# N12166: 2004 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: 14500831
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 29, 2004
- Certificate issued: June 30, 2026
- Expires: June 30, 2033
- Mode S code: A05AB2
- 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=12166
- Page: https://openairdocs.org/aircraft/N12166

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/N12166/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 N12166.

## FAA accident and incident reports (1)

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 20060502007249I](https://openairdocs.org/incident/20060502007249I), May 2, 2006: Emb EMB145XR (N12166), Houston, TX, Minor damage. (-23) Aircraft N12166, flight 3161, blew both left main tires on takeoff. The flight departed george bush Intercontinental airport Houston, Texas (iah) at 4:02…

## Service difficulty reports (52, 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 ASOA201909084049](https://openairdocs.org/sdr/ASOA201909084049), Sep 8, 2019: GLOWSTRIP. DIRTY. IAH - FLIGHT 4307 THE CREW REPORTED THAT THE PHOTO LUMINESCENT LIGHT STRIP NEAR THE GALLEY DOOR DID NOT GLOW. MAINTENANCE REMOVED THE AFFECTED STRIP, CLEANED AN
- [SDR ASOA2018122695353](https://openairdocs.org/sdr/ASOA2018122695353), Dec 19, 2018: BATTERY PACK. INOPERATIVE. DURING ADS-B MOD LINE THE #2 AND #3 EMERGENCY BATTERY WERE DEAD. MX REMOVED AND REPLACED #2 AND #3 EMERGENCY LIGHT BATTERY PACK WITH OPERATIONAL CHECK GOOD. A/C
- [SDR ASOA2018101864060](https://openairdocs.org/sdr/ASOA2018101864060), Oct 16, 2018: LIGHT. INOPERATIVE. IAH - FLIGHT 4363, DURING MAINTENANCE INSPECTION THE LEFT HAND EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECT
- [SDR ASOA2018101864059](https://openairdocs.org/sdr/ASOA2018101864059), Oct 16, 2018: LIGHT. INOPERATIVE. IAH - FLIGHT 4363, DURING MAINTENANCE INSPECTION THE PAX DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LI
- [SDR ASOA2018082214044](https://openairdocs.org/sdr/ASOA2018082214044), Aug 21, 2018: INVERTER. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE LT EMERGENCY EXIT DOOR LOWER LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INVERTER, OPS TESTED WIT
- [SDR ASOA201808104041](https://openairdocs.org/sdr/ASOA201808104041), Aug 6, 2018: SMOKE DETECTOR. INOPERATIVE. THE CREW REPORTED A LAVATORY SMOKE MESSAGE ON THE EICAS. MAINTENANCE CLEANED THE CONNECTOR PLUG ON THE SMOKE DETECTOR PANEL, OPS TESTED WITH NO DEFECTS AND THE 
- [SDR ASOA201702205012](https://openairdocs.org/sdr/ASOA201702205012), Feb 20, 2017: FAN. SEIZED. PILOT REPORTED A LOUD GRINDING AND VIBRATION NOISE IN THE VICINITY OF ROW 8 ASSOCIATED WITH A BURNING ODOR. REMOVED AND REPLACED RECIRCULATING FAN OPS CHECKED G
- [SDR ASOA20160810043](https://openairdocs.org/sdr/ASOA20160810043), Aug 10, 2016: UNKNOWN. ODOR. PILOT REPORTED A STRONG SMOKE ODOR IN COCKPIT AND FORWARD CABIN NO VISIBLE SMOKE. ENGINE 1 AND APU RUNNING WITH BOTH PACKS ON. MX PERFORMED OPERATIONAL CHECKS O
