# N12157: 2004 Embraer EMB-145XR

- Status: Valid registration
- Airframe: [Embraer EMB-145XR](https://openairdocs.org/model/embraer-emb-145xr) (registry code 3260214, 55 seats)
- Engine: [Rolls-Royce AE3007 series](https://openairdocs.org/engine/rolls-royce-ae3007-series) (registry code 54582)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 145787
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 21, 2004
- Certificate issued: May 31, 2019
- Expires: May 31, 2029
- Mode S code: A05A90
- 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=12157
- Page: https://openairdocs.org/aircraft/N12157

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/N12157/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 N12157.

## FAA accident and incident reports

None matched to N12157.

## Service difficulty reports (53, 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 JJBA20220203001](https://openairdocs.org/sdr/JJBA20220203001), Feb 3, 2022: CHARGER. INOPERATIVE. BOTH OVER WING EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED OVER WING EMERGENCY LIGHT BULB. OPS CHECK FAILED. REMOVED AND REPLACED EMERGENCY LIGHT BAT
- [SDR JJBA20211030066](https://openairdocs.org/sdr/JJBA20211030066), Oct 30, 2021: LAMP. DIM. EMERGENCY LIGHT DIM IN GALLEY OVERHEAD PANEL. REMOVED AND REPLACED LIGHT BULB. OPS CHECK SAT
- [SDR JJBA20210605009](https://openairdocs.org/sdr/JJBA20210605009), Jun 5, 2021: BULB. INOPERATIVE. LH OVER WING EMERGENCY LIGHT DIM. R&R OVER WING EMERGENCY LIGHT BULB. OPS CHECK SAT.
- [SDR JJBA20210123023](https://openairdocs.org/sdr/JJBA20210123023), Jan 23, 2021: TRANSMISSION. INOPERATIVE. FLAP FAIL ON EICAS AND FLAPS DIDN'T MOVE WHEN FLAP 9 SELECTED. CMC: LEFT TRANSMISSION BRAKE FAIL TODAY, LGEU FAIL 2 DAYS AGO. INSPECTED FLEXIBLE LINES FOR WATER
- [SDR JJBA202002052001](https://openairdocs.org/sdr/JJBA202002052001), Feb 2, 2020: ENGINE. LEAKING. SMOKE IN CABIN AFTER TAKE OFF AND AFTER TYPE 4 DE-ICING. DISSIPATED QUICKLY. PERFORMED TECHNICAL INSTRUCTION. FOUND OIL IN #2 ENGINE WATER WASH PORT. ENGINE WIL
- [SDR JJBA202001221006](https://openairdocs.org/sdr/JJBA202001221006), Jan 21, 2020: UNKNOWN. SMOKE. SMOKE REPORTED IN CABIN AFTER TAKEOFF. PERFORMED INSPECTION AND CHECK OF THE GASPER SYSTEM MUFFLERS. NO DEFECTS NOTED. CHECKED OIL LEVEL. FOUND TO BE WITHIN LIM
- [SDR JJBA2019123128012](https://openairdocs.org/sdr/JJBA2019123128012), Dec 28, 2019: HOSE. LEAKING. HYDRAULIC 2 LOW QUANTITY EICAS MESSAGE IN FLIGHT. FOUND SUCTION HOSE CONNECTED TO NUMBER TWO EDP LEAKING. R&R SUCTION HOSE. OPS CHECK AND LEAK CHECK SAT. NO DEF
- [SDR JJBA201906198014](https://openairdocs.org/sdr/JJBA201906198014), Jun 18, 2019: UNKNOWN. ODOR. STRONG ELECTRICAL/SMOKE SMELL IN FLIGHT STATION. PERFORMED TROUBLESHOOTING, FOUND SAT. INSPECTED FWD AVIONICS COMP, FOUND SAT. RAN BOTH AIR CON PACKS FOR 30 MIN
- [SDR JJBA20190504004](https://openairdocs.org/sdr/JJBA20190504004), May 4, 2019: LIGHT. INOPERATIVE. EXTERNAL SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R&R LIGHT BULB ON SERVICE DOOR EXTERIOR EMERGENCY LIGHT. LIGHT WORK INTERMITTENTLY. R&R EXTERIOR SERVICE DOOR
- [SDR JJBA201904083004](https://openairdocs.org/sdr/JJBA201904083004), Apr 3, 2019: HANDLE. MISINSTALLED. OVER WING EMERGENCY EXITS UPPER ASSIST HANDLES INSTALLED UPSIDE DOWN. REINSTALLED UPPER ESCAPE HATCH HANDLES IN APPROPRIATE POSITION.
