairdocs.org/ad/2024-14-03): Autopilot System · Garmin GFC 500 Autopilot (STC SA01866WI). Effective Aug 20, 2024
- [AD 2023-10-02](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 2018-02-04](https://openairdocs.org/ad/2018-02-04): Exhaust Noise Suppressor · Aerospace Welding Minneapolis A1754001-23, A1754001-25, 172 and 3 more. Effective Feb 21, 2018
- [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 2013-03-15](https://openairdocs.org/ad/2013-03-15): Aircraft Fuel Distribution System · Cessna 172R and 172S. Effective Mar 19, 2013
- [AD 2012-22-01](https://openairdocs.org/ad/2012-22-01): Aircraft Fuel Distribution System · Cessna 172R and 172S. Effective Dec 28, 2012
- [AD 2012-02-02](https://openairdocs.org/ad/2012-02-02): Fuel · Cessna 172R and 172S. Effective Mar 13, 2012
- [AD 2011-06-02](https://openairdocs.org/ad/2011-06-02): Engine · TAE 125-01 Engine Installation (Technify Motors STC SA01303WI). Effective May 26, 2011
- [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 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 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 2001-06-17](https://openairdocs.org/ad/2001-06-17): Engine Idle Speed and Fuel Control Mixture Setting · Cessna 172R and 172S. Effective Apr 20, 2001
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998
- [AD 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 1998
- [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996
- [AD 90-06-03 R1](https://openairdocs.org/ad/90-06-03-R1): Exhaust Heater/Muffler Assembly · Cessna 172, 172A, 172B and 16 more. Effective Mar 27, 1991
- [AD 79-10-14 R1](https://openairdocs.org/ad/79-10-14-R1): Fuel Tank Venting · Cessna 140A, 150, 150A and 172 more. Effective May 30, 1988
- [AD 79-08-03](https://openairdocs.org/ad/79-08-03): Electrical System · Cessna 120, 140, 140A and 152 more. Effective Jun 6, 1979
- [AD 77-02-09](https://openairdocs.org/ad/77-02-09): Wing Flap System · Cessna 150, 150A, 150B and 61 more. Effective Feb 3, 1977
- [AD 74-06-02](https://openairdocs.org/ad/74-06-02): AVCON Mufflers · Lycoming 150 and160 hp Model O-320-( ) engine (Williams Robert or Barbara STC SA750CE or 3 others). Effective Mar 18, 1974
- [AD 74-04-01](https://openairdocs.org/ad/74-04-01): Aft Fuselage Bulkhead Assembly · Cessna 172, 172A, 172B and 16 more. Effective Feb 12, 1974
- [AD 73-23-07](https://openairdocs.org/ad/73-23-07): Defective Spar Attachment Fittings · Cessna 150, 150A, 150B and 68 more. Effective Nov 19, 1973
- [AD 73-17-01](https://openairdocs.org/ad/73-17-01): Fuel Transfer Pump Placard · Cessna 170, 170A, 170B and 53 more. Effective Aug 16, 1973
- [AD 71-22-02](https://openairdocs.org/ad/71-22-02): Cracks In Nose Gear Fork · Cessna 150, 150A, 150B and 52 more. Effective Nov 9, 1971
- [AD 71-18-01](https://openairdocs.org/ad/71-18-01): Fuel Selector Valve Placard · Cessna 172, 172A, 172B and 16 more. Effective Aug 31, 1971
- [AD 69-15-03](https://openairdocs.org/ad/69-15-03): Muffler Assembly · Lycoming O-320-A1A, A1B, A3A, A3B or Lycoming O-320-B1A, B1B… (D'Shannon Products STC SA135CE or 8 others). Effective Aug 20, 1969
- [AD 68-17-04](https://openairdocs.org/ad/68-17-04): Stall Warning System · Cessna 150, 150A, 150B and 63 more. Effective Sep 7, 1968

