# N14198: 2006 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: 14500951
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 9, 2006
- Certificate issued: April 21, 2021
- Expires: April 30, 2028
- Mode S code: A0AA1B
- 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=14198
- Page: https://openairdocs.org/aircraft/N14198

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/N14198/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 N14198.

## FAA accident and incident reports

None matched to N14198.

## Service difficulty reports (101, 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 JJBA20261021006](https://openairdocs.org/sdr/JJBA20261021006), Oct 20, 2026: VALVE. INOPERATIVE. ON CLIMBOUT AT 12000`, A BLEED LEAK 1 WARNING MESSAGE ON THE EICAS AND BUTTON. LEVELED OFF AT 15000` & FOLLOWED QRH THEN DESCEND TO 10000`. DESELECTED BLEED 1 A
- [SDR JJBA20260817013](https://openairdocs.org/sdr/JJBA20260817013), Aug 17, 2026: LAMP. INOPERATIVE. CEILING EMERGENCY LIGHTS INOPERATIVE AT ROW 2 AND 23. REMOVED AND REPLACED ROW 3 AND 23 AISLE EMERGENCY LIGHTS. OPS CHECK SAT.
- [SDR JJBA20260817011](https://openairdocs.org/sdr/JJBA20260817011), Aug 16, 2026: LAMP. INOPERATIVE. FWD RH EMERGENCY EXTERIOR LIGHT INOPERATIVE. REMOVED AND REPLACED FWD RH EMERGENCY LIGHT. OPS CHECK SAT.
- [SDR JJBA20260518010](https://openairdocs.org/sdr/JJBA20260518010), May 14, 2026: FUSE. INOPERATIVE. EMERGENCY LIGHTS ASSOCIATED WITH BPS2 INOP. R&R F2 FUSE ON BPS2 CHARGER. OP CHECK GOOD
- [SDR JJBA20260501032](https://openairdocs.org/sdr/JJBA20260501032), Apr 30, 2026: LIGHT SYS. FAULTED. 18CD LOWER EXIT MARKER ON ESCAPE HATCH INOPERATIVE. PERFORMED ELECTRICAL RESET AND PERFORMED EMERGENCY LIGHT OPS CHECK. OPS CHECK GOOD.
- [SDR JJBA20260423016](https://openairdocs.org/sdr/JJBA20260423016), Apr 20, 2026: LAMP. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT LAMP. OPS CHECK FAILED. FOUND 2 BROKEN WIRES LEADING TO LIGHT ASSEMB
- [SDR JJBA20260417014](https://openairdocs.org/sdr/JJBA20260417014), Apr 16, 2026: INVERTER. INOPERATIVE. FWD-MOST CEILING EMERGENCY EXIT LIGHT INOPERATIVE. FOUND COCKPIT STEP EXIT LIGHT ALSO INOPERATIVE. REMOVED AND REPALCED INVERTER #1. OPS CHECK SAT.
- [SDR JJBA20260327011](https://openairdocs.org/sdr/JJBA20260327011), Mar 24, 2026: LAMP. INOPERATIVE. LH AFT EXT EMERGENCY LIGHT INOPERATIVE. RELAMPED LH AFT EMERGENCY LIGHT. OPS CHECK GOOD.
- [SDR JJBA20250611011](https://openairdocs.org/sdr/JJBA20250611011), Jun 9, 2025: UNKNOWN. ODOR. FOUL AIR SMELL COMING FROM AIR CONDITIONING IN CABIN AND FLIGHT DECK THROUGHOUT THE FLIGHT (OILY SMELL). INSPECTED E1, E2 AND APU FOR OIL LEAKS. NO OIL LEAKS NO
- [SDR JJBA20250403010](https://openairdocs.org/sdr/JJBA20250403010), Apr 2, 2025: SIGN. INOPERATIVE. LH LOWER EMERGENCY EXIT DOOR SIGN INOPERATIVE. REMOVED AND REINSTALLED EMERGENCY EXIT MARKING SIGN AT LH LOWER CABIN ESCAPE HATCH. OPS CHECK SAT.