- [SDR JJBA20190105004](https://openairdocs.org/sdr/JJBA20190105004), Jan 5, 2019: SIGN. UNSECURE. EMERGENCY EXIT SIGN AT ROW 18 IS DANGLING. REATTACHED ROW 18 EMERGENCY EXIT SIGN. NO OTHER DEFECTS NOTED AT THIS TIME.
- [SDR JJBA20190101001](https://openairdocs.org/sdr/JJBA20190101001), Jan 1, 2019: SIGN. UNSECURE. EMERGENCY EXIT SIGN AT ROW 18 FELL OFF. RE SECURED EMERGENCY EXIT SIGN. NO DEFECTS NOTED AT THIS TIME.
- [SDR JJBA20181221031](https://openairdocs.org/sdr/JJBA20181221031), Dec 21, 2018: CONNECTOR. DIRTY. FWD MID CEILING EMERGENCY EXIT SIGN INOPERATIVE. CLEANED CONNECTORS. OPS CHECK SAT. NO OTHER DEFECTS NOTED AT THIS TIME.
- [SDR JJBA201811305024](https://openairdocs.org/sdr/JJBA201811305024), Nov 5, 2018: TORQUE TUBE. UNSECURE. MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE. INSPECTED AND FOUND MAIN DOOR FWD INTERMIDIATE TORQUE TUBE CIRCLET UNSECURE THAT ALLOWED TORQUE TUBE TO FLOAT LATERAL
- [SDR JJBA20181016011](https://openairdocs.org/sdr/JJBA20181016011), Oct 16, 2018: GUSSET. CORRODED. LT IB FLOORBEAM LOWER SILL HAS CORROSION IN BETWEEN FR 36-39. R&R LT I/B FLOORBEAM LOWER STILL [GUSSET] AT FR36-39.
- [SDR JJBA20181016010](https://openairdocs.org/sdr/JJBA20181016010), Oct 16, 2018: DOOR SILL. CORRODED. RT OB FLOORBEAM LOWER SILL HAS CORROSION IN BETWEEN FR 41-48. REPLACED LT OB FLOORBEAM LOWER SILL IN BETWEEN FR 41-48.
- [SDR JJBA20181016009](https://openairdocs.org/sdr/JJBA20181016009), Oct 16, 2018: DOOR SILL. CORRODED. RT OB FLOORBEAM LOWER SILL HAS CORROSION IN BETWEEN FR 48-52 AS MARKED. R&R RT OB FLOORBEAM SILL FR 48-52.
- [SDR JJBA20181016008](https://openairdocs.org/sdr/JJBA20181016008), Oct 16, 2018: DOOR SILL. CORRODED. RT OB FLOORBEAM SILL HAS CORROSION BETWEEN FR 41-48. R&R RT OB FLOORBEAM SILL BETWEEN 41-48.
- [SDR JJBA20181016007](https://openairdocs.org/sdr/JJBA20181016007), Oct 16, 2018: CROSSBEAM. CORRODED. CORROSION-CABIN FLOOR STRUCTURE, RT FLOOR CROSSBEAM AT FR 28. R&R, MATCH DRILLED, ALODINE TREATED AND PRIMERED CROSSBEAM AT FR28 BETWEEN RT OMEGA BEAM AND FLOOR
- [SDR JJBA20181016006](https://openairdocs.org/sdr/JJBA20181016006), Oct 16, 2018: FITTING. CORRODED. SHEAR CLIP AT FR 65 BETWEEN STR 13L AND 15L CORRODED. R&R SHEAR CLIP AT FR65 BETWEEN 13L AND 15L.
- [SDR JJBA20181016005](https://openairdocs.org/sdr/JJBA20181016005), Oct 16, 2018: BEAM. CORRODED. CARGO DOOR CUTOUT LWR BEAM CORRODED. INSTALLED NEW CARGO DOOR CUTOUT LWR BEAM.
- [SDR JJBA20181016004](https://openairdocs.org/sdr/JJBA20181016004), Oct 16, 2018: FITTING. CORRODED. SHEAR CLIP CORRODED AT FR 68. LWR AFT CORNER OF CARGO DOOR OPENING. INSTALLED NEW SECTION OF SHEAR CLIP AT FR 58 STR 15L.
- [SDR JJBA20181016003](https://openairdocs.org/sdr/JJBA20181016003), Oct 16, 2018: FLOOR SUPPORT. CORRODED. LT OMEGA BEAM HAS CORROSION AT FR 59 & 60. INSTALLED REPAIR DOUBLES FOR DAMAGED AREA AT NUTPLATE HOLES IN LT OMEGA BEAM AT FR 59 & FR 60.
- [SDR JJBA201807101002](https://openairdocs.org/sdr/JJBA201807101002), Jul 7, 2018: ENGINE. NOT REPORTED. SMOKE IN THE COCKPIT. R&R NR 1 ENGINE. OPS AND LEAK CHECK SAT. NO OTHER DEFECTS NOTED AT THIS TIME.
