# N670AE: 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: 145790
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 12, 2004
- Certificate issued: October 18, 2011
- Expires: October 31, 2027
- Mode S code: A8DBBD
- 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=670AE
- Page: https://openairdocs.org/aircraft/N670AE

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/N670AE/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 N670AE.

## 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 20220617006409I](https://openairdocs.org/incident/20220617006409I), Jun 17, 2022: Embraer EMB-145LR (N670AE), Rochester, MN, Minor damage. On June 17,2022,Rochester tower reports, Rochester, MN (rst): ENY3649, E145, ord-rst, pilot reported a bird strike (hawk) on a 2 mi final rwy 31. Acft landed…
- [Incident 20101010054319I](https://openairdocs.org/incident/20101010054319I), Oct 10, 2010: Embraer EMB-145LR (N670AE), Dallas Fort Wor, TX, Minor damage. After landing at dfw, while taxing to the assigned gate position, the crew noticed the right main inboard (#3) brake temperature was in the mid amber range. As…

## Service difficulty reports (203, 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 HNAA2026101500988](https://openairdocs.org/sdr/HNAA2026101500988), Aug 27, 2026: DOUBLER. GOUGED. PILOTS' BULKHEAD UPPER OTBD GUIDE PIN HOLE IS GOUGED. INSTALLED THE NEW FABRICATED DOUBLER AND SACRIFICIAL PLATE FOR THE REPAIR ON PILOTS' BULKHEAD UPPER OTBD G
- [SDR HNAA2026101500987](https://openairdocs.org/sdr/HNAA2026101500987), Aug 27, 2026: SHEAR TIE. CRACKED. SHEAR TIE IS CRACKED AT FR 68 BETWEEN STGR. 6L AND 7L. RAR SHEAR TIE AT FR 68 BETWEEN STGR 6L AND 7L IAW EMB 145 SRM 53-31-04RE FIGURE 205.
- [SDR HNAA2026101500986](https://openairdocs.org/sdr/HNAA2026101500986), Aug 27, 2026: SHEAR TIE. CRACKED. SHEAR TIE IS CRACKED AT FRAME 16 BETWEEN STRINGERS 15R-16R. R & R SHEAR TIE AT FRAME 16 BETWEEN STRINGERS 15R-16R IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026101500985](https://openairdocs.org/sdr/HNAA2026101500985), Aug 27, 2026: SHEAR TIE. CRACKED. SHEAR TIE IS CRACKED AT FRAME 15 BETWEEN STRINGERS 15R-16R. R & R SHEAR TIE AT FRAME 15 BETWEEN STRINGERS 15R-16R IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026100900967](https://openairdocs.org/sdr/HNAA2026100900967), Aug 27, 2026: GUSSET. CORRODED. RIGHT CROSSBEAM GUSSET HAS CORROSION AT FR57. REMOVED AND REPLACED RT CROSSBEAM AT FR 57 IAW SRM 51-40-02.
- [SDR HNAA2026100900974](https://openairdocs.org/sdr/HNAA2026100900974), Aug 27, 2026: FLOOR SUPPORT. CORRODED. PAX ENTRYWAY FWD FLOOR SUPPORT HAS CORROSION. REMOVED AND REPLACED PAX ENTRYWAY FWD FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR HNAA2026100900973](https://openairdocs.org/sdr/HNAA2026100900973), Aug 27, 2026: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT HAD CORROSION AT MULTIPLE LOCATIONS FROM FR52-59. RAR CENTER FUSELAGE IV RT FLOOR SILL IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026100900972](https://openairdocs.org/sdr/HNAA2026100900972), Aug 27, 2026: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT HAD CORROSION AT FR 57. R & R CENTER FUSELAGE IV, THE LT FLOOR SUPPORT NR 7 IAW IAW SRM 51-40-02.
