# N676AE: 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: 14500807
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 21, 2004
- Certificate issued: September 14, 2011
- Expires: September 30, 2027
- Mode S code: A8F207
- 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=676AE
- Page: https://openairdocs.org/aircraft/N676AE

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/N676AE/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 N676AE.

## 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 20101125055519I](https://openairdocs.org/incident/20101125055519I), Nov 25, 2010: Embraer EMB-145LR (N676AE), Memphis, TN, No damage. Aircraft was being vectored at 4000 ft to an ILS approach to rwy 36R. Shortly after intecepting the final approach course, it encountered turbulence, which was…

## Service difficulty reports (115, 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 SIMA20220519001](https://openairdocs.org/sdr/SIMA20220519001), May 19, 2022: NONE. UNSERVICEABLE. FWD F/A FLASHLIGHT BASE BROKEN-C/A-REMOVED & REPLACED FWD F/A FLASHLIGHT ASSY IAW AMM 33-50-16.OPS CK FOUND OK.
- [SDR SIMA20220502001](https://openairdocs.org/sdr/SIMA20220502001), May 2, 2022: NONE. NONE. BLEED 1 LEAK WARNING WITH APU BLEED OPEN PACK 1 ON-C/A-REMOVED AND REPLACED JOINT #1 AND #25 BLEED SYSTEM O-RINGS. LEAK CHECK GOOD IAW ETN-EM-36-038
- [SDR SIMA20211227005](https://openairdocs.org/sdr/SIMA20211227005), Dec 27, 2021: VALVE. LEAKING. LOUD NOISE AFTER STARTING ENGINE NR 2 FOLLOWED BY A VERY STRONG FISHY SMELL. PERFORMED GVI OF BOTH PACK DUCTS IAW EMB 145 AMM 21-51-14-200-801-A WHILE RUNNING P
- [SDR SIMA20211117004](https://openairdocs.org/sdr/SIMA20211117004), Nov 17, 2021: NONE. NONE. AFT EMERGENCY FLASHLIGHT HOLDER BROKEN.-C/A-RAR CABIN AFT EMERGENCY FLASHLIGHT AND BASE. OPS CHECKED GOOD IAW AMM 33-50-16.
- [SDR SIMA20210727001](https://openairdocs.org/sdr/SIMA20210727001), Jul 27, 2021: FLASHLIGHT ASSY. INOPERATIVE. FWD CABIN EMERGENCY FLASHLIGHT WILL NOT CHARGE REF: LOGPAGE 4702705 ITEM 1 MEL 2532 - AUTH# 070310M-C-C/A-RAR FWD CABIN EMEREGENCY FLASHLIGHT ASSY IAW EMB 145 A
- [SDR SIMA20210720002](https://openairdocs.org/sdr/SIMA20210720002), Jul 20, 2021: FLASHLIGHT. INOPERATIVE. CABIN FORWARD FLASHLIGHT INOP-C/A-DEFERRED FWD CAB FLASHLIGHT. M PROCEDURE C/W
- [SDR SIMA20210427003](https://openairdocs.org/sdr/SIMA20210427003), Apr 27, 2021: WARNING LIGHT. FALSE INDICATION. BLEED 2 FAIL ON TAKE-OFF ROLL AT 70 KNTS , TO-1 WAS SELECTED DUE TO PERFORMANCE MESSAGE WENT AWAY REJECTED TAKE-OFF.-C/A-DEFERRED ENGINE 2 BLEED SYSTEM, M PROCE
