# N12142: 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: 145735
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2005
- Certificate issued: January 30, 2019
- Expires: January 31, 2029
- Mode S code: A05A68
- 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=12142
- Page: https://openairdocs.org/aircraft/N12142

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/N12142/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 N12142.

## 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 20180807010359I](https://openairdocs.org/incident/20180807010359I), Aug 7, 2018: Embraer EMB-145XR (N12142), New York City, NY, No damage. At approximately 1430 local time on August 7, 2018 trans states airlines flight lof 4697 enroute from Washington dulles international airport, Washington, DC…
- [Incident 20100317029449I](https://openairdocs.org/incident/20100317029449I), Mar 17, 2010: Embraer EMB-145XR (N12142), Minneapolis, MN, Minor damage. Aircraft departed msp rnway 17 at 6:20AM. On climbout aircraft hit large birds and declared an emergency and returned to land on rnwy 30L. Leading edge of left…

## Service difficulty reports (91, 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 JJBA20261014002](https://openairdocs.org/sdr/JJBA20261014002), Oct 12, 2026: PLACARD. MISSING. RT EMERGENCY EXIT WINDOW INTERIOR PLACARD MISSING. INSTALLED RT EMERGENCY EXIT WINDOW INTERIOR PLACARD AS REQUIRED.
- [SDR JJBA20260805002](https://openairdocs.org/sdr/JJBA20260805002), Aug 4, 2026: INVERTER. INOPERATIVE. NR 2 EMERGENCY LIGHT BATTERY LOWER INVERTER INOPERATIVE. REMOVED AND REPLACED LOWER INVERTER AT NR 2 EMERGENCY LIGHT BATTERY. OPS CHKD GOOD.
- [SDR JJBA20260423017](https://openairdocs.org/sdr/JJBA20260423017), Apr 22, 2026: BATTERY PACK. MISINSTALLED. SEVERAL EMERGENCY LIGHTS INOPERATIVE. FOUND #3 BPS NOT INSTALLED CORRECTLY. REINSTALLED. OPS CHECK GOOD.
- [SDR JJBA20250623016](https://openairdocs.org/sdr/JJBA20250623016), Jun 17, 2025: LAMP. INOPERATIVE. MCD EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MCD EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK FAILED. SUSPECT BAD HOUSING. REMOVED AND REPLACED LI
- [SDR JJBA20250623015](https://openairdocs.org/sdr/JJBA20250623015), Jun 17, 2025: SIGN. INOPERATIVE. EXIT LOCATING SIGN MID CEILING FWD INOPERATIVE. REMOVED AND REPLACED EXIT LOCATING SIGN FWD SIDE MID CEILING. OPS CHECK SAT.
- [SDR JJBA20250417059](https://openairdocs.org/sdr/JJBA20250417059), Apr 15, 2025: LAMP. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. FOUND LIGHT COVER BROKEN WHEN CHANGING BULB ON LIGHT. REMOVED AND REPLACED BULB AND LIGHT COVER ON SERVICE DOOR EMERGE
- [SDR JJBA20250401039](https://openairdocs.org/sdr/JJBA20250401039), Mar 30, 2025: LAMP. INOPERATIVE. LH AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH AFT EXTERIOR EMERGENCY LIGHT. OPS CHECK SAT.
- [SDR JJBA20250303008](https://openairdocs.org/sdr/JJBA20250303008), Mar 1, 2025: LAMP. INOPERATIVE. LH LOWER EXT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH LOWER EXT EMERGENCY LIGHT. OPS CHECK SAT.
- [SDR JJBA20241118005](https://openairdocs.org/sdr/JJBA20241118005), Nov 15, 2024: BATTERY PACK. INOPERATIVE. SEVERAL EMERGENCY LIGHTS OUT. REMOVED AND REPLACED EMERGENCY BATTERY #2. OPS CHECK SAT.
