# N11187: 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: 14500927
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 15, 2005
- Certificate issued: August 25, 2020
- Expires: August 31, 2027
- Mode S code: A0337A
- 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=11187
- Page: https://openairdocs.org/aircraft/N11187

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/N11187/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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CEN11IA234](https://openairdocs.org/ntsb/CEN11IA234), Mar 18, 2011: Embraer EMB-145XR (N11187), Akron, OH, incident, minor damage. Probable cause: The uncommanded left deflection of the airplane's nosewheel for reasons that could not be determined because postincident examination of the nosewheel steering system did not reveal any anomalies…

## FAA accident and incident reports (2)

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 20110318005379I](https://openairdocs.org/incident/20110318005379I), Mar 18, 2011: Embraer EMB-145XR (N11187), North Canton, OH, Minor damage. CENI11A234 expressjet 5916 kcakappendix update 03/21/2011-leahy summaryon March 18, 2011, at 12:08 am EST, an Embraer emb 145 (N11187) operated by express jet…
- [Incident 20100512033542I](https://openairdocs.org/incident/20100512033542I), May 12, 2010: Embraer EMB-145XR (N11187), Knoxville, TN, Minor damage. Ground crew, working for delta airlines ground operation company regional elite airline services. Wing walker left line of sight of tug operator, when wing…

