# N675AE: 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: 14500806
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 19, 2004
- Certificate issued: September 23, 2011
- Expires: September 30, 2027
- Mode S code: A8EE50
- 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=675AE
- Page: https://openairdocs.org/aircraft/N675AE

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/N675AE/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 N675AE.

## 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 20041116030149I](https://openairdocs.org/incident/20041116030149I), Nov 16, 2004: Emb EMB145LR (N675AE), Wichita, KS. (-23) On November 16, 2004, aircraft N675AE flight no. 3915 while enroute from ord to ict the eicas malfunctioned. According to the captain and first officer,…

## Service difficulty reports (146, 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 SIMA20220908001](https://openairdocs.org/sdr/SIMA20220908001), Sep 8, 2022: NONE. NONE. DURING PS-2 FOUND FWD FA EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-RAR FWD FA EMERGENCY FLASHLIGHT IAW EMB 145 AMM 33-50-16. NO FURTHER DEFECTS NOTED.
- [SDR SIMA20220614002](https://openairdocs.org/sdr/SIMA20220614002), Jun 14, 2022: INVERTER. UNSERVICEABLE. LH OVERWING EMERGENCY EXIT LIGHTED MARKER SIGN INOP-C/A-RAR #4 EMERGENCY LIGHT DC/AC INVERTER IAW AMM 33-50-11 OPC GOOD .
- [SDR SIMA20220502003](https://openairdocs.org/sdr/SIMA20220502003), May 2, 2022: NONE. NONE. AIRCRAFT NOT PRESSURIZING EMERGENCY DECLARED. CABIN ALT, AP AND RATE DROPPED TO ZERO IN CLIMB AND STAYED AT ZERO UNTIL WE RAN CHECKLIST AND NEVER RECOVERED. -C/
- [SDR SIMA20220426001](https://openairdocs.org/sdr/SIMA20220426001), Apr 26, 2022: NONE. NONE. LED EMERGENCY FLASHLIGHT MISSING IN REAR OF PLANE-C/A-FLIGHT CREW PLACARDED AFT FA EMERGENCY FLASHLIGHT. M PROCEDURES C/W. MEL 25-32 AUTH 040347M-C MOC 437847. 
- [SDR SIMA20220218006](https://openairdocs.org/sdr/SIMA20220218006), Feb 18, 2022: NONE. NONE. LOWER LH EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR LH EXTERNAL EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECKED BAD SEE ITEM 2 THIS NRWC
- [SDR SIMA20211211001](https://openairdocs.org/sdr/SIMA20211211001), Dec 11, 2021: NONE. NONE. LH OVERWING EMERGENCY LIGHT INTERMITTENT-C/A-FOUND LH OVERWING EMERGENCY LIGHT BULB SOCKET DAMAGED. RAR LH OVERWING EMERGENCY LIGHT HOUSING IAW EMB 145 AMM 33-5
- [SDR SIMA20211013001](https://openairdocs.org/sdr/SIMA20211013001), Oct 13, 2021: NONE. NONE. AFT EMERGENCY FLASHLIGHT INOP. MEL 2532 - AUTH# 10-100M-C ORIGINAL LOGPAGE 4755585 ITEM 1-C/A-RAR EMERGENCY AFT FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16-000-801
- [SDR SIMA20211007002](https://openairdocs.org/sdr/SIMA20211007002), Oct 7, 2021: NONE. NONE. AFT LAV FLASHLIGHT HOLDER BROKEN-C/A-DEFERRED AFT LAV FLASHLIGHT HOLDER BROKEN AUTH#100100M-C EXP.10/17/21 REF. MEL 25-32
- [SDR SIMA202108232001](https://openairdocs.org/sdr/SIMA202108232001), Aug 22, 2021: LAMP. INOPERATIVE. SEAT 12A OVERWING EMERGENCY LIGHT INOP-C/A-RAR SEAT 12A OVERWING EMERGENCY LIGHT LAMP IAW EMB145 AMM 33-50-07. OPC GOOD.
