# N14116: 2002 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: 145672
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2005
- Certificate issued: February 23, 2018
- Expires: February 29, 2028
- Mode S code: A0A901
- 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=14116
- Page: https://openairdocs.org/aircraft/N14116

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/N14116/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 N14116.

## FAA accident and incident reports

None matched to N14116.

## Service difficulty reports (59, 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 RAIA2019062950002](https://openairdocs.org/sdr/RAIA2019062950002), Jun 25, 2019: HINGE. CRACKED. RH O/B FLAP SHROUD AFT HINGE IS CRACKED @ O/B END. REMOVED RH O/B FLAP SHROUD. REMOVED & REPLACED RH OB FLAP SHROUD HINGE. INSTALLED RH O/B FLAP LOWER SHROUD.
- [SDR RAIA2019062950001](https://openairdocs.org/sdr/RAIA2019062950001), Jun 25, 2019: HINGE. CRACKED. LH I/B FLAP SHROUD FWD HINGE IS CRACKED AT O/B END. REMOVED LH INBD FLAP SHROUD. REMOVED & REPLACED LH I/B FLAP SHROUD FWD HINGE. INSTALLED LH INBD FLAP SHROUD.
- [SDR RAIA2019021500001](https://openairdocs.org/sdr/RAIA2019021500001), Feb 10, 2019: DUCT. RUPTURED. WING ANTI-ICE VALVE FAIL. INSPECTED BLEED SYSYEM AND FOUND PACK 1 DUCT RUPTURED. DEFERED PACK 1. R & R PACK 1 ACM EXHAUST DUCTING. OPS AND LEACK CHECK GOOD.
- [SDR RAIA201901040001](https://openairdocs.org/sdr/RAIA201901040001), Jan 4, 2019: DISPLAY. MALFUNCTIONED. SMOKE COMMING OUT OF TOP OF GLARESHIELD, SMELLS ELECTRICAL. (FOUND TO BE NR 2 MFD). DEFERED NR 2 MFD. R&R NR 2 MFD. OPS CHECK GOOD.
- [SDR RAIA201810100001](https://openairdocs.org/sdr/RAIA201810100001), Oct 10, 2018: LINE. LEAKING. BLEED 2 OVERTEMP. FOUND AIRLINE TO LOW TEMP THERMOSTAT TO BE LEAKING. R&R OF SUPPLY LINE. OPS AND LEAKS CHECKS GOOD AT THIS TIME.
- [SDR RAIA201807010002](https://openairdocs.org/sdr/RAIA201807010002), Jul 1, 2018: ROLLER. OUT OF ADJUST. MAIN CABIN DOOR DIFFICULT TO OPEN. ADJUSTED DOOR ROLLERS, OPS CHECK GOOD.
- [SDR RAIA201805180001](https://openairdocs.org/sdr/RAIA201805180001), May 18, 2018: ACTUATOR. FAULTY. AIRCRAFT REPORTED RUDDER SHAKING VIOLENTLY/VIBRATING. R&R RUDDER ACTUATOR. OPS CHECK PENDING ARRIVAL OF NEW BUSHING. OPS CHECK GOOD. WILL UPDATE LATER WITH INFO
- [SDR RAIA201804060002](https://openairdocs.org/sdr/RAIA201804060002), Apr 6, 2018: WARNING MESSAGE. ILLUMINATED. BLEED OVERTEMP BOTH ENGINES IN ICING CONDITIONS. PERFORMED HIGH POWER BLEED TEST WITH FLIGHT CREW, COULD NOT DUPLICATE. OPS CHECKED GOOD.
- [SDR RAIA201801030001](https://openairdocs.org/sdr/RAIA201801030001), Jan 3, 2018: LIGHT. CONTAMINATED. RIGHT FWD WING TO FUSELAGE FAIRING EXTERIOR FLOOD LIGHT INOPERATIVE. FOUND MOISTURE INSIDE THE LIGHT COVER. R & R THE LIGHT ASSEMBLY. R & R THE NR 2 EMERGENCY B
