# N14204: 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 AE-3007A1E](https://openairdocs.org/engine/rolls-royce-ae-3007a1e) (registry code 54169)
- 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: 14500968
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 22, 2006
- Certificate issued: December 19, 2019
- Expires: December 31, 2029
- Mode S code: A0AC93
- 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=14204
- Page: https://openairdocs.org/aircraft/N14204

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.

## ADs that may apply (OpenAirDocs): 84 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 AE-3007A1E)

- [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 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 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 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

### 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 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 2008-19-51](https://openairdocs.org/ad/2008-19-51) (historical): AE 3007A, AE 3007A1, AE 3007A1E and 5 more

All 93: https://openairdocs.org/aircraft/N14204/ads.md

## Information bulletins (advisory) (8 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 AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N14204.

## FAA accident and incident reports

None matched to N14204.

## Service difficulty reports (57, 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 JJBA20210429054](https://openairdocs.org/sdr/JJBA20210429054), Apr 29, 2021: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE. R&R #1, #2, AND #4 EMERGENCY LIGHT BATTERIES. OPS CHECK GOOD. #1 PN ABS-2013-1A SN 50056 ; #2 PN ABS-2013-1A SN 54281 ; #4 PN ABS-
- [SDR JJBA20210411016](https://openairdocs.org/sdr/JJBA20210411016), Apr 11, 2021: CHARGER. INOPERATIVE. BOTH LH EXTERNAL EMERGENCY LIGHTS AND RH OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. R&R EMERGENCY BATTERY CHARGER #4. R&R LH LOWER WING FUSELAGE AND THE RI
- [SDR JJBA20212250001](https://openairdocs.org/sdr/JJBA20212250001), Feb 25, 2021: SEAT FRAME. CRACKED. SEAT 23A AISLE SIDE FRAME CRACKED. REMOVED AND REPLACED PAX SEAT 23A.
- [SDR JJBA20201226029](https://openairdocs.org/sdr/JJBA20201226029), Dec 26, 2020: LAMP. INOPERATIVE. LT FORWARD EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R LT FORWARD EXTERNAL EMERGENCY LIGHT LAMP. OPERATIONS CHECK SATISFACTORY.
- [SDR JJBA202002174006](https://openairdocs.org/sdr/JJBA202002174006), Feb 14, 2020: MUFFLER. TORN. STRONG BURNING SMELL FROM BEHIND CREW CLOSET/CABIN. R&R #1 DUAL TEMPERATURE CONTROL VALVE. OPS CHECK FAILED, BURNING SMELL PERSISTS. REMOVED AIR CYCLE MACHINE F
