# N667GB: 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: 145784
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 19, 2004
- Certificate issued: September 22, 2011
- Expires: September 30, 2027
- Mode S code: A8CED2
- 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=667GB
- Page: https://openairdocs.org/aircraft/N667GB

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/N667GB/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 N667GB.

## FAA accident and incident reports

None matched to N667GB.

## Service difficulty reports (124, 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 SIMA20220725001](https://openairdocs.org/sdr/SIMA20220725001), Jul 25, 2022: LAMP. BURNED OUT. SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD. END.
- [SDR SIMA20220425002](https://openairdocs.org/sdr/SIMA20220425002), Apr 25, 2022: NONE. INOPERATIVE. FA EMER. FLASH LIGHT BATTERY REQ REPLACEMENT PER PS-2 CHECK PG 15. ITEM 12-C/A-DEFERRED PER MEL 25-32 AUTH# 040330M-C EXP 05/05/22 CA PENDING
- [SDR SIMA20220415004](https://openairdocs.org/sdr/SIMA20220415004), Apr 15, 2022: NONE. CRACKED. AFT FA FLASHLIGHT CRADLE CRACKED-C/A-RAR AFT FA FLASHLIGHT ASSY IAW ETN-EM-33-059. OPS CHECK GOOD. MEL RESTORED.
- [SDR SIMA20220225002](https://openairdocs.org/sdr/SIMA20220225002), Feb 25, 2022: NOT REPORTED. NOT REPORTED. SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECKED GOOD. END.
- [SDR SIMA20211111002](https://openairdocs.org/sdr/SIMA20211111002), Nov 11, 2021: NONE. NONE. ON DEPARTURE, UPON RETRACTING THE LANDING GEAR CREW RECEIVED LG/LEVER DISAGREE MESSAGE. COMPLIED WITH QRH RECEIVED WARNING AGAIN.UNABLE TO GET GEAR TO RETRACT A
- [SDR SIMA20210405004](https://openairdocs.org/sdr/SIMA20210405004), Apr 5, 2021: SENSOR. MALFUNCTIONED. "BRAKE OVERHEAT" ON EICAS IN FLIGHT ON LEFT HAND, INBOARD-C/A-RAR LH INBOARD TEMPERATURE SENSOR IAW EMB 145 AMM 32-47-01. OPERATIONAL CHECK GOOD.
- [SDR SIMA20210221001](https://openairdocs.org/sdr/SIMA20210221001), Feb 21, 2021: LENS. DESTROYED. MAIN DOOR EXTERNAL EMERGENCY LIGHT LENS SHATTERED. C/A-MAIN DOOR EXTERNAL EMERGENCY LIGHT LENS R & R IAW EMB145 AMM 33-50-10.
- [SDR SIMA20200928004](https://openairdocs.org/sdr/SIMA20200928004), Sep 28, 2020: ENGINE. VIBRATION. NR 2 ENGINE RUMBLE WHEN MOVEMENT BETWEEN MIDRANGE AND IDLE ON THE THROTTLE QUADRANT VIBRATIONS FELT IN RUDDER PEDALS ON THE GROUND AND IN THE AIR ON DESCENT AND
- [SDR SIMA202009154001](https://openairdocs.org/sdr/SIMA202009154001), Sep 14, 2020: HANDLE. LACK OF LUBE. MAIN CABIN DOOR NOT CLOSING ALL THE WAY. C/A LUBRICATED OUTSIDE HANDLE, OPENED AND CLOSED. OPERATIONAL CHECK GOOD, IAW EMB145 AMM 52-10-01.
