# N683AE: 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: 14500833
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 4, 2004
- Certificate issued: September 14, 2011
- Expires: September 30, 2027
- Mode S code: A90E61
- 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=683AE
- Page: https://openairdocs.org/aircraft/N683AE

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/N683AE/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 N683AE.

## FAA accident and incident reports

None matched to N683AE.

## Service difficulty reports (166, 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 HNAA2026041200283](https://openairdocs.org/sdr/HNAA2026041200283), Apr 12, 2026: SWITCH. FAILED. MAIN PITCH TRIM INOP MESSAGE DURING CLIMB USING CAPT YOKE SWITCH. R&R PITCH TRIM SWITCH IAW EMBR AMM 27-40-03. PERFORMED HORIZONTAL STAB ADJUSTMENT TEST EMBR 14
- [SDR HNAA2026032700249](https://openairdocs.org/sdr/HNAA2026032700249), Mar 26, 2026: SWITCH. INTERMITTENT. DURING CLIMB PITCH TRIM MAIN AND BACKUP FAILED ON BOTH SIDES WITH NO EICAS MESSAGES, NO CMC MESSAGES. WAS STUCK UP 2 DEGREES. NO CMC MESSAGES. FACT 26MAR26 08:0
- [SDR HNAA2025100300661](https://openairdocs.org/sdr/HNAA2025100300661), Sep 26, 2025: FLOOR SUPPORT. CORRODED. F068535 CORROSION ON LH OTBD #2 FLOOR SILL. REMOVED AND REPLACED FLOOR SILL ON LH OTBD #2 FLOOR SILL IAW EMB145 SRM 51-40-02.
- [SDR HNAA2025100300670](https://openairdocs.org/sdr/HNAA2025100300670), Sep 9, 2025: SKIN. BUCKLED. F069494 RH WHEEL WELL INTERNAL SKIN IS BUCKLED AT FR3. REPAIRED BUCKLED RH WHEEL WELL INTERNAL SKIN AT FR 3 IAW PIEDMONT EO1-53-25-0329 AND ETD2025-145-928107.
- [SDR HNAA2025100300669](https://openairdocs.org/sdr/HNAA2025100300669), Sep 5, 2025: CROSSBEAM. DAMAGED. CROSSMEMBER AT FRAME 5 HAS ELONGATED FASTENER HOLES NEAR STGR 15R. REPAIRED CROSSMEMBER AT FR 5 ELONGATED FASTENER HOLES NEAR STR 15R IAW EO1-53-25-0326 AND ETD
- [SDR HNAA2025100300668](https://openairdocs.org/sdr/HNAA2025100300668), Sep 5, 2025: FRAME. DAMAGED. FRAME 5 HAS ELONGATED FASTENER HOLES NEAR STGR 15R. REPAIRED FR 5 ELONGATED FASTENER HOLES NEAR STR 15R IAW EO1-53-25-0330 AND ETD2025-145-927849.
- [SDR HNAA2025100300675](https://openairdocs.org/sdr/HNAA2025100300675), Sep 4, 2025: SHEAR TIE. DAMAGED. FRAME 3 BETWEEN STR 14R AND 17R IS DENTED AND BENT AT SKIN ATTACHMENT FLANGE. RAR FR3 BETWEEN STGR 11R-19R IAW EMB 145 SRM 51-40-02
- [SDR HNAA2025100300667](https://openairdocs.org/sdr/HNAA2025100300667), Sep 4, 2025: FRAME. DAMAGED. FRAME 4 IS DAMAGED AT STGR 15R. REPAIRED FR 4 DAMAGE AT STR 15R IAW PIEDMONT EO1-53-25-0327 AND ETD2025-145-927854.
