# N14105: 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: 145649
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2005
- Certificate issued: July 1, 2026
- Expires: July 31, 2033
- Mode S code: A0A8DD
- Registered owner: [Delux Public Charter LLC](https://openairdocs.org/faa-owner/DELUX%20PUBLIC%20CHARTER%20LLC)
- Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas)
- Owner type: LLC
- Owner's area on the map: 32.8483° N, 96.8255° W: Placed by OpenAirDocs at the center of ZIP code 75209, 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=14105
- Page: https://openairdocs.org/aircraft/N14105

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/N14105/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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB WPR10LA395](https://openairdocs.org/ntsb/WPR10LA395), Aug 10, 2010: Embraer EMB-145XR (N14105), Salt Lake City, UT, substantial damage. Probable cause: An in-flight collision with a bird while on the downwind leg of the traffic pattern during a visual approach.

## NTSB investigations on N14105 not matched to an aircraft (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB FTW77FRA06](https://openairdocs.org/ntsb/FTW77FRA06), Jan 7, 1977: N.American T-28A (N14105), Addicks, TX, destroyed

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20120725017829I](https://openairdocs.org/incident/20120725017829I), Jul 25, 2012: Embraer EMB-145XR (N14105), Chicago, IL, No damage. United express flight #5959, Chicago to memphis, was on taxi out and an American plane pulled in front of them. The pilot had to slam on the brakes and the…
- [Accident 20100810040909A](https://openairdocs.org/incident/20100810040909A), Aug 10, 2010: Embraer EMB-145XR (N14105), Salt Lake City, UT, Substantial damage. The aircraft was at 11,000 feet and approximately 5 miles west of the airport on a downwind slowing from 280 knots to 190 knots. The flight crew was receiving…

## Reports on N14105 not matched to an aircraft (1)

They name N14105, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Accident 19770107000649A](https://openairdocs.org/incident/19770107000649A), Jan 7, 1977: Namer T28A (N14105), Addicks, TX, Substantial damage. Eng failed approximately 5000FT AGL over airport. ELT not found at wreckage site.

