# N14143: 2003 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: 145739
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2005
- Certificate issued: December 10, 2019
- Expires: December 31, 2029
- Mode S code: A0A967
- 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=14143
- Page: https://openairdocs.org/aircraft/N14143

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/N14143/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 N14143.

## 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 20141013018979I](https://openairdocs.org/incident/20141013018979I), Oct 13, 2014: Embraer EMB-145XR (N14143), Milwaukee, WI, Minor damage. October 13, 2014 at 1900 CDT an expressjet EMB145XR N14143 flight number ASQ4580 departed runway 7R. Upon climb out a passenger reported to the cabin attendant…

## Service difficulty reports (72, 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 JJBA20260706005](https://openairdocs.org/sdr/JJBA20260706005), Jul 3, 2026: ICS BOX. INOPERATIVE. IC 1 FAIL ON EICAS AFTER PFD 1, MFD 1 AND EICAS DISPLAYS BLANKED OUT. REMOVED AND REPLACED IC #1 IC-600. OPS CHECK SAT.
- [SDR JJBA20260413011](https://openairdocs.org/sdr/JJBA20260413011), Apr 12, 2026: ROLLER. LACK OF LUBE. MCD DIFFICULT TO OPEN OR CLOSE. LUBRICATED MCD ROLLER. OPS CHECK GOOD.
- [SDR JJBA20250515059](https://openairdocs.org/sdr/JJBA20250515059), May 14, 2025: UNKNOWN. ODOR. BURNING RUBBER SMELL AFTER TAKE OFF ON CLIMB. PERFORMED FIM PROCEDURES. PERFORMED HIGH POWER ENGINE RUNS. NO SMOKE OR ODOR PRESENT. ALL INDICATIONS NORMAL.
- [SDR JJBA20250328038](https://openairdocs.org/sdr/JJBA20250328038), Mar 24, 2025: UNKNOWN. ODOR. WEIRD CHEMICAL SMELL COMING FROM COCKPIT ON DESCENT. PERFORMED WITH ENGINE BLEED 1 AND 2. OC SAT. RAN PACK SYSTEM DURING HIGH POWER RUN ON FULL HOT AND FULL COL
- [SDR JJBA20250120017](https://openairdocs.org/sdr/JJBA20250120017), Jan 16, 2025: LAMP. INOPERATIVE. RIGHT EXTERIOR FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT EXTEIOR FWD EMERGENCY LIGHT. OPS CHECK SAT
- [SDR JJBA20241209006](https://openairdocs.org/sdr/JJBA20241209006), Dec 5, 2024: A/C PACK. ODOR. DIRTY SOCK SMELL ON DECENT FROM PACK 1. FOLLOWED FIM. DIRTY SOCK SMELL ODOR WAS NOT PRESENT AT THIS TIME. PERFORMED GVI INSPECTION OF THE #1 PACK SYSTEM, NO DEF
- [SDR JJBA20230404002](https://openairdocs.org/sdr/JJBA20230404002), Apr 4, 2023: UNKNOWN. UNKNOWN. CRACK ALONG INTERNAL FUEL TANK DOUBLER UNDER RH WING RIB 9 FOUND CRACK TO BE MIGRATING ACROSS DOUBLER THROUGH 3 HIGH LOCK (FWD) HOLES. REMOVED HILOCK COLLARS FR
- [SDR JJBA20220711008](https://openairdocs.org/sdr/JJBA20220711008), Jul 9, 2022: LAMP. INOPERATIVE. LH FORWARD EXTERNAL EMERGENCY LIGHT INOP. R/R LH FORWARD EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT
- [SDR JJBA20220619014](https://openairdocs.org/sdr/JJBA20220619014), Jun 19, 2022: NONE. INOPERATIVE. SMOKE SMELL FROM COCKPIT DURING DEP CLIMB OUT. REMOVED AND REPLACED SLEEVES BETWEEN DUAL TEMP CONTROL VALVE AND Y-DUCT ON #2 PACK VALVE. REMOVED AND REPLACED #2
- [SDR JJBA20220401002](https://openairdocs.org/sdr/JJBA20220401002), Apr 1, 2022: LAMP. INOPERATIVE. EMERGENCY CEILING LIGHT IN COCKPIT INOPERATIVE. REMOVED AND REPLACED EMERGENCY CEILING LIGHT IN COCKPIT. OPS CHECK SAT
- [SDR JJBA20211125047](https://openairdocs.org/sdr/JJBA20211125047), Nov 25, 2021: UNKNOWN. UNKNOWN. RH FWD FUSELAGE I, TWO LIGHTING STRIKES SUSPECTED BTW FR 1A & 2 AND ABOVE STR 13R. DURING LIGHTING STRIKE INVESTIGATION MULTIPLE STRIKE SPOTS BLENDED WITHIN LIM
- [SDR JJBA20211125045](https://openairdocs.org/sdr/JJBA20211125045), Nov 25, 2021: UNKNOWN. UNKNOWN. MULTIPLE DENTS FOUND ON EXTERNAL SKIN OF MAIN DOOR BTW STR 06L AND STR 08L, STR 12L AND STR 15L. MULTIPLE DENTS ON EXT SIGN OF MAIN DOOR BTW STR 06L-08L AND STR
- [SDR JJBA20211125044](https://openairdocs.org/sdr/JJBA20211125044), Nov 25, 2021: NONE. NONE. CF1, SKIN FOUND WITH EXISTING BLEND BTW FR 20-21 STR 11-12L. CF1, SKIN BTW FR 20-21 AND STR 11-12L FOUND BLENDED OUT OF LIMITS. REPAIR WAS MADE.
- [SDR JJBA20211124046](https://openairdocs.org/sdr/JJBA20211124046), Nov 24, 2021: UNKNOWN. UNKNOWN. RIVET FOUND ON LEADING EDGE II RH. DENT AT RIVET LOCATION OF LEADING EDGE II RH FOUND OUT OF LIMITS AND NEEDS REPAIR PARTS FOR REPAIR SPLICE AND FILLER FABRICAT
- [SDR JJBA20211124043](https://openairdocs.org/sdr/JJBA20211124043), Nov 24, 2021: NONE. NONE. CENTER FUSE II, FRAME 25 CRACKED BTW STR 16R-15R. FRAME REPAIRED
- [SDR JJBA20211124041](https://openairdocs.org/sdr/JJBA20211124041), Nov 24, 2021: NONE. NONE. CRACK FOUND ON LH FRAME 59 BTW STR 15L-16L IN CF IV AREA. FRAME REPAIRED
- [SDR JJBA20211124040](https://openairdocs.org/sdr/JJBA20211124040), Nov 24, 2021: SKIN. DAMAGED. FWD FUSELAGE 1 RH SKIN AT FR 3 BTW STR 01R-13R SEVERAL RIVETS NOT PROPERLY INSTALLED. PAINT STRIPPED ON FWD FUSELAGE I RH, STR 01R-13R FOR INVESTIGATION ON FWD 
- [SDR JJBA20211124039](https://openairdocs.org/sdr/JJBA20211124039), Nov 24, 2021: DOUBLER. CORRODED. CORROSION FOUND ON ANTENNA INNER DOUBLER BTW FR 65-66 AND STR 21LH + STR 21RH. REMOVED R. ALT ANTENNA FOR ACCESS, REMOVED INNER AND OTHER DOUBLER FOR INVESTIGAT
- [SDR JJBA20211118038](https://openairdocs.org/sdr/JJBA20211118038), Nov 18, 2021: SKIN. DENTED. LH FWD FUSELAGE II, DENT FOUND ON EXTERNAL SKIN BTW FR 8-9 AND STR 18L-20L. DENT REMOVED BY CUT OUT ON LH FWD FUSE II EXTERNAL SKIN BTW FR 8-9 AND STR 18L-20L. 
