# N689EC: 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: 14500853
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 6, 2004
- Certificate issued: September 29, 2011
- Expires: September 30, 2027
- Mode S code: A9250D
- 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=689EC
- Page: https://openairdocs.org/aircraft/N689EC

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/N689EC/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 N689EC.

## FAA accident and incident reports

None matched to N689EC.

## Service difficulty reports (171, 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 HNAA2026071300594](https://openairdocs.org/sdr/HNAA2026071300594), Jul 11, 2026: HYDRAULIC SYSTEM. LOW. HYD 1 LOW DISPLAYED IN FLIGHT. SERVICED NR 1 HYD SYSTEM IAW AMM 12-13-01. OPS CHECK GOOD AT THIS TIME. OK FOR SERVICE
- [SDR HNAA2026052600434](https://openairdocs.org/sdr/HNAA2026052600434), May 23, 2026: BLEED VALVE. FAILED. E1 HSV FAIL ON EICAS FACT 23MAY26 17:19 GSO. R & R NR 1 HSV IAW AMM 36-11-02. OPS AND LEAK CHECK GOOD.
- [SDR HNAA2026050400366](https://openairdocs.org/sdr/HNAA2026050400366), May 2, 2026: WINDSHIELD. NO DISCREPANCY. BIRD STRIKE DURING TAKEOFF. PERFORMED BIRDSTRIKE INSPECTION IAW 05-50-08. CLEANED BIRD REMAINS OFF WINDSHIELD. NO DAMAGE/DEFECTS NOTED. AIRCRAFT OK FOR SERVICE 
- [SDR HNAA2026020100107](https://openairdocs.org/sdr/HNAA2026020100107), Feb 1, 2026: ADC. FAILED. ADC 1 FAILED IN FLIGHT FACT 01FEB26 17:47 ALB R&R'D ADC1 AT POS 100 IAW EMB145 AMM 34-15-01. PERFORMED LEAK CHECK IAW AMM 34-13-00. OPS CHECK DONE IAW AMM 34-15
- [SDR HNAA2025090100583](https://openairdocs.org/sdr/HNAA2025090100583), Aug 30, 2025: ACM. SMOKE. SMOKE IN CABIN DURING CRUISE AT FL250. INSPECTED PACK SYSTEM, FOUND #200 ACM SIEZED W/ MELTED DUCTS ON #200 DUAL TEMP CONTROL VALVE. R/R'D DUCTS ON #200 DUAL TE
- [SDR HNAA2025081200567](https://openairdocs.org/sdr/HNAA2025081200567), Aug 12, 2025: FAN. CLOGGED. FA REPORTS RUBBER HOSE SMELL WITH HISSING NOISE IN A ISLE GASPER AREA BETWEEN ROWS 2 AND 8 WITH GASPER FAN RUNNING. FOUND SEAT 8B GASPER TO BE CLOGGED. R/R'D PS
- [SDR HNAA2025040800197](https://openairdocs.org/sdr/HNAA2025040800197), Apr 9, 2025: ENGINE. BIRD INGESTION. BIRD STRIKE ON #2 ENGINE. #2 ENG CHANGE. SEE W/C 71-00-00 ON WORK PACKAGE.