## Service difficulty reports (55, 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 ASOA2019120264065](https://openairdocs.org/sdr/ASOA2019120264065), Nov 25, 2019: CONNECTOR. DISCONNECTED. IAH-FLIGHT 4270, THE CREW REPORTED SEVERAL INTERIOR EMERGENCY EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE RECONNECTED A CANNON PLUG ABOVE THE SERVICE DOOR CEILIN
- [SDR ASOA2019100193055](https://openairdocs.org/sdr/ASOA2019100193055), Sep 24, 2019: FITTING. LEAKING. THE CREW REPORTED HYDRAULIC #1 SYSTEM LOW QUANTITY MESSAGE IN FLIGHT. FLUID DEPLETING RAPIDLY. THE AIRCRAFT DIVERTED INTO BUF AND LANDED WITHOUT FURTHER INCICEN
- [SDR ASOA201702134007](https://openairdocs.org/sdr/ASOA201702134007), Feb 13, 2017: ENGINE. LEAKING. GPT- THE CREW REPORTED SUSPECTED OIL LEAK NR 1 & 2 ENGINES AND A STRONG BURNT OIL DOOR IN THE COCKPIT. THE AIRCRAFT LANDED IN GPT WITHOUT INCIDENT, WHERE MAINTE
- [SDR ASOA20160530038](https://openairdocs.org/sdr/ASOA20160530038), May 30, 2016: BATTERY. INOPERATIVE. DURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE SERVICE DOOR EMERGENCY LIGHT BATTERY A
- [SDR ASOA201601010020](https://openairdocs.org/sdr/ASOA201601010020), Jan 1, 2016: BATTERY. INOPERATIVE. THE CREW REPORTED CAPTAIN`S EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE CAPTAIN`S EMERGENCY FLASHLIGHT BATTERY. OPS CHECKS WERE GOOD.
- [SDR ASOA20150511023](https://openairdocs.org/sdr/ASOA20150511023), May 11, 2015: HOSE. LOOSE. CREW REPORTED SMOKE IN CABIN AFTER TAKEOFF. ACFT AIR RETURN BACK TO DEPARTURE. MAINTENANCE INSPECTED AND FOUND HOSE TO NR 1 RECIRCULATION FAN MUFFLER CAUSING CO
- [SDR ASOA20150509022](https://openairdocs.org/sdr/ASOA20150509022), May 9, 2015: BATTERY PACK. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE AFT CABIN EMERGENCY EXIT SIGN AND LT AND RT OVERWING EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. MX R & R THE NR 4 EMERGENCY 
- [SDR ASOA20140731062](https://openairdocs.org/sdr/ASOA20140731062), Jul 31, 2014: SCREW. BACKED OUT. DURING "A" CHECK, FOUND LT OVERWING EXIT JAMMED. WILL NOT OPEN MAINTANCE FOUND SCREW BACKED OUT ON TRIM. REPLACED SCREW AND PREFORMED OPS CHECK. OPS CHECK GOOD.
- [SDR ASOA20140515073](https://openairdocs.org/sdr/ASOA20140515073), May 15, 2014: BATTERY PACK. DISCHARGED. DURING A MAINTENANCE INSPECTION, EMERGENCY EXIT LIGHTS ON THE INTERIOR EXIT HATCH WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT BATTE
- [SDR ASOA20140222031H](https://openairdocs.org/sdr/ASOA20140222031H), Feb 22, 2014: SMOKE DETECTOR. FALSE ACTIVATION. THE CREW REPORTED A BAGGAGE FIRE LIGHT IN FLIGHT. THE CREW DISCHARGED THE BAGGAGE FIRE EXTINGUISHERS AND THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED
- [SDR ASOA20140222028](https://openairdocs.org/sdr/ASOA20140222028), Feb 22, 2014: SMOKE DETECTOR. FALSE ACTIVATION. THE CREW REPORTED A CARGO FIRE LIGHT IN FLIGHT. THE CREW DISCHARGED THE CARGO FIRE EXTINGUISHERS AND THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE
- [SDR ASOA20140221017](https://openairdocs.org/sdr/ASOA20140221017), Feb 21, 2014: SMOKE DETECTOR. FAULTY. CREW REPORTED THE BAGGAGE FIRE EXTINGUISHER LIGHT ILLUMINATED INFLIGHT. NO SIGN OF FIRE, BLEW BOTTLES. MAINTENANCE R & R THE BAGGAGE FIRE BOTTLES. AGAIN REPORTE
