# N14173: 2004 Embraer EMB-145XR

- Status: Valid registration
- Airframe: [Embraer EMB-145XR](https://openairdocs.org/model/embraer-emb-145xr) (registry code 3260214, 55 seats)
- Engine: [Rolls-Royce AE3007 series](https://openairdocs.org/engine/rolls-royce-ae3007-series) (registry code 54582)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 14500872
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 26, 2004
- Certificate issued: May 5, 2020
- Expires: May 31, 2027
- Mode S code: A0A9D0
- Registered owner: [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC)
- Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago)
- Owner type: Corporation
- Owner's area on the map: 41.8813° N, 87.6375° W: Placed by OpenAirDocs at the center of ZIP code 60606, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14173
- Page: https://openairdocs.org/aircraft/N14173

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 Rolls-Royce AE3007 model are included.

## ADs that may apply (OpenAirDocs): 95 in force

### Matched by airframe (Embraer EMB-145XR)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-08-07](https://openairdocs.org/ad/2025-08-07): Flight Controls · Embraer EMB-145, EMB-145ER, EMB-145MR and 4 more. Effective Jun 26, 2025
- [AD 2024-26-07](https://openairdocs.org/ad/2024-26-07): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 11, 2025
- [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 2021-07-14](https://openairdocs.org/ad/2021-07-14): Main landing gear · Yaborã Indústria Aeronáutica EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Apr 20, 2021
- [AD 2021-04-09](https://openairdocs.org/ad/2021-04-09): Engine fuel and control · Yaborã Indústria Aeronáutica EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Mar 30, 2021
- [AD 2019-03-30](https://openairdocs.org/ad/2019-03-30): Engine Exhaust · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 26, 2019
- [AD 2017-15-16](https://openairdocs.org/ad/2017-15-16): Flight controls · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Sep 5, 2017
- [AD 2017-12-09](https://openairdocs.org/ad/2017-12-09): Fuel · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Jul 20, 2017
- [AD 2017-09-09](https://openairdocs.org/ad/2017-09-09): Passenger Compartment Equipment · Boeing 717-200, MD-90-30, CL-600-2C10 (Regional Jet Series 700) and 17 more. Effective Jun 28, 2017
- [AD 2017-04-12](https://openairdocs.org/ad/2017-04-12): Ice and rain protection · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Mar 29, 2017
- [AD 2015-02-13](https://openairdocs.org/ad/2015-02-13): Nacelles/pylons; Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 6, 2015
- [AD 2013-22-18](https://openairdocs.org/ad/2013-22-18): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Nov 20, 2013
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2010-16-02](https://openairdocs.org/ad/2010-16-02): Airborne Auxiliary Power · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 9, 2010
- [AD 2010-16-01](https://openairdocs.org/ad/2010-16-01): Fuel · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Sep 9, 2010
- [AD 2010-12-07](https://openairdocs.org/ad/2010-12-07): Wings · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jul 22, 2010
- [AD 2010-11-01](https://openairdocs.org/ad/2010-11-01): Fuselage · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jul 6, 2010
- [AD 2010-10-11](https://openairdocs.org/ad/2010-10-11): Landing gear · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jun 21, 2010
- [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010
- [AD 2010-03-07](https://openairdocs.org/ad/2010-03-07): Landing gear · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 11, 2010
- [AD 2009-26-02](https://openairdocs.org/ad/2009-26-02): Ice and rain protection · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 19, 2010
- [AD 2009-01-05](https://openairdocs.org/ad/2009-01-05): Maximum takeoff weight (MTOW) · Embraer EMB-145, EMB-145EP, EMB-145ER and 4 more. Effective Mar 27, 2009
- [AD 2008-22-19](https://openairdocs.org/ad/2008-22-19): Flight deck · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 19, 2008
- [AD 2008-17-05](https://openairdocs.org/ad/2008-17-05): Fuel tanks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 23, 2008
- [AD 2008-12-07](https://openairdocs.org/ad/2008-12-07): Fuel leakage · Embraer EMB-135BJ (Legacy 600) and EMB-145XR. Effective Jul 16, 2008
- [AD 2008-10-08](https://openairdocs.org/ad/2008-10-08): Reduces the compliance time for doing the modification · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective May 23, 2008
- [AD 2008-05-02](https://openairdocs.org/ad/2008-05-02): Tail section or rudder pedals · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Apr 8, 2008
- [AD 2008-03-03](https://openairdocs.org/ad/2008-03-03): Elevator control system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Feb 14, 2008
- [AD 2007-24-03](https://openairdocs.org/ad/2007-24-03): Forward fuselage right hand (RH) side skin · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jan 2, 2008
- [AD 2007-13-03](https://openairdocs.org/ad/2007-13-03): Ventral fuel tank · Embraer EMB-145XR. Effective Jul 25, 2007
- [AD 2007-10-11](https://openairdocs.org/ad/2007-10-11): Electrical bonding clamps · Embraer EMB-135BJ (Legacy 600), EMB-135LR, EMB-145LR and 2 more. Effective Jun 21, 2007
- [AD 2007-04-09](https://openairdocs.org/ad/2007-04-09): Left- and right-hand windshield temperature controllers · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 23, 2007
- [AD 2007-04-03](https://openairdocs.org/ad/2007-04-03): Pitot static heating relay K0057 · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 21, 2007
- [AD 2006-26-04](https://openairdocs.org/ad/2006-26-04): Passenger seat tracks · Embraer EMB-145XR. Effective Jan 31, 2007
- [AD 2006-21-04](https://openairdocs.org/ad/2006-21-04): Clear-ice indication lamp · Embraer EMB-135BJ (Legacy 600) and EMB-145XR. Effective Nov 17, 2006
- [AD 2006-19-04](https://openairdocs.org/ad/2006-19-04): Honeywell COM unit and Mode S transponder · Bombardier BD-700-1A10, BD-700-1A11, 550 and 26 more. Effective Oct 17, 2006
- [AD 2006-18-03](https://openairdocs.org/ad/2006-18-03): Flap system interface wiring · Embraer EMB-145XR. Effective Oct 4, 2006
- [AD 2006-16-17](https://openairdocs.org/ad/2006-16-17): Torque values of the screws that attach the seat tracks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 25, 2006
- [AD 2006-07-01](https://openairdocs.org/ad/2006-07-01): Horizontal stabilizer control unit (HSCU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective May 1, 2006
- [AD 2006-03-06](https://openairdocs.org/ad/2006-03-06): Pilot's and co-pilot's seat tracks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 13, 2006
- [AD 2005-25-17](https://openairdocs.org/ad/2005-25-17): Auxiliary power unit (APU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 18, 2006
- [AD 2005-24-11](https://openairdocs.org/ad/2005-24-11): Elevator gust lock system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 9, 2006
- [AD 2005-24-02](https://openairdocs.org/ad/2005-24-02): Airplane flight manual (AFM) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 28, 2005
- [AD 2005-23-20](https://openairdocs.org/ad/2005-23-20): Auxiliary power unit (APU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 27, 2005
- [AD 2005-23-13](https://openairdocs.org/ad/2005-23-13): Nose landing gear (NLG) wheel · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 19, 2005
- [AD 2005-22-08](https://openairdocs.org/ad/2005-22-08): Total air temperature (TAT) sensor heating system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Nov 30, 2005
- [AD 2005-20-37](https://openairdocs.org/ad/2005-20-37): Main landing gear (MLG) trailing arms and integrity of the MLG pivot axle sealant. · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Nov 16, 2005
- [AD 2005-14-02](https://openairdocs.org/ad/2005-14-02): Left and right engine fire handles · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Aug 15, 2005
- [AD 2005-14-03](https://openairdocs.org/ad/2005-14-03): Engine-driven hydraulic pump · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Aug 10, 2005