- [SDR HNAA2025030300117](https://openairdocs.org/sdr/HNAA2025030300117), Mar 2, 2025: BLEED VALVE. ABNORMAL. REJECTED T/O WITH HSV 2 FAIL DISPLAYED MSG WENT AWAY AFTER THRUST LEVERS PULLED BACK (DEACTIVATED BLEED VLV 2). R&R'D #200 HSV IAW 36-11-02-04 OPS CHECK GOOD NO
- [SDR HNAA2024103001043](https://openairdocs.org/sdr/HNAA2024103001043), Sep 30, 2024: FLOOR SUPPORT. CORRODED. E058889 CARGO DOOR LOWER CUTOUT FLOOR SILL CORRODED. RAR CARGO DOOR LOWER CUTOUT FLOOR SILL IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024103001048](https://openairdocs.org/sdr/HNAA2024103001048), Sep 28, 2024: FLOOR SUPPORT. CORRODED. E058583 PAX DOOR LWR FWD FLOOR SUPPORT HAS CORROSION AROUND NUT-PLATES HOLES. RAR PAX DOOR LWR FWD FLOOR SUPPORT IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024103001047](https://openairdocs.org/sdr/HNAA2024103001047), Sep 28, 2024: FLOORBEAM. CORRODED. E058611 GALLEY FLOOR CROSSBEAM AT FR-20 BETWEEN STGRS 21L/18L HAS CORROSION. BLENDED OUT CORROSION ON GALLEY FLOOR CROSSBEAM AT FR-20 BETWEEN STGRS 21L/18L IAW 
- [SDR HNAA2024103001046](https://openairdocs.org/sdr/HNAA2024103001046), Sep 28, 2024: FLOOR SUPPORT. CORRODED. E058596 PAX DOOR LWR AFT FLOOR SUPPORT HAS CORROSION AROUND NUT-PLATES HOLES. RAR PAX DOOR LWR AFT FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024103001042](https://openairdocs.org/sdr/HNAA2024103001042), Sep 28, 2024: DOOR SILL. CORRODED. E058598 SERVICE DOOR LWR CENTER SILL HAS CORROSION AROUND NUT-PLATES HOLES. PREPPED, FABRICATED, AND INSTALLED DOUBLERS ON SERVICE DOOR CENTER SILL IAW EMB 145 
- [SDR HNAA2024103001045](https://openairdocs.org/sdr/HNAA2024103001045), Sep 27, 2024: ATTACH FITTING. GOUGED. E058125 RH AILERON DAMPENER ATTACHMENT FITTING IS GOUGED IN MULTIPLE AREAS (ON AILERON). REMOVED AND REPLACED RH AILERON DAMPENER FITTING IAW EMB 145 SRM 51-40-
- [SDR HNAA2024103001041](https://openairdocs.org/sdr/HNAA2024103001041), Sep 27, 2024: HOUSING. CORRODED. E058328 RH HORIZONTAL STAB SPHERICAL BEARING HOUSING PITTED. RPAIRED IAW SRM 55-30-02
- [SDR HNAA2024103001040](https://openairdocs.org/sdr/HNAA2024103001040), Sep 27, 2024: PROFILE. CORRODED. E058190 PAX DOOR LWR AFT PROFILES HAS CORROSION AROUND NUTPLATES HOLES. REPAIRED IAW EMB 145 SRM 52-10-04 STEP 3 FIGURE 201 SHEET 3 AND PIEDMONT EO1-52-24-0623.
- [SDR HNAA2024103001044](https://openairdocs.org/sdr/HNAA2024103001044), Sep 23, 2024: TORQUE BOX. DAMAGED. E056822 RH WING TORQUE BOX 1 LOWER FWD CENTER FASTENER HOLE IS OVERSIZED AND DAMAGED. PREPPED, FABRICATED, AND INSTALLED BUSHINGS AND HILOCK IN RH WING TORQUE B
- [SDR SIMA20220103001](https://openairdocs.org/sdr/SIMA20220103001), Jan 3, 2022: NONE. NONE. INCORRECT FLIGHT ATTENDANT FLASHLIGHT INSTALLED-C/A-RAR FA FLASHLIGHT WITH CORRECT LED FLASHLIGHT ASSY IAW EMB-145 AMM 33-50-16 AND ETN-EM-33-059. OPC GOOD.