- [SDR SIMA20210114002](https://openairdocs.org/sdr/SIMA20210114002), Jan 14, 2021: WARNING MESSAGE. FALSE ACTIVATION. ABORTED TAKEOFF AT 40 KTS DUE TO WARNING MASTER LIGHT AND THEN 'TRIM' AURAL MESSAGE. THE TRIM WAS SET TO 8 UP. C/A: PERFORMED OPERATIONAL CHECK OF THE HORIZ STA
- [SDR SIMA20200706002](https://openairdocs.org/sdr/SIMA20200706002), Jul 6, 2020: WARNING SYSTEM. FALSE ACTIVATION. DURING FCF AURAL WARNING OF TOO LOW TERRAIN, STARTED AT 10,000 FT AND STOPPED AT 22,000 FT. NO AURAL WARNINGS AT 20,000 FT. DURING DESCENT, WARNING OCCURED AT 2
- [SDR SIMA202002031004](https://openairdocs.org/sdr/SIMA202002031004), Jan 31, 2020: SKIN. GOUGED. FUSELAGE SKIN IS GOUGED JUST BELOW PANEL 113EL AT FRAMES 6-7 BETWEEN STRINGERS 13L-15L-C/A-ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE SKIN GOUGE JUST BELOW PANEL
- [SDR SIMA202002030005](https://openairdocs.org/sdr/SIMA202002030005), Jan 30, 2020: CROSSBEAM. CORRODED. CENTER OMEGA BEAM CORRODED AT CROSS BEAM FRAME 49-C/A-ACCOMPLISHED REPAIR OF CENTER OMEGA BEAM CROSS BEAM FRAME 49 IAW EMB 145 SRM 53-00-10 FIG 203 AND ERS-EM-5
- [SDR SIMA202002030004](https://openairdocs.org/sdr/SIMA202002030004), Jan 30, 2020: FLOORBEAM. CORRODED. LH OMEGA BEAM IS CORRODED AT FRAME 29-C/A-ACCOMPLISHED REPAIR TO LH OMEGA BEAM CORROSION AT FRAME 29 IAW ERS-EM-53MR-4020 PT. A REV: ORIGINAL
- [SDR SIMA20200130002](https://openairdocs.org/sdr/SIMA20200130002), Jan 30, 2020: BEAM. CORRODED. LH OMEGA BEAM IS CORRODED AT FRAME 29-C/A-ACCOMPLISHED REPAIR TO LH OMEGA BEAM CORROSION AT FRAME 29 IAW ERS-EM-53MR-4020 PT. A REV: ORIGINAL.
- [SDR SIMA20200130001](https://openairdocs.org/sdr/SIMA20200130001), Jan 30, 2020: BEAM. CORRODED. CENTER OMEGA BEAM IS CORRODED AT FRAME 29-C/A-ACCOMPLISHED REPAIR TO CENTER OMEGA BEAM CORROSION AT FRAME 29 IAW ERS-EM-53MR-4017 PT. A REV: ORIGINAL
- [SDR SIMA202001297005](https://openairdocs.org/sdr/SIMA202001297005), Jan 27, 2020: RIB. CRACKED. LH WING RIB 21 FOUND CRACKED INSIDE PANEL 551CB-C/A-ACCOMPLISHED DOUBLER REPAIR OF LH WING RIB 21 IAW EMB 145 SRM 57-20-07 ITEM 4.
- [SDR SIMA202001297006](https://openairdocs.org/sdr/SIMA202001297006), Jan 27, 2020: SKIN. DAMAGED. THREE SHARP PROTRUSIONS WERE FOUND IN THE FUSELAGE SKIN BETWEEN FRAMES 27-28 AND STRINGERS 18L-19L-C/A-FORWARD PROTRUSION FOUND TO BE OUT OF LIMITS IAW EMB 145 
- [SDR SIMA202001276001](https://openairdocs.org/sdr/SIMA202001276001), Jan 26, 2020: FRAME. CRACKED. DURING HMBV INSPECTION, QA FOUND FRAME 66 IS CRACKED AT STRINGER 16R. -C/A-REMOVED AND REPLACED FRAME 66 IAW EMB 145 SRM 51-40-02.