- [SDR JJBA20211118034](https://openairdocs.org/sdr/JJBA20211118034), Nov 18, 2021: NONE. NONE. CF1 FLOOR STRUCTURE PROFILE OMEGA BTW FR 20-23 LH CORRODED. AFTER FURTHER INVESTIGATION OMEGA BEAM FOUND CRACKED AT FASTENERS LOCATION. CF1 FLOOR STRUCTURE, OME
- [SDR JJBA202108030026](https://openairdocs.org/sdr/JJBA202108030026), Jul 30, 2021: GLOWSTRIP. CRACKED. PHOTOLUMINESCENT STRIP CRACKED AT SEAT 1A. R/R PHOTOLUMINECENT STRIP
- [SDR JJBA2021310002](https://openairdocs.org/sdr/JJBA2021310002), Mar 10, 2021: SEAT FRAME. CRACKED. FOUND SEATS 23A, 22A, 24A, 21A, 7A, 5A HAVE A CRACK BELOW ARMREST ON STRUCTURE. R&R 23A, 22A, 24A, 21A, 7A, 5A SEATS. OPS CHECK SAT. NO DEFECTS NOTED.
- [SDR JJBA202006242006](https://openairdocs.org/sdr/JJBA202006242006), Jun 22, 2020: ELECTRONIC UNIT. INOPERATIVE. LG AIR GROUND FAIL EICAS MESSAGE IMMEDIATELY AFTER TAKE OFF. ADJUST NLG TORQUE LINK TARGET. PERFORM GEAR SWINGS FAIL. TROUBLESHOT TO LGEU. R&R LGEU AND GEAR SWI
- [SDR JJBA202006054003](https://openairdocs.org/sdr/JJBA202006054003), Jun 4, 2020: CHARGER. INOPERATIVE. FORWARD EXTERNAL EMERGENCY LIGHTS FWD OF WING INOPERATIVE. REMOVED AND REPLACED NR 2 BATTERY CHARGER ASSEMBLY. REMOVED AND REPLACED BURNT OUT BULBS. OPS CHECK S
- [SDR JJBA202006052002](https://openairdocs.org/sdr/JJBA202006052002), Jun 2, 2020: FASTENER. LOOSE. RIGHT PASSENGER CABIN, ESCAPE HATCH DOOR TOOK SEVERAL MINUTES TO REMOVE DOOR TO FOM. FOUND FASTENERS THAT ATTACH SIDEWALL PANEL TO EMERGENCY EXIT DOOR FRAME LOO
- [SDR JJBA2020031108003](https://openairdocs.org/sdr/JJBA2020031108003), Mar 8, 2020: WARNING SYSTEM. FALSE ACTIVATION. LG LEVER DISAGREE ON TAKE-OFF. PERFORMED GVI OF NLG, MLG, AND WHEEL WELLS WITH NO DEFECTS. CHECKED CMC WITH NO FAULTS. PERFORMED GEAR SWINGS. FOUND TO BE TRANSI
- [SDR JJBA2020012219005](https://openairdocs.org/sdr/JJBA2020012219005), Jan 19, 2020: WARNING MESSAGE. FALSE ACTIVATION. LG LEVER DISAGREE MASTER WARNING ON TAKE OFF. CHECKED FOR PROPER UP LOCK HOOK POSITIONS. NO FAULTS FOUND. CHECKED PROX SWITCHES FOR CONDITION AND SECURITY. NO D
- [SDR JJBA20200117004](https://openairdocs.org/sdr/JJBA20200117004), Jan 17, 2020: CHARGER. INOPERATIVE. BOTH OVER WING EMERGENCY LIGHTS INOPERATIVE. R&R #4 EMERGENCY LIGHT BATTERY. OPS CHECK FAILED. R&R BATTERY CHARGER ASSEMBLY. OPS CHECK SAT. ORIGINAL BATTERY STI
- [SDR JJBA20190920006](https://openairdocs.org/sdr/JJBA20190920006), Sep 20, 2019: UNKNOWN. NOISY. LEFT OVER WING EMERGENCY EXIT WHISTLES. REMOVED AND REINSTALLED EMERGENCY EXIT AND THEN PERFORMED PRESSURIZATION PROCEDURE. NO DEFECTS NOTED AND LEAK CHECK SAT 
- [SDR JJBA20190830014](https://openairdocs.org/sdr/JJBA20190830014), Aug 30, 2019: ELECTRONIC UNIT. FAULTY. ON APU START SEVERAL EICAS MESSAGES APPEARED AND REMAIN ON. R&R AC STATIC INVERTER. OPS CHECK SAT. ONLY FOR THE MESSAGE 115 VAC BUS OFF. OPS CHECK FAIL FOR ALL 
- [SDR JJBA2019082917013](https://openairdocs.org/sdr/JJBA2019082917013), Aug 17, 2019: ELECTRONIC UNIT. INOPERATIVE. LANDING GEAR AIR/GROUND FAIL ON ROTATION, GEAR WILL NOT RETRACT. R&R LEGU. JACKED AND SWUNG GEAR MULTIPLE TIMES. OPS CHECK SAT. NO OTHER DEFECTS NOTED.
