# N23139: 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: 145731
- 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: A20F1A
- 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=23139
- Page: https://openairdocs.org/aircraft/N23139

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/N23139/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 N23139.

## FAA accident and incident reports

None matched to N23139.

## Service difficulty reports (81, 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 JJBA20260810004](https://openairdocs.org/sdr/JJBA20260810004), Aug 7, 2026: LAMP. INOPERATIVE. AFT LAST ROW CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAST ROW EMERGENCY LAMP. OPS CHECKED SAT.
- [SDR JJBA20260720010](https://openairdocs.org/sdr/JJBA20260720010), Jul 14, 2026: BATTERY. INOPERATIVE. MULTIPLE INTERIOR EMERGENCY LIGHTS INOPERATIVE (SERVICE DOOR EXIT IDENTIFIER SIGN, EXIT MARKING SIGN ABOVE FA SEAT, EMERGENCY ROW AFT EXIT LOCATING SIGN, MOST A
- [SDR JJBA20260604003](https://openairdocs.org/sdr/JJBA20260604003), Jun 2, 2026: HANDLE. MISINSTALLED. LH AND RH OVERWING EMERGENCY EXIT DOOR HANDLES INSTALLED UPSIDE DOWN. REINSTALLED LH AND RH EMERGENCY EXIT DOOR HANDLES TO PROPER CONFIGURATION. OPS CHECK SAT. 
- [SDR JJBA20260604001](https://openairdocs.org/sdr/JJBA20260604001), Jun 1, 2026: BATTERY. INOPERATIVE. WING AND AISLE 1 EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY #1. OPS CHECK SAT.
- [SDR JJBA20260601030](https://openairdocs.org/sdr/JJBA20260601030), May 28, 2026: INVERTER. FAULTED. ROW 18 FRONT CEILING EXIT SIGN LIGHT INOPERATIVE. REMOVED AND REPLACED ROW 18 FWD EXIT SIGN. OPS CHECK FAILED. SWAPPED INVERTER 4 AND 6. OPS CHECK SAT.
- [SDR JJBA20260505001](https://openairdocs.org/sdr/JJBA20260505001), May 3, 2026: LIGHT. INOPERATIVE. OVERHEAD EXIT ROW EMERGENCY LIGHT INOPERATIVE (FWD). REMOVED AND REPLACED FWD OVERHEAD EXIT ROW EMERGENCY LIGHT.
- [SDR JJBA20251204003](https://openairdocs.org/sdr/JJBA20251204003), Dec 1, 2025: LAMP. INOPERATIVE. RH LATERAL WING-TO-FUSELAGE FAIRING EMERGENCY LIGHT INOPERATIVE. RH SIDE CENTER FAIRING EXTERNAL EMERGENCY LIGHT ACCESS PANEL HAS 4 STRIPPED SCREWS. REMOVED AND
- [SDR JJBA20251023049](https://openairdocs.org/sdr/JJBA20251023049), Oct 21, 2025: BATTERY PACK. INOPERATIVE. SEVERAL GALLEY AREA EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BPS #2. OPS CHECK GOOD.
- [SDR JJBA20251023048](https://openairdocs.org/sdr/JJBA20251023048), Oct 21, 2025: BATTERY. INOPERATIVE. OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BPS #4. OPS CHECK GOOD.
- [SDR JJBA20250428068](https://openairdocs.org/sdr/JJBA20250428068), Apr 25, 2025: LIGHT. MISINSTALLED. RH OVERWING EMERGENCY EXIT LIGHT INSTALLED UPSIDE DOWN. REMOVED AND REPLACED RH OVERWING EMERGENCY EXIT LIGHT HOUSING.
- [SDR JJBA20250414058](https://openairdocs.org/sdr/JJBA20250414058), Apr 13, 2025: BATTERY. INOPERATIVE. EMERGENCY EXIT LIGHTS AT ROW 18 INOPERATIVE AND EMERGENCY CEILING LIGHTS AT 18. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY FOR ROW 18. OPS CHECK GOOD.
- [SDR JJBA20230710007](https://openairdocs.org/sdr/JJBA20230710007), Jul 7, 2023: CONTROL UNIT. INOPERATIVE. NO BRAKES ON LANDING BRAKE INB INOPERATIVE MESSAGE FLASHED ON EICAS. REMOVED AND REPLACED #2 & 3 BRAKES. REMOVED AND REPLACED BCU. OPS CHECK SAT. BOTH LEFT AND 
