# N17159: 2004 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: 145792
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 19, 2004
- Certificate issued: May 31, 2019
- Expires: May 31, 2029
- Mode S code: A1200D
- 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=17159
- Page: https://openairdocs.org/aircraft/N17159

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/N17159/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 N17159.

## 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 20260802009859I](https://openairdocs.org/incident/20260802009859I), Aug 2, 2026: Embraer EMB-145XR (N17159), Dulles, WA, Minor damage. Aircraft [privacy data omitted], UCA4914, waiting at runway 30 adviced tower that they could not accept departure due to bad weather conditions. Flight crew…
- [Incident 20230512002799I](https://openairdocs.org/incident/20230512002799I), May 12, 2023: Embraer EMB-145XR (N17159), Houston, TX, Minor damage. On may 12, 2023, incident aircraft operated in revenue service with 49 passengers and 3 crew, from George Bush Intercontinental/Houston airport (iah) to…

## Service difficulty reports (77, 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 JJBA20260819016](https://openairdocs.org/sdr/JJBA20260819016), Aug 19, 2026: BATTERY PACK. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS INOPERATIVE. LH/RH EXTERIOR OVERWING, CABIN RH OVERWING, AISLE EMERGENCY LIGHT AFT AND ROW 18, CENTER FWD EXIT LOCATING SIGN AND MCD E
- [SDR JJBA20260520021](https://openairdocs.org/sdr/JJBA20260520021), May 11, 2026: SHEAR PANEL. GOUGED. APU INTERIOR GOUGE ON SHEAR PANEL. BLEND OUT WAS PERFORMED.
- [SDR JJBA20260520020](https://openairdocs.org/sdr/JJBA20260520020), May 11, 2026: FRAME. BENT. APU INTERIOR, FRAME SHAPE U FWD-TO-REAR MULTIPLES BENT. RECOUNTOUR WAS PERFORMED.
- [SDR JJBA20260520018](https://openairdocs.org/sdr/JJBA20260520018), May 11, 2026: SKIN. NICKED. NICK ON FUSELAGE SKIN LT NEAR FR 10 BETWEEN STGR 15 - STGR 17. PERMANENT REINFORCEMENT REPAIR WAS PERFORMED.
- [SDR JJBA20260520017](https://openairdocs.org/sdr/JJBA20260520017), May 11, 2026: SKIN. GOUGED. LH FWD FUSELAGE SKIN GOUGE / NICK BETWEEN FRM 10-11 STGR 15-17. PERMANENT REINFORCEMENT REPAIR WAS PERFORMED.
- [SDR JJBA20260520023](https://openairdocs.org/sdr/JJBA20260520023), May 9, 2026: SKIN. DAMAGED. CREASE ON LH FWD FUSELAGE BETWEEN STGRS 15-16 AND FRAMES 11-12 CLOSE TO FRAME 12. RECOUNTOUR WAS PERFORMED.
- [SDR JJBA20260520022](https://openairdocs.org/sdr/JJBA20260520022), May 9, 2026: SKIN. CANNING. LH APU SKIN OIL CANNING AND DENT. PERMANENT REINFORCEMENT REPAIR WAS PERFORMED.
- [SDR JJBA20260520019](https://openairdocs.org/sdr/JJBA20260520019), May 9, 2026: INLET. GOUGED. APU INLET INTERIOR GOUGE/DENT ON LOWER SKIN. DOUBLER REPAIR WAS PERFORMED
- [SDR JJBA20260327014](https://openairdocs.org/sdr/JJBA20260327014), Mar 26, 2026: INVERTER. INOPERATIVE. EMERGENCY MARKING SIGN ON RH EXIT HATCH INOPERATIVE. SLAVED IN RH EMERGENCY EXIT MARKER ASSEMBLY. OPS CHECK FAILED. AIRCRAFT RETURNED TO ORIGINAL CONFIGURATION.