- [SDR HNAA2026100900971](https://openairdocs.org/sdr/HNAA2026100900971), Aug 27, 2026: SHEAR TIE. CORRODED. THERE IS CORROSION ON A SHEAR TIE, IN-LINE WITH FR65, STR 20-21L. R & R SHEAR TIE IN-LINE WITH FR65 AT STR 20-21L IAW SRM 51-40-02.
- [SDR HNAA2026100900969](https://openairdocs.org/sdr/HNAA2026100900969), Aug 27, 2026: FLOOR SUPPORT. CORRODED. L3 OTBD FLOOR SUPPORT CORRODED. R & R L3 OTBD FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR HNAA2026100900968](https://openairdocs.org/sdr/HNAA2026100900968), Aug 27, 2026: FLOOR SUPPORT. CORRODED. LEFT NR 4 OTBD FLOOR SUPPORT CORRODED. R & R L4 OTBD FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR HNAA2026100900697](https://openairdocs.org/sdr/HNAA2026100900697), Aug 27, 2026: GUSSET. CORRODED. RH CROSSBEAM GUSSET HAS CORROSION AT FR57. REMOVED AND REPLACED RH CROSSBEAM AT FR 57 IAW SRM 51-40-02.
- [SDR HNAA2202610090096](https://openairdocs.org/sdr/HNAA2202610090096), Aug 27, 2026: GUSSET. CORRODED. RH CROSSBEAM GUSSET HAS CORROSION AT FR 57. REMOVED AND REPLACED RT CROSSBEAM AT FR 57 IAW SRM 51-40-02.,
- [SDR HNAA2026092500910](https://openairdocs.org/sdr/HNAA2026092500910), Aug 27, 2026: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT HAD CORROSION AT MULTIPLE LOCATIONS FROM FR 52-59. R & R CENTER FUSELAGE IV RH FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR HNAA2026092500909](https://openairdocs.org/sdr/HNAA2026092500909), Aug 27, 2026: FLOOR SUPPORT. CORRODED. CENTER FUSELAGE IV, THE LH FLOOR SUPPORT HAD CORROSION AT FR 57. R & R CENTER FUSELAGE IV, THE LT FLOOR SUPPORT NR 7 IAW SRM 51-40-02.
- [SDR HNAA2026092500906](https://openairdocs.org/sdr/HNAA2026092500906), Aug 27, 2026: FLOOR SUPPORT. CORRODED. PAX ENTRYWAY FWD FLOOR SUPPORT HAD CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR HNAA2026092500905](https://openairdocs.org/sdr/HNAA2026092500905), Aug 27, 2026: FLOOR SUPPORT. CORRODED. LEFT NR 3 OTBD FLOOR SUPPORT CORRODED. R & R L3 OTBD FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR HNAA2026092500904](https://openairdocs.org/sdr/HNAA2026092500904), Aug 27, 2026: FLOORBEAM. CORRODED. LEFT NR 4 OTBD FLOOR SUPPORT CORRODED. R & R L4 OTBD FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR HNAA2026092500903](https://openairdocs.org/sdr/HNAA2026092500903), Aug 27, 2026: FLOORBEAM. CORRODED. CENTER FUSELAGE IV, THE RH CROSS BEAM GUSSET HAD CORROSION AT FR57. REMOVED AND REPLACED RT CROSS BEAM AT FR57 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026100900970](https://openairdocs.org/sdr/HNAA2026100900970), Aug 26, 2026: SKIN. CORRODED. CARGO DOOR CUTOUT, THERE IS CORROSION ON THE LOWER EDGE OF THE DOOR CUTOUT, IN-LINE WITH FR 66. REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT SILL IAW SRM 51-40-
- [SDR HNAA2026092500908](https://openairdocs.org/sdr/HNAA2026092500908), Aug 26, 2026: SHEAR TIE. CORRODED. CARGO UNDERFLOOR, THERE IS CORROSION ON A SHEAR TIE, IN-LINE WITH FR 65, STR 20L-21L. R & R SHEAR TIE IN-LINE WITH FR65 AT STR 20L-21L IAW SRM 51-40-02.
- [SDR HNAA2026092500907](https://openairdocs.org/sdr/HNAA2026092500907), Aug 26, 2026: DOOR FRAME. CORRODED. CARGO DOOR CUTOUT, THERE IS CORROSION ON THE LOWER EDGE OF THE DOOR CUTOUT, IN-LINE WITH FR 66. REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT SILL IAW SRM 51-40-
- [SDR HNAA2026101500989](https://openairdocs.org/sdr/HNAA2026101500989), Aug 25, 2026: SKIN. DAMAGED. FOUND RELEVANT INDICATIONS ON FUSELAGE SKIN AT FR 75 AT NEAR STGR 2L. FR 75 REPAIR MEMBERS INSTALLED AS REQUIRED IAW EMB 145 SRM 53-31-01-RE ITEM 11, FIGURE 219
- [SDR HNAA2026101500993](https://openairdocs.org/sdr/HNAA2026101500993), Aug 24, 2026: RIB. DAMAGED. WHILE PERFORMING HFEC INSPECTION ON LT WING SPAR I LOWER FLANGES AT RIB 9 FOUND A RELEVANT INDICATION. REPAIRED LH WING SPAR I LOWER FLANGE AT RIB 9 IAW SRM 57-
- [SDR HNAA2026101500990](https://openairdocs.org/sdr/HNAA2026101500990), Aug 24, 2026: RIB. CRACKED. RIGHT WING RIB 5 IS CRACKED. R & R RIGHT WING RIB 5 IAW AERNNOVA TI-145-26-139 IAW ETD-2026-145-014875 REV.A. AND EO1-57-26-0487
- [SDR HNAA2026011000007](https://openairdocs.org/sdr/HNAA2026011000007), Jan 8, 2026: SIGN. FAILED. EMERGENCY EXIT LIGHT BY TOP OF L/H EMG EXIT IS INOP. R&R L/H TOP EMG EXIT SIGN IAW AMM 33-50-14
- [SDR HNAA2025121500859](https://openairdocs.org/sdr/HNAA2025121500859), Dec 14, 2025: CRADLE. INOPERATIVE. COPILOT EMERGENCY FLASHLIGHT WILL NOT CHARGE FACT 14DEC25 10:16 ROA RAR FLASHLIGHT BASE IRT AMM 33-50-16 OPS CHECK GOOD
- [SDR HNAA2025101400698](https://openairdocs.org/sdr/HNAA2025101400698), Oct 11, 2025: LIGHT. INOPERATIVE. OVHD EMERGENCY LIGHT AT ROW 11 INOPERATIVE. R & R EMERGENCY LIGHT ASSY ON SIDEWALL AT ROW 12 IAW AMM 33-50-14. OPS CK GOOD
- [SDR HNAA2025100600677](https://openairdocs.org/sdr/HNAA2025100600677), Oct 3, 2025: SIGN. INOPERATIVE. LH PAX EMERGENCY EXIT LATCH LIGHT PANEL INOPERATIVE. R & R PANEL IAW AMM3-50-14.