- [SDR JJBA20220629026](https://openairdocs.org/sdr/JJBA20220629026), Jun 29, 2022: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS AT EMERGENCY EXIT DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES #3 AND #4. OPS CHECK SAT #3 - ABS-2013-1A SN 53157 TSN 31901
- [SDR JJBA20211214028](https://openairdocs.org/sdr/JJBA20211214028), Dec 14, 2021: NONE. NONE. VENTRAL TANK FRONTAL FACE LIP TO ATTACH THE PANELS IS BARE METAL. CUTOUT DONE ON VENTRAL TANK FWD FACE LIP AND PART FABRICATED. VENTRAL TANK FRONTAL FACE LIP RE
- [SDR JJBA20211214027](https://openairdocs.org/sdr/JJBA20211214027), Dec 14, 2021: NONE. NONE. CORROSION FOUND ON LOWER SKIN UNDER RAD ALT ANTENNA #2 AFT SUPPORT BTW FR 68-69 IN REAR FUSE I AREA. RAD ALT #2 ANTENNA, SUPPORT, SUPPORT ASSEMBLY AND FAIRING R
- [SDR JJBA20211214026](https://openairdocs.org/sdr/JJBA20211214026), Dec 14, 2021: NONE. NONE. DENT FOUND ON RH SKIN BTW FR 25-26 AND BTW STR 13R-12R IN CF II AREA. DENT FOUND ON RH SKIN BTW FR 25-26 AND BTW STR 13R-12R IN CFII AREA. CUT-OUT PERFORMED ON 
- [SDR JJBA20211214025](https://openairdocs.org/sdr/JJBA20211214025), Dec 14, 2021: NONE. NONE. CORROSION FOUND ON LOWER SKIN BTW FR 20-21 AND BTW STR 21L-21R IN CF1 DOOR STRUCTURE AREA. SKIN AT FR20-21 BTW 21L-21R CORROSION BLENDED FOR ENGINEERING REVIEW.
- [SDR JJBA20211214024](https://openairdocs.org/sdr/JJBA20211214024), Dec 14, 2021: NONE. NONE. DENTS FOUND ON LH SKIN BTW FR 19-21 AND BTW STR 11L-12L IN CF I AREA. LH SKIN BTW FR19-21 AND BTW STR 11L-12L IN CF! AREA, PATCH REMOVED FOR INVESTIGATION. 3 DE
- [SDR JJBA20211214019](https://openairdocs.org/sdr/JJBA20211214019), Dec 14, 2021: NONE. NONE. DAMAGE FOUND ON RH OUTBD OMEGA BEAM AT FR 48 IN FLOOR STRUCTURE CF III AREA. ON RH OUTBD OMEGA BEAM AT FR48 IN FLOOR STRUCTURE CF3 AREA, DAMAGE CUTOUT ON RH OME
- [SDR JJBA20211129018](https://openairdocs.org/sdr/JJBA20211129018), Nov 29, 2021: NONE. NONE. LH OMEGA BEAM FOUND CRACKED AT FR 24, AND FR 25 AND BOTTOM FLANG FOUND CORRODED. REPLACED WITH NEW PART LH OMEGA BEAM BTW FR 23-29
- [SDR JJBA202108131030](https://openairdocs.org/sdr/JJBA202108131030), Aug 11, 2021: LIGHT. MISSING. EMERGENCY FLOOR STRIP AT 1A MISSING. INSTALLED EMERGENCY FLOOR STRIP.
- [SDR JJBA20210511013](https://openairdocs.org/sdr/JJBA20210511013), May 11, 2021: CONNECTOR. BURNED. ON DEPARTURE, SMOKE WAS COMING FROM FWD ENTRANCE COMPARTMENT AND THE LIGHT ABOVE THE FWD ENTRANCE COMPARTMENT. FOUND LH FWD PAX CABIN CEILING LIGHT BULB CONNECT
- [SDR JJBA20220302008](https://openairdocs.org/sdr/JJBA20220302008), Mar 2, 2021: BATTERY PACK. INOPERATIVE. FWD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED #1 EMERGENCY BATTERY. OPS CHECK SAT
- [SDR JJBA20212260006](https://openairdocs.org/sdr/JJBA20212260006), Feb 26, 2021: SEAT FRAME. CRACKED. SEATS 22A, 10A & 9A AISLE SIDE FRAME CRACKED. REMOVED AND REPLACED SEATS 10A, 9A & 22A.
- [SDR JJBA20210301036](https://openairdocs.org/sdr/JJBA20210301036), Feb 26, 2021: LIGHT. INOPERATIVE. BOTH LH SIDE EXTERNAL EMERGENCY LIGHTS INOPERATIVE. R&R LH SIDE EXTERNAL EMERGENCY LIGHTS. OPS CHECK SAT.
- [SDR JJBA20201212010](https://openairdocs.org/sdr/JJBA20201212010), Dec 12, 2020: PUMP. LEAKING. NR 1 HYD PUMP FAIL ADVISORY AFTER GEAR EXTENSION. INVESTIGATION FOUND HYD LEAK ON RT GEAR ACTUATOR LINES. R & R ACTUATOR LINE. RII ON GEAR SWINGS, INSTALL PER G