- [SDR JJBA20260327010](https://openairdocs.org/sdr/JJBA20260327010), Mar 24, 2026: LAMP. INOPERATIVE. LH EMERGENCY EXIT CEILING AND AISLE 4 LIGHT INOPERATIVE. REMOVED AND REPLACED LH EMERGENCY EXIT CEILING AND AISLE 4 LIGHT BULBS. OPS CHECK SAT.
- [SDR JJBA20260209021](https://openairdocs.org/sdr/JJBA20260209021), Feb 7, 2026: PLATE. CORRODED. RT FWD WTF FAIRING EMERGENCY LIGHT PLATE SHOWING SIGNS OF CORROSION. REMOVED AND REPLACED RT FWD WTF FAIRING EMERGENCY LIGHT PLATE. LIGHT OPS CHECK SAT. APPLIED
- [SDR JJBA20251209022](https://openairdocs.org/sdr/JJBA20251209022), Dec 9, 2025: FUSE. INOPERATIVE. BOTH OVERWING AFT EXTERNAL EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED F1 FUSE ON NR 4 BATTERY CHARGER. OPS CHECK GOOD.
- [SDR JJBA20250918030](https://openairdocs.org/sdr/JJBA20250918030), Sep 18, 2025: LAMP. INOPERATIVE. LH WING/FUSELAGE FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT LAMP OF FORWARD LOWER FAIRING. OPS CHECK SAT.
- [SDR JJBA20250825053](https://openairdocs.org/sdr/JJBA20250825053), Aug 23, 2025: BATTERY. DISCHARGED. MULTIPLE EMERGANCY LIGHTS OUT. COCKPIT STEP, MAIN DOOR EXIT, AISLE LIGHT 1, MAIN ENTRANCE CEILING, EXIT AISLE CEILING LIGHT 1. R+R EMERGANCY LIGHT BATT 1. OPS C
- [SDR JJBA20250609005](https://openairdocs.org/sdr/JJBA20250609005), Jun 4, 2025: DOOR SILL. CORRODED. CORROSION FOUND ON AFT SERVICE DOOR THRESHOLD AT FRAME 22. REPAIRED SERVICE DOOR AFT SILL. COMPLETED EDDY CURRENT HIGH FREQUENCY INSPECTION OF AFT SERVICE DOOR 
- [SDR JJBA20250113011](https://openairdocs.org/sdr/JJBA20250113011), Jan 12, 2025: LAMP. INOPERATIVE. LH EXTERNAL OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LH EXTERNAL OVERWING EMERGENCY EXIT LIGHT. OPS CHECK SAT.
- [SDR JJBA20240502001](https://openairdocs.org/sdr/JJBA20240502001), May 1, 2024: LAMP. INOPERATIVE. RH EXTERNAL EMERGENCY LIGHT ON FWD LOWER FAIRING INOPERATIVE. REMOVED AND REPLACED RH EXTERNAL EMERGENCY LIGHT BULB. ISSUE REMAINS. RMOVED AND REPLACED RH EXTER
- [SDR JJBA20240415033](https://openairdocs.org/sdr/JJBA20240415033), Apr 13, 2024: LAMP. INOPERATIVE. COCKPIT CEILING EMERGENCY LIGHT OUT. REMOVED AND REPLACED BULB. OPS CHECK SAT.