### Matched by engine (Lycoming IO-360-L2A)

- [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 2020-25-12](https://openairdocs.org/ad/2020-25-12): Reciprocating Engine Power Section · Superior Air Parts IO-360-A1A1, IO-360-A1A2, IO-360-A2A1 and 146 more. Effective Jan 15, 2021
- [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 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 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 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 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 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 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 2006-10-21](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 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 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 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 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 96-23-03](https://openairdocs.org/ad/96-23-03): High pressure fuel pumps · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 174 more. Effective Dec 23, 1996
- [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 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 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 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

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

- [AD 2008-03-02](https://openairdocs.org/ad/2008-03-02) (historical): Fuel return line assembly · Cessna 172R and 172S. Effective Mar 6, 2008
- [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 2000-04-01](https://openairdocs.org/ad/2000-04-01) (historical): Oil Pressure Switch · Cessna 172R, 172S, 182S and 2 more. Effective Mar 11, 2000
- [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 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 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 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 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) (23 in force)

- [SAIB CE-19-01 R1](https://openairdocs.org/saib/CE-19-01%20R1): Engine Oil and Airplane Hour Meter; Pressure Switch Failure. Issued Dec 6, 2022
- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-18-23](https://openairdocs.org/saib/CE-18-23): Passenger Compartment Equipment - Installation of F. Atlee Dodge Aircraft Services LLC. Folding Jump Seats. Issued Jul 19, 2018
- [SAIB CE-17-25](https://openairdocs.org/saib/CE-17-25): ELEVATOR TORQUE TUBE  Inspections for cracks and corrosion in elevator torque tubes. Issued Aug 25, 2017
- [SAIB CE-12-02R1](https://openairdocs.org/saib/CE-12-02R1): Alternative Method of Compliance to Airworthiness Directive 2001-06-17. Issued Nov 13, 2014
- [SAIB CE-12-15](https://openairdocs.org/saib/CE-12-15): DC Power Distribution System - Avionics Master Switch. Issued Jan 30, 2012
- [SAIB CE-12-03](https://openairdocs.org/saib/CE-12-03): Fuel Control; Engine Performance with the Throttle Control at Idle. Issued Oct 26, 2011
- [SAIB CE-11-37](https://openairdocs.org/saib/CE-11-37): Engine Oil: Oil Filter Interference. Issued May 31, 2011
- [SAIB CE-11-36](https://openairdocs.org/saib/CE-11-36): Flight Controls  Frayed Aileron Cables. Issued May 31, 2011
- [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-09-42](https://openairdocs.org/saib/CE-09-42): Lights - Landing Light, Beacon Light and Taxi Light Switch Applications. Issued Jul 24, 2009
- [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-01-41R2](https://openairdocs.org/saib/CE-01-41R2): Flight Controls. Issued Oct 1, 2007
- [SAIB CE-06-46R1](https://openairdocs.org/saib/CE-06-46R1): . Issued Sep 18, 2006
- [SAIB CE-02-20](https://openairdocs.org/saib/CE-02-20): . Issued Mar 14, 2002
- [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-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 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 CE-12-02](https://openairdocs.org/saib/CE-12-02) (historical): Alternative Method of Compliance to Airworthiness Directive 2001-06-17. Issued Oct 24, 2011
- [SAIB CE-10-40](https://openairdocs.org/saib/CE-10-40) (historical): Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanes. Issued Jul 27, 2010
- [SAIB CE-01-41R1](https://openairdocs.org/saib/CE-01-41R1) (historical): Cracks in plastic or non-metallic control wheels. Issued Jan 10, 2007
- [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 N313AA.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20220918022219I](https://openairdocs.org/incident/20220918022219I), Sep 18, 2022: Cessna 172S (N313AA), Grand Prairie, TX, Minor damage. During the landing phase of flight the pilot veered off the runway resulting in the propeller striking the dirt. Propeller showed signs of damage and there was…

