# N14148: 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: 145751
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 20, 2003
- Certificate issued: January 31, 2019
- Expires: January 31, 2029
- Mode S code: A0A96C
- 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=14148
- Page: https://openairdocs.org/aircraft/N14148

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/N14148/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 N14148.

## FAA accident and incident reports

None matched to N14148.

## Service difficulty reports (68, 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 JJBA20260526025](https://openairdocs.org/sdr/JJBA20260526025), May 19, 2026: RADOME. DAMAGED. LIGHTNING STRIKE HIT AIRCRAFT. PERFORMED LIGHTNING STRIKE INSPECTION. FOUND DAMAGE TO RADOME, LH & RH SPRING TABS & RH WINGLET. REMOVED AND REPLACED RADOME.
- [SDR JJBA20260427027](https://openairdocs.org/sdr/JJBA20260427027), Apr 27, 2026: LAMP. INOPERATIVE. ROW 3 CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED ROW 3 CEILING EMERGENCY LIGHT. OPS CHECK SAT
- [SDR JJBA20260312007](https://openairdocs.org/sdr/JJBA20260312007), Mar 11, 2026: WIRE. ARCED. DURING OCF, ODOR IN COCKPIT DURING CLIMB 10,000 - 20,000 FT. PERFORM GVI OF RECIRC FAN MUFFLERS & RECIR FANS. R & R BLOWN LT RECIRC MUFFLER. PERFORMED GVI OF LT
- [SDR JJBA20260312006](https://openairdocs.org/sdr/JJBA20260312006), Mar 10, 2026: MUFFLER. BLOWN. STRONG BURNING ELECTRICAL/RUBBER/PLASTIC SMELL DURING CLIMB STARTING IN FLIGHT DECK. OCF REQUESTED. FOUND A PACK 1 WITH A SLIGHT MEK ODOR. FOUND LH RECIRC MUFFL
- [SDR JJBA20251219027](https://openairdocs.org/sdr/JJBA20251219027), Dec 18, 2025: LAMP. INOPERATIVE. COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT. OPS CHECK SAT.
- [SDR JJBA20250417060](https://openairdocs.org/sdr/JJBA20250417060), Apr 15, 2025: LAMP. INOPERATIVE. LH OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT LAMP. OPS CHECK SAT.
- [SDR JJBA20241204001](https://openairdocs.org/sdr/JJBA20241204001), Dec 2, 2024: DISPLAY. FAILED. DURING FLIGHT CAPT MFD FAILED TO BLACK SCREEN FOLLOWED BY SMOKE IN THE COCKPIT. REMOVED AND REPLACED CAPT MFD AND OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. NO M
- [SDR JJBA20240906004](https://openairdocs.org/sdr/JJBA20240906004), Sep 4, 2024: LAMP. INOPERATIVE. EMERGENCY LIGHTS ON CEILING PANELS AT SEATS 3, 18, AND 23 INOPERATIVE. REMOVED AND REPLACED AISLE EMERGENCY LIGHT LAMPS. OPS CHECK SAT.
- [SDR JJBA20240903018](https://openairdocs.org/sdr/JJBA20240903018), Aug 31, 2024: LAMP. INOPERATIVE. LH FWD LOWER FAIRING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH FWD LOWER FAIRING EMERGENCY LIGHT BULB. OPS CHECK SAT.
