# N14180: 2005 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: 14500900
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 25, 2005
- Certificate issued: June 4, 2020
- Expires: June 30, 2027
- Mode S code: A0A9F0
- 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=14180
- Page: https://openairdocs.org/aircraft/N14180

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/N14180/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 N14180.

## FAA accident and incident reports

None matched to N14180.

## Service difficulty reports (85, 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 JJBA20221121016](https://openairdocs.org/sdr/JJBA20221121016), Nov 18, 2022: ACTUATOR CABLE. JAMMED. MAIN CABIN DOOR WON'T OPEN, ACTUATING MECHANISM JAMMED. INSPECTED AND FOUND MAIN DOOR FORWARD LOCK JAMMING. ADJUSTED MAIN CABIN DOOR CABLE D TO FRONT LOCK BOX. 
- [SDR JJBA20211027060](https://openairdocs.org/sdr/JJBA20211027060), Oct 27, 2021: NONE. NONE. MCD EXTERIOR EMERGENCY LIGHT INOPERATIVE. R&R MCD EXT EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.
- [SDR JJBA20210611019](https://openairdocs.org/sdr/JJBA20210611019), Jun 11, 2021: SKIN. DENTED. LH WING INBD LEADING EDGE HAS A DENT. ACCOMPLISHED PERMANENT REPAIR TO THE LEFT HAND WING LEADING EDGE 1 BY REMOVING DAMAGE, NDT PERFORMED. FABRICATED AND INSTA
- [SDR JJBA20210607013](https://openairdocs.org/sdr/JJBA20210607013), Jun 7, 2021: FLOOR SUPPORT. CORRODED. CABIN FLOOR SUPPORTS IN MIDDLE SECTION (FR 23-FR 59) POSSIBLE CORROSION. EVALUATED AREA RH FLOOR SUPPORT BTW FR 23-25, FR53-57. FOUND TO BE IN LIMIT, APPLIED AL
- [SDR JJBA20210606012](https://openairdocs.org/sdr/JJBA20210606012), Jun 6, 2021: FLOORBEAM. CORRODED. LAV FLOOR BEAMS BL 19L, BL 0, BL 19R SIGNS OF CORROSION. EVALUATED AND REMOVED CORROSION ON LAV FLOOR BEAMS. FOUND TO BE 100% OUT OF LIMITS. REMOVED AND INSTALL
- [SDR JJBA20210604011](https://openairdocs.org/sdr/JJBA20210604011), Jun 4, 2021: SEAT TRACK. DAMAGED. LH COCKPIT SEAT TRACK HAVE ELONGATED HOLES (LH AND RH SIDE) AND CHAFFED. EVALUATED LH COCKPIT SEAT TRACK. FOUND TO BE OUT OF LIMITS. COUNTER SIDE EXCEEDS THE MI
- [SDR JJBA20210602007](https://openairdocs.org/sdr/JJBA20210602007), Jun 2, 2021: FLOOR SUPPORT. CORRODED. CABIN FLOOR SUPPORTS IN FWD SECTION (FWD OF FR 23) POSSIBLE CORROSION. REMOVED CORROSION ON GUSSET AND BEAM ASTER EVAL. FOUND BOTH PARTS TO BE OUT OF LIMITS. RE
- [SDR JJBA20210522026](https://openairdocs.org/sdr/JJBA20210522026), May 22, 2021: SEAT TRACK. DAMAGED. RH COCKPIT SEAT TRACK HAVE ELONGATED HOLES (LH SIDE AND RH SIDE) AND CHAFED. REMOVED AND REPLACED 2 EA TRACKS AT RH COCKPIT (LH SIDE AND RH SIDE).
