# N16895: 2007 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: 172S10618
- Year built: 2007
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal, utility
- Airworthiness date: October 29, 2007
- Certificate issued: December 3, 2007
- Expires: February 28, 2029
- Mode S code: A11317
- Registered owner: [Luxair LLC](https://openairdocs.org/faa-owner/LUXAIR%20LLC)
- Location: [College Station, TX](https://openairdocs.org/faa-place/TX/College%20Station)
- Owner type: LLC
- Owner's area on the map: 30.5611° N, 96.2751° W: Placed by OpenAirDocs at the center of ZIP code 77845, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16895
- Page: https://openairdocs.org/aircraft/N16895

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 N16895.

## 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 20151017019429I](https://openairdocs.org/incident/20151017019429I), Oct 17, 2015: Cessna 172S (N16895), Lake Charles, LA, Minor damage. While attemping to land requested a go around, during go around, aircraft encounted a prop strike.

## Reports on N16895 not matched to an aircraft (1)

They name N16895, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20001206023989I](https://openairdocs.org/incident/20001206023989I), Dec 6, 2000: Doug DC982 (N16895), Orlando, FL, Minor damage. (-23)On December 6, 2000, a signature flight support beltloader caused minor damage to the door sill plate and lower skin under the aft cargo pit area. A…

