# N13124: 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: 145689
- 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: A081A3
- 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=13124
- Page: https://openairdocs.org/aircraft/N13124

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/N13124/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 N13124.

## 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 20121223028309I](https://openairdocs.org/incident/20121223028309I), Dec 23, 2012: Embraer EMB-145XR (N13124), Omaha, NE, No damage. Aircraft experienced pressurization problem and returned to airport. Manual pressurization inop.
- [Incident 20040224007899I](https://openairdocs.org/incident/20040224007899I), Feb 24, 2004: Emb EMB145XR (N13124), Buffalo, NY. (-23) On February 24, 2004, at 1035 pm EDT, an Embraer 145XR, N13124, flight 3359, operated by Continental airlines express diverted and landed on runway 5 at…

## Service difficulty reports (106, 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 JJBA20260220057](https://openairdocs.org/sdr/JJBA20260220057), Feb 18, 2026: WIRE. BROKEN. MCD EXTERNAL EMERG LIGHT INOPERATIVE. FOUND BROKEN WIRE BEFORE SPLICE SP7426 REPAIRED WIRE. R/R MCD EXT EMER LIGHT ASSY OPS CHECK SAT.
- [SDR JJBA20260115025](https://openairdocs.org/sdr/JJBA20260115025), Jan 12, 2026: ENGINE. FAILED. ON CLIMBOUT HEARD A BIG BANG FROM NR 1 ENGINE AND NR 1 ENGINE SHUTDOWN. ALL INDICATORS WERE IN THE NORMAL ON TAKE OFF. DID ATTEMPT ANOTHER ENGINE RESTART IN FLI
- [SDR JJBA20250707001](https://openairdocs.org/sdr/JJBA20250707001), Jul 4, 2025: LAMP. INOPERATIVE. MCD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MCD EMERGENCY LIGHT LAMP. OPS CHECK SAT.
- [SDR JJBA20250127021](https://openairdocs.org/sdr/JJBA20250127021), Jan 24, 2025: LAMP. INOPERATIVE. RH OVERWING EMERGENCY LIGHT OUT. REMOVED AND REPLACED BULB. OPS CHECK SAT.
- [SDR JJBA20230317024](https://openairdocs.org/sdr/JJBA20230317024), Mar 14, 2023: UNKNOWN. UNKNOWN. RH WING BOTTOM LATERAL FAIRING ANGLE BRACKETS CRACKED AT FR46, FR48, FR48.5, FR50 (BOTH BRACKETS). COMPLETED THE REPAIR OF THE RH WING BOTTOM LATERAL FAIRING AN
- [SDR JJBA20230313017](https://openairdocs.org/sdr/JJBA20230313017), Mar 9, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR BRACKET AT FS 21 AT SERVICE DOOR. REMOVED AND REPLACED FLOOR BRACKET AT FS 21 AT SERVICE DOOR.
- [SDR JJBA20220919022](https://openairdocs.org/sdr/JJBA20220919022), Sep 16, 2022: LAMP. INOPERATIVE. SEAT 18C&D OVER WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SEAT 18CD OVER WING EMERGENCY LIGHT LAMP. OPS CHECK GOOD
- [SDR JJBA20220808001](https://openairdocs.org/sdr/JJBA20220808001), Aug 3, 2022: BATTERY PACK. INOPERATIVE. RH EMERGENCY EXIT LOWER LIGHT INOPERATIVE. REMOVED AND REPLACED RH EMERGENCY EXIT LOWER LIGHT. OPS CHECK FAILED. REMOVED AND REPLACED EMERGENCY BATTERY #3. OPS 
- [SDR JJBA20220410013](https://openairdocs.org/sdr/JJBA20220410013), Apr 10, 2022: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT NEAR MAIN DOOR INOPERATIVE. REMOVED AND REPLACED #1 EMERGENCY BATTERY. OPS CHECK SAT AT THIS TIME
- [SDR JJBA202201186020](https://openairdocs.org/sdr/JJBA202201186020), Jan 16, 2022: B-NUT. LOOSE. HYD SYS 1 FAIL ON EICAS. LH NLG DOOR ACTUATOR HOSE B NUT LOOSE AND LEAKING - RESECURED. REPLENISHED #1 HYD SYSTEM. LEAK AND OPS CHECK SAT.