## Service difficulty reports (65, 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 JJBA20220309034](https://openairdocs.org/sdr/JJBA20220309034), Mar 9, 2022: NOT REPORTED. NOT REPORTED. LANDING GEAR AIR GROUND FAIL ON ROTATION (TAKE OFF). DURING JACKING NLG STRUT FAILED TO FULLY EXTEND AUTOMATICALLY AND L PROXIMITY SWITCH FAILED TO ENGAGE. 1 NE
- [SDR JJBA20211227036](https://openairdocs.org/sdr/JJBA20211227036), Dec 27, 2021: PRESSURE SENSOR. INOPERATIVE. RUDDER 1-2 INOPERATIVE ON SHORT FINAL INTERMITTENT. DAU WAS REPLACED AND SUSPECTED TO BE CAUSE OF MULTIPLE SYSTEM MALFUNCTIONS. AFTER TAKE OFF THE DAU 2A FAIL M
- [SDR JJBA20210516014](https://openairdocs.org/sdr/JJBA20210516014), May 16, 2021: PLACARD. MISINSTALLED. PLACARDS ON EMERGENCY EXIT DOORS ARE INCORRECTLY APPLIED. FOUND LH AND RH ESCAPED HATCH IN WRONG POSITIONS, MOVED ESCAPE HATCHES TO CORRECT POSITIONS. OPS CHECK
- [SDR JJBA20210403008](https://openairdocs.org/sdr/JJBA20210403008), Apr 3, 2021: SEAT FRAME. CRACKED. CRACKED AISLE SIDE FRAMES ON SEATS 8A, 9A, AND 22A. R&R SEATS 8A, 9A, AND 22A.
- [SDR JJBA20210125025](https://openairdocs.org/sdr/JJBA20210125025), Jan 25, 2021: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS, BATTERY NR 2 INOPERATIVE. R & R EMERGENCY LIGHTS, BATTERY NR 2. OPERATIONS TEST SATISFACTORY.
- [SDR JJBA20210123041](https://openairdocs.org/sdr/JJBA20210123041), Jan 23, 2021: CONNECTOR. DISCONNECTED. AFT EMERGENCY CEILING LIGHT EXIT SIGN INOPERATIVE. DISCONNECTED CONNECTOR AND RECONNECTED CONNECTOR. OPERATIONS CHECK SATISFACTORY.
- [SDR JJBA20210108002](https://openairdocs.org/sdr/JJBA20210108002), Jan 8, 2021: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS LT & RT MARKERS & OVERHEAD ON EXIT ROW 18 INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY. OPERATIONS CHECK GOOD.
- [SDR JJBA20201210011](https://openairdocs.org/sdr/JJBA20201210011), Dec 10, 2020: CONNECTOR. UNSECURE. LT EMERGENCY EXIT SIGN LIGHT (UPPER) INOPERATIVE AT SEAT 18A. ADJUSTED ELECTRICAL CONNECTORS. OPERATIONS CHECK SATISFACTORY.
- [SDR JJBA202008310025](https://openairdocs.org/sdr/JJBA202008310025), Aug 30, 2020: SIGN. INOPERATIVE. LT AFT UPPER EMERGENCY LIGHT/MARKING SIGN ASSEMBLY INOPERATIVE. R&R LT AFT UPPER EMERGENCY MARKING ASSEMBLE. OPERATIONS CHECK SATISFACTORY.
- [SDR JJBA20191021009](https://openairdocs.org/sdr/JJBA20191021009), Oct 21, 2019: LIGHT. MISSING. MISSING EMERGENCY LIGHT STRIP BY ENTRANCE. INSTALLED EMERGENCY LIGHT STRIP. NO DEFECTS NOTED AT THIS TIME.
- [SDR JJBA201908195007](https://openairdocs.org/sdr/JJBA201908195007), Aug 15, 2019: WARNING MESSAGE. FALSE INDICATION. BATTERY 1 OVER TEMP MESSAGE ON EICAS. PERFORMED QRH PROCEDURES. R&R BATTERY 1. OPS CHECK SAT. BATTERY TEMP WITHIN LIMITS
- [SDR JJBA2019041109007](https://openairdocs.org/sdr/JJBA2019041109007), Apr 9, 2019: CARBON SEAL. FAILED. FUMES DETECTED IN BOTH COCKPIT AND CABIN DURING DESCENT. R&R #1 ENGINE NO 0 CARBON SEAL AND FAN DRIVE SHAFT. OPS AND LEAK CHECK SAT. DECONTAMINATED PACKS 1 AND 
- [SDR JJBA201902069050](https://openairdocs.org/sdr/JJBA201902069050), Jan 29, 2019: FLOORBEAM. TORN. RIGHT FLOOR BEAM AT FR 23 TORN / DAMAGED AT NUT PLATE HOLE. REPAIRED RIGHT FLOOR BEAM AT FR 23 TORN / DAMAGED AT NUT PLATE HOLE BY CUT OUT, DOUBLER FABRICATION 
