# N14188: 2005 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: 14500929
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 21, 2005
- Certificate issued: August 25, 2020
- Expires: August 31, 2027
- Mode S code: A0A9F8
- 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=14188
- Page: https://openairdocs.org/aircraft/N14188

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/N14188/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 N14188.

## 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 20120225003189I](https://openairdocs.org/incident/20120225003189I), Feb 25, 2012: Embraer EMB-145XR (N14188), Chicago, IL, No damage. Flight attendant became nauseous and called the captain to inform him that she was not well. The captain sent a deadheading pilot to check on the flight…

## Service difficulty reports (57, 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 JJBA20260702002](https://openairdocs.org/sdr/JJBA20260702002), Jul 1, 2026: HANDLE. MISINSTALLED. EXIT ROW LEFT SIDE EXIT DOOR UPPER GRAB HANDLE INSTALLED UPSIDE DOWN. LT EMERGENCY EXIT UPPER GRAB HANDLE INSTALLED PROPERLY.
- [SDR JJBA20260624016](https://openairdocs.org/sdr/JJBA20260624016), Jun 22, 2026: LAMP. INOPERATIVE. AISLE EMERGENCY LIGHT IN ROW 3 INOPERATIVE. REMOVED AND REPLACED AISLE EMERGENCY LIGHT. OPS CHECK SAT.
- [SDR JJBA20260209023](https://openairdocs.org/sdr/JJBA20260209023), Feb 6, 2026: SENSOR. INOPERATIVE. FLAP FAIL MESSAGE WHEN ON APPROACH. REMOVED AND INSTALLED FLAP POWER DRIVE UNIT. INSTALLED CANNON PLUGS AND FLEXIBLE SHAFTS - DURING OPS CHECK FOUND FLAP POWER 
- [SDR JJBA20251231039](https://openairdocs.org/sdr/JJBA20251231039), Dec 29, 2025: THRUST REVERSER. DAMAGED. LEFT ENGINE THRUST REVERSER FWD OUTBOARD EDGE DAMAGED AND TORN. THE REPAIR HAS BEEN COMPLETED.
- [SDR JJBA20251231038](https://openairdocs.org/sdr/JJBA20251231038), Dec 29, 2025: SKIN. DENTED. APU COWLING LOWER SKIN FOUND WITH TWO PROTRUSIONS. DENTS 1 AND 2 WERE REPAIRED. DENT 3 IS FREE OF SHARP EDGES AND THERE ARE NO SIGNS OF MISSING OR PULLED FASTEN
- [SDR JJBA20251231036](https://openairdocs.org/sdr/JJBA20251231036), Dec 26, 2025: SKIN. DAMAGED. APU COWLING WITH SKIN DAMAGED ON REAR EDGE LH AREA. APU COWLING SKIN ON FR06 FOUND WITH SEVERAL CRACKS ON EDGE. WORK WAS PERFORMED ON THE APU COWLING ACCOMPLISH
- [SDR JJBA20251231037](https://openairdocs.org/sdr/JJBA20251231037), Dec 23, 2025: DOOR FRAME. DAMAGED. AFT TOP CORNER OF BAGGAGE DOOR AIRFRAME SIDE MISSING A SECTION OF MATERIAL WHERE BAGGAGE DOOR MATES COMPLY WITH PERMANENT REPAIR. PERMANENT REPAIR WAS PERFORMED
- [SDR JJBA20251226032](https://openairdocs.org/sdr/JJBA20251226032), Dec 12, 2025: FLOOR PANEL. CRACKED. CRACKS ON FLOOR PANELS 262AF AND 262BF. REPAIR WAS PERFORMED.
- [SDR JJBA20251226034](https://openairdocs.org/sdr/JJBA20251226034), Dec 11, 2025: NUT. CORRODED. ALL FOUR APU COWLING ATTACH SPHERICAL NUTS RUSTED AND BOLTS ALSO. REMOVAL OF RUST WAS PERFORMED.
- [SDR JJBA20251211033](https://openairdocs.org/sdr/JJBA20251211033), Dec 11, 2025: PLATE. SCRATCHED. NOSE LANDING GEAR WELL WALL RH FOUND WITH SCRATCHES ON PLATE. DIGITAL PLATE WAS REPLACED.
- [SDR JJBA20251024063](https://openairdocs.org/sdr/JJBA20251024063), Oct 20, 2025: PLATE. CRACKED. RH AILERON DAMPER MOUNT PLATE CRACKED. FULLY REMOVED RH AILERON ASSY AND INSTALLED NEW AILERON.