### Matched by engine (Rolls-Royce AE3007 series)

- [AD 2020-16-13](https://openairdocs.org/ad/2020-16-13): Turbine Engine Compressor Section · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Aug 14, 2020
- [AD 2018-17-04](https://openairdocs.org/ad/2018-17-04): Turbine section · Rolls-Royce AE 2100D2A, AE 2100D3 and AE 3007A2. Effective Sep 21, 2018
- [AD 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018
- [AD 2017-11-05](https://openairdocs.org/ad/2017-11-05): Turbine/ turboprop Engine, Turbine Section · Rolls-Royce AE 3007C and AE 3007C1. Effective Jul 18, 2017
- [AD 2015-02-08](https://openairdocs.org/ad/2015-02-08): Turbine wheels · Rolls-Royce AE 2100D2, AE 2100D2A, AE 2100D3 and 11 more. Effective Mar 11, 2015
- [AD 2013-26-06](https://openairdocs.org/ad/2013-26-06): High-pressure turbine (HPT) stage 2 wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Feb 7, 2014
- [AD 2011-22-03](https://openairdocs.org/ad/2011-22-03): Low-cycle fatigue cracks · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 4 more. Effective Nov 17, 2011
- [AD 2009-24-04](https://openairdocs.org/ad/2009-24-04): Fan spinner · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 5 more. Effective Dec 28, 2009
- [AD 2009-04-03](https://openairdocs.org/ad/2009-04-03): 2nd stage, 3rd stage, and 4th stage compressor wheels · Rolls-Royce AE 1107C and AE 3007A1E. Effective Mar 24, 2009
- [AD 2007-24-05](https://openairdocs.org/ad/2007-24-05): Engine oil temperature · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 8 more. Effective Jan 2, 2008
- [AD 2004-04-05](https://openairdocs.org/ad/2004-04-05): Engine oil system · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Mar 9, 2004
- [AD 2003-25-08](https://openairdocs.org/ad/2003-25-08): 1st and 2nd stage turbine spacers · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 3 more. Effective Jan 21, 2004
- [AD 2001-25-05](https://openairdocs.org/ad/2001-25-05): Compressor Cone Shafts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jan 23, 2002
- [AD 2001-19-03](https://openairdocs.org/ad/2001-19-03): High Pressure Turbine 1st to 2nd Stage Turbine Spacer · Rolls-Royce AE 3007A and AE 3007C. Effective Oct 29, 2001
- [AD 2001-17-31](https://openairdocs.org/ad/2001-17-31): Second Stage High Pressure Turbine Wheel · Rolls-Royce AE 2100A, AE 2100C, AE 2100D3 and 2 more. Effective Oct 5, 2001
- [AD 2000-18-06](https://openairdocs.org/ad/2000-18-06): Digital Electronic Controls · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 22, 2000
- [AD 2000-13-01](https://openairdocs.org/ad/2000-13-01): Turbine Wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 1, 2000
- [AD 2000-11-22](https://openairdocs.org/ad/2000-11-22): Critical Life-Limited Parts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Aug 7, 2000
- [AD 99-03-03](https://openairdocs.org/ad/99-03-03): Full Authority Digital Engine Control (FADEC) · Rolls-Royce AE 3007A and AE 3007A1/1. Effective Feb 16, 1999
- [AD 98-11-32](https://openairdocs.org/ad/98-11-32): Sump Magnetic Chip Collector Plug · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Jun 18, 1998