- [SDR ASOA20160519023](https://openairdocs.org/sdr/ASOA20160519023), May 19, 2016: ACM. ODOR. PILOT REPORTED A LOUD HISSING NOISE BY EXIT ROW WITH PACK 2 ON WITH A BURNING ODOR IN COCKPIT. PLACED ON MEL 5/19/16, 5/21/16. MAINTENANCE R & R NR 2 AIR CYCLE 
- [SDR ASOA20160417023C](https://openairdocs.org/sdr/ASOA20160417023C), Apr 17, 2016: FIRE WARNING. FALSE ACTIVATION. THE CREW REPORTED BAGGAGE SMOKE LIGHT ON, OVERHEAD ILLUMINATED AFTER TAKEOFF. THE CREW RAN THE QRH AND DEPLOYED THE FIREBOTTLES. THE ACFT LANDED WITHOUT FURTHER
- [SDR ASOA20151211071](https://openairdocs.org/sdr/ASOA20151211071), Dec 11, 2015: YOKE. CRACKED. DURING SCHEDULED MAINTENANCE THE NR 1 ENGINE FORWARD YOKE FITTING WAS FOUND CRACKED. LENGTH OF CRACK WAS .088". MAINTENANCE REPLACED THE NR 1 ENGINE LOWER YOKE 
- [SDR ASOA20150118006](https://openairdocs.org/sdr/ASOA20150118006), Jan 18, 2015: CONTROL PANEL. FAULTY. THE CREW REPORTED A LAVATORY SMOKE WARNING INDICATION IN FLIGHT. PULLED CIRCUIT BREAKERS IAW QRH. NO SMOKE WAS INDICATED BY F/A. MAINTENANCE INSPECTED AND REPLA
- [SDR ASOA20150117005](https://openairdocs.org/sdr/ASOA20150117005), Jan 17, 2015: SMOKE DETECTOR. FAULTY. THE CREW REPORTED A LAVATORY SMOKE ON EICAS IN FLIGHT. CREW PULLED THE CIRCUIT BREAKER IAW QRH. NO SIGNS OF SMOKE IN FIGHT. MAINTENANCE INSPECTED AND REPLACED T
- [SDR ASOA201580116003](https://openairdocs.org/sdr/ASOA201580116003), Jan 16, 2015: SMOKE DETECTOR. FALSE ACTIVATION. THE CREW REPORTED LAVATORY SMOKE INDICATION ON EICAS AFTER DEPARTURE. NO VISUAL SMOKE. MAINTENANCE INSPECTED AND PERFORMED LAVATORY SMOKE DETECTION SYS OPS CHEC
- [SDR ASOA20140930289V](https://openairdocs.org/sdr/ASOA20140930289V), Sep 30, 2014: BEAM. CORRODED. DURING C-CHECK, CARGO DOOR CUT OUT LOWER BEAM CORRODED. R & R CARGO DOOR LOWER BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130913108](https://openairdocs.org/sdr/ASOA20130913108), Sep 13, 2013: FLAPPER VALVE. TORN. EXCESSIVE AMOUNT OF FUEL LEAKING OUT OF THE LT AILERON, FUEL LEAK FROM ROTATION UNTIL TWO MINUTES. . DURING CLIMB, SEEMED TO STOP DURING LEVEL OFF. MX INSPECTED
- [SDR C2XA11CL247](https://openairdocs.org/sdr/C2XA11CL247), Nov 11, 2011: ACTUATOR. MALFUNCTIONED. CLE FLT 4469 THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE FOR 3 -5 SECONDS WHEN EXTENDING GEAR ON APPROACH. THE MESSAGE DISAPPEARED AND ALL INDICATI
- [SDR C2XA11IA217](https://openairdocs.org/sdr/C2XA11IA217), Sep 13, 2011: CONNECTOR. LOOSE. DRO - FLIGHT 2077, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE WHEN SELECTING GEAR DOWN AND FLAPS 22 AT APPROXIMATELY 2500FT AGL. THE AIRCRAFT LANDED
- [SDR C2XA11IA216](https://openairdocs.org/sdr/C2XA11IA216), Sep 13, 2011: CONNECTOR. LOOSE. DRO - FLIGHT 2077, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE WHEN SELECTING GEAR DOWN AND FLAPS 22 AT APPROXIMATELY 2500FT AGL. THE AIRCRAFT LANDED