- [SDR JJBA20240528059](https://openairdocs.org/sdr/JJBA20240528059), May 25, 2024: DUCT. UNSECURE. SMELL OF SMOKE (BURNING RUBBER) ON CLIMB OUT WITH EXCESSIVE AMOUNTS OF CONDENSATION FROM #1 PACK. FOUND BOTH NACA RAM AIR INLET DUCTS (191GL), NOT SECURED; RH P
- [SDR JJBA20240523058](https://openairdocs.org/sdr/JJBA20240523058), May 17, 2024: FLOOR SUPPORT. CORRODED. CENTER FUSELAGE 1 - RH OMEGA BEAM UPPER SURFACE - BETWEEN FR18 - FR19 - CORROSION. PROCEEDED TO FABRICATE DOUBLE AND INSTALLED DOUBLER.
- [SDR JJBA20230530020](https://openairdocs.org/sdr/JJBA20230530020), May 27, 2023: SENSOR. INOPERATIVE. FLAP FAILURE ON APPROACH, FLAP STOPPED AT 38 DEGREES. RESET FLAPS. EICAS MESSAGE CLEARED AND FLAPS OPS CHECKED NORMAL. PERFORMED GVI OF FFL. LH FLAP VELOCITY SE
- [SDR JJBA20230320026](https://openairdocs.org/sdr/JJBA20230320026), Mar 17, 2023: LAMP. INOPERATIVE. MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB ON MCD EMERGENCY LIGHT. OPS CHECK FAIL. LIGHT ASESEMBLY FOUND TO BE INOPERATIVE. REMOVED 
- [SDR JJBA20230320025](https://openairdocs.org/sdr/JJBA20230320025), Mar 17, 2023: BATTERY PACK. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS INOPERATIVE. DETERMINED FAULT TO BE BAD BATT 1 AND 4. REMOVED AND REPLACED BOTH BATTERIES. OPS CHECK SAT BATTERY PACK #4 PN: ABS-2013-
- [SDR JJBA20220921026](https://openairdocs.org/sdr/JJBA20220921026), Sep 18, 2022: NONE. FAILED. SUPPLEMENTAL (NEW) INFORMATION: REMOVED AND REPLACED NOSE LANDING GEAR. OPS AND LEAK CHECK SAT.
- [SDR JJBA20220502012](https://openairdocs.org/sdr/JJBA20220502012), May 2, 2022: NONE. NONE. REAR FUSELAGE SKIN HAS CORROSION UNDER #2 RAT ANTENNA ON EXTERNAL AND INTERNAL SURFACES. REPAIRED REAR FUSELAGE SKIN UNDER #2 RAT ANTENNA.
- [SDR JJBA20220420009](https://openairdocs.org/sdr/JJBA20220420009), Apr 20, 2022: NONE. NONE. REAR FUSELAGE SKIN HAS CORROSION UNDER #2 RAR ANTENNA ON EXTERNAL AND INTERNAL SURFACES. REPAIRED REAR FUSELAGE SKIN UNDER #2 RAR ANTENNA.
- [SDR JJBA20220412008](https://openairdocs.org/sdr/JJBA20220412008), Apr 12, 2022: NONE. NONE. LH OMEGA BEAM AT FR 38 - FR 44 HAS CORROSION AROUND SURFACE OF FASTENER HOLES. REMOVED AND REPLACED LH OMEGA BEAM.
- [SDR JJBA20220325011](https://openairdocs.org/sdr/JJBA20220325011), Mar 25, 2022: NONE. NONE. CORROSION FOUND ON THE OMEGA BEAM LOCATED BETWEEN FR59 TO FR 61, Y.00-19. REPAIRED OMEGA BEAM AT FR 59 - FR61 AND Y.00-16
- [SDR JJBA20220325010](https://openairdocs.org/sdr/JJBA20220325010), Mar 25, 2022: NONE. NONE. CORROSION FOUND ON THE OMEGA BEAM LOCATED BETWEEN FR59 TO FR 61. REPAIRED OMEGA BEAM AT FR 59 - FR61 AND Y.00+16
- [SDR JJBA20211024054](https://openairdocs.org/sdr/JJBA20211024054), Oct 24, 2021: INVERTER. FAULTY. EXIT MARKING ASSEMBLY FORWARD OF SEAT 3C INOPERATIVE. SWAPPED EXIT MARKING WITH EXIT SIGN ABOVE FA SEAT. FAULT DID NOT FOLLOW. SWAPPED EMERGENCY LIGHT DC/AC INV
- [SDR JJBA20210920031](https://openairdocs.org/sdr/JJBA20210920031), Sep 20, 2021: BATTERY. INOPERATIVE. RH FWD EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PLACARD ASSEMBLY. OPS CHECK BAD. R&R CHASSIS ASSEMBLY AND BATTERY PACK. OPS CHECK SAT
- [SDR JJBA20210316012](https://openairdocs.org/sdr/JJBA20210316012), Mar 12, 2021: LIGHT. INOPERATIVE. RH FWD WING TO FUSELAGE EMERGENCY LIGHT INOPERATIVE. R&R RH FWD WING TO FUSELAGE EMERGENCY LIGHT. OPS CHECK SAT.
- [SDR JJBA20211110012](https://openairdocs.org/sdr/JJBA20211110012), Jan 11, 2021: SEAT. CRACKED. SEATS 2A, 3A, 4A, 8A, 9A, 11A, 19A, 22A, AND 23A ALL HAVE A CRACK IN THE RADIUS OF THE BASE ASSEMBLY BELOW THE AISLE SIDE ARM REST. REPLACED SEATS 2A, 3A, 4A, 8