- [SDR HNAA202510030075](https://openairdocs.org/sdr/HNAA202510030075), Sep 4, 2025: FRAME. DAMAGED. FRAME 3 BETWEEN STR 14R AND 17R IS DENTED AND BENT AT SKIN ATTACHMENT FLANGE. RAR FR3 BETWEEN STGR 11R-19R IAW EMB 145 SRM 51-40-02
- [SDR HNAA2025100300674](https://openairdocs.org/sdr/HNAA2025100300674), Sep 4, 2025: STRINGER. DAMAGED. STRINGER 14R HAS AN OVERSIZED HOLE AT FR2. RAR STRINGER 14R BTW FR 1A-6 IAW EMB 145 SRM 51-40-02. DURING REPLACEMENT FOUND 13 HOLES BETWEEN FR 2-3 TO ONLY HAVE 
- [SDR HNAA2025100300676](https://openairdocs.org/sdr/HNAA2025100300676), Sep 4, 2025: FRAME. DAMAGED. FRAME 4 IS DAMAGED AT STGR 15R. REPAIRED FR 4 DAMAGE AT STR 15R IAW EO1-53-25-0327 AND ETD2025-145--927854.
- [SDR HNAA2025100300664](https://openairdocs.org/sdr/HNAA2025100300664), Aug 27, 2025: FLOOR SUPPORT. CORRODED. F068625 GALLEY FLOOR SUPPORT BRACKET AT FR-23 AND STGR-16 HAS CORROSION. RAR GALLEY FLOOR SUPPORT BRACKET AT FR-23 AND R/H STGR 16 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2025100300673](https://openairdocs.org/sdr/HNAA2025100300673), Aug 26, 2025: SHEAR TIE. CRACKED. F068552 SHEAR CLIP IS CRACKED AT FRAME 26 BETWEEN STRINGERS 16R-17R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 26 BETWEEN STRINGERS 16R-17R IAW EMB 145 SRM 51-40
- [SDR HNAA2025100300672](https://openairdocs.org/sdr/HNAA2025100300672), Aug 26, 2025: SKIN. DAMAGED. F068464 FWD FUSELAGE I SKIN PANEL FROM FR 1A-3 STR 14R TO THE NLG CUTOUT REQUIRES REPLACEMENT DUE TO MULTIPLE TOOL MARKS. REMOVED MULTIPLE TOOLING MARKED FWD FU
- [SDR HNAA2025100300666](https://openairdocs.org/sdr/HNAA2025100300666), Aug 26, 2025: FLOOR SUPPORT. CORRODED. F068510 CABIN L/H OMEGA BEAM GUSSET BETWEEN FR-35/38 HAVE CORROSION. REMOVED AND REPLACED CABIN L/H OMEGA BEAM GUSSET #4 IAW EMB 145 SRM 51-40-02
- [SDR HNAA2025100300665](https://openairdocs.org/sdr/HNAA2025100300665), Aug 26, 2025: FLOORBEAM. CORRODED. F068508 CORROSION ON LH #3 FLOOR BEAM GUSSET. REMOVED AND REPLACED LH #3 FLOOR BEAM GUSSET IAW EMB 145 SRM 51-40-02
- [SDR HNAA2025100300663](https://openairdocs.org/sdr/HNAA2025100300663), Aug 26, 2025: FLOORBEAM. CORRODED. F068549 CORROSION ON RH CROSS FLOORBOARD SUPPORT AT FRAME 28. R & R RH CROSS FLOORBOARD SUPPORT AT FRAME 28 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2025100300662](https://openairdocs.org/sdr/HNAA2025100300662), Aug 26, 2025: FLOOR SUPPORT. CORRODED. F068545 CABIN L/H OMEGA BEAM GUSSET BETWEEN FR-51/53 HAVE CORROSION. REMOVED AND REPLACED L/H OMEGA BEAM GUSSET #6 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2025100300660](https://openairdocs.org/sdr/HNAA2025100300660), Aug 26, 2025: FLOOR SUPPORT. CRACKED. F068523 CABIN CENTER OMEGA BEAM GUSSET BETWEEN FR-39/42 HAVE CORROSION. REMOVED AND REPLACED CABIN CENTER OMEGA BEAM GUSSET BTW FR 39-42 (NO.4) IAW EMB 145 SRM 
- [SDR HNAA2025100300671](https://openairdocs.org/sdr/HNAA2025100300671), Aug 20, 2025: SKIN. CRACKED. F066756 REAR FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACK AT FR 77 BETWEEN STGR 6R / 7R. ACCOMPLISHED BUSHING REPAIR ON REAR FUSELAGE EXTERNAL SKIN AT FR 77 BETWEE
- [SDR HNAA2023120400454](https://openairdocs.org/sdr/HNAA2023120400454), Dec 3, 2023: UNKNOWN. UNKNOWN. AUTO FAIL WITH AUTO TRIM FAIL. OPS CHECK AUTOPILOT AND AUTO PILOT TRIM IAW 22-11-00. OPS CHECK GOOD CLEAR MEL 22-1-1.