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

- [AD 2008-13-14](https://openairdocs.org/ad/2008-13-14) (historical): Fuel system limitations (FSL) · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jul 30, 2008
- [AD 2007-12-17](https://openairdocs.org/ad/2007-12-17) (historical): Metallic tubes enclosing the vent and pilot valve wires · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Jul 19, 2007
- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 2006-20-08](https://openairdocs.org/ad/2006-20-08) (historical): Rod ends of aileron power control actuator, superseding AD 99-05-04 · Embraer EMB-145, EMB-145EP, EMB-145ER and 4 more. Effective Nov 8, 2006
- [AD 2006-04-02](https://openairdocs.org/ad/2006-04-02) (historical): Pitot static heating relay K0057 · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Mar 31, 2006
- [AD 2005-26-15](https://openairdocs.org/ad/2005-26-15) (historical): Certain components of the elevator control system · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 8 more. Effective Feb 3, 2006
- [AD 2005-25-04](https://openairdocs.org/ad/2005-25-04) (historical): Tail section or rudder pedals · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Dec 23, 2005
- [AD 2010-19-01](https://openairdocs.org/ad/2010-19-01) (historical): High pressure turbine · Rolls-Royce AE 3007A. Effective Oct 27, 2010
- [AD 2009-08-51](https://openairdocs.org/ad/2009-08-51) (historical): High-pressure turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 6 more. Effective May 27, 2009
- [AD 2008-26-06](https://openairdocs.org/ad/2008-26-06) (historical): High-pressure turbine (HPT) · AE 3007A. Effective Jan 8, 2009
- [AD 2008-19-51](https://openairdocs.org/ad/2008-19-51) (historical): AE 3007A, AE 3007A1, AE 3007A1E and 5 more
- [AD 2001-08-15](https://openairdocs.org/ad/2001-08-15) (historical): Oil System · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective May 14, 2001
- [AD 2000-09-05](https://openairdocs.org/ad/2000-09-05) (historical): Cone Shafts · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jul 5, 2000
- [AD 99-02-51](https://openairdocs.org/ad/99-02-51) (historical): Starter Shaft Seal · AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Apr 20, 1999

All 109: https://openairdocs.org/aircraft/N14173/ads.md

## Information bulletins (advisory) (10 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB AIR-20-17](https://openairdocs.org/saib/AIR-20-17): Air Conditioning - Cabin Pressure Control System. Issued Nov 3, 2020
- [SAIB NM-19-17](https://openairdocs.org/saib/NM-19-17): Ice and Rain Protection: Electrical Wiring Terminations at Pitot and TAT Relays. Issued Dec 5, 2019
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008
- [SAIB NM-08-15](https://openairdocs.org/saib/NM-08-15): Instruments: Contamination of the Attitude Heading Reference System (AHRS) Computers. Issued Mar 26, 2008
- [SAIB NM-07-40](https://openairdocs.org/saib/NM-07-40): Embraer EMB-135/145 Landing Gear Incident. Issued Jul 9, 2007
- [SAIB NM-07-20](https://openairdocs.org/saib/NM-07-20): Flight Data Recorders. Issued Mar 21, 2007
- [SAIB NE-11-22](https://openairdocs.org/saib/NE-11-22): Engine Controls. Issued Feb 23, 2011
- [SAIB CE-00-18](https://openairdocs.org/saib/CE-00-18): . Issued Mar 30, 2000
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N14173.

## FAA accident and incident reports

None matched to N14173.