- [SDR JJBA20201229034](https://openairdocs.org/sdr/JJBA20201229034), Dec 29, 2020: SKIN. DENTED. SUSPECTED DENT FOUND ON CENTER FUSE II, BETWEEN FR 27-28 AND BETWEEN STR 1L-2L. DENT ON CENTER FUSE II, BETWEEN FR 27-28 AND BETWEEN STR 1L-2L REPAIRED.
- [SDR JJBA20201216033](https://openairdocs.org/sdr/JJBA20201216033), Dec 16, 2020: SKIN. DENTED. DENT ON LT FWD FUSE II, BETWEEN CUT OUT EXTERNAL POWER RECEPTACLE AND STR 15L. PAINT REMOVED AT DENTED AREA. AFTER INVESTIGATION, A CHAFING IS FOUND ON LT FWD F
- [SDR ASOA202009124023S](https://openairdocs.org/sdr/ASOA202009124023S), Sep 12, 2020: LIGHT. INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY FOR SEATS 19A-21A. OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO
- [SDR ASOA2020091424023](https://openairdocs.org/sdr/ASOA2020091424023), Sep 12, 2020: SOCKET. BURNED. BHM-FLIGHT 4369, THE CREW REPORTED SMELL OF SMOKE AND VISIBLE SMOKE ON SIDEWALL LIGHT PANEL 20A WITH A VISIBLE BURN MARK. THE AIRCRAFT LANDED IN BHM WITHOUT INC
- [SDR RAIA2020031100001](https://openairdocs.org/sdr/RAIA2020031100001), Feb 28, 2020: SUPPORT. CORRODED. DISCOVERED SURFACE CORROSION ON FUSELAGE SERVICE DOOR CUTOUT THRESHOLD SUPPORT STRUCTURE AROUND FLOOR TRIM NUTPLATE LOCATIONS----REMOVED AND REPLACED ITEM WITH 
- [SDR RAIA2020031080002](https://openairdocs.org/sdr/RAIA2020031080002), Feb 28, 2020: SHEAR TIE. CRACKED. SHEAR CLIP FRAME AT STR 18L-19L IS CRACKED ......REMOVED AND REPLACED SHEAR CLIP AT STR 18L=19L
- [SDR RAIA2020031080001](https://openairdocs.org/sdr/RAIA2020031080001), Feb 28, 2020: ANGLE. CORRODED. CARGO Z ANGLE IS CORRODED..........REMOVED AND REPLACED CARGO Z ANGLE
- [SDR RAIA2019121760001](https://openairdocs.org/sdr/RAIA2019121760001), Dec 16, 2019: UNKNOWN. ODOR. ELECTRICAL SMELL IN COCKPIT.CREW REPRTS A FAINT ELECTRICAL SMELL AND SMOKE VENTING INTO COCKPIT THROUGH CAPTS FWD WINDSHIELD SEAL ON THE LH SIDE.SMELL AND SMOKE
- [SDR RAIA201907270002](https://openairdocs.org/sdr/RAIA201907270002), Jul 27, 2019: THERMOSTAT. MALFUNCTIONED. BLEED 1 & 2 OVERTEMP DURING CLIMBOUT IN ICING( EMER DECLARED). R&R #2 FAN AIR VALVE HIGH TEMP THERMOSTAT AND #2 LOW TEMP THERMOSTAT INLET HOSE, ALL OPS CHECK GO
- [SDR RAIA2019032200001](https://openairdocs.org/sdr/RAIA2019032200001), Mar 22, 2019: BUTTON. DEFECTIVE. RUDDER SYSTEM 1-2 INOP MESSAGE AFTER YAW DAMPER FAIL MESSAGE. WENT AWAY, CAME BACK THEN WENT AWAY. SYS 1 PRESSURE 3100. SYSTEM 2 3000. REFER TO DISCREPANCY 1, L
- [SDR RAIA201812120001](https://openairdocs.org/sdr/RAIA201812120001), Dec 12, 2018: CONNECTOR. BURNED. LAV SMOKE EICAS ON TAKE OFF. FOUND CONNECTOR P8100 BURNT. R&R PLUG. OPS CHECK GOOD.
- [SDR RAIA2018090670001](https://openairdocs.org/sdr/RAIA2018090670001), Aug 7, 2018: CARBON SEAL. LEAKING. AT 290 SMOKE IN CABIN AND FLT DECK. NOTE FILLED FROM AFT TO FORWARD. UPON INSPECTION FOUND 0 CARBON SEAL LEAKING AND SHAFT SEAL SPINNER LOOSE. REFERENCE STANDAR
- [SDR RAIA201801120001](https://openairdocs.org/sdr/RAIA201801120001), Jan 12, 2018: SENSOR. DIRTY. NR 1 AND 2 BLEED OVERTEMP. CLEANED THE TEMP SENSORS AND PERFORMED AN OPS CHECKED GOOD.
- [SDR RAIA201709010002](https://openairdocs.org/sdr/RAIA201709010002), Sep 1, 2017: BULB. INOPERATIVE. CEILING AISLE FLOOD LIGHT AT ROW 12 INOPERATIVE. R & R THE BULBS, OPS CHECKED GOOD.