- [SDR SIMA202007276001](https://openairdocs.org/sdr/SIMA202007276001), Jul 26, 2020: WARNING MESSAGE. FALSE ACTIVATION. FLT EXPERIENCED TWO HIGHSPEED WARNINGS DESCENDING 11000.1ST <10 SECOND 250-280. 2ND, 8 SECONDS 250-270.FLAPS AND GEAR WERE UP. PERFORMED PHASE 1 INSPECTION FOR 
- [SDR SIMA202007131003](https://openairdocs.org/sdr/SIMA202007131003), Jul 11, 2020: HANDLE. LACK OF LUBE. MAIN CABIN DOOR DIFFICULT TO CLOSE ALL INDICATIONS NORMAL. LUBRICATED EXTERNAL HANDLE. CLEANED AND SERVICED MAIN DOOR ROLLERS. OPS CHECK GOOD IAW AMM 52-18-00 &
- [SDR SIMA202005121004](https://openairdocs.org/sdr/SIMA202005121004), May 11, 2020: WIRE. BROKEN. FOUND BROKE WIRE NEAR EMERGENCY FLOOR LIGHT ASSEMBLY P/N 6636-7-C/A-REMOVED AND REPLACED EMERGENCY FLOOR LIGHT ASSEMBLY P/N 6636-7 IAW EMB-145 AMM 33-50-08 OPER
- [SDR SIMA202005121003](https://openairdocs.org/sdr/SIMA202005121003), May 11, 2020: CONNECTOR. BROKEN. MOST AFT FLOOR PROXIMITY EMERGENCY LIGHTING STRIP HAS ONE BROKEN ELECTRICAL CONNECTOR-C/A-REPAIRED CONNECTOR FOR EMERGENCY LIGHTING STRIP IAW SWPM 20-21-00. OPC
- [SDR SIMA2020041615001](https://openairdocs.org/sdr/SIMA2020041615001), Apr 15, 2020: BATTERY PACK. DISCHARGED. SERVICE DOOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED #2 EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK IAW AMM 33-50-04. PERFORMED WIRING REPAIR ON WIRE W19
- [SDR SIMA202004032002](https://openairdocs.org/sdr/SIMA202004032002), Apr 2, 2020: CRADLE. DAMAGED. FWD CABIN EMER FLASHLIGHT CRADLE DAMAGED-C/A-RAI NEW FWD CABIN FLASHLIGHT CRADLE IAW EMB 145 AMM33-50-16. LED IS ON GREEN WITH BUTTON PRESSED.
- [SDR SIMA202003110003](https://openairdocs.org/sdr/SIMA202003110003), Mar 10, 2020: LIGHT. INOPERATIVE. FWD LH EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR LH FWD EXTERNAL EMERGENCY LIGHT LAMP IAW EMB-145 AMM 33-50-10. OPC GOOD
- [SDR SIMA202003110002](https://openairdocs.org/sdr/SIMA202003110002), Mar 10, 2020: CONNECTOR. DISCONNECTED. CABIN AISLE FWD CEILING EMERGENCY LIGHT IS INOP-C/A- FOUND #1 EMERG BATTERY SUPPLY CONNECTOR DISCONNECTED. RECONNECTED IAW EMB-145 AMM 33-50-04. OPC GOOD.
- [SDR SIMA2020033102003](https://openairdocs.org/sdr/SIMA2020033102003), Feb 2, 2020: SKIN. CANNING. LEFT HAND VERTICAL STABILIZER SKIN JUST FORWARD OF TAIL ACCESS PANEL 324EL HAS OIL CANNING.-C/A-C/W REPAIR OF VERTICAL STABILIZER SKIN LOCATED JUST FWD OF TAIL 
- [SDR SIMA2020013017013](https://openairdocs.org/sdr/SIMA2020013017013), Jan 17, 2020: FITTING. CHAFED. RIGHT HAND AILERON DAMPER FITTING CHAFFED.-C/A-REMOVED AND REPLACED DAMPER FITTING ASSY IAW EO-EM-27MR-112.