- [SDR JJBA20210519021](https://openairdocs.org/sdr/JJBA20210519021), May 19, 2021: REINFORCEMENT. CORRODED. PAX DOOR THRESHOLD REINFORCING STRUCTURE HAS CORROSION THREE DIFFERENT BRACKETS. REMOVED AND REPLACED 2 NEW BRACKETS ON PAX DOOR OUTBD BRACKETS PAINT DAMAGE ONL
- [SDR JJBA20210518019](https://openairdocs.org/sdr/JJBA20210518019), May 18, 2021: HINGE. WORN. PAX DOOR, UPPER SIDE HINGE ATTACHMENT FITTING HAS WEAR MARKS AND GAUGING. BLENDED OUT DAMAGE.
- [SDR JJBA20210518018](https://openairdocs.org/sdr/JJBA20210518018), May 18, 2021: HINGE. CRACKED. PAX DOOR, LWR SIDE HINGE ATTACHMENT FITTING HAS CRACK MARK. BLENDED OUT DAMAGE.
- [SDR JJBA20210518017](https://openairdocs.org/sdr/JJBA20210518017), May 18, 2021: FLOORBEAM. CORRODED. FRM 23, 15R, RBL 0.0'-27.0" FLOOR BOARD SUPPORT BEAM HAS CORROSION (FLOOR STRUCTURE). REMOVED AND REPLACED ANGLE (SUPPORT).
- [SDR ASOA2020031184003](https://openairdocs.org/sdr/ASOA2020031184003), Mar 8, 2020: LIGHT. OVERHEATED. IAH - FLIGHT 4328, THE CREW REPORTED CEILING LIGHT SMOKE SMELL 1A & 2A. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND
- [SDR ASOA2019041065049](https://openairdocs.org/sdr/ASOA2019041065049), Apr 6, 2019: GROUND STUD. DAMAGED. CREW REPORTED ROW 18 EMERGENCY LIGHTS WILL NOT ILLUMINATE FACING A/C FRONT BACK SIDE WORKS. MX INSPECTED AND FOUND W192-8819-22N (GROUND STUD GS8517DC) DAMAGED 
- [SDR ASOA201807095161](https://openairdocs.org/sdr/ASOA201807095161), Jul 9, 2018: INVERTER. INOPERATIVE. DURING MX INSPECTION THE LOWER EMERGENCY LIGHT ON THE SERVICE DOOR WAS INOP. MX REMOVED AND REPLACED THE NR 2 INVERTER WITH OPERATIONAL CHECK GOOD. A/C WAS APPR
- [SDR ASOA201806267116](https://openairdocs.org/sdr/ASOA201806267116), Jun 26, 2018: FITTING. CRACKED. TYS A/C CAME IN FOR A 2A INSPECTION WHEN INSPECTION FOUND THE LEFT ENGINE LOWER FWD AFT FITTING CRACKED AND VERIFIED BY NDT METHODS. MAINTENANCE REMOVED AND REP
- [SDR ASOA201702020046](https://openairdocs.org/sdr/ASOA201702020046), Feb 2, 2017: SKIN. CRACKED. DURING C-CK. FUSELAGE SKIN CRACK AT FR 75 BTW STR 2L-3L. REPAIRED FUSELAGE SKIN IAW SRM 53-31-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160912046](https://openairdocs.org/sdr/ASOA20160912046), Sep 12, 2016: COMPUTER. FAULTED. CREW REPORTED THE ACFT GOES INTO R/O AND G/A MODE DURING TAKEOFF AND ON APPROACH AND UNABLE TO SWITCH OUT OF IT. MAINTENANCE R & R IC-600 NR 2 WITH OPS CHECK GO
- [SDR ASOA20160912049C](https://openairdocs.org/sdr/ASOA20160912049C), Sep 12, 2016: COMPUTER. MALFUNCTIONED. THE CREW REPORTED THE AIRCRAFT GOES INTO A ROLL AND GA MODE DURING TAKOFF AND ON APPROACH AND UNABLE TO SWITCH OUT OF IT. MAINTENANCE INSPECTED AND REPLACED THE
- [SDR ASOA20150815045](https://openairdocs.org/sdr/ASOA20150815045), Aug 15, 2015: YOKE. CRACKED. DURING MAINTENANCE THE NR 2 ENGINE FORWARD LOWER YOKE FITTING WAS FOUND CRACKED. MAINTENANCE REPLACED THE NR 2 ENGINE YOKE FITTING IAW STS EA 26-2014-063.