- [SDR JJBA20230616013](https://openairdocs.org/sdr/JJBA20230616013), May 12, 2023: TIRE. FAILED. BLEW LEFT TIRES DURING TAKE OFF ROLL. 120 KTS ATO, DID NOT DECLARE EMERGENCY, NO BRAKE OVERTEMP EICAS MESSAGE, TEMP CARROT AT TOP OF GREEN RANGE. 185F DEGREES R
- [SDR JJBA20230109008](https://openairdocs.org/sdr/JJBA20230109008), Dec 29, 2022: FLOOR SUPPORT. CRACKED. CF 3, LH OMEGA BEAM, CRACK SUSPECTED AT FRAME LOCATION 36, 37. CRACK (1X) FOUND ONLY AT FR36. NO MORE ACTION AT FRAME 37. LH OMEGA BEAM REPAIRED WITH ANGLE AT F
- [SDR JJBA20230103035](https://openairdocs.org/sdr/JJBA20230103035), Dec 29, 2022: FLOOR SUPPORT. CRACKED. CF 2, UNDER FLOOR, LH OMEGA BEAM CRACK SUSPECTED AT FRAME 33-35. LH OMEGA BEAM REPAIRED AT FR 33-35 WITH A DOUBLER AND FILLER
- [SDR JJBA20221222017](https://openairdocs.org/sdr/JJBA20221222017), Dec 19, 2022: SKIN. CORRODED. CORROSION ON REAR FUSE 2 LOWER SKIN. BTW FR 80-61 AND BTW STR 19L-21L. ON FR2 LOWER SKIN, BTW FR80-81 AND BTW STR 19L-21L, CORROSION BLENDE DOUT OF LIMITS. CUTO
- [SDR JJBA20221222018](https://openairdocs.org/sdr/JJBA20221222018), Dec 15, 2022: FLOOR SUPPORT. CORRODED. CF4, CENTER OMEGA BEAM CORROSION UNDER NUT-PLATE BTW FRAME 59-61. CORROSION ON CENTER OMEGA BEAM BLENDED AND FOUND OUT OF LIMIT AT 2X NUT PLATE LOCATION FR59 AN
- [SDR JJBA20221222016](https://openairdocs.org/sdr/JJBA20221222016), Dec 13, 2022: GUSSET. CORRODED. CF4, LH GUSSET CORRODED BTW FRAME 59-61. CORROSION ON LH GUSSET FR 59-61 BLENDED AND FOUND OUT OF LIMIT. LH GUSSET BTW FR59 AND 61 REPLACED. CUT OUT PERFORMED A
- [SDR JJBA20220719012](https://openairdocs.org/sdr/JJBA20220719012), Jul 13, 2022: PANEL. MISUSED. RH OVER WING EXTERNAL EMERGENCY LIGHT INSTALLED UPSIDE-DOWN. RE-ORIENTATED RH OVER WING EXT EMERGENCY LIGHT.
- [SDR JJBA20220627022](https://openairdocs.org/sdr/JJBA20220627022), Jun 27, 2022: PROXIMITY SWITCH. UNKNOWN. LG AIR GND FAIL AS GEAR UP WAS SELECTED DURING CLIMB OUT. DISCONNECTED BOTH LH AND RH MLG WOW PROX SWITCHES. INSPECTED FOR SIGNS OF CORROSION ON SWITCHES AND CA
- [SDR JJBA20220430005](https://openairdocs.org/sdr/JJBA20220430005), Apr 30, 2022: UNKNOWN. OUT OF ADJUST. STEERING INOPERATIVE DISPLAYED UPON LANDING - OCF FLIGHT. INSPECTED AND FOUND FEED BACK POTENTIOMETER OUT OF ADJUSTMENT, ADJUSTED FEEB BAC POTENTIOMETER. REMOVE
- [SDR JJBA20220131032](https://openairdocs.org/sdr/JJBA20220131032), Jan 31, 2022: NOT REPORTED. NOT REPORTED. FOUND RH ENGINE FORCED CORE TO BYPASS MIXER CRACKED AT BOLT HOLES #7 AND #1 POSITIONS. REMOVED AND INSTALLED RH ENGINE BYPASS MIXER.
- [SDR JJBA20220120025](https://openairdocs.org/sdr/JJBA20220120025), Jan 20, 2022: GLOWSTRIP. MISSING. PHOTO LUMINESCENT STRIP PIECE MISSING ON THE FLOOR NEAR SEAT 3. REPLACED FLOOR EMERGENCY LIGHT STRIP BY SEAT 3
- [SDR JJBA20211024055](https://openairdocs.org/sdr/JJBA20211024055), Oct 24, 2021: FAIRING. INOPERATIVE. MCD EMERGENCY LIGHT INOPERATIVE. R&R MCD EMERGENCY LIGHT HOUSING. OPS CHECK SAT.