- [SDR SIMA2020012917011](https://openairdocs.org/sdr/SIMA2020012917011), Jan 17, 2020: FITTING. CHAFED. LEFT HAND AILERON DAMPER FITTING CHAFFED. LEFT HAND AILERON PCA FITTING OUTBD HAT BUSHING IS MIGRATED OUT. -C/A-INSTALLED NEW AILERON DAMPER FITTING ASSY IAW EO
- [SDR SIMA202001176002](https://openairdocs.org/sdr/SIMA202001176002), Jan 16, 2020: SHEAR TIE. CORRODED. FRAME 65 SHEAR CLIP CORRODED AT CARGO SILL LEVEL.-C/A-COMPLETED REPAIR OF FRAME 65 SHEAR CLIP IAW SRM 53-31-04.
- [SDR SIMA2020012414004](https://openairdocs.org/sdr/SIMA2020012414004), Jan 14, 2020: DOOR SILL. CORRODED. SERVICE DOOR SILL HAS CORROSION. (CENTER)-C/A-REMOVED AND REPLACED SERVICE DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA2020012113002](https://openairdocs.org/sdr/SIMA2020012113002), Jan 13, 2020: FRAME. CRACKED. RIGHT SIDE OF FRAME 10 HAS A 1/2" CRACK JUST BELOW F/O'S DV WINDOW SILL.-C/A-REPLACED RH FRAME 10 IAW SRM 51-40-02.
- [SDR SIMA202001308010](https://openairdocs.org/sdr/SIMA202001308010), Jan 8, 2020: ANGLE. CRACKED. L/H VERT TO FUSELAGE ANGLE IS CRACKED AT FR 76.(CRACK APROX 1 INCH LONG) -C/A-INSTALLED NEW ANGLE IAW SRM 51-40-02.
- [SDR SIMA202001280009](https://openairdocs.org/sdr/SIMA202001280009), Jan 8, 2020: STRINGER CLIP. CRACKED. STRINGER CLIP AT FRAME 80 AND STR 7L HAS A 3/8" CRACK. -C/A-REMOVED AND REPLACED STRINGER CLIP AT FRAME 80 AND STR. 7L IAW SRM 51-40-02. RESTORED SURFACE PROTEC
- [SDR SIMA2020012708008](https://openairdocs.org/sdr/SIMA2020012708008), Jan 8, 2020: SHEAR TIE. CRACKED. STRINGER CLIP AT FRAME 80 AND STR 9R HAS A 3/8 CRACK. (EVALUATED AND FOUND SHEAR CLIP AT FRAME 80 STRINGER 9R NOT TO BE CRACKED. CRACKED SHEAR CLIP IS LOCATED A
- [SDR SIMA202001280007](https://openairdocs.org/sdr/SIMA202001280007), Jan 8, 2020: SKIN. CRACKED. L/H REAR FUSELAGE II SKIN IS CRACKED AROUND A RIVET AT FR 78. (CRACK APROX 1/4 INCH LONG) -C/A-REPAIRED IAW SRM 53-32-01.
- [SDR SIMA202001280006](https://openairdocs.org/sdr/SIMA202001280006), Jan 8, 2020: SKIN. CRACKED. L/H REAR FUSELAGE II SKIN IS CRACKED AROUND A RIVET AT FR 79. (CRACK APROX 1/4 INCH LONG) -C/A-REPAIRED IAW SRM 53-32-01.
- [SDR SIMA2020012208005](https://openairdocs.org/sdr/SIMA2020012208005), Jan 8, 2020: BRACKET. CRACKED. CARGO DOOR TORSION BAR BRACKET ON FRAME 61 HAS A 1/16" CRACK. -C/A-RAR'D CARGO DOOR TORSION BAR BRACKET ON FRAME 61 IAW SRM-51-40-02. REF NRTC E764850 FOR LIFTI
- [SDR SIMA202001208004](https://openairdocs.org/sdr/SIMA202001208004), Jan 8, 2020: STIFFENER. CRACKED. STIFFENER ON THE AFT SIDE OF FRAME 68 FOR CARGO DOOR HOLD OPEN STRUT RECEPTACLE HAS TWO 1/2" CRACKS.C/A-RAR STIFFENERR IAW SRM 51-40-02.