- [SDR JJBA20250602095](https://openairdocs.org/sdr/JJBA20250602095), May 29, 2025: LIGHT. MISINSTALLED. RH OVERWING EXTERNAL EMERGENCY LIGHT INSTALLED UPSIDE DOWN. REMOVED AND REINSTALLED RH OVERWING EXTERNAL EMERGENCY LIGHT IN CORRECT POSITION.
- [SDR JJBA20250507032](https://openairdocs.org/sdr/JJBA20250507032), May 6, 2025: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS ON INTERIOR FAILED OPS CHECK. CHARGED BATTERIES. PERFORMED CHECK OF EMERGENCY LIGHTING SYSTEM. OPS CHECK SAT
- [SDR JJBA20240916012](https://openairdocs.org/sdr/JJBA20240916012), Sep 13, 2024: WIRE. DAMAGED. MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. FOUND INCOMPLETE / DIRTY GROUND. CLEANED AND REINSTALLED GROUND WIRE TERMINAL. OPS CHECK SAT
- [SDR JJBA20240916010](https://openairdocs.org/sdr/JJBA20240916010), Sep 10, 2024: LAMP. INOPERATIVE. EMERGENCY EXIT AISLE CEILING LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT CEILING LAMP. OPS CHECK SAT.
- [SDR JJBA20240916009](https://openairdocs.org/sdr/JJBA20240916009), Sep 10, 2024: LAMP. INOPERATIVE. MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN DOOR EMERGENCY EXIT LAMP. OPS CHECK SAT
- [SDR JJBA20230410004](https://openairdocs.org/sdr/JJBA20230410004), Apr 8, 2023: UNKNOWN. UNKNOWN. #1 EMERGENCY LIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY. OPS CHECK SAT
- [SDR JJBA20230130021](https://openairdocs.org/sdr/JJBA20230130021), Jan 17, 2023: FLOOR SUPPORT. CORRODED. CF 3, LH OMEGA BEAM #6 INBD FLANGE BTWN FRAME 47-53 FOUND CORRODED. CF3, LH OMEGA BEAM #6 INBD FLANGE BLENDED OUT OF LIMITS. CF3, LH OMEGA BEAM TRIM REMOVED FOR
- [SDR JJBA20230130018](https://openairdocs.org/sdr/JJBA20230130018), Jan 17, 2023: FRAME. CRACKED. CF 4, FRAME 59, LH FRAME SECTION FOUND CRACKED BTW STR 15L-16L. CF4, FR59, LH FRAME SECTION SPLICE BTW STR 14L-16L REMOVED FOR ACCESS. CF4, FR59, LH FRAME SECTI
- [SDR JJBA20230130020](https://openairdocs.org/sdr/JJBA20230130020), Jan 16, 2023: SKIN. DAMAGED. FWD FUSELAGE EXT, DAMAGE FOUND ON LH SIDE SKIN BTW FR 9-10 AND BTW STR 13L-15L. FWD FUSELAGE EXT, L SIDE SKIN BTW FR 9-10 AND BTW STR 13L-15L, DAMAGE BLENDED FO
- [SDR JJBA20230130019](https://openairdocs.org/sdr/JJBA20230130019), Jan 16, 2023: FLOOR SUPPORT. CRACKED. CF2, LH OMEGA BEAM #3 CRACKS SUSPECTED FOUND AT FRAME 33-34 ON FLOOR STRUCTURE. AFTER NDT INSPECTION, TWO CRACKS CONFIRMED ON LH OMEGA BEAM #3 AT FR33 AND FR 34
- [SDR JJBA20220525055](https://openairdocs.org/sdr/JJBA20220525055), May 25, 2022: NONE. SEIZED. SMOKE AND FUMES IN THE COCKPIT AND CABIN. FOUND PACK 1 ACM TO BE SEIZED. REMOVED AND REPLACED LH ACM/ OPS CHECK GOOD.
- [SDR JJBA20210604010](https://openairdocs.org/sdr/JJBA20210604010), Jun 4, 2021: BATTERY PACK. INOPERATIVE. RH EMERGENCY LIGHT INOPERATIVE. R&R LIGHT BULB. OPS CHECK NOT SAT. REMOVED AND REPLACED #2 BATTERY POWER SUPPLY, OPS CHECK SAT.
- [SDR ASOA2019121633069](https://openairdocs.org/sdr/ASOA2019121633069), Dec 13, 2019: SIGN. INOPERATIVE. DURING C CHECK INSPECTION FOUND EMERGENCY EXIT SIGN ABOVE FORWARD F/A SEAT INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN. OPERATIONAL CHECKS WERE GO
- [SDR ASOA2019121633068](https://openairdocs.org/sdr/ASOA2019121633068), Dec 13, 2019: INVERTER. INOPERATIVE. DURING C CHECK INSPECTION FOUND #1 INVERTER FOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED #1 EMERGENCY LIGHT INVERTER, OPERATIONAL CHECKS WERE GOOD.
