# N14125: 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: 145690
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2005
- Certificate issued: July 30, 2019
- Expires: July 31, 2029
- Mode S code: A0A923
- 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=14125
- Page: https://openairdocs.org/aircraft/N14125

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/N14125/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 N14125.

## 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 20250526004909I](https://openairdocs.org/incident/20250526004909I), May 26, 2025: Embraer EMB-145XR (N14125), Washington, DC, Minor damage. Flight [privacy data omitted]reported a bird strike on an extended downwind for rwy 19 landing iad. The aircraft was at 3000 ft when the event occurred with no…

## Reports on N14125 not matched to an aircraft (1)

They name N14125, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19970322010289I](https://openairdocs.org/incident/19970322010289I), Mar 22, 1997: Cessna 182P (N14125), Wichita, KS, Minor damage. Narrative: pilot started aircraft on gpu power after previous unsuccessful attempts resulted in a depleted battery. Engine went to full throttle. Pilot was…

## Service difficulty reports (100, 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 JJBA20260323009](https://openairdocs.org/sdr/JJBA20260323009), Mar 22, 2026: BATTERY PACK. INOPERATIVE. SEVERAL EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BPS2. OPS CHECK GOOD.
- [SDR JJBA20251125110](https://openairdocs.org/sdr/JJBA20251125110), Nov 25, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT #2 BPS INOPERATIVE. REMOVED AND REPLACED #2 BPS. OPS CHECK GOOD.
- [SDR JJBA20250728091](https://openairdocs.org/sdr/JJBA20250728091), Jul 27, 2025: SIGN. INOPERATIVE. EXIT ROW OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN. NO DEFECTS NOTED.
- [SDR JJBA20250602094](https://openairdocs.org/sdr/JJBA20250602094), May 27, 2025: SKIN. DAMAGED. DAMAGE TO RIGHT SIDE OF NOSE AT FRAME 7, BETWEEN STRINGER 6R AND 9R. FOUND DENT LOCATED AT FRAME 7 BETWEEN STRINGER 6R AND 9R. FOUND SKIN CREASES BETWEEN FRAME 
- [SDR JJBA20250318014](https://openairdocs.org/sdr/JJBA20250318014), Mar 18, 2025: LIGHT. MISINSTALLED. FLOOR EMERGENCY EXIT STRIP BACKWARDS AT 1A. REINSTALLED EMERGENCY STRIP CORRECTLY.
- [SDR JJBA20250303010](https://openairdocs.org/sdr/JJBA20250303010), Mar 1, 2025: DUCT. UNSECURE. ON DEPARTURE SMOKE COMING OUT OF VENT AT SEAT 7A. SMOKE FOUND TO BE CONDENSATION/VAPOR FROM PACKS SYSTEM. INSPECTED WATER SPRAY NOZZLES. NO DEFECTS NOTED. UPON 
- [SDR JJBA20250210010](https://openairdocs.org/sdr/JJBA20250210010), Feb 10, 2025: LAMP. INOPERATIVE. RH SIDE CENTER FAIRING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RH SIDE CENTER FAIRING EMERGENCY LIGHT. OPS CHECK SAT.