- [SDR JJBA202502265044](https://openairdocs.org/sdr/JJBA202502265044), Feb 21, 2025: SKIN. DENTED. DENTS ON RH CENTER FUSE I SKIN, BTW SKIN JUNCTION 02 AND FR 15 AND BTW STR 16R-17R. REPAIR DOUBLER ON RH CENTER FUSE I SKIN, BTW FR 14-15 AND BTW STR 16R-17R
- [SDR JJBA202502265043](https://openairdocs.org/sdr/JJBA202502265043), Feb 20, 2025: REPAIR. DAMAGED. REPAIR DOUBLER ON LH CENTER FUSE I SKIN, BTW FR 19-20 AND BTW STR 14L-15L. REPAIR DOUBLER REMOVED TO INVESTIGATE ON LH CENTER FUSE I SKIN BTW FR19-20 AND BTW ST
- [SDR JJBA20250225042](https://openairdocs.org/sdr/JJBA20250225042), Feb 19, 2025: RIVET. LOOSE. MIDDLE OF RUDDER I, LH SKIN RIVETS LOOSE ON ANCHOR NUT FOR RUDDER DEFLECTION TOOL INSTALLATION. REPAIR DOUBLER ON LH RUDDER I SKIN BTW RIB ZV2312-ZV2601
- [SDR JJBA202502265041](https://openairdocs.org/sdr/JJBA202502265041), Feb 19, 2025: SKIN. DAMAGED. MIDDLE OF RUDDER II, LH SKIN, RIVETS HOLES ELONGATED ON ANCHOR NUT FOR RUDDER DEFLECTION TOOL INSTALLATION. REPAIR DOUBLER ON LH RUDDER II SKIN BTW RIB ZV2067-Z
- [SDR JJBA202502265037](https://openairdocs.org/sdr/JJBA202502265037), Feb 19, 2025: BEAM. CORRODED. CARGO DOOR ENTRY, LOWER BEAM FOUND CORRODED. LOWER BEAM REMOVED AND REPLACED.
- [SDR JJBA202502265038](https://openairdocs.org/sdr/JJBA202502265038), Feb 18, 2025: SHEAR TIE. CRACKED. REAR FUSELAGE I, FRAME 66, BTW STR 6L-7L, SHEAR CLIP FOUND CRACKED. RF I, FR66 BTW STR 6L-7L SHEAR CLIP REMOVED FOR REPLACEMENT. SHEAR CLIP FR66 MADE REPAIR PAR
- [SDR JJBA202502265040](https://openairdocs.org/sdr/JJBA202502265040), Feb 13, 2025: REPAIR. DAMAGED. REPAIR DOUBLER ON LH CENTER FUSE I SKIN BTW FR20-21 AND BTW STR 13L-14L. LH CENTER FUSE I, SKIN BTW FR 20-21 AND BTW STR 13L - 14L DOUBLER REMOVED. SKIN REPAIRE
- [SDR JJBA20250225035](https://openairdocs.org/sdr/JJBA20250225035), Feb 12, 2025: PANEL. CRACKED. HORIZONTAL - OVERHEAD PANEL IN COCKPIT FOUND CRACKED IN 2 PLACES. AFTER NDT INVESTIGATION, ONLY 1 CRACK FOUND ON RH SIDE. RH SIDE CRACK CUTOUT. RH SIDE REPAIRED
- [SDR JJBA20250225034](https://openairdocs.org/sdr/JJBA20250225034), Feb 12, 2025: BEAM. CORRODED. CF IV, CENTER BEAM FOUND CORRODED BTW FR 59-61. CF4, CENTER BEAM BTW FR59-61 CORRODED OUT OF LIMIT. CF4, CENTER BEAM BTW FR 59-61 CUTOUT (2X) PERFORMED. CENTER 
- [SDR JJBA20250225033](https://openairdocs.org/sdr/JJBA20250225033), Feb 12, 2025: SKIN. DENTED. EXTERNAL CENTER FUSELAGE, SKIN DENTED BTW FRAME 19-20 AND BTW STR 11L-12L. EXTERNAL CENTER FUSE, BTW FR 19-20 AT STR 11L. EXISTING RIVET REMOVED FOR REPAIR DOUB
- [SDR JJBA20250213023](https://openairdocs.org/sdr/JJBA20250213023), Feb 7, 2025: SPAR. CRACKED. VERT STAB AFT OF REAR SPAR 3, LH SKIN UPPER AND LOWER PROFILE CRACKED. REMOVED AND REPLACED