- [SDR SIMA2020011708003](https://openairdocs.org/sdr/SIMA2020011708003), Jan 8, 2020: DOOR SILL. CORRODED. CARGO DOOR SILL IS CORRODED.-C/A-COMPLETED INSTALLATION OF NEW CARGO DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA2020012106007](https://openairdocs.org/sdr/SIMA2020012106007), Jan 6, 2020: ATTACH ANGLE. CRACKED. RIGHT UPPER WING TO FUSELAGE FAIRING LOWER AFT ATTACH ANGLE HAS 1/4" CRACK ON THE AFT END. -C/A-REPAIRED RIGHT UPPER WING TO FUSELAGE FAIRING AFT LOWER ATTACH A
- [SDR SIMA2020012106006](https://openairdocs.org/sdr/SIMA2020012106006), Jan 6, 2020: ATTACH ANGLE. CRACKED. RIGHT UPPER WING TO FUSELAGE FAIRING LOWER 2ND FROM THE AFT ATTACH ANGLE HAS 1/4" CRACK ON FWD END. -C/A-REPAIRED RIGHT UPPER WING TO FUSELAGE FAIRING LOWER 2ND
- [SDR SIMA2019112219005](https://openairdocs.org/sdr/SIMA2019112219005), Nov 19, 2019: CARBON SEAL. FAILED. STRONG BURNING SMELL EACH TIME ANTI-ICEING CAME ON-C/A-REMOVED AND REPLACED RH ENGINE #0 CARBON SEAL IAW RRMM TASK 72-25-25-000-801 & 72-25-25-400-801 AND OPC I
- [SDR SIMA20190908004](https://openairdocs.org/sdr/SIMA20190908004), Sep 8, 2019: ANTI-ICE VALVE. FAILED. SUPPLEMENTAL ENG(2) ANTI ICE FAIL. C/A-ENG 2 A/ICE VLV FAIL MSG ON CMC, FOLLOWED FIM TASK 30-21-00-810-804-A. FAIL RT ENGINE A/ICE VALVE. DEFERRED PER MEL 30-11
- [SDR SIMA2019082019001](https://openairdocs.org/sdr/SIMA2019082019001), Aug 19, 2019: O-RING. BLOWN. DURING CLIMB WHILE PERFORMING THE ICE PROTECTION TEST PNEUMATIC RECEIVED AN EICAS BLEED NR 2 WARNING MESSAGE. COMPLIED WITH CHECKLIST PROCEDURES AND DECLARED AN
- [SDR SIMA201908198001](https://openairdocs.org/sdr/SIMA201908198001), Aug 18, 2019: FLASHLIGHT. FAILED. SMELL OF ELECT SMOKE IN COCKPIT.NO VISIBLE SMOKE.WINDSHIELD HEAT WENT OUT IN DECENT.NO EICAS MSG , NO POPPED CB'S , NO SWITCH ANOMOLY. UPON ARRIVAL TO COCKPIT D
- [SDR SIMA20181218002](https://openairdocs.org/sdr/SIMA20181218002), Dec 18, 2018: LIGHT. INOPERATIVE. AFT CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED AFT CEILING EMERGENCY LIGHT BULB IAW AMM 33-50-10, OPS CHECK GOOD.
- [SDR SIMA20180921003](https://openairdocs.org/sdr/SIMA20180921003), Sep 21, 2018: ROLLER. LACK OF LUBE. MAIN CABIN DOOR DIFFICULT TO CLOSE-C/A-OPENED AND CLOSED DOOR SEVERAL TIMES. DID NOT FEEL ANY DIFFICULTY CLOSING DOOR. DID REMOVE SOME INSULATION THAT WAS EXPOS
- [SDR SIMA20180723003](https://openairdocs.org/sdr/SIMA20180723003), Jul 23, 2018: DOOR SEAL. DIRTY. MAIN DOOR DIFFICULT TO CLOSE-C/A-CLEANED AND LUBRICATED DOOR SEALS. PERFORMED OPS CHECