# N11181: 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: 14500904
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 14, 2005
- Certificate issued: June 4, 2020
- Expires: June 30, 2027
- Mode S code: A03374
- 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=11181
- Page: https://openairdocs.org/aircraft/N11181

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/N11181/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 N11181.

## NTSB investigations on N11181 not matched to an aircraft (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 ATL83FID03](https://openairdocs.org/ntsb/ATL83FID03), Dec 21, 1982: Cessna 150 (N11181), Lynchburg, VA, destroyed

## FAA accident and incident reports

None matched to N11181.

## Reports on N11181 not matched to an aircraft (1)

They name N11181, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Accident 19821221064919A](https://openairdocs.org/incident/19821221064919A), Dec 21, 1982: Cessna 150L (N11181), Lynchburg, VA, Substantial damage. Student pilot crashed airplane short of runway during approach for landing. Turbulence had been forecast low level.

## Service difficulty reports (67, 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 JJBA20220305006](https://openairdocs.org/sdr/JJBA20220305006), Mar 5, 2022: LAMP. INOPERATIVE. RH OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPS CHECK SAT
- [SDR JJBA20210407014](https://openairdocs.org/sdr/JJBA20210407014), Apr 7, 2021: LINE. CHAFED. E2 OIL LOW PRESSURE EICAS MASTER WARNING IN FLIGHT. OIL ON COWLINGS AFTER LANDING. FOUND CHAFED OIL LINE CONNECTED TO AGB TO OIL TANK PRESSURE LINE. R&R THE OIL
- [SDR JJBA2021360004](https://openairdocs.org/sdr/JJBA2021360004), Mar 6, 2021: SEAT FRAME. CRACKED. CRACK AT SEATS 3A, 2A & 18A STRUCTURE BELOW ARMREST. R&R SEATS 18A, 3A & 2A.
- [SDR JJBA20201223027](https://openairdocs.org/sdr/JJBA20201223027), Dec 23, 2020: CONTROL UNIT. INOPERATIVE. BRAKE INBOARD INOPERATIVE MESSAGE ON EICAS. INSPECTED FOR HYDRAULIC LEAKS ON INBOARD BRAKES. CHECKED HYDRAULIC LEVEL AND PRESSURE. NO DEFECTS FOUND. R & R BRAKE
- [SDR JJBA202007297004](https://openairdocs.org/sdr/JJBA202007297004), Jul 27, 2020: INVERTER. INOPERATIVE. EMERGENCY LIGHT INOPERATIVE ABOVE SERVICE DOOR. R&R INVERTER #2. OPS CHECK SAT.
- [SDR JJBA202003265020](https://openairdocs.org/sdr/JJBA202003265020), Mar 25, 2020: DOUBLER. CORRODED. CORROSION - COCKPIT FLOOR DOUBLER Y=+293.0 FR10/11. REMOVED AND REPLACED COCKPIT FLOOR DOUBLER AT Y= +293.0 AND 3EA. REPAIR DOUBLER
- [SDR JJBA202003265019](https://openairdocs.org/sdr/JJBA202003265019), Mar 25, 2020: GUSSET. CORRODED. CORROSION - COCKPIT FLOOR DOUBLER Y=-607 FR8/11. REMOVED AND REPLACED LH OB COCKPIT GUSSET FR8-11.