## Service difficulty reports (80, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR JJBA20221129029](https://openairdocs.org/sdr/JJBA20221129029), Nov 26, 2022: SKIN. DENTED. FUSELAGE SKIN DENT HAS CREASE/GOUGE. DENT IS 3.75" X 2.25" AT FR 23-24, STR 12L-13L. DEPTH 0.125, FR 23 TO DENT IS 1", FR24 TO DENT IS 1.5", STR 13L TO DENT IS 
- [SDR JJBA20211228037](https://openairdocs.org/sdr/JJBA20211228037), Dec 28, 2021: NONE. NONE. OVERWING EMERGENCY EXIT COVERS ARE LOOSE. RESECURED EMERGENCY EXIT COVERS
- [SDR JJBA20211205005](https://openairdocs.org/sdr/JJBA20211205005), Dec 5, 2021: NONE. NONE. ROW 18 EMERGENCY LIGHTS DO NOT COME ON WHEN SWITCH IS ACTIVATED. CHARGED EMERGENCY LIGHT BATTERIES USING AC POWER. OPS CHECK OF EMERGENCY LIGHTS SAT. NO OTHER D
- [SDR JJBA20210803024](https://openairdocs.org/sdr/JJBA20210803024), Aug 3, 2021: LIGHT. UNSECURE. EMERGENCY PATH LIGHTING STRIP NEAR 1A IS DISLODGED. SECURED IN PLACED EMERGENCY PATH LIGHTING STRIP NEAR 1A WITH TAPE.
- [SDR JJBA20210528029](https://openairdocs.org/sdr/JJBA20210528029), May 28, 2021: FAN. ODOR. PLASTIC BURNING SMELL NEAR ROW 18, WITH VISIBLE SMOKE COMING FROM FLOOR VENT IN THE ISLE. FOUND CONDENSATION COMING FROM DISCONNECTED FAN #2 HOSE. RECONNECTED F
- [SDR JJBA20210510001](https://openairdocs.org/sdr/JJBA20210510001), May 8, 2021: INSTRUMENT PANEL. MULTIPLE FAIL. AVIONICS MASTER 2 LIGHTED WHILE PRESSED IN, CA MFD INOPERATIVE, FO PFD INOPERATIVE, #2 FMS INOPERATIVE, #2 RMU INOPERATIVE. R&R AVIONICS MASTER #2 PUSH BUTTON. 
- [SDR JJBA20210415051](https://openairdocs.org/sdr/JJBA20210415051), Apr 15, 2021: SEALANT. MISSING. REMOVED SEALANT AROUND THE RH AND LH MLG LOWER SIDE STRUT BEARING FLANGE. APPLIED SEALANT AROUND RH AND LH MLG LOWER SIDE STRUT BEARING.
- [SDR JJBA20210304002](https://openairdocs.org/sdr/JJBA20210304002), Mar 4, 2021: LIGHT. MISINSTALLED. LH AND RH EXTERIOR OVER-WING EMERGENCY EXIT LIGHTS ARE INSTALLED UPSIDE DOWN. REMOVED AND REINSTALLED LH AND RH EXTERIOR OVER-WING EMERGENCY LIGHT EXIT PANELS.
- [SDR JJBA20210121034](https://openairdocs.org/sdr/JJBA20210121034), Jan 21, 2021: SHEAR TIE. CORRODED. CORROSION ON AFT SHEAR CLIP OF CARGO DOOR, AT FR 68 BETWEEN STR 15L-16L. ON AFT SHEAR CLIP OF CARGO DOOR, AT FR 68 BETWEEN STR 15L-16L CORROSION BLENDED OUT OF 
- [SDR JJBA20210121028](https://openairdocs.org/sdr/JJBA20210121028), Jan 21, 2021: FLOOR SUPPORT. CORRODED. CENTER OMEGA BEAM CORRODED ON TOP SURFACE (AFTER REMOVAL OF GUSSET) CORROSION LEVEL 2. CENTER OMEGA BEAM CORRODED ON TOP SURFACE BLENDED OUT OF LIMIT AT TWO PLA
- [SDR JJBA20210121027](https://openairdocs.org/sdr/JJBA20210121027), Jan 21, 2021: FLOOR SUPPORT. CORRODED. RT OMEGA BEAM CORRODED ON TOP SURFACE (AFTER REMOVAL OF GUSSET) CORROSION LEVEL 2. RT OMEGA BEAM CORRODED ON TOP SURFACE BLENDED OUT OF LIMIT AT TWO PLACES. RT 
- [SDR JJBA20210121022](https://openairdocs.org/sdr/JJBA20210121022), Jan 21, 2021: SKIN. CHAFED. LT SIDE RUDDER 1, FRONT SPAR SKIN CHAFED ON 2 PLACES BETWEEN RIB ZV 2601.0 AND RIB ZV 3179.0. LT SIDE RUDDER 1, FRONT SPAR SKIN CHAFED ON 2 PLACES BETWEEN RIB Z
- [SDR JJBA20210121021](https://openairdocs.org/sdr/JJBA20210121021), Jan 21, 2021: DOUBLER. CORRODED. CARGO AREA UNDER FLOOR CORROSION FOUND RAD ALT ANTENNA. CORROSION LEVEL 2: AT REAR FUSELAGE RADIO ALT ANTENNA, DOUBLER AND LOUVER FOR INVESTIGATION CUT OUT DONE
- [SDR JJBA20210120036](https://openairdocs.org/sdr/JJBA20210120036), Jan 20, 2021: SPAR. CRACKED. LT AND RT PYLON SPAR II 2X CRACK (ONE EACH SIDE) ON RIVET HOLE. 1 BUSHING (FLUSH-PYLON) LOCALLY FABRICATED, 1 BUSHING (PYLON) LOCALLY FABRICATED. DAMAGED HOLES 
- [SDR JJBA20210120035](https://openairdocs.org/sdr/JJBA20210120035), Jan 20, 2021: RIVET. MISSING. BAGGAGE DOOR FWD TRACK RIVET MISSING LOWER END. AFTER INVESTIGATION BAGGAGE DOOR FWD TRACK FOUND CORRODED AND BLENDED OUT OF LIMITS AT RIVET HOLE LOCATION & 1 A
- [SDR JJBA20210120033](https://openairdocs.org/sdr/JJBA20210120033), Jan 20, 2021: DOUBLER. CORRODED. LOWER FUSELAGE ANTENNA RAD ALT NO 1 INTERNAL DOUBLER CORRODED. CUT OUT DONE. DOUBLER HOLES PATTERN DRILLED ON SKIN. DOUBLER INSTALLED WITH FILLER.