## 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 N16895 not matched to an aircraft (65, newest 50)

They name N16895, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR CALA0200321](https://openairdocs.org/sdr/CALA0200321), May 27, 2002: BATTERY PACK. DISCHARGED. THE OVERHEAD EMERGENCY LIGHTS AT ROW 5-9 STAYED ON WHEN POWER WAS SECURED DURING TEST. THE EMERGENCY LIGHT B5-101 BATTERY PACK WAS REMOVED AND REPLACED IAW MM 3
- [SDR CALA0200320](https://openairdocs.org/sdr/CALA0200320), May 26, 2002: WIRE. BROKEN. INSPECTION FOUND THE L-2 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE IAW STANDARD WIRING PRACTICES 20-10-03 AND OPEARTION CHECKED GOOD IAW MM 3
- [SDR CALA0200319](https://openairdocs.org/sdr/CALA0200319), May 24, 2002: SKIN. DENTED. INSPECTION FOUND FUSELAGE BELLY SKIN DENTED AT STA 1212, L29L TO L29R. THE AREA WAS REPAIRED IAW ECRA 5331-01114 AND EA 9-5330-2-A0954.
- [SDR CALA0200318](https://openairdocs.org/sdr/CALA0200318), May 24, 2002: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED IN AFT PIT AT STA 1322, RBL 29-30. REMOVED TWO INTERCOSTALS AND TWO BULKHEAD ATTACH ANGLES TO GAIN ACCESS TO FRAME. INSTALLED NE
- [SDR CALA0200317](https://openairdocs.org/sdr/CALA0200317), May 23, 2002: FRAME. CORRODED. AFT PIT STATION 1322 - 1309 AT L28 - L27 FRAME CORRODED. REMOVED FABRICATED AND REINSTALLED FRAME PER SRM 53-01 FIG1, 51-30-2, 51-30-5, AND 51-10-03.
- [SDR CALA0200316](https://openairdocs.org/sdr/CALA0200316), May 23, 2002: WEB. CORRODED. L2 DOORWAY CUSP WEB CORRODED LBL 44 TO LBL 54 AT STATION FS 1168. REMOVED AND REPLACED WEB AND STIFFENER PER SRM 51-30-2 AND 51-30-5.
- [SDR CALA0200315](https://openairdocs.org/sdr/CALA0200315), May 23, 2002: WEB. CORRODED. AFT PIT WEB CORRODED AT STATION 1322 - 1309 R28 - R27. REMOVED, FABRICATED AND REINSTALLED INTERCOSTAL PER SRM 51-30-5 AND 51-30-2.
- [SDR CALA0200312](https://openairdocs.org/sdr/CALA0200312), May 21, 2002: TRIM TAB. GOUGED. RIGHT AILERON CONTROL TAB UPPER SURFACE GOUGED. REMOVED, REPAIRED, AND BALANCED CONTROL TAB PER MM 27-10-02, SRM 51-70-1, AND SRM 57-50-1. REINSTALLED PER MM 27
- [SDR CALA0200311](https://openairdocs.org/sdr/CALA0200311), May 21, 2002: SKIN. DENTED. LEFT ELEVATOR LOWER SKIN DENTED. REMOVED ELEVATOR, REPAIRED AND BALANCED PER SRM 55-03 FIG 14, 55-20-2. REINSTALLED PER MM 27-30-02 AND 27-30-00.
- [SDR CALA0200310](https://openairdocs.org/sdr/CALA0200310), May 20, 2002: FRAME. CHAFED. TAIL COMPARTMENT STATION 1401 AT LONGERON 21 R FRAME HAS DEEP CHAFE. BLENDED DAMAGE AND INSTALLED REPAIR PER SRM 51-30-2, 51-30-5, AND 53-03 FIG 4.
- [SDR CALA0200309](https://openairdocs.org/sdr/CALA0200309), May 20, 2002: FRAME. CHAFED. AFT ACCESSORY COMPARTMENT FRAME AT STATION 1380 LEFT SIDE HAS CHAFED FRAME WEB. CUT OUT DAMAGED AREA OF WEB, FABRICATED AND INSTALLED REPAIR PER SRM 53-01 FIG 9
- [SDR CALA0200308](https://openairdocs.org/sdr/CALA0200308), May 20, 2002: RIB DOUBLER. CRACKED. HORIZONTAL STABILIZER RIGHT INBOARD LEADING EDGE OF ELEVATOR INTERNAL RIB DOUBLER CRACKED BELOW DUCT COUPLING. REMOVED AND REPLACED RIB DOUBLER PER SRM 51-30-2.