- [SDR HNAA2023051600160](https://openairdocs.org/sdr/HNAA2023051600160), May 15, 2023: UNKNOWN. UNKNOWN. PACK 2 OVERHEAT DISPLAYED ON EICAS DURING TAKE OFF, AIR COND PACK N650 AND ABOVE AMENDED. R & R PACK 2 OVERTEMP SWITCH, TEMP SENSOR, AND CONDENSOR MIXER. RAN EN
- [SDR HNAA2023031100079](https://openairdocs.org/sdr/HNAA2023031100079), Mar 5, 2023: UNKNOWN. UNKNOWN. VERTICAL STABILIZER LH AND RH SPHERICAL BEARING HOUSINGS ARE OUT OF DIMENSIONAL TOLERANCE. REPAIRED IAW EO1-55-23-0044
- [SDR HNAA2023031000074](https://openairdocs.org/sdr/HNAA2023031000074), Feb 27, 2023: UNKNOWN. UNKNOWN. COCKPIT LH LATERAL BRACKET, LH OF OVERHEAD PANEL, BETWEEN FR 12 AND 13 CRACKED. REPAIRED IAW 145 SRM51-40-02
- [SDR HNAA2023031000075](https://openairdocs.org/sdr/HNAA2023031000075), Feb 26, 2023: NONE. NONE. PILOT'S BULKHEAD UPPER OTBD GUIDE PIN HOLE IS GOUGED. REPAIRED IAW EO1-53-23-0046
- [SDR HNAA2023031100082](https://openairdocs.org/sdr/HNAA2023031100082), Feb 23, 2023: UNKNOWN. UNKNOWN. LH WING TIP UPPER ATTACHMENT FLANGE IS SCRATCHED. REPAIRED IAW EMB145 SRM 51-10-03 AND 57-20-07AD
- [SDR HNAA2023031100080](https://openairdocs.org/sdr/HNAA2023031100080), Feb 23, 2023: UNKNOWN. UNKNOWN. FRAME 65 IS CHAFED BETWEEN STRINGERS 2L-3L. REPAIRED IAW ETD 2023-145-004197
- [SDR HNAA2023031000076](https://openairdocs.org/sdr/HNAA2023031000076), Feb 23, 2023: UNKNOWN. UNKNOWN. RH FWD VERTICAL STAB TO FUSELAGE ANGLE HAS POSSIBLE CRACK AT MARKED LOCATIONS. REPAIRED IAW EMB145 SRM 51-40-02
- [SDR HNAA2023031000073](https://openairdocs.org/sdr/HNAA2023031000073), Feb 23, 2023: UNKNOWN. UNKNOWN. AFT UPPER L/H SIDE OF FUSELAGE FR78 HAS ONE (1) FASTNER WITH POSSIBLE CRACKED SKIN. REPAIRED IAW EO1-53-23-0042
- [SDR HNAA2023031000072](https://openairdocs.org/sdr/HNAA2023031000072), Feb 23, 2023: UNKNOWN. UNKNOWN. AFT UPPER L/H SIDE OF FUSELAGE FR78 HAS ONE (1) FASTNER WITH POSSIBLE CRACKED SKIN. REPAIRED IAW EO1-53-23-0042
- [SDR HNAA2023030800064](https://openairdocs.org/sdr/HNAA2023030800064), Feb 22, 2023: UNKNOWN. UNKNOWN. LEVEL 2 CORROSION ON CARGO DOOR SILL. REPAIRED IAW SRM 51-40-02, 51-20-03, AND 51-40-06
- [SDR HNAA2023030800086](https://openairdocs.org/sdr/HNAA2023030800086), Feb 19, 2023: UNKNOWN. UNKNOWN. LEVEL 2 CORROSION IN LAV FLOOR GUSSET BETWEEN FRAMES 59-61. REPAIRED IAW EMB145 SRM 51-10-03, 51-40-02, 51-20-03, AND 53-24-10AD
- [SDR HNAA2023031100077](https://openairdocs.org/sdr/HNAA2023031100077), Feb 19, 2023: UNKNOWN. UNKNOWN. LEVEL 2 CORROSION IN GALLEY FLOOR LH CROSSBEAM AT FRAME 18. REPAIRED IAW EMB145 SRM 51-40-02, 51-20-01, AND 51-21-06.