- [SDR JJBA20210120032](https://openairdocs.org/sdr/JJBA20210120032), Jan 20, 2021: FLOOR SUPPORT. DAMAGED. DAMAGE ON LT CENTER FUSE 1 BETWEEN FR 23 JUNCTION 03 AND BETWEEN STR 19L-20L. DAMAGE ON LT CENTER FUSE 1 BETWEEN FR 23 JUNCTION 03 AND BETWEEN STR 19L-20L, AREA
- [SDR JJBA20210120031](https://openairdocs.org/sdr/JJBA20210120031), Jan 20, 2021: SKIN. CORRODED. CARGO AREA UNDER FLOOR FR 67 AROUND WATER DRAIN SKIN SHOW SIGN OF CORROSION, CORROSION LEVEL 2. CARGO AREA UNDER FLOOR FR 67 AROUND WATER DRAIN SKIN SHOW SIGN O
- [SDR JJBA20210120030](https://openairdocs.org/sdr/JJBA20210120030), Jan 20, 2021: SKIN. CRACKED. RF 1 LT FUSELAGE SKIN AT FR 75.700 BELOW STGR 2L 2 CRACK FOUND AT ONE RIVET LOCATION. ON RF1 LT FUSELAGE SKIN AT FR 75.700 BELOW STGR 2L CUT OUT DONE. ON RF1 LT
- [SDR JJBA20210120029](https://openairdocs.org/sdr/JJBA20210120029), Jan 20, 2021: DOUBLER. DAMAGED. PRESS BULKHEAD DOUBLER REPAIR EVALUATION FWD PRESS BULKHEAD AND REMOVE THE DOUBLER INSTALLED ON THE FORWARD PRESSURE BULKHEAD. DOUBLER REMOVED FOR REPAIR EVALUA
- [SDR JJBA20210112012](https://openairdocs.org/sdr/JJBA20210112012), Jan 12, 2021: FLOOR SUPPORT. CRACKED. CF3, LT OMEGA BEAM OUTBD ANGLE CRACKED. CF3, LT OMEGA BEAM OUTBD ANGLE REPAIRED.
- [SDR JJBA202002109002](https://openairdocs.org/sdr/JJBA202002109002), Feb 9, 2020: LIGHT. INOPERATIVE. ISLE PATH EMERGENCY PHOTO-LUMINESCENT INCORRECT AT 1A WITH EMERGENCY RED MARKS. R&R PHOTO-LUMINESCENT FLOOR STRIP LIGHT. NO FURTHER DEFECTS NOTED.
- [SDR JJBA2020013029008](https://openairdocs.org/sdr/JJBA2020013029008), Jan 29, 2020: LIGHT. INOPERATIVE. SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R SERVICE DOOR EXTERNAL EMERGENCY LIGHT.
- [SDR JJBA201912165005](https://openairdocs.org/sdr/JJBA201912165005), Dec 15, 2019: LAMP. INOPERATIVE. SERVICE DOOR EXTERNAL EMERGENCY LIGHT FLICKERS. REMOVED AND REPLACED EMERGENCY LIGHT LAMP. OPS CHECK SAT.
- [SDR JJBA201904264016](https://openairdocs.org/sdr/JJBA201904264016), Apr 24, 2019: SIGN. UNSECURE. EXIT SIGN AT ROW 18 UNSECURED. RE-SECURED EXIT SIGN ON ROW 18. OPS CHECK SAT.
- [SDR JJBA2019040331015](https://openairdocs.org/sdr/JJBA2019040331015), Mar 31, 2019: SELECTOR. MALFUNCTIONED. WHEN FLAP HANDLE WAS PLACED TO 0, FLAPS 9 INDICATED ON EICAS. R&R FLAP SELECTOR LEVER.
- [SDR JJBA20190319007](https://openairdocs.org/sdr/JJBA20190319007), Mar 19, 2019: ACM. SEIZED. SMOKE IN THE COCKPIT AND CABIN. FOUND NR 1 ACM SEIZED. REMOVED AND REPLACED ACM. OPS CHECK OF NR 1 ACM SAT.
- [SDR JJBA20190103003](https://openairdocs.org/sdr/JJBA20190103003), Jan 3, 2019: POWER SUPPLY. INOPERATIVE. BOTH OVER WING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY FOR OVER WING EXTERIOR EMERGENCY LIGHTS. OPS CHECK SAT.
- [SDR JJBA20181229032](https://openairdocs.org/sdr/JJBA20181229032), Dec 29, 2018: CRADLE. DEFECTIVE. LT AND RT EXTERNAL EMERGENCY LIGHTS ON CENTER FAIRINGS INOPERATIVE. R&R NR 4 EMERGENCY BATTERY CRADLE. OPS CHECK SAT.
- [SDR JJBA201812076004](https://openairdocs.org/sdr/JJBA201812076004), Dec 6, 2018: SKIN. CORRODED. AIRCRAFT DATA PLATE FORWARD RIGHT RIVET IS LOOSE AND SKIN AREA AT FORWARD SIDE HAS SURFACE CORROSION. CORROSION EXTENDS 100% THROUGH SKIN AND REQUIRES CUT-OUT A
- [SDR ASOA201710247023](https://openairdocs.org/sdr/ASOA201710247023), Oct 24, 2017: STRUCTURE. CORRODED. A/C IS IN A C-CHECK STATUS WHEN INSPECTION FOUND THE RT VERTICAL STAB WITH CORROSION. MAINTENANCE REMOVED THE CORROSION IAW WITH SRM 55-30-02. ALL WORK ACCOMPLI
- [SDR ASOA201710247022](https://openairdocs.org/sdr/ASOA201710247022), Oct 24, 2017: STRUCTURE. CORRODED. A/C IS IN A C-CHECK STATUS WHEN INSPECTION FOUND THE LT VERTICAL STAB WITH CORROSION. MAINTENANCE REMOVED THE CORROSION OF THE VERTICAL STAB IAW SRM 55-30-02. A
- [SDR ASOA201710047021](https://openairdocs.org/sdr/ASOA201710047021), Oct 4, 2017: SHEAR TIE. CORRODED. CARGO DOOR CUT-OUT AT FRAME 65 LOWER SHEAR TIE CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SHEAR TIE.
- [SDR ASOA201710047017](https://openairdocs.org/sdr/ASOA201710047017), Oct 4, 2017: PROFILE. DAMAGED. CARGO DOOR LOWER PROFILE IS DAMAGED ON FORWARD LOWER CORNER. REMOVED AND REPLACED LOWER PROFILE, PRIMED AND PAINTED.