- [SDR ASOA2019112683065](https://openairdocs.org/sdr/ASOA2019112683065), Oct 28, 2019: FLOOR SUPPORT. CORRODED. DURING C CHECK INSPECTION FOUND FLOORBOARD SILL CORRODED AT FRAME 18-23 LEFT SIDE. MAINTENANCE REPLACED FLOORBOARD SILL AT FRAME 18-23.
- [SDR ASOA2019112073059](https://openairdocs.org/sdr/ASOA2019112073059), Oct 27, 2019: GUSSET. CORRODED. DURING C CHECK INSPECTION FOUND LAV LEFT GUSSET CORRODED AROUND FORWARD SCREW HOLE. MAINTENANCE REPLACED LAV LEFT HAND GUSSET.
- [SDR ASOA201912043066](https://openairdocs.org/sdr/ASOA201912043066), Oct 24, 2019: SKIN. DENTED. DURING C CHECK INSPECTION FOUND MAIN CABIN DOOR EDGE SKIN DENTED AT LOWER AFT CORNER. MAINTENANCE REPAIRED I/A/W ETD2019-145-156108 AND SRM 52-10-01
- [SDR ASOA2019112043063](https://openairdocs.org/sdr/ASOA2019112043063), Oct 24, 2019: PIN. CORRODED. DURING C CHECK INSPECTION FOUND RIGHT SIDE HORIZONTAL STABILIZER HINGE PIN CORRODED. MAINTENANCE REPLACED RIGHT HORIZONTAL STABILIZER HINGE PIN.
- [SDR ASOA2019112133064](https://openairdocs.org/sdr/ASOA2019112133064), Oct 23, 2019: HINGE PIN. CORRODED. DURING C CHECK INSPECTION FOUND LEFT HAND HORIZONTAL STABILIZER HINGE PIN CORRODED. MAINTENANCE REPLACED LEFT HAND HORIZONTAL STABILIZER HINGE PIN.
- [SDR ASOA2019112033062](https://openairdocs.org/sdr/ASOA2019112033062), Oct 23, 2019: FLOORBEAM. CORRODED. DURING C CHECK INSPECTION FOUND FLOORBEAM AT FRAME 62 /STRINGER 16R TO BE CORRODED. MAINTENANCE REPLACED CORRODED FLOORBEAM AT FRAME 62/ STRINGER 16
- [SDR ASOA2019112023061](https://openairdocs.org/sdr/ASOA2019112023061), Oct 22, 2019: FLOOR SUPPORT. CORRODED. DURING C CHECK INSPECTION FOUND LEFT HAND FLOOR SILL CORRODED @ AFT SCREW HOLE FRAME 59. MAINTNENACE REPLACED LEFT FLOOR SILL @FRAME 53-59,
- [SDR ASOA2019112023060](https://openairdocs.org/sdr/ASOA2019112023060), Oct 22, 2019: GUSSET. CORRODED. DURING C CHECK INSPECTION FOUND CENTER LAV GUSSET CORRODED @AFT SCREW HOLE. MAINTNENACE REPLACED THE LAV CENTER GUSSET.