- [SDR JJBA201902069049](https://openairdocs.org/sdr/JJBA201902069049), Jan 29, 2019: STRINGER. CHAFED. STRINGER 2L BETWEEN FRAMES 20 AND 21 CHAFFED. REMOVED CHAFE FROM STRINGER 2L BETWEEN FRAMES 20 AND 21 VIA BLEND OUT. AFTER BLEND OUT 0.018 DEPTH AND 4.190 LENGT
- [SDR JJBA201902068048](https://openairdocs.org/sdr/JJBA201902068048), Jan 28, 2019: FLOOR SUPPORT. CORRODED. CORROSION - LH OMEGA BEAM LOWER FLANGE FR 23-29. REMOVED CORROSION FROM LH OMEGA BEAM LOWER FLANGE FR 23-29 VIA BLEND OUT. AFTER BLEND OUT 0.017 MATERIAL WAS RE
- [SDR JJBA201902068047](https://openairdocs.org/sdr/JJBA201902068047), Jan 28, 2019: SKIN. CRACKED. HFEC INSPECTION SHOWS THE EXTERNAL FUSELAGE SKIN TO HAVE A CRACK APPROXIMATELY .25" LONG AT FRAME 75 AND STRINGER 2L AS MARKED. INSTALLED NEW FABRICATED DOUBLER
- [SDR JJBA201902068046](https://openairdocs.org/sdr/JJBA201902068046), Jan 28, 2019: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON LEFT OMEGA BEAM JUST AFT OF FR 59 UPON POST REMOVAL INSPECTION OF LH FLOOR BEAM GUSSET BETWEEN FRAMES 59-61. PERFORMED CUT OUT, FABRICATED AN
- [SDR JJBA201902068045](https://openairdocs.org/sdr/JJBA201902068045), Jan 28, 2019: FLOOR SUPPORT. CORRODED. CORROSION ON CENTER OMEGA BEAM AT FR 20 UNDERNEATH SILL. REMOVED AND REPLACED CENTER OMEGA BEAM AT FR 20. RESTORED SURFACE PROTECTION.
- [SDR JJBA201902067044](https://openairdocs.org/sdr/JJBA201902067044), Jan 27, 2019: FLOOR SUPPORT. CORRODED. CORRODED LH FLOOR BEAM GUSSET BETWEEN FR 59-61 AROUND NUT PLATE. REMOVED AND REPLACED LH OMEGA BEAM GUSSET FRAME 59-61. RESTORED SURFACE PROTECTION. LEVEL 2 COR
- [SDR JJBA201902065043](https://openairdocs.org/sdr/JJBA201902065043), Jan 25, 2019: SEAL. CORRODED. CARGO, BAGGAGE COMPARTMENT FWD BULKHEAD FLOOR SEAL CORRODED AT FRAME 61 LEFT SIDE AT FLOOR LEVEL. REMOVED AND REPLACED FLOOR SEAL IN CARGO, BAGGAGE COMPARTMENT 
- [SDR JJBA201902065042](https://openairdocs.org/sdr/JJBA201902065042), Jan 25, 2019: FLOOR SUPPORT. CORRODED. CORROSION - LH OB SILL FR 29-35 AS MARKED. REMOVED AND REPLACED LH FLOOR SILL AT FR 29-35. RESTORED SURFACE PROTECTION. LEVEL 2 CORROSION.
- [SDR JJBA20190205041](https://openairdocs.org/sdr/JJBA20190205041), Jan 25, 2019: FLOOR SUPPORT. CORRODED. CORROSION - LH OMEGA BEAM LOWER FLANGE FR 29-35. REPAIRED CORROSION - LH OMEGA BEAM LOWER FLANGE FR 29-35 BY REAMING, FILLING WITH HYSOL, DOUBLER FABRICATION AN
- [SDR JJBA2019020613040](https://openairdocs.org/sdr/JJBA2019020613040), Jan 23, 2019: FLOOR SUPPORT. CORRODED. LH OMEGA BEAM AT FR 46 TO FR 49 HAS CORROSION AS MARKED. INSTALLED REPAIR DOUBLER AND TOP COAT.
- [SDR JJBA2019020617039](https://openairdocs.org/sdr/JJBA2019020617039), Jan 17, 2019: FRAME. CORRODED. STOP SIGN DOUBLER AT FR 22 HAS CORROSION. REMOVED, REPLACED AND TOP COATED STOP SIGN DOUBLER AT FR 22. CORROSION LEVEL 2
- [SDR JJBA201811165005](https://openairdocs.org/sdr/JJBA201811165005), Nov 15, 2018: FAN. INOPERATIVE. AT CRUISE HEARD BUZZING NOISE FROM UNDER CAPTAIN'S FLOOR AND SMELLED SMOKE. (CREW MENTIONED A SMOKE DID DEVELOP). FOUND THAT THE #2 ELECTRONIC COMPARTMENT FAN W