## 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 N313AA not matched to an aircraft (34)

They name N313AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR ABXR201072000023A](https://openairdocs.org/sdr/ABXR201072000023A), Sep 16, 2008: CHECK VALVE. CRACKED. (ABXR) DURING A MX INSP EVENT, WHILE DOING AN INSP OF THE NR 1 ENG 8TH STAGE CHECK VALVE IAW AD 90-12-02 IAW SB 36-2078, REV 2, FOUND APPROX A 1 INCH CRACK IN T
- [SDR AALA20020795](https://openairdocs.org/sdr/AALA20020795), May 29, 2002: IDG. FAILED. JFK - FLT 679 - DURING TAKEOFF RECEIVED EICAS MESSAGES, RIGHT GEN OFF, RIGHT GEN DRIVE LT, AND RIGHT UTIL BUS RESET GEN DRIVE LIGHT ON STEADY. COMPLETED CHECKLI
- [SDR AALA20020834](https://openairdocs.org/sdr/AALA20020834), May 29, 2002: IDG. FAILED. JFK - FLT 679 - EN ROUTE JFK-AUA - RIGHT ENGINE IDG FAILED. RETURNED JFK LANDING WITHOUT INCIDENT. REPLACED RIGHT ID GENERATOR. PERFORMED OPERATIONS CHECKED PER
- [SDR AALA20010909](https://openairdocs.org/sdr/AALA20010909), May 3, 2001: BATTERY PACK. DISCHARGED. JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FLICKER AT ROWS 30 THROUGH 37 LEFT. REPLACED BATTERY PACK FOR ROWS 30 THROUGH 37. SYSTEM GROUND CHECKE
- [SDR AALA20010166](https://openairdocs.org/sdr/AALA20010166), Jan 30, 2001: LIGHT. DAMAGED. BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT MID GALLEY DAMAGED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT MID GALLEY. SYSTEM GROUND CHECKED NORM
- [SDR AALA20000408](https://openairdocs.org/sdr/AALA20000408), Mar 8, 2000: WIRE. DAMAGED. JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE SEAT PATH LIGHT AT ROW 35 INOPERATIVE. REPAIRED WIRE AT SEAT 35A. SYSTEM GROUND CHECK NORMAL OPERATION
- [SDR AALA991696](https://openairdocs.org/sdr/AALA991696), Nov 8, 1999: GIRT BAR. BROKEN. SFO - DURING OVERNIGHT MAINTENANCE, RIGHT SLIDE PACK RELEASE BAR BRACKETS BROKEN. REPLACED RIGHT SLIDE PACK. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA991175](https://openairdocs.org/sdr/AALA991175), Aug 14, 1999: CONNECTOR. LOOSE. MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 28B AND 32B INOPERATIVE. RESECURED CONNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHTS A
- [SDR AALA984259](https://openairdocs.org/sdr/AALA984259), Dec 14, 1998: FLOORBEAM. CORRODED. AFW - FLOORBEAM AT STATION 1480 HAS CORROSION REMOVAL ON UPPER SURFACE. BLENDED OUT CORROSION, ALODINE AND PRIMED ALL BLENDS AND REPAIR PARTS WITH 2 COATS BMS 1
- [SDR AALA981416](https://openairdocs.org/sdr/AALA981416), Jul 21, 1998: CONNECTOR. FAILED. SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT 37B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT CONNECTOR AT SEAT 37B. SYSTEM GROUND C
- [SDR AALA981283](https://openairdocs.org/sdr/AALA981283), Jun 29, 1998: COFFEE MAKER. FAILED. LHR - FLT 0046 - EN ROUTE ORD/LHR - BUSINESS CLASS NR 3 COFFEE MAKER EMITTED SMOKE. TURNED OFF COFFEE MAKER. LANDED LHR WITHOUT INCIDENT. REPLACED NR 3 COFFEE M