- [SDR SIMA20211217001](https://openairdocs.org/sdr/SIMA20211217001), Dec 17, 2021: NONE. NONE. E2 SHUTOFF AT FL240/ SPD 290KTS/ OIL QUANTITY WENT TO RED AT 3 QTS. FLT DECLRD EMERG. LANDED SAFELY-C/A-REMOVED AND REPLACED #2 ENGINE IAW ENGINE REMOVAL AND IN
- [SDR SIMA20211212001](https://openairdocs.org/sdr/SIMA20211212001), Dec 12, 2021: NONE. NONE. FWD FA EMERGENCY FLASHLIGHT HOLDER ASSEMBLY BROKEN-C/A-FLIGHT CREW PLACARDED FWD FA EMERGENCY FLASHLIGHT HOLDER ASSEMBLY M PROCEDURES C/W REF: MEL 25-32 AUTH: 1
- [SDR SIMA20210920003](https://openairdocs.org/sdr/SIMA20210920003), Sep 20, 2021: NONE. NONE. CA DECLARED EMERGENCY DUE TO UNRELIABLE AIRSPEED. AMBER IAS ON AIRSPEED INDICATOR FOLLOWED BY SPS ADVANCED EICAS MSG. QRH PROCEDURE C/W. AIRSPEED RETURNED TO NO
- [SDR SIMA20210614001](https://openairdocs.org/sdr/SIMA20210614001), Jun 14, 2021: LIGHT. INOPERATIVE. FLOOR EMERGENCY LIGHTS, 2 AND 3 INOP. R & R 2 AND 3 FLOOR PROXIMITY EMERGENCY LIGHT STRIPS IAW EMB145 AMM 33-50-12. OPS CHECK GOOD
- [SDR SIMA20210516003](https://openairdocs.org/sdr/SIMA20210516003), May 16, 2021: INVERTER. INOPERATIVE. ROW 12 OVERHEAD EMERGENCY LIGHT INOP-C/A-RAR #6 EMERGENCY DC/AC INVERTER IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. OPC GOOD
- [SDR SIMA20210301002](https://openairdocs.org/sdr/SIMA20210301002), Mar 1, 2021: WIRE. DAMAGED. SEVENTH EMERGENCY LIGHT STRIP ON LH SIDE FLOOR WIRES DAMAGED, LIGHT INOP-C/A-RAR FLOOR STRIP EMERGENCY LIGHT IAW EMB145 AMM 33-50-12. OPS CHECK GOOD.
- [SDR SIMA202009098005](https://openairdocs.org/sdr/SIMA202009098005), Sep 8, 2020: WARNING MESSAGE. ILLUMINATED. SPS 2 INOP WARNING AND SPS ADVANCED CAUTION ON EICAS DURING APPROACH TO LANDING. C/A PERFORMED FIM TASKS 27-36-00. SPS ADVANCED MESSAGE REMAINS, SEE AML 4558647
- [SDR SIMA202009065002](https://openairdocs.org/sdr/SIMA202009065002), Sep 5, 2020: CLAMP. LOOSE. BLEED 1 LEAK IN FLIGHT (DIVERTED BACK TO DFW) NO EMERGENCY DECLARED. -C/A-OPENED PACK 1 TO VERIFY BLEED LEAK TIGHTENED HOSE CLAMPS WAITED FOR EICAS MESSAGE. OPC
- [SDR SIMA202009064001](https://openairdocs.org/sdr/SIMA202009064001), Sep 4, 2020: COMPUTER. MALFUNCTIONED. ON DESCENT SPS 2 INOPERABLE WARNING WENT AWAY, BUT CAME RIGHT BACK AS WE RAN THE QRH SPS 1 INOPERABLE AS WELL WE ALSO RECEIVED STICK PUSHER FAIL AND SPS ADVANCE
- [SDR SIMA20200827001](https://openairdocs.org/sdr/SIMA20200827001), Aug 27, 2020: DOOR SILL. CORRODED. SSI 53-30-48; CARGO DOOR SILL IS CORRODED. -C/A-EVALUATED CORROSION ON CARGO DOOR CENTER SILL AND FOUND TO BE OUT OF LIMITS IAW EMB 145 SRM 53-31-15AD. REMOVED 
- [SDR SIMA202008276002](https://openairdocs.org/sdr/SIMA202008276002), Aug 26, 2020: STRUCTURE. CORRODED. SSI 53-30-03; FRAME 68 CARGO DOOR LATERAL L-SHAPE IS CORRODED. -C/A-ACCOMPLISHED PERMANENT REPAIR ON FRAME 68 CARGO DOOR LATERAL L-SHAPE SHEAR CLIP IAW EMB 145 
- [SDR SIMA202008276001](https://openairdocs.org/sdr/SIMA202008276001), Aug 26, 2020: RIB. CRACKED. LH WING RIB 21 IS CRACKED INSIDE PANEL 551CB (AS MARKED).-C/A-REMOVED, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND SHIM AT LH WING RIB 21 IAW EMB 145 S
- [SDR SIMA202008242004](https://openairdocs.org/sdr/SIMA202008242004), Aug 22, 2020: WEB. GOUGED. CARGO DOOR INTERNAL WEB STRUCTURE GOUGED. REPAIRED CARGO DOOR INNER WEB IAW SRM 52-30-01.