- [SDR ASOA20150620059](https://openairdocs.org/sdr/ASOA20150620059), Jun 20, 2015: INVERTER. INOPERATIVE. DURING PREFLIGHT THE EXIT ROW EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO
- [SDR ASOA20150318019](https://openairdocs.org/sdr/ASOA20150318019), Mar 18, 2015: CONTROLLER. FAILED. THE CREW REPORTED WINDSHIELD HEAT NR 1 FAIL RESULTING IN ELECTRICAL OVERHEAT SMELL. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD HEAT TEMP CONTROL
- [SDR ASOA20141016114R](https://openairdocs.org/sdr/ASOA20141016114R), Oct 16, 2014: INVERTER. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE FWD EMERGENCY EXIT ROW AISLE LIGHT WOULD NOT ILLUMINATE. MX R & R THE NR 6 EMERGENCY LIGHT SYSTEM INVERTER WITH OPS CHECK GOO
- [SDR ASOA20140930083](https://openairdocs.org/sdr/ASOA20140930083), Sep 30, 2014: LIGHT. INOPERATIVE. THE CREW REPORTED OVERHEAD EMERGENCY EXIT LIGHT AT ROW 12 DID NOT ILLUMINATE DURING TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT LIGHT AT ROW 12.
- [SDR ASOA20140705092](https://openairdocs.org/sdr/ASOA20140705092), Jul 5, 2014: LIGHT. INOPERATIVE. DURING PREFLIGHT THE CREW REPORTED THAT THE EMERGENCY LIGHT WAS INOPERATIVE OVER SEAT 18C ON THE FORWARD SIDE. MAINTENANCE R & R THE AFFECTED LIGHT ASSY, OPERAT
- [SDR V0XD201405250122](https://openairdocs.org/sdr/V0XD201405250122), May 29, 2014: SKIN. DENTED. DENT ON REAR FUSELAGE SKIN, FRAME 78 STRINGER 6L. REPAIRED DENT IAW EC 5330-02473.
- [SDR V0XD2014052518021](https://openairdocs.org/sdr/V0XD2014052518021), May 28, 2014: STRUCTURE. CORRODED. WASTE DRAIN VALVE COMPARTMENT CORRODED. R & R WASTE DRAIN VALVE COMPARTMENT IAW SRM 51-40-02.
- [SDR V0XD2014052518020](https://openairdocs.org/sdr/V0XD2014052518020), May 25, 2014: FLOOR SUPPORT. CORRODED. CORROSION ON RT FLOOR SUPPORT FRAMES 41-48. R & R RT FLOOR SUPPORT IAW SRM 51-40-02, 51-40-04, 51-40-06.
- [SDR V0XD2014052518019](https://openairdocs.org/sdr/V0XD2014052518019), May 25, 2014: CHANNEL. CORRODED. SERVICE DOOR FRAME CHANNEL CORRODED AT THREE NUT PLATE LOCATIONS. R & R SERVICE DOOR FRAME CHANNEL IAW SRM 51-40-02, 51-20-03.
- [SDR V0XD2014052518018](https://openairdocs.org/sdr/V0XD2014052518018), May 25, 2014: SUPPORT. CORRODED. CORROSION ON LT SUPPORT AT FRAME 64 S15L. BLENDED CORROSION MATERIAL LOSS WAS .003" WITHIN LIMITS IAW SRM 53-31-10.
- [SDR V0XD2014052518017](https://openairdocs.org/sdr/V0XD2014052518017), May 25, 2014: BEAM. CORRODED. LAV LT BEAM CAP CORRODED. BLENDED CORROSION, REMOVED .005" OF MATERIAL LOSS. FOUND TO BE WITHIN LIMITS IAW SRM 53-24-10, WO 80225, WC 1184.
