# N671AE: 2004 Embraer EMB-145LR

- Status: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212, 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: 145793
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 25, 2004
- Certificate issued: September 16, 2011
- Expires: September 30, 2027
- Mode S code: A8DF74
- Registered owner: [American Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRLINES%20INC)
- Location: [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth)
- Owner type: Corporation
- Owner's area on the map: 32.8240° N, 97.0491° W: Placed by OpenAirDocs at the center of ZIP code 76155, 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=671AE
- Page: https://openairdocs.org/aircraft/N671AE

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): 110 in force

### Matched by airframe (Embraer EMB-145LR)

- [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 2017-04-12](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 2012-19-06](https://openairdocs.org/ad/2012-19-06): Stabilizers · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 9 more. Effective Oct 29, 2012
- [AD 2011-21-15](https://openairdocs.org/ad/2011-21-15): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 7 more. Effective Nov 23, 2011
- [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 2008-10-08](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 2007-10-11](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 2006-19-04](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 2006-16-17](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
- [AD 2005-13-22](https://openairdocs.org/ad/2005-13-22): Electric fuel pumps · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jul 7, 2005
- [AD 2005-05-09](https://openairdocs.org/ad/2005-05-09): Forward upper liners · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Apr 14, 2005
- [AD 2005-04-05](https://openairdocs.org/ad/2005-04-05): Air turbine starter (ATS) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 24, 2005
- [AD 2005-01-05](https://openairdocs.org/ad/2005-01-05): Nose Landing Gear Wheel Nuts and Associated Inner and Outer Seals, and Reidentifying the Landing Gear Strut · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Feb 9, 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 2001-17-04](https://openairdocs.org/ad/2001-17-04) (historical): Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Sep 5, 2001
- [AD 2000-04-09](https://openairdocs.org/ad/2000-04-09) (historical): Elevator Servo Tab and Spring Tab Hinge Fittings of the Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Mar 10, 2000
- [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 126: https://openairdocs.org/aircraft/N671AE/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 N671AE.

## FAA accident and incident reports

None matched to N671AE.