- [SDR JJBA20240425061](https://openairdocs.org/sdr/JJBA20240425061), Apr 24, 2024: LAMP. INOPERATIVE. OVERWING EMERGENCY LIGHT LAMP INOPERATIVE AT BOTH SEATS. REMOVED AND REPLACED BOTH EMERGENCY LIGHT LAMPS. OPS CHECK SAT
- [SDR JJBA20240314047](https://openairdocs.org/sdr/JJBA20240314047), Mar 12, 2024: WIRE HARNESS. INOPERATIVE. #2 ENG OIL TEMP REACHED 132 DEGREES DURING CLIMB. OIL TEMP STABILIZED AT 122 DEGREES. REMOVED AND REPLACED RH ENG OIL TEMP/PRESS SENSOR. DID NOT FIX. REMOVED AN
- [SDR JJBA20240129047](https://openairdocs.org/sdr/JJBA20240129047), Jan 25, 2024: WIRE. BROKEN. RT EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RH EXT EMERGENCY LIGHT LAMP AND ASSY. NO FIX. VERIFIED CONTINUITY FROM P0782 PIN 7 TO GROUND GS852
- [SDR JJBA20240102035](https://openairdocs.org/sdr/JJBA20240102035), Dec 29, 2023: BATTERY PACK. INOPERATIVE. RH FWD WING EMERGENCY LIGHT OUT. FOUND RH FWD WING, SERVICE DOOR EXIT SIGN, AND FWD LWR RH EMERGENCY EXIT SIGN DIMMING UNTIL OFF. REMOVED AND REPLACED #2 EMERGE
- [SDR JJBA20231023039](https://openairdocs.org/sdr/JJBA20231023039), Oct 20, 2023: UNKNOWN. UNKNOWN. EMERGENCY LIGHT ON MCD INOPERATIVE. REMOVED AND REPLACED MCD LAMP. OPS CHECK FAIL REMOVED MCD LINER. FOUND GROUNDING WIRE NOT ATTACHED TO EMERGENCY LIGHT HOUSIN
- [SDR JJBA20230921042](https://openairdocs.org/sdr/JJBA20230921042), Sep 20, 2023: BATTERY PACK. INOPERATIVE. FOUND FWD CABIN EMERGENCY LIGHT TOP AND BOTTOM ENTRY WAY AND ABOVE FLIGHT ATT SEAT OUT. REMOVED AND REPLACED #1 EMERGENCY BATTERY. OPS CHECK SAT. NO DEFECTS NOT
- [SDR JJBA20230227015](https://openairdocs.org/sdr/JJBA20230227015), Feb 22, 2023: LAMP. INOPERATIVE. AISLE EMERGENCY LIGHTS 3, 4 AND 18CD INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT LAMPS. OPS CHECK SAT
- [SDR JJBA20221227024](https://openairdocs.org/sdr/JJBA20221227024), Dec 25, 2022: UNKNOWN. ODOR. SMELL IN CABIN POSSIBLY PAC. PERFORMED CABIN VISUAL INSPECTION, RE-RUN PACK AND NO SMELL DETECTED. OPS CHECK SAT
- [SDR JJBA20221223019](https://openairdocs.org/sdr/JJBA20221223019), Dec 21, 2022: LIGHT. INTERMITTENT. EMERGENCY LIGHTS NOT ARMED EICAS INTERMITTENTLY DISPLAYED. PERFORMED ELECTRICAL RESET AND OPS TEST FOR EMERGENCY LIGHTING. OPS CHECKED GOOD.
- [SDR JJBA20221125021](https://openairdocs.org/sdr/JJBA20221125021), Nov 23, 2022: ACM. LOCKED. FOUL ODOR ON CLIMB/DESCENT BETWEEN 5000` AND 14000` PERFORMED ROLLS ROYCE FIM. COMPLIED WITH #1 ENGINE BORESCOPE INSPECTION ENGINE FLOWPATH AREA, NO OIL POOLING
- [SDR JJBA20220523038](https://openairdocs.org/sdr/JJBA20220523038), May 23, 2022: NONE. INOPERATIVE. ALL BATTERY 1 EMERGENCY LIGHTS ARE INOPERATIVE. TESTED BATTERY 1. BATTERY VOLTAGE WITHIN LIMITS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND CHARGER #1. OP
- [SDR JJBA20220416022](https://openairdocs.org/sdr/JJBA20220416022), Apr 16, 2022: NONE. UNKNOWN. BRAKE DEGRADE MESSAGE ON EICAS. REMOVED AND REPLACED INBD RH BRAKE CONTROL VALVE. OPS AND LEAK CHECK SAT. PERFORMED TAXI CHECK OF AIRCRAFT. NO DEFECTS NOTED DUR
