# N11107: 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: 145654
- 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: A03262
- 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=11107
- Page: https://openairdocs.org/aircraft/N11107

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/N11107/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 N11107.

## FAA accident and incident reports

None matched to N11107.

## Service difficulty reports (71, 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 JJBA20220304004](https://openairdocs.org/sdr/JJBA20220304004), Mar 4, 2022: LAMP. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT ASSEMBLY. OPS CHECK FAIL. UPON FURTHER INVESTIGATION FOUND BROKEN SP
- [SDR JJBA20220304003](https://openairdocs.org/sdr/JJBA20220304003), Mar 4, 2022: LAMP. INOPERATIVE. LH EXTERNAL EMERGENCY WING FAIRING LIGHT FOUND TO BE DIM. REMOVED AND REPLACED LH EXTERNAL EMERGENCY WING FAIRING LIGHT. OPS CHECK FAILED. FOUND HOUSING TO HAVE
- [SDR JJBA20210217018](https://openairdocs.org/sdr/JJBA20210217018), Feb 17, 2022: NOT REPORTED. NOT REPORTED. FLOOR PATH LIGHTING STRIP "EXIT" PLACARDS ARE MISPOSITIONED. CORRECTLY ORIENTED FLOOR PATH LIGHTING STRIPS "EXIT" PLACARDS.
- [SDR JJBA2022020431033](https://openairdocs.org/sdr/JJBA2022020431033), Jan 31, 2022: COFFEEMAKER. ODOR. FA REPORTS BURNING SMELL FROM COFFEE MAKERS. CLEANED UP COFFEE BREW WARMER, PERFORMED VISUAL INSPECTION COFFEE BREW CRACKS, WIRES. NO DEFECTS NOTED. OPS CHECK G
- [SDR JJBA20211213009](https://openairdocs.org/sdr/JJBA20211213009), Dec 13, 2021: LAMP. INOPERATIVE. EMERGENCY EXIT LIGHT FORWARD OF WING INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK SAT.
- [SDR JJBA20210603008](https://openairdocs.org/sdr/JJBA20210603008), Jun 3, 2021: INVERTER. INOPERATIVE. FWD CEILING CABIN EMERGENCY EXIT LOCATOR LIGHT INOPERATIVE. R&R EMERGENCY LIGHT INVERTER 6. OPS CHECK SAT.
- [SDR JJBA20210517015](https://openairdocs.org/sdr/JJBA20210517015), May 17, 2021: BULB. BURNED OUT. ENTRYWAY EMERGENCY LIGHT BULB BURNT OUT. R&R ENTRYWAY LIGHT BULB. OPS CHECK SAT.
- [SDR ASOA2020071304016](https://openairdocs.org/sdr/ASOA2020071304016), Jul 10, 2020: DISPLAY. INOPERATIVE. IAH - FLIGHT 3980, THE CREW REPORTED PFD#1 FAIL "SMOKED SMELL". THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED PFD#1, OPERATIONAL
- [SDR ASOA2020030433020](https://openairdocs.org/sdr/ASOA2020030433020), Feb 3, 2020: SKIN. CHAFED. DURING C CHECK INSPECTION FOUND LEFT ELEVATOR LEADING EDGE SKIN WAS CHAFED INTERNALLY JUST FORWARD OF CUTOUT REINFORCEMENT BETWEEN RIB YH983.4 AND YH1280. MAINT
- [SDR ASOA2020030693026](https://openairdocs.org/sdr/ASOA2020030693026), Jan 29, 2020: RIB. CORRODED. DURING C CHECK INSPECTION FOUND VENTRAL TANK FORWARD FACE OF RIB 1 HAS CORROSION AT LOWER CENTER SUPPORT BRACKET. MAINTENANCE REPAIRED VENTRAL TANK RIB 1 I/A/W 