- [SDR HNAA2025042800223](https://openairdocs.org/sdr/HNAA2025042800223), Apr 25, 2025: FAN. FAILED. LH SIDE ROW 4 THRU 6 HAD SMOKE. TURNED OFF RECIRC FAN AND SMOKE CLEARED. PERFORMED OPS CHECK OF AIR DISTRIBUTION SYSTEM IRW AMM 21-20-00 RAN PACK 1 AND 2 FOR 1 
- [SDR HNAA2025042100213](https://openairdocs.org/sdr/HNAA2025042100213), Apr 19, 2025: CONTROL LEVER. FAULTED. AT 330 ALT LG DISAGREE MESSAGE DISPLAYED. FOLLOWED QRH WOULD NOT CLEAR. TROUBLE SHOT IAW FIM 32-32-00-810-803-A STEPS 1, 2, 9, 22 NO FAULTS FOUND. R&R LANDING G
- [SDR HNAA2024120901165](https://openairdocs.org/sdr/HNAA2024120901165), Dec 6, 2024: EXCITER. FAULTED. E2 HUNG START AT 30%N2 ON FADEC A. CREW STOPPED START SEQ WHEN FUEL SMELLED IN A/C. FACT 06DEC24 21:38 PHL R&R E2 LEFT IGNITION EXCITER IAW RRM 74-13-10. STARTE
- [SDR HNAA2024102201019](https://openairdocs.org/sdr/HNAA2024102201019), Oct 22, 2024: A/C PACK. ODOR. OIL SMELL FROM NO.1 BLEED SYSTEM CLEARS WHEN NO.1 PACK IS SHUT DOWN. FACT 22OCT24 12:50 CLT RAN PACKS ON APU FOR 15 MIN NO OIL SMELL NOTED OK FOR SERVICE AT THI
- [SDR HNAA2024071500539](https://openairdocs.org/sdr/HNAA2024071500539), Jul 12, 2024: ACM. FAILED. SMOKE SMELL IN FLIGHT DECK WITH PACK 1 OPERATING. C/W FLT CREW PROCEDURES MEL 12JUL24 C19403 21-15-21 AIR COND PACK N650 AND ABOVE. FACT 12JUL24 DURING OPERATIN
- [SDR HNAA2024071500537](https://openairdocs.org/sdr/HNAA2024071500537), Jul 11, 2024: UNKNOWN. ODOR. DURING HANDOVER NOTICED STRONG ELECTRICAL BURNING SMELL WITH VISIBLE SMOKE IN COCKPIT. FACT 11JUL24 19:48 LYH T/S ELECTRICAL BURNING SMELL WITH VISIBLE SMOKE. R
- [SDR HNAA2024062000492](https://openairdocs.org/sdr/HNAA2024062000492), Jun 19, 2024: UNKNOWN. ODOR. STRONG BURNING SMELL IN FLT DECK. RAN PACKS 1 AND 2 FOR SEVERAL HOURS OPENED PACK PANELS 1 AND 2 INSPECTED FOR SIGNS OF BURNING NO SMELL INSPECTED COCKPIT AVION
- [SDR HNAA2024053100480](https://openairdocs.org/sdr/HNAA2024053100480), May 30, 2024: UNKNOWN. UNKNOWN. IN CRUISE LOUD POP FOLLOWED BY LOUD RUSHING AIR SOUND AT ROW 13. FACT 30MAY24 17:20 CLT INSPECTED ECS PACKS, RAM AND DUCTS WHILE A/C PRESSURIED TO 7PSI. NO LEAK
- [SDR HNAA2024051600417](https://openairdocs.org/sdr/HNAA2024051600417), May 12, 2024: SHEAR TIE. CRACKED. E031785 SHEAR CLIP IS CRACKED AT FRAME 25 BETWEEN STRINGERS 15R AND 16R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 25 BETWEEN STRINGERS 15R AND 16R IAW EMB145 SR
- [SDR HNAA2024051600412](https://openairdocs.org/sdr/HNAA2024051600412), May 7, 2024: REPAIR. CORRODED. E035316 PREVIOUS REPAIR AT FR 20 CORRODED. REMOVED PREVIOUS CORRODED REPAIR AT FR 20, PERFORMED PERMANENT REPAIR TO LH OMEGA BEAM AT FR 20 IAW PIEDMONT EO1-53-2
- [SDR HNAA2024051600402](https://openairdocs.org/sdr/HNAA2024051600402), Apr 21, 2024: NUT PLATE. CORRODED. E030534 CARGO DOOR STAY ROD STOW BRACKET NUTPLATES HAVE CORRISION. REMOVED AND REPLACED LOWER INBOARD L-PROFILE IAW EMB-145 SRM 51-10-03, SRM 52-30-04 AD, TABLE