- [SDR JJBA20241125008](https://openairdocs.org/sdr/JJBA20241125008), Nov 22, 2024: BATTERY PACK. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS/EXIT SIGNS ARE INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPS CHECK SAT.
- [SDR JJBA20241003002](https://openairdocs.org/sdr/JJBA20241003002), Oct 2, 2024: INVERTER. INOPERATIVE. AFT OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED AFT OVERHEAD EMERGENCY EXIT SIGN. OPS CHECK FAILED. REMOVED AND REPLACED #4 EMERGENCY LIGHT D
- [SDR JJBA20230424009](https://openairdocs.org/sdr/JJBA20230424009), Apr 20, 2023: LAMP. INOPERATIVE. RH EXTERNAL OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RH OVERWING EMERGENCY BULB. OPS CHECK SAT
- [SDR JJBA20230315016](https://openairdocs.org/sdr/JJBA20230315016), Mar 10, 2023: UNKNOWN. UNKNOWN. LIGHTNING STRIKE DURING DECENT THROUGH 8,000. PERFORMED LIGHTNING STRIKE INSPECTION. ALL 5 DISPLAY UNITS MAGNETIZED DUE TO LIGHTNING STRIKE. REMOVED AND REPLACE
- [SDR JJBA20230303002](https://openairdocs.org/sdr/JJBA20230303002), Mar 1, 2023: LAMP. INOPERATIVE. COCKPIT CEILING EMERGENCY LIGHT OUT. REMOVED AND REPLACED COCKPIT CEILING EMERGENCY LIGHT. OPS CHECK SAT.
- [SDR JJBA20221227023](https://openairdocs.org/sdr/JJBA20221227023), Dec 23, 2022: BATTERY PACK. INOPERATIVE. RH FWD EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RH FWD EXTERNAL EMERGENCY LIGHT. REMOVED AND REPLACED #2 EMERGENCY LIGHT BATTERY. OPS CHECK SA
- [SDR JJBA20211211008](https://openairdocs.org/sdr/JJBA20211211008), Dec 11, 2021: LAMP. INOPERATIVE. INOPERATIVE AISLE EMERGENCY LIGHT LAMP LOCATED AT WING EMERGENCY EXIT. REMOVED AND REPLACED AISLE EMERGENCY LIGHT LAMP LOCATED AT WING EMERGENCY EXIT. OPS CHECK
- [SDR JJBA20211017029](https://openairdocs.org/sdr/JJBA20211017029), Oct 17, 2021: NONE. NONE. LARGE EXIT SIGN NEXT TO RH EMERGENCY EXIT DOOR DOES NOT ILLUMINATE. R&R EXIT MARKING SIGN ASSEMBLY. OPS CHECK SAT
- [SDR JJBA202108250056](https://openairdocs.org/sdr/JJBA202108250056), Aug 20, 2021: RIB. CRACKED. FF2, LH FUSE OVER WINDSHIELD, RIB OVER HEAD PANEL HORIZONTAL CRACKED AT ANCHOR NUT LOCATION. PANEL REPAIRED
- [SDR JJBA2021082518054](https://openairdocs.org/sdr/JJBA2021082518054), Aug 18, 2021: DOUBLER. CORRODED. CORROSION ON LOWER REAR FUSE 1, ON ANTENNA DOUBLER FOR AFT RADIO ALTIMETER #2 BTW FR 68-69. SKIN REPAIRED.
- [SDR JJBA2021082517055](https://openairdocs.org/sdr/JJBA2021082517055), Aug 17, 2021: DOUBLER. CORRODED. CORROSION ON LOWER REAR FUSE 1, ON ANTENNA DOUBLER FOR FWD RADIO ALTIMETER #2 BTW FR 65-56. SKIN REPAIRED.