- [SDR V0XD2014052518016](https://openairdocs.org/sdr/V0XD2014052518016), May 25, 2014: CAP. CORRODED. LEFT NLG TRUNNION CAP HAS PITTING. REMOVED MINOR PITTING ON LT NLG TRUNNION CAP IAW SRM 53-11-08, WO 80225, W/C 1177.
- [SDR V0XD2014052518015](https://openairdocs.org/sdr/V0XD2014052518015), May 25, 2014: FLOOR SUPPORT. CORRODED. CORROSION ON RT FLOOR SUPPORT AFT OF FRAME 50. R & R RT FLOOR SUPPORT FROM FRAMES 48-52 IAW SRM 51-40-02, 51-20-03.
- [SDR V0XD2014052518014](https://openairdocs.org/sdr/V0XD2014052518014), May 25, 2014: FLOORBEAM. CORRODED. RT FLOORBEAM ANGLE CORRODED AT FRAME 23. R & R RT FLOORBEAM ANGLE IAW SRM 51-40-02, WO 80225, WC 1183.
- [SDR V0XD2014052518013](https://openairdocs.org/sdr/V0XD2014052518013), May 25, 2014: FLOOR SUPPORT. CORRODED. CORROSION ON LT FLOOR SUPPORT. R & R LT FLOOR SUPPORT FROM FRAMES 18 - 24 IAW SRM 51-40-02, 51-40-09, 51-20-03.
- [SDR V0XD2014052518012](https://openairdocs.org/sdr/V0XD2014052518012), May 25, 2014: FLOORBEAM. CORRODED. CORROSION UNDER LAV FLOOR PANEL 261DF ON FLOORBEAM. R & R FLOORBEAM ANGLE IAW SRM 51-40-02.
- [SDR V0XD2014052518011](https://openairdocs.org/sdr/V0XD2014052518011), May 25, 2014: FLOOR SUPPORT. CORRODED. CORROSION ON LT FLOOR SUPPORT AT FRAME 49. BLENDED CORROSION AND FOUND WITHIN LIMITS IAW SRM 53-23-10. NDT PERFORMED.
- [SDR V0XD2014052318010](https://openairdocs.org/sdr/V0XD2014052318010), May 22, 2014: FLOOR SUPPORT. CORRODED. AFT CARGO BAY FLOOR SUPPORT CORRODED AT FRAME 65. BLENDED CORROSION IAW SRM 53-31-10, FOUND TO BE WITH IN LIMITS IAW SRM 53-31-10, SWPM 20-21-00, AND CPM 51-21-
- [SDR V0XD2014052318009](https://openairdocs.org/sdr/V0XD2014052318009), May 22, 2014: SPLICE. CORRODED. FLOOR SUPPORT CONNECTION SPLICE CORRODED AT FRAME 35 UNDER FLOORBOARD 252AF. BLENDED CORRODED AREA IAW SRM 53-23-10, AREA LESS THAN 10 PERCENT MATERIAL LOSS, FO
- [SDR V0XD2014052318008](https://openairdocs.org/sdr/V0XD2014052318008), May 22, 2014: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT FROM FRAMES 24-36 IS CORRODED. REMOVED CORRODED FLOOR SUPPORT AND INSTALLED NEW IAW SRM 51-4-02, AND SWPM 20-21-00.
- [SDR V0XD2014052318007](https://openairdocs.org/sdr/V0XD2014052318007), May 22, 2014: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT FWD OF FRAME 26 LT SIDE. REMOVED CORRODED FLOOR SUPPORT AND INSTALLED NEW IAW SRM 51-40-02, 51-20-03, 51-40-06, AND SWPM 20-22-00.
- [SDR V0XD2014052318006](https://openairdocs.org/sdr/V0XD2014052318006), May 21, 2014: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM. R & R FLOORBEAM IAW SRM 51-40-02, 51-20-03 AND, 51-40-02.
- [SDR V0XD2014052318005](https://openairdocs.org/sdr/V0XD2014052318005), May 21, 2014: WINDOW FRAME. CORRODED. RIGHT WINDSHIELD ASSY FRAME IS CORRODED IN MULTIPLE AREAS. BLENDED CORRODED AREAS IAW ACMM 56-10-01, FOUND TO BE WITHIN LIMITS IAW MM 56-10-01. NDT PERFORMED, N