- [SDR JJBA20180404003](https://openairdocs.org/sdr/JJBA20180404003), Apr 4, 2018: LIGHT. UNKNOWN. EMERGENCY LIGHT INOPERATIVE AT ROW 18A. PERFORMED AN OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM. OPS CHECK GOOD. NO OTHER DEFECTS NOTED.
- [SDR JJBA20171125010](https://openairdocs.org/sdr/JJBA20171125010), Nov 25, 2017: WIRE. UNSECURE. OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. SECURED THE WIRE TERMINALS.
- [SDR JJBA20171005003](https://openairdocs.org/sdr/JJBA20171005003), Oct 5, 2017: LAMP. UNSECURE. FIRST CEILING EMERGENCY LIGHT INOPERATIVE. ADJUSTED THE LAMP, OPS CHECKED GOOD.
- [SDR JJBA201708220018](https://openairdocs.org/sdr/JJBA201708220018), Aug 20, 2017: BATTERY PACK. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACKS NR 1 AND 2.
- [SDR JJBA20170601002](https://openairdocs.org/sdr/JJBA20170601002), Jun 1, 2017: LIGHT. INTERMITTENT. LIGHT OVER LEFT EMERGENCY EXIT INOPERATIVE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM OPS CHECK SAT.
- [SDR JJBA20170406006](https://openairdocs.org/sdr/JJBA20170406006), Apr 6, 2017: LIGHT. MALFUNCTIONED. FWD EMERGENCY LIGHT AT ROW 18 INOPERATIVE. IAW MX CONTROL, CYCLED EMERGENCY LIGHTS, OPS CHECKED GOOD. NO MX ACTION REQUIRED
- [SDR ASOA2016115005](https://openairdocs.org/sdr/ASOA2016115005), Jan 14, 2016: SKIN. DENTED. FORWARD FUSELAGE 1, SKIN LT SIDE HAS DAMAGE FROM A BIRD STRIKE. CUTOUT DAMAGED AREA, FABRICATED DOUBLER AND FILLER. REMOVED DAMAGED SECECTION OF RIB 4 AND SPLIC
- [SDR ASOA20141026300](https://openairdocs.org/sdr/ASOA20141026300), Oct 26, 2014: CONTROL PANEL. FAILED. DURING FLIGHT, RAPID DEPRESSURIZATION AT 36,000 FT. R & R CPAM IAW AMM 21-32-01. OPS AND LEAK CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20141021117R](https://openairdocs.org/sdr/ASOA20141021117R), Oct 21, 2014: INVERTER. INOPERATIVE. DURING MX INSPECTION THE FWD AISLE OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE R & R THE NR 6 EMERGENCY LIGHT INVERTER WITH OPS CHECK GOOD.
- [SDR ASOA20140704077](https://openairdocs.org/sdr/ASOA20140704077), Jul 4, 2014: INVERTER. INOPERATIVE. DURING ROUTINE CHECK, THE LOWER SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE R & R NR 2 EMERGENCY LIGHT SYS INVERTER AND OPS CHECKED SUC
- [SDR ASOA20140516055](https://openairdocs.org/sdr/ASOA20140516055), May 16, 2014: LIGHT. INOPERATIVE. PILOT REPORTED EMERGENCY EXIT SIGN INOPERATIVE. MX RESET SYS AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140322067](https://openairdocs.org/sdr/ASOA20140322067), Mar 22, 2014: BRACKET. CRACKED. DURING C-CHECK, FOUND BRACKET SUPPORTING A OVERFLOW LINE FROM THE VENTRAL TANK CRACKED. MAINTENANCE FABRICATED A NEW BRACKET AND INSTALLED IAW SRM 53-20-07.
- [SDR ASOA20140318050](https://openairdocs.org/sdr/ASOA20140318050), Mar 18, 2014: CHANNEL. CORRODED. DURING C-CHECK, FOUND THE OMEGA BEAM AND TOPCAP CORRODED. MAINTENANCE INSTALLED A NEW REPAIR TO THE OMEGA BEAM WITH A NEW TOP CAP IAW EC 5310-01473 AND SRM 51-4