- [SDR ASOA202002193015](https://openairdocs.org/sdr/ASOA202002193015), Jan 9, 2020: SKIN. CORRODED. DURING C CHECK INSPECTION FOUND CORROSSION ON FUSELAGE SKIN AT AFT RADIO ALTIMETER AT FRAME 65 STRINGER 21L-21R. MAINTENANCE REPAIRED I/A/W ETD2020-145-001101
- [SDR ASOA2020030463025](https://openairdocs.org/sdr/ASOA2020030463025), Jan 6, 2020: FLOOR SUPPORT. CORRODED. DURING C CHECK INSPECTION FOUND FLOOR BOARD SUPPORT CORRODED FRAME 18-23 STRINGER 15L-16L. MAINTENANCE REPLACED FLOOR BOARD SUPPORT
- [SDR ASOA202002193016](https://openairdocs.org/sdr/ASOA202002193016), Jan 5, 2020: DOUBLER. CORRODED. DURING C CHECK INSPECTION FOUND CORROSSION AND MISSING RIVET ON AFT RADIO ALTIMETER BASE FRAME 68-69 AND STRINGER 21L-21R. MAINTENANCE PERFROMED REPAIR I/A/W ET
- [SDR ASOA2020020353006](https://openairdocs.org/sdr/ASOA2020020353006), Jan 5, 2020: BEARING CAP. CORRODED. DURING C CHECK INSPECTION FOUND RIGHT FORWARD MAIN LANDING GEAR BEARING CAP HAD CORROSION/PITTING. MAINTENANCE REPLACED THE RIGHT FORWARD MAIN LANDING GEAR BEAR
- [SDR ASOA2020021903017](https://openairdocs.org/sdr/ASOA2020021903017), Jan 3, 2020: SKIN SPLICE. CORRODED. DURING C CHECK INSPECTION SKIN SPLICE WAS FOUND CORRODED AT FRAME 60-61 STRINGER 20R-21R. MAINTENANCE REPAIRED I/A/W SRM 53-00-02 AND 51-40-02.
- [SDR ASOA2020020633014](https://openairdocs.org/sdr/ASOA2020020633014), Jan 3, 2020: GUSSET. CORRODED. DURING C CHECK INSPECTION FOUND LAV FLOOR CENTER GUSSET AT FRAME 61 HAS SURFACE CORROSION. MAINTENANCE REPLACED LAV FLOOR CENTER GUSSET.
- [SDR ASOA2020020633013](https://openairdocs.org/sdr/ASOA2020020633013), Jan 3, 2020: GUSSET. CORRODED. DURING C CHECK INSPECTION FOUND CENTER FUSELAGE IV FLOOR GUSSET HAT BEAM AT FRAME 61 HAD CORROSION. MAINTENANCE REPLACED GUSSET HAT BEAM AT FRAME 61
- [SDR ASOA202002033008](https://openairdocs.org/sdr/ASOA202002033008), Jan 3, 2020: BEARING CAP. CORRODED. DURING C CHECK INSPECTION FOUND LEFT AFT MAIN LANDING GEAR BEARING CAP HAD CROSSION PITTING IN 1 AREA. MAINTENANCE INSPECTED AND REMOVED CORROSION IA/W SRM 57-5
- [SDR ASOA202002033007](https://openairdocs.org/sdr/ASOA202002033007), Jan 3, 2020: BEARING CAP. CORRODED. DURING C CHECK INSPECTION FOUND LEFT FORWARD MAIN LANDING GEAR BEARING CAP HAD 3 AREAS OF CORROSION/PITTING. MAINTENANCE REPLACED LEFT FORWARD MAIN LANDING GEAR
- [SDR ASOA202001313005](https://openairdocs.org/sdr/ASOA202001313005), Jan 3, 2020: FLOOR SUPPORT. CORRODED. DURING HEAVY CHECK INSPECTION FOUND CORROSION ON CENTER LAV FLOORBOARD SUPPORT AT FRAME 60-61. MAINTENANCE REPLACED LAV CENTER FLOOR BOARD SUPPORT. (GUSSET)