- [SDR JJBA20211004003](https://openairdocs.org/sdr/JJBA20211004003), Oct 4, 2021: NONE. NONE. SUPPLEMENTAL INFORMATION: IN PREPARATION FOR OCF, PILOT FELT RATCHETING IN AILERON CONTROL. FLIGHT NEVER OCCURRED. DURING TROUBLESHOOTING, MECHANIC CYCLED THE S
- [SDR JJBA20210922016](https://openairdocs.org/sdr/JJBA20210922016), Sep 22, 2021: NONE. NONE. CENTER FUSE IV, UNDER FLOOR, FRAME 59 CORRODED BTW STR 21R-21L. FR 59 SEGMENT BTW STR 20R-20L CUT OUT SPLICE REPAIR. FR 59 SEGMENT BTW STR 20R-20L. 2 SPLICE REP
- [SDR JJBA20210922034](https://openairdocs.org/sdr/JJBA20210922034), Sep 22, 2021: NONE. NONE. CORROSION FOUND ON CENTER AISLE LH OMEGA BEAM LOCATED BETWEEN FR 23- FR 29. REMOVED AND REPLACED LH OMEGA BEAM, LOCATED BETWEEN FR 23-FR29
- [SDR JJBA2021092200021](https://openairdocs.org/sdr/JJBA2021092200021), Sep 22, 2021: NONE. NONE. THE PASSENGER FWD CABIN LH FLOOR OMEGA DOUBLER HAS CORROSION ON THE FWD SURFACE BETWEEN FR 14 TO FR 18. REMOVED AND REPLACED DIGITAL PLATE ON PASSENGER FWD CABI
- [SDR JJBA20210922020](https://openairdocs.org/sdr/JJBA20210922020), Sep 22, 2021: NONE. NONE. CORROSION AT MULTIPLE LOCATONS FOUND ON RH CENTER AISLE LONGITUDINAL BEAM LOCATED BETWEEN FR29-FR36 Y.00+8. REMOVED AND REPLACED BEAM ASSEMBLY ON RH CENTER AISL
- [SDR JJBA20210922019](https://openairdocs.org/sdr/JJBA20210922019), Sep 22, 2021: NONE. NONE. CORROSION NOTED AT ELT ANTENNA MOUNTING SURFACE. EVALUATED CORROSION AT ELT ANTENNA DOUBLER AND FOUND OUT OF LIMITS. REMOVED AND REPLACED ELT ANTENNA DOUBLER.
- [SDR JJBA20210922018](https://openairdocs.org/sdr/JJBA20210922018), Sep 22, 2021: NONE. NONE. AFTER REMOVAL OF UPPER TCAS ANTENNA, INSPECTED AIRCRAFT SKIN FOUND SEVERAL SCRATCHES AT MATING SURFACE. REMOVED SCRATCHES ON UPPER TCAS ATTENNA DOUBLER BY BLEND
- [SDR JJBA20210922017](https://openairdocs.org/sdr/JJBA20210922017), Sep 22, 2021: NONE. NONE. CARGO DOOR INTERNAL STRUCTURE LOWER WEB HAS MULTIPLE AREAS OF SCREW INDENTION DAMAGE. REMOVED AND REPLACED AFT CARGO DOOR INNER SKIN WEB.
