# N41104: 2002 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: 145646
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2005
- Certificate issued: October 30, 2019
- Expires: October 31, 2029
- Mode S code: A4DA4C
- 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=41104
- Page: https://openairdocs.org/aircraft/N41104

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/N41104/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 N41104.

## FAA accident and incident reports

None matched to N41104.

## Service difficulty reports (66, 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 RAIA2019101590002](https://openairdocs.org/sdr/RAIA2019101590002), Oct 9, 2019: BRACKET. BINDING. DISCREPANT CONDITION: DURING A DEPARTMENT OF DEFENSE SCHEDULED AUDIT IT WAS FOUND THAT THE FORWARD LEFT HAND PORTABLE BREATHING EQUIPMENT CONTAINER WAS DIFFICUL
- [SDR RAIA2019082310001](https://openairdocs.org/sdr/RAIA2019082310001), Aug 21, 2019: LIGHT. INOPERATIVE. LEFT AFT WING TO FUSLAGE FAIRING EXTERIOR FLOOD LIGHT NR 5 WAS INOPERATIVE. R & R LEFT OVERWING EMERGENCY LIGHT. OPS CHECKED GOOD.
- [SDR RAIA2019040850001](https://openairdocs.org/sdr/RAIA2019040850001), Apr 5, 2019: O-RING. FAILED. BLEED 1 LEAK CLIMBING THROUGH 11K FT. NO VISIBLE MOISTURE... FOUND LEAKS AT SENSORS 15,17 AND 9. REPLACED O-RINGS AT LOCATIONS 15,17 AND 9. LEAK CHECK GOOD AT T
- [SDR RAIA201903260001](https://openairdocs.org/sdr/RAIA201903260001), Mar 26, 2019: O-RING. DAMAGED. BLEED LEAK 1 IN FLIGHT. FOUND LEAKING DUCT AT AFT BULKHEAD FWD OF APU FIREWALL. R2 O-RING LEAK AND OPS CHECK GOOD.
- [SDR RAIA201903170001](https://openairdocs.org/sdr/RAIA201903170001), Mar 17, 2019: HYDRAULIC LINE. DAMAGED. ENGINE 1 HYD SYSTEM FAILURE WITH ASSOCIATED MESSAGES. INSPECTED NR 1 EDP, HYD HOSE DAMAGED. R&R'D SYSTEM NR 1 PRESSURE(PUMP) HOSE OPS AND LEAK CHECK GOOD.
- [SDR RAIA2018122200001](https://openairdocs.org/sdr/RAIA2018122200001), Dec 20, 2018: A/C PACK. OVERTEMP. PACK 2 OVERHEAT WITH BURING SMELL IN COCKPIT. COMPLIED WITH STEPS 5 BLOCK 1, 2, AND 12 OF EIM TGASK. COMPLED WITH BLOCK 2 STEPS 1 AND 2 WITH BOTH ENGINES AT TAK
- [SDR RAIA201707110001](https://openairdocs.org/sdr/RAIA201707110001), Jul 11, 2017: LIGHT. CRACKED. EMERGENCY LIGHT STRIP IS CRACKED ACROSS FROM SEAT 2A. R & R THE LIGHT STRIP, OPS CHECK GOOD.
- [SDR RAIA201602010001](https://openairdocs.org/sdr/RAIA201602010001), Feb 1, 2016: LIGHT. INOPERATIVE. PAX DOOR EMERGENCY FLOOD LIGHT NR 1 INOPERATIVE. R & R PAX DOOR EMERGENCY FLOOD LIGHT. OPS CHECKED GOOD.
- [SDR RAIA201601060002](https://openairdocs.org/sdr/RAIA201601060002), Jan 6, 2016: POWER SUPPLY. INOPERATIVE. NR 11 MAIN DOOR EXIT MARKER LIGHT IS INOPERATIVE. R & R NR1 BATTERY POWER SUPPLY. OPS CHECK GOOD.
- [SDR RAIA201601060001](https://openairdocs.org/sdr/RAIA201601060001), Jan 6, 2016: POWER SUPPLY. INOPERATIVE. NR 1 MAIN DOOR EXTERIOR FLOOD LIGHT ON BOTTOM SIDE OF THE PLUG DOOR HINGE IS INOPERATIVE. R & R NR 1 BATTERY POWER SUPPLY. OPS CHECK GOOD.
- [SDR RAIA201512230001](https://openairdocs.org/sdr/RAIA201512230001), Dec 23, 2015: PROXIMITY SWITCH. INOPERATIVE. NOSE GEAR DOOR DID NOT CLOSE AFTER GEAR RETRACTION, 1 MAIN GEAR POSSIBLY DOWN DURING CLIMB, RETURNED TO BLOCK. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDI
- [SDR RAIA201505270001](https://openairdocs.org/sdr/RAIA201505270001), May 27, 2015: BLEED VALVE. FAILED. APU BLEED VALVE FAILED MESSAGE FOLLOWED BY APU FAILED MESSAGE ON EICAS, APU INDICATED 28V ON BUSS, ACFT RETURNED TO BLOCKS. REPLACED THE BLEED VALVE, OPS CHECKE
- [SDR ASOA20131231144R](https://openairdocs.org/sdr/ASOA20131231144R), Dec 31, 2013: CONNECTOR. UNSECURE. THE CENTER OVERHEAD EMERGENCY EXIT LIGHT ABOVE ROW 18 WAS REPORTED INOPERATIVE. MX SECURED CONNECTOR ON SIGN AND OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR R
- [SDR ASOA20131230143](https://openairdocs.org/sdr/ASOA20131230143), Dec 30, 2013: PANEL. INOPERATIVE. THE CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT SIGN WAS REPORTED INOPERATIVE. MX R & R THE LIGHT PANEL ASSY WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR R
- [SDR ASOA20121003130](https://openairdocs.org/sdr/ASOA20121003130), Oct 3, 2012: POWER SUPPLY. INOPERATIVE. DURING MX INSPECTION, AN OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, OPS TESTED WITH NO DEFECTS, A
- [SDR ASOA11IA004](https://openairdocs.org/sdr/ASOA11IA004), Nov 22, 2011: WARNING MESSAGE. FALSE ACTIVATION. DURING CLIMB, THE CREW RECEIVED AN AUTOPILOT FAIL MESSAGE ON THE EICAS DISPLAY. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORME
- [SDR ASOA20111120004](https://openairdocs.org/sdr/ASOA20111120004), Nov 20, 2011: AOA. BURNED. ACFT WAS ENROUTE WHEN LIGHTNING STRUCK ACFT CAUSING A BURNING ODOR IN THE CABIN. THE CREW LANDED SAFELY. MX COMPLIED WITH A LIGHTNING STRIKE INSPECTION IAW AMM2
- [SDR C2XA11CL210](https://openairdocs.org/sdr/C2XA11CL210), Sep 18, 2011: LIGHT. INOPERATIVE. CORRECTED SDR FOR A/C 41104 NEW NUMBER: DURING ROUTINE MAINTENANCE THE RIGHT EXTERNAL FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND R
- [SDR C2XA11CL209A](https://openairdocs.org/sdr/C2XA11CL209A), Sep 18, 2011: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE THE RIGHT EXTERNAL FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OP
- [SDR C2XA11TY016](https://openairdocs.org/sdr/C2XA11TY016), Feb 16, 2011: ENGINE. MALFUNCTIONED. TYS - A/C WAS EN ROUTE FROM IAH TO IND WHEN THE CREW REPORTED A HAZY SMOKE IN CABIN, AFTER LANDING MOSTLY IN THE AFT CABIN. LANDING WAS NORMAL AND NO ICIAS INDI
- [SDR C2XA11CL032](https://openairdocs.org/sdr/C2XA11CL032), Feb 2, 2011: ENGINE. CONTAMINATED. MHT FLT 2635 - THE CREW REPORTED SMOKE IN THE CABIN, COCKPIT AFTER TAKEOFF. ALSO RECEIVED A LAV SMOKE MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO MHT AND LAN
- [SDR C2XA11SH031](https://openairdocs.org/sdr/C2XA11SH031), Jan 30, 2011: ATTACH BRACKET. DAMAGED. SHV - DURING C-CHECK LT AILERON I/B HAT BUSHING OF O/B ATTACHMENT POINT OF PCA IS MIGRATED. REPLACED ATTACHMENT BRACKET IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS A
- [SDR C2XA11SH030](https://openairdocs.org/sdr/C2XA11SH030), Jan 30, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 48-49. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-21-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11CL007](https://openairdocs.org/sdr/C2XA11CL007), Jan 7, 2011: COFFEEMAKER. CONTAMINATED. THE CREW REPORTED A BURNING SMELL IN THE GALLEY. MAINTENANCE INSPECTED AND FOUND PLASTIC DEBRIS ON THE NR 2 COFFEE POT. REMOVED DEBRIS AND OPERATIONAL CHECKS WE
- [SDR C2XA10RI130](https://openairdocs.org/sdr/C2XA10RI130), Oct 15, 2010: PANEL. INOPERATIVE. FLIGHT 3009 - EWR - FLIGHT CREW REPORTED LAV SMOKE TEST INOPERATIVE. EWR MX REMOVED AND REPLACED LAV SMOKE PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. A