- [SDR JJBA2021082017046](https://openairdocs.org/sdr/JJBA2021082017046), Aug 17, 2021: FRAME. CRACKED. FR 59 BTW STR 16-17 FOUND CRACKED. CRACKED SECTION OF FRAME 59, BTW STR 16-17. REMOVED FOR REPAIR. REPAIR PARTS FOR CRACKED FR 59, BTW STR 16-17 LOCALLY FABRICA
- [SDR JJBA20210817043](https://openairdocs.org/sdr/JJBA20210817043), Aug 17, 2021: FLOOR SUPPORT. CORRODED. ON CF3:CENTER OMEGA BEAM BTW FR46-53 LOWER FLANGE CORRODED. CF3, CENTER BEAM BLENDED OUT OF LIMITS BTW FR 47 & 48. PERFORMED CUT OUT BTW FR 47 & 48. CF3 CENTER 
- [SDR JJBA20210810044](https://openairdocs.org/sdr/JJBA20210810044), Aug 10, 2021: YOKE. CRACKED. FOLLOWING NDT INSPECTION ON TASK 54-50-00-255-803-A00, 2X CRACKS FOUND ON PYLON YOKES UPPER FLANGE 2X HOLES LOCATIONS. OPEN L/H AND R/H PYLON YOKES UPPER FLANGE
- [SDR JJBA20210810041](https://openairdocs.org/sdr/JJBA20210810041), Aug 10, 2021: SKIN. DENTED. DENT WITH RIVET PLUGS ON R/H LOWER FWD FUSE 2, BTW FR 11-12 AND BTW STR 20R-21R. PERFORMED CUT-OUT ON R/H LOWER FWD FUSE 2, BTW FR 11-12 AND BTW STR 20R-21R. PR
- [SDR JJBA20210809047](https://openairdocs.org/sdr/JJBA20210809047), Aug 9, 2021: FLOOR SUPPORT. CORRODED. CF1, R/H, BEAM HAT SECTION, BTW FRAMES 18-20, FOUND CORRODED. ON CF1, R/H, BEAM HAT SECTION, BTW FR18-20 BLENDED AND FOUND OUT OF LIMIT. ON CF1, R/H, BEAM HAT S
- [SDR JJBA20210809045](https://openairdocs.org/sdr/JJBA20210809045), Aug 9, 2021: SHEAR TIE. CRACKED. RF1, AT FR 71 BTW STR 6L-10L, SHEAR CLIP CRACKED. SHEAR CLIP FR 71 BTW STR 6L-10L WAS REMOVED. RF 1, AT FR 71 BTW STR 6L-10L, NEW SHEAR CLIP LOCALLY FABRICATED.
- [SDR JJBA20210809040](https://openairdocs.org/sdr/JJBA20210809040), Aug 9, 2021: FRAME. CORRODED. RF1, AT FR 65, FRAME UPPER Z SECTION CORRODED AT ANCHOR NUT LOCATIONS RF1, FR65 ON FRAME UPPER Z AT ANCHOR NUT LOCATION, FRAME BLENDED OUT OF LIMIT. RF1, FR65 R
- [SDR JJBA20210404009](https://openairdocs.org/sdr/JJBA20210404009), Apr 4, 2021: ARMREST. CRACKED. SEAT 23A, 20A, 10A, 9A, 8A, 5A, 4A, 3A ARMREST STRUCTURE IS CRACKED. R&R SEAT ASSEMBLY AT 23A, 20A, 10A, 9A, 8A, 5A, 4A, 3A
- [SDR JJBA20210327030](https://openairdocs.org/sdr/JJBA20210327030), Mar 27, 2021: SEAL. DETERIORATED. DECLARED EMERGENCY, DUE TO LOUD NOISE FROM DV WINDOW CAPT SIDE. UPON RETURN TO HRL DETECTED DV WINDOW SEAL ON CAPT SIDE COMING APART. R&R CAPT SIDE DV WINDOW SE
- [SDR JJBA20210205009](https://openairdocs.org/sdr/JJBA20210205009), Feb 5, 2021: LIGHT. UNSECURE. PHOTO LUMINESCENT STRIP DOES NOT ILLUMINATE PROPERLY (HAS BREAKS). RE SECURED PHOTO LUMINESCENT STRIP.
- [SDR JJBA20201212016](https://openairdocs.org/sdr/JJBA20201212016), Dec 12, 2020: SKIN. CRACKED. CRACK ON LOWER REAR FUSE 1, BETWEEN FR 75-75A AND BETWEEN STR 21L-21R. ON LOWER REAR FUSE 1, BETWEEN FR 75-75A BETWEEN STR 21L-21R, PAINT STRIPPED FOR INVESTIGA