- [SDR JJBA202002141003](https://openairdocs.org/sdr/JJBA202002141003), Feb 11, 2020: CLAMP. LEAKING. ENGINE #2 BLEED LEAK IN FLIGHT. PERFORMED NITROGEN LEAK CHECK OF RH BLEED AIR DUCTS. FOUND LEAK AT DUCTS/CLAMPS AFT OF BLEED VALVE, BETWEEN BLEED VALVE & PRECOO
- [SDR JJBA201908074001](https://openairdocs.org/sdr/JJBA201908074001), Aug 4, 2019: ENGINE. SPARKS. DURING E1 START SPARKS/FLAMES REPORTED COMING FROM BOTTOM/FRONT OF ENGINE BY OUTER AIRCRAFT. NO INDICATIONS NOTED IN COCKPIT. FOUND E1 ATS DAMAGED AND NR 1 ENGI
- [SDR JJBA20190105016](https://openairdocs.org/sdr/JJBA20190105016), Jan 5, 2019: SUPPORT. CRACKED. CRACK IN RT OMEGA BEAM I/B SUPPORT AFT SECTION BETWEEN FR 47-48. REMOVED AND REPLACED RT OMEGA BEAM I/B SUPPORT AFT SECTION BETWEEN FR 47-48.
- [SDR JJBA20190105015](https://openairdocs.org/sdr/JJBA20190105015), Jan 5, 2019: FITTING. CRACKED. CRACK IN SHEAR CLIP FR 80 BETWEEN STR 6-7L. INSTALLED NEW SHEAR CLIP FR 8 BETWEEN STR 6-7L.
- [SDR JJBA20190105014](https://openairdocs.org/sdr/JJBA20190105014), Jan 5, 2019: FITTING. CRACKED. CRACK IN SHEAR CLIP FR 73 BETWEEN STR 8-9R. REMOVED AND REPLACED SHEAR CLIP FOR FR 73 STR 8-9R.
- [SDR JJBA20190105013](https://openairdocs.org/sdr/JJBA20190105013), Jan 5, 2019: FITTING. CRACKED. CRACK IN SHEAR CLIP FR 65 BETWEEN STR 7-9L. REMOVED AND REPLACED SHEAR CLIP FR65 BETWEEN STR 7-9L AND RESTORED FINISH.
- [SDR JJBA20190105012](https://openairdocs.org/sdr/JJBA20190105012), Jan 5, 2019: FITTING. CRACKED. CRACK IN SHEAR CLIP FR 65 BETWEEN STR 18-19L. REMOVED AND REPLACED SHEAR CLIP AT FR 65 BETWEEN STR 18L - STR 19L.
- [SDR JJBA20190105010](https://openairdocs.org/sdr/JJBA20190105010), Jan 5, 2019: SKIN. DENTED. DENT BELOW GPU DOOR REQUIRES PERMANENT REPAIR WITHIN 4000 FC. INSTALLED DOUBLER, BELOW GPU DOOR, FR 6 + 4.5", STR 15L
- [SDR JJBA20190105009](https://openairdocs.org/sdr/JJBA20190105009), Jan 5, 2019: FRAME. CRACKED. CRACK IN FR 72 BETWEEN STR 16-17L. REPAIRED FR 72 BETWEEN STR 16-17L.
- [SDR JJBA20190105008](https://openairdocs.org/sdr/JJBA20190105008), Jan 5, 2019: SUPPORT. CRACKED. CRACK IN RT OMEGA BEAM O/B SUPPORT AFT SECTION BETWEEN FR 47-48. REMOVED AND REPLACED RT OMEGA BEAM O/B SUPPORT AFT SECTION BETWEEN FR 47-50.
- [SDR JJBA20190105007](https://openairdocs.org/sdr/JJBA20190105007), Jan 5, 2019: HINGE FITTING. DEFECTIVE. LT ELEVATOR I/B HINGE FITTING BEARING ROTATING IN HOUSING. REMOVED WORN LT ELEVATOR I/B HINGE FITTING AND INSTALLED NEW LT ELEVATOR HINGE FITTING.
- [SDR JJBA20190105006](https://openairdocs.org/sdr/JJBA20190105006), Jan 5, 2019: FITTING. CRACKED. CRACK IN SHEAR CLIP FR 72 BETWEEN STR 17L - 18L. REMOVED AND REPLACED THE SHEAR CLIP BETWEEN STRINGER 17L - 18L ON FRAME 72.
- [SDR JJBA20190104005](https://openairdocs.org/sdr/JJBA20190104005), Jan 4, 2019: THRESHOLD. CORRODED. CORROSION IN CARGO DOOR THRESHOLD BEAM BETWEEN FR 65-68. REMOVED AND REPLACED AFT CARGO THRESHOLD BEAM FROM FR 65- FR 68. CORROSION FOUND TO BE LEVEL 2.