- [SDR JJBA202003265014](https://openairdocs.org/sdr/JJBA202003265014), Mar 25, 2020: SUPPORT. CORRODED. RH WING - O/B LWR SHROUD, O/B BOTH CENTERS AND I/B SPRING SUPPORTS HAVE CORROSION. REMOVED AND REPLACED RH WING - OB LWR SHROUD, OB BOTH CENTERS AND I/B SPRING 
- [SDR JJBA202003264015](https://openairdocs.org/sdr/JJBA202003264015), Mar 24, 2020: SUPPORT. CORRODED. L/H WING - I/B LWR SHROUD, I/B SPRING SUPPORT HAVE CORROSION AS MARKED. REMOVED AND REPLACED L/H WING - I/B LWR SHROUD, I/B SPRING SUPPORT
- [SDR JJBA202003264013](https://openairdocs.org/sdr/JJBA202003264013), Mar 24, 2020: SUPPORT. CORRODED. L/H WING - O/B LWR SHROUD, O/B AND BOTH CENTER SPRING SUPPORTS HAVE CORROSION AS MARKED. REMOVED AND REPLACED 3EA L/H WING O/B LWR SHROUD, O/B AND BOTH CENTER S
- [SDR JJBA202003261016](https://openairdocs.org/sdr/JJBA202003261016), Mar 21, 2020: SUPPORT. CORRODED. R/H WING - I/B LWR SHROUD, I/B AND O/B SPRING SUPPORT HAVE CORROSION AS MARKED. INSTALLED NU PLATES, REMOVED AND REPLACED R/H WING - I/B LWR SHROUD, I/B AND O/B
- [SDR JJBA2020032616018](https://openairdocs.org/sdr/JJBA2020032616018), Mar 16, 2020: SKIN. NOT REPORTED. LOCATE THE CIRCULAR DOUBLER REPAIR AT FRAME 28, STRINGER 16R. REMOVE THE DOUBLER, REPORT THE SKIN CONDITION TO RTS FOR PERMANENT REPAIR INSTRUCTIONS AND DAMAGE 
- [SDR JJBA2020032615021](https://openairdocs.org/sdr/JJBA2020032615021), Mar 15, 2020: SKIN. DAMAGED. FOUND SEVERAL TOOLING MARKS BELOW ADF ANTENNA. INSTALLED REPAIR DOUBLER TO INTERNAL FUSELAGE BETWEEN FR42-FR44 STR1R
- [SDR JJBA2020032015011](https://openairdocs.org/sdr/JJBA2020032015011), Mar 15, 2020: DOUBLER. CORRODED. RH WING PANEL 198 DOUBLER FOR NUT PLATES HAS CORROSION ALONG DOUBLER AS MARKED. FABRICATED, LOCTED, DRILLED, ALODINED AND PRIMED 2(EA) DOUBLERS ON RH WING PANEL
- [SDR JJBA2020032015010](https://openairdocs.org/sdr/JJBA2020032015010), Mar 15, 2020: DOUBLER. CORRODED. CORROSION - COCKPIT FLOOR DOUBLER Y=+607.0 FR 9/10. REMOVED AND REPLACED RH OB COCKPIT GUSSET
- [SDR JJBA2020032015009](https://openairdocs.org/sdr/JJBA2020032015009), Mar 15, 2020: DOUBLER. CORRODED. CORROSION - COCKPIT FLOOR DOUBLER Y=-293.0 FR9/11. SPLICED IN NEW PILOT INBD FLOOR DOUBLER AND DOUBLERS
- [SDR JJBA2020032614017](https://openairdocs.org/sdr/JJBA2020032614017), Mar 14, 2020: SKIN. NOT REPORTED. LOCATE THE CIRCULAR DOUBLER REPAIR AT FRAMES 19-20, STRINGERS 15L-17L REMOVE THE DOUBLER, REPORT THE SKIN CONDITION TO RTS FOR PERMANENT REPAIR INSTRUCTIONS AND
- [SDR JJBA2020032005008](https://openairdocs.org/sdr/JJBA2020032005008), Mar 5, 2020: FLOOR SUPPORT. CORRODED. LH OMEGA BEAM CORRODED AS MARKED FROM FR 50-45. REMOVED AND REPLACED LH OMEGA BEAM FR45-52. CORROSION FOUND TO BE LEVEL 2
- [SDR JJBA2020032003007](https://openairdocs.org/sdr/JJBA2020032003007), Mar 3, 2020: FLOOR SUPPORT. CORRODED. R/H OMEGA BEAM CORRODED ON FR23 AS MARKED. REPAIRED RH OMEGA BEAM CORRODED ON FR23 BY CUTTING OUT THE DAMAGE AND INSTALLING A DOUBLER. CORROSION FOUND TO BE LEV