- [SDR SIMA20210618001](https://openairdocs.org/sdr/SIMA20210618001), Jun 18, 2021: LAMP. INOPERATIVE. AFT OVERWING EMERGENCY LIGHT INOP-C/A-RAR AFT OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A NO FIX. RAR OVERWING EMERGENCY
- [SDR SIMA20210521002](https://openairdocs.org/sdr/SIMA20210521002), May 21, 2021: LAMP. INOPERATIVE. RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD. END.
- [SDR SIMA20210513001](https://openairdocs.org/sdr/SIMA20210513001), May 13, 2021: CRADLE. BROKEN. FORWARD CABIN EMERGENCY FLASHLIGHT HAS BROKEN HOLDER.-C/A-RAR FORWARD CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16 AND ETN-EM-33-059. OPS CHECK 
- [SDR SIMA20210508002](https://openairdocs.org/sdr/SIMA20210508002), May 8, 2021: LAMP. INOPERATIVE. SEAT 12A AND ROW 7A AISLE EMERGENCY LIGHT INOP-C/A-RAR SEAT 12A AND 7A AISLE EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A OPS CHEC
- [SDR SIMA20210206001](https://openairdocs.org/sdr/SIMA20210206001), Feb 6, 2021: LAMP. INOPERATIVE. LH FWD EXTERIOR EMERGENCY LIGHT INOP-C/A-RAR LH FWD EXTERIOR EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10, NO FIX. PERFORMED TROUBLESHOOTING OF EMERGENCVY LIGH
- [SDR SIMA20201223002](https://openairdocs.org/sdr/SIMA20201223002), Dec 23, 2020: SMOKE DETECTOR. FALSE ACTIVATION. LAV SMOKE AT GATE. C/A: PERFORMED OPERATIONAL TEST OF LAV SMOKE SYSTEM, IAW EMB AMM 26-14-00, MESSAGE CLEARED.
- [SDR SIMA20201122001](https://openairdocs.org/sdr/SIMA20201122001), Nov 22, 2020: BULB. INOPERATIVE. AFT EMERGENCY LIGHT ON LT WING TO FUSELAGE PANEL INOPERABLE. C/A: REMOVED AND REPLACED EMERGENCY LIGHT BULB, IAW EMB 145 AMM 33-50-10. OPERATIONS CHECKED GOOD.
- [SDR SIMA20201030001](https://openairdocs.org/sdr/SIMA20201030001), Oct 30, 2020: LAMP. INOPERATIVE. DURING PS-2 CHECK FOUND LT EXTERNAL EMERGENCY LIGHT INOPERABLE. C/A: R & R LT EXTERNAL EMERGENCY LIGHT LAMP, IAW EMB 145 AMM 33-50-10.
- [SDR SIMA20201011001](https://openairdocs.org/sdr/SIMA20201011001), Oct 11, 2020: LAMP. INOPERATIVE. LT AFT OVERWING EMERGENCY LIGHT INOPERABLE. C/A: R & R LT AFT OVERWING EMERGENCY LIGHT LAMP, IAW AMM 33-50-10. OPERATIONS CHECK GOOD, IAW AMM 33-50-00.
- [SDR SIMA202009132001](https://openairdocs.org/sdr/SIMA202009132001), Sep 12, 2020: LIGHT. INOPERATIVE. DURING PS-1 FOUND LT EXTERNAL EMERGENCY LIGHT ABOVE WING INOP. C/A-R & R LT EXTERNAL EMERGENCY LIGHT ABOVE WING, IAW EMB 145 AMM 33-50-10.