- [SDR C2XA11IA215](https://openairdocs.org/sdr/C2XA11IA215), Sep 13, 2011: FADEC. MALFUNCTIONED. DRO - FLIGHT 6077, THE CREW REPORTED SELECTING "CLB" THRUST DURING TAKEOFF RESULTED IN A T/O 1 DISPLAY ON EICAS (INADEQUATE THRUST POWER) AND AFTER SELECTING CR
- [SDR C2XA11IA214](https://openairdocs.org/sdr/C2XA11IA214), Sep 13, 2011: FADEC. MALFUNCTIONED. DRO - FLIGHT 6077, THE CREW REPORTED SELECTING "CLB" THRUST DURING TAKEOFF RESULTED IN A T/O 1 DISPLAY ON EICAS (INADEQUATE THRUST POWER) AND AFTER SELECTING CR
- [SDR C2XA11IA213](https://openairdocs.org/sdr/C2XA11IA213), Sep 13, 2011: CONTROL MODULE. DEFECTIVE. DRO - FLIGHT 6077, THE CREW REPORTED SELECTING "CLB" THRUST DURING TAKEOFF RESULTED IN A T/O 1 DISPLAY ON EICAS (INADEQUATE THRUST POWER) AND AFTER SELECTING CR
- [SDR C2XA11IA211](https://openairdocs.org/sdr/C2XA11IA211), Sep 13, 2011: UNKNOWN. MALFUNCTIONED. DEN - FLIGHT 6086, DURING T/O THE CREW REPORTED THAT UPON COMMANDING "CLB" THRUST, THE THRUST RATING WENT TO "T/O RSV", AND DURING DESCENT WENT TO "T/O RSV " TH
- [SDR C2XA11IA208](https://openairdocs.org/sdr/C2XA11IA208), Sep 9, 2011: PROXIMITY SWITCH. DIRTY. IAH - FLIGHT 6148, DURING LANDING GEAR EXTENSION THE CREW REPORTED A LG AIR GRND FAIL CAUTION THAT CLEARED IMMEDIATELY AFTER THE GEAR LOCKED DOWN. THE AIRCRAFT 
- [SDR C2XA11RI083](https://openairdocs.org/sdr/C2XA11RI083), May 18, 2011: PROXIMITY SWITCH. DEFECTIVE. FLIGHT 2489 - EWR - FLIGHT CREW REPORTED, COULD NOT MOVE L/G LEVER UNTIL 3DR OR 4TH TRY PUSH LEVER UP AFTER T/O. EWR MX REMOVED AND REPLACED RELAY K0024 AND NOS
- [SDR C2XA11RI082](https://openairdocs.org/sdr/C2XA11RI082), May 18, 2011: RELAY. DEFECTIVE. FLIGHT 2489 - EWR - FLIGHT CREW REPORTED, COULD NOT MOVE L/G LEVER UNTIL 3DR OR 4TH TRY PUSH LEVER UP AFTER TAKEOFF. EWR MX REMOVED AND REPLACED RELAY K0024 AND
- [SDR C2XA11RI076](https://openairdocs.org/sdr/C2XA11RI076), May 11, 2011: PROXIMITY SWITCH. MALFUNCTIONED. FLIGHT 2337 - EWR - FLIGHT CREW REPORTED LG AIR/GND FAIL ON EICAS WHEN YOU LOWER THE LANDING GEAR MOMENTARILY THEN CLEARS. EWR MX REMOVED AND REPLACED NR 2 NOSE
- [SDR C2XA11RI075](https://openairdocs.org/sdr/C2XA11RI075), May 11, 2011: ACTUATOR. MALFUNCTIONED. FLIGHT 2337 - EWR - FLIGHT CREW REPORTED LG AIR/GND FAIL ON EICAS WHEN YOU LOWER THE LANDING GEAR MOMENTARILY THEN CLEARS. EWR MX REMOVED AND REPLACED NR 2 NOSE
- [SDR C2XA11RI067](https://openairdocs.org/sdr/C2XA11RI067), May 6, 2011: ELECTRONIC UNIT. MALFUNCTIONED. FLIGHT 2473 - EWR - FLIGHT CREW REPORTED LG AIR/GND FAIL MESSAGES POPS UP EVERY TIME GEAR IS SET TO DOWN POSITION. MESSAGE GOES AWAY AFTER FEW SECONDS. EWR MX R