- [SDR RAIA201710200001](https://openairdocs.org/sdr/RAIA201710200001), Oct 20, 2017: BULB. INOPERATIVE. EMERGENCY AISLE FLOOD LIGHT AT ROW 3 IS INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.
- [SDR RAIA201707150001](https://openairdocs.org/sdr/RAIA201707150001), Jul 15, 2017: BEARING. FAILED. SMOKE AND ACRID ODOR ENROUTE IN COCKPIT. INSPECTED AND FOUND BEARING FAILED ON THE NR 1 PACK. REMOVED AND REPLACED THE NR 1 AIR CYCLE MACHINE, OPS CHECKED GOOD.
- [SDR RAIA201603290001](https://openairdocs.org/sdr/RAIA201603290001), Mar 29, 2016: FLASHLIGHT. INOPERATIVE. F/O FLASHLIGHT NOT INDICATING CHARGING. REMOVED LIGHT CLEANED CONTACTS AND REINSTALLED. OPS CHECK GOOD.
- [SDR RAIA201601030001](https://openairdocs.org/sdr/RAIA201601030001), Jan 3, 2016: A/C PACK. LOCKED. VISUAL SMOKE IN THE COCKPIT AFTER ENGINE START UP AND PACKS RESET. INSPECTED AND FOUND NR 2 PACK COOLING TURBINE FAILED TO TURN WITH PACK VALVE OPEN, TURBINE LO
- [SDR RAIA201508250001](https://openairdocs.org/sdr/RAIA201508250001), Aug 25, 2015: BULB. INOPERATIVE. PAX DOOR EMERGENCY LIGHT NR 1 INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECKED GOOD.
- [SDR RAIA201508040001](https://openairdocs.org/sdr/RAIA201508040001), Aug 4, 2015: GROUND WIRE. BROKEN. SERVICE DOOR EMERGENCY FLOOD LIGHT NR 5 INOPERATIVE. MAINTENANCE REPAIRED BROKEN GROUND WIRE, OPS CHECK GOOD.
- [SDR RAIA201506120001](https://openairdocs.org/sdr/RAIA201506120001), Jun 12, 2015: BULB. INOPERATIVE. EMERGENCY LIGHT OVER ROW 18 WILL NOT ILLUMINATE ON AFT SIDE. MAINTENANCE REPLACED THE BULB, OPS CHECKED GOOD.
- [SDR ASOA20141217118](https://openairdocs.org/sdr/ASOA20141217118), Dec 12, 2014: SKIN. CRACKED. LEFT REAR FUSELAGE SKIN CRACKED FRAMES 77, 78 AND 79. REPAIRED IAW ETD2014-145-101077-A.
- [SDR ASOA20130120241](https://openairdocs.org/sdr/ASOA20130120241), Jan 20, 2013: WEB. CORRODED. ACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND AT A SCREW HOLE IN CLOSEOUT WEB AT FRAME 65 AT CARGO DOOR CUTOUT. MX REMOVED CORROSION AND FABRICATED A NEW PA
- [SDR ASOA20130120240](https://openairdocs.org/sdr/ASOA20130120240), Jan 20, 2013: STRINGER. CORRODED. ACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND BETWEEN FRAMES 59 AND 60 AT STRINGER 19L. MX BLENDED CORROSION (.018) MATERIAL LOSS. FABRICATED A NEW PART, AL
- [SDR ASOA20130120239](https://openairdocs.org/sdr/ASOA20130120239), Jan 20, 2013: SKIN. CORRODED. A/C IN FOR A C-CHECK WHEN CORROSION WAS FOUND BETWEEN FRAMES 68 AND 69 AND STRINGER 21L AND 22R. MX FABRICATED, DRILL A NEW DOUBLER AND INSTALL IAW ETD2013-145-
- [SDR ASOA20130120238](https://openairdocs.org/sdr/ASOA20130120238), Jan 20, 2013: SHEAR TIE. CORRODED. ACFT IN FOR A C-CHECK WHEN CORROSION WAS FOUND ON DOUBLER AT FRAME 65 AT CARGO DOOR CUTOUT. MX REMOVED THE CORRODED SHEAR FOOT IAW SRM 51-40-02. REPLACED NEW SH