## Service difficulty reports (130, 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 SIMA20220404001](https://openairdocs.org/sdr/SIMA20220404001), Apr 4, 2022: LAMP. INOPERATIVE. GALLEY CEILING EMERGENCY LIGHT INOP-C/A-RAR GALLEY CEILING EMERGENCY LAMP IAW AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECK GOOD. END.
- [SDR SIMA20220226002](https://openairdocs.org/sdr/SIMA20220226002), Feb 26, 2022: NOT REPORTED. NOT REPORTED. SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.
- [SDR SIMA20211222003](https://openairdocs.org/sdr/SIMA20211222003), Dec 22, 2021: NONE. NONE. PASSENGER SEAT 15A AND 16A EMERGENCY LIGHT FLOOR POWER STRIP WIRE BORKEN.-C/A-RAR EMERGENCY FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-50-12 OPC GOOD
- [SDR SIMA202108154001](https://openairdocs.org/sdr/SIMA202108154001), Aug 14, 2021: LAMP. INOPERATIVE. GALLEY EMERGENCY LIGHT INOP. R & R GALLEY EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD. END.
- [SDR SIMA20210618002](https://openairdocs.org/sdr/SIMA20210618002), Jun 18, 2021: INVERTER. INOPERATIVE. EMERGENCY INTERIOR LIGHT ADJ TO RH EMERGENCY EXIT INOP-C/A-REF TURNOVER, COMPLETED RAR OF #5 EMERG LIGHTS INVERTER IAW AMM 33-50-11. OPC GOOD.
- [SDR SIMA20210225002](https://openairdocs.org/sdr/SIMA20210225002), Feb 24, 2021: FLASHLIGHT ASSY. BROKEN. AFT CABIN EMERGENCY FLASHLIGHT HOLDER HAD BROKEN CLIP-C/A-R & R AFT CABIN EMERGENCY FLASHLIGHT HOLDER ASSEMBLY IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-8
- [SDR SIMA20210113001](https://openairdocs.org/sdr/SIMA20210113001), Jan 13, 2021: LIGHT. INOPERATIVE. AFT RT OVERWING EMERGENCY LIGHT INOPERABLE. C/A: R & R AFT RT OVERWING EMERGENCY LIGHT ASSEMBLY OPERATIONS CHECK GOOD, IAW AMM 33-50-10.
- [SDR SIMA20201217001](https://openairdocs.org/sdr/SIMA20201217001), Dec 17, 2020: BULB. INOPERATIVE. RT UPPER EMERGENCY EXIT LIGHT INOPERABLE. C/A: R & R RT UPPER EMERGENCY LIGHT BULB, IAW EMB 145 AMM 33-50-10. OPERATIONS CHECK GOOD. NO DEFECTS NOTED.
- [SDR SIMA20201128004](https://openairdocs.org/sdr/SIMA20201128004), Nov 28, 2020: LAMP. INOPERATIVE. RT OVERWING EMERGENCY LIGHT INOPERABLE. C/A: R & R RT OVERWING EMERGENCY LIGHT LAMP, IAW EMB AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A. OPERATIONS CHEC
- [SDR SIMA202007232002](https://openairdocs.org/sdr/SIMA202007232002), Jul 22, 2020: LIGHT. INOPERATIVE. FOUND RT WING EMERGENCY LIGHT INOPERATIVE DURING PS-1 CHECK. REMOVED AND INSTALLED A NEW RT WING EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECKED GOOD. NO DEFECTS 
- [SDR SIMA2020031614003](https://openairdocs.org/sdr/SIMA2020031614003), Mar 14, 2020: LIGHT. INOPERATIVE. RH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RH OVERWING EMERGENCY LIGHT IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECKED GOOD. E
- [SDR SIMA202003110001](https://openairdocs.org/sdr/SIMA202003110001), Mar 10, 2020: LIGHT. INOPERATIVE. R/H WING EMERGENCY LIGHT INOP-C/A-RAR R/H WING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.
- [SDR SIMA202003032005](https://openairdocs.org/sdr/SIMA202003032005), Mar 2, 2020: TRANSDUCER. FAILED. H.S. REJECTED T/O (80 KTS) DUE E2 A/I FAIL ON T.O. ROLL-C/A-RRMOVED AND REPLACED ENGINE #2 ANTI-ICING PRESSURE TRANDUCER IAW EMB145 AMM 30-21-06 LEAK/ OPS CHECK
- [SDR SIMA202002132004](https://openairdocs.org/sdr/SIMA202002132004), Feb 12, 2020: ANTI-ICE VALVE. FAILED. E1 A/ICE FAIL MESSAGE DURING CLIMB. RAN CHECHLIST, BUT MESSAGE REMAINED AND VALVE WOULD NOT OPEN WITH OVERRIDE NOB IN ALL. ALSO GOT AN ENG A/I OVERPRESS ADVISOR
- [SDR SIMA201912275002](https://openairdocs.org/sdr/SIMA201912275002), Dec 25, 2019: BATTERY PACK. INOPERATIVE. DURING PS-1 CHECK, FOUND EMERGENCY LIGHT INOPERATIVE BETWEEN 12A AND 9A. REMOVED AND REPLACED THE NR 3 BATTERY POWER SUPPLY AND BATTERY IAW AMM 33-50-04, OPS-CH
- [SDR SIMA201912274001](https://openairdocs.org/sdr/SIMA201912274001), Dec 24, 2019: BATTERY PACK. DISCHARGED. FOUND EMERGENCY LIGHT BATTERY PACKS NR 2 AND 3 LOW, LIGHTS SHUT OFF AFTER APPOX 10 SECONDS. REMOVED AND REPLACED THE NR 2 BATTERY. OPS CHECKED GOOD IAW AMM 33-5