- [SDR SIMA202008254004](https://openairdocs.org/sdr/SIMA202008254004), Aug 24, 2020: POWER SUPPLY. INOPERATIVE. MULITPLE INTERIOR EMERGENCY LIGHTS INOP, AISLE LIGHT 4, AISLE LIGHT 3, FLOOR STRIP 6, 7, 8-C/A-REMOVED AND REPLACED BATTERY POWER SUPPLY AND CHARGER ASSEMBLY #4
- [SDR SIMA202008254003](https://openairdocs.org/sdr/SIMA202008254003), Aug 24, 2020: POWER SUPPLY. INOPERATIVE. COCKPIT FLOOD LIGHT, AISLE LIGHT 1 EMERGENCY LIGHTS INOP-C/A-REMOVED AND REPLACED BATTERY POWER SUPPLY #1 AND CHARGER ASSEMBLY IAW EMB 145 AMM 33-50-04. OPERATI
- [SDR SIMA2020072019004](https://openairdocs.org/sdr/SIMA2020072019004), Jul 19, 2020: WARNING SYSTEM. ACTIVATED. TOO LOW TERRAIN AURAL WARNING INTERMITENTLY IN FLIGHT AT CRUISE FL 240.
- [SDR SIMA2020031210006](https://openairdocs.org/sdr/SIMA2020031210006), Mar 10, 2020: SPAR. CRACKED. DURING HMBV INSPECTION, QC FOUND THE LH WING SPAR I CRACKED AT RIB 9.-C/A-ACCOMPLISHED REPAR TO LH WING SPAR I AT RIB 9 IAW ERS-EM-57MR-1231.
- [SDR SIMA202003098005](https://openairdocs.org/sdr/SIMA202003098005), Mar 8, 2020: FLOOR SUPPORT. CORRODED. DURING HMBV INSPECTION, QC FOUND LH OMEGA BEAM SIDEWALL CORRODED BETWEEN FR 58-59.-C/A-REPAIRED LH OMEGA BEAM BETWEEN FR 58-59 IAW EO EM-53MR-1518 PT. A.
- [SDR SIMA202003098004](https://openairdocs.org/sdr/SIMA202003098004), Mar 8, 2020: FLOOR SUPPORT. CORRODED. DURING HMBV INSPECTION, QC FOUND CENTER OMEGA BEAM SIDEWALL CORRODED BETWEEN FR 58-59.-C/A-REPAIRED CENTER OMEGA BEAM BETWEEN FR 58-59 IAW EO EM-53MR-1518 PT. B
- [SDR SIMA202003054007](https://openairdocs.org/sdr/SIMA202003054007), Mar 4, 2020: SHEAR TIE. CORRODED. DURING HMBV INSPECTION, QC FOUND THE FR 65 SHEAR CLIP CORRODED AT THE CARGO DOOR LWR SILL.-C/A-PERFORMED PERMANENT REPAIR TO FR 65 SHEAR CLIP AT CARGO DOOR LWR 
- [SDR SIMA202003054006](https://openairdocs.org/sdr/SIMA202003054006), Mar 4, 2020: SHEAR TIE. CORRODED. DURING HMBV INSPECTION, QC FOUND THE FR 68 SHEAR CLIP CORRODED AT THE CARGO DOOR LWR SILL.-C/A-PERFORMED PERMANENT REPAIR TO FR 68 SHEAR CLIP AT CARGO DOOR LWR 
- [SDR SIMA202003054005](https://openairdocs.org/sdr/SIMA202003054005), Mar 4, 2020: DOOR SILL. CORRODED. DURING HMBV INSPECTION, QC FOUND THE CARGO DOOR CUTOUT LWR SILL CORRODED.-C/A-REMOVED AND REPLACED THE CARGO DOOR LWR SILL IAW EMB 145 SRM 51-40-02 AND 51-20-03
- [SDR SIMA202003036007](https://openairdocs.org/sdr/SIMA202003036007), Feb 26, 2020: FLOOR SUPPORT. CORRODED. OMEGA BEAM UNDER CENTER LAV FLOOR GUSSET IS CORRODED -C/A-REPAIRED OMEGA BEAM UNDER CTR LAV FLOOR GUSSET IAW EMB 145 SRM 53-24-10RE
- [SDR SIMA2020030420005](https://openairdocs.org/sdr/SIMA2020030420005), Feb 20, 2020: FRAME. CRACKED. FR25 IS CRACKED BETWEEN STR 16R-15R-C/A-INSTALLED SPLICE REPAIR ON FR25 BETWEEN STR16R-15R IAW EMB 145 SRM 53-00-04
- [SDR SIMA2020029007](https://openairdocs.org/sdr/SIMA2020029007), Feb 19, 2020: YOKE. CRACKED. RIGHT FWD PYLON LOWER YOKE WAS CRACKED. REMOVED AND INSTALLED SERVICABLE YOKE IAW ERS-EM-54MR-698.
