# N11127: 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: 145697
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2005
- Certificate issued: August 30, 2019
- Expires: August 31, 2029
- Mode S code: A032A8
- 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=11127
- Page: https://openairdocs.org/aircraft/N11127

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/N11127/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 N11127.

## 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 20180731018489I](https://openairdocs.org/incident/20180731018489I), Jul 31, 2018: Embraer EMB-145XR (N11127), Denver, CO, Minor damage. At touchdown, all four main landing gear tires ceased to rotate and subsequently suffered damage to the tire and wheel assemblies which included loss of tire…

## Service difficulty reports (60, 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 RAIA2020021520001](https://openairdocs.org/sdr/RAIA2020021520001), Feb 12, 2020: ENGINE. ODOR. SMOKE IN CABIN AT ROW 3 AND AFT CABIN. COMPLIED WITH FIM AND FOUND NO EVIDENCE OR SMELL ANY BURNT. RAN ENGINES AND APU WITH PACKS ON. NO SMELL OR SMOKE NOTED IN
- [SDR RAIA201909140001](https://openairdocs.org/sdr/RAIA201909140001), Sep 14, 2019: MOUNT BRACKET. CORRODED. MOUNTING PLATE FOR THE RA #2 AFT ANTENNA ON AFT FUSELAGE SEPARATING FROM FUSELAGE. CLEANED SKIN AND FOUND NO CORROSION ON FUSELAGE ONLY RA MOUNTING BRACKET. NO 
- [SDR RAIA201909110001](https://openairdocs.org/sdr/RAIA201909110001), Sep 11, 2019: SKIN. CRACKED. MOUNTING PLATE FOR RADIO ALTIMETER #2 FWD ANTENNA ON AFT FUSELAGE IS SEPARATING FROM THE AIRCRAFT. CORROSION FOUND BETWEEN MOUNTING PLATE AND SKIN OF FUSELAGE. 
- [SDR RAIA2018121440002](https://openairdocs.org/sdr/RAIA2018121440002), Dec 4, 2018: SUPPORT BRACKET. GOUGED. L/H BLEED SYSTEM SUPPORT BRACKET IS GOUGED... REOMOVED AND REPLACED SUPPORT BRACKET...
- [SDR RAIA2018121440001](https://openairdocs.org/sdr/RAIA2018121440001), Dec 4, 2018: ACCESS DOOR. CRACKED. EXT POWER ACCESS DOOR IS CRACKED... REOMEVED AND REPLACED EXTERNAL POWER DOOR
- [SDR RAIA201812142001](https://openairdocs.org/sdr/RAIA201812142001), Dec 2, 2018: FLOOR SUPPORT. DAMAGED. LAV L/H FLOOR SUPPORT ASSY AT FR 60 IS DAMAGED... REMOVED AND REPLACED DAMAGED SUPPORT...
- [SDR RAIA2018121430007](https://openairdocs.org/sdr/RAIA2018121430007), Nov 30, 2018: DOOR FRAME. CRACKED. BAGGAGE DOOR FRAME AFT EXT FLANGE IS CRACKED AT BOTTOM END... REPAIRED BAGGAGE DOOR IAW ETD2018-145-129196
- [SDR RAIA2018121430006](https://openairdocs.org/sdr/RAIA2018121430006), Nov 30, 2018: GUSSET. CORRODED. R/H FLOOR SUPPORT GUSSET BETWEEN FR 59-61 IS CORRODED.... REMOVED AND REPLACED GUSSET...
- [SDR RAIA2018121430005](https://openairdocs.org/sdr/RAIA2018121430005), Nov 30, 2018: GUSSET. CORRODED. L/H FLOOR SUPPORT GUSSET BETWEEN FR 59-61 IS CORRODED.... REMOVED AND REPLACED GUSSET...
- [SDR RAIA2018121430004](https://openairdocs.org/sdr/RAIA2018121430004), Nov 30, 2018: BEAM. CORRODED. LOWER CARGO ENTRY BEAM BETWEEN FR 65-68 IS CORRODED AROUND FASTNER HOLES... REMOVED AND REPLACED CARGO ENTRY BEAM...
- [SDR RAIA2018121430003](https://openairdocs.org/sdr/RAIA2018121430003), Nov 30, 2018: PROFILE. BENT. AFT "T" PROFILE AT FR 66 ON CARGO ENTRY RAMP IS BENT... REMOVED AND REPLACED "T" PROFILE...