- [SDR AALA980094](https://openairdocs.org/sdr/AALA980094), Jan 9, 1998: FMC. FAILED. LHR - FLT 0095 - IN-FLIGHT, RIGHT FMC FAILED. REPLACED RT FMC AND RT CDU. PERFORMED CROSS-LOAD PER SIC 2900. ALL OPS AND INDICATIONS NOW NORMAL. 31334F8FF/1520.
- [SDR AALA971671](https://openairdocs.org/sdr/AALA971671), Sep 1, 1997: PIN. NEEDED RESEATED. SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 31H INOPERATIVE. RESEATED PIN AT CONNECTOR FOR EMERGENCY EXIT LIGHT AT PAX SEAT 31H. SYSTEM GROUN
- [SDR AALA971670](https://openairdocs.org/sdr/AALA971670), Sep 1, 1997: LIGHT. DEFECTIVE. SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 29H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HOUSING ASSEMBLY AT PAX SEAT 29H. SYSTEM GROUND CH
- [SDR AALA970721](https://openairdocs.org/sdr/AALA970721), Apr 10, 1997: IDG. FAILED. RIGHT GEN DRIVE LIGHT ILLUMINATED. RIGHT GEN DRIVE DISCONNECTED IN FLIGHT. PLACARDED RIGHT ENG IDG INOP PER MEL. ACCOMPLISHED MPM 24-01 ENTERED IN MIC. REMOVED 
- [SDR AALA970172](https://openairdocs.org/sdr/AALA970172), Jan 16, 1997: APU. LOW OIL. JFK - FLT 0105 - TAKEOFF + 1 HR RIGHT GEN CONT OFF LIGHT ILLUMINATED. TROUBLESHOT SYSTEM. REPLACED RIGHT IDG. ALL SYS CKS NORMAL. TAKEOFF + 4 HRS APU SHUT DOWN 
- [SDR AALA960874](https://openairdocs.org/sdr/AALA960874), Jun 7, 1996: CONNECTOR. LOOSE. SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 29AB INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR ON BACK OF LIGHT ASSEMBLY AT PAX
- [SDR AALA960243](https://openairdocs.org/sdr/AALA960243), Feb 7, 1996: WIRE. BROKEN. SFO - DURING OVERNIGHT CHECK, MID-GALLEY EMERGENCY EXIT EGRESS LIGHTS INOPERATIVE. REPAIRED BROKEN WIRES AT MID-GALLEY FOR EMERGENCY EXIT EGRESS LIGHTS. SYSTEM 
- [SDR AALA960194](https://openairdocs.org/sdr/AALA960194), Jan 24, 1996: SKIN. GOUGED. AFW - FUSELAGE SKIN GOUGED FORWARD OF LOWER FORWARD CORNER OF FORWARD CARGO DOOR CUT-OUT. BLENDED GOUGE, PARENT MATERIAL .202 INCH THICK. LOW POINT OF BLEND .14
- [SDR AALA960193](https://openairdocs.org/sdr/AALA960193), Jan 24, 1996: STRINGER. CORRODED. AFW - STRINGER CORRODED. DAMAGE REQUIRED REMOVAL OF .70 INCH OF STRINGER FORWARD OF SPLICE. REMOVED ALL CORROSION. FABRICATED AND INSTALLED REPAIR SPLICE. REPAI
- [SDR AALA960192](https://openairdocs.org/sdr/AALA960192), Jan 24, 1996: CHORD. CORRODED. AFW - FOUND AND BLENDED CORROSION IN TWO LOCATIONS ON INNER SURFACE OF FAIL-SAFE CHORD. REMOVED CORROSION. ROTO-PEENED TREATED AND PAINTED. APPROVED BY ENGINEER
- [SDR AALA960191](https://openairdocs.org/sdr/AALA960191), Jan 24, 1996: SPLICE. CORRODED. AFW - STRINGER CORRODED. DAMAGE REQUIRED REMOVAL OF .90 INCH OF STRINGER AT AFT END OF SPLICE. REMOVED CORROSION. FABRICATED AND INSTALLED NEW REPAIR SPLICE. AP
