# N12122: 2003 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: 145684
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2005
- Certificate issued: June 26, 2019
- Expires: June 30, 2029
- Mode S code: A05A22
- Registered owner: [Untied Airlines Inc](https://openairdocs.org/faa-owner/UNTIED%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=12122
- Page: https://openairdocs.org/aircraft/N12122

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/N12122/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 N12122.

## FAA accident and incident reports

None matched to N12122.

## Reports on N12122 not matched to an aircraft (1)

They name N12122, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19970119000549I](https://openairdocs.org/incident/19970119000549I), Jan 19, 1997: Cessna 172M (N12122), Rockwall, TX, Minor damage. Narrative: on January 19, 1997, at approximately 1600 CST, mr. Douglas f. early, private pilot, landed a Cessna 172, N12122 at F46, Rockwall, Texas and ran off…

## Service difficulty reports (59, 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 RAIA2019083028001](https://openairdocs.org/sdr/RAIA2019083028001), Aug 28, 2019: FUEL CAP. UNSECURE. R/H WING FUEL CAP UNSECURED IN FLIGHT. SECURED FEUL CAP AND INSPECTED FOR DAMAGE. NONE FOUND.
- [SDR RAIA201901130001](https://openairdocs.org/sdr/RAIA201901130001), Jan 13, 2019: PUMP. INOPERATIVE. HYDRAULIC SYSTEM NR 1 LOW QUANITY FOLLOWED BY HYDRAULIC SYSTEM NR 1 FAILURE. (HYD SYS PRESSURE WAS NOTED AT ZERO WHEN THE FAILURE MESSAGE CAME UP ALONG WITH NR 
- [SDR RAIA201812200008](https://openairdocs.org/sdr/RAIA201812200008), Dec 20, 2018: PROXIMITY SWITCH. MALFUNCTIONED. LANDING GEAR AIR GROUND FAIL EICAS MESSAGE. R&R BOTH AIR/GROUND PROX SWITCHES. CHECKED CONNECTORS AND HARNESSES FOR ALL LANDING GEAR. NO DEFECTS NOTED.
- [SDR RAIA2018101980001](https://openairdocs.org/sdr/RAIA2018101980001), Oct 18, 2018: UNKNOWN. MALFUNCTIONED. HIGH STAGE VALVE 1 FAIL ON TAKE OFF ROLL. SWAPPED HIGH STAGE VALVE FROM E1 TO E2 AND E2 TO E1. OPS CHECK GOOD ON BOTH HIGH STAGE VALVES.
- [SDR RAIA201810090001](https://openairdocs.org/sdr/RAIA201810090001), Oct 9, 2018: VALVE. MALFUNCTIONED. BLEED 2 OVERTEMP. R2 FAN AIR VALVE. OPS CHECK GOOD.
- [SDR RAIA2018082530001](https://openairdocs.org/sdr/RAIA2018082530001), Aug 23, 2018: RMU. BURNED OUT. RMU 1 WENT BLANK WITH BURING SMELL IN COCKPIT. R & R THE NR 1 RMU. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR RAIA201807250001](https://openairdocs.org/sdr/RAIA201807250001), Jul 25, 2018: CONTROL UNIT. MALFUNCTIONED. MAIN PITCH TRIM INOP IN FLIGHT. REMOVED/REPLACED HORIZONTAL STAB CONTROLLER UNIT IAW AMM 27-40-01. OPS TEST GOOD AT THIS TIME.
- [SDR RAIA2018053130001](https://openairdocs.org/sdr/RAIA2018053130001), May 23, 2018: PANEL. DETACHED. TWO WING PANELS FELL OFF IN FLT ON LT AND RT WINGS. REPLACED THE INSPECTION PANELS.
- [SDR RAIA201803130001](https://openairdocs.org/sdr/RAIA201803130001), Mar 13, 2018: LIGHT. INOPERATIVE. PAX DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE LIGHT ASSEMBLY. OPS CHECKED GOOD.
- [SDR RAIA201801100001](https://openairdocs.org/sdr/RAIA201801100001), Jan 10, 2018: LINE. DISCONNECTED. NR 2 PACK FAILED WITH NO WARNING IN FLT. INSPECTED THE NR 2 PACK AND FOUND THE SENSE LINE DISCONNECTED. CONNECTED THE SENSE LINE, OPS CHECKED GOOD.