- [SDR ASOA201612187008](https://openairdocs.org/sdr/ASOA201612187008), Dec 17, 2016: BATTERY. DISCHARGED. EMERGENCY LIGHTS OPERATING OFF THE NR 2 EMERGENCY LIGHT BATTERY ARE INOP. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY. OPS CHECK GOOD.
- [SDR ASOA201612187009](https://openairdocs.org/sdr/ASOA201612187009), Dec 5, 2016: CARBON SEAL. LEAKING. WHEN OPERATING ON ENGINE BLEEDS WITH PACKS ON, THERE WAS A SMELL OF OIL IN THE FLIGHT DECK WHEN AT LOW POWER SETTINGS. REMOVED AND REPLACED CARBON SEAL. OPS AND
- [SDR ASOA20160530034](https://openairdocs.org/sdr/ASOA20160530034), May 30, 2016: ACM. FAILED. THE CREW REPORTED SMOKE IN COCKPIT AND CABIN. MAINTENANCE INSPECTED AND REPLACED THE PACK NR 1 ACM. OPS CHECKS WERE GOOD.
- [SDR ASOA20160205004](https://openairdocs.org/sdr/ASOA20160205004), Feb 5, 2016: BATTERY PACK. INOPERATIVE. DURING MAINTENANCE INSPECTION THE CEILING EMERGENCY LIGHTS ABOVE ROW 12 AND LT/RT OVERWING EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE R & R NR 4 EMERGENCY 
- [SDR ASOA20151103056R](https://openairdocs.org/sdr/ASOA20151103056R), Nov 3, 2015: BATTERY PACK. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE NR 3 EMERGENCY LIGHT BATTERY WAS DISCOVERED INOPERATIVE. MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT BATTERY WITH OPS CHECK GO
- [SDR ASOA20150821046](https://openairdocs.org/sdr/ASOA20150821046), Aug 21, 2015: INVERTER. INOPERATIVE. DURING ROUTINE MAINTENANCE THE LT SERVICE DOOR EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT INVERTER. OPS CHECKS WER
- [SDR ASOA20150526051](https://openairdocs.org/sdr/ASOA20150526051), May 26, 2015: FUSE. FAILED. DURING MAINTENANCE INSPECTION, THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R A BLOWN FUSE IN THE NR 4 EMERGENCY LIGHT POWER
- [SDR ASOA20150218054V](https://openairdocs.org/sdr/ASOA20150218054V), Feb 18, 2015: DOOR SILL. CORRODED. SERVICE DOOR SILL CORRODED BETWEEN FRAMES 20-22. R & R DOOR SILL IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150218053V](https://openairdocs.org/sdr/ASOA20150218053V), Feb 18, 2015: SUPPORT. CORRODED. CARGO LOWER BEAM CORRODED BETWEEN FRAMES 65-68. R & R CARGO DOOR LOWER CUTOUT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20141111132](https://openairdocs.org/sdr/ASOA20141111132), Nov 11, 2014: LIGHT. ODOR. THE CREW REPORTED AN ELECTRICAL BURNING ODOR FROM THE LAVATORY LIGHT AFTER THE LATCH WAS CLOSED. THE ACFT LANDED WITHOUT INCIDENT. R & R THE LIGHT BALLAST, OPS 
- [SDR ASOA20140927109](https://openairdocs.org/sdr/ASOA20140927109), Sep 27, 2014: CHARGER. INOPERATIVE. DURING MAINTENANCE INSPECTION, BOTH AFT EXTERIOR OVERWING EMERGENCY LIGHTS WERE DISCOVERED INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARG
- [SDR ASOA20140922108](https://openairdocs.org/sdr/ASOA20140922108), Sep 22, 2014: ENGINE. LEAKING. CREW REPORTED A LAVATORY SMOKE WARNING ON EICAS AFTER TAKEOFF. ACFT PERFORMED AN AIR TURN BACK WHERE IT LANDED WITHOUT INCIDENT. NR 2 ENGINE WAS R & R AND OPS C
- [SDR ASOA20130813149H](https://openairdocs.org/sdr/ASOA20130813149H), Aug 15, 2013: SKIN. CRACKED. DURING 2A INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 79 BELOW STRINGER 05R. MX REMOVED THE DAMAGE AROUND THE RIVET AND PER
- [SDR ASOA2013153](https://openairdocs.org/sdr/ASOA2013153), Aug 13, 2013: SKIN. CRACKED. DURING 2A INSPECTION, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77 BELOW STRINGER 03L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING 
- [SDR ASOA20130813152](https://openairdocs.org/sdr/ASOA20130813152), Aug 13, 2013: SKIN. CRACKED. DURING 2A INSPECTION THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE A CRACK AT A RIVET ON FRAME 77 BELOW STRINGER 08L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING
- [SDR ASOA20130813151H](https://openairdocs.org/sdr/ASOA20130813151H), Aug 13, 2013: SKIN. CRACKED. DURING 2A INSPECTION THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE 3 EA CRACKS TOTALING 6.74MM (.026") AT A RIVET ON FRAME 79 BELOW STRINGER 05L. MX REMOVED THE DA