- [SDR CALA0200302](https://openairdocs.org/sdr/CALA0200302), May 20, 2002: SEAT TRACK. CORRODED. LEFT OUTBOARD SEAT TRACK HAS EXFOLIATION CORROSION STATION 1174 TO 1309. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-5 AND 51-30-1.
- [SDR CALA0200304](https://openairdocs.org/sdr/CALA0200304), May 17, 2002: INTERCOSTAL. CORRODED. AFT PIT F/S 1136 TO 1155 LONGERON 30 INTERCOSTAL CORRODED. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-5.
- [SDR CALA0200303](https://openairdocs.org/sdr/CALA0200303), May 17, 2002: SEAT TRACK. WORN. FIRST OFFICER UPPER AND LOWER SEAT TRACK WORN. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-1, 51-30-2, AND 51-10-4.
- [SDR CALA2000292](https://openairdocs.org/sdr/CALA2000292), May 16, 2002: INTERCOSTAL. F/S 1212 LONGERON 28 RIGHT INTERCOATAL CORRODED 1"X1". INSTALLED NEW INTERCOSTAL IAW SRM 51-30-5.
- [SDR CALA2000291](https://openairdocs.org/sdr/CALA2000291), May 15, 2002: INTERCOSTAL. F/S 1193 LONGERON 28 RIGHT INTERCOSTAL CORRODED 20"X1". INSTALLED NEW INTERCOSTAL T & L ANGLES IAW SRM 51-30-5.
- [SDR CALA2000290](https://openairdocs.org/sdr/CALA2000290), May 15, 2002: FRAME. AFT PIT, F/S 1041, LONGERON 30 FRAME ATTACH ANGLE CORRODED - 80". REPLACED FRAME ANGLE IAW SRM 51-30-5.
- [SDR CALA2000289](https://openairdocs.org/sdr/CALA2000289), May 15, 2002: FRAME. TAIL COMPARTMENT RH SIDE STA 1446 AT LONGERON 18R FRAME HAS DEEP 1"X1" CHAFE. INSTALLED ANGLE AND FILLER IAW SRM 51-30-5, 51-30-2, 51-70-5, FIG 1.
- [SDR CALA2000284](https://openairdocs.org/sdr/CALA2000284), May 13, 2002: SKIN. CHAFED. MID CARGO DOOR LOWER AFT CORNER SKIN CHAFED. INSTALLED DOUBLER IAW SRM 51-30-1 AND 51-30-5.
- [SDR CALA2000283](https://openairdocs.org/sdr/CALA2000283), May 13, 2002: SKIN. SKIN DAMAGED AFT OF PITOT TUBE AT STA 76 R/S FWD OF COCKPIT WINDOW 3"X4". INSTALLED CLASS II REPAIR IAW SRM 53-04 FIG 12B.
- [SDR CALA2000282](https://openairdocs.org/sdr/CALA2000282), May 13, 2002: SKIN. DENTED. MID CARGO DOOR, OUTER SKIN HAS A SHARP DENT. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-2, 52-05, FIG 1.
- [SDR CALA2000281](https://openairdocs.org/sdr/CALA2000281), May 13, 2002: FRAME. CHAFED. TAIL COMPARTMENT STA 1418 AT LONGERON 15R FRAME HAS DEEP CHAFE. INSTALLED REPAIR AND SHIMS IAW SRM 51-30-2, 51-30-5, 53-03, FIG 4.
- [SDR CALA2000270](https://openairdocs.org/sdr/CALA2000270), May 9, 2002: WEB. CUSP WEB L/S AFT OF L-2 DOOR IS CORRODED 20"X38". REMOVED WEB IAW SRM 53-01. INSTALLED WEB IAW SRM 51-30-2 & 51-30-5, 53-01 FIG 1.
- [SDR CALA2000269](https://openairdocs.org/sdr/CALA2000269), May 9, 2002: SHEAR TIE. AFT PIT F/S 1193 LONGERON 30 SHEAR TIE IS CORRODED 0.5 INCHES. REMOVED AND REINSTALLED NEW SHEAR TIE IAW SRM 51-30-2.
- [SDR CALA2000268](https://openairdocs.org/sdr/CALA2000268), May 9, 2002: SEAT TRACK. SEAT TRACK AT F/S 390 RH O/B IS HEAVILY CORRODED APPROXIMATELY 4"X19'. REMOVED AND REINSTALLED AIR GRILL F/S 200-484 RH O/B IAW SRM 51-30-1. REMOVED AND REINSTA
- [SDR CALA2000265](https://openairdocs.org/sdr/CALA2000265), May 7, 2002: SEAT TRACK. CABIN FLOOR SEAT TRACK RBL 24 F/S 984 AND 1003 HAS SURFACE CORROSION. REMOVED SEAT RACK FROM STA 789-1032 RBL24 IAW SRM 51-30-5 AND INSTALLED NEW TRACK IAW SRM 