- [SDR JJBA2021091508028](https://openairdocs.org/sdr/JJBA2021091508028), Sep 8, 2021: MUFFLER. DISCONNECTED. PACK 2 OVERHEAT IN FLIGHT. PACK 1 MUFFLER DISCONNECTED. RECONNECTED MUFFLER. OPS CHECK SAT
- [SDR JJBA20210805025](https://openairdocs.org/sdr/JJBA20210805025), Aug 5, 2021: DAU. INOPERATIVE. DAU #2 WRN MIS CMP. R&R #2 DAU, PERFORMED DAU #2 OPS CHECK. OPS CHECK GOOD.
- [SDR JJBA20210424040](https://openairdocs.org/sdr/JJBA20210424040), Apr 24, 2021: LIGHT. INOPERATIVE. MAIN DOOR EMERGENCY CEILING LIGHT INOPERATIVE. R&R MAIN DOOR EMERGENCY CEILING LIGHTS. OPS CHECK SAT.
- [SDR JJBA20210120020](https://openairdocs.org/sdr/JJBA20210120020), Jan 20, 2021: SKIN. DENTED. MULTIPLE DENTS CARGO DOOR SKIN. 8 DENTS ARE FOUND ON CARGO DOOR. CARGO DOOR REPAIRED.
- [SDR ASOA201910148455](https://openairdocs.org/sdr/ASOA201910148455), Oct 8, 2019: RELAY. INOPERATIVE. THE CREW REPORTED THAT THE EMERGENCY LIGHTS FAILED TO ARM, AND THAT THE SWITCH WORKS IN THE IN AND OFF POSITIONS ONLY. MAINTENANCE REMOVED AND REPLACED RELAY K0
- [SDR ASOA201901067004](https://openairdocs.org/sdr/ASOA201901067004), Jan 6, 2019: FRAME. CRACKED. A/C IS IN C-CHECK WHEN INSPECTION FOUND FRAME CRACKED IN THE COCKPIT CEILING FWD OF SPEAKERS ON THE RT SIDE. MAINTENANCE REPAIRED THE FRAME IN THE COCKPIT CEILI
- [SDR ASOA201901067003](https://openairdocs.org/sdr/ASOA201901067003), Jan 6, 2019: CONNECTOR. MISSING. TYS A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE LT 191 PANEL EMERGENCY LIGHT CONNECTOR MISSING. MAINTENANCE INSTALLED A NEW CONNECTOR IAW SWPM 2
- [SDR ASOA201901097005](https://openairdocs.org/sdr/ASOA201901097005), Jan 5, 2019: FLOOR SUPPORT. CORRODED. CORROSION ON GALLEY CENTER OMEGA BEAM TOP CAP. REMOVED CENTER OMEGA BEAM TOP CAP. REPAIRED CENTER OMEGA BEAM BY CUTTING OUT THE CORRODED AREA, INSTALLED EXTERNA
- [SDR ASOA201812237191](https://openairdocs.org/sdr/ASOA201812237191), Dec 23, 2018: FLOOR SUPPORT. CORRODED. RIGHT HAND OMEGA BEAM IS CORRODED AT FRAME 60. - CORRECTIVE ACTION - REPAIRED OMEGA BEAM AT FRAME 60 IAW EMB245XR SRM 53-24-10, REPAIR 3, DOUBLER - .040" 2024-T
- [SDR ASOA201704197007](https://openairdocs.org/sdr/ASOA201704197007), Apr 20, 2017: BATTERY. DEFECTIVE. A/C IN FOR A 3A INSPECTION AND WE FOUND THE NR 1 EMERGEENCY CEILING LIGHT FLASH ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE NR 1 BATTERY TRAY IAW AMM 33-50
- [SDR ASOA20160923052C](https://openairdocs.org/sdr/ASOA20160923052C), Sep 23, 2016: BATTERY. INOPERATIVE. MAINTENANCE REPORTED FORWARD RIGHT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. THE NR 2 EMERGENCY LIGHT BATTERY WAS REPLACED. OPERATIONAL CHECKED GOOD.