- [SDR JJBA20200807004](https://openairdocs.org/sdr/JJBA20200807004), Aug 7, 2020: SKIN. CRACKED. SUSPECTED CRACKS ON RH L/E III COMING FROM OUTBOARD TWO VORTILONS AND EXTENDING UPWARD. R&R #3 RH WING LEADING EDGE. OPS CHECK LEAK CHECK SAT AT THIS TIME
- [SDR JJBA202005041001](https://openairdocs.org/sdr/JJBA202005041001), May 1, 2020: BATTERY. DISCHARGED. BOTH OVER WING EMERGENCY LIGHTS ARE INOPERATIVE. R&R EMERGENCY LIGHT BATTERY #4. OPS CHECK SAT.
- [SDR JJBA2019080171021](https://openairdocs.org/sdr/JJBA2019080171021), Jul 31, 2019: LIGHT. MISINSTALLED. RH OVER WING EXTERNAL EMERGENCY LIGHT UPSIDE DOWN. RE POSITIONED RH OVER WING EXTERNAL EMERGENCY LIGHT.
- [SDR JJBA201906021016](https://openairdocs.org/sdr/JJBA201906021016), Jun 1, 2019: GROUND WIRE. FAILED. MAIN CABIN DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. DISASSEMBLE AND TESTING REVEALS BAD GROUND. CORRECT CIRCUIT WIRES. OPS CHECK SAT.
- [SDR ASOA201905244019](https://openairdocs.org/sdr/ASOA201905244019), May 24, 2019: RIB. CRACKED. IAH - DURING MAINTENANCE INSPECTION CRACKS WERE DETECTED AROUND THE NUT PLATE HOLES FOR THE GRAB HANDLE IN THE COCKPIT ON OVERHEAD RIB. MAINTENANCE PERFORMED A 
- [SDR ASOA201905184018](https://openairdocs.org/sdr/ASOA201905184018), May 18, 2019: PANEL. CRACKED. IAH - DURING MAINTENANCE INSPECTION THE RT OVERHEAD PANEL IN THE COCKPIT WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH TECH
- [SDR ASOA201905014013](https://openairdocs.org/sdr/ASOA201905014013), May 1, 2019: STRAKE. DENTED. HOB- DURING PREFLIGHT INSPECTION THE CREW REPORTED A DENT IN THE LEFT HAND REAR STRAKE BETWEEN FRAMES 9 & 10. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE 
- [SDR ASOA2018082073053](https://openairdocs.org/sdr/ASOA2018082073053), Aug 7, 2018: FLOOR SUPPORT. CORRODED. DURING A C CHECK INSPECTION, FOUND CORROSION ON THE FLOOR SUPPORT AT FRAME 61. MAINTENANCE REPLACED THE LEFT FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR ASOA2018080877049](https://openairdocs.org/sdr/ASOA2018080877049), Jul 27, 2018: SKIN SPLICE. CORRODED. DURING A C CHECK INSPECTION, THE SKIN SPLICE BETWEEN FRAMES 23 - 24, STRINGERS 18R AND 19R WAS CORRODED. MAINTENANCE REPAIRED THE SKIN IAW SRM 53-00-02.
- [SDR ASOA2018082043052](https://openairdocs.org/sdr/ASOA2018082043052), Jul 24, 2018: DOUBLER. CORRODED. DURING A C CHECK INSPECTION, FOUND CORROSION AT FRAME 61, STRINGER 16L. MAINTENANCE REPLACED CARBON CROSSBEAM PARTITION SUPPORT DOUBLER IAW SRM 51-40-02
- [SDR ASOA2018081723051](https://openairdocs.org/sdr/ASOA2018081723051), Jul 22, 2018: SKIN. CRACKED. DURING A C CHECK INSPECTION, FOUND THE FUSEALGE SKIN CRACKED AT FRAME 75, STRINGER 2L. MAINTENANCE REPAIRED THE SKIN IAW SRM 53-31-01, ITEM 5.
- [SDR ASOA20180808048](https://openairdocs.org/sdr/ASOA20180808048), Jul 18, 2018: RIB. CRACKED. DURING A C CHECK INSPECTION, FOUND CRACK ON LEFT WING RIB 21 AROUND RIVET HOLE .250 LENGTH. MAINTENANCE PERFORMED REPAIR IA/W SRM 1142 57-20-07 AND ETD 2018-145
- [SDR ASOA201703183049](https://openairdocs.org/sdr/ASOA201703183049), Mar 18, 2017: LIGHT. BURNED. BURNING ELECTRICAL ODOR FORWARD FRONT OF CABIN. FOUND ROW 7A SIDE WALL LIGHT RETAINER TO BE BURNING. REMOVED THE LIGHT IAW AMM 33-21-06.