- [SDR SIMA202008242002](https://openairdocs.org/sdr/SIMA202008242002), Aug 22, 2020: SKIN. CRACKED. LH UPPER AFT FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L, CRACK IS APPROX. 3/8? LONG ENDS ARE MARKED.-C/A-FABRICATED AND INSTALLED A REPAIR
- [SDR SIMA202008251003](https://openairdocs.org/sdr/SIMA202008251003), Aug 21, 2020: DOUBLER. GOUGED. 2 PREVIOUSLY INSTALLED DOUBLERS ON CARGO DOOR LOWER WEB SECTION GOUGED. -C/A-REMOVED, FABRICATED AND INSTALLED DOUBLERS FOR CARGO DOOR INNER LOWER WEB IAW EMB 1
- [SDR SIMA20200821002](https://openairdocs.org/sdr/SIMA20200821002), Aug 21, 2020: DOOR FRAME. CORRODED. CARGO DOOR LOWER FRAME CORRODED AT SCREW HOLE. REMOVED AND REPLACED THE CARGO DOOR LOWER FRAME IAW SRM 51-40-02.
- [SDR SIMA202008210002](https://openairdocs.org/sdr/SIMA202008210002), Aug 20, 2020: FLOOR SUPPORT. CORRODED. CENTER OMEGA BEAM AT FR 24-25 IS CORRODED. -C/A-BLENDED OUT CORROSION ON CENTER OMEGA BEAM AT FR 24-25 IAW SRM 51-10-03 AND CPM 51-14-02. REMAINING THICKNESS FO
- [SDR SIMA2020082519006](https://openairdocs.org/sdr/SIMA2020082519006), Aug 19, 2020: FRAME. CORRODED. FRAME 65 IS CORRODED ABOVE CARGO DOOR SILL.-C/A-REMOVED AND REPLACED FR 65 SECTION AT CARGO DOOR CUTOUT IAW EMB 145 SRM 51-40-02. REPLACEMENT PN: 145-64106-001 
- [SDR SIMA2020082419005](https://openairdocs.org/sdr/SIMA2020082419005), Aug 19, 2020: SHEAR TIE. CORRODED. FRAME 65 CARGO DOOR SHEAR TIE WAS CORRODED. REMOVED AND REPLACED FR 65 CARGO DOOR SHEAR TIE IAW SRM 51-40-02.
- [SDR SIMA20200817001](https://openairdocs.org/sdr/SIMA20200817001), Aug 17, 2020: FRAME. CRACKED. DURING HMBV INSPECTION, FR 73 CRACKED BETWEEN STR 15R-16R-C/A-RAR FR 73 LOWER SECTION TO REPAIR CRACK BETWEEN STR 15R-16R IAW EMB 145 SRM 51-40-02
- [SDR SIMA202008174004](https://openairdocs.org/sdr/SIMA202008174004), Aug 14, 2020: FITTING. DAMAGED. RH AILERON PCA FITTING HAS ELONGATED BUSHING HOLES-C/A-RAR RH AILERON PCA FITTING IAW EO-EM-27MR-112
- [SDR SIMA202008174003](https://openairdocs.org/sdr/SIMA202008174003), Aug 14, 2020: SERVICE PANEL. CORRODED. LAV BUCKET CORRODED AROUND SERVICING NIPPLE AND DRAIN HANDLE-C/A-RAR LAV BUCKET IAW EMB 145 SRM 51-40-02 AND 51-20-03
- [SDR SIMA20200813002](https://openairdocs.org/sdr/SIMA20200813002), Aug 13, 2020: FLOOR SUPPORT. CORRODED. DURING HMBV INSPECTION, QA FOUND THE LH OMEGA BEAM AT FR 24-25 CORRODED-C/A-ACCOMPLISHED PERMANENT REPAIR ON LH OMEGA BEAM AT FR 24-25 IAW ERS-EM-53MR-4163. REP
- [SDR SIMA20200726008](https://openairdocs.org/sdr/SIMA20200726008), Jul 26, 2020: BULB. INOPERATIVE. EMERGENCY LIGHT ON CEILING PANEL AT 7A INOP. C/A COMPLETE: REMOVED AND REPLACED BULB ON CEILING PANEL 7A, IAW EMB 145 AMM 33-50-08. CHECKS GOOD.