- [SDR JJBA20220325050](https://openairdocs.org/sdr/JJBA20220325050), Mar 25, 2022: LAMP. INOPERATIVE. OVERWING EMERGENCY LIGHT AT SEAT 18CD INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT AT SEAT 18CD. OPS CHECK SAT
- [SDR JJBA20220216014](https://openairdocs.org/sdr/JJBA20220216014), Feb 16, 2022: NOT REPORTED. NOT REPORTED. SCRATCH ON RH WING L/E #2 SKIN AT 56" FROM INBD EDGE & 12.5" FROM LOWER EDGE. SCRATCH ON RH WING LE #2 AT 56" FROM INBD EDGE & 12.5" FROM LOWER EDGE FOUND OUT O
- [SDR JJBA20220202013](https://openairdocs.org/sdr/JJBA20220202013), Feb 2, 2022: NOT REPORTED. NOT REPORTED. AT CF 4 AREA, CORROSION FOUND ON CENTER OMEGA BEAM FLOOR STRUCTURE BTW FR 59 TO FR 60. CORROSION ON CENTER OMEGA BEAM BTW FR 59 TO 60 FOUND OUT OF LIMITS. CUT-O
- [SDR JJBA20210404011](https://openairdocs.org/sdr/JJBA20210404011), Apr 4, 2021: ARMREST. CRACKED. SEAT 23A, 5A, 4A, 3A, 2A ARMREST STRUCTURE IS CRACKED. REMOVED AND REPLACED SEAT ASSEMBLY 23A, 5A, 4A, 3A, 2A
- [SDR JJBA2020071309001](https://openairdocs.org/sdr/JJBA2020071309001), Jul 9, 2020: SENSOR. MALFUNCTIONED. NR 2 HIGH OIL TEMP INDICATION MAX TEMP NOTED 171 / PERFORMED PRECAUTIONARY ENGINE SHUT DOWN. NO ABNORMAL OIL QUANTITY, PRESSURE, OR ITT. NO EMERGENCY DECLARED, 
- [SDR JJBA2020032623022](https://openairdocs.org/sdr/JJBA2020032623022), Mar 23, 2020: LEVER. BENT. SERVICE DOOR OPEN RED EICAS INDICATION. FOUND TOP RIGHT MICRO SWITCH LEVER TO BE BENT AND LOOSE. R&R MICRO SWITCH LEVER. OPS CHECK SAT. NO DEFECTS AT THIS TIME.
- [SDR ASOA201903215045](https://openairdocs.org/sdr/ASOA201903215045), Mar 21, 2019: CONTROL VALVE. FAULTY. PILOT REPORTED BRAKE DEGRADED AFTER TAXING INTO POSITION ON RUNWAY. A/C RETURN TO GATE. MX REMOVED AND REPLACED THE INBOARD BRAKE CONTROL VALVE WITH OPERATIONAL
- [SDR ASOA2018121723074](https://openairdocs.org/sdr/ASOA2018121723074), Dec 12, 2018: SKIN. CRACKED. DURING C CHECK INSPECTION FOUND REAR FUSELAGE I SKIN CRACKED AT FRAME 75 BETWEEN STR 2R AND 3R. MAINTENANCE REPAIRED I/A/W SRM 53-31-01.
- [SDR ASOA201812175376](https://openairdocs.org/sdr/ASOA201812175376), Dec 5, 2018: CHANNEL. CRACKED. DURING C CHECK INSPECTION FOUND FRAME 10 CHANNEL BRACKET LHS CRACKED BELOW CAPTAINS DV WINDOW. MAINTENANCE REPLACED FRAME 10 CHANNEL BRACKET ON LEFT SIDE.
- [SDR ASOA201812173075](https://openairdocs.org/sdr/ASOA201812173075), Dec 1, 2018: BRACKET. CRACKED. DURING C CHECK INSPECTION FOUND LEFT AILERON DAMPER BRACKET CRACKED. MAINTENANCE REPLACED THE AILERON DAMPER BRACKET.
- [SDR ASOA2018121353073](https://openairdocs.org/sdr/ASOA2018121353073), Nov 25, 2018: FLOOR SUPPORT. CORRODED. LAV CENTER FLOOR BEAM BETWEEN FRAMES 59 AND 61 CORRODED AROUND SCREW HOLES. MAINTENANCE REPLACED LAV FLOOR BEAM BETWEEN FRAME 59 AND 61.