- [SDR RAIA2018121430002](https://openairdocs.org/sdr/RAIA2018121430002), Nov 30, 2018: PROFILE. BENT. FWD "T" PROFILE AT FR 66 ON CARGO ENTRY RAMP IS BENT... REMOVED AND REPLACED "T" PROFILE...
- [SDR RAIA2018121430001](https://openairdocs.org/sdr/RAIA2018121430001), Nov 30, 2018: SUPPORT. CRACKED. BAGGAGE DOOR HOLD OPEN ROD SUPPORT IS CRACKED ON FR 68... REMOVED AND REPLACED BAGGAGE DOOR HOLD OPEN ROD SUPPORT...
- [SDR RAIA2018121490002](https://openairdocs.org/sdr/RAIA2018121490002), Nov 29, 2018: STRUCTURE. CORRODED. AFT "U" SHAPE BETWEEN FR 18 AND FR19 AT PAX DOOR IS CORRODED... REMOVED AND REPLACED "U" SHAPE
- [SDR RAIA201811290001](https://openairdocs.org/sdr/RAIA201811290001), Nov 29, 2018: STRUCTURE. CORRODED. FWD "U" SHAPE BETWEEN FR 18 AND FR19 AT PAX DOOR IS CORRODED... REMOVED AND REPLACED "U" SHAPE
- [SDR RAIA201807260001](https://openairdocs.org/sdr/RAIA201807260001), Jul 26, 2018: WINDOW. OUT OF ADJUST. F/O DV WINDOW W/N CLOSE. ADJUSTED FO'S DV WINDOW AND PERFORMED OPS CHECK. OPS CHECK GOOD AND NO DEFECTS NOTED AT THIS TIME.
- [SDR RAIA201709150001](https://openairdocs.org/sdr/RAIA201709150001), Sep 15, 2017: SHUTOFF VALVE. LEAKING. NR 2 BLEED LEAK EICAS MESSAGE. SECURED LEAK AT PRSOV VALVE, OPS CHECKED GOOD.
- [SDR RAIA201709060002](https://openairdocs.org/sdr/RAIA201709060002), Sep 6, 2017: CONTAINER. TORN. CAPTAIN`S LIFE VEST POUCH TORN. R & R THE LIFE VEST.
- [SDR RAIA201709060001](https://openairdocs.org/sdr/RAIA201709060001), Sep 6, 2017: FLASHLIGHT. INOPERATIVE. FIRST OFFICER`S FLASHLIGHT WAS INOPERATIVE. R & R THE FLASHLIGHT. OPS CHECKED GOOD.
- [SDR RAIA201610310001](https://openairdocs.org/sdr/RAIA201610310001), Oct 31, 2016: CARBON SEAL. LEAKING. OIL PRESSURE WENT INTO RED ON FINAL APPROACH. OIL ON NR 1 COWLING. R & R NR 1 ENGINE GENERATOR IAW AMM 24-31-01 AND CORRESPONDING CARBON SEAL WAS R & R IAW MM 7
- [SDR ASOA20160310010](https://openairdocs.org/sdr/ASOA20160310010), Mar 8, 2016: SKIN. DENTED. DENT IN ACFT SKIN FORWARD OF SERVICE DOOR AT FRAME 18, STR 11R AND AFT OF SERVICE DOOR BETWEEN FRAMES 23, 24 AND STR 12R, 13R. CUTOUT THE CREASES, FABRICATED AN
- [SDR ASOA20160207005R](https://openairdocs.org/sdr/ASOA20160207005R), Feb 7, 2016: ACM. SMOKE. SMOKE WAS REPORTED IN COCKPIT. ACFT RETURNED TO GATE AND NR 1 PACK WAS PLACED ON MEL. MAINTENANCE R & R NR 1 ACM WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETU
- [SDR ASOA20150308059](https://openairdocs.org/sdr/ASOA20150308059), Mar 8, 2015: DOOR SILL. CORRODED. DURING C-CHECK THE SERVICE DOOR 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 ASOA20140826108](https://openairdocs.org/sdr/ASOA20140826108), Aug 26, 2014: UNKNOWN. ODOR. THE CREW REPORTED A STRONG OIL AND DIRTY PACK ODORS IN THE COCKPIT DURING DESCENT AND LANDING. LANDED WITHOUT INCIDENT, MAINTENANCE R & R THE NR 1 ENGINE, OPS T
- [SDR ASOA20130312092](https://openairdocs.org/sdr/ASOA20130312092), Mar 12, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK CENTER OMEGA BEAM CORRODED (LOCAL LEVEL 2) AT NUTPLATES AT FRAME 59-61. MX PERFORMED REPAIR OF CENTER OMEGA BEAM AT FRAME 59 IAW SRM 51-40-02 AND