- [SDR ASOA20121005143T](https://openairdocs.org/sdr/ASOA20121005143T), Oct 4, 2012: STRUCTURE. CORRODED. CORROSION OUT OF LIMITS AFTER BLEND-OUT, AT NUT PLATE HOLES ON BOTTOM OF PAX DOOR STRUCTURE. REMOVED CORROSION AND INSTALLED NUT PLATE DOUBLERS.
- [SDR ASOA20120925140](https://openairdocs.org/sdr/ASOA20120925140), Sep 24, 2012: ENGINE. SMOKE. LAV SMOKE WARNING ON CLIMB-OUT WITH ELECTRICAL BURNING ODOR. ACFT WAS FERRIED TO FOR NR 2 ENGINE CHANGE.
- [SDR C2XA11RI179](https://openairdocs.org/sdr/C2XA11RI179), Nov 11, 2011: LIGHT. INOPERATIVE. DURING SCHEDULED MX INSPECTION ROW 12BC OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. RIC MX REMOVED AND REPLACED ROW 12BC OVERHEAD EMERGENCY EXIT 
- [SDR C2XA11IA190](https://openairdocs.org/sdr/C2XA11IA190), Aug 31, 2011: WARNING SYSTEM. FALSE ACTIVATION. DEN - FLIGHT 6158, THE CREW REPORTED AN INTERMITTENT BAGGAGE SMOKE INDICATION ON EICAS. MAINTENANCE INSPECTED THE AIRCRAFT OPERATIONALLY TESTED THE BAGGAGE SMOK
- [SDR C2XA11CL104](https://openairdocs.org/sdr/C2XA11CL104), Apr 24, 2011: PROXIMITY SWITCH. FAULTY. THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON TAKEOFF. MX INSPECTED AND REPLACED THE LT GEAR WOW PROXIMITY SWITCH. ADJUSTED ALL MAIN GEAR WOW PROX
- [SDR C2XA11IA061](https://openairdocs.org/sdr/C2XA11IA061), Mar 25, 2011: ELECTRONIC UNIT. INOPERATIVE. IAH - FLIGHT 2025 THE CREW REPORTED A LANDING GEAR AIR / GRND FAIL MESSAGE ON CLIMBOUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENAN
- [SDR C2XA11IA058](https://openairdocs.org/sdr/C2XA11IA058), Mar 21, 2011: ELECTRONIC UNIT. DEFECTIVE. IAH - FLIGHT 2405, DURING CRUISE FLIGHT, THE CREW REPORTED A LANDING GEAR AIR / GROUND FAIL MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHO
- [SDR C2XA11SHO55](https://openairdocs.org/sdr/C2XA11SHO55), Mar 5, 2011: PANEL. OPEN. FLIGHT 3157, AC N14105, IAH TO SLC TWO PANELS OPENED IN FLIGHT ON RT LOWER ENGINE COWLING. SLC MAINTENANCE ADJUSTED OIL SERVICE DOOR HINGE TO ALLOW CLOSURE OF D
- [SDR C2XA10RI129](https://openairdocs.org/sdr/C2XA10RI129), Oct 15, 2010: DOOR. OUT OF ADJUST. FLIGHT 2985 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR HARD TO OPEN. EWR MX ADJUSTED AND LUBED THE MAIN CABIN DOOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULL
- [SDR C2XA10TY148](https://openairdocs.org/sdr/C2XA10TY148), Sep 19, 2010: SKIN. DAMAGED. AIRCRAFT HIT A FLOCK OF SEAGULLS AT 11000 FT. AIRCRAFT SUFFERED A BIRD STRIKE TO THE FWD FUSELAGE DAMAGING THE UPPER SKINS AND SUPPORTING STRUCTURE BETWEEN FRM 
- [SDR C2XA10TY029](https://openairdocs.org/sdr/C2XA10TY029), Feb 17, 2010: SKIN. DENTED. DENT ON FUSELAGE UNDER STR 11L BETWEEN FRM 19-20. CUT OUT DAMAGE, FABRICATED FILLER & DOUBLER AND INSTALLED IAW ETD2010-145/01128.
- [SDR C2XA10TY018](https://openairdocs.org/sdr/C2XA10TY018), Jan 23, 2010: ENGINE. MALFUNCTIONED. MSP - EWR ON CLIMBOUT THRU APPROX 14000 TO APPROX 24000 AN ACRID BURNING SMELL THOUGHT TO BE COMING FROM THE PACKS - COULD NOT ISOLATE WHICH PACK - SMELL THEN D
- [SDR C2XATY](https://openairdocs.org/sdr/C2XATY), Jan 23, 2010: ENGINE. MALFUNCTIONED. MSP - EWR ON CLIMBOUT THRU APPROX 14000 TO APPROX 24000 AN ACRID BURNING SMELL THOUGHT TO BE COMING FROM THE PACKS - COULD NOT ISOLATE WHICH PACK- SMELL THEN DI
- [SDR C2XA09RI137](https://openairdocs.org/sdr/C2XA09RI137), Aug 4, 2009: LINE. CONTAMINATED. FLIGHT 2557 - EWR - FLIGHT CREW REPORTED CAPT / F/O AIRSPEED /ALT INDICATOR MISCOMPARE. FLIGHT CREW DIVERTED TO CMH AND LANDED ACFT UNEVENTFULLY. MX DRAINED PIT