- [SDR RAIA201703120001](https://openairdocs.org/sdr/RAIA201703120001), Mar 12, 2017: FCU. INOPERATIVE. FLAP FAIL MESSAGE INFLIGHT. R & R THE FECU, OPS CHECKED GOOD. ACFT FOR SERVICE.
- [SDR RAIA201612090001](https://openairdocs.org/sdr/RAIA201612090001), Dec 9, 2016: POWER SUPPLY. INOPERATIVE. LEFT EXTERIOR FWD EMERGENCY LIGHT INOPERATIVE. R & R THE NR 1 BATTERY POWER SUPPLY, OPS CHECKED GOOD.
- [SDR ASOA20160329012](https://openairdocs.org/sdr/ASOA20160329012), Mar 28, 2016: SKIN. DAMAGED. LIGHTNING STRIKE AT FRAME 29 BETWEEN STR 15L AND 16L. CUTOUT DAMAGED AREA, FABRICATED DOUBLER AND FILLER. INSTALLED IAW SRM 53-22-01. ACFT RELEASED AND RETURNED
- [SDR ASOA20160301016H](https://openairdocs.org/sdr/ASOA20160301016H), Mar 1, 2016: POWER SUPPLY. INOPERATIVE. THE LT FWD EMERGENCY LIGHT ON PANEL 191 WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 1 EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFEC
- [SDR ASOA20160105001](https://openairdocs.org/sdr/ASOA20160105001), Jan 5, 2016: TANK. CHAFED. ACFT IS IN FOR A C-CHECK INSPECTION. INSPECTION FOUND THE VENTRAL TANK CHAFE AT A PREVIOUS LOWER SKIN PATCH BETWEEN TANK DRAINS. THE OLD DOUBLER HAS BEEN REMOVE
- [SDR ASOA20141021119](https://openairdocs.org/sdr/ASOA20141021119), Oct 21, 2014: WIRE HARNESS. ODOR. CREW REPORTED A BURNING ODOR NEAR SEAT 4A DURING TAKEOFF AND LANDING. MAINTENANCE R & R THE CABIN LIGHT WIRE HARNESS WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR 
- [SDR ASOA20140922106](https://openairdocs.org/sdr/ASOA20140922106), Sep 22, 2014: CHARGER. INOPERATIVE. DURING MX INSPECTION, THE FWD LT SIDE EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R THE NR 1 EMERGENCY LIGHT SYS BATTERY CHARGER ASSY WITH OPS CHECKE
- [SDR ASOA201400710213](https://openairdocs.org/sdr/ASOA201400710213), Jul 10, 2014: INVERTER. INOPERATIVE. DURING RON ROUTINE MAINTENANCE, SEVERAL EMERGENCY LIGHTS IN THE COCKPIT AND FORWARD CABIN WERE FOUND INOPERATIVE DURING FUNCTIONAL TEST. MAINTENANCE R & R THE N
- [SDR ASOA20131123445](https://openairdocs.org/sdr/ASOA20131123445), Nov 23, 2013: FLOOR SUPPORT. CRACKED. RT OMEGA BEAM OTBD CRACKED AT FRAME 47. R & R OMEGA BEAM.
- [SDR ASOA20131123444](https://openairdocs.org/sdr/ASOA20131123444), Nov 23, 2013: FLOOR SUPPORT. CRACKED. RT OMEGA BEAM, INBD, AT FRAME 47 CRACKED. R & R OMEGA BEAM.
- [SDR ASOA20131123443](https://openairdocs.org/sdr/ASOA20131123443), Nov 23, 2013: FRAME. CRACKED. WHILE INSTALLING SHEAR TIE FOUND CRACK IN FRAME 25 BETWEEN STRINGER 15 & 16R. TRIMMED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER/FILLER IAW ETD2013-145-0594
- [SDR ASOA20131123442](https://openairdocs.org/sdr/ASOA20131123442), Nov 23, 2013: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AT FRAME 25 BETWEEN STRINGER 15 & 16R. R & R SHEAR TIE

All 91: https://openairdocs.org/aircraft/N12142/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/N12142/stcs.md

## Earlier aircraft with N12142

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N12142 before.

- [Cancelled 1932-09-13](https://openairdocs.org/deregistered/N12142-1932-09-13): Stinson JR. S, S/N 8103, built 1931. Owner: [Hilliker Harry S](https://openairdocs.org/faa-owner/HILLIKER%20HARRY%20S), [Buffalo, NY](https://openairdocs.org/faa-place/NY/Buffalo)

## 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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