- [SDR ASOA20130311091V](https://openairdocs.org/sdr/ASOA20130311091V), Mar 12, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK RT OMEGA BEAM CORRODED (LOCAL LEVEL 2) AT NUTPLATES AT FRAME 59-61. MX PERFORMED REPAIR AND INSTALLED DOUBLER REPAIR AT RT OMEGA BEAM AT FRAME 60
- [SDR ASOA20130226090](https://openairdocs.org/sdr/ASOA20130226090), Mar 7, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59-61. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01473. THE AC
- [SDR ASOA20130130008R](https://openairdocs.org/sdr/ASOA20130130008R), Jan 30, 2013: CHARGER. INOPERATIVE. DURING MX INSPECTION, THE EMERGENCY EXIT LIGHT AT SEAT 2B WAS FOUND INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT BATTERY CHARGER AND BATTERY PACK WITH OPS CHE
- [SDR ASOA20121129144](https://openairdocs.org/sdr/ASOA20121129144), Nov 29, 2012: ENGINE. SMOKE. THE CREW REPORTED A LAVATORY SMOKE WARNING ON EICAS WITH SMOKE IN THE CABIN SEEMING TO COME FROM THE LIGHTS. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITH
- [SDR ASOA2011121822013](https://openairdocs.org/sdr/ASOA2011121822013), Dec 18, 2011: AUDIO PANEL. FAILED. POST-FLIGHT CREW REPORTED CAPTAINS AUDIO PANEL INOPERATIVE AND THEN POPPED CIRCUIT BREAKER WITH ELECTRICAL ODOR IN COCKPIT. MX PERFORMED GVI AT CAPTAINS AUDIO P
- [SDR ASOA2011112001001](https://openairdocs.org/sdr/ASOA2011112001001), Nov 20, 2011: FAN. FAILED. DURING DESCENT THE CREW REPORTED SMOKE IN THE COCKPIT AND DECLARED AN EMERGENCY LANDING, WITHOUT INCIDENT. UPON INSPECTION, MX DETERMINED THE SOURCE OF SMOKE TO
- [SDR C2XA11IA258](https://openairdocs.org/sdr/C2XA11IA258), Nov 12, 2011: ENGINE. MALFUNCTIONED. DURING CRUISE THE CREW REPORTED A LAV SMOKE INDICATION WARNING HOWEVER NO VISUAL SMOKE WAS NOTED. THE AIRCRAFT DIVERTED TO ICT AND LANDED WITHOUT INCIDENT WHERE
- [SDR C2XA11SH096](https://openairdocs.org/sdr/C2XA11SH096), Jun 26, 2011: SKIN. CRACKED. SHV - DURING C-CK - LT SKIN HAS CRACKS AROUND 4 RIVETS. REPAIRED SKIN IAW EC5330-02432. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11TY068](https://openairdocs.org/sdr/C2XA11TY068), May 27, 2011: UNKNOWN. SMOKE. SMOKE IN CABIN DURING CLIMBOUT. AIR RETURN. C/W FIM TASK CARDS. NO DEFECTS FOUND AND AIRCRAFT RETURNED TO SERVICE.
- [SDR C2XA11TY065](https://openairdocs.org/sdr/C2XA11TY065), May 27, 2011: UNKNOWN. SMOKE. TYS - A/C EN ROUTE FROM CLT TO IAH WHEN SMOKE WAS SEEN IN THE CABIN, CREW RETURN TO CLT WITHOUT INCIDENT OR INJURY. MAINTENANCE RAN A/C ON THE GROUND PER FIM 21
- [SDR C2XA11RI094](https://openairdocs.org/sdr/C2XA11RI094), May 25, 2011: FLAPPER VALVE. LEAKING. FLIGHT 2143 - GSP - FLIGHT CREW REPORTED THAT APPEARED TO BE A LEAK OF FUEL ON LEFT WING, CONFIRMED BY TOWER IN FLT. CREW PERFORMED AIR RETURN AND LANDED UNEVEN
- [SDR C2XA10IA102](https://openairdocs.org/sdr/C2XA10IA102), Mar 25, 2010: UNKNOWN. MALFUNCTIONED. IAH - FLIGHT 2878, THE CREW REPORTED COMING OUT OF PIT THAT THE GEAR WOULD NOT RETRACT WHEN COMMANDED, AND RECEIVED EICAS WARNING LG/LEVER DISAGREE. THE GEAR EV
- [SDR C2XA10IA015](https://openairdocs.org/sdr/C2XA10IA015), Jan 13, 2010: FUEL LINE. LEAKING. IAH - FLIGHT 2337, THE CREW REPORTED, SMELLED FUEL AFTER T/O WITH THE APU RUNNING BLEEDS AND AGAIN AFTER STARTING THE APU UPON PARKING AT IAH. THE AIRCRAFT LAND
