# N11106: 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: 145650
- 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: A03261
- 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=11106
- Page: https://openairdocs.org/aircraft/N11106

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/N11106/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 N11106.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20121014026179I](https://openairdocs.org/incident/20121014026179I), Oct 14, 2012: Embraer EMB-145XR (N11106), Chicago, IL, No damage. Aircraft departed ord and lavatory smoke detector activated and then cabin and cockpit had odor and presence of smoke. Crew returned to ord landing on runway…
- [Incident 20100519037299I](https://openairdocs.org/incident/20100519037299I), May 19, 2010: Embraer EMB-145XR (N11106), No damage. Contact asap event review chairman.

## Service difficulty reports (136, 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 JJBA20210331004](https://openairdocs.org/sdr/JJBA20210331004), Mar 31, 2021: ARMREST. CRACKED. FOUND CRACK ON SEAT 4A ARMREST STRUCTURE. R&R PASSENGER SEAT 4A. NO FURTHER DAMAGE NOTED.
- [SDR JJBA20201210012](https://openairdocs.org/sdr/JJBA20201210012), Dec 10, 2020: FUSE. FAILED. BOTH LT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED (1) FUSE ON NR 4 EMERGENCY BATTERY TRAY. OPERATIONS CHECK GOOD.
- [SDR JJBA20201113010](https://openairdocs.org/sdr/JJBA20201113010), Nov 13, 2020: SKIN. CRACKED. REAR FUSE 1, LOWER SKIN CRACKED AT FR 75A BETWEEN STR 21P-21S. REPAIRED DOUBLER AND TRIPLER INSTALLED AND FRAME BOTTOM SECTION REPLACED.
- [SDR JJBA20201109007](https://openairdocs.org/sdr/JJBA20201109007), Nov 9, 2020: SKIN. DAMAGED. DURING REMOVAL OF REPAIR DOUBLER LOCATED ON RT CENTER FUSE 1 BETWEEN FRAME 19-20 AND STR 18-19R. RT CENTER FUSELAGE I BETWEEN FR 19-20 AND BETWEEN STR 18R-20R D
- [SDR JJBA20201103006](https://openairdocs.org/sdr/JJBA20201103006), Nov 3, 2020: SKIN. DAMAGED. SKIN DAMAGE ON RT FWD FUSE 2, BETWEEN FR 11-12 AND BETWEEN STR 17R-18R. SKIN REPAIRED ON RT FWD FUSELAGE 2, BETWEEN FR 11-12, BETWEEN STR 17R-18R.
- [SDR RAIA2020031910001](https://openairdocs.org/sdr/RAIA2020031910001), Mar 11, 2020: FLOOR SUPPORT. CORRODED. LAV CENTER OMEGA BEAM AT FR 59 HAS CORROSION AROUND NUT PLATE HOLE - CUT-OUT DAMAGE AROUND NUT PLATE HOLE AT FR 59 CENTER OMEGA BEAM. PERFORMED HF EC INSPECTION
- [SDR RAIA2020031980001](https://openairdocs.org/sdr/RAIA2020031980001), Mar 8, 2020: FLOOR SUPPORT. CORRODED. FRAME 18 AFT DIGITAL SUPPORT IS CORRODED - REMOVED AFT DIGITAL SUPPORT AT FR 18. INSTALLED AFT DIGITAL SUPPORT AT FR 18.
- [SDR RAIA2020032640002](https://openairdocs.org/sdr/RAIA2020032640002), Mar 4, 2020: CHANNEL. CRACKED. CHANNEL IS CRACKED AT FR 10 UNDER RH DV WINDOW - R&R LH FR 10 UNDER DV WINDOW. INSTALLED NEW RH FR 10 UNDER DV WINDOW.
- [SDR RAIA2020032640001](https://openairdocs.org/sdr/RAIA2020032640001), Mar 4, 2020: CHANNEL. CRACKED. CHANNEL IS CRACKED AT FR 10 UNDER LH DV WINDOW - R&R LH FR 10 CHANNEL.