- [SDR ASOA20160712033](https://openairdocs.org/sdr/ASOA20160712033), Jul 12, 2016: INVERTER. INOPERATIVE. DURING MX INSPECTION THE RT WING EXTERIOR EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE R & R NR5 INVERTER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR R
- [SDR ASOA20151212090](https://openairdocs.org/sdr/ASOA20151212090), Dec 12, 2015: DISPLAY. SHORTED. THE CREW REPORTED THAT THE EICAS WENT OUT ON DESCENT, ACCOMPANIED BY AN ELECTRICAL BURNING ODOR IN THE COCKPIT. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENAN
- [SDR ASOA201509257075](https://openairdocs.org/sdr/ASOA201509257075), Sep 27, 2015: LIGHT. INOPERATIVE. DURING ROUTINE CHECK THE RT EMERGENCY LIGHT MARKER ON THE EXIT DOOR WAS FOUND TO BE INOPERATIVE, MAINTENANCE R & R THE AFFECTED LIGHT MARKER ASSY, OPERATIONALLY
- [SDR ASOA201509257074H](https://openairdocs.org/sdr/ASOA201509257074H), Sep 27, 2015: INVERTER. INOPERATIVE. DURING ROUTINE CHECK, THE SERVICE DOOR EMERGENCY EXIT LIGHT IDENTIFIER WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED NR 2 EMERGENCY LIGHT INVERTER
- [SDR ASOA20140815087](https://openairdocs.org/sdr/ASOA20140815087), Aug 15, 2014: SENSOR. DISCONNECTED. F/A REPORTED SMOKE COMING FROM FLOOR VENT AT ROW NR 7 WHILE CLIMBING OUT AT 400 FT WITH BOTH PACKS OPERATING OFF APU. F/A DESCRIBED SMOKE AS "THICK AND GREY" MO
- [SDR ASOA20131107125](https://openairdocs.org/sdr/ASOA20131107125), Nov 7, 2013: LIGHT. MALFUNCTIONED. DURING MX INSPECTION THE LOWER GALLEY EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MX RESET SYS AND PERFORMED OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN 
- [SDR ASOA20130928113](https://openairdocs.org/sdr/ASOA20130928113), Sep 28, 2013: LIGHT. INOPERATIVE. THE SECOND FLOOR EMERGENCY LIGHT WAS REPORTED INOPERATIVE. MX R & R LIGHT. OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130309022](https://openairdocs.org/sdr/ASOA20130309022), Mar 9, 2013: LIGHT. INOPERATIVE. DURING MX INSPECTION, THE SERVICE DOOR EMERGENCY EXIT LIGHT ON HINGE SHROUD WAS FOUND INOPERATIVE. MX R & R THE SERVICE DOOR EMERGENCY EXIT LIGHT ASSY WITH OPS 
- [SDR ASOA20120404048](https://openairdocs.org/sdr/ASOA20120404048), Mar 27, 2012: SKIN. CORRODED. SURFACE CORROSION ALONG ENTIRE MOUNTING EXTERIOR SURFACE AND FASTENER HOLES AT BAGGAGE DOOR BUMPER PLATE. BLENDED, TREATED, PRIMED CORROSION AT BAGGAGE DOOR BUM

All 77: https://openairdocs.org/aircraft/N17159/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/N17159/stcs.md

## Earlier aircraft with N17159

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N17159 before.

- [Cancelled 1938-02-15](https://openairdocs.org/deregistered/N17159-1938-02-15): Stinson SR-9C, S/N 5119. Owner: [Aviation Manufacturing Corporation](https://openairdocs.org/faa-owner/AVIATION%20MANUFACTURING%20CORPORATION), [Downey, CA](https://openairdocs.org/faa-place/CA/Downey)

## 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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