- [SDR JJBA20210922015](https://openairdocs.org/sdr/JJBA20210922015), Sep 22, 2021: NONE. NONE. MAIN CABIN - RH O/B FLOOR BOARD SUPPORT STRUCTURE HAS CORROSION MULTIPLE LOCATIONS BETWEEN FR 40 TO FR 41 RH. REMOVED AND REPLACED SILL IN MAIN CABIN - RH OB FL
- [SDR JJBA20210922014](https://openairdocs.org/sdr/JJBA20210922014), Sep 22, 2021: NONE. NONE. AFT CARGO COMPARTMENT AT DOOR CUT-OUT LOWER FRAME HAS 3 SCREW HOLES SHOWING SIGNS OF CORROSION BETWEEN FRAME 65 - 68. REMOVED AND REPLACED AFT CARGO COMPARTMENT
- [SDR JJBA20210922013](https://openairdocs.org/sdr/JJBA20210922013), Sep 22, 2021: NONE. NONE. THE PASSENGER ENTRY DOOR WAY FWD FRAME LOWER SPLICE TO FLOOR BEAM IS CRACKED. REMOVED AND REPLACED LOWER REINFORCEMENT SPLICE TO FLOOR BEAM PASSENGER ENTRY DOOR
- [SDR JJBA202109083012](https://openairdocs.org/sdr/JJBA202109083012), Sep 3, 2021: FLOOR SUPPORT. CORRODED. THE PASSENGER CABIN RH SIDE OMEGA FLOOR BEAM DOUBLER HAS CORROSION JUST FWD OF FR19 UPPER SURFACE. BLENDED CORROSION ON RH OMEGA BEAM JUST FORWARD OF FRAME 19. 
- [SDR JJBA20210822011](https://openairdocs.org/sdr/JJBA20210822011), Aug 22, 2021: FRAME. CRACKED. DIRECTLY UNDER CAPTAINS DV WINDOW CUTOUT FRAME 10 CRACKED. REMOVED CHANNEL UNDER CAPTAINS DV WINDOW CUTOUT AT FR10. LOCATED AND DRILLED NEW CHANNEL UNDER CAPTAI
- [SDR JJBA20210822010](https://openairdocs.org/sdr/JJBA20210822010), Aug 22, 2021: SUPPORT. CORRODED. CARGO DOOR CUTOUT INTERNAL SUPPORT STRUCTURE CORRODED AT FWD LOWER EDGE. REMOVED LOWER PART OF SHEAR CLIP. LOCTED AND DRILLED NEW LOWER END OF SHEAR CLIP. INSTA
- [SDR JJBA20210822009](https://openairdocs.org/sdr/JJBA20210822009), Aug 22, 2021: SUPPORT BEAM. CRACKED. PASSENGER DOOR UPPER AFT REINFORCING SUPPORT BEAM CRACKED AT FR19 AND STGR 3L. REMOVED BEAM AT FR19, LEFT STRINGER 3. LOCATED, DRILLED, DEBURRED NEW SUPPORT BEA
- [SDR JJBA20210822008](https://openairdocs.org/sdr/JJBA20210822008), Aug 22, 2021: DOUBLER. DAMAGED. LH - FR 14 BETWEEN STGR LH7 AND STGR LH8 - LH BULKHEAD - SUPPORT DOUBLER - HOLE ELONGATED. REMOVED EXISTING DOUBLER. FABRICATED REPAIR DOUBLER. CLEANED, TREATED
- [SDR JJBA2021090822007](https://openairdocs.org/sdr/JJBA2021090822007), Aug 22, 2021: SKIN. CRACKED. EXTERNAL SKIN CRACKED AT FO'S DV WINDOW CUTOUT AFT UPPER CORNER. CUTOUT DAMAGED AREA AND REMOVED ALL EXISTING FASTENERS IN REPAIR AREA. TREATED AND PRIMED FUSEL
- [SDR JJBA2021090822006](https://openairdocs.org/sdr/JJBA2021090822006), Aug 22, 2021: FRAME. CRACKED. DIRECTLY UNDER FO'S DV WINDOW CUTOUT FRAME 10 CRACKED. REMOVED CHANNEL UNDER FO'S DV WINDOW CUTOUT AT FR10. LOCATED AND DRILLED NEW CHANNEL UNDER FO'S DV WINDOW
- [SDR JJBA2021090885005](https://openairdocs.org/sdr/JJBA2021090885005), Aug 5, 2021: ATTACH FITTING. CORRODED. LEFT WING AILERON ATTACHMENT LUGS "4" EACH HAVE LIGHT SURFACE CORROSION EXPOSED AND BARE METAL. BLENDED CORROSION 4 EACH LUGS.