- [SDR JJBA20250213025](https://openairdocs.org/sdr/JJBA20250213025), Feb 6, 2025: SHEAR TIE. CRACKED. IN REAR FUSELAGE, AT BULKHEAD 80, SHEAR CLIP CRACKED ON LH SIDE BETWEEN STRINGER 5L AND STRINGER 7L. IN REAR FUSELAGE AT BULKHEAD 80, SHEAR CLIP BTW STR 5L-7L P
- [SDR JJBA20250213024](https://openairdocs.org/sdr/JJBA20250213024), Feb 6, 2025: FAIRING. CRACKED. AFT BODY FAIRING ON THE RH SIDE, ONE RIB IS CRACKED. AFT BODY FAIRING ON THE RH SIDE, ONE RIB REMOVED AND REPLACED
- [SDR JJBA20250225039](https://openairdocs.org/sdr/JJBA20250225039), Feb 5, 2025: SKIN. CRACKED. CRACK FOUND AROUND RIVET ON LH REAR FUSE II SKIN AT FR 79 STR 7L-8L. CRACK AROUND RIVET AT SKIN FR79 BTW STR 7L-8L REPAIRED
- [SDR JJBA20250213018](https://openairdocs.org/sdr/JJBA20250213018), Feb 5, 2025: GUSSET. CORRODED. CENTER FUSELAGE IV, CENTER GUSSET BTW FRAME 59-61 FOUND CORRODED. CF4, CENTER GUSSET BTW FR 59-61 CORRODED OUT OF LIMITS. GUSSET REMOVED FOR REPLACEMENT. GUSSET
- [SDR JJBA20250213026](https://openairdocs.org/sdr/JJBA20250213026), Feb 4, 2025: SUPPORT. CORRODED. REAR FUSELAGE I, LH SILL BTW FRAME 61-65 FOUND CORRODED. LH SILL BTW FR 64-65 BLENDED OUT OF LIMIT. REAR FUSELAGE I, LH CARBON BULKHEAD REMOVED FOR ACCESS. RF I
- [SDR JJBA20250213022](https://openairdocs.org/sdr/JJBA20250213022), Feb 4, 2025: SUPPORT. CORRODED. CENTER FUSELAGE II, RH SILL BTW FRAME 29-35 FOUND CORRODED. CENTER FUSELAGE II, RH SILL BTW FR 29-35, CORROSION BLENDED OUT OF LIMIT. RH SILL BTW FR 29-35 REMOV
- [SDR JJBA20250213020](https://openairdocs.org/sdr/JJBA20250213020), Feb 4, 2025: TEE ANGLE. CORRODED. REAR FUSELAGE 1, LH T-POST AT FR61 FOUND CORRODED. RF1, LH T-POST AT FR61 BLENDED OUT OF LIMITS. LH T-POST AT FR61 REMOVED FOR REPLACEMENT. LH T-POST NEW PART I
- [SDR JJBA20250210015](https://openairdocs.org/sdr/JJBA20250210015), Feb 4, 2025: ANGLE. CRACKED. CENTER FUSELAGE 1, AT FRAME 14 AND STR 16L, REINFORCEMENT ANGLE FOUND CRACKED. AT CF1, AT FR 14 STR 16L REINFORCEMENT ANGLE REMOVED FOR REPLACEMENT. AT CF1 AT F
- [SDR JJBA20250213021](https://openairdocs.org/sdr/JJBA20250213021), Feb 3, 2025: SUPPORT. CORRODED. CENTER FUSELAGE III, RH SILL BTW FRAME 35-41 FOUND CORRODED. RH SILL BTW FR 35-41 BLENDED OUT OF LIMITS. RH SILL BTW FR 35-41 REMOVED FOR REPLACEMENT. ON CF III
- [SDR JJBA20250213019](https://openairdocs.org/sdr/JJBA20250213019), Jan 29, 2025: FLOOR SUPPORT. DAMAGED. CENTER FUSELAGE III, LH OMEGA BEAM BTW FRAME 50-46, OUTBD ANGLE, SURFACE BARE METAL. AFTER BEING CLEANED, FOUND TO BE CRACKED, REMOVED AND REPLACED.