- [SDR V0XD2014052318004](https://openairdocs.org/sdr/V0XD2014052318004), May 20, 2014: WINDOW FRAME. CORRODED. LEFT WINDSHIELD ASSY FRAME IS CORRODED IN MULTIPLE AREAS. BLENDED CORRODED AREAS IAW ACMM 56-10-01, FOUND TO BE WITHIN LIMITS IAW ACMM 56-10-01. NDT PERFORMED, 
- [SDR ASOA20130305020R](https://openairdocs.org/sdr/ASOA20130305020R), Mar 5, 2013: WIRE. DAMAGED. CREW REPORTED THE F/O'S FLASHLIGHT WAS NOT CHARGING. MX REPAIRED THE WIRE ON THE F/O'S FLASHLIGHT CHARGER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETUR
- [SDR ASOA20121009131](https://openairdocs.org/sdr/ASOA20121009131), Oct 9, 2012: LIGHT. MALFUNCTIONED. DURING POST FLIGHT INSPECTION, CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT SHUTOFF. SWITCHES WERE CYCLED ON AND OFF AND THE LIGHTS EXTINGUISED, AND THE AC
- [SDR ASOA20120711051](https://openairdocs.org/sdr/ASOA20120711051), Jul 11, 2012: SIGN. INOPERATIVE. FWD FACING CEILING EMERGENCY SIGN OVERWING FOUND INOPERATIVE. MX R & R EMERGENCY EXIT CEILING SIGN WITH OPS CHECK SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVIC
- [SDR ASOA20120604051](https://openairdocs.org/sdr/ASOA20120604051), Jun 4, 2012: ENGINE. LEAKING. CREW REPORTED SMOKE IN THE LAVATORY. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. ENGINE LEAKING, MX REPLACED THE NR 2 ENGINE. OPS CHECKED GOOD.
- [SDR ASOA20120508095](https://openairdocs.org/sdr/ASOA20120508095), May 8, 2012: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AT FR 73, BETWEEN STR 8BR AND 9BR. MX R & R THE SHEAR TIE IAW SRM 51-10-03 AND 51-40-02.
- [SDR ASOA20120508094](https://openairdocs.org/sdr/ASOA20120508094), May 8, 2012: FLOOR SUPPORT. CRACKED. SPLICE BRACKET CRACKED AT THE LT OMEGA BEAM BETWEEN FR 16 AND 17. MX R & R THE SPLICE BRACKET IAW SRM 51-20-03 AND 51-40-02. ACFT WILL BE RELEASED AT THE END OF

All 85: https://openairdocs.org/aircraft/N14180/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/N14180/stcs.md

## Earlier aircraft with N14180

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N14180 before.

- [Cancelled 1971-12-07](https://openairdocs.org/deregistered/N14180-1971-12-07): Piper PA-23-250, S/N 27-4745. Exported to Australia. Owner: [Moody Walter](https://openairdocs.org/faa-owner/MOODY%20WALTER), [Lock Haven, PA](https://openairdocs.org/faa-place/PA/Lock%20Haven)
- [Cancelled 1935-03-31](https://openairdocs.org/deregistered/N14180-1935-03-31): Stinson SR-5A, S/N 9273-A. Owner: [John C Barstow](https://openairdocs.org/faa-owner/JOHN%20C%20BARSTOW), [Midland, MI](https://openairdocs.org/faa-place/MI/Midland)

## 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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