- [SDR SIMA20200726007](https://openairdocs.org/sdr/SIMA20200726007), Jul 26, 2020: FLOOR SUPPORT. CORRODED. RT FLOOR SILL HAS CORROSION AT FR 31, AS MARKED. C/A COMPLETE: FOUND CORROSION ON RT FLOOR SILL AT FR 31 TO BE OUT OF LIMITS, IAW EMB 145SRM 53-22-10. R & R CAB
- [SDR SIMA20200726006](https://openairdocs.org/sdr/SIMA20200726006), Jul 26, 2020: CRADLE. BROKEN. EMERGENCY FLASHLIGHT CRADLE ON LAV WALL IS BROKEN. C/A COMPLETE: R & R EMERGENCY FLASHLIGHT CRADLE ON LAV WALL, IAW EMB 145 AMM 33-50-16. OPS CHECK GOOD.
- [SDR SIMA20200726009](https://openairdocs.org/sdr/SIMA20200726009), Jul 26, 2020: POWER SUPPLY. NOT REPORTED. STD REQ A110 OPS A. REPLACE EPSU CRJ WC 33-002 OR EMB WC 33-700-19 PN: 11-0049 SN: 18369 POS: 2. C/A COMPLETE: PCW BY RECORDS REVIEW AND DVI OF EQUIPMENT INSTAL
- [SDR SIMA20200726005](https://openairdocs.org/sdr/SIMA20200726005), Jul 26, 2020: FLOOR SUPPORT. CORRODED. LT FLOOR SILL HAS CORROSION AT FR32, AS MARKED. C/A COMPLETE: BLENDED AND FOUND AREAS AT LT FLOOR SILL AT FR 32 TO BE OUT OF LIMITS, IAW EMB 145 SRM 51-10-03 AN
- [SDR SIMA20200726004](https://openairdocs.org/sdr/SIMA20200726004), Jul 26, 2020: CONNECTOR. BROKEN. EMERGENCY LIGHT STRIP NR 6 HAS BROKEN CONNECTOR. C/A COMPLETE: REMOVED AND REPLACED EMERGENCY LIGHT STRIP NR 6 BROKEN CONNECTOR, IAW EMB 145 SWPM 20-21-00.
- [SDR SIMA202007189003](https://openairdocs.org/sdr/SIMA202007189003), Jul 9, 2020: CHARGER. INOPERATIVE. DURING PS-1 INSP FOUND EMERGENCY LIGHTS AT SERVICE DOOR AND RH WING TO FUSELAGE FAIRING INOP.-C/A-RAR #2 EMERGENCY BATTERY AND CHARGER ASSY IAW E145 AMM 33-50-0
- [SDR SIMA2020040130001](https://openairdocs.org/sdr/SIMA2020040130001), Mar 30, 2020: BATTERY. DISCHARGED. SUPPLEMENTAL MAIN DOOR (ENTRANCE CEILING) EMERG LIGHT INOP. CONTINUITY TO GROUND WHEN CONNECTOR P8500 (BATTERY CRADLE) DISCONNECTED AND POSITIVE WIRE AT BULB (W
- [SDR SIMA2020040130003](https://openairdocs.org/sdr/SIMA2020040130003), Mar 30, 2020: BATTERY. BROKEN. #4 EMERGENCY LIGHT BATTERY HAS A BROKEN CAM LOCK.-C/A-REPLACED #4 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04. OPS GOOD

All 171: https://openairdocs.org/aircraft/N689EC/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/N689EC/stcs.md

## Related

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

---
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