- [SDR ASOA20130113230](https://openairdocs.org/sdr/ASOA20130113230), Jan 13, 2013: DOOR FRAME. CORRODED. FORWARD LOWER CORNER SERVICE DOOR CUT-OUT CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SERVICE DOOR FRAME.
- [SDR ASOA20130113229](https://openairdocs.org/sdr/ASOA20130113229), Jan 13, 2013: ATTACH ANGLE. CORRODED. CARGO DOOR CUT-OUT LOWER BEAM ATTACH ANGLE FRAME 65 CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R ANGLE.
- [SDR ASOA20130113228](https://openairdocs.org/sdr/ASOA20130113228), Jan 13, 2013: SILL. CORRODED. LT SILL FRAME 46 IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SILL.
- [SDR ASOA20130113227](https://openairdocs.org/sdr/ASOA20130113227), Jan 13, 2013: BEAM. CORRODED. CARGO DOOR CUT-OUT LOWER BEAM FRAME 65 TO 68 CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R LOWER BEAM.
- [SDR ASOA20120521048](https://openairdocs.org/sdr/ASOA20120521048), May 21, 2012: UNKNOWN. ODOR. THE CREW REPORTED STRONG BURNING ODOR COMING FROM ROW 17-19. MX INSPECTED AND PERFORMED ENGINE RUNS WITH BOTH PACKS SYS ON. NO ODOR WAS NOTED. THE ACFT RELEASED
- [SDR ASOA20120403048](https://openairdocs.org/sdr/ASOA20120403048), Apr 3, 2012: INVERTER. INOPERATIVE. THE CREW REPORTED THE RT CABIN FORWARD LOWER EMERGENCY EXIT IDENTIFIER WAS FOUND TO BE INOPERATIVE. MX R & R THE NR 3 EMERGENCY LIGHT INVERTER, OPS TESTED WITH 
- [SDR C2XA11CL177](https://openairdocs.org/sdr/C2XA11CL177), Jul 28, 2011: BATTERY. OVERTEMP. SDF FLT 6074 THE CREW REPORTED A BATTERY NR 2 EICAS WARNING MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 AND NR 2 BATTERY. OPERATIONAL CHECKS 
- [SDR C2XA11RI096](https://openairdocs.org/sdr/C2XA11RI096), May 25, 2011: SMOKE WARNING. INOPERATIVE. FLIGHT 2761 - RIC - FLIGHT CREW REPORTED LAV SMOKE TEST INOPERATIVE. RIC MX MEL`ED THE SYSTEM. EWR MX PERFORMED OPERATIONAL CHECK SEVERAL TIMES SUCCESSFULLY. AC
- [SDR C2XA11RI072](https://openairdocs.org/sdr/C2XA11RI072), May 6, 2011: WIRE. BROKEN. EWR MX - DURING ROUTINE MAINTENANCE, EWR MX FOUND LAV SMOKE DET TEST INOPERATIVE. EWR MX REPAIRED BROKEN WIRE W743-8019-22 AND CONNECTOR P8200. MX PERFORMED OPE
- [SDR C2XA11SH022](https://openairdocs.org/sdr/C2XA11SH022), Feb 4, 2011: ANTI-ICE VALVE. ACTIVATED. DURING FLT NR 2035, AT CRUISE, THE AIR CREW RECEIVED AN ENGINE 1 ANTI-ICE FAIL MESSAGE. THE FLIGHT WAS DIVERTED TO SHV AND LANDED WITHOUT INCIDENT. MAINTENANCE 
- [SDR C2XA10IA164](https://openairdocs.org/sdr/C2XA10IA164), May 31, 2010: INVERTER. INOPERATIVE. IAH - FLIGHT 2917, THE CREW REPORTED THE RIGHT EXIT DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE INVERTER, OPERATION