- [SDR JJBA20181229028](https://openairdocs.org/sdr/JJBA20181229028), Dec 29, 2018: TRUNNION. CORRODED. LT MLG FWD UPPER TRUNNION HAS CORROSION. REMOVED AND REPLACED LT MLG FWD UPPER TRUNNION FITTING.
- [SDR JJBA20181226027](https://openairdocs.org/sdr/JJBA20181226027), Dec 26, 2018: DOUBLER. CORRODED. CORROSION IN FR.65 AT LOWER CARGO DOOR STOP. INSTALLED SPLICE DOUBLER AT FR 65 BETWEEN STR 14L - STR 15L.
- [SDR JJBA20181226026](https://openairdocs.org/sdr/JJBA20181226026), Dec 26, 2018: FLOOR SUPPORT. CORRODED. RT OMEGA BEAM FR 59 - FR 61 TOP AND BOTTOM NUT PLATE HOLES HAVE CORROSION. REPAIRED RT OMEGA BEAM FR 59 - FR 61 TOP AND BOTTOM NUT PLATE HOLES. CORROSION FOUND 
- [SDR JJBA20181222025](https://openairdocs.org/sdr/JJBA20181222025), Dec 22, 2018: FITTING. CORRODED. CORROSION IN LATERAL "L" SHAPE FR.65 AT LOWER DOOR STOP. REPAIRED "L" SHAPE (SHEAR CLIP) PARTIAL AT FR 65 BETWEEN STR 15L - STR 18L. CORROSION FOUND TO BE LEVEL
- [SDR JJBA20181213024](https://openairdocs.org/sdr/JJBA20181213024), Dec 13, 2018: FLOOR SUPPORT. CORRODED. LT OMEGA BEAM CENTER AISLE FLOOR FLANGE CORRODED BETWEEN FRAMES 22/23 AS MARKED. CUT OUT, FABRICATED AND INSTALLED REPAIR DOUBLER ON LT OMEGA BEAM BETWEEN FRAME
- [SDR JJBA2018061904005](https://openairdocs.org/sdr/JJBA2018061904005), May 4, 2018: CONTROLLER. FAULTY. DURING CLIMBOUT, IN AUTO PRESSURIZATION. THE CABIN ALTITUDE RAPIDLY CLIMBED AND REACHED 11,000 FT. IN MANUAL MODE CREW MANUALLY WERE ABLE TO BRING CABIN ALTITUD
- [SDR JJBA20180424007](https://openairdocs.org/sdr/JJBA20180424007), Apr 24, 2018: RELAY. MALFUNCTIONED. BAGG EXT BTL INOPERATIVE MESSAGE ON EICAS IN FLIGHT. R & R RELAY K0625. MESSAGE EXTINGUISHED. R & R TOP AND BOTTOM EXTINGUISHER BOTTLES. LEAK CHECK SAT.
- [SDR JJBA20180423006](https://openairdocs.org/sdr/JJBA20180423006), Apr 23, 2018: WARNING MESSAGE. FALSE ACTIVATION. BAGG EXT BTL INOP MSG IN FLIGHT. PERFORMED SYS OPS CHECK OPS CHECK SAT
- [SDR JJBA2018042300005](https://openairdocs.org/sdr/JJBA2018042300005), Apr 21, 2018: EXTINGUISHER. INOPERATIVE. CARGO FIRE EXTINGUISHER BOTTLE INOPERATIVE CAUTION MESSAGE APPEARED AND DISAPPEARED AFTER 10 MINUTES. EXTINGUISGHER BUTTON ILLUMINATED. R & R THE FIRE BOTTLE. O
- [SDR JJBA20170918029](https://openairdocs.org/sdr/JJBA20170918029), Sep 18, 2017: SKIN. DAMAGED. DAMAGE FOUND ON THE FUSELAGE, AFT OF THE PAX DOOR.
- [SDR JJBA20170601001](https://openairdocs.org/sdr/JJBA20170601001), Jun 1, 2017: BULB. INOPERATIVE. EMERGENCY LIGHT OVER EXIT AT ROW 18 INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.
- [SDR JJBA20170106011](https://openairdocs.org/sdr/JJBA20170106011), Jan 6, 2017: ENGINE. OIL CONSUMPTION. LAVATORY SMOKE WARNING INFLIGHT. OIL CONSUMPTION ISSUE HAS BLED INTO THE PACK SYSTEM. R & R NR 2 ENGINE OPS & LEAK CHECK SAT.
- [SDR ASOA20160119006C](https://openairdocs.org/sdr/ASOA20160119006C), Jan 19, 2016: COFFEEMAKER. ODOR. THE CREW REPORTED A BURNING ODOR FROM THE COFFEE POTS. MAINTENANCE INSPECTED AND FOUND ELECTRICAL RESET NO LONGER ATTACHED TO TOP OF COFFEE BREWER. THE NR 1 COF
- [SDR ASOA20141228158](https://openairdocs.org/sdr/ASOA20141228158), Dec 28, 2014: ENGINE. LEAKING. THE CREW REPORTED SMOKE IN THE CABIN WHEN PACK 2 WAS IN OPERATION. THE ACFT LANDED AT DEPARTURE WITHOUT INCIDENT WHERE MAINTENANCE R & R THE NR 2 ENGINE, DECONT
- [SDR ASOA20140823096](https://openairdocs.org/sdr/ASOA20140823096), Aug 23, 2014: SKIN. DAMAGED. ACFT WAS FOUND TO HAVE A GOUGE ON FUSELAGE SKIN UNDER THE NR 2 ENGINE. MAINTENANCE CUTOUT THE DAMAGE AREA UNDER NR 2 ENGINE FROM FRAMES 68 TO 70 STRINGER 14R. F
- [SDR ASOA20140416063](https://openairdocs.org/sdr/ASOA20140416063), Apr 16, 2014: INVERTER. INOPERATIVE. DURING PREFLIGHT INSPECTION, CREW REPORTED EMERGENCY LIGHTS, IN GALLEY WERE NOT WORKING. MAINTENANCE R & R THE LOWER INVERTER, OPS TESTED WITH NO DEFECTS, AND T
- [SDR ASOA20140317029](https://openairdocs.org/sdr/ASOA20140317029), Mar 17, 2014: BEAM. CORRODED. DURING C-CHECK. CARGO DOOR LOWER CUT OUT CORRODED BETWEEN FRAMES 65-68. R & R CARGO DOOR LOWER BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131227464](https://openairdocs.org/sdr/ASOA20131227464), Dec 27, 2013: LIGHT. INOPERATIVE. FORWARD PARTITION EMERGENCY LIGHT OUT. R & R EMEGENCY LIGHT. OPS CHECKED GOOD.
- [SDR ASOA20120919081](https://openairdocs.org/sdr/ASOA20120919081), Sep 19, 2012: VALVE. TORN. AIR RETURN, TOWER REPORTED WHITE VAPOR STREAMING OF RT WING ON CLIMB OUT WITH CREW NOTING FUEL IMBALANCE DEVELOPING. MX R & R THE RT WING OTBD FLAP VALVE WITH L
- [SDR ASOA20120808126T](https://openairdocs.org/sdr/ASOA20120808126T), Aug 5, 2012: PUMP. FAILED. NR 1 HYDRAULIC SYS OVERHEATED. R & R NR 1 ENGINE DRIVEN PUMP.
- [SDR C2XA11RI161](https://openairdocs.org/sdr/C2XA11RI161), Oct 5, 2011: PRESSURE SWITCH. FAULTY. FLT 4174 RIC-CREW REPORTED RUDDER SYSTEM NR 1 INOP MESSAGE ON EICAS DURING TAKEOFF ROLL LESS THAN 40 KTS AND ABORTED TAKEOFF WITHOUT INCIDENT. RIC MX REMOVED AN
- [SDR C2XA11CL091](https://openairdocs.org/sdr/C2XA11CL091), Apr 9, 2011: SMOKE DETECTOR. NO TEST. CLE FLT 2528 THE CREW REPORTED THE LAV SMOKE DETECTOR WOULD NOT TEST. MAINTENANCE REPLACED THE LAV SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11IA067](https://openairdocs.org/sdr/C2XA11IA067), Apr 4, 2011: SMOKE DETECTOR. DEFECTIVE. SAV - FLIGHT 2334, DURING CRUISE INSPECTION THE CREW REPORTED A LAV SMOKE INDICATION ON EICAS. THE AIRCRAFT LANDED AT SAV WITHOUT INCIDENT WHERE CONTRACT MAINTE