- [SDR JJBA20250225036](https://openairdocs.org/sdr/JJBA20250225036), Jan 27, 2025: SUPPORT. CRACKED. REAR FUSELAGE I, BTW FRAME 67-68 AT BTW STR 4R-5R, SUPPORT FOUND CRACKED. REAR FUSELAGE I, BTW FRAME 67-68 BTW STR 4R-5R, SUPPORT REMOVED FOR REPLACEMENT. REAR 
- [SDR JJBA20241018010](https://openairdocs.org/sdr/JJBA20241018010), Oct 16, 2024: LAMP. INOPERATIVE. LH OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH OVERWING EMERGENCY LIGHT LAMP. OPS CHECK SAT.
- [SDR JJBA20240808011](https://openairdocs.org/sdr/JJBA20240808011), Aug 8, 2024: INVERTER. INOPERATIVE. SERVICE DOOR UPPER EXIT SIGN EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR UPPER EXIT SIGN EMERGENCY LIGHT. OPS CHECK FAIL. REMOVED AND REPLACE
- [SDR JJBA20240314048](https://openairdocs.org/sdr/JJBA20240314048), Mar 13, 2024: SIGN. INOPERATIVE. SERVICE DOOR CEILING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN. OPS CHECK SAT.
- [SDR JJBA20220926041](https://openairdocs.org/sdr/JJBA20220926041), Sep 26, 2022: SHAFT. LOOSE. MCD WONT OPEN FROM INSIDE. INSPECTED AND FOUND MCD INTERNAL HANDLE LOOSE IN SHAFT, TIGHTENED HANDLE BOLT. OPS CHECK GOOD, NO ADJUSTMENTS MADE.
- [SDR JJBA20220914009](https://openairdocs.org/sdr/JJBA20220914009), Sep 11, 2022: NONE. UNKNOWN. FUMES IN THE CABIN AND COCKPIT. SMOKE IN THE CABIN. REMOVED AND REPLACED #1 WS TEMP CONTROLLER. NO FURTHER FAULTS FOUND. FOUND DAMAGE ON #1 WS TEMP CONTROLLER. 
- [SDR JJBA20220801035](https://openairdocs.org/sdr/JJBA20220801035), Jul 30, 2022: LIGHT. INOPERATIVE. PHOTOLUMINESCENT STRIP NEAR GALLEY LOOSE. RESECURED PHOTOLUMINESCENT STRIP
- [SDR JJBA20220707003](https://openairdocs.org/sdr/JJBA20220707003), Jul 2, 2022: LAMP. INOPERATIVE. EMERGENCY LIGHT OVER SEAT 18A INOP. R/R EMERGENCY LIGHT LAMP OVER SEAT 18A. OPS CHECK SAT.