- [SDR ASOA202001313004](https://openairdocs.org/sdr/ASOA202001313004), Jan 3, 2020: GUSSET. CORRODED. DURING HEAVY MAINTENANCE CHECK CORROSSION WAS FOUND ON RIGHT SIDE LAV FLOORBOARD SUPPORT. AT FRAME 60 THRU61. MAINTENANCE REPLACED HAT BEAM GUSSET AT FRAME 60 T
- [SDR ASOA202002263018](https://openairdocs.org/sdr/ASOA202002263018), Jan 2, 2020: CHANNEL. CORRODED. DURING C CHECK INSPECTION FOUND SERVICE DOOR SILL CORRODED@HOLES FOR SCREWS. MAINTENANCE REPLACED THE SERVICE DOOR SILL CHANNEL.
- [SDR ASOA2020030313019](https://openairdocs.org/sdr/ASOA2020030313019), Dec 31, 2019: DOOR FRAME. CORRODED. DURING C CHECK INSPECTION CARGO DOOR CUTOUT SILL BEAM CORRODED AT FORWARD CORNER. MAINTENANCE REPLACED THE LOWER FRAME DOOR CARGO DOOR BEAM.
- [SDR ASOA2020030403024](https://openairdocs.org/sdr/ASOA2020030403024), Dec 30, 2019: SKIN. DAMAGED. DURING C CHECK INSPECTION RIGHT INBOARD FLAP UPPER SURFACE HAS DAMAGED COMPOSITE AT INBOARD EDGE. MAINTENANCE REPAIRED COMPOSITE DAMAGE AT UPPER SKIN INBOARD ED
- [SDR ASOA202002063012](https://openairdocs.org/sdr/ASOA202002063012), Dec 26, 2019: ROD. CORRODED. DURING C CHECK INSPECTION FOUND LEFT APU LOWER MOUNTING ROD END CORRODED.MAINTENANCE REPLACED LEFT LOWER ROD ASSEMBLY.
- [SDR ASOA20200206311](https://openairdocs.org/sdr/ASOA20200206311), Dec 26, 2019: SUPPORT ROD. CORRODED. DURING C CHECK INSPECTION FOUND UPPER APU MOUNTING RODENDS CORRODED. MAINTENANCE REPLACED APU UPPER SUPPORT RODS .
- [SDR ASOA2020304223022](https://openairdocs.org/sdr/ASOA2020304223022), Dec 22, 2019: RIB. CRACKED. DURING C CHECK INSPECTION THE LEFT WING RIB 21 WAS FOUND CRACKED. MAINTENANCE PERFORMED REPAIR I/A/W SRM 57-20-07.
- [SDR ASOA20200203009](https://openairdocs.org/sdr/ASOA20200203009), Dec 20, 2019: DOUBLER. CORRODED. DURING C CHECK INSPECTION FOUND CENTER FUSELAGE IV DRAIN PLUG DOUBLER HAD CORROSION, FRAME 53-FRAME 54 STRINGER 21 LH TO 21 RH. MAINTENANCE REPLACED DOUBLER I/A
- [SDR ASOA2020030493023](https://openairdocs.org/sdr/ASOA2020030493023), Dec 19, 2019: RIB. CRACKED. DURING C CHECK INSPECTION FOUND RIGHT WING RIB 21 CRACKED. MAINTENANCE REPAIRED RIGHT WING RIB 21 I/A/W SRM 57-20-07.
- [SDR ASOA2020030453021](https://openairdocs.org/sdr/ASOA2020030453021), Dec 15, 2019: SKIN. GOUGED. DURING C CHECK INSPECTION FOUND GOUGE ON FORWARD FUSELAGE SKIN II BELOW GPU ACCESS DOOR. MAINTENANCE REPAIRED DAMAGED SKIN I/A/W SRM 53-12-01 AND ETD2020-145-00
- [SDR ASOA201906294038](https://openairdocs.org/sdr/ASOA201906294038), Jun 29, 2019: LIGHT. INOPERATIVE. IAH - FLIGHT 4197, THE CREW REPORTED THAT THE EMERGENCY LIGHT NEAR THE EXIT DOOR IN THE CEILING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE 