- [SDR C2XA11RI011](https://openairdocs.org/sdr/C2XA11RI011), Jan 15, 2011: CONTROL PANEL. INOPERATIVE. FLIGHT 2050 - RIC - FLIGHT CREW REPORTED "LAV SMOKE" ON EICAS WITH ALARM, BUT NO SMOKE OR ODOR NOTICED. ALARM WENT AWAY AFTER ABOUT 1 MINUTE. RIC MX INSPECTED W
- [SDR C2XA10SH439](https://openairdocs.org/sdr/C2XA10SH439), Dec 28, 2010: SMOKE DETECTOR. FALSE ACTIVATION. LAV SMOKE DETECTOR FAIL MESSAGE ON EICAS. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW AMM 26-14-01 & TASK CARD 6271001. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FO
- [SDR C2XA10RI0142](https://openairdocs.org/sdr/C2XA10RI0142), Nov 29, 2010: SMOKE WARNING. FALSE ACTIVATION. FLIGHT 2345 - EWR - FLIGHT CREW REPORTED MOMENTARILY FALSE LAV SMOKE INDICATION ON EICAS. EWR MX RESET THE SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. 
- [SDR C2XA10CL163](https://openairdocs.org/sdr/C2XA10CL163), Oct 31, 2010: CONTROLLER. FAULTY. CLE - FLT 2635 THE CREW REPORTED THE CABIN PRESSURE CLIMBED TO 9200FT IN AUTO MODE AT 36000FT. MAINTENANCE INSPECTED AND REPLACED THE CABIN PRESSURIZATION CONTR
- [SDR C2XA09RI201](https://openairdocs.org/sdr/C2XA09RI201), Dec 3, 2009: SPLICE. DAMAGED. FLIGHT 2236 - EWR - FLIGHT CREW REPORTED SPARKS COMING FROM CAPTAIN INSTRUMENTS. EWR MX REPAIRED WIRE SPLICES 2160 AND SP 2163 AND PERFORMED OPERATIONAL CHECK S
- [SDR C2XA09RI173](https://openairdocs.org/sdr/C2XA09RI173), Oct 9, 2009: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 2964 - EWR - FLIGHT CREW REPORTED AIR GROUND FAIL INDICATION ON EICAS. EWR MX RESET THE SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APP
- [SDR C2XA09IA075](https://openairdocs.org/sdr/C2XA09IA075), Mar 12, 2009: SOLENOID VALVE. FAULTY. DURING CLIMB THE CREW NOTED ABNORMAL NOISE AT THE NOSE LANDING GEAR WHEN THE WAS SELECTED TO RETRACT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. 
- [SDR C2XA08CL129](https://openairdocs.org/sdr/C2XA08CL129), Dec 11, 2008: SUMP. LEAKING. IAH FLIGHT NR 2249 THE CREW REPORTED A LAV SMOKE WARNING IN FLIGHT. THE CABIN FILLED WITH SMOKE MINUTES AFTER TAKEOFF. THE ACFT RETURNED TO IAH AND LANDED WITHO
- [SDR C2XA08RI169](https://openairdocs.org/sdr/C2XA08RI169), Nov 10, 2008: PANEL. DEFECTIVE. FLIGHT 2761 - EWR - FLIGHT CREW REPORTED LAV SMOKE INDICATION ON EICAS DURING CLIMBING, BUT NO SMOKE NOTICED. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTION PA

All 57: https://openairdocs.org/aircraft/N14204/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/N14204/stcs.md

## Related

- Other Embraer EMB-145XR aircraft: https://openairdocs.org/model/embraer-emb-145xr/aircraft.md
- The Rolls-Royce AE-3007A1E engine: https://openairdocs.org/engine/rolls-royce-ae-3007a1e.md

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.