- [SDR JJBA201902273013](https://openairdocs.org/sdr/JJBA201902273013), Feb 23, 2019: UNKNOWN. MALFUNCTIONED. CABIN WILL NOT MAINTAIN PRESSURIZATION OPERATING ON ONE PACK. PERFORMED AIRCRAFT PRESSURIZATION WITH BOTH PACKS OPERATIVE. NO PRESSURE LOSS NOTED. OPS CHECK SAT
- [SDR JJBA20190128036](https://openairdocs.org/sdr/JJBA20190128036), Jan 28, 2019: SENSOR. INOPERATIVE. ON DECENT FROM 8-6000 FEET CREW HAD AURAL AND EICAS MESSAGE. LAV SMOKE WARNING IN FLIGHT PROCEDURE PER QRH PULLED C/B E9 AND E10. NO APU RUNNING. NO SMOKE NOTED
- [SDR JJBA20180524011](https://openairdocs.org/sdr/JJBA20180524011), May 24, 2018: FLOORBEAM. CORRODED. CENTER FLOORBEAM IS CORRODED AT FR 50-61. FABRICATED AND INSTALLED REPAIR DOUBLER ONTO CENTER FLOORBEAM AT FR 59-61. HFEC INSPECTION FOUND NOTED NO DEFECTS IN C
- [SDR JJBA20180312002](https://openairdocs.org/sdr/JJBA20180312002), Mar 12, 2018: LIGHT. DEFECTIVE. EXTERNAL EMERGENCY LIGHT AT MAIN DOOR INOP. TROUBLE SHOT TO BAD CONTACT ASSY. R&R MAIN CABIN DOOR LIGHT ASSY. OPS CK SAT MEL CLEARED.
- [SDR JJBA20180312001](https://openairdocs.org/sdr/JJBA20180312001), Mar 12, 2018: WIRE. BROKEN. EXTERNAL EMERGENCY LIGHT AT LT FORWARD LOWER FAIRING INOP. REMOVED AND REPLACED NR 1 BATTERY CHARGER ASSY FOR EMERGENCY LIGHTS. OPS CHECK FAILED. FOUND BROKEN/C
- [SDR ASOA20161002057C](https://openairdocs.org/sdr/ASOA20161002057C), Oct 2, 2016: BUTTON. FAILED. THE CREW REPORTED WINDSHIELD HEAT NR 1 FAILED IN FLIGHT AND HAD ELECTRICAL BURNING ODOR. MAINTENANCE REPLACED THE WINDSHIELD HEAT SYSTEM PUSH BUTTON. OPS CHECKE
- [SDR ASOA20160112001](https://openairdocs.org/sdr/ASOA20160112001), Jan 12, 2016: VALVE. FAULTY. PILOT REPORTED LOST PRESSURIZATION GOING THROUGH 10,000 FT. MAINTENANCE R & R AIR DISTRIBUTION GROUND CONNECTION VALVE WITH OPS CHECK GOOD. ACFT WAS APPROVED FO
- [SDR ASOA20151226209](https://openairdocs.org/sdr/ASOA20151226209), Dec 26, 2015: BEAM. CORRODED. DURING C-CHECK, BAGGAGE DOOR LOWER CUTOUT CORRODED. R & R CARGO DOOR LOWER CUTOUT SUPPORT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20151212206](https://openairdocs.org/sdr/ASOA20151212206), Dec 12, 2015: SKIN. CRACKED. DURING C-CHECK. FUSELAGE CRACKED AROUND RIVET FRAME 79, STR 5-6L. REPAIRED RIVET AREA ON FUSELAGE AROUND RIVET FROM 79, STR 5L-6L IAW SRM 53-32-01. ACFT APPROVE
- [SDR ASOA20151212205V](https://openairdocs.org/sdr/ASOA20151212205V), Dec 12, 2015: SKIN. CRACKED. DURING C-CHECK. FUSELAGE CRACKED AROUND RIVET FRAME 78, STR 5-6R. REPAIRED AREA ON FUSELAGE AROUND RIVET FROM 78 IAW SRM 53-32-01. ACFT APPROVED FOR RETURN TO S
- [SDR ASOA20150416023C](https://openairdocs.org/sdr/ASOA20150416023C), Apr 16, 2015: FITTING. CRACKED. DURING ROUTINE MAINTENANCE THE NR 1 PYLON FOWARD YOKE FITTING WAS FOUND CRACKED. MAINTENANCE REPLACED THE YOKE FITTING IAW STS EA 26-2014-063.