- [SDR C2XA09RI222](https://openairdocs.org/sdr/C2XA09RI222), Dec 21, 2009: PROXIMITY SWITCH. MALFUNCTIONED. FLIGHT 2484 - EWR - FLIGHT CREW REPORTED SPOILER FAILURE INDICATION ON EICAS DURING LANDING. CREW ABORTED APPROACH. CREW LANDED ACFT UNEVENTFULLY. EWR MX REMOVE
- [SDR C2XA09SH447](https://openairdocs.org/sdr/C2XA09SH447), Nov 22, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 29. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09 SH424](https://openairdocs.org/sdr/C2XA09%20SH424), Nov 15, 2009: SKIN. CRACKED. SHV - DURING C-CHECK RT FRAME 78 HAS VISUAL EVIDENCE OF CRACKS AROUND RIVETS. MAINTENANCE PERFORMED REPAIR ON RT FRAME 78 STRINGER 6R IAW EC5330-02011. THE AIRC
- [SDR C2XA09SH423](https://openairdocs.org/sdr/C2XA09SH423), Nov 15, 2009: RIVET. WORN. SHV - DURING C-CHECK SMOKING RIVETS AT LT FRAME 78. MAINTENANCE PERFORMED REPAIR ON FRAME 78 STRINGER 6L IAW EC5330-02011. THE AIRCRAFT WAS APPROVED FOR RETURN 
- [SDR C2XA09SH416](https://openairdocs.org/sdr/C2XA09SH416), Nov 11, 2009: BRACKET. CORRODED. SHV - DURING C-CHECK CARGO DOOR FWD TRIANGLE BRACKET IS CORRODED (LEVEL 2 LOCAL). MAINTENANCE BLENDED AND EVALUATED THE CORROSION ON THE CARGO DOOR FWD TRIANGLE
- [SDR C2XA09SH411](https://openairdocs.org/sdr/C2XA09SH411), Nov 9, 2009: SUPPORT. CORRODED. SHV - DURING C-CHECK, TOILET WASTE DRAIN VALVE CORRODED. REMOVED AND REPLACED TOILET WASTE DRAIN VALVE SUPPORT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED F
- [SDR C2XA09RI183](https://openairdocs.org/sdr/C2XA09RI183), Oct 24, 2009: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 2353 - YQM - FLIGHT CREW REPORTED LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. CREW DOWN POWERED ACFT AND MESSAGE DISAPPEAR. ACFT RETURNED TO SERVICE.
- [SDR C2XA09RI091](https://openairdocs.org/sdr/C2XA09RI091), May 3, 2009: DUCT. DEFECTIVE. FLIGHT 2753 - EWR - FLIGHT CREW REPORTED BLEED OVERTEMP - PACK NR 2 OVERHEAT ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFUL. EWR MX REMOVED AND 
- [SDR C2XA08CL040](https://openairdocs.org/sdr/C2XA08CL040), Mar 30, 2008: INVERTER. INOPERATIVE. CLE FLIGHT2252 - THE CREW REPORTED CABIN CEILING EMERGENCY LIGHT WAS INOPERATIVE AT THE OVERWING EMERGENCY EXIT. MAINTENANCE INSPECTED AND REPLACED THE NR 5 EME
- [SDR C2XA08SH041](https://openairdocs.org/sdr/C2XA08SH041), Feb 29, 2008: FITTING. WORN. SHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA ACTUATOR ATTACHMENT FITTING ON THE AILERON SPAR HAD MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REP
- [SDR C2XA07IA039](https://openairdocs.org/sdr/C2XA07IA039), Feb 18, 2007: FUEL SYS. LEAKING. IAH - FLIGHT 2097, DURING PREFLIGHT INSPECTION THE CREW REPORTED A FUEL SMELL IN THE COCKPIT WITH THE APU ON. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE 
- [SDR C2XA07IA038](https://openairdocs.org/sdr/C2XA07IA038), Feb 15, 2007: FUEL NOZZLE. UNKNOWN. IAH - FLIGHT 2041, THE CREW REPORTED A FUEL SMELL IN THE CABIN ON START. MAINTENANCE PLACED THE APU ON MEL 49-00-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO

All 60: https://openairdocs.org/aircraft/N11127/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/N11127/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.