- [SDR JJBA20220706002](https://openairdocs.org/sdr/JJBA20220706002), Jul 2, 2022: LAMP. INOPERATIVE. EMERGENCY LIGHT AT CELING PANEL 243DLC INOP. R/R EMERGENY LIGHT LAMP AT CELING PANEL 243DLC
- [SDR JJBA20220322048](https://openairdocs.org/sdr/JJBA20220322048), Mar 22, 2022: BATTERY. OVERTEMP. BATT 2 OVERTEMP EICAS MESSAGE. REPLACED #2 MAIN BATTERY AND OPS CHECKED GOOD,
- [SDR JJBA20220306009](https://openairdocs.org/sdr/JJBA20220306009), Mar 6, 2022: STRAP. MISSING. FLOOR EMERGENCY LIGHT STRIP MISSING BY GALLEY. REPLACED EMERGENCY LIGHT STRIP.
- [SDR JJBA20211216021](https://openairdocs.org/sdr/JJBA20211216021), Dec 16, 2021: NONE. NONE. LH AND RH OVERWING EXTERNAL EMERGENCY EXIT LIGHTS ARE INSTALLED UPSIDE DOWN. REMOVED AND REINSTALLED EXTERNAL EMERGENCY LIGHTS.
- [SDR JJBA20211118028](https://openairdocs.org/sdr/JJBA20211118028), Nov 18, 2021: STRAP. MISSING. EMERGENCY EXIT LIGHTING STRIP MISSING BY 1A. R&R EMERGENCY EXIT LIGHTING STRIP.
- [SDR JJBA20211101011](https://openairdocs.org/sdr/JJBA20211101011), Nov 1, 2021: NONE. NONE. SMALL DENT FOUND IN BOTTOM CORNER OF MAIN DOOR. CUT OUT PERFORMED, FILLER AND DOUBLER FABRICATED. DENT ON BOTTOM AFT CORNER OF THE MAIN DOOR REPAIRED.
- [SDR JJBA20211101010](https://openairdocs.org/sdr/JJBA20211101010), Nov 1, 2021: NONE. NONE. AS PER CUSTOMER REQUEST, REPAIR DOUBLER ON RH CENTER FUSE 1 BTW FR 22A-23 AND BTW STR 13R-14R, NEED TO BE REMOVED FOR INVESTIGATION. REMOVED REPAIR DOUBLER ON R
- [SDR JJBA20211101009](https://openairdocs.org/sdr/JJBA20211101009), Nov 1, 2021: NONE. NONE. CORROSION FOUND ON LH AFT L-SHAPE CARGO DOOR SURROUND STRUCTURE AT FR68 BTW STR 15-17. AT FR 68 BTW STR 15 AND 17 SHEAR CLIP BLENDED AND FOUND OUT OF LIMIT. "L"
- [SDR JJBA20211101008](https://openairdocs.org/sdr/JJBA20211101008), Nov 1, 2021: NONE. NONE. NICKS FOUND ON TOP SKIN AROUND EXISTING REPAIR DOUBLER BTW FR 54 TO 55 AND STR 1R TO 1L IN CENTER FUSE IV AREA. ON TOP SKIN AROUND EXISTING REPAIR DOUBLER BTW F
- [SDR JJBA20211101007](https://openairdocs.org/sdr/JJBA20211101007), Nov 1, 2021: NONE. NONE. 2 DENT FOUND SKIN BTW FR 6 AND JUN 1 BTW STR 13-15 LH. ON LH FWD FUSE 1 SKIN, BTW FR 6-7 AND BTW STR 13L-15L DENTS (2X) ARE OUT OF LIMITS. PERFORMED CUT OUT AND
- [SDR JJBA20211101006](https://openairdocs.org/sdr/JJBA20211101006), Nov 1, 2021: NONE. NONE. CF1, BTW FR 13-14 AND BTW STR 10R-11R, SKIN DAMAGED DURING RIVET REPLACEMENT. BTW FR 13-14 AND BTW STR 10-11 RH REPAIR ON SKIN PERFORMED

All 101: https://openairdocs.org/aircraft/N14198/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/N14198/stcs.md

## 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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