- [SDR JJBA202001064001](https://openairdocs.org/sdr/JJBA202001064001), Jan 4, 2020: MUFFLER. UNSECURE. RETURN TO FIELD DUE TO PAX COMPLAINTS OF EXTREME AMOUNTS OF CONDENSATION AND BANGING NOISES AROUND ROW 9 RIGHT SIDE. R&R PACK MUFFLER. OPS CHECK SAT.
- [SDR JJBA201912264010](https://openairdocs.org/sdr/JJBA201912264010), Dec 24, 2019: CONTROL MODULE. FAILED. SMOKE COMING FROM FA PANEL. PERFORMED GVI OF COMPONENTS & CONNECTORS AROUND FA PANEL. FOUND CONTROL MODULE UNIT BURNED OUT. R&R CONTROL MODULE UNIT. OPS CHECK S
- [SDR JJBA201910185007](https://openairdocs.org/sdr/JJBA201910185007), Oct 15, 2019: LIGHT. MISSING. ISLE PATH EMERGENCY STRIP FO SIDE NEXT TO GALLEY WITH RED DOTS IS MISSING. INSTALLED EMERGENCY STRIP NEXT TO GALLEY AS REQUIRED.
- [SDR JJBA201910185006](https://openairdocs.org/sdr/JJBA201910185006), Oct 15, 2019: LIGHT. MISINSTALLED. ISLE PATH EMERGENCY STRIP ON CAPTAIN SIDE NEXT TO MAIN CABIN DOOR BACKWARDS. CORRECTLY INSTALLED EMERGENCY STRIP ON CAPTAINS SIDE NEXT TO MAIN CABIN DOOR AS REQ
- [SDR JJBA20190808003](https://openairdocs.org/sdr/JJBA20190808003), Aug 8, 2019: LATCH. NO TEST. THE PRESSURE RELIEF LATCH ON THE COCKPIT DOOR FAILED FUNCTIONAL TEST, REQUIRED TOO MUCH FORCE TO OPEN AND CLOSE PAST DETENT. CLEANED PRESSURE RELIEF LATCH BOLT.
- [SDR JJBA20190718016](https://openairdocs.org/sdr/JJBA20190718016), Jul 18, 2019: BATTERY PACK. DISCHARGED. EMERGENCY EXIT LIGHT ABOVE SERVICE DOOR INOPERATIVE. R&R EMERGENCY EXIT LIGHT AND R&R BATTERY #2. OPS CHECK SAT.
- [SDR JJBA20190129038](https://openairdocs.org/sdr/JJBA20190129038), Jan 29, 2019: ECS. CONTAMINATED. SMOKE IN THE COCKPIT ON TAKE-OFF ROLL. ON TAKE-OFF ROLL ADVANCED THROTTLES COCKPIT FILLED WITH SMOKE. NO SMOKE IN CABIN, DID NOT DECLARE EMERGENCY, APU NOT ON, 
- [SDR JJBA201811095003](https://openairdocs.org/sdr/JJBA201811095003), Nov 5, 2018: RECEPTACLE. DAMAGED. GPU EXTERNAL SOCKET DAMAGED. RECONTOURED DENTED AREA AFT OF FR 06. ACCOMPLISHED 30X DET VISUAL INSPECTION ON AND AROUND REWORKED AREA. FABRICATED REPAIR PARTS. 
- [SDR JJBA20180927012](https://openairdocs.org/sdr/JJBA20180927012), Sep 27, 2018: SOLENOID VALVE. FAILED. NOSE GEAR DOOR OPENED INFLIGHT ON DECENT AT 6000 FT. R&R NLG DOOR SOLENOID VALVE. OPS & LEAK CHECK SAT.
- [SDR JJBA20180827013](https://openairdocs.org/sdr/JJBA20180827013), Aug 27, 2018: SIGN. DETACHED. FORWARD OVERHEAD EMERGENCY EXIT SIGN DETACHED. ATTACHED THE FORWARD OVERHEAD EMERGENCY EXIT SIGN. OPS CHECKED SAT.
- [SDR ASOA201701103001](https://openairdocs.org/sdr/ASOA201701103001), Jan 10, 2017: CLAMP. WORN. THE CREW REPORTED BLEED NR 1 LEAK WARNING IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE CLAMP ON LEFT PRECOOLER FORWARD DUCT. OPERATIONAL CHECKS WERE GOOD.