- [SDR C2XA11RI066](https://openairdocs.org/sdr/C2XA11RI066), May 6, 2011: ACTUATOR. MALFUNCTIONED. FLIGHT 2473 - EWR - FLIGHT CREW REPORTED LG AIR/GND FAIL MESSAGES POPS UP EVERY TIME GEAR IS SET TO DOWN POSITION. MESSAGE GOES AWAY AFTER FEW SECONDS. EWR MX R
- [SDR C2XA11RI065](https://openairdocs.org/sdr/C2XA11RI065), May 6, 2011: ACTUATOR. MALFUNCTIONED. FLIGHT 2473 - EWR - FLIGHT CREW REPORTED LG AIR/GND FAIL MESSAGES POPS UP EVERY TIME GEAR IS SET TO DOWN POSITION. MESSAGE GOES AWAY AFTER FEW SECONDS. EWR MX R
- [SDR C2XA11RI068](https://openairdocs.org/sdr/C2XA11RI068), May 5, 2011: STRUT. LOW. FLIGHT 2897 - EWR - FLIGHT CREW REPORTED L/G AIR/GND FAIL MESSAGE FOR 5 SECONDS AFTER GEAR EXTENSION. EWR MX CHECKED CMC - NO AIR'GRD FAIL MESSAGE WAS FOUND. MX
- [SDR C2XA11RI064](https://openairdocs.org/sdr/C2XA11RI064), May 5, 2011: WIRE HARNESS. CHAFED. FLIGHT 2533 - EWR - FLIGHT CREW REPORTED L/G AIR GROUND FAIL MESSSAGE FLASHES A FEW SECOMNDS AFTER GEAR EXTENSION. EWR MX REMOVED AND REPLACED DOWN LOCK PROXIMI
- [SDR C2XA11CL047](https://openairdocs.org/sdr/C2XA11CL047), Feb 11, 2011: WIRE HARNESS. FAULTY. ORD FLT 5849 - THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE ON APPROACH WHEN THE LANDING GEAR WAS LOWERED. RECYCLED GEAR AND MESSAGE CLEARED. MESSAGE
- [SDR C2XA11CL028](https://openairdocs.org/sdr/C2XA11CL028), Jan 28, 2011: TRIM SWITCH. FAULTY. IAD FLT 5977 - THE CREW REPORTED CAPTAINS PITCH TRIM SWITCH WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE TRIM SWITCH AND OPERATIONAL CHECKS WERE GOOD
- [SDR C2XA11CL013](https://openairdocs.org/sdr/C2XA11CL013), Jan 14, 2011: ELECTRONIC UNIT. FAULTY. ORD FLT 5896 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT AND THE LEF
- [SDR C2XA11CL002](https://openairdocs.org/sdr/C2XA11CL002), Jan 2, 2011: CONNECTOR. LOOSE. THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL IN FLT. MAINTENANCE INSPECTED AND CLEANED, LUBED AND CHECKED SECURITY OF WEIGHT ON WHEELS PROXIMITY SWITCHES. S
- [SDR C2XA10TY186](https://openairdocs.org/sdr/C2XA10TY186), Dec 8, 2010: TANK. GOUGED. BOTTOM CENTER OF VENTRAL TANK IS GOUGED FROM FAIRING. REPAIRED GOUGE AND REWORKED FAIRING IAW EC2810-01053.
- [SDR C2XA08IA207](https://openairdocs.org/sdr/C2XA08IA207), Sep 4, 2008: BATTERY PACK. DISCHARGED. DURING INSPECTION, THE NR (1) EMERGENCY LIGHT BATTERY WAS FOUND TO BE DEAD. MAINT REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY. OPS CHECKED WITH NO
- [SDR C2XA08RI111](https://openairdocs.org/sdr/C2XA08RI111), Aug 19, 2008: VALVE. INOPERATIVE. FLIGHT 502 - RDU - FLIGHT CREW PERFORMED AIR RETURN DUE TO FUEL LEAKING FROM RT WING. CREW LANDED ACFT UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED FLAP VALVE
- [SDR C2XA08ON149](https://openairdocs.org/sdr/C2XA08ON149), Jun 25, 2008: DIODE. LOOSE. FLT 1380 - JQF - FLIGHT CREW REPORTED LT FWD EXTERNAL EMERGENCY LIGHT INOP. MX PERSONNEL RESEATED DIODE OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASE
- [SDR C2XA08ON137](https://openairdocs.org/sdr/C2XA08ON137), Jun 14, 2008: FUEL. LEAKING. FLT 0222 - TUL - FLIGHT CREW REPORTED RT WING FUEL LEAK. MX PERSONNEL REMOVED AND REPLACED RT WING CONDUIT LINE. OPS AND LEAK CHECKED SATISFACTORY AND ACFT WAS 
- [SDR C2XA08ON092](https://openairdocs.org/sdr/C2XA08ON092), Feb 15, 2008: CHARGER. INOPERATIVE. FLT MX - SAN - WHILE PERFORMING ROUTING CHECK MX PERSONNEL FOUND PILOT'S EMERGENCY LIGHT NR 1 AISLE EMERGENCY LIGHT AND FWD EMERGENCY LIGHTS DO NOT ILLUMINATE. 
- [SDR C2XA08ON087](https://openairdocs.org/sdr/C2XA08ON087), Feb 8, 2008: DOOR. OUT OF ADJUST. FLT 2 - ONT TO ONT - FLIGHT CREW REPORTED MAIN DOOR HARD TO OPEN. MX PERSONNEL TIGHTENED BOLTS ON HANDLE POT, CLEANED/LUBE ROLLERS, OPERATIONALLY CHECKED SATISF
- [SDR C2XA08ON080](https://openairdocs.org/sdr/C2XA08ON080), Feb 3, 2008: ILS SYSTEM. FLUCTUATES. FLT 0025 - TUS TO ICT - FLIGHT CREW REPORTED ILS FLUX ON CAT II WHILE ON APPROACH INTO MCI. AIRCRAFT DIVERTED TO ICT, WHERE FLIGHT CREW RESET BOTH NAV SYSTEMS A
- [SDR C2XA07IA215](https://openairdocs.org/sdr/C2XA07IA215), Sep 28, 2007: BATTERY PACK. DISCHARGED. MCI - DURING MAINTENANCE INSPECTION, THE MAIN DOOR, AND GALLEY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EM
- [SDR C2XA07SH051](https://openairdocs.org/sdr/C2XA07SH051), Aug 21, 2007: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND RIGHT OMEGA BEAM NUT PLATE HOLE AFT OF FRM 23 HAS CORROSION. MAINTENANCE REPAIRED RIGHT OMEGA BEAM AT FRM 23 IAW EC 5320-
- [SDR C2XA07SH050](https://openairdocs.org/sdr/C2XA07SH050), Aug 21, 2007: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND GALLEY CTR OMEGA BEAM AT FRAME 17 TO FRAME 24 WITH CORROSION. MAINTENANCE REMOVED & REPLACED CENTER OMEGA BEAM AT FRAME 1
- [SDR C2XA07IA007](https://openairdocs.org/sdr/C2XA07IA007), Jan 1, 2007: FUSE. BLOWN. IAH - FLIGHT 2644, DURING PRE-FLIGHT INSPECTION THE EMERGENCY LIGHT AT THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT ROW B
- [SDR C2XA06IA067](https://openairdocs.org/sdr/C2XA06IA067), May 2, 2006: TIRE. BLEW OUT. FLIGHT 3161, DURING TAKEOFF THE CREW REPORTED THA THE NR 1 AND NR 2 MAIN TIRES BLEW. THE AIRCRFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT.THIS SDR FILED

All 52: https://openairdocs.org/aircraft/N12166/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/N12166/stcs.md

## Earlier aircraft with N12166

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N12166 before.

- [Cancelled 1977-06-24](https://openairdocs.org/deregistered/N12166-1977-06-24): Cessna 172M, S/N 17261853, built 1973. Exported to Canada. Owner: [Midalta Aviation/ Wetherall Fred](https://openairdocs.org/faa-owner/MIDALTA%20AVIATION%2F%20WETHERALL%20FRED), [Longmont, CO](https://openairdocs.org/faa-place/CO/Longmont)

## 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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