- [SDR SIMA201912274003](https://openairdocs.org/sdr/SIMA201912274003), Dec 24, 2019: BULB. INOPERATIVE. LEFT FORWARD LOWER FAIRING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-10.
- [SDR SIMA201912274002](https://openairdocs.org/sdr/SIMA201912274002), Dec 24, 2019: LIGHT. INOPERATIVE. FLOOR PROXIMITY STRIP NR 1 AFT SECTION INOPERATIVE. REMOVED AND REPLACED FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD, NO FURTHER DEFECTS NOTE
- [SDR SIMA201912032003](https://openairdocs.org/sdr/SIMA201912032003), Dec 2, 2019: BATTERY PACK. INOPERATIVE. DURING PS-1 CHECK FOUND MULTIPLE EMERGENCY LIGHTS OUT NEAR CENTER FUSELAGE.-C/A-REMOVED AND REPLACED #3 EMERGENCY LIGHT BATTERY AND CHARGER ASSEMBLY IAW EMB 145
- [SDR SIMA201911143010](https://openairdocs.org/sdr/SIMA201911143010), Nov 13, 2019: UNKNOWN. SMOKE. ON TAXI OUT AFTER SWITCHING PACK 1 BACK ON, COCKPIT FILLED WITH SMOKE. AFTER SWITCHING PACK 1 BACK OFF SMOKE DISSIPATED-C/A-PERFORMED FIM TASK PROCEDURES EMB 14
- [SDR SIMA201911087004](https://openairdocs.org/sdr/SIMA201911087004), Nov 7, 2019: LIGHT. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.
- [SDR SIMA201910086010](https://openairdocs.org/sdr/SIMA201910086010), Oct 6, 2019: WIRE. BROKEN. 3EA WIRES BROKEN ON EMERGENCY LIGHT STRIP FLOOR CONNECTIONS-C/A-REPAIRED 3EA WIRES AT FLOOR PAELS 261BF AND 251FF IAW SWPM 20-21-00. OPS CHK GOOD
- [SDR SIMA201910086009](https://openairdocs.org/sdr/SIMA201910086009), Oct 6, 2019: WIRE. BROKEN. 1EA BROKEN WIRE ON EMERGENCY LIGHT STRIP AT FLOOR PANEL 251BF-C/A-REPAIRED 1EA WIRES AT FLOOR PANEL 251BF IAW SWPM 20-21-00. OPS CHK GOOD
- [SDR SIMA201910083010](https://openairdocs.org/sdr/SIMA201910083010), Oct 3, 2019: SHUNT. GOUGED. FRAME 80 AFT SIDE AT APU SHUNT CONNECTION IS GOUGED (FRAME REINFORCEMENT)-C/A-REMOVED AND REPLACED REINFORCEMENT IAW SRM 53-32-04, GPM17-13 AND SRM 51-40-02.
- [SDR SIMA201910083009](https://openairdocs.org/sdr/SIMA201910083009), Oct 3, 2019: SHEAR TIE. CORRODED. SSI 53-30-48 FR 65 SHEAR CLIP IS CORRODED AT CARGO DOOR SILL AND ABOVE GUIDE PLATE-C/A-REMOVED AND INSTELLED SERVICEABLE SECTION OF FRAME 65 SHEAR IAW EMB 145 S
- [SDR SIMA201910083008](https://openairdocs.org/sdr/SIMA201910083008), Oct 3, 2019: RIB. CRACKED. LH WING RIB 21 IS CRACKED INSIDE PANEL 551CB.-C/A-REPAIRED LH WING RIB 21 INSIDE PANEL 551CB IAW EMB 145 SRM 57-20-07, ITEM #4.
- [SDR SIMA201910083007](https://openairdocs.org/sdr/SIMA201910083007), Oct 3, 2019: DOOR SILL. CORRODED. CARGO DOOR LOWER SILL IS CORRODED-C/A-REMOVED AND REPLACED CARGO DOOR LOWER SILL IAW EMB-145 SRM 51-40-02.
- [SDR SIMA201910083006](https://openairdocs.org/sdr/SIMA201910083006), Oct 3, 2019: STRINGER. CRACKED. STGR 6R CRACKED AT FR 13-C/A-REMOVED AND INSTALLED NEW STRINGER 6R AT FRAME 13 IAW EMB 145 SRM 51-40-02.
- [SDR SIMA201910083005](https://openairdocs.org/sdr/SIMA201910083005), Oct 3, 2019: FLOOR SUPPORT. CRACKED. LH OMEGA BEAM OUTBD SUPPORT IS CRACKED AT PREVIOUS REPAIR AT FR 47-C/A-REMOVED AND REPLACED L/H OMEGA OUTBD SUPPORT AT FR 47 IAW EMB 145 SRM 53-23-02 AND SRM 51
- [SDR SIMA201910083004](https://openairdocs.org/sdr/SIMA201910083004), Oct 3, 2019: STOP FITTING. DAMAGED. CARGO DOOR FWD CONTINUOS STOP IS BENT AND CRACKED AT LOWER END-C/A-REMOVED AND INSTALLED NEW CARGO DOOR FWD CONTINUOS STOP IAW EMB 145 SRM 51-40-02
- [SDR SIMA201910083003](https://openairdocs.org/sdr/SIMA201910083003), Oct 3, 2019: RIB. CRACKED. RH WING RIB 21 IS CRACKED INSIDE PANEL 651CB. REPAIRED RH WING RIB 21 INSIDE PANEL 651CB IAW EMB 145 SRM 57-20-07, ITEM #4
- [SDR SIMA201910083011](https://openairdocs.org/sdr/SIMA201910083011), Oct 3, 2019: FLOOR SUPPORT. CORRODED. SSI 53-20-11 LH OMEGA BEAM SIDEWALL CORRODED AT FR 29. REPAIRED LH OMEGA BEAM SIDEWALL AT FR 29 IAW ENVOY ERS-EM-53MR-3903
- [SDR SIMA201910083012](https://openairdocs.org/sdr/SIMA201910083012), Oct 3, 2019: FRAME. GOUGED. FR 68 Z FRAME IS GOUGED AROUND 4 SCREW HOLES RH SIDE LOWER END-C/A-REMOVED AND REPLACED GOUGED FR 68 Z FRAME IAW EMB 145 SRM 51-40-02.
- [SDR SIMA201910083002](https://openairdocs.org/sdr/SIMA201910083002), Oct 3, 2019: RIB. CRACKED. LEFT ELEVATOR INBOARD HINGE CUTOUT INBOARD NOSE RIB IS CRACKED -C/A-REMOVED AND INSTALLED NEW INBD NOSE RIB ON THE LEFT ELEVATOR INBOARD HINGE CUTOUT IAW EMB 14