- [SDR JJBA20210729004](https://openairdocs.org/sdr/JJBA20210729004), Jul 29, 2021: ATTACH FITTING. CORRODED. RIGHT WING AILERON ATTACHMENT LUGS "4" EACH HAVE LIGHT SURFACE CORROSION EXPOSED AND BARE METAL. BLENDED CORROSION 4 EACH AREAS ON RIGHT AILERON LUGS UPPER SURF
- [SDR JJBA20210303001](https://openairdocs.org/sdr/JJBA20210303001), Mar 3, 2021: CONTROLLER. INOPERATIVE. AUTOPILOT AND YAW DAMP WOULD NOT ENGAGE AFTER TAKE OFF, NO VERTICAL MODE AVAILABLE. NO LATERAL MODE AVAILABLE. PERFORMED AP FUNCTIONAL CHECK. OPS CHECK SAT. NO 
- [SDR JJBA20201230032](https://openairdocs.org/sdr/JJBA20201230032), Dec 30, 2020: SWITCH. FAILED. PITCH TRIM MAIN INOPERATIVE IN FLIGHT. REMOVED AND REPLACED FO YOKE PITCH TRIM SWITCH. OPERATIONS CHECK GOOD.
- [SDR JJBA20201124022](https://openairdocs.org/sdr/JJBA20201124022), Nov 24, 2020: SKIN. CRACKED. CRACK ON REAR FUSE 1 LOWER SKIN, AT DRAIN MAST BETWEEN FR 75 JUNCTION 07 AND BETWEEN STR 21L-21R. REAR FUSELAGE 1 BETWEEN FR 75 & JUNCTION 07 BETWEEN STR 21L &2
- [SDR JJBA20201124021](https://openairdocs.org/sdr/JJBA20201124021), Nov 24, 2020: SHEAR TIE. CRACKED. REAR FUSELAGE 1, FRAME 75A LOWER LEG CRACKED. REAR FUSELAGE 1 FRAME 75A LOWER SECTION LOWER LEG REPAIRED.
- [SDR JJBA20201121020](https://openairdocs.org/sdr/JJBA20201121020), Nov 21, 2020: SKIN. DENTED. DENT ON LT CENTER FUSE 1, BETWEEN FR 20-21 AND BETWEEN STR 13L-14L. LT CENTER FUSE 1, BETWEEN FR 20-21 AND BETWEEN STR 13L-14L, SKIN REPAIRED.
- [SDR JJBA20201116019](https://openairdocs.org/sdr/JJBA20201116019), Nov 16, 2020: SKIN. DEFORMED. FWD FUSELAGE LT SIDE, THE SKIN IS DEFORMED AROUND THE TAT PROBE. ON FWD FUSELAGE LT SIDE SKIN, AROUND TAT PROBE, PAINT STRIPPED FOR INVESTIGATION. TAT PROBE INN
- [SDR RAIA201903220003](https://openairdocs.org/sdr/RAIA201903220003), Mar 22, 2019: SHEAR TIE. CRACKED. RT AT FLOOR LEVEL SHEAR CLIP AT FRAME 25 IS CRACKED. REMOVED AND REPLACED SHEAR CLIP AT FRAME 25 RT.
- [SDR RAIA201903180002](https://openairdocs.org/sdr/RAIA201903180002), Mar 18, 2019: GUSSET. CORRODED. LAV RT GUSSET HAS CORROSION. REMOVED AND REPLACED LAV RT GUSSETT.
- [SDR RAIA201903180001](https://openairdocs.org/sdr/RAIA201903180001), Mar 18, 2019: DOOR SILL. CORRODED. LAV RT FLOOR SILL HAS CORROSION AT FR 59. REMOVED AND REPLACED RT LAV FLOOR SILL.
- [SDR RAIA201903160004](https://openairdocs.org/sdr/RAIA201903160004), Mar 16, 2019: SHEAR TIE. CRACKED. SHEAR CLIP AT FRAME 15 AND STR 15R IS CRACKED. REMOVED AND REPLACED SHEER CLIP AT FRAME 15 AND STR 15R.
- [SDR RAIA201903160002](https://openairdocs.org/sdr/RAIA201903160002), Mar 16, 2019: ANGLE. CORRODED. CARGO DOOR LOWER THRESHOLD Z ANGLE IS CORRODED. REMOVED AND REPLACED CARGO DOOR THRESHOLD Z ANGLE.