- [SDR ASOA2019021593015](https://openairdocs.org/sdr/ASOA2019021593015), Feb 9, 2019: SKIN. CRACKED. DURING SCHEDULED MAINTNENACE CHECKS FOUND SKIN DAMAGE AT THE #2 RADIO ALTIMETER BASE BETWEEN FRAMES 68-69 AND STRINGERS 21L-21R. THE DAMAGE IS IN THE FORM OF CR
- [SDR ASOA2018121424071](https://openairdocs.org/sdr/ASOA2018121424071), Dec 12, 2018: SKIN. DENTED. IAH FLIGHT 4446, DURING GROUND INSPECTION A DENT WAS FOUND ON THE FUSELAGE SKIN AFT OF THE MAIN DOOR BETWEEN FRAME 19-20 AT STRINGER 4L-5L. MAINTENANCE REMOVED 
- [SDR ASOA2018121194070](https://openairdocs.org/sdr/ASOA2018121194070), Dec 9, 2018: SIGN. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT SIGN ON THE LEFT HAND COCKPIT PARTITION WA SFOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE
- [SDR ASOA20160802017](https://openairdocs.org/sdr/ASOA20160802017), Aug 2, 2016: LIGHT. DEFECTIVE. ACFT WAS FOUND TO HAVE THE EMERGENCY LIGHT STRIP DAMAGED AT THE AFT GALLEY. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP AT THE AFT GALLEY IAW AMM
- [SDR ASOA20150723038](https://openairdocs.org/sdr/ASOA20150723038), Jul 23, 2015: INVERTER. INOPERATIVE. DURING ROUTINE MAINTENANCE THE RT EMERGENCY EXIT ROW DOOR LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE RT EXIT DOOR EMERGENCY LIGHT INVERTER. OPS CHECK
- [SDR ASOA20141215102](https://openairdocs.org/sdr/ASOA20141215102), Dec 15, 2014: INVERTER. FAULTY. DURING ROUTINE MAINTENANCE THE AFT AISLE CELING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 6 EMERGENCY LIGHT INVERTER. OPS CHECKS WERE G
- [SDR ASOA20131116128](https://openairdocs.org/sdr/ASOA20131116128), Nov 16, 2013: BATTERY PACK. DISCHARGED. DURING MX INSPECTION, THE NR 3 EMERGENCY LIGHT BATTERY FAILED OPS CHECK. MAINTENANCE R & R THE BATTERY PACK AND OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN
- [SDR ASOA20130908164](https://openairdocs.org/sdr/ASOA20130908164), Sep 8, 2013: FLAPPER VALVE. LEAKING. AFTER DEPARTURE, RECEIVED A REPORT FROM THE TOWER THAT THEY WERE VENTING FUEL FROM THE RT WING. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLAC
- [SDR ASOA20120828071](https://openairdocs.org/sdr/ASOA20120828071), Aug 28, 2012: UNKNOWN. SMOKE. THE CREW REPORTED SMOKE IN CABIN DURING CLIMBOUT WHEN ENGINE BLEED 1 SELECTED. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED N
- [SDR ASOA20120524107](https://openairdocs.org/sdr/ASOA20120524107), May 23, 2012: FLOOR SUPPORT. CORRODED. GALLEY AREA FWD DIGITAL CORRODED IN SEVERAL AREAS BEYOND LIMITS. REMOVED CORROSION, FABRICATED FILLER AND DOUBLER, PRIMED AND PAINTED.
- [SDR C2XA10IA232](https://openairdocs.org/sdr/C2XA10IA232), Aug 16, 2010: ENGINE. LEAKING. PHX - FLIGHT 2843 THE CREW REPORTED SMOKE IN THE CABIN AND COCKPIT ON SHORT FINAL FOLLOWED BY A LAV SMOKE WARNING ON EICAS. THE AIRCRAFT LANDED AT PHX WITHOUT I
- [SDR C2XA10IA210](https://openairdocs.org/sdr/C2XA10IA210), Jul 27, 2010: PROBE. INOPERATIVE. IAH - FLIGHT 3137, THE CREW REPORTED THAT THE PITOT 3 HEAT WAS INOPERATIVE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT AND MAINTENANCE REMOVE
- [SDR C2XA10IA077](https://openairdocs.org/sdr/C2XA10IA077), Feb 23, 2010: CONTROL UNIT. INOPERATIVE. IAH - FLIGHT 2233, DURING CRUISE FLIGHT THE CREW REPORTED A PITCH TRIM FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE 
- [SDR C2XA10RI027](https://openairdocs.org/sdr/C2XA10RI027), Feb 5, 2010: FLAPPER VALVE. LEAKING. FLIGHT 3150 - PBI - DURING CLIMB CREW REPORTED RT WING FUEL LEAK. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED FLAPPER VA
- [SDR C2XA09IA167](https://openairdocs.org/sdr/C2XA09IA167), Jun 29, 2009: TRANSCEIVER. INOPERATIVE. IAH - FLT 4918 - THE CREW REPORTED THAT THE WEATHER RADAR WAS INOPERATIVE AND GAVE CODES 16 & 24 IN TEST MODE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITH
- [SDR C2XA09IA073](https://openairdocs.org/sdr/C2XA09IA073), Mar 11, 2009: CONTROL UNIT. FAULTY. DURING CLIMB THE CREW RECEIVED A FLAP FAIL MESSAGE AND ELECTED TO RETURN TO IAH. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED FLAP ELECTRON
- [SDR C2XA09RI021](https://openairdocs.org/sdr/C2XA09RI021), Feb 7, 2009: OIL COOLER. CONTAMINATED. FLIGHT 2342 - EWR - FLIGHT CREW REPORTED LAV SMOKE ON EICAS ON T/O AND PAX DESCRIBED DISTINCT ODOR ON T/O AND LANDING. EWR MX CLEANED APU OIL COOLER AND PERFORM

All 57: https://openairdocs.org/aircraft/N14188/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/N14188/stcs.md

## 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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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.