- [SDR ASOA201612234113](https://openairdocs.org/sdr/ASOA201612234113), Dec 23, 2016: LIGHT. DISCHARGED. THE FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHT STRIPS AT SEATS 18 A & D WERE NOT ILLUMINATING. MAINTENANCE CHARGED THE EMERGENCY LIGHT STRIOS, OPERATIONALLY 
- [SDR ASOA20160406033](https://openairdocs.org/sdr/ASOA20160406033), Apr 6, 2016: BATTERY PACK. DISCHARGED. DURING MAINTENANCE INSPECTION THE LT AND RT AFT OVER THE WINGS EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK, O
- [SDR ASOA20140607080](https://openairdocs.org/sdr/ASOA20140607080), Jun 7, 2014: WIRE HARNESS. BURNED. THE CREW REPORTED AN ELECTRICAL BURNING ODOR AT 11A. MAINTENANCE INSPECTED THE ACFT AND R & R THE LIGHT HARNESS FOR SEAT 11A, OPERATIONALLY TESTED WITH NO DEFEC
- [SDR ASOA20140602062](https://openairdocs.org/sdr/ASOA20140602062), Jun 2, 2014: BATTERY PACK. DISCHARGED. DURING MX INSPECTION THE AFT CABIN CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT BATTERY WITH OPS CHECK GOOD. ACFT WAS APPROV
- [SDR ASOA20131102267](https://openairdocs.org/sdr/ASOA20131102267), Nov 3, 2013: SHEAR TIE. CORRODED. DURING C-CHECK, THE SHEAR TIE AT FRAME 68 BETWEEN STRINGERS 15-16L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IA
- [SDR ASOA20131102266](https://openairdocs.org/sdr/ASOA20131102266), Nov 3, 2013: FRAME. CORRODED. DURING C-CHECK, FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15-16L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01505. A
- [SDR ASOA20131102265](https://openairdocs.org/sdr/ASOA20131102265), Nov 3, 2013: FRAME. CRACKED. DURING C-CHECK THE FRAME 10 SEGMENT BETWEEN STRINGERS 9-10L WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FRAME SEGMENT IAW SRM 51-40-02. THE ACFT WAS APPROVED
- [SDR ASOA20131102264](https://openairdocs.org/sdr/ASOA20131102264), Nov 3, 2013: DOOR FRAME. CORRODED. DURING C-CHECK. THE MAIN DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5210-01154. THE ACFT 
- [SDR ASOA20131102263](https://openairdocs.org/sdr/ASOA20131102263), Nov 3, 2013: SKIN. CRACKED. DURING C-CHECK, THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 5-7R. MAINTENANCE REMOVED THE CRACKS BY REAMING AND 
- [SDR ASOA20131102262](https://openairdocs.org/sdr/ASOA20131102262), Nov 3, 2013: SKIN. CRACKED. DURING C-CHECK, CRACKS WERE FOUND AROUND FASTENERS ON THE LT AFT SKIN FROM FRAMES 77-79 AND STRINGERS 5-7L. MX REMOVED THE CRACKS BY REAMING AND PERFORMED BUSHI
- [SDR ASOA20131008395](https://openairdocs.org/sdr/ASOA20131008395), Oct 5, 2013: MOUNT. CRACKED. NR 2 ENGINE MOUNT YOKE LOWER, FWD EAR AFT FITTING IS CRACKED. R & R NR 2 ENGINE MOUNT YOKE. ACFT RELEASED AND RETURNED TO SERVICE.

All 81: https://openairdocs.org/aircraft/N23139/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/N23139/stcs.md

## Earlier aircraft with N23139

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N23139 before.

- [Cancelled 1971-04-05](https://openairdocs.org/deregistered/N23139-1971-04-05): Piper-Ribnicky J3C-65, S/N 2919, built 1939. Owner: [St Francis Busting Co](https://openairdocs.org/faa-owner/ST%20FRANCIS%20BUSTING%20CO), [Parkin, AR](https://openairdocs.org/faa-place/AR/Parkin)

## 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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