- [SDR ASOA201610100726](https://openairdocs.org/sdr/ASOA201610100726), Oct 10, 2016: BEAM. CORRODED. DURING C-CHECK. CARGO DOOR CUTOUT LOWER BEAM CORRODED. REMOVED AND REPLACED CARGO DOOR LOWER BEAM IAW SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160508029](https://openairdocs.org/sdr/ASOA20160508029), May 8, 2016: BATTERY PACK. INOPERATIVE. DURING ROUTINE MAINTENANCE, MULTIPLE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.
- [SDR ASOA20150426038H](https://openairdocs.org/sdr/ASOA20150426038H), Apr 26, 2015: INVERTER. INOPERATIVE. THE CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE THE F/A HEADSET WAS INOPERATIVE. MAINTENANCE R & R THE NR 1 INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS NOTE
- [SDR ASOA20141220154H](https://openairdocs.org/sdr/ASOA20141220154H), Dec 20, 2014: LIGHT. INTERMITTENT. THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ABOVE THE FORWARD F/A SEAT WAS INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHT SYSTEM, OPS TESTED WITH NO DEF
- [SDR ASOA20140801083](https://openairdocs.org/sdr/ASOA20140801083), Aug 1, 2014: SMOKE WARNING. FALSE ACTIVATION. CREW REPORTED LAVATORY SMOKE WARNING INTERMITTENTLY ALARMS. MX PERFORMED LAV SMOKE OPS CHECKS IAW SUPPLEMENT 26-14-00, OPS CHECKED GOOD. ACFT WAS APPROVED FOR R
- [SDR ASOA20140702052](https://openairdocs.org/sdr/ASOA20140702052), Jul 2, 2014: BATTERY. DISCHARGED. THE CREW REPORTED GALLEY AND ROW 3 EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.
- [SDR ASOA20140509058](https://openairdocs.org/sdr/ASOA20140509058), May 8, 2014: DOOR SILL. CORRODED. DURING C-CHECK THE FORWARD 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 ASOA20140509057](https://openairdocs.org/sdr/ASOA20140509057), May 8, 2014: 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 ASOA20140506056V](https://openairdocs.org/sdr/ASOA20140506056V), May 6, 2014: YOKE. CRACKED. DURING C-CHECK, THE NR 1 ENGINE FORWARD LOWER YOKE FITTING WAS FOUND TO BE CRACKED, VERIFIED WITH EDDY CURRENT. MAINTENANCE R & R THE FITTING IAW EC5450-01087. 
- [SDR ASOA20130829159](https://openairdocs.org/sdr/ASOA20130829159), Aug 29, 2013: CONTROLLER. SMOKE. THE CREW REPORTED ELECTRICAL SMOKE COMING FROM THE VS BUTTON OF THE FLIGHT GUIDANCE PANEL. MX R & R THE FLIGHT GUIDANCE CONTROLLER, OPERATIONALLY TESTED WITH NO
- [SDR ASOA20130808146H](https://openairdocs.org/sdr/ASOA20130808146H), Aug 8, 2013: RELAY. INOPERATIVE. THE CREW REPORTED THAT PACK 1 AND 2 VALVES CLOSED IN FLIGHT. THE ACFT RETURNED TO WHERE IT LANDED WITHOUT INCIDENT. MX R & R RELAY K0435, OPS TESTED BOTH PACKS 
- [SDR ASOA20130116236](https://openairdocs.org/sdr/ASOA20130116236), Jan 16, 2013: INVERTER. INOPERATIVE. AFT OVERWING EXIT LOCATOR LIGHT INOPERATIVE. R & R NR 4 INVERTER. OPS CHECKED GOOD.