All 80: https://openairdocs.org/aircraft/N14173/reports.md

## STCs that may be installed (OpenAirDocs) (56, 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 (Embraer EMB-145XR)

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST02176AT-D](https://openairdocs.org/stc/ST02176AT-D): Installation of a Teledyne Mini Flight Data Acquistion Unit. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST02310AT](https://openairdocs.org/stc/ST02310AT): Installation of SAF-T-GLO photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST01409LA](https://openairdocs.org/stc/ST01409LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC ST01984LA-D](https://openairdocs.org/stc/ST01984LA-D): Modification and installation of passenger seats, passenger service units and filler panels, seat track covers, and seat row placards. Safran Cabin Inc
- [STC ST04219NY](https://openairdocs.org/stc/ST04219NY): Installation of SpaceX Starlink Aviation System. Aerospace Design & Compliance LLC
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST00640DE](https://openairdocs.org/stc/ST00640DE): Installation of Tropospheric Airborne Meteorolocigal Data Reporting System (TAMDAR). FLYHT Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC ST04177NY](https://openairdocs.org/stc/ST04177NY): Installation of ALI LED Cabin Lighting, Cabin and Crew AC Power Outlets, LH Fwd Closet and Misc Cabin Mods. C & L STC Holdings LLC
- [STC ST01983WI](https://openairdocs.org/stc/ST01983WI): Installation of a folding stair in the main entrance for models equipped with a side-hinged main door. Worldwide Aviation Engineering LLC
- [STC ST04212NY](https://openairdocs.org/stc/ST04212NY): Installation of Universal UNS-1Lw Flight Management System. C&L Engineering Services, LLC
- [STC ST04213NY](https://openairdocs.org/stc/ST04213NY): PAX Social Distance Floorplan Reconfiguration. C&L Engineering Services LLC
- [STC ST04281AT](https://openairdocs.org/stc/ST04281AT): Installation for the Upgrade of the NZ-2000 FMS computer for software version NZ6. Chippewa Aerospace Inc
- [STC ST03158CH-D](https://openairdocs.org/stc/ST03158CH-D): Installation of a Reconfiguration of a Cabin Floorplan. Standard Aero Business Aviation Services LLC
- [STC SA9087SC-D](https://openairdocs.org/stc/SA9087SC-D): RECORE® Hamilton Sundstrand heat exchanger, P/N 816630-1 / -2 in accordance with Honeywell LORI Sealed Drawing List SDL3869-1 Rev. A, dated June 7, 2005 or later FAA approved revision. Honeywell International Inc
- [STC ST00818DE](https://openairdocs.org/stc/ST00818DE): Installation of Honeywell Control Display Unit (CDU) model CD-830. Premier Air Center LLC d/b/a West Star Aviation
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST09858SC](https://openairdocs.org/stc/ST09858SC): Installation of cabin automatic coffee brewing system. Safran Cabin Germany Gmbh
- [STC ST03420NY](https://openairdocs.org/stc/ST03420NY): Installation of a Cabin Interior. Delta Engineering Corporation
- [STC ST02327LA](https://openairdocs.org/stc/ST02327LA): Installation of replacement proximity sensor harness assembly part numbers used on the nose and main landing gears. Safran Electrical Components USA Inc
- [STC ST10550SC](https://openairdocs.org/stc/ST10550SC): Installation of a WeatherMASTER X-Band Fuselage Nose Radome Assembly. The NORDAM Group LLC
- [STC ST04316CH](https://openairdocs.org/stc/ST04316CH): Installation of a Smartsky System in accordance with StandardAero Master Data List 1034570, Revision (C), dated March 23, 2019 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST03177NY](https://openairdocs.org/stc/ST03177NY): Installation of a Honeywell ADS-B (Out), EHS and FreeFlight GPS. Delta Engineering Corporation
- [STC ST01520WI](https://openairdocs.org/stc/ST01520WI): Installation of the Concorde RG-442 VRSLA Battery and Temperature Sensor in place of the original Nickel-Cadmium Battery. Concorde Battery Corporation