- [SDR ASOA201218004](https://openairdocs.org/sdr/ASOA201218004), Feb 18, 2012: TANK. CHAFED. ACFT IS IN FOR A 3C INSPECTION, WHEN INSPECTION FOUND THE VENTRAL TANK BOTTOM CENTER CHAFED. MX PERFORMED A DOUBLER REPAIR ON THE VENTRAL TANK. FABRICATED AND I
- [SDR ASOA20120222009](https://openairdocs.org/sdr/ASOA20120222009), Feb 16, 2012: FLOOR SUPPORT. CORRODED. LT OMEGA BEAM TOP CAP CORRODED AT FRM 61. R & R TOP CAP.
- [SDR ASOA20120222008](https://openairdocs.org/sdr/ASOA20120222008), Feb 16, 2012: FLOOR SUPPORT. CORRODED. CTR OMEGA BEAM TOP CAP CORRODED AT FRM 61 CARBON BEAM. R & R TOP CAP.
- [SDR ASOA20120222007](https://openairdocs.org/sdr/ASOA20120222007), Feb 16, 2012: FLOOR SUPPORT. CORRODED. RT OMEGA BEAM TOP CAP CORRODED AT FRM 61 CARBON BEAM. R & R TOPCAP.
- [SDR ASOA20120222006](https://openairdocs.org/sdr/ASOA20120222006), Feb 16, 2012: SILL. CORRODED. RT LAVATORY FLOOR SILL CORRODED AT FRM 61 CARBON BEAM. REPLACED FLOOR SILL AT FRM 61.
- [SDR ASOA20120222005T](https://openairdocs.org/sdr/ASOA20120222005T), Feb 16, 2012: BRACKET. WORN. LT AILERON PCA BRACKET FITTING MOST OTBD HAT BUSHING MIGRATED. R & R BRACKET.
- [SDR ASOA20120222010](https://openairdocs.org/sdr/ASOA20120222010), Feb 15, 2012: SILL. CORRODED. LEFT CABIN FLOOR SILL CORRODED FRM 18-23. R & R FLOOR SILL FRM 18-23.
- [SDR C2XA11CL075](https://openairdocs.org/sdr/C2XA11CL075), Mar 18, 2011: UNKNOWN. MALFUNCTIONED. ORD FLT 5916 - THE CREW REPORTED AIRCRAFT PULLED TO THE LEFT ON LANDING. CREW DISCONNECTED NOSE WHEEL STEERING AND LOST CONTROL OF AIRCRAFT. THE AIRCRAFT DEPART
- [SDR C2XA11CL043](https://openairdocs.org/sdr/C2XA11CL043), Feb 8, 2011: CONTROL UNIT. FAULTY. THE CREW REPORTED A LOUD BANGING NOISE AND SHUTTER ON GEAR RETRACTION. MAINTENANCE INSPECTED AND REPLACED THE BRAKE CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11CL037](https://openairdocs.org/sdr/C2XA11CL037), Jan 28, 2011: CONNECTOR. LOOSE. ORD FLT 5992 - THE CREW REPORTED A NOSE GEAR INDICATION NOT SHOWING DOWN. MAINTENANCE INSPECTED AND CLEANED AND RE-SECURED THE CONNECTORS ON THE NOSE GEAR DOWN 
- [SDR C2XA10CL143](https://openairdocs.org/sdr/C2XA10CL143), Sep 1, 2010: PRESSURE SWITCH. BROKEN. CLE FLT 5916 THE CREW REPORTED AN ENGINE 2 BLEED VALVE FAIL MESSAGE APPEARED AT 60 KNTS. THE TAKEOFF WAS ABORTED AND TAXIED BACK TO GATE. MAINTENANCE INSPECTED 
- [SDR C2XA10TY116](https://openairdocs.org/sdr/C2XA10TY116), Aug 18, 2010: AILERON. DAMAGED. TYS - A/C WAS FOUND WITH A POSSIBLE LIGHTNING STRIKE INDICATION. THE LEFT AILERON WAS BURNT. MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION AND R/R THE LEF

All 65: https://openairdocs.org/aircraft/N11187/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/N11187/stcs.md

## Earlier aircraft with N11187

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N11187 before.

- [Cancelled 1997-06-23](https://openairdocs.org/deregistered/N11187-1997-06-23): Raytheon 1900D, S/N UE273. Exported to Australia. Owner: [Rangeflyers Inc](https://openairdocs.org/faa-owner/RANGEFLYERS%20INC), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N11187-undated): Franklin Glider PS-2, S/N 125. Triennial form not returned

## 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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