- [SDR AALA960190](https://openairdocs.org/sdr/AALA960190), Jan 24, 1996: REAR SPAR. CORRODED. AFW - FOUND AND REMOVED CORROSION ON WING BOX REAR SPAR ASSY UPPER CHORD. CORROSION ALSO REMOVED FROM UPPER SKIN AT SAME LOCATION AND LOWER CHORD TO FLOOR BEAM 
- [SDR AALA960189](https://openairdocs.org/sdr/AALA960189), Jan 24, 1996: STRINGER. CORRODED. AFW - STRINGER CORRODED. DAMAGE REQUIRED THE REMOVAL OF 2.5 INCHES OF STRINGER AT AFT END OF SPLICE. REMOVED CORROSION. FABRICATED AND INSTALLED NEW REPAIR SPLI
- [SDR AALA960188](https://openairdocs.org/sdr/AALA960188), Jan 24, 1996: SKIN. CORRODED. AFW - CORROSION REMOVED FROM CENTER WING UPPER SKIN AT AFT DRAINS LOCATIONS. APPROVED AND REPAIRED PER INSTRUCTIONS OF MRB 767-1117. TST: 42,562.49 HRS. CYCLES,
- [SDR AALA960187](https://openairdocs.org/sdr/AALA960187), Jan 24, 1996: FLOOR BEAM. CORRODED. AFW - FOUND AND REMOVED CORROSION ON FLOOR BEAM. AFTER BLENDING, FOUND BEYOND SRM LIMITS. EDDY CHECKED BLEND-OUTS. ROTO-PEENED AND REFINISHED BLENDED AREAS. APP
- [SDR AALA960186](https://openairdocs.org/sdr/AALA960186), Jan 24, 1996: FLOOR BEAM. CORRODED. AFW - FLOOR BEAM CORRODED AND BLENDED ON THE UPPER OUTER SURFACE. FOUND THE BLEND-OUT EXCEEDED SRM LIMITS. REMOVED FLOOR BEAM SECTION FROM STA 849 TO STA 878. S
- [SDR AALA960185](https://openairdocs.org/sdr/AALA960185), Jan 24, 1996: FLOOR BEAM. CORRODED. AFW - FLOOR BEAM CORRODED. AFTER BLENDING, FOUND DAMAGE BEYOND SRM LIMITS. ALODINED BLENDED AREA. FABRICATED AND INSTALLED REPAIR STOP USING .050 INCH 301 1/2 H
- [SDR AALA960184](https://openairdocs.org/sdr/AALA960184), Jan 24, 1996: CHORD. CORRODED. AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE 146T1213-11 INNER CHORD. THE BLEND-OUT EXCEEDS SRM MAXIMUM LIMITS. REFINISHED BLENDED AREA PER
- [SDR AALA960183](https://openairdocs.org/sdr/AALA960183), Jan 24, 1996: FLOOR BEAM. GOUGED. AFW - FLOOR BEAM WEB GOUGED. DAMAGE BLENDED AND FOUND BEYOND SRM LIMITS. FABRICATED AND INSTALLED .071 INCH THICK 7075-T6 DOUBLER. APPROVED BY ENGINEERING PER M
- [SDR AALA960182](https://openairdocs.org/sdr/AALA960182), Jan 24, 1996: CHORD. CORRODED. AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE INNER CHORD IN AFT CARGO. PRIMED AND FILLED BLENDED AREA. APPROVED FOR CONTINUED SERVICE WITH 
- [SDR AALA960181](https://openairdocs.org/sdr/AALA960181), Jan 24, 1996: CHORD. CORRODED. AFW - OVERSIZED EXISITNG HOLE ON CHORD TO ELIMINATE INNER GRANULAR CORROSION. INSTALLED FREEZE PLUG IN HOLE AFTER DRILLING. DRILLED NEW HOLE THROUGH FREEZE PLUG
- [SDR AALA960180](https://openairdocs.org/sdr/AALA960180), Jan 24, 1996: BULKHEAD. CORRODED. AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE MAIN CABIN PRESSURE DECK. BLEND-OUTS EXCEEDED SRM MAXIMUM LIMITS. REMOVED CORROSION, ROTO-PEEN
- [SDR AALA950514](https://openairdocs.org/sdr/AALA950514), Mar 23, 1995: EEL WIRE. BROKEN. MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FIRST CLASS GALLEY INOPERATIVE. REPLACED BROKEN/SHORTED EMERGENCY FLOOR LIGHT WIRES AT FWD FLIGHT ATTEND