- [SDR ASOA20120723063](https://openairdocs.org/sdr/ASOA20120723063), Jul 23, 2012: BATTERY. DISCHARGED. DURING ROUTINE MX, THE AFT OVERHEAD EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX ARMED AND RECHARGED THE EMERGENCY LIGHT SYS. OPS CHECKED GOOD.
- [SDR ASOA20120531042](https://openairdocs.org/sdr/ASOA20120531042), May 31, 2012: BATTERY PACK. FAILED. DURING MX INSPECTION, THE NR 4 EMERGENCY LIGHT BATTERY WAS FOUND TO NOT BE HOLDING CHARGE. MX R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-04 WITH 
- [SDR ASOA20120406021](https://openairdocs.org/sdr/ASOA20120406021), Apr 6, 2012: STRINGER. CORRODED. DURING C-CHECK, STRINGER 21R CORRODED BETWEEN FRAME 12-13. R & R STRINGER WITH NEW STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120406020](https://openairdocs.org/sdr/ASOA20120406020), Apr 6, 2012: STRINGER. CORRODED. DURING C-CHECK, STRINGER 21L CORRODED BETWEEN FRAMES 12-13. R & R STRINGER WITH NEW STRINGER 21L, FRAME 9-13 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN 
- [SDR ASOA20111211014](https://openairdocs.org/sdr/ASOA20111211014), Dec 11, 2011: ELECTRONIC UNIT. FAULTY. THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE. MX INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPS CHECKS WERE GOOD.
- [SDR C2XA11TY169](https://openairdocs.org/sdr/C2XA11TY169), Nov 9, 2011: SENSOR. DEFECTIVE. TYS - A/C WAS EN ROUTE FROM ORD TO CHS WHEN THE E1 HP SHOWED A HIGH VIBE INDICATION/SHUT DOWN IN FLIGHT. NO OTHER ABNORMAL CONDITIONS OCCURRED. A/C DIVERTED TO 
- [SDR C2XA11RI171](https://openairdocs.org/sdr/C2XA11RI171), Oct 19, 2011: ACTUATOR. FAULTY. FLT 5862 IAD CREW REPORTED LG AIR/GRND FAIL MESSAGE ON EICAS DURING GEAR EXTENSION. GEAR OPERATED NORMALLY AND A/C LANDED WITHOUT INCIDENT. IAD MX REMOVED AND R
- [SDR C2XA11RI136](https://openairdocs.org/sdr/C2XA11RI136), Aug 16, 2011: FUEL LINE. LEAKING. FLIGHT 2566 - EWR - FLIGHT CREW REPORTED STRONG FUEL SMELL IN COCKPIT DURING TAXI. EWR MX PERFORMED GVI ON APU AREA AND FOUND FCU LINES LEAKING. SUSPECT SMELL I

All 67: https://openairdocs.org/aircraft/N11181/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/N11181/stcs.md

## Earlier aircraft with N11181

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N11181 before.

- [Cancelled 1997-05-13](https://openairdocs.org/deregistered/N11181-1997-05-13): Raytheon 58, S/N TH1801. Exported to Indonesia. Owner: [Hawker Pacific Inc](https://openairdocs.org/faa-owner/HAWKER%20PACIFIC%20INC), [Sun Valley, CA](https://openairdocs.org/faa-place/CA/Sun%20Valley)
- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N11181-undated): Cessna 150L, S/N 15075241

## 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

---
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.