- [SDR RAIA2020040130004](https://openairdocs.org/sdr/RAIA2020040130004), Mar 3, 2020: WEB. CRACKED. L/H W/W REAR WEB IS CRACKED AT TOP O/B CORNER....R&R L/H W/W REAR WEB.
- [SDR RAIA2020032730003](https://openairdocs.org/sdr/RAIA2020032730003), Mar 3, 2020: WEB. CRACKED. LH W/W REAR WEB IS CRACKED AT TOP O/B CORNER - R/R LH W/W REAR WEB, NEEDS BELLY FAIRING TEMP INSTALLED TO PICK UP NUTPLATE HOLES. INSTALLED NUTPLATES ON LH W/W 
- [SDR RAIA2020032130002](https://openairdocs.org/sdr/RAIA2020032130002), Mar 3, 2020: ANGLE. CORRODED. CARGO DOOR UPPER & LOWER EDGE HAS LIGHT CORROSION AROUND FASTENER HOLES - REMOVED LOWER DOOR ANGLE, UPPER ANGLE FOUND TO BE PAINT DAMAGE PREPPED AND PAINTED AFF
- [SDR RAIA2020031930001](https://openairdocs.org/sdr/RAIA2020031930001), Mar 3, 2020: FITTING. CRACKED. #1 ENGINE PYLON FWD YOKE LOWER FWD LINKAGE FITTING IS CRACKED - REMOVED AND REPLACED #1 ENGINE PYLON FWD YOKE LOWER FWD LINKAGE FITTING.
- [SDR RAIA2020032620029](https://openairdocs.org/sdr/RAIA2020032620029), Mar 2, 2020: FLOOR SUPPORT. CORRODED. CENTER OMEGA BEAM UPPER DIGITAL HAS CORROSION AROUND FASTENER HOLE AT FR 16 - BEGAN REPAIR ON THE FWD DIGITAL PLATE, CENTER OMEGA BEAM AT FR 16. COMPLETED REPAI
- [SDR RAIA2020032620028](https://openairdocs.org/sdr/RAIA2020032620028), Mar 2, 2020: SUPPORT ANGLE. CRACKED. LH OVER WING LATERAL FAIRING NUTPLATE SUPPORT ANGLE ON L/E OF WING UPPER SURFACE IS CRACKED AT FR 41 - REPAIRED LH OVER WING NUTPLATE SUPPORT ANGLE AT FR 41, ST
- [SDR RAIA2020032120027](https://openairdocs.org/sdr/RAIA2020032120027), Mar 2, 2020: SUPPORT. CRACKED. LH OVER WING LATERAL FAIRING NUTPLATE ATTACH ANGLE SUPPORT ON SIDE OF FUSELAGE BELOW OVER WING EXIT IS CRACKED - REMOVED LH OVERWING LATERAL FAIRING ATTACH ANGL
- [SDR RAIA2020032120026](https://openairdocs.org/sdr/RAIA2020032120026), Mar 2, 2020: SHEAR TIE. CRACKED. MAIN CABIN FR 16 SHEER CLIP IS CRACKED AT STR 15 RH - REMOVED AND REPLACED SHEER CLIP AT FR 16 RH SIDE.