- [SDR C2XA09IA260](https://openairdocs.org/sdr/C2XA09IA260), Oct 16, 2009: INVERTER. INOPERATIVE. MCI - DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT LIGHT ON THE AFT GALLEY BULKHEAD WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER
- [SDR C2XA09SH286](https://openairdocs.org/sdr/C2XA09SH286), Aug 18, 2009: BRACKET. DAMAGED. SHV - DURING C-CHECK RT AILERON DAMPER BRACKET ON AILERON DAMAGED. MAINTENANCE REMOVED AND REPLACED RT AILERON DAMPER INBOARD BRACKET IAW EMB-145 SRM 51-40-02. 
- [SDR C2XA09SH285](https://openairdocs.org/sdr/C2XA09SH285), Aug 18, 2009: ATTACH BRACKET. GOUGED. SHV - DURING C-CHECK RT AILERON PCA ATTACHMENT BRACKET ON AILERON IS GOUGED. MAINTENANCE REMOVED AND REPLACED RT AILERON PCA ATTACHMENT BRACKET IAW EC5750-01177
- [SDR C2XA09SH284](https://openairdocs.org/sdr/C2XA09SH284), Aug 18, 2009: FITTING. WORN. SHV - DURING C-CHECK RT GROUND SPOILER O/B HINGE I/B HAT BUSHING IS MIGRATED. MAINTENANCE REMOVED AND REPLACED RT GROUND SPOILER O/B FITTING IAW EMB-145 AMM 57-
- [SDR C2XA09RI121](https://openairdocs.org/sdr/C2XA09RI121), Jun 22, 2009: DOOR. OUT OF ADJUST. FLIGHT CREW REPORTED MAIN PAX DOOR HARD TO OPEN AND CLOSE. MX ADJUSTED, CLEANED AND LUBED MAIN PAX DOOR AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED 
- [SDR C2XA08IA145](https://openairdocs.org/sdr/C2XA08IA145), Jun 24, 2008: CONTROL PANEL. SHORTED. FLIGHT 2885 - THE FLIGHT CREW REPORTED A BURNING SMELL EMANATING FROM THE FLIGHT DIRECTOR PANEL. THE PANEL WAS REPLACED. OPERATIONALLY TESTED AND THE DISCREPANC
- [SDR C2XA08TY051](https://openairdocs.org/sdr/C2XA08TY051), May 18, 2008: SEAL. LEAKING. LAV SMOKE DETECTOR WENT OFF ON SHORT FINAL AND WENT AWAY AFTER LANDING/IDLE SET. FOUND ENGINE NR 1 ZERO BEARING SEAL LEAKING. AIRCRAFT STILL IN MAINTENANCE.
- [SDR C2XA08IA119](https://openairdocs.org/sdr/C2XA08IA119), Apr 28, 2008: UNKNOWN. ODOR. IAH - FLIGHT 2096, THE CREW REPORTED A NOTICEABLE SCENT PF JET FUEL WHEN THRUST LEVERS ADVANCED FOR T/O WITH THE PACKS ON, APU BLEED OPEN, AND ENGINE BLEEDS OFF
- [SDR C2XA08IA110](https://openairdocs.org/sdr/C2XA08IA110), Apr 13, 2008: UNKNOWN. ODOR. IAH - FLIGHT 2121, ON TAKEOFF THE CREW REPORTED A FUEL ODOR THAT GOES AWAY WHEN SWITCHING FROM APU BLEED TO ENGINE BLEED. THE AIRCRAFT LANDED AT IAH WITHOUT INC
- [SDR C2XA08IA074](https://openairdocs.org/sdr/C2XA08IA074), Mar 1, 2008: UNKNOWN. ODOR. IAH - FLIGHT 2084, THE CREW REPORTED A STRONG FUEL ODOR AFTER TAKEOFF THAT WENT AWAY WHEN ENGINE BLEEDS WERE SELECTED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDE
- [SDR C2XA08IA050](https://openairdocs.org/sdr/C2XA08IA050), Feb 4, 2008: UNKNOWN. ODOR. IAH - FLIGHT 2428, THE CREW REPORTED STRONG FUEL SMELL ON TAKEOFF WITH APU POWERING PACKS. MAINTENANCE OPERATIONALLY CHECKED THE PACKS WITH APU BLEED AIR WITH N