- [SDR RAIA201708310002](https://openairdocs.org/sdr/RAIA201708310002), Aug 31, 2017: BULB. INOPERATIVE. LEFT AFT EMERGENCY EXIT DOOR LIGHT NR 23 INOPERATIVE. R & R THE BULB, OPS CHECKED GOOD.
- [SDR RAIA201701100001](https://openairdocs.org/sdr/RAIA201701100001), Jan 10, 2017: BULB. INOPERATIVE. PAX DOOR SWING ARM EMERGENCY LIGHT IS INOPERATIVE AND LENS IS CRACKED. REMOVED AND REPLACED THE BULB AND LENS OPS CHECKED GOOD.
- [SDR RAIA201608170001](https://openairdocs.org/sdr/RAIA201608170001), Aug 17, 2016: VALVE. INOPERATIVE. THE NR 1 PACK VALVE CLOSED MESSAGE ON EICAS WITH CB F7 TRIPPED. R & R THE NR 1 PACK VALVE OPS CHECK GOOD.
- [SDR RAIA201607240001](https://openairdocs.org/sdr/RAIA201607240001), Jul 24, 2016: CRADLE. INOPERATIVE. AFT FA FLASHLIGHT HOLDER NOT CHARGING THE FLASHLIGHT.
- [SDR RAIA201605020001](https://openairdocs.org/sdr/RAIA201605020001), May 2, 2016: STRUT. UNDERSERVICED. LANDING GEAR WOULD NOT RETRACT. LANDING GEAR AIR, GROUND FAIL MSG ON EICAS. DURING INSPECTION, TROUBLESHOOTING FOUND NLG LEG NOT CENTERING. PERFORMED SERVICING 
- [SDR RAIA201602220002](https://openairdocs.org/sdr/RAIA201602220002), Feb 22, 2016: BULB. INOPERATIVE. PAX DOOR EMERGENCY FLOOD LIGHT NR 1 INOPERATIVE. R & R PAX DOOR EMERGENCY FLOOD LIGHT BULB. OPS CHECK GOOD.
- [SDR RAIA201601210001](https://openairdocs.org/sdr/RAIA201601210001), Jan 21, 2016: BULB. INOPERATIVE. PASSENGER DOOR EMERGENCY LIGHT NR 1 INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.
- [SDR ASOA20150706024](https://openairdocs.org/sdr/ASOA20150706024), Jul 5, 2015: INVERTER. INOPERATIVE. NR 1 & NR 3 INVERTER FOR EMERGENCY LIGHTS INOPERATIVE. R & R NR 1 & NR 3 INVERTER. OPS CHECK GOOD ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20150521118](https://openairdocs.org/sdr/ASOA20150521118), May 21, 2015: DOOR SILL. CORRODED. DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140909106](https://openairdocs.org/sdr/ASOA20140909106), Sep 5, 2014: FADEC. UNKNOWN. NR 1 ENGINE HAD UNCOMMANDED THRUST REDUCTION DURING FLIGHT. R & R NR 1 FADEC. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20140513071](https://openairdocs.org/sdr/ASOA20140513071), May 13, 2014: ENGINE. SMOKE. THE CREW REPORTED THAT THE CABIN AND FLT DECK FILLED WITH SMOKE DURING CLIMB. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE
- [SDR ASOA20130924171](https://openairdocs.org/sdr/ASOA20130924171), Sep 24, 2013: ACM. SEIZED. CREW REPORTED SMOKE IN THE COCKPIT AND FWD CABIN IN FLIGHT, SMOKE SMELLED ELECTRICAL AND DISSIPATED AFTER A COUPLE OF MINUTES. NO ABNORMAL INDICATIONS IN FLIGHT
- [SDR ASOA20130222264](https://openairdocs.org/sdr/ASOA20130222264), Feb 22, 2013: LIGHT. INOPERATIVE. LEFT OVERWING EXIT LIGHT INOPERATIVE. R & R LT OVERWING EMERGENCY EXIT LIGHT.
- [SDR ASOA20130209260](https://openairdocs.org/sdr/ASOA20130209260), Feb 9, 2013: DOUBLER. CORRODED. ACFT IS FOR A ESCALATION WORK WHEN THE FUSELAGE WAS FOUND CHAFED FROM CONTACT FROM A LANYARD INSIDE RT PYLON. MX INSTALL A DOUBLER OVER BLENDED AREA THAT WAS CH
- [SDR ASOA20120117002](https://openairdocs.org/sdr/ASOA20120117002), Jan 17, 2012: POWER SUPPLY. INOPERATIVE. DURING SCHEDULED MX INSPECTION, IT WAS FOUND THAT THE AFT LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MX R & R THE NR 4 BATTERY 
- [SDR C2XA11TY081](https://openairdocs.org/sdr/C2XA11TY081), Jun 9, 2011: CHARGER. INOPERATIVE. RT EMERGENCY LIGHT ON PANEL 191 INOP. REMOVED AND REPLACED POWER SUPPLY CHARGER NR 2 IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO
- [SDR C2XA11CL100](https://openairdocs.org/sdr/C2XA11CL100), Apr 21, 2011: SWITCH. FAULTY. THE CREW REPORTED A RUDDER 1 & 2 INOP MESSAGE IN CLIMB AT FL340. SWITCHING SYS 2 OFF CAUSED SYS 1 TO WORK NORMALLY. THE ACFT DIVERTED AND LANDED WITHOUT INCIDEN
- [SDR C2XA11RI021](https://openairdocs.org/sdr/C2XA11RI021), Feb 13, 2011: ACM. DEFECTIVE. FLIGHT 2746 - EWR - FLIGHT CREW REPORTED AUTO PRESS ERRACTIC AND FAIL. EWR MX REMOVED AND REPLACED NR 1 ACM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT W
- [SDR C2XA10R1155](https://openairdocs.org/sdr/C2XA10R1155), Dec 18, 2010: ADC. FAILED. FLIGHT 2746 EWR-YQB FLIGHT CREW REPORTED NR 1 AIR DATA COMPUTER FAILED WITH A RED X OVER NR 1 TAPE. CREW PERFORMED AIR RETURN TO EWR AND LANDED ACFT UNEVENFULLY
- [SDR C2XA10CL132](https://openairdocs.org/sdr/C2XA10CL132), Aug 13, 2010: SMOKE DETECTOR. MALFUNCTIONED. THE CREW REPORTED A BAG SMOKE INOP MESSAGE ON THE EICAS. MAINTENANCE INSPECTED AND REPLACED THE BAG SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10IA227](https://openairdocs.org/sdr/C2XA10IA227), Aug 12, 2010: SMOKE DETECTOR. MALFUNCTIONED. IAH - FLIGHT 2274, DURING PREFLIGHT INSPECTION A BAGGAGE SMOKE INDICATION ON EICAS WAS REPORTED. THE BOTTLES WERE BLOWN AS PRECAUTION. MAINTENANCE INSPECTED THE
- [SDR C2XA10IA226](https://openairdocs.org/sdr/C2XA10IA226), Aug 12, 2010: SMOKE DETECTOR. MALFUNCTIONED. IAH - FLIGHT 2274, DURING PREFLIGHT INSPECTION A BAGGAGE SMOKE INDICATION ON EICAS WAS REPORTED. THE BOTTLES WERE BLOWN AS PRECAUTION. MAINTENANCE INSPECTED THE
- [SDR C2XA10TY075](https://openairdocs.org/sdr/C2XA10TY075), Apr 29, 2010: BATTERY. FAILED. BACK-UP BATTERY FAILED FUNCTION CHECK. REMOVED AND REPLACED BACK-UP BATTERY IAW EMB 145 AMM 24-35-01. OPS CHECK GOOD.
- [SDR C2XA10IA057](https://openairdocs.org/sdr/C2XA10IA057), Feb 7, 2010: PRESSURE SYSTEM. MALFUNCTIONED. FLIGHT 2010 - CLIMBING THROUGH FL320 PRESSURIZATION ^P WAS 8 AND CABIN ALTITUDE WAS 8000. THE AIRCRAFT DESCENDED TO FL240 AT WHICH TIME THE ^P WAS 6.6 AND CABIN
- [SDR C2XA10RI007](https://openairdocs.org/sdr/C2XA10RI007), Jan 6, 2010: UNKNOWN. ODOR. FLIGHT 2279 - EWR - FLIGHT CREW REPORTED ON THE GROUND IN EWR, DURING APU START, SMELL OF FUEL COMING OUT OF THE PACKS. EWR MX PERFORMED OPERATIONAL CHECK OF AP
- [SDR C2XA09229](https://openairdocs.org/sdr/C2XA09229), Dec 27, 2009: ENGINE. SMOKE. FLIGHT 3060 - EWR - FLIGHT CREW REPORTED NR 1 ENGINE EMITTING AN UNUSUAL AMOUNT OF SMOKE AFTER BEING SHUTDOWN. EWR MX RAN ENGINE AND PERFORMED OPERATIONAL CHECK
- [SDR C2XA09SH371](https://openairdocs.org/sdr/C2XA09SH371), Oct 21, 2009: SUPPORT BRACKET. CORRODED. SHV - DURING C-CHECK FWD AILERON QUADRANT TORQUE TUBE SUPPORT BRACKET HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 12A-13 AND BETWEEN STRINGERS 21R-20R. MAINTENANCE R
- [SDR C2XA09SH370](https://openairdocs.org/sdr/C2XA09SH370), Oct 21, 2009: SKIN. DENTED. SHV - DURING C-CHECK DENT BETWEEN FRAMES 25 AND 26 BETWEEN STRINGER 14R AND 15R. MAINTENANCE PERFORMED REPAIR OF DENT BETWEEN FRAMES 25 AND 26 BETWEEN STRINGERS
- [SDR C2XA09SH369](https://openairdocs.org/sdr/C2XA09SH369), Oct 21, 2009: RIVET. MISSING. SHV - DURING C-CHECK MISSING 7 RIVETS IN STRINGER 21L AT FRAME 15 (WHERE SHORING SUPPORT WAS PLACED). MAINTENANCE INSTALLED 7 RIVETS IN STRINGER 21L AT FRAME 15