- [SDR ASOA2018120763070](https://openairdocs.org/sdr/ASOA2018120763070), Nov 24, 2018: SKIN. CORRODED. DURING HEAVY CHECK INSPECTION CORROSION WAS FOUND ON THE LOWER FUSELAGE SKIN AT THE RADIO ALTIMETER II LOCATION. FRAME 65 TO FRAME 66.MAINTENANCE REPAIRED I/A/W
- [SDR ASOA2018121093072](https://openairdocs.org/sdr/ASOA2018121093072), Nov 19, 2018: BRACKET. CRACKED. DURING C CHECK INSPECTION THE FLIGHT COMPARTMENT WINDOW STRUCTURE SUPPORTING THE FORWARD FUSELAGE II DOME SKIN WAS FOUND CRACKED. MAINTENANCE PERFORMED SPLICE R
- [SDR ASOA2018122315379](https://openairdocs.org/sdr/ASOA2018122315379), Nov 15, 2018: SKIN. CRACKED. DURING C CHECK INSPECTION FOUND CRACK ON RIGHT WING LOWER SKIN SURFACE ADACENT TO RIB 9. MAINTENANCE REPAIRED I/A/W ETD2018-145-131015.
- [SDR ASOA2018121843077](https://openairdocs.org/sdr/ASOA2018121843077), Nov 14, 2018: RIB. CRACKED. DURING C CHECK INSPECTION FOUND CRACK ON RIGHT WING RIB 21. REPAIRED RIB 21 ON RIGHT WING I/A/W SRM 57-20-07 AND ETD 2018-145-131536
- [SDR ASOA2018110530367](https://openairdocs.org/sdr/ASOA2018110530367), Oct 30, 2018: ACTUATOR. FAILED. THE CREW REPORTED A MAIN PITCH TRIM FAILURE IN CRUISE FLIGHT. MAINTENANCE REPLACED THE HORIZONTAL STABILIZER ACTUATOR. OPS CHECKED GOOD.
- [SDR ASOA20151103131](https://openairdocs.org/sdr/ASOA20151103131), Nov 2, 2015: INVERTER. INOPERATIVE. OVERHEAD EXIT LOCATOR SIGN INOPERATIVE. R & R THE OVERWING EMERGENCY EXIT LOCATOR SIGN AND THE EMERGENCY LIGHT AC/DC INVERTER. OPS CHECK GOOD ACFT RELEASED AND 
- [SDR ASOA20150403033](https://openairdocs.org/sdr/ASOA20150403033), Apr 3, 2015: FIRE DETECTOR. FALSE INDICATION. THE CREW REPORTED AN APU FIRE INDICATION IN FLIGHT, TRANSIENT MESSAGE. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT, FOUND NO INDICATIO
- [SDR ASOA20141226156](https://openairdocs.org/sdr/ASOA20141226156), Dec 26, 2014: SMOKE WARNING. FALSE ACTIVATION. THE CREW REPORTED RECEIVING A LAVATORY SMOKE WARNING DURING CLIMB. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT, PERFORMED 
- [SDR ASOA20131114199](https://openairdocs.org/sdr/ASOA20131114199), Nov 14, 2013: FLAPPER VALVE. WORN. AFTER TAKEOFF FLUID WAS WITNESSED TREAMING FROM THE LT WING. THE CREW ELECTED TO RETURN TO THE AIRPORT WHERE THE AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE FOUND
- [SDR ASOA20130708097](https://openairdocs.org/sdr/ASOA20130708097), Jul 8, 2013: CONTROL PANEL. INOPERATIVE. DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOPERATIVE FROM THE F/A PANEL. MX R & R THE AFFECTED PANEL, OPS TESTED WITH NO DEF
- [SDR ASOA20121120109](https://openairdocs.org/sdr/ASOA20121120109), Nov 20, 2012: CHARGER. INOPERATIVE. DURING MX INSPECTION THE COCKPIT OVERHEAD AND FRONT AISLE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX R & R NR 1 EMERGENCY LIGHT BATERY CHARGER ASSY WITH OPS CH