- [SDR C2XA08IA048](https://openairdocs.org/sdr/C2XA08IA048), Jan 30, 2008: UNKNOWN. ODOR. IAH - FLT 2593, THE CREW REPORTED STRONG FUEL SMELL AFTER T/O APU POWERING, PACKS SMELL GOES AWAY AFTER SWITCHING PACKS TO ENG BLEED. A/C RELEASED IAW MEL 49-00
- [SDR C2XA07TY039](https://openairdocs.org/sdr/C2XA07TY039), Jul 18, 2007: INVERTER. INOPERATIVE. EMERGENCY LIGHT ABOVE SERVICE DOOR INOP. REMOVED AND REPLACED NR 3 INVERTER IAW EMB 145 XR AMM 33-50-00, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVI
- [SDR C2XA07CL045](https://openairdocs.org/sdr/C2XA07CL045), May 14, 2007: EXHAUST MIXER. FAILED. CLE FLIGHT 2541 UPON ARRIVING IN CLE FROM AUS THE NR 1 ENGINE EXHAUST MIXER ASSEMBLY WAS FOUND TO BE MISSING LARGE PIECES. THE EXHAUST CONE WAS DAMAGED AND THE 
- [SDR C2XA07RI027](https://openairdocs.org/sdr/C2XA07RI027), May 5, 2007: CONNECTOR. LOOSE. FLT 2868 - EWR - CREW REPORTED, -E2 FIRE DET FAIL-. ENGINE INDICATION NORMAL, MESSAGE APPEARED ABOVE FL 320 /OAT - 58 C. EWR MX FOUND CONNECTOR LOOSE (P0915). M
- [SDR C2XA07IA071](https://openairdocs.org/sdr/C2XA07IA071), Mar 26, 2007: COFFEEMAKER. ODOR. IAH FLIGHT 2560, THE CREW REPORTED THAT THE COFFEEMAKER HAD A BURNING SMELL IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED T
- [SDR C2XA06IA063](https://openairdocs.org/sdr/C2XA06IA063), Apr 25, 2006: CARBON SEAL. LEAKING. IAH - FLIGHT 3472, THE CREW REPORTED LAV SMOKE AT 12,000 FEET. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED T
- [SDR C2XA06IA061](https://openairdocs.org/sdr/C2XA06IA061), Apr 24, 2006: CONTROL PANEL. INOPERATIVE. IAH - FLIGHT 2738, THE CREW REPORTED A LAV SMOKE WARNING ON CLIMB WITH NO SMOKE PRESENT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENA

All 59: https://openairdocs.org/aircraft/N14116/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/N14116/stcs.md

## Earlier aircraft with N14116

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N14116 before.

- [Cancelled 1977-02-28](https://openairdocs.org/deregistered/N14116-1977-02-28): Piper PA-23-250, S/N 27-3726. Exported to Chile. Owner: [Hooten Lewis D](https://openairdocs.org/faa-owner/HOOTEN%20LEWIS%20D), [Jacksonville, IL](https://openairdocs.org/faa-place/IL/Jacksonville)
- [Cancelled 1970-04-07](https://openairdocs.org/deregistered/N14116-1970-04-07): North American T-28B, S/N 517673. Exported to Taiwan. Owner: [Winter Wolf & Co](https://openairdocs.org/faa-owner/WINTER%20WOLF%20%26%20CO), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)
- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N14116-undated): Aeronca C-3, S/N A-416, built 1934. Owner: [Aeronautical Corporation Of America](https://openairdocs.org/faa-owner/AERONAUTICAL%20CORPORATION%20OF%20AMERICA), [Cincinnati, OH](https://openairdocs.org/faa-place/OH/Cincinnati)

## 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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