- [SDR SIMA202001221001](https://openairdocs.org/sdr/SIMA202001221001), Jan 21, 2020: FLOOR SUPPORT. CORRODED. DURING HMBV INSPECTION, QA FOUND THE LH OMEGA BEAM CORRODED AT CROSS MEMBER FR-59-C/A-ACCOMPLISHED A PERMANENT REPAIR ON THE LH OMEGA BEAM AT CROSS MEMBER FR-59
- [SDR SIMA202001210002](https://openairdocs.org/sdr/SIMA202001210002), Jan 20, 2020: SHEAR TIE. CORRODED. DURING HMBV INSPECTION, QA FOUND THE CARGO DOOR CUTOUT FR 65 SHEAR CLIP CORRODED-C/A-PERFORMED A PERMANENT REPAIR ON THE CARGO DOOR CUTOUT FR 65 SHEAR CLIP IAW 
- [SDR SIMA202001210003](https://openairdocs.org/sdr/SIMA202001210003), Jan 20, 2020: DOOR SILL. CORRODED. DURING HMBV INSPECTION, QA FOUND THE CARGO DOOR SILL CORRODED-C/A-REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB 145 SRM 51-40-02. REPLACEMENT SILL P/N 145-25
- [SDR SIMA20200120001](https://openairdocs.org/sdr/SIMA20200120001), Jan 20, 2020: BEAM. CORRODED. HMBV INSPECTION, QA FOUND THE LH OMEGA BEAM CORRODED DURING UNDER CROSS MEMBER AT FR 54-C/A-ACCOMPLISHED A PERMANENT REPAIR ON THE LH OMEGA BEAM UNDER CROSS MEM
- [SDR SIMA2020012019006](https://openairdocs.org/sdr/SIMA2020012019006), Jan 19, 2020: SHUNT. CORRODED. DURING ACCOMPLISHMENT OF EO-2400-018 (APU SHUNT GROUND IMPROVEMENT), FOUND THE APU SHUNT AREA ON FR 80 TO BE CORRODED-C/A-ACCOMPLISHED APU SHUNT REPAIR ON FR 80
- [SDR SIMA202001176001](https://openairdocs.org/sdr/SIMA202001176001), Jan 16, 2020: SKIN. DENTED. AIRCRAFT ARRIVED WITH TDMI 676T5345 TO REPAIR A DENT TO THE RH CENTER FUSELAGE BETWEEN FR 15-16 AND STGR 12R-13R-C/A-PERFORMED PERMANENT REPAIR ON DENT ON RH CE
- [SDR SIMA2020021122006](https://openairdocs.org/sdr/SIMA2020021122006), Dec 20, 2019: WIRE. BROKEN. 1EA PROX LIGHT WITH OUT ARROWS HAVE BROKEN WIRES-C/A-COMPLETE:REMOVED AND REPLACED 1EA PROX LIGHT WITHOUT ARROWS IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD.
- [SDR SIMA2020021122007](https://openairdocs.org/sdr/SIMA2020021122007), Dec 20, 2019: CONNECTOR. DISCONNECTED. OVERWING CABIN CEILING PANEL FWD EMERGENCY EXIT SIGN DOES NOT ILLUMINATE-C/A-COMPLETE:CONNECTED CABIN OVERWING CEILING PANEL FWD EMERGENCY LIGHT AS REQUIRED IAW
- [SDR SIMA2020021122008](https://openairdocs.org/sdr/SIMA2020021122008), Dec 20, 2019: WIRE. BROKEN. LH NO. 3 EMERGENCY LIGHT STRIP DOES NOT ILLUMINATE-C/A-COMPLETE:SPLICED BROKEN WIRE W192-8679-22 AT LH FR 32/33 IAW EMB 145 SWPM 20-21-00, WM 33-50-50, AMM 33-5
- [SDR SIMA2020021122005](https://openairdocs.org/sdr/SIMA2020021122005), Dec 20, 2019: WIRE. BROKEN. AFT EMERGRNCY FLASHLIGHT BASE (SP3558)WIRE SPLICE BROKEN-C/A-COMPLETE:REPAIRED WIRE W775-0006-24BK/SP3558 ON AFT EMERGENCY FLASHLIGHT BASE IAW EMB 145 SWPM 20-2
- [SDR SIMA2020021120009](https://openairdocs.org/sdr/SIMA2020021120009), Dec 20, 2019: FLOOR SUPPORT. CORRODED. SSI #53-20-11 L/H OMEGA BEAM CORRODED AT CROSS BEAM FR-44-C/A-COMPLETE:ACCOMPLISHED PERMANENT REPAIR ON L/H OMEGA BEAM CORRODED AT CROSS BEAM AT FR-44 IAW ERS-E
- [SDR SIMA20190910001](https://openairdocs.org/sdr/SIMA20190910001), Sep 10, 2019: INVERTER. INOPERATIVE. #1 FLOOR PROX EMERG LIGHT STRIP IS INOP. C/A-REMOVED AND REPLACED #2 DC/AC EMERGENCE EXIT LIGHTING INVERTER. OPS CHECKED GOOD IAW AMM 33-50-11.