- [SDR HNAA2024051600411](https://openairdocs.org/sdr/HNAA2024051600411), Apr 20, 2024: SUPPORT RIB. CRACKED. E033873 SERVICE DOOR INTERNAL WEB SUPPORT RIB AT STGR 11R CRACKED. REMOVED AND REPLACED SERVICE DOOR INTERNAL WEB SUPPORT RIB AT STGR 11R IAW EMB 145 SRM 51-40-
- [SDR HNAA2024051600401](https://openairdocs.org/sdr/HNAA2024051600401), Apr 20, 2024: FRAME. CORRODED. E033874 FRAME 20 CORRODED JUST ABOVE SERVICE DOOR LOWER CENTER SILL.. REMOVED CORRODED FR 20, PREPPED AND INSTALLED SERVICEABLE FR 20 BTW STGR 5R-18R IAW PIEDMO
- [SDR HNAA2024051600410](https://openairdocs.org/sdr/HNAA2024051600410), Apr 15, 2024: STRINGER. CRACKED. E032626 STRINGER 6R IS CRACKED AT FRAME 13. REMOVED AND REPLACED STRINGER 6R AT FRAME 13 IAW EMB145 SRM 51-40-02.
- [SDR HNAA2024051600409](https://openairdocs.org/sdr/HNAA2024051600409), Apr 13, 2024: SUPPORT. CORRODED. E032496 GALLEY FWD DIGITAL IS CORRODED AT LH AND CENTER BEAM POSITIONS ON AFT END. REPAIRED GALLEY FWD DIGITAL CORROSION AT LH AND CENTER BEAM POSITIONS ON AFT 
- [SDR HNAA2024051600400](https://openairdocs.org/sdr/HNAA2024051600400), Apr 13, 2024: FLOORBEAM. CORRODED. E032495 FR 20 CROSSBEAM CORRODED AT RH SIDE. : REMOVED AND REPLACED FR 20 CENTER AISLE CROSSBEAM IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024051600399](https://openairdocs.org/sdr/HNAA2024051600399), Apr 13, 2024: FLOOR SUPPORT. CORRODED. E032414 CORROSION ON LH OMEGA BEAM #2 GUSSET. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE L/H OMEGA BEAM #2 GUSSET IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024051600398](https://openairdocs.org/sdr/HNAA2024051600398), Apr 13, 2024: FLOOR SUPPORT. CORRODED. E032410 CORROSION ON CENTER OMEGA BEAM #1 GUSSET. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE CENTER OMEGA BEAM #1 GUSSET IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024051600394](https://openairdocs.org/sdr/HNAA2024051600394), Apr 12, 2024: SEAT TRACK. CORRODED. E031925 CORROSION ON RH #2 OTBD SEAT TRACK. RAR RH #2 OTDB SEAT TRACK IAW EMB 145 AMM 53-01-06
- [SDR HNAA2024051600419](https://openairdocs.org/sdr/HNAA2024051600419), Apr 12, 2024: SHEAR TIE. CRACKED. E031803 SHEAR CLIP IS CRACKED AT FRAME 58 BETWEEN STRINGERS 15L-16L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 58 BETWEEN STRINGERS 15L-16L IAW EMB145 SRM 51-40-
- [SDR HNAA2024051600408](https://openairdocs.org/sdr/HNAA2024051600408), Apr 12, 2024: SHEAR TIE. CRACKED. E031914 SHEAR CLIP CRACKED AT FR62, BETWEEN STR 08R-07R. RAR SHEAR CLIP AT FR 62, BETWEEN STR 08R-07R IAW EMB 145 SRM 51-40-02

All 203: https://openairdocs.org/aircraft/N670AE/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/N670AE/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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.