- [SDR C2XA10IA249](https://openairdocs.org/sdr/C2XA10IA249), Sep 8, 2010: SWITCH. DEFECTIVE. IAH - FLIGHT 2020, THE CREW REPORTED A BLEED ONE OVERTEMP IN ICING CONDITIONS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVE
- [SDR C2XA10CL041](https://openairdocs.org/sdr/C2XA10CL041), Mar 3, 2010: SMOKE DETECTOR. FAILED. DURING ROUTINE MAINTENANCE THE AFT CARGO SMOKE DETECTOR FAILED THE TASK CARD 26-15-01-212-001-A00 OPERATIONAL CHECKS. MAINTENANCE REPLACED THE SMOKE DETECTOR AN
- [SDR C2XA09IA288A](https://openairdocs.org/sdr/C2XA09IA288A), Nov 10, 2009: PROXIMITY SWITCH. INOPERATIVE. IAH - FLIGHT 2365, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL AND E1-2 TR DISAGREE MESSAGES IN CRUISE. WHEN EXTENDING THE LANDING GEAR ON APPROACH, ALL ME
- [SDR C2XA09TY165](https://openairdocs.org/sdr/C2XA09TY165), Jul 15, 2009: SILL. CORRODED. SERVICE DOOR SILL CORRODED AT SCREW HOLES. BLENDED MINOR CORROSION IAW SRM 51-10-03, RESTORED FINISH.
- [SDR C2XA09TY164](https://openairdocs.org/sdr/C2XA09TY164), Jul 15, 2009: SKIN. DENTED. 2 DENTS, LT FUSELAGE BETWEEN FR 19 AND 20. REPAIRED DAMAGE IAW IC2009-145/04712. REFINISHED SURFACE IAW CPM51-21-07, EC5330-01937.
- [SDR C2XA09TY162](https://openairdocs.org/sdr/C2XA09TY162), Jul 15, 2009: FLOOR SUPPORT. CORRODED. ACFT IN C-CHECK WHEN THE INBD SIDE OF THE LT OMEGA BEAM WAS FOUND CORRODED AT FR 54 THRU FR 58. MX BLENDED THE SURFACE CORROSION IAW SRM 51-10-03 AND ALODINED, 
- [SDR C2XA09TY160](https://openairdocs.org/sdr/C2XA09TY160), Jul 15, 2009: SILL. CORRODED. ACFT IN C-CHECK AND THE RT FLOOR SILL AT FR 36 THRU FR 42 WAS FOUND CORRODED. MX REMOVED AND REPLACED THE FLOOR SILL IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED
- [SDR C2XA09TY159](https://openairdocs.org/sdr/C2XA09TY159), Jul 15, 2009: SILL. CORRODED. ACFT IN C-CHECK AND THE RT FLOOR SILL FROM FR 42 THRU FR 48 WAS FOUND CORRODED. MX REMOVED AND REPLACED THE FLOOR SILL IAW SRM 51-40-02 AND CPM 51-21-04-05-06. 
- [SDR C2XA09TY158](https://openairdocs.org/sdr/C2XA09TY158), Jul 15, 2009: SILL. CORRODED. ACFT IN C-CHECK AND THE RT FLOOR SILL AT FRAME 33 THRU FRAME 34 WAS FOUND CORRODED. MX BLENDED OUT THE CORROSION, FOUND TO BE WITHIN LIMITS. ALLODINED, PRIMED A
- [SDR C2XA09TY157](https://openairdocs.org/sdr/C2XA09TY157), Jul 15, 2009: SILL. CORRODED. AIRCRAFT IN C-CHECK STATUS AND THE LT FLOOR SILL AT FRAME 32 THRU FRAME 33 WAS FOUND CORRODED. MX REMOVED AND REPLACED THE FLOOR SILL IAW SRM 51-40-02. ALL WORK
- [SDR C2XA09TY155](https://openairdocs.org/sdr/C2XA09TY155), Jul 14, 2009: SKIN. GOUGED. ACFT CURRENTLY IN A C-CHECK STATUS WHEN INSP FOUND A GOUGE ON THE PAX DOOR AFT SIDE LWR EDGE. MX MEASURED, BLENDED AND INSTALL A DOUBLER OVER THE DAMAGED AREA. 
- [SDR C2XA09TY166](https://openairdocs.org/sdr/C2XA09TY166), Jul 13, 2009: SILL. CORRODED. RT FLOOR SILL CORRODED AT FRM 50. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-23-10, RESTORED FINISH.
- [SDR C2XA09TY154](https://openairdocs.org/sdr/C2XA09TY154), Jul 13, 2009: SILL. CORRODED. LT FLOOR SILL CORRODED AT FRM 47. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02.
- [SDR C2XA09TY153](https://openairdocs.org/sdr/C2XA09TY153), Jul 13, 2009: SILL. CORRODED. LT FLOOR SILL AT FRM 32-33 HAS CORROSION. REMOVED AND REPLACED SILL IAW SRM 51-40-02.