## STCs that may be installed (OpenAirDocs) (351, 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 172S)

- [STC SA01233SE](https://openairdocs.org/stc/SA01233SE): Fabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assembly. ABI, LLC
- [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 SA02069AK](https://openairdocs.org/stc/SA02069AK): Fabrication and installation of the Airglas, Inc., Landes PA32-206LA Nose Fork equipped with up to a 8.50 x 6 tire. Airglas Inc
- [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 SA03932NY](https://openairdocs.org/stc/SA03932NY): Installation and maintenance of XCAM Pod on port or starboard wing strut. 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 SA12276IB](https://openairdocs.org/stc/SA12276IB): Payload System Installation. Icarus Aero Inc
- [STC SA04075CH](https://openairdocs.org/stc/SA04075CH): Installation of Dynon EFIS-D10A EAA sales kit part number 102778-000. Dynon Avionics Inc
- [STC SA02595AK](https://openairdocs.org/stc/SA02595AK): Fabrication and installation of Airglas Inc. cargo pod kit model LC172. Airglas 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 172 Series
- [STC SA01801AT](https://openairdocs.org/stc/SA01801AT): For the Cessna 172 airplane models incorporating Lycoming O-320 engines: Modification of the standard exhaust system as documented in Laminar Flow Systems Installation Instructions Document, "Laminar Flow System Extractor Exhaust System" Revision A, dated, November 20, 1998 and Technical Drawing List, Book No. PFS-B-800, dated, November 16, 1998 or per Power Flow Systems, Inc. Installation Instructions Document PFS-0058-00, Rev. A, dated October 5, 2001 and Master Drawing List, Report No. PFS-0032-00, Rev. IR, dated August 10, 2000, or later FAA approved revisions. For the Cessna 172 airplane models incorporating Lycoming O-320 ,O-360 0r IO-360 engines: Modify the standard exhaust system as document in Power Flow Systems, Inc. Installation Instructions Document PFS-13250-00, Rev B, dated, December 9, 2002 and Master Drawing list PFS-13240-00, Rev, IR, dated October 3, 2002. Power Flow Systems Inc
- [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 SA02588AK](https://openairdocs.org/stc/SA02588AK): Installation of Ground Adjustable Sensenich Composite 2G0M8S14/C76PGF Propeller. Sensenich Propeller Company
- [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 SA39CH](https://openairdocs.org/stc/SA39CH): Installation of an Amphibian Landing Gear Position Advisory System/Laser Gear Advisory System. Wipaire Inc
- [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 SA02006CH](https://openairdocs.org/stc/SA02006CH): Installation of air conditioning system. Kelly Aerospace Thermal Systems LLC
- [STC SA00871SE](https://openairdocs.org/stc/SA00871SE): Installation of cockpit sunvisors. Rosen Sunvisor 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 SA02575AK](https://openairdocs.org/stc/SA02575AK): Installation of the nose tire scraper P/N TSL-100. Aero Twin 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 SA00897WI](https://openairdocs.org/stc/SA00897WI): Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery. Aero-Mach Wilco LLC
- [STC SA01552WI](https://openairdocs.org/stc/SA01552WI): Installation of Supplemental Audio System, including #2 GMA 1347 Audio Panel. Yingling Aircraft Inc
- [STC SA00709SE](https://openairdocs.org/stc/SA00709SE): Installation of replacement control surface skin panels. Athena Aircraft, LLC
- [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 SA910CE](https://openairdocs.org/stc/SA910CE): Installation of wing leading edge cuffs, drooped tips, stall fences and Aileron gap seals. (172, 172Q LANDPLANE) (172P LANDPLANE AND FLOATPLANE). Curry Aviation LLC

All 351: https://openairdocs.org/aircraft/N313AA/stcs.md

## Related

- Other Cessna 172S aircraft: https://openairdocs.org/model/cessna-172s/aircraft.md
- The Lycoming IO-360-L2A engine: https://openairdocs.org/engine/lycoming-io-360-l2a.md

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