- [SDR C2XA09SH368](https://openairdocs.org/sdr/C2XA09SH368), Oct 21, 2009: SUPPORT BRACKET. CORRODED. SHV - DURING C-CHECK SUPPORT BRACKET BETWEEN FRAMES 12-13, BETWEEN STRINGERS 21L-20L HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED SUPPORT BRA
- [SDR C2XA09SH367](https://openairdocs.org/sdr/C2XA09SH367), Oct 21, 2009: SUPPORT BRACKET. CORRODED. SHV - DURING C-CHECK SUPPORT BRACKET BETWEEN FRAME 12-13, BETWEEN STRINGER 21R-20R HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED SUPPORT BRACK
- [SDR C2XA09SH366](https://openairdocs.org/sdr/C2XA09SH366), Oct 21, 2009: FITTING. CORRODED. SHV - DURING C-CHECK SHEAR CLIP AT FRAME 11 BETWEEN STRINGERS 21L AND 21R HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF SHEAR CLIP AT FRAME 11 
- [SDR C2XA09SH365](https://openairdocs.org/sdr/C2XA09SH365), Oct 21, 2009: SKIN. CORRODED. SHV - DURING C-CHECK FUSELAGE SKIN INTERNAL PITTING CORROSION (LEVEL 2 LOCAL) AT FRAME 12 STRINGER 21R. MAINTENANCE PERFORMED REPAIR OF FUSELAGE SKIN AT FRAME 1
- [SDR C2XA09SH364](https://openairdocs.org/sdr/C2XA09SH364), Oct 21, 2009: SUPPORT BRACKET. CORRODED. SHV - DURING C-CHECK SUPPORT BRACKET BETWEEN FRAME 12-13, BETWEEN STRINGERS 21R-20R HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED SUPPORT BRAC
- [SDR C2XA09SH362](https://openairdocs.org/sdr/C2XA09SH362), Oct 21, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION (LEVEL 2 LOCAL) ON I/B SIDE FRAME 19-23. MAINTENANCE NEW REPAIR ON LT OMEGA BEAM AT FRAME 20 I/B SIDE IAW EMB-1
- [SDR C2XA09SH361](https://openairdocs.org/sdr/C2XA09SH361), Oct 21, 2009: DOUBLER. CORRODED. SHV - DURING C-CHECK RT OMEGA BEAM DOUBLER AT FRAME 22 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED RT OMEGA BEAM DOUBLER AT FRAME 22 IAW EMB
- [SDR C2XA09SH360](https://openairdocs.org/sdr/C2XA09SH360), Oct 21, 2009: SKIN. CRACKED. SHV - DURING C-CHECK RIVETS AT FRAME 79 STRINGER 4L TO 6L SHOW VISIBLE EVIDENCE OF CRACKS. MAINTENANCE PERFORMED CORRECTIVE ACTION REPAIR OF CRACKS ON FUSELAGE 
- [SDR C2XA09SH359](https://openairdocs.org/sdr/C2XA09SH359), Oct 21, 2009: SKIN. CRACKED. SHV - DURING C-CHECK RIVETS AT FRAME 78 STRINGER 4L TO 6L SHOW VISIBLE EVIDENCE OF CRACKS. MAINTENANCE PERFORMED CORRECTIVE ACTION REPAIR FOR CRACKS ON FUSELAGE
- [SDR C2XA09SH358](https://openairdocs.org/sdr/C2XA09SH358), Oct 21, 2009: SKIN. CRACKED. SHV - DURING C-CHECK RIVETS AT FRAME 79 STRINGER 4R SHOWS VISIBLE EVIDENCE OF CRACKS. MAINTENANCE PERFORMED CORRECTIVE ACTION REPAIR FOR CRACKS ON FUSELAGE SKIN
- [SDR C2XA09SH357](https://openairdocs.org/sdr/C2XA09SH357), Oct 21, 2009: SKIN. CRACKED. SHV - DURING C-CHECK RIVETS AT FRAME 78 STRINGER 6R SHOWS VISIBLE EVIDENCE OF CRACKS. MAINTENANCE PERFORMED CORRECTIVE ACTION REPAIR FOR CRACKS ON FUSELAGE SKIN

All 59: https://openairdocs.org/aircraft/N12122/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/N12122/stcs.md

## Earlier aircraft with N12122

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N12122 before.

- [Cancelled 1936-10-01](https://openairdocs.org/deregistered/N12122-1936-10-01): Stinson U, S/N 9010. Owner: [Tri American Aviation Inc](https://openairdocs.org/faa-owner/TRI%20AMERICAN%20AVIATION%20INC), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)

## 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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