- [SDR ASOA201902264007](https://openairdocs.org/sdr/ASOA201902264007), Feb 26, 2019: BATTERY PACK. DISCHARGED. ** SUPPLEMENTAL TO ASOA201802264007 CONTROL NUMBER SHOULD HAVE BEEN ASOA201902264007*** IAH- DURING MAINTENANCE INSPECTION SEVERAL EMERGENCY LIGHTS WEER FOUND T
- [SDR ASOA201902264008](https://openairdocs.org/sdr/ASOA201902264008), Feb 26, 2019: BATTERY PACK. DISCHARGED. IAH - DURING MAINTENANCE INSPECTION SEVERAL EMERGENCY LIGHTS WEER FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AND TWO EMERGENCY LIG
- [SDR ASOA201802177017](https://openairdocs.org/sdr/ASOA201802177017), Feb 17, 2018: SKIN. DENTED. FOUND A CREASED AREA AFT OF A RECENT REPAIR BETWEEN FRAMES 19 - 20 AND STRINGERS 11L AND 12L. MAINTENANCE REMOVED THE OLD DOUBLER AND CUT OUT THE DAMAGE AREA AN
- [SDR ASOA20140529087](https://openairdocs.org/sdr/ASOA20140529087), May 29, 2014: BRACKET. WORN. DURING C-CHECK, INSPECTION FOUND THE LT AILERON PCA BRACKET INBD HAT BUSHING FOR INBD ATTACH POINT HAS NO INTERFERENCE FIT. MAINTENANCE R & R THE LT AILERON PCA
- [SDR ASOA20140219019](https://openairdocs.org/sdr/ASOA20140219019), Feb 19, 2014: SWITCH. MALFUNCTIONED. THE CREW REPORTED AT FL350 WITH THRUST SET FOR CRUISE FLIGHT, THEY EXPERIENCED TWO AUTO RELIGHT SEQUENCES WITH NO ASSOCIATED CAUTION AND WARNING MESSAGES BUT DI
- [SDR ASOA20130610057](https://openairdocs.org/sdr/ASOA20130610057), Jun 10, 2013: UNKNOWN. ODOR. CREW REPORTED A ODOR OF SMOKE IMMEDIATELY AFTER THE ACFT WAS POSSIBLY STRUCK BY LIGHTNING. MX INSPECTED ACFT, RAN AIR CONDITIONING PACKS, TAXIED, AND HAD ELECTR
- [SDR ASOA20130424039](https://openairdocs.org/sdr/ASOA20130424039), Apr 24, 2013: OIL SYSTEM. OVERSERVICED. CREW REPORTED A STRONG ELECTRICAL ODOR IN COCKPIT AND CABIN AT FL220. MX PERFORMED FAULT ISOLATION TASK 21-20-00-810-801A AND 21-20-00-810-803A WITH NO DEFECTS 
- [SDR ASOA20121224182](https://openairdocs.org/sdr/ASOA20121224182), Dec 21, 2012: WIRE. SHORTED. MAIN DOOR EMERGENCY LIGHT AND MAIN ENTRANCE EMERGENCY LIGHT INOPERATIVE. REPAIRED SHORTED WIRE AT OVERHEAD LIGHT. OPS CHECK GOOD.
- [SDR ASOA20121025085](https://openairdocs.org/sdr/ASOA20121025085), Oct 25, 2012: ENGINE. LEAKING. THE CREW REPORTED SMOKE IN THE COCKPIT & CABIN AFTER TAKE-OFF, ALONG WITH LAVATORY SMOKE MESSAGE WARNING. AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURT
- [SDR ASOA20120508096](https://openairdocs.org/sdr/ASOA20120508096), May 8, 2012: FUEL TANK. GOUGED. BOTTOM CENTER OF THE VENTRAL TANK WAS FOUND GOUGED. MX REPAIRED VENTRAL TANK BY INSTALLING A DOUBLER IAW EC 2810-01053. ALL WORK ACCOMPLISHED AND WILL BE RELEAS
- [SDR ASOA20120405037](https://openairdocs.org/sdr/ASOA20120405037), Apr 5, 2012: BATTERY. DISCHARGED. DURING ROUTINE MX, EMERGENCY LIGHT INOPERATIVE AT EXIT ROW 12 A, B, C. REPLACED NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.