- [SDR C2XA09TY140](https://openairdocs.org/sdr/C2XA09TY140), Jul 6, 2009: INVERTER. INOPERATIVE. LT EMERGENCY ESCAPE HATCH EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD.
- [SDR C2XA09IA114](https://openairdocs.org/sdr/C2XA09IA114), May 1, 2009: RELAY. INOPERATIVE. IAH - FLIGHT 3137, THE CREW REPORTED THAT AFTER T/O THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENAN
- [SDR C2XA09SH060](https://openairdocs.org/sdr/C2XA09SH060), Mar 1, 2009: CARBON SEAL. DAMAGED. PACK NR 1 PRODUCED TERRIBLE ODOR OF BURNT OIL. CABIN WAS SLIGHTLY HAZY TOWARDS END OF FLIGHT. ODOR PRESENT IN ALL PHASES OF FLIGHT. SHV MAINTENANCE REMOVED AND 
- [SDR USAA2009022690447](https://openairdocs.org/sdr/USAA2009022690447), Mar 1, 2009: CARBON SEAL. DAMAGED. PACK NR 1 PRODUCED TERRIBLE ODOR OF BURNT OIL. CABIN WAS SLIGHTLY HAZY TOWARDS END OF FLIGHT. ODOR PRESENT IN ALL PHASES OF FLIGHT. SHV MAINTENANCE REMOVED AND 
- [SDR USAA20090225BB042](https://openairdocs.org/sdr/USAA20090225BB042), Mar 1, 2009: CARBON SEAL. DAMAGED. PACK NR 1 PRODUCED TERRIBLE ODOR OF BURNT OIL. CABIN WAS SLIGHTLY HAZY TOWARDS END OF FLIGHT. ODOR PRESENT IN ALL PHASES OF FLIGHT. SHV MAINTENANCE REMOVED AND 
- [SDR C2XA09RI030](https://openairdocs.org/sdr/C2XA09RI030), Feb 25, 2009: SMOKE WARNING. FALSE ACTIVATION. FLIGHT 2165 - EWR - FLIGHT CREW REPORTED LAV SMOKE WARNING ON EICAS DURING FLIGHT. EWR MX PERFORMED OPERATIONAL CHECK IN THE SYSTEM AND NO FAULTS WERE FOUND. AI
- [SDR C2XA09RI011](https://openairdocs.org/sdr/C2XA09RI011), Jan 9, 2009: UNKNOWN. ODOR. FLIGHT 2393 - EWR - FLIGHT CREW REPORTED THAT DURING CLIMB OUT, "LAV SMOKE" INDICATION SHOWED ON EICAS AND FLIGHT ATTENDANT SAID SHE COULD SMELL SMOKE IN CABIN/
- [SDR C2XA09TY008](https://openairdocs.org/sdr/C2XA09TY008), Jan 9, 2009: SMOKE DETECTOR. FALSE ACTIVATION. WHILE CLIMBING OUT OF EWR, THE FLIGHT ATTENDANT SMELLED FUMES AND SMOKE IN THE CABIN AND LAV. CREW RETURNED TO EWR AND MX RAN BOTH ENGINES AND FOUND TO BE GLYCO
- [SDR C2XA08RI166](https://openairdocs.org/sdr/C2XA08RI166), Nov 13, 2008: SWITCH. OUT OF POSITION. FLIGHT 2539 - RIC - FLIGHT CREW REPORTED FUEL XFER CRITICAL MESSAGE ON EICAS. FLIGHT CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT UNEVENTFULLY. RIC MX FOUND PO
- [SDR C2XA08IA018](https://openairdocs.org/sdr/C2XA08IA018), Jan 8, 2008: RELAY. INOPERATIVE. IAH - FLIGHT 2555, THE CREW REPORTED BRAKE INBOARD INOP ON EICAS DURING LANDING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLA
- [SDR C2XA08IA002](https://openairdocs.org/sdr/C2XA08IA002), Dec 25, 2007: UNKNOWN. ODOR. IAH - FLIGHT 2901 THE CREW REPORTED SMOKE SMELL FROM THE RECIRC FANS. THE AIRCRAFT LANDED AT IAH UNEVENTFULLY WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPS CHEC
- [SDR C2XA07TY057](https://openairdocs.org/sdr/C2XA07TY057), Oct 11, 2007: BRACKET. DAMAGED. TYS DURING A CURRENT C-CHECK INSPECTION THE RIGHT AILERON PCA BRACKET WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REPLACED THE PCA BRACKET IAW EMB 145XR AMM 27-1
- [SDR C2XA07TY056](https://openairdocs.org/sdr/C2XA07TY056), Oct 11, 2007: BRACKET. DAMAGED. TYS - DURING A CURRENT C-CHECK INSPECTION THE LT AILERON PCA BRACKET HAD A BUSHION THAT WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REPLACED THE PCA BRACKET AND 