- [SDR SIMA202003029007](https://openairdocs.org/sdr/SIMA202003029007), Feb 19, 2020: YOKE. CRACKED. RH FWD PYLON LWR YOKE CRACKED-C/A-REMOVED AND INSTALLED SERVICABLE YOKE IAW ERS-EM-54MR-698
- [SDR SIMA202002918004](https://openairdocs.org/sdr/SIMA202002918004), Feb 18, 2020: FITTING. CRACKED. LH ENGINE FWD YOKE LWR FWD FITTING CRACKED. REMOVED AND INSTALLED A SERVICABLE LT FWD YOKE LWR FWD FITTING IAW EO ERS-EM-54MR-698.
- [SDR SIMA202003027003](https://openairdocs.org/sdr/SIMA202003027003), Feb 17, 2020: SKIN. GOUGED. CARGO DOOR INNER LWR SKIN SECTION HAS MULTIPLE GOUGES AND CORRODED FASTENER HOLE-C/A-REPAIRED BAGGAGE DOOR INNER LWR SKIN SECTION INSTALLED DOUBLER IAW EMB 145 
- [SDR SIMA2020033014004](https://openairdocs.org/sdr/SIMA2020033014004), Feb 14, 2020: CROSSBEAM. CORRODED. CROSSBEAM AT FR 20 IS CORRODED.-C/A-COMPLETE:REMOVED AND REPLACED CROSSBEAM AT FR 20 IAW EMB145 SRM 51-40-02, ETN-EM-53-139
- [SDR SIMA2020032714003](https://openairdocs.org/sdr/SIMA2020032714003), Feb 14, 2020: CROSSBEAM. CORRODED. CROSSBEAM BETWEEN FR 24-25 IS CORRODED.-C/A-COMPLETE:REMOVED AND REPLACED CROSSBEAM BETWEEN FR 24-25 WITH SERVICEABLE PART IAW EMB 145 SRM 51-40-02
- [SDR SIMA2020032714002](https://openairdocs.org/sdr/SIMA2020032714002), Feb 14, 2020: WIRE. BROKEN. L/H EMERGENCY LIGHT STRIP #4 HAS A BROKEN WIRE.-C/A-COMPLETE:REPAIRED BROKEN WIRE ON #4 EMERGENCY LIGHT STRIP IAW EMB 145 SWPN 20-21-00. SEE E770710 FOR OPC OF 
- [SDR SIMA202001087004](https://openairdocs.org/sdr/SIMA202001087004), Jan 7, 2020: BULB. INOPERATIVE. ON PS CHECK FOUND RH FWD EXTERIOR EMG LIGHT INOP-C/A-REMOVED AND REPLACED RH FWD EXTERIOR EMG LIGHT BULB IAW AMM 33-50-10 OPS CHECK GOOD
- [SDR SIMA202001063004](https://openairdocs.org/sdr/SIMA202001063004), Jan 3, 2020: LIGHT. DAMAGED. FWD, RH PROXIMITY FLOOR STRIP IS DAMAGED.-C/A-REMOVED AND REPLACED RH PROXIMITY STRIP IAW AMM 33-50-12.