- [SDR SIMA201910083001](https://openairdocs.org/sdr/SIMA201910083001), Oct 3, 2019: DOOR FRAME. CORRODED. CARGO DOOR LOWER FRAME IS CORRODED AROUND 2 SCREW HOLES AT FWD END.-C/A-REMOVED AND INSTALLED NEW CARGO DOOR LOWER FRAME IAW EMB 145 SRM 51-20-03, 51-40-06 AND 
- [SDR SIMA20190721001](https://openairdocs.org/sdr/SIMA20190721001), Jul 21, 2019: ECU. FAILED. AFTER TAKE OFF UPON RETRACTING THE FLAPS, WE GOT FLAPS FAIL MESSAGE ON THE EICAS. FLAPS DID NOT RETRACT AND STAYED AT 9*. WE COMPLIED WITH CHECKLIST AND LANDED 
- [SDR SIMA201809187005](https://openairdocs.org/sdr/SIMA201809187005), Sep 17, 2018: INVERTER. INOPERATIVE. EMEREGENCY EXIT LIGHTED SIGN ON BACKSIDE OF AFT CALLEY (FACING THE SEATS) INOP. REMOVED AND REPLACED NR 2 DC/AC INVERTER IAW AMM 33-50-11 AND EMERGENCY LIGHTS O
- [SDR SIMA201808275002](https://openairdocs.org/sdr/SIMA201808275002), Aug 25, 2018: GENERATOR. MALFUNCTIONED. NR 3 GENERATOR OFF BUSS DURING TAKEOFF ROLL. REMOVED AND REPLACED THE NR 3 GENERATOR IAW WC 24-800-00, OP CHECKED GOOD AND LEAK CHECKED GOOD.
- [SDR SIMA2018082019001](https://openairdocs.org/sdr/SIMA2018082019001), Aug 19, 2018: CONTROL UNIT. FAILED. FLAP FAIL AFTER TAKE OFF STUCK AT 9. CMC HAD MULTIPLE OCURRENCES OF DRIVE SENSOR FAIL. HAD ONE OCURRENCE OF FLAP RT TRANSMISSION FAIL. TROUBLESHOT IAW FIM 27-51
- [SDR SIMA201808032001](https://openairdocs.org/sdr/SIMA201808032001), Aug 2, 2018: LAMP. INOPERATIVE. EMERGENCY LIGHT AT THE SERVICE DOOR WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.
- [SDR SIMA20180224002](https://openairdocs.org/sdr/SIMA20180224002), Feb 24, 2018: CHARGER. FAILED. BOTH AFT OVERWING EMERGENCY LIGHTS FAILED TO ILLUMINATE. COMPLIED WITH FIM 33-50-00. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND CHARGER IAW 33-50
- [SDR SIMA20180217012](https://openairdocs.org/sdr/SIMA20180217012), Feb 17, 2018: CHARGER. INOPERATIVE. BOTH AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY AND CHARGER IAW W/C 33-700-19. OPS CHECKED GOOD.
- [SDR SIMA20180215005](https://openairdocs.org/sdr/SIMA20180215005), Feb 15, 2018: BATTERY PACK. INOPERATIVE. SEVERAL EMERGENCY LIGHTS FOUND INOPERATIVE, LT AND RT EXTERNAL OVERWING. REMOVED AND REPLACED THE NR 4 BATTERY, PERFOMED AN OPS CHECK IAW 33-700-17. OPS CHECKED
- [SDR SIMA20180215004](https://openairdocs.org/sdr/SIMA20180215004), Feb 15, 2018: CONTACTOR. DIRTY. AFT GALLEY EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND CLEANED THE CONTACTORS IAW GENERAL MAINTENANCE, OPS CHECKED GOOD.
- [SDR SIMA20180202003](https://openairdocs.org/sdr/SIMA20180202003), Feb 2, 2018: POWER SUPPLY. FAILED. LEFT AND RIGHT OVERWING EXTERNAL EMERGENCY LIGHTS FAILED TO ILLUMINATE. TROUBLESHOT IAW WM 33-50-50, AND R 7 R THE NR 4 EPSU IAW AMM 30-50-04. OPS CHECKED GOOD.
- [SDR SIMA20180202002](https://openairdocs.org/sdr/SIMA20180202002), Feb 2, 2018: WIRE HARNESS. FAILED. RECEIVED A LANDING GEAR AIR/GND FAIL CAUTION MESSAGE DURING CLIMBOUT. COULD NOT BRING GEAR UP. MESSAGE EXTINGUISHED 2 MINUTES LATER. BROUGHT GEAR UP. LANDED BAC
- [SDR SIMA20180107003](https://openairdocs.org/sdr/SIMA20180107003), Jan 7, 2018: CHARGER. FAILED. BOTH AFT OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT CHARGER AND BATTERY ASSY, OPS CHECKED BAD IAW AMM 33-50-04.
- [SDR SIMA20171214002](https://openairdocs.org/sdr/SIMA20171214002), Dec 14, 2017: FUSE. FAILED. LH AND RH AFT OVERWING EMERGENCY LIGHTS INOP.-C/A-T/S PER FIM 33-50-00-810-804A. FOUND #4 EMERGENCY BATTERY POWER SUPPLY FUSE F1 INOP. REMOVED AND REPLACED #4 E
- [SDR SIMA20171108006](https://openairdocs.org/sdr/SIMA20171108006), Nov 8, 2017: POWER SUPPLY. INOPERATIVE. BOTH OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-50-04. OPS GOOD.
- [SDR SIMA20171101001](https://openairdocs.org/sdr/SIMA20171101001), Nov 1, 2017: BATTERY. DISCHARGED. LT AND RT OVERWING EMERGENCY LIGHT INOP. REPLACED NR 4 EMERGENCY BATTERY AND BATTERY POWER SUPPLY IAW AMM 33-50-04 OPS GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/