- [SDR C2XA07IA124](https://openairdocs.org/sdr/C2XA07IA124), May 26, 2007: INVERTER. INOPERATIVE. IAH - FLIGHT 2739, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN ON THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPL
- [SDR C2XA07IA104](https://openairdocs.org/sdr/C2XA07IA104), May 1, 2007: CONNECTOR. DISCONNECTED. IAH - FLIGHT 2110, DURING PREFLIGHT INSPECTION AN EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR ON THE SIGN, OPERATIONALL
- [SDR C2XA07IA017](https://openairdocs.org/sdr/C2XA07IA017), Jan 20, 2007: INVERTER. INOPERATIVE. BFL - FLIGHT 2608, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE GALLEY AND RIGHT WING EMERGENCY EXIT SIGNS WERE FOUND TO BE INOPERATIVE. MAINTENANCE 
- [SDR C2XA07RI003](https://openairdocs.org/sdr/C2XA07RI003), Jan 16, 2007: FAN. CONTAMINATED. FLT 2279 - ORF - DURING CRUISE, CREW DETECTED SMOKE IN COCKPIT WHEN RECIRC FAN WAS ON. MX FOUND PIECE OF INSULATION ON FWD AVIONICS FAN. MX REMOVED INSULATION A
- [SDR C2XA06BT058](https://openairdocs.org/sdr/C2XA06BT058), Dec 19, 2006: INVERTER. INOPERATIVE. EWR LOG SQUAWK EMERGENCY LIGHT ABOVE GALLEY DOOR INOP. REMOVED AND REPLACED INVERTER ABOVE GALLEY DOOR IAW EMB145 AMM 33-50-11. OPS CHECK GOOD.
- [SDR C2XA06SD018](https://openairdocs.org/sdr/C2XA06SD018), Nov 25, 2006: GLOWSTRIP. MISSING. SDF - FIRST FWD LT PHOTOLUMINESCENT FLOOR LIGHTING SECTION MISSING. INSTALLED FIRST FWD LT PHOTOLUMINESCENT FLOOR LIGHT IAW EMB 145 AMM 33-50-02. OPS CHECK GOOD
- [SDR C2XA06SD019](https://openairdocs.org/sdr/C2XA06SD019), Nov 25, 2006: GLOWSTRIP. MISSING. SDF - FIRST FWD RT PHOTOLUMINESCENT FLOOR LIGHTING SECTION MISSING. INSTALLED FWD RT PHOTOLUMINESCENT FLOOR STRIP IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD.
- [SDR C2XA06IA180](https://openairdocs.org/sdr/C2XA06IA180), Nov 13, 2006: LIGHT. INOPERATIVE. IAH - FLIGHT 2265, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE EXIT SIGN ON THE FORWARD RIGHT BULKHEAD TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLAC
- [SDR C2XA06SH082](https://openairdocs.org/sdr/C2XA06SH082), Aug 20, 2006: LIGHT. INOPERATIVE. SHV - DURING ROUTINE INSPECTION THE CABIN EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW EMB 145 XR AMM
- [SDR C2XA06IA109](https://openairdocs.org/sdr/C2XA06IA109), Jul 12, 2006: LIGHT. INOPERATIVE. IAH - FLIGHT 2183, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE CABIN BULKHEAD EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHT SY
- [SDR C2XA06SH025](https://openairdocs.org/sdr/C2XA06SH025), Feb 23, 2006: FLOORBEAM. CORRODED. DURING C-CHECK, THE CENTER OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED AT FRAME 49. MAINTENANCE REMOVED THE CORROSION AND REPROTECTED THE AREA IAW EC5310-01371. 

All 55: https://openairdocs.org/aircraft/N14105/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/N14105/stcs.md

## Earlier aircraft with N14105

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N14105 before.

- [Cancelled 1947-10-06](https://openairdocs.org/deregistered/N14105-1947-10-06): Macdonald Vance F SPORTFLIGHT-A, S/N 1. Owner: [Chazick John M](https://openairdocs.org/faa-owner/CHAZICK%20JOHN%20M), [Flint, MI](https://openairdocs.org/faa-place/MI/Flint)

## 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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