- [SDR SIMA201906187001](https://openairdocs.org/sdr/SIMA201906187001), Jun 17, 2019: TANK UNIT. FAILED. FUEL IND TANK NO 2 SHOWING DASHES. REMOVED AND REPLACED R/H TANK UNIT #4 IAW AMM 28-41-02. OPS CHECK GOOD.
- [SDR SIMA20190213002](https://openairdocs.org/sdr/SIMA20190213002), Feb 13, 2019: LIGHT. INOPERATIVE. EMERGENCY LIGHT OVER SERVICE DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT MARKING LIGHT. OPC GOOD IAW AMM 33-50-14.
- [SDR SIMA201812281004](https://openairdocs.org/sdr/SIMA201812281004), Dec 21, 2018: UNKNOWN. ODOR. STRONG BURNING / MILDEW MOLDY SMELL DURING VECTORS TO APPROACH AND LAND. OCCURRED AFTER MODERATE TURB DURING DESENT. WITH CONSTANT AND CONTINUOUS THRUST LEVER M
- [SDR SIMA201812241003](https://openairdocs.org/sdr/SIMA201812241003), Dec 21, 2018: HYDRAULIC SYSTEM. LEAKING. INBND MIA DECLARED EMRGENCY FOR BURNING OIL SMELL. LNDD SAFELY.IN REFERENCE TO LG PG 4445943 ITEM 1 STRONG BURNING SMELL, FOUND EVIDENCE OF A POSSIBLE EXTERNAL 
- [SDR SIMA2018121712010](https://openairdocs.org/sdr/SIMA2018121712010), Dec 12, 2018: UNKNOWN. ODOR. ON DESCENT AT FLIGHT IDLE, MUSKY SMELL / ODOR FOR ABOUT A MINUTE, WENT AWAY WHEN TAKEN OUT OF IDLE. NO NOTICE OF SMELL AFTER LANDING / TAXI. TRANSFERED TO NRWC 
- [SDR SIMA2018121412007](https://openairdocs.org/sdr/SIMA2018121412007), Dec 12, 2018: UNKNOWN. ODOR. ON DESCENT AT FLIGHT IDLE, MUSKY SMELL / ODOR FOR ABOUT A MINUTE, WENT AWAY WHEN TAKEN OUT OF IDLE. NO NOTICE OF SMELL AFTER LANDING / TAXI. TRANSFERED TO NRWC 
- [SDR SIMA201812110004](https://openairdocs.org/sdr/SIMA201812110004), Dec 10, 2018: UNKNOWN. ODOR. STRONG CHEMICAL ODOR IN COCKPIT AND CABIN ON DESCENT ENGINES WERE AT IDOL WHEN ODOR WAS FIRST SMELLED.-C/A-PERFORMED ENGINE RUNS AS PER ETN-EM-72-034. NO ODOR D
- [SDR SIMA201812108002](https://openairdocs.org/sdr/SIMA201812108002), Dec 8, 2018: LIGHT. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOP-C/A-REMOVD AND REPLACED SERVICER DOOR EMERGENCY LIGHT IAW EMB 145 AMM 33-50-09-000-801 AND 33-50-09-400-801 OPS CHECK GOOD
- [SDR SIMA201810154001](https://openairdocs.org/sdr/SIMA201810154001), Oct 14, 2018: BONDING JUMPER. BROKEN. SUPPLEMENTAL AT 36000 CABIN ALTITUDE WENT TO 10000 GOT A MASTER WARNING. C/A-DEFERRED PRESSURIZATION CONTROL SYS AUTOMATIC MODE (M) CW. MEL 21-17 AUTH 100429DM-
- [SDR SIMA2018072322002](https://openairdocs.org/sdr/SIMA2018072322002), Jul 22, 2018: ROLLER. DIRTY. MAIN DOOR DIFFICULT TO CLOSE. CLEAN AND SERVICED MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02. OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR SIMA201807121004](https://openairdocs.org/sdr/SIMA201807121004), Jul 11, 2018: LIGHT. INOPERATIVE. MAIN DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPC OF LIGHT LAMP GOOD AT THIS
- [SDR SIMA20180627001](https://openairdocs.org/sdr/SIMA20180627001), Jun 27, 2018: DOOR SEAL. LACK OF LUBE. FA REPORTS MAIN ENTRY DOOR VERY HARD TO OPEN & CLOSE. MAIN ENTRY DOOR SEAL AND FOLDABLE DOOR LUBRICATED IAW AMM 52-11-00 OPENING AND CLOSING CHECK PASS.