- [SDR JJBA20201212018](https://openairdocs.org/sdr/JJBA20201212018), Dec 12, 2020: SKIN. DENTED. DENT ON FWD FUSE 1 BETWEEN FRAMES 3-4 STR 9-11R. DOUBLER AND FILLER FABRICATED, LOCATED AND DRILLED. DENT ON FWD FUSE BETWEEN FR 3-4 STR 9-11R, REPAIRED.
- [SDR JJBA20201207008](https://openairdocs.org/sdr/JJBA20201207008), Dec 7, 2020: SKIN. CANNING. DENT WITH OIL CANNING EFFECT ON LT CENTER FUSE 1, BETWEEN FR 22-23 AND BETWEEN STR 14P-15P. DENT WITH OIL CANNING AT LT CENTER FUSE 1, BETWEEN FR 22-23 AND BETW
- [SDR JJBA20201207007](https://openairdocs.org/sdr/JJBA20201207007), Dec 7, 2020: SKIN. CANNING. DENT WITH OIL CANNING EFFECT ON LT CENTER FUSE 1, BETWEEN FR 20-21 AND BETWEEN STR 13P-14P. DENT WITH OIL CANNING AT LT CENTER FUSE 1, BETWEEN FR 20-21, AND BET
- [SDR RAIA2020031960001](https://openairdocs.org/sdr/RAIA2020031960001), Mar 16, 2020: FILTER. DIRTY. BLEED 1 OVERHEAT. INSPECTED & RAN BLLED 1 ADJUSTMENT AND TEST. NO FAULTS FOUND. CLEANED FAN AIR VALVE FILTER. OPS CHECK GOOD.
- [SDR RAIA2019100740001](https://openairdocs.org/sdr/RAIA2019100740001), Oct 4, 2019: WIRE HARNESS. SPARKS. PAX AT 24CD NOTICED SPARKS AND FUMES COMING FROM OVERHEAD AREA NEAR SIDEWALL. R & R THE LIGHT ASSY HARNESS. OPS CHECKED GOOD .
- [SDR RAIA201907190002](https://openairdocs.org/sdr/RAIA201907190002), Jul 18, 2019: LIGHT. INOPERATIVE. RT FWD WING EMERGENCY FLOOD LIGHT (LIGHT # 4) IS INOP. R&R RT FWD WING EMERGENCY FLOOD LIGHT BULB. OPS CHECK GOOD.
- [SDR RAIA201907190001](https://openairdocs.org/sdr/RAIA201907190001), Jul 18, 2019: BATTERY. WEAK. SERVICE DOOR EXIT IDENTIFIER (LIGHT #10) IS INOP. R&R #2 EMERGENCY BATTERY POWER SUPPLY. OPS CHECK GOOD.
- [SDR RAIA201905020001](https://openairdocs.org/sdr/RAIA201905020001), May 2, 2019: WARNING SYSTEM. FALSE ACTIVATION. ON CLIMBOUT BAG DOOR OPEN & CABIN FAIL TO PRESSURIZE. CLOSED BAG DOOR & PERFORMED PRESSURIZATION. BAG DOOR INDICATION NORMAL. NO LEAKS NOTED.
- [SDR RAIA2019042110003](https://openairdocs.org/sdr/RAIA2019042110003), Apr 11, 2019: GUSSET. CORRODED. CENTER GUSSET AT FRAMEV59 HAS SIGNS OF CORROSION. REMOVED AND RPLACED CENTER GUSSET AT FRAME 59
- [SDR RAIA2019042110002](https://openairdocs.org/sdr/RAIA2019042110002), Apr 11, 2019: FLOORBOARD. CORRODED. R/H DIGITAL OF SERVICE DOOR AT FLOORBOARD 232DF HAS CORROSION AROUND SCREW HOLE .........REMOVED CORRODED SECTION FABRICATED DOUBLER INSTALLED DOUBLER ON R/N DI
- [SDR RAIA2019042110001](https://openairdocs.org/sdr/RAIA2019042110001), Apr 11, 2019: FLOOR SUPPORT. CORRODED. L/H OMEGA BEAM DIGITAL AT FRAME 18 AFT U CHANEL OF PAX DOOR HAS CORROSION. REMOVED AND REPLACED U CHANEL AFT OF PAX DOOR
- [SDR RAIA2019042390003](https://openairdocs.org/sdr/RAIA2019042390003), Apr 9, 2019: SUPPORT. CRACKED. CARGO BAY FWD RAMP ANGLE AND UPPER AND LOWER SUPPORTS ARE CRACKED ......REMOVED AND REPLACED CARGO BAY FWD RAMP ANGLE AND UPPER AND LOWER SUPPORTS