- [SDR ASOA20120229028](https://openairdocs.org/sdr/ASOA20120229028), Feb 29, 2012: UNKNOWN. ODOR. AFTER SHUTTING DOWN THE APU ON ARRIVAL CREW REPORTED AN ELECTRICAL BURNING ODOR. MX INSPECTED THE ACFT WITH NO DEFECTS NOTED, OPS TESTED APU WITH NO DEFECTS NOT
- [SDR ASOA2012180003](https://openairdocs.org/sdr/ASOA2012180003), Feb 18, 2012: SKIN. GOUGED. ACFT HAD GROUND DAMAGE AND WAS FERRIED FOR THE REPAIRS. THE FUSELAGE BETWEEN FR 65 TO FR 66 AND BETWEEN STR 17L AND 18L WERE DAMAGED. THE WORK WAS ACCOMPLISHED 
- [SDR C2XA11CL211](https://openairdocs.org/sdr/C2XA11CL211), Sep 20, 2011: TRIM SWITCH. FAULTY. THE CREW REPORTED A PITCH TRIM BACK-UP FAIL MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BACK-UP PITC
- [SDR C2XA11RI131](https://openairdocs.org/sdr/C2XA11RI131), Aug 9, 2011: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 3124 - EWR - FLIGHT CREW REPORTED L/G AIR GROUND FAIL INDICATION ON EICAS. EWR MX PERFORMED AIR GROUND SYSTEM RESET AND PERFORMED OPERATIONAL CHECK SUCCE
- [SDR C2XA11RI078](https://openairdocs.org/sdr/C2XA11RI078), May 12, 2011: AUDIO PANEL. DEFECTIVE. FLIGHT 4940 - EWR - FLIGHT CREW REPORTED FO AUDIO CONTROL PANEL GAVE OUT ELECTRICAL SMELL. EWR MX REMOVED AND REPLACED FO AUDIO CONTROL PANEL AND PERFORMED OPER
- [SDR C2XA10RI156](https://openairdocs.org/sdr/C2XA10RI156), Dec 12, 2010: SWITCH. INOPERATIVE. FLIGHT 2640 - MSN - FLIGHT CREW REPORTED WING ANTI-ICE FAIL IN ICE CONDITION - ANTI ICE INOPERATIVE. EWR MX REMOVED AND REPLACED NR 2 WING LOW PRESSURE SWITCH A
- [SDR C2XA10SH323](https://openairdocs.org/sdr/C2XA10SH323), Oct 4, 2010: SKIN. CRACKED. SHV - DURING C-CHECK EXTERNAL FUSELAGE HAS POSSIBLE CRACKS AROUND FASTENER HEAD AT FRAME 78 STR 5L. MAINTENANCE PERFORMED REPAIR ON FRAME 78-79 STR 5L-6L IAW EC
- [SDR C2XA10SH322](https://openairdocs.org/sdr/C2XA10SH322), Oct 4, 2010: CROSSBEAM. CORRODED. SHV - DURING C-CHECK CROSSBEAM AT FRAME 23 FROM CENTER OMEGA BEAM TO RT AFT FLOOR SILL HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CROSSBEAM

All 71: https://openairdocs.org/aircraft/N11107/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/N11107/stcs.md

## Earlier aircraft with N11107

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N11107 before.

- [Cancelled 1975-10-03](https://openairdocs.org/deregistered/N11107-1975-10-03): Cessna 150L, S/N 15075203. Exported to Canada. Owner: [Frankfort Aviation Service Inc](https://openairdocs.org/faa-owner/FRANKFORT%20AVIATION%20SERVICE%20INC), [Frankfort, IL](https://openairdocs.org/faa-place/IL/Frankfort)
- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N11107-undated): Hughes 269C, S/N 311039

## 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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