- [SDR HNAA2023030800068](https://openairdocs.org/sdr/HNAA2023030800068), Feb 19, 2023: UNKNOWN. UNKNOWN. LEVEL 2 CORROSION ON CROSS BEAM BRACKET BETWEEN LH FLOOR GUSSET AND LH FLOOR SIL IN LAV AREA BETWEEN FRAMES 60-61. REPAIRED IAW EMB145 SRM 51-20-03 AND 51-40-02
- [SDR HNAA2023030800067](https://openairdocs.org/sdr/HNAA2023030800067), Feb 19, 2023: UNKNOWN. UNKNOWN. LEVEL 2 CORROSION ON SPLICE BRACKET ON LH FLOOR SILL IN LAV BETWEEN FRAMES 60-61. REPAIRED IAW EMB145 SRM 51-20-03, AND 51-40-02.
- [SDR HNAA2023030800066](https://openairdocs.org/sdr/HNAA2023030800066), Feb 19, 2023: NONE. NONE. LEVEL 2 CORROSOIN IN LAV FLOOR GUSSET BETWEEN FRAMES59-61. REPAIRED IAW EMB145 SRM 51-10-03, 53-24-10AD, 51-40-02, AND 51-20-03.
- [SDR HNAA2023030800065](https://openairdocs.org/sdr/HNAA2023030800065), Feb 16, 2023: UNKNOWN. UNKNOWN. LEVEL 2 CORROSION ON LH #3 FLOOR SILL. REPAIRED IAW EMB145 SRM 51-40-02, 51-20-03, AND 51-40-09
- [SDR HNAA2023030800062](https://openairdocs.org/sdr/HNAA2023030800062), Feb 12, 2023: UNKNOWN. UNKNOWN. LEVEL 2 CORROSOIN ON INTERNAL FUSELAGE REINFORCEMENT SKIN PLATE BETWEEN FRAMES 61-62 STRINGERS 20L-21L. REPAIRED IAW EMB145 SRM 51-40-02 AND SB145-53-0068 FIG 7
- [SDR HNAA2023030800063](https://openairdocs.org/sdr/HNAA2023030800063), Feb 11, 2023: UNKNOWN. UNKNOWN. LEVEL 2 CORROSION ON INTERNAL FUSELAGE SKIN PLATE BETWEEN FRAMES 62-63 STRINGERS 20L-21L. REPAIRED IAW EMB145 SRM 51-40-02 AND SB145-53-0068
- [SDR HNAA2023010500018](https://openairdocs.org/sdr/HNAA2023010500018), Jan 4, 2023: CLAMP. LOOSE. ON DESENT, ACFT THROUGH RAIN & TURBULENCE. A SUDDEN ELECTRICAL ODOR IN FLT DECK & GALLEY FOR APPROX 5 MINS. ODOR DISSIPATED ON ITS OWN WITHOUT CREW INPUT. AT GA
- [SDR HNAA2022111400302](https://openairdocs.org/sdr/HNAA2022111400302), Nov 12, 2022: LOCALIZER. FAULTED. BOTH LOCALIZER SIGNALS UNRELIABLE ON APPROACH TO FWA. DIVERTED TO DAY. PERFORMED VOR/ILS SYSTEM OPERATIONAL TEST IAW AMM 34-32-00-700-801-A. VOR/ILS SYSTEMS #1 
- [SDR HNAA2022062300226](https://openairdocs.org/sdr/HNAA2022062300226), Jun 22, 2022: NONE. NONE. PDIS 683 28-41 2646932 22JUN22 CLT CLOSE AFTER TAKE OFF #1 FUEL QTY READ 0 AND TOTAL FUEL QTY READ 0 FACT 22JUN22 18:39 CLT UPON ARRIVAL TO A/C FOUND FUEL QTY T
- [SDR HNAA2021102600523](https://openairdocs.org/sdr/HNAA2021102600523), Oct 23, 2021: CONTROL UNIT. FAULTED. FLAP FAILURE ON APPROACH, FLAP FAIL STUCK ON 14 DEGREES. R+R FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02-000/400-801-A. OPS CHECK GOOD OK FOR SERVICE.