- [SDR SIMA2018061110001](https://openairdocs.org/sdr/SIMA2018061110001), Jun 10, 2018: LAMP. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-09-000-801-A, AND 33-50-09-400-801-A. OPS CHECKED GOOD.
- [SDR SIMA20180422002](https://openairdocs.org/sdr/SIMA20180422002), Apr 22, 2018: LAMP. INOPERATIVE. MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A-A. OPS CHECKED GOOD.
- [SDR SIMA20180406002](https://openairdocs.org/sdr/SIMA20180406002), Apr 6, 2018: SMOKE DETECTOR. FALSE ACTIVATION. CARGO SMOKE ILLUMINATED ON EICAS, BOTTLES BLOWN, WARNING ON BOTH EICAS AND CARGO EXTNGUISHING BUTTON. CARGO SMOKE DETECTOR AND RELAYS K0630, K0625, K0629 HAVE B
- [SDR SIMA2018003230002](https://openairdocs.org/sdr/SIMA2018003230002), Mar 22, 2018: LAMP. INOPERATIVE. MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. OPS CHEC
- [SDR SIMA201802220003](https://openairdocs.org/sdr/SIMA201802220003), Feb 20, 2018: BULB. INOPERATIVE. AFT CABIN FLASHLIGHT INOP. REMOVED AND REPLACED AFT CABIN FLASHLIGHT BULB IAW AMM 33-50-16. OPS CK GOOD MEL RESTORED.
- [SDR SIMA20180107004](https://openairdocs.org/sdr/SIMA20180107004), Jan 7, 2018: STRUCTURE. DAMAGED. MAIN CABIN PAX ENTRY DOOR WONT OPEN ALL THE WAY, PLASTIC PIECE IN THE WAY. REMOVED THE DOOR TRIM AND REMOVED AND REPLACED MAIN DOOR HINGE PANEL IAW AMM 25-23-04
- [SDR SIMA20171226004](https://openairdocs.org/sdr/SIMA20171226004), Dec 26, 2017: ACM. FAILED. DURING TAXI, RECEIVED A BOTH ENGINES OFF, SMOKE IN THE COCKPIT AND CABIN. FOLLOWED EPC PROCEDURES FOR CABIN COCKPIT FIRE, SMOKE, FUMES, AND SMOKE SUBSIDED. RAN 
- [SDR SIMA20171221004](https://openairdocs.org/sdr/SIMA20171221004), Dec 21, 2017: LIGHT. SMOKE. SMOKE FROM FIRST OFFICER`S CHART HOLDER LIGHT WHEN ON. REMOVED AND REPLACED THE CHART HOLDER IAW AMM 25-12-11. OPS CHECKED GOOD.
- [SDR SIMA20171019005](https://openairdocs.org/sdr/SIMA20171019005), Oct 19, 2017: LAMP. INOPERATIVE. MAIN DOOR ENTRY EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-06-000-801-A, AND 33-50-06-400-801-A.. OPS CHECKED GOOD.

All 115: https://openairdocs.org/aircraft/N676AE/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/N676AE/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.