- [SDR RAIA2020032020025](https://openairdocs.org/sdr/RAIA2020032020025), Mar 2, 2020: SUPPORT ANGLE. CORRODED. MAIN CABIN CENTER OMEGA BEAM O/B LOWER SUPPORT ANGLE IS CORRODED AND CRACKED BETWEEN FR 46 & 47 - REMOVED OMEGA BEAM LWR SUPPORT, PICKED UP HOLES IN NEW SUPPORT
- [SDR RAIA202003200024](https://openairdocs.org/sdr/RAIA202003200024), Mar 2, 2020: DOOR SILL. CORRODED. RH FLOOR SILL FWD OF SERVICE DOOR AT FR 20 HAS CORROSION AROUND NUTPLATE HOLE - FABRICATED FWD SILL REPAIR. INSTALLED FWD SILL REPAIR ON RH FLOOR SILL FWD OF SE
- [SDR RAIA2020031920023](https://openairdocs.org/sdr/RAIA2020031920023), Mar 2, 2020: DOOR SILL. CORRODED. MAIN CABIN RH FLOOR SILL HAS CORROSION ON UPPER SURFACE AT FR 50 - REMOVED RH FLOOR SILL AT FR 50. STARTED LOCATING FASTENER HOLES IN NEW RH FLOOR SILL AT FR 50
- [SDR RAIA2020031920017](https://openairdocs.org/sdr/RAIA2020031920017), Mar 2, 2020: DOOR SILL. CORRODED. MAIN CABIN RH SIDE FLOOR SILL HAS CORROSION AT FR 40 ON UPPER SURFACE. REMOVED FLOOR SILL AT FR 40, LOCATED FASTENER AND STARTED INSTALL. COMPLETED INSTALL OF N
- [SDR RAIA2020031920022](https://openairdocs.org/sdr/RAIA2020031920022), Mar 2, 2020: SUPPORT. CRACKED. MAIN CABIN LH OMEGA BEAM O/B LOWER SUPPORT IS CRACKED BETWEEN FR 47 & 48 - BEGAN REMOVING HI-LOK COLLARS FROM THE LH OMEGA BEAM O/B LOWER SUPPORT AT FR 47 & 48.
- [SDR RAIA2020031920021](https://openairdocs.org/sdr/RAIA2020031920021), Mar 2, 2020: SUPPORT ANGLE. CRACKED. MAIN CABIN RH OMEGA BEAM I/B LOWER SUPPORT ANGLE IS CRACKED BETWEEN FR 47 & 48 - REPAIRED RH OMEGA BEAM I/B LOWER SUPPORT AT FR 47.
- [SDR RAIA2020031920020](https://openairdocs.org/sdr/RAIA2020031920020), Mar 2, 2020: SUPPORT ANGLE. CRACKED. MAIN CABIN RH OMEGA BEAM O/B LOWER SUPPORT ANGLE IS CRACKED BETWEEN FR 47 & 48 - REMOVED O/B LOWER SUPPORT AND LOCATED HOLES IN NEW PART. INSTALLED RH OMEGA BEA
- [SDR RAIA2020031920019](https://openairdocs.org/sdr/RAIA2020031920019), Mar 2, 2020: DOOR SILL. CORRODED. MAIN CABIN RH SIDE FLOOR SILL HAS CORROSION BETWEEN FR 40 THRU 47 - REMOVED & REPLACED MAIN CABIN RH FLOOR SILL BETWEEN FR 40 THRU 47.
- [SDR RAIA2020031920018](https://openairdocs.org/sdr/RAIA2020031920018), Mar 2, 2020: DOOR SILL. CORRODED. MAIN CABIN LH SIDE FLOOR SILL HAS CORROSION ON UPPER SURFACE BETWEEN FR 26 THRU 39 - R&R LH FLOOR SILL AT FR 36 THRU 39.
- [SDR RAIA2020031920016](https://openairdocs.org/sdr/RAIA2020031920016), Mar 2, 2020: SEAT TRACK. CORRODED. RH SIDEWALL SEAT TRACKS HAVE LIGHT CORROSION BETWEEN FR 28 THRU 32 - REMOVED SEAT TRACK ON WALL AT FRAME 29. INSTALLED SEAT TRACK AT FRAME 29.
- [SDR RAIA2020031920015](https://openairdocs.org/sdr/RAIA2020031920015), Mar 2, 2020: SHEAR TIE. CRACKED. MAIN CABIN FR 26 SHEER CLIP IS CRACKED AT STR 16 RH - R/R MAIN CABIN FR 26 SHEER CLIP AT STR 16 RH.
- [SDR RAIA2020031920014](https://openairdocs.org/sdr/RAIA2020031920014), Mar 2, 2020: SHEAR TIE. CRACKED. MAIN CABIN FR 25 SHEER CLIP IS CRACKED AT STR 15 RH - R&R MAIN CABIN FR 25 SHEER CLIP AT STR 15 RH.