- [SDR ASOA20120222025H](https://openairdocs.org/sdr/ASOA20120222025H), Feb 22, 2012: FIRE LOOP. FALSE ACTIVATION. THE CREW REPORTED AN APU FIRE IN FLIGHT. THE ACFT LANDED WITHOUT INCIDENT WHERE MX INSPECTED THE ACFT WITH NO EVIDENCE OF, OR INDICATION OF FIRE. REMOVED AND RE
- [SDR ASOA20120221026](https://openairdocs.org/sdr/ASOA20120221026), Feb 21, 2012: SMOKE DETECTOR. FALSE ACTIVATION. THE CREW REPORTED A LAVATORY SMOKE MESSAGE ON EICAS. MX R & R THE LAVATORY SMOKE DETECTOR, OPERATIONALLY TESTED WIH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FO
- [SDR C2XA11RI162](https://openairdocs.org/sdr/C2XA11RI162), Oct 9, 2011: SMOKE DETECTOR. DEFECTIVE. FLT 4614 STL-EWR. CREW REPORTED LAV SMOKE WARNING DURING FLIGHT WITH NO SMELL OR SIGN OF FIRE OR SMOKE. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB14
- [SDR C2XA11IA038](https://openairdocs.org/sdr/C2XA11IA038), Mar 1, 2011: TRIM SWITCH. INOPERATIVE. MCI - FLIGHT 6208, THE CREW REPORTED THE F/O'S PITCH TRIM SWITCH WAS INOPERATIVE. THE AIRCRAFT RETURNED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REM
- [SDR C2XA11SH050](https://openairdocs.org/sdr/C2XA11SH050), Mar 1, 2011: LINE. DAMAGED. SHV - BLEED 1 OVERTEMP MESSAGE ON EICAS. REMOVED AND REPLACED FLEXIBLE REFERNCE LINE ON AFT BLEED 1 THERMOSTAT IAW EMB 145 AMM 20-10-03. AIRCRAFT WAS APPROVED F
- [SDR C2XA10CL148](https://openairdocs.org/sdr/C2XA10CL148), Sep 17, 2010: ACTUATOR. MALFUNCTIONED. THE CREW REPORTED A "PITCH TRIM BACKUP" INOP MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE HORIZONTAL STAB ACTUATOR. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10RI114](https://openairdocs.org/sdr/C2XA10RI114), Sep 13, 2010: CONTROL UNIT. INOPERATIVE. FLIGHT 2968 - BOS - FLIGHT CREW REPORTED MAIN AND BACK UP TRIM INOPERATIVE AT FL350, AND NOSE PITCHED UP 3 DEG. EWR MX REMOVED AND REPLACED PITCH TRIM ACTUATOR 

All 68: https://openairdocs.org/aircraft/N14148/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/N14148/stcs.md

## Earlier aircraft with N14148

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N14148 before.

- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N14148-undated-27-4710): Piper PA-23-250, S/N 27-4710. Owner: [Piper Aircraft Lockhaven](https://openairdocs.org/faa-owner/PIPER%20AIRCRAFT%20LOCKHAVEN)
- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N14148-undated-301): Bosworth Cecil BOSWORTH-LONGSTER HL, S/N 301, built 1934. Owner: [Briggs Benjamin](https://openairdocs.org/faa-owner/BRIGGS%20BENJAMIN), [Charlotte, MI](https://openairdocs.org/faa-place/MI/Charlotte)

## 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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