- [SDR RAIA201903160001](https://openairdocs.org/sdr/RAIA201903160001), Mar 16, 2019: DOOR SILL. CORRODED. SERVICE DOOR SILL AT FRAME 19-21 IS CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL AT FRAME 19-21.
- [SDR RAIA201902020001](https://openairdocs.org/sdr/RAIA201902020001), Feb 2, 2019: PROXIMITY SWITCH. DIRTY. LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. CLEANED DIRT AND DEBRIS OFF ALL PROX SWITCHES. OPS CHECK GOOD AT THIS TIME.
- [SDR RAIA201810040003](https://openairdocs.org/sdr/RAIA201810040003), Oct 4, 2018: INDICATION SYS. MALFUNCTIONED. TOTAL FUEL QUANTITY SHOWES AMBER DASHES INTERMITTENTLY THROUGHOUT FLT. RESET FUEL SYSTEM IAW 28-41-00. SYSTEM CHECK GOOD.
- [SDR RAIA201806090001](https://openairdocs.org/sdr/RAIA201806090001), Jun 9, 2018: O-RING. DAMAGED. BLEED 1 LEAK AFTER TAKE OFF. REMOVED AND REPLACED JOINT 28 O-RINGS. PERFORMED LEAK CHECK OF BLEED SYSTEM. OPS CHECK/LEAK CHECK GOOD AT THIS TIME.
- [SDR RAIA201801050001](https://openairdocs.org/sdr/RAIA201801050001), Jan 5, 2018: DUCT. DISCONNECTED. NR 2 PACK VALVE CLOSED MESSAGE. TROUBLESHOT AND FOUND THE DUCT DISCONNECTED ON THE NR 2 PACK VALVE. SECURED THE DUCT AND OPS CHECKED GOOD.
- [SDR RAIA201707290002](https://openairdocs.org/sdr/RAIA201707290002), Jul 29, 2017: FLAP TRACK. CRACKED. FLAP OVERSPEED 290 KNOTS AT FLAPS 9. PERFORMED MAX FLAP EXTENDED SPEED INSPECTION, FAILED NDI TESTING ON LEFT WING O/B FLAP INBD TRACK AND RIGHT WING O/B FLAP I
- [SDR RAIA201701170001](https://openairdocs.org/sdr/RAIA201701170001), Jan 17, 2017: TRANSDUCER. INOPERATIVE. NR 2 ENGINE ANTI ICE EICAS CAME ON. RAN CHECK LIST TEST AND VALVE NEVER OPENED AFTER MULTIPLE ATTEMPTS. R & R THE NR 2 ENG ANTI ICE PRESSURE TRANSDUCER. OPS CHE
- [SDR RAIA201611280001](https://openairdocs.org/sdr/RAIA201611280001), Nov 28, 2016: ANTI-ICE VALVE. INOPERATIVE. NR 1 AND 2 ENGINE ANTI ICE FAILED MESSAGE WHEN BOTH ANTI ICE VALVES HAVE BEEN DEFERRED. R & R THE ANTI ICE VALVE IAW AMM 30-21-01, OPS CHECKED GOOD.
- [SDR RAIA201601280001](https://openairdocs.org/sdr/RAIA201601280001), Jan 28, 2016: BULB. INOPERATIVE. RIGHT WING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. RELAMPED RT EXTERIOR EMERGENCY LIGHT. OPS CHECK GOOD.

All 106: https://openairdocs.org/aircraft/N13124/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/N13124/stcs.md

## Earlier aircraft with N13124

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N13124 before.

- [Cancelled 1999-11-15](https://openairdocs.org/deregistered/N13124-1999-11-15): Cessna 172M, S/N 17262514. Exported to Germany. Owner: [Gauvin Jeff M](https://openairdocs.org/faa-owner/GAUVIN%20JEFF%20M), [Detroit, MI](https://openairdocs.org/faa-place/MI/Detroit)
- [Cancelled 1934-08-31](https://openairdocs.org/deregistered/N13124-1934-08-31): Levene Ben E-403 GLIDER, S/N 5, built 1932. Owner: [Levene Ben](https://openairdocs.org/faa-owner/LEVENE%20BEN), [Philadelphia, PA](https://openairdocs.org/faa-place/PA/Philadelphia)

## 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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