- [SDR HNAA2021052500224](https://openairdocs.org/sdr/HNAA2021052500224), May 21, 2021: INDICATOR. FAULTED. PDIS 683 28-41 2407312 21MAY21 GSP CLOSE ON DECENT FUEL 1 QTY DISPLAYED 0LBS. 10 MINUTES LATER FUEL QTY 2 DISPLAYED 0LBS. BOTH INDICATIONS CAME BACK AFTER 1 MIN
- [SDR HNAA2021030800094](https://openairdocs.org/sdr/HNAA2021030800094), Mar 7, 2021: UNKNOWN. ODOR. PDIS 683 21-01 2532571 08MAR21 FLO ASSGN PACK 2 OVERHEAT WITH BURNING SMELL IN COCKPIT AND TR OUBLE COOLING A/C. BURNING SMELL ALSO NOTICED WITH O NLY PACK 1 RU
- [SDR HNAA2021021100048](https://openairdocs.org/sdr/HNAA2021021100048), Feb 10, 2021: UNKNOWN. ODOR. PDIS 683 21-01 2343301 10FEB21 SDF CLOSE ON TAKEOFF AT APPROX 115KTS BURNING SMELL NOTICED IN FLIGHT DECK, FOLLOWED BY ICE COND A/ICE INOP MSG ON EICAS. FACT 10
- [SDR HNAA2021010500004](https://openairdocs.org/sdr/HNAA2021010500004), Dec 31, 2020: SWITCH. MALFUNCTIONED. AFTER T/O SMOKE SMELL IN COCKPIT. SHORTLY AFTER PACK 1 OVERHEAT MESSAGE ON EICAS. PACK 1 SHUTDOWN AUTOMATICALLY AND SMELL DISAPPATED W/I 3-4 SECONDS. CW FIM TAS
- [SDR HNAA2020120700336](https://openairdocs.org/sdr/HNAA2020120700336), Dec 5, 2020: PRESSURE SWITCH. MALFUNCTIONED. PDIS 683 27-21 2302681 05DEC20 ALB CLOSE. ON CLIMB OUT RUD 1-2 FAIL EICAS MESSAGE PRESENTED. PERFORMED QRH RUD SYSTEM 1 CAME BACK ONLINE. FACT 05DEC20 12:34 ALB
- [SDR HNAA2020051800149](https://openairdocs.org/sdr/HNAA2020051800149), May 9, 2020: SENSOR. FAILED. FLAP FAIL EICAS MESSAGE ON ARRIVAL TO HTS WHEN FLAPS SELECTED TO 9 DEGREES WITH NO FLAP MOVEMENT. R&R'D L/H FLAP VELOCITY SENSOR IAW AMM 27-51-12. RAN FLAPS UP 
- [SDR HNAA2020050500148](https://openairdocs.org/sdr/HNAA2020050500148), May 4, 2020: WARNING SYSTEM. FALSE ACTIVATION. FLAP FAIL ON EICAS WHEN FLAPS SELECTED DOWN. TROUBLESHOT IAW FIM TASK 27-51-00-810-816-A, STEPS 1,2,3, OPS CHECK IAW 27-51-00-700-801-A. NO DEFECTS NOTED AT THI

All 166: https://openairdocs.org/aircraft/N683AE/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/N683AE/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.