- [SDR C2XA09TY151](https://openairdocs.org/sdr/C2XA09TY151), Jul 13, 2009: SHEAR TIE. CRACKED. SHEAR CLIP HAS A CRACK AT FR 81 AND STR 10L. REMOVED AND REPLACED CRACKED SHEAR CLIP IAW SRM 51-40-02.
- [SDR C2XA09TY138](https://openairdocs.org/sdr/C2XA09TY138), Jul 4, 2009: SKIN. DENTED. FUSELAGE DENTED AT FRM 28, STR 13R. REPAIRED BY CUTTING OUT DAMAGED AREA, FABRICATED FILLER AND INSTALLED DOUBLER IAW EC5330-01936. AIRCRAFT STILL IN C-CHECK.
- [SDR C2XA09TY137](https://openairdocs.org/sdr/C2XA09TY137), Jul 1, 2009: SILL. CORRODED. LT FLOOR SILL CORRODED AT FRAME 47. REMOVED AND REPLACED FLOOR SILL.
- [SDR C2XA09TY136](https://openairdocs.org/sdr/C2XA09TY136), Jul 1, 2009: SILL. CORRODED. LT FLOOR SILL IS CORRODED AT FRM 49. REMOVED AND REPLACED FLOOR SILL.
- [SDR C2XA09TY135](https://openairdocs.org/sdr/C2XA09TY135), Jul 1, 2009: SILL. CORRODED. AFT GUSSET IN GALLEY AREA CORRODED. THE AFT GUSSET WAS REMOVED AND REPLACED.
- [SDR C2XA09TY133](https://openairdocs.org/sdr/C2XA09TY133), Jun 29, 2009: SILL. CORRODED. TYS - AIRCRAFT CURRENTLY IN A C-CHECK STATUS AND INSPECTION FOUND THE RT FLOOR SILL FROM FR 53 TO FR 59 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SIL
- [SDR C2XA09TY134](https://openairdocs.org/sdr/C2XA09TY134), Jun 29, 2009: SILL. CORRODED. TYS - AIRCRAFT IN C-CHECK STATUS AND INSPECTION FOUND THE LT FLOOR SILL AT FR 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB 145XR SRM 51-
- [SDR C2XA09IA145A](https://openairdocs.org/sdr/C2XA09IA145A), Jun 4, 2009: CONTROLLER. INOPERATIVE. THE CREW REPORTED A WINDSHIELD HEAT FAIL MESSAGE ON EICAS. THE ACFT DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. MX PLACEDTHE WINDSHIELD HEAT ON MEL, AND THE ACF
- [SDR C2XA09TY104](https://openairdocs.org/sdr/C2XA09TY104), Jun 4, 2009: WARNING SYSTEM. MALFUNCTIONED. TYS - AIRCRAFT EN ROUTE FROM IAH TO ORF WHEN THE WINDSHIELD HEAT FAIL. AIRCRAFT DIVERTED TO BNA AND SWAPPED AIRCRAFT TO 192. MAINTENANCE COULDN'T DUPLICATE PROB
- [SDR C2XA08IA251](https://openairdocs.org/sdr/C2XA08IA251), Dec 11, 2008: ENGINE. SMOKE. IAH - FLIGHT 2160, THE FLIGHT ATTENDANT REPORTED THAT A HAZE DEVELOPED IN THE CABIN FOLLOWED BY A MOMENTARY LAV SMOKE INDICATION. THE ACFT RETURNED TO IAH WHERE
- [SDR C2XA08RI177](https://openairdocs.org/sdr/C2XA08RI177), Dec 3, 2008: CONTROL PANEL. DEFECTIVE. FLIGHT 2966 - EWR - FLIGHT CREW REPORTED LAVATORY SMOKE INDICATION ON EICAS DURING CLIMBING WITH A SLIGHT SMELL OF SMOKE. CREW PERFORMED AIR RETURN AND LANDED A

All 66: https://openairdocs.org/aircraft/N41104/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/N41104/stcs.md

## Earlier aircraft with N41104

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N41104 before.

- [Cancelled 1975-03-20](https://openairdocs.org/deregistered/N41104-1975-03-20): Cessna 310R, S/N 310R0076, built 1975. Exported to Democratic Republic of the Congo. Owner: [Floair Inc](https://openairdocs.org/faa-owner/FLOAIR%20INC), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- [Cancelled 1948-09-27](https://openairdocs.org/deregistered/N41104-1948-09-27): Piper J-3, S/N 7760. Owner: [Bailey Charles Edward](https://openairdocs.org/faa-owner/BAILEY%20CHARLES%20EDWARD), [Madison, NC](https://openairdocs.org/faa-place/NC/Madison)

## 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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