- [SDR JJBA20171127011](https://openairdocs.org/sdr/JJBA20171127011), Nov 27, 2017: HOUSING. UNKNOWN. OVER WING EMERGENCY EXIT LIGHTS INOPERATIVE ON BOTH SIDES. R & R THE NR 4 EMERGENCY BATTERY HOUSING.
- [SDR JJBA20170830027](https://openairdocs.org/sdr/JJBA20170830027), Aug 30, 2017: DOOR. UNSECURE. LOUD WHISTLING NOISE IN THE CABIN DURING FLIGHT. SECURED THE EMERGENCY EXIT DOOR PRESSURE CHECKED, NO LEAKS NOTED. OPS CHECKED GOOD.
- [SDR ASOA20150616020](https://openairdocs.org/sdr/ASOA20150616020), Jun 16, 2015: INVERTER. INOPERATIVE. THE LEFT EMERGENCY EXIT LOWER EXIT IDENTIFIER WAS INOPERATIVE. R & R THE NR 4 INVERTER. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20140523090](https://openairdocs.org/sdr/ASOA20140523090), May 23, 2014: DOOR SILL. CORRODED. DURING C-CHECK, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140520089](https://openairdocs.org/sdr/ASOA20140520089), May 20, 2014: BEAM. CORRODED. DURING C-CHECK, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERV
- [SDR ASOA201306180049](https://openairdocs.org/sdr/ASOA201306180049), Jun 18, 2013: LIGHT. BURNED. CREW REPORTED AN ELECTRICAL ODOR WHILE TAXIING TO RUNWAY. MX INSPECTED AND REPLACED THE CABIN LIGHT ASSY AT SEATS 3B/C AND 4B/C. ALL OPS CHECKS WERE GOOD.
- [SDR C2XA11TY083](https://openairdocs.org/sdr/C2XA11TY083), Jun 13, 2011: ACTUATOR. BYPASSING. A/C WAS FERRIED FROM MEM TO TYS WHEN A/C PTRIM WAS FOUND INOP ON CLIMBOUT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STAB ACTUATOR IAW CHRONIC WORK SHEET 
- [SDR C2XA11CL143](https://openairdocs.org/sdr/C2XA11CL143), Jun 11, 2011: OUTFLOW VALVE. FAILED. MSN FLT 6120 - THE CREW REPORTED THAT DURING DESCENT THE CABIN WAS NOT DEPRESSURIZING. CABIN RATE VARIED FROM -1000 FT/MIN TO +450-500 FT/MIN. TRIED USING MANUA
- [SDR C2XA11RI007](https://openairdocs.org/sdr/C2XA11RI007), Jan 16, 2011: UNKNOWN. ODOR. FLIGHT 2599 - EWR - FLIGHT CREW REPORTED BURNING SMELL (ELECTRICAL) FROM COFFEE POTS. EWR MX PERFORMED OPERATIONAL CHECK OF COFFEE MAKERS AND FOUND NO DEFECTS F
- [SDR C2XA10SH271](https://openairdocs.org/sdr/C2XA10SH271), Aug 16, 2010: BEAM. CORRODED. SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED FROM FRAMES 65-68 AND STRINGERS 15-16L. MAINTENANCE REMOVED AND REPLACED THE AFFE
- [SDR C2XA10SH270](https://openairdocs.org/sdr/C2XA10SH270), Aug 15, 2010: BRACKET. CORRODED. SHV - DURING C-CHECK BAGGAGE DOOR FWD RAMP ANGLE BRACKET CORRODED (LEVEL 2 LOCAL) AROUND NUT PLATE HOLE. MAINTENANCE PERFORMED REPAIR TO BAGGAGE DOOR FWD RAMP A
- [SDR C2XA10SH269](https://openairdocs.org/sdr/C2XA10SH269), Aug 15, 2010: SUPPORT. CORRODED. SHV - DURING C-CHECK LT UPPER SEAT TRACK SUPPORT CORRODED (LEVEL 2 LOCAL) AROUND RIVET AT FRAME 50. MAINTENANCE PERFORMED REPAIR ON LT UPPER SEAT TRACK SUPPORT 
- [SDR C2XA10SH268](https://openairdocs.org/sdr/C2XA10SH268), Aug 15, 2010: DOOR FRAME. CORRODED. SHV - DURING C-CHECK CARGO DOOR INTERNAL FRAME IS CORRODED (LEVEL 2 WIDESPREAD) AROUND 5 NUT PLATE HOLES. MAINTENANCE PERFORMED REPAIR ON CARGO DOOR INTERNAL FR
- [SDR C2XA10SH267](https://openairdocs.org/sdr/C2XA10SH267), Aug 15, 2010: FRAME. CRACKED. SHV - DURING C-CHECK RT FRAME 10 HAS WORKING RIVET BELOW DV WINDOW. MAINTENANCE REMOVED AND REPLACED RT FRAME 10 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPR
- [SDR C2XA10IA217](https://openairdocs.org/sdr/C2XA10IA217), Aug 3, 2010: ISIS UNIT. INOPERATIVE. IAH - FLIGHT 2910, THE CREW REPORTED THAT ISIS WAS INOPERATIVE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED 
- [SDR C2XA10CL045](https://openairdocs.org/sdr/C2XA10CL045), Mar 18, 2010: TRANSMITTER. FAULTY. IAH FLT 2124 - THE CREW REPORTED FUEL USED INDICATOR WAS NOT WORKING. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 
- [SDR C2XA09RI117](https://openairdocs.org/sdr/C2XA09RI117), Jun 5, 2009: LIGHT. INOPERATIVE. FLIGHT CREW REPORTED AISLE PATH LIGHTING INOPERATIVE. MX REMOVED AND REPLACED LIGHTING STRIP AT ROW 12 AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED T
- [SDR C2XA09CL010](https://openairdocs.org/sdr/C2XA09CL010), Jan 15, 2009: PITOT SYSTEM. CONTAMINATED. YYZ FLIGHT NR 2365 THE CREW REPORTED AN IAS COMPARISON ERROR, ALT COMPARISON ERROR, SPS ADVANCE AND AUTOPILOT FAIL MSG IN CRUISE. THE ACFT DIVERTED INTO CLE AND
- [SDR C2XA08TY107](https://openairdocs.org/sdr/C2XA08TY107), Sep 24, 2008: BATTERY. DISCHARGED. A/C IS CURRENTLY IN C CHECK AND DURING AN OPS CHECK THE ROW 12 CEILING AND SIDEWALL EMERGENCY LIGHTS WERE INOP. MX R&R THE NR 3 POWER SUPPLY IAW EMB XR AMM 33-5
- [SDR C2X2008F00010](https://openairdocs.org/sdr/C2X2008F00010), Jul 13, 2008: FCU. INOPERATIVE. FLIGHT 2245 - OKC - FLIGHT CREW REPORTED VENTRAL TANK FAIL MESSAGE ON EICAS. CREW DIVERTED FLIGHT AND LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED VENTRAL F
- [SDR C2XA08CL081](https://openairdocs.org/sdr/C2XA08CL081), Jul 4, 2008: RELAY. FAULTY. IAH - FLIGHT 2738 - THE CREW REPORTED A "VENTRAL XFER INOP" MESSAGE ON THE ECIAS IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENA
- [SDR C2XA08IA088](https://openairdocs.org/sdr/C2XA08IA088), Mar 21, 2008: UNKNOWN. ODOR. YYT - FLIGHT 2507, THE CREW REPORTED A BURNING SMELL THROUGH THE PACKS WITH THE APU RUNNING. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL 49-00-
- [SDR C2XA08RI035](https://openairdocs.org/sdr/C2XA08RI035), Mar 4, 2008: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 3098 - EWR - DURING PREFLIGHT, CREW REPORTED AIR/GRND FAIL MESSAGE ON EICAS. SYSTEM WAS RESET AND MESSAGE WENT AWAY. AIRCRAFT WAS APPROVED TO RETURN TO S
- [SDR C2XA08IA069](https://openairdocs.org/sdr/C2XA08IA069), Feb 11, 2008: SOLENOID VALVE. DEFECTIVE. IAH - FLIGHT 2388, THE CREW REPORTED THAT THE NOSE LANDING GEAR DOORS OPENED BY THEMSELVES IN FLIGHT AT FL370. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAIN
- [SDR C2XA07BT031](https://openairdocs.org/sdr/C2XA07BT031), Mar 18, 2007: ACTUATOR. LACK OF LUBE. EWR FLT 3084 LOG SQUAWK FLAP FAIL DURING APPROACH. LUBRICATED ALL 8 FLAP SCREW JACK ACTUATORS IAW EMB145XR AMM 27-51-00 AND REMOVED AND REPLACED FLAP SELECTOR L
- [SDR C2XA07SH014](https://openairdocs.org/sdr/C2XA07SH014), Mar 9, 2007: ANGLE. CORRODED. SHV DURING C-CHECK CORROSION DAMAGE WAS FOUND AT THE CARGO DOOR BOTTOM INBOARD "L" ANGLE NUTPLATES. MAINTENANCE REPAIRED CARGO DOOR BOTTOM INBOARD "L" ANGLE IAW

All 53: https://openairdocs.org/aircraft/N12157/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/N12157/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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