- [SDR RAIA2019042390002](https://openairdocs.org/sdr/RAIA2019042390002), Apr 9, 2019: ANGLE. CORRODED. CARGO BAY DOOR CUT OUT Z ANGLE HAS CORROSION......REMOVE AND REPLACED CARGO BAY DOOR CUTOUT Z ANGLE
- [SDR RAIA2019042390001](https://openairdocs.org/sdr/RAIA2019042390001), Apr 9, 2019: ANGLE. CRACKED. CARGO BAY AFT RAMP ANGLE AND UPPER AND LOWER SUPPORTS ARE CRACKED...........REMOVED AND REPLACED CARGO BAY AFT RAMP ANGLE AND UPPER AND LOWER SUPPORTS
- [SDR RAIA201902150001](https://openairdocs.org/sdr/RAIA201902150001), Feb 15, 2019: UNKNOWN. SMOKE. SMOKE IN THE COCKPIT. PERFORMED FIM TASK 21-20-00. NO DEFECTS NOTED. NO SMOKE DETECTED DURING ENGINE RUNS.
- [SDR RAIA2019020860001](https://openairdocs.org/sdr/RAIA2019020860001), Feb 6, 2019: THERMOSTAT. FAILED. BLEED 1 OVERTEMP EICAS MSG ON CLIMBOUT. PERFORMED QRH CHECKLIST, MESSAGE CLEARED. R/R HIGH TEMP THERMOSTAT. PERFORMED OPS CHECK. OPS CHECK GOOD.
- [SDR RAIA201810100002](https://openairdocs.org/sdr/RAIA201810100002), Oct 10, 2018: ANTI-ICE SYSTEM. FAILED. ENGINE NR 1 ANTI-ICE FAIL WHILE IN ICING CONDITIONS. DEFERRED E-1 ANTI-ICE VALVE. MORE INFORMATION WHEN AVAILABLE.
- [SDR RAIA2018072410001](https://openairdocs.org/sdr/RAIA2018072410001), Jul 21, 2018: GENERATOR. MALFUNCTIONED. GEN 3 OFF BUSS EICAS MESSAGE. R&R NR 3 ENG GEN OPS CHECK GOOD AT THIS TIME.
- [SDR RAIA2018071311001](https://openairdocs.org/sdr/RAIA2018071311001), Jul 11, 2018: BOLT. LOOSE. POST FLIGHT, FOUND CABIN DOOR HARD TO OPEN. FOUND 2 EACH BOLTS LOOSE ON INTERIM HANDLE BRACKET. TIGHTENED BOLTS. OPS CHECK GOOD.
- [SDR RAIA20180602001](https://openairdocs.org/sdr/RAIA20180602001), May 31, 2018: UNKNOWN. UNKNOWN. ELEVATOR CONTROL CABLES FELT STIFF, LIKE THE CABLES WERE RUBBING. PERFORMED VISUAL INSPECTION OF ELEVATOR CONTROL CABLES. NO DISCREPANCIES NOTED. ISOLATED THE E
- [SDR RAIA201803270001](https://openairdocs.org/sdr/RAIA201803270001), Mar 27, 2018: CLAMP. LOOSE. NR 1 BLEED LEAK DURING FLIGHT. BLEED LEAK CHECKED. FOUND MULTIPLE LEAKS IN PYLON. LOOSENED AND TIGHTENED ALL CLAMPS. LEAK TESTED GOOD.

All 100: https://openairdocs.org/aircraft/N14125/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/N14125/stcs.md

## Earlier aircraft with N14125

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N14125 before.

- [Cancelled 1951-04-24](https://openairdocs.org/deregistered/N14125-1951-04-24): Aeronca C-3, S/N A-425. Owner: [Hamilton Raymond B](https://openairdocs.org/faa-owner/HAMILTON%20RAYMOND%20B), [Vicksburg, MS](https://openairdocs.org/faa-place/MS/Vicksburg)

## 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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