- [SDR ASOA20141020116](https://openairdocs.org/sdr/ASOA20141020116), Oct 20, 2014: CHARGER. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE FWD OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE R & R THE NR 1 BATTERY CHARGER WITH OPS CHECK GOOD. ACFT
- [SDR ASOA20141017111](https://openairdocs.org/sdr/ASOA20141017111), Oct 17, 2014: TIRE. FAILED. DURING TAKEOFF, NR 2 TIRE BLEW FROM FOD DAMAGE CAUSING MULTIPLE DAMAGES TO THE RT GEAR AUX DOOR. MAINTENANCE R & R THE RT MLG AUX DOOR IAW AMM 32-10-07. ALL WOR
- [SDR ASOA20141015110](https://openairdocs.org/sdr/ASOA20141015110), Oct 15, 2014: ENGINE. FOD. WHILE ON TAKEOFF THE NR 2 TIRE BLEW APART IMBEDDING PART OF TIRE IN THE NR 2 ENGINE AND DAMAGING THE FLAP. THE NR 2 ENGINE WILL BE CHANGED AND THE FLAP TEMPORAR
- [SDR ASOA20140224020](https://openairdocs.org/sdr/ASOA20140224020), Feb 24, 2014: LIGHT. BURNED. CREW REPORTED SMOKE COMING FROM CABIN OVERHEAD LIGHTS AT SEAT 23A. MX INSPECTED AND FOUND LIGHT RECEPTACLE BURNED. R & R SIDEWALL LIGHT ASSY WITH OPS CHECKED GO
- [SDR ASOA20131109271](https://openairdocs.org/sdr/ASOA20131109271), Nov 9, 2013: FITTING. WORN. DURING C-CHECK, THE LT WING AILERON PCA FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE FITTING IAW SRM 51-40-02. THE 
- [SDR ASOA20131109270](https://openairdocs.org/sdr/ASOA20131109270), Nov 9, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01443. ACFT 
- [SDR ASOA20130624334](https://openairdocs.org/sdr/ASOA20130624334), Jun 23, 2013: FLOOR SUPPORT. CRACKED. CENTER OMEGA BEAM SPLICE BETWEEN FRAMES 16 AND 17 CRACKED ON LT SIDE. R & R OMEGA BEAM SPLICE BETWEEN FRAME 16 AND 17.
- [SDR ASOA20130624333](https://openairdocs.org/sdr/ASOA20130624333), Jun 23, 2013: FLOOR SUPPORT. CRACKED. LEFT OMEGA BEAM, RT AND LT SPLICE BETWEEN FRAMES 16 AND 17 CRACKED. R & R OMEGA BEAM SPLICE BETWEEN FRAME 16 AND 17.

All 72: https://openairdocs.org/aircraft/N14143/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/N14143/stcs.md

## Earlier aircraft with N14143

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N14143 before.

- [Cancelled 1971-11-12](https://openairdocs.org/deregistered/N14143-1971-11-12): North American T-28D, S/N 51-3785. Owner: [Winter Wolff & Co](https://openairdocs.org/faa-owner/WINTER%20WOLFF%20%26%20CO), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)

## 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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