- [SDR RAIA2020031920013](https://openairdocs.org/sdr/RAIA2020031920013), Mar 2, 2020: DOOR SILL. CORRODED. MAIN CABIN LH FLOOR SILL HAS CORROSION FROM FR 26 THRU 29 - REMOVED MAIN CABIN LH FLOOR SILL FR 26-29, STARTED LOCATING FASTENER HOLES. COMPLETED INSTALL OF NEW
- [SDR RAIA2020031920012](https://openairdocs.org/sdr/RAIA2020031920012), Mar 2, 2020: SEAT TRACK. CORRODED. LH SIDEWALL SEAT TRACK HAS CORROSION BETWEEN FR 20 THRU 23 - REMOVED THE LH SIDEWALL SEAT TRACK. INSTALLED SEAT TRACK LH.
- [SDR RAIA2020031920011](https://openairdocs.org/sdr/RAIA2020031920011), Mar 2, 2020: RIVET. DEFECTIVE. MAIN CABIN CENTER OMEGA BEAM UPPER DIGITAL HAS CORROSION BETWEEN FR 20 THRU 23 - UPON FURTHER INSPECTION FOUND TO BE DAMAGED PAINT AND HIGH RIVETS. REMOVED AND 
- [SDR RAIA2020031920010](https://openairdocs.org/sdr/RAIA2020031920010), Mar 2, 2020: THRESHOLD. CORRODED. SERVICE DOOR THRESHOLD HAS CORROSION AROUND NUTPLATE HOLES BETWEEN FR 20 THRU 22 - R&R SERVICE DOOR THRESHOLD BETWEEN FR 20-22.
- [SDR RAIA2020031920009](https://openairdocs.org/sdr/RAIA2020031920009), Mar 2, 2020: STRUCTURE. CORRODED. MAIN CABIN STOP SIGN ON RH OMEGA BEAM HAS CORROSION AT FR 20 ON UPPER SURFACE - R&R MAIN CABIN STOP SIGN ON RH OMEGA BEAM AT FR 20.
- [SDR RAIA2020031920008](https://openairdocs.org/sdr/RAIA2020031920008), Mar 2, 2020: ANGLE. CORRODED. MAIN CABIN CENTER OMEGA BEAM RAMP ANGLE SUPPORT AFT END HAS CORROSION ON LOWER SIDE AT FR 20 - REMOVED RAMP ANGLE AT FR 20. INSTALLED GALLEY RAMP ANGLE AT FR 20
- [SDR RAIA2020031920007](https://openairdocs.org/sdr/RAIA2020031920007), Mar 2, 2020: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR SUPPORT BETWEEN LH OMEGA BEAM AND CENTER OMEGA BEAM AT FR 20 HAS CORROSION - REMOVED FLOOR SUPPORT BETWEEN LH & CTR OMEGA BEAM AT FR 20. INSTAL
- [SDR RAIA2020031920006](https://openairdocs.org/sdr/RAIA2020031920006), Mar 2, 2020: FLOOR SUPPORT. BENT. LH FLOOR STEP UP BETWEEN CENTER OMEGA BEAM AND RH OMEGA BEAM IS BENT AT FR 18 - R&R FLOOR STEP UP AT FR 18
- [SDR RAIA2020031920005](https://openairdocs.org/sdr/RAIA2020031920005), Mar 2, 2020: DOOR SILL. CORRODED. LH FLOOR SILL HAS CORROSION AT FR 20 - REMOVED THE LH FLOOR SILL AT FR 20. INSTALLED LH FLOOR SILL AT FR 20.
- [SDR RAIA2020030620004](https://openairdocs.org/sdr/RAIA2020030620004), Mar 2, 2020: DOOR SILL. CORRODED. MAIN CABIN RH FLOOR SILL HAS CORROSION FROM FR 30 THRU 35 RH - REMOVED AND LOCATED HOLES TO NEW SILL. INSTALLED FLOOR SILL AT FR 30.
- [SDR RAIA2020030620002](https://openairdocs.org/sdr/RAIA2020030620002), Mar 2, 2020: DOOR SILL. CORRODED. MAIN CABIN LH FLOOR SILL HAS CORROSION FROM FR 30 THRU 25 - R&R LH FLOOR SILL FROM FRAME 30 THRU 35.