- [STC ST00361BO](https://openairdocs.org/stc/ST00361BO): Installation of a Honeywell Primus II (XS-852) ADS-B Out System. Pro Star Aviation, LLC
- [STC ST04282CH](https://openairdocs.org/stc/ST04282CH): Installation of Honeywell CD-830 Control Display Unit (CDU). Nextant Aerospace
- [STC ST01702WI](https://openairdocs.org/stc/ST01702WI): Change seating configuration to 30 passengers by removal of seats. Worldwide Aircraft Engineering LLC
- [STC ST04108CH](https://openairdocs.org/stc/ST04108CH): Installation of Gogo Business Aviation ATG-8000 High Speed Internet with Wireless Local Area Network (WLAN). Nextant Aerospace
- [STC ST04367AT](https://openairdocs.org/stc/ST04367AT): Removal of the Existing Honeywell DL-900 or DL-950 Data Loader and Installation of the Honeywell DL-1000 Data Loader. Chippewa Aerospace Inc
- [STC ST04190AT](https://openairdocs.org/stc/ST04190AT): Installation of an ADS-B Out. Chippewa Aerospace Inc
- [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST04282AT](https://openairdocs.org/stc/ST04282AT): Installation of the Honeywell DU-875 LCD Flight Display. Chippewa Aerospace Inc
- [STC ST04015AT](https://openairdocs.org/stc/ST04015AT): Installation of the Honeywell NZ-2000 FMS/GPS System with or without WAAS/LPV. Chippewa Aerospace Inc
- [STC ST09859AC](https://openairdocs.org/stc/ST09859AC): Installation of a SkyTender Beverage Trolley. ASIG LLC
- [STC ST04263AT](https://openairdocs.org/stc/ST04263AT): Modification of Interior Arrangement Configuration from 50 to 30 Passenger Seats (All Tourist Class). VIA Airlines Inc
- [STC ST04191AT](https://openairdocs.org/stc/ST04191AT): Installation of the Honeywell Sky Connect Tracker Iridium Satcom System. Chippewa Aerospace Inc
- [STC ST02524LA](https://openairdocs.org/stc/ST02524LA): Installation of TCAS version 7.0. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST03483AT](https://openairdocs.org/stc/ST03483AT): Installation of a Portable Beverage Dispensing System, P/N B43-FA-001. Dynamo Beverage Company, USA, L.L.C
- [STC ST03999AT](https://openairdocs.org/stc/ST03999AT): Installation of a Single Honeywell HF-1050 HF Communication System. Chippewa Aerospace Inc
- [STC ST01619CH](https://openairdocs.org/stc/ST01619CH): Installation of a Lavatory Service Shutoff Valve. AeroControlex Group TransDigm Inc
- [STC ST03994AT](https://openairdocs.org/stc/ST03994AT): Installation of Bleed Air Coupling Sleeve Kit. Seal Dynamics
- [STC ST02638AT](https://openairdocs.org/stc/ST02638AT): Installation of an improved aircraft toilet rinse/fill shutoff valve and asociated hardware. Parker Hannifin Corporation, Parker Aerospace
- [STC ST03890AT](https://openairdocs.org/stc/ST03890AT): Installation of an L-3 Communications Micro Quick Access Recorder (MQAR). Chippewa Aerospace, Inc
- [STC ST02882CH-D](https://openairdocs.org/stc/ST02882CH-D): Installation of a Honeywell Flight Management System (FMS #2). Standard Aero
- [STC ST02803CH-D](https://openairdocs.org/stc/ST02803CH-D): Installation of a Honeywell KHF-1050 system. Standard Aero

All 56: https://openairdocs.org/aircraft/N14173/stcs.md

## Earlier aircraft with N14173

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N14173 before.

- [Cancelled 1972-01-07](https://openairdocs.org/deregistered/N14173-1972-01-07): Piper PA-23-250, S/N 27-4736. Exported to Mexico. Owner: [Alaska Transportation Co](https://openairdocs.org/faa-owner/ALASKA%20TRANSPORTATION%20CO), [San Jose, CA](https://openairdocs.org/faa-place/CA/San%20Jose)
- [Cancelled 1940-07-14](https://openairdocs.org/deregistered/N14173-1940-07-14): Stinson SR-5A, S/N 9263-A, built 1934. Owner: [Colbach Troy L](https://openairdocs.org/faa-owner/COLBACH%20TROY%20L), [Santa Ana, CA](https://openairdocs.org/faa-place/CA/Santa%20Ana)

## Related

- Other Embraer EMB-145XR aircraft: https://openairdocs.org/model/embraer-emb-145xr/aircraft.md
- The Rolls-Royce AE3007 series engine: https://openairdocs.org/engine/rolls-royce-ae3007-series.md

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