All 130: https://openairdocs.org/aircraft/N671AE/reports.md

## STCs that may be installed (OpenAirDocs) (75, 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-145LR)

- [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 ST02216AT-D](https://openairdocs.org/stc/ST02216AT-D): Installation of Teledyne Mini Flight Data Acquisition Unit in a Provisioned EMB-135/145. 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 ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [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 ST04527CH](https://openairdocs.org/stc/ST04527CH): Installation of a 16 passenger configuration. C&L STC Holdings 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 ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [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 ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST01039DE](https://openairdocs.org/stc/ST01039DE): Passenger seating arrangement for 30 or less passengers. Deluxe Public Charter LLC
- [STC ST04537NY](https://openairdocs.org/stc/ST04537NY): Installation of Air Filtration. Kilroy Aviation LLC
- [STC ST09858SC](https://openairdocs.org/stc/ST09858SC): Installation of cabin automatic coffee brewing system. Safran Cabin Germany Gmbh
- [STC ST04255CH](https://openairdocs.org/stc/ST04255CH): Installation of an Automatic Dependent Surveillance-Broadcast (ADS-B Out) System. ENVOY AIR
- [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 ST04423NY](https://openairdocs.org/stc/ST04423NY): Installation of ADS-B Out. FTI Engineering Nework GmbH
- [STC ST00015IB](https://openairdocs.org/stc/ST00015IB): Installation of a Honeywell HF Communication System, model KHF 1050, with provisions for a dual installation. Embraer Engineering & Technology Center - USA Inc
- [STC ST00014IB](https://openairdocs.org/stc/ST00014IB): Installation of a second Honeywell HF Communication System, model KHF 1050. Embraer Engineering & Technology Center - USA Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST04333NY](https://openairdocs.org/stc/ST04333NY): Installation of sat: Tglo® Photolumincsccnt Aisle Path Marking System. STG Aerospace Ltd
- [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 ST000081B](https://openairdocs.org/stc/ST000081B): Installation of a second SELCAL channel. EMBRAER - Empresa Brasileira de Aeronautica
- [STC ST00008IB](https://openairdocs.org/stc/ST00008IB): Installation of a second SELCAL channel. EMBRAER - Empresa Brasileira de Aeronautica
- [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

All 75: https://openairdocs.org/aircraft/N671AE/stcs.md

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/aircraft.md
- The Rolls-Royce AE3007 series engine: https://openairdocs.org/engine/rolls-royce-ae3007-series.md

---
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