- [SDR RAIA2020032710014](https://openairdocs.org/sdr/RAIA2020032710014), Mar 1, 2020: SHEAR TIE. CRACKED. INSIDE ACCESS 312AR FRAME 80 SHEER CLIP IS CRACKED BETWEEN STR 4 & 5RH - DRILLED OUT RIVETS AND REWORKED SHEER CLIP OFF OF AIRPLANE, HOLES NEED TO BE PICKED UP 
- [SDR RAIA2020031910013](https://openairdocs.org/sdr/RAIA2020031910013), Mar 1, 2020: SHEAR TIE. CRACKED. SHEER CLIP CRACKED AT FR 62 BETWEEN STR 6L-7L - PERFORMED HF EC INSPECTION OF SHEER CLIP CRACK CONFIRMED, GOOD TO CONTINUE WITH REPAIR. REMOVED CRACKED SHEER CL
- [SDR RAIA2020031910012](https://openairdocs.org/sdr/RAIA2020031910012), Mar 1, 2020: DOOR SILL. CORRODED. LH LAV FLOOR SILL HAS CORROSION AROUND NUT PLATE HOLES - R&R LH LAV FLOOR SILL.
- [SDR RAIA2020031910011](https://openairdocs.org/sdr/RAIA2020031910011), Mar 1, 2020: GUSSET. CORRODED. LH LAV GUSSET HAS CORROSION AROUND NUT PLATE HOLES - REMOVED LH LAV GUSSET. LOCATED HOLES ON NEW LH LAV GUSSET AND INSTALLED.
- [SDR RAIA2020031910010](https://openairdocs.org/sdr/RAIA2020031910010), Mar 1, 2020: GUSSET. CORRODED. CTR GUSSET IN LAV HAS CORROSION AROUND NUT PLATE HOLES - REMOVED CTR GUSSET AT LAV. LOCATED HOLES ON NEW CTR LAV GUSSET AND INSTALLED.
- [SDR RAIA2020031910009](https://openairdocs.org/sdr/RAIA2020031910009), Mar 1, 2020: GUSSET. CORRODED. RH LAV GUSSET HAS CORROSION AROUND NUT PLATE HOLES - REMOVED RH LAV GUSSET. LOCATED HOLES IN NEW GUSSET AND INSTALLED RH LAV GUSSET.
- [SDR RAIA2020031910008](https://openairdocs.org/sdr/RAIA2020031910008), Mar 1, 2020: DOOR SILL. CORRODED. RH LAV FLOOR SILL HAS CORROSION AROUND NUT PLATE HOLES - REMOVED CORROSION ON RH LAV FLOOR SILL AROUND NUT PLATE HOLE.
- [SDR RAIA2020031910007](https://openairdocs.org/sdr/RAIA2020031910007), Mar 1, 2020: SUPPORT BEAM. BENT. CARGO FLOOR SUPPORT BEAM IS BENT AT FR-68 BETWEEN CTR AND LH GUSSETS - REMOVED AND REPLACED SUPPORT BEAM AT FR 68.
- [SDR RAIA2020031910006](https://openairdocs.org/sdr/RAIA2020031910006), Mar 1, 2020: ATTACH BRACKET. CRACKED. CARGO RAMP FWD SUPPORT LOWER ATTACH BRACKET IS CRACKED - REMOVED AND REPLACED BRACKET.
- [SDR RAIA2020031910005](https://openairdocs.org/sdr/RAIA2020031910005), Mar 1, 2020: SHEAR TIE. CRACKED. SHEER CLIP IS CRACKED FR67 BETWEEN STR 6L-7L - REMOVED SHEEAR CLIP AT FR67. INSTALLED SHEER CLIP AT FR 67.

All 136: https://openairdocs.org/aircraft/N11106/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/N11106/stcs.md

## Earlier aircraft with N11106

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N11106 before.

- [Cancelled 1977-07-06](https://openairdocs.org/deregistered/N11106-1977-07-06): Cessna 150L, S/N 15075202. Owner: [M J Inc](https://openairdocs.org/faa-owner/M%20J%20INC), [Cedar Rapids, IA](https://openairdocs.org/faa-place/IA/Cedar%20Rapids)

## 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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