- [SDR CALA2000264](https://openairdocs.org/sdr/CALA2000264), May 7, 2002: SKIN. ONE INCH DENT AT F/S 237, 17L-18L. REF. NON ROUTINE 4684047, REPAIRED DENT AT STA 229 PER ECRA 5330-03055.
- [SDR CALA2000263](https://openairdocs.org/sdr/CALA2000263), May 7, 2002: SKIN. RIGHT FORWARD FUSELAGE SKIN HAS 2" CREASE BETWEEN LONGERON 25 & LONGERON 26 AT APPROXIMATELY F/S 141. CUT OUT DAMAGE IAW SRM53-04 FIG 38, SHEET 34. INSTALLED RE
- [SDR CALA2000262](https://openairdocs.org/sdr/CALA2000262), May 7, 2002: SEAT TRACK. CAPTAINS UPPER AND LOWER SEAT TRACKS WORN, REPAIRED AND REINSTALLED TRACKS IAW SRM 51-30-1 & 53-40-01.
- [SDR CALA2000261](https://openairdocs.org/sdr/CALA2000261), May 7, 2002: INTERCOSTAL. AFT PIT F/S 1146 TO 1155 BETWEEN LONGERON 30 & 29R INTERCOSTAL CORROSION 10 INCHES LONG. REMOVED INTERCOSTAL IAW SRM 51-30-2 AND 51-30-5. REPLACED INTERCOSTAL I
- [SDR CALA2000457](https://openairdocs.org/sdr/CALA2000457), May 6, 2002: SHEAR TIE. AFT PIT, F/S 1212 LONGERON 30 SHEAR TIE HAS 3 INCHES OF CORROSION. REMOVED SHEAR TIE IAW SRM 51-30-2. INSTALLED NEW SHEAR TIE IAW SRM 51-30-2.
- [SDR CALA2000259](https://openairdocs.org/sdr/CALA2000259), May 6, 2002: SHEAR TIE. F/S 1309 BETWEEN LONGERON 14R AND 15R SHEAR TIE IS CRACKED 12 INCHES. REMOVED OUTER CHORD DOUBLER AND SHEAR TIE IAW SRM 51-30-4 AND 51-30-5. INSTALLLED SHEAR TI
- [SDR CALA2000258](https://openairdocs.org/sdr/CALA2000258), May 6, 2002: SHEAR TIE. F/S 1309 BETWEEN LONGERON 41L AND 15L SHEAR TIE IS CRACKED 12 INCHES. REMOVED OUTER CHORD, DOUBLER AND SHEAR TIE IAW SRM 51-10-4 AND SRM 51-31-1. INSTALLED NEW 
- [SDR CALA0200256](https://openairdocs.org/sdr/CALA0200256), May 1, 2002: WEB. CORRODED. CUSP WEB IS CRACKED AND CORRODED AT STA 218 L18R RBL 56. CUT OUT CORRODED AREA IAW SRM 53-01, FIG 4. FABRICATED NEW DOUBLER IAW SRM 55-14-2 AND 53-01, FIG 4. IN
- [SDR CALA0200253](https://openairdocs.org/sdr/CALA0200253), Apr 29, 2002: SKIN. DAMAGED. INSPECTION FOUND A CREASE IN FUSELAGE SKIN AT STA 218 BETWEEN STRINGER 16R AND 17R. THE CREASED AREA WAS REMOVED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALL
- [SDR CALA0200252](https://openairdocs.org/sdr/CALA0200252), Apr 29, 2002: SKIN. DAMAGED. INSPECTION FOUND A CREASE IN FUSELAGE SKIN AT STA 420 AND 446 BETWEEN STRINGER 22L AND 23L. THE CREASED AREAS WERE CUT OUT IAW SRM 53-04, FIGURE 38. A DOUBLER, 
- [SDR CALA0200251](https://openairdocs.org/sdr/CALA0200251), Apr 29, 2002: PAN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR PAN AT FORWARD AND AFT SIDE. THE CRACK WAS LOCATED AT RADIUS BELOW LATCH. THE CRACKS WERE STOP DRILLED IAW
- [SDR CALA0200294](https://openairdocs.org/sdr/CALA0200294), Apr 27, 2002: STIFFENER. CORRODED. VERTICAL STIFFENER FOR ATTACH ANGLE FOR FRAME CORRODED AT FS 1322 LONGERON 30. REMOVED AND REINSTALLED FABRICATED ANGLE PER SRM 51-30-2, 51-30-5, AND 53-01 FIG1
- [SDR CALA0200293](https://openairdocs.org/sdr/CALA0200293), Apr 26, 2002: WEB. CRACKED. FORWARD ENTRY DOOR JAMB INNER WEB CRACKED AT STATION 200 LONGERON 14L. INSTALLED REPAIR PER EC/RA 5314-01011 AND EA 9-5314-2-A0950.
- [SDR CALA0200238](https://openairdocs.org/sdr/CALA0200238), Apr 24, 2002: SKIN. DENTED. INSPECTION FOUND TWO DENTS IN THE FUSELAGE SKIN AT STA 232, LONGERON 17R. THE DENTS WERE REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-4, 
- [SDR CALA0100500](https://openairdocs.org/sdr/CALA0100500), May 24, 2001: SPAR. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN VERTICAL STABILIZER LT FRONT SPAR AT CANTED FRAME STA 1388. THE CRACK WAS LOCATED NINE INCHES UP FROM BOTTOM END. THE SPAR W
- [SDR CALA0100498](https://openairdocs.org/sdr/CALA0100498), May 23, 2001: CLIP. OUT OF ADJ. THE CABIN AFT ENTRY DOOR TAIL CONE RELEASE HANDLE PULL FORCE WAS LOW. THE TAIL CONE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.
- [SDR CALA0100497](https://openairdocs.org/sdr/CALA0100497), May 23, 2001: CLIP. OUT OF ADJ. THE EXTERIOR TAIL CONE RELEASE HANDLE PULL FORCE WAS LOW. THE TAIL CONE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.
- [SDR CALA0100496](https://openairdocs.org/sdr/CALA0100496), May 23, 2001: CLIP. OUT OF ADJ. THE INTERIOR TAIL CONE RELEASE HANDLE PULL FORCE WAS EXCESSIVE. THE TAIL CONE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.
- [SDR CALA0100490](https://openairdocs.org/sdr/CALA0100490), May 22, 2001: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN TAIL COMPARTMENT BELTFRAME AT STA 1418, LONGERON 2L TO 2R. REPAIRED IAW DRAWING SR09530003.
- [SDR CALA0100488](https://openairdocs.org/sdr/CALA0100488), May 21, 2001: BATTERY PACK. DISCHARGED. INSPECTION FOUND FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-53-00.
- [SDR CALA0100483](https://openairdocs.org/sdr/CALA0100483), May 20, 2001: WEB. CRACKED. INSPECTION FOUND TWO .5 INCH CRACKS IN FORWARD LOWER SILL PLATE WEB AT AFT BAGGAGE BIN DOOR JAMB AREA. THE SILL PLATE WEB WAS REMOVED AND REPLACED IAW SRM 51-30
- [SDR CALA0100478](https://openairdocs.org/sdr/CALA0100478), May 18, 2001: PAN. CORRODED. INSPECTION FOUND FORWARD BAGGAGE BIN DOOR PAN CORRODED BETWEEN LOWER DOOR STOPS AT STA 389-408. SPLICES WERE INSTALLED ON FORWARD CARGO DOOR PAN IAW SRM 53-05, 
- [SDR CALA9900006](https://openairdocs.org/sdr/CALA9900006), Jan 2, 1999: CABLES. OUT OF ADJUST. THE TAIL CONE RELEASE PULL WAS BELOW LIMITS WHEN USING INTERIOR OR EXTERIOR TAIL CONE HANDLE. THE CABLES, LATCHES AND CLIPS WERE ADJUSTED IAW MM 53-53-00.

All 65: https://openairdocs.org/aircraft/N16895/unmatched-reports.md

## 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/N16895/stcs.md

## Earlier aircraft with N16895

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N16895 before.

- [Cancelled 1974-06-12](https://openairdocs.org/deregistered/N16895-1974-06-12): Douglas C-47, S/N 16709. Owner: [Weyerhaeuser International Inc](https://openairdocs.org/faa-owner/WEYERHAEUSER%20INTERNATIONAL%20INC), [Gig Harbor, WA](https://openairdocs.org/faa-place/WA/Gig%20Harbor)

## 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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