- [SDR SIMA202001063003](https://openairdocs.org/sdr/SIMA202001063003), Jan 3, 2020: CONNECTOR. BROKEN. MOST AFT PROXIMITY FLOOR LIGHT STRIP ELECTRICAL CONNECTOR BROKE OFF WIRING ON A/C SIDE.-C/A-INSTALLED NEW CONNECTOR IAW SWPM 20-50-01, COMPLIED WITH OPS CHECK I
- [SDR SIMA2020010229004](https://openairdocs.org/sdr/SIMA2020010229004), Dec 29, 2019: LAMP. INOPERATIVE. AFT EMERG. CEILING LIGHT IS INOP-C/A-REMOVED AND REPLACED AFT EMERG. CEILING LIGHT LAMP, OPC GOOD, IAW AMM 33-50-08
- [SDR SIMA201908264001](https://openairdocs.org/sdr/SIMA201908264001), Aug 24, 2019: ACM. FAILED. AFTER TAKEOFF FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN AND A BURNING SMELL. ALSO REPORTED AN ABNORMAL SOUND COMING FROM ENGINE OR ACM. "TRANSFERRED TO NRWC 
- [SDR SIMA201906132004](https://openairdocs.org/sdr/SIMA201906132004), Jun 12, 2019: SIGN. BROKEN. EXIT SIGN OVER THE SERVICE DOOR IS BROKEN AND COMING OFF-C/A-REMOVED AND REPLACED EXIT SIGN I/A/W A.M.M. 33-50-15 OPS CHECK NORMAL.
- [SDR SIMA201906065002](https://openairdocs.org/sdr/SIMA201906065002), Jun 5, 2019: INVERTER. INOPERATIVE. FROM SEATS 8A TO 11A [FLOOR STRIPS 4&5] FLOOR EMERGENCY PROXIMITY LIGHTS INOP-C/A-REMOVED AND REPLACED EMERGENCY LIGHT DC/AC INVERTER 5 IAW AMM 33-50-11,OPS TES
- [SDR SIMA201906043004](https://openairdocs.org/sdr/SIMA201906043004), Jun 3, 2019: HOLDER. FAILED. FO CHART HOLDER SMOKING-C/A-FOUND SMOKE COMING FROM CHART HOLDER LIGHT AND COCKPIT READING LIGHT CB POPED. RAR CHART HOLDER ASSEMBLY REF AMM 25-12-11. OPS CHECK
- [SDR SIMA2019021107005](https://openairdocs.org/sdr/SIMA2019021107005), Feb 7, 2019: LIGHT. MALFUNCTIONED. LH OVER-WING EMERGENCY LIGHT IS INOP.-C/A-COMPLIED WITH OPERATIONAL CHECK OF LH OVERWING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. NO DEFECT NOTED.
- [SDR SIMA2019020413004](https://openairdocs.org/sdr/SIMA2019020413004), Jan 30, 2019: FLAP SYSTEM. MALFUNCTIONED. FLAP FAIL ON FINAL-C/A-RAI LH FSA #1,#2 ,#3 IAW EMB 145 AMM 27-51-09 AND AMM 27-51-10 OPS TEST GOOD. REMOVED AND REPLACED LH FVS AIRFRAME CONNECTOR J1111 IAW EM
- [SDR SIMA20190125001](https://openairdocs.org/sdr/SIMA20190125001), Jan 25, 2019: SHAFT. CONTAMINATED. FLAP FAIL ON APPROACH AFTER FCF, 30 MIN IN FLT A/C COLD SOAKED FLAP FAIL ON EICAS UPON SELECTING FLAPS 9 DEGREES. C/A-TROUBLE SHOT IAW FIM 27-51-00-810-804-A FO
- [SDR SIMA201812076002](https://openairdocs.org/sdr/SIMA201812076002), Dec 6, 2018: ANTI-ICE VALVE. FAILED. AFTER PERFORMING ICE DET TEST IN THE AIR, E1 "OPEN" INSCRIPTION LIGHT EXTINGUISHED...WHICH IS REQ TO BE ILLUMINATED PER MEL 30-11.-C/A-REMOVED AND REPLACED #1 E
- [SDR SIMA201804160001](https://openairdocs.org/sdr/SIMA201804160001), Apr 16, 2018: BRAKE ASSY. LEAKING. DURING LANDING, SMOKE REPORTED COMING FROM LEFT LANDING GEAR. FOUND THE NR 4 BRAKE ASSEMBLY LEAKING. REPLACED IAW 32-600-14. FOUND THE NR 4 TIRE WORN TO LIMITS.

All 146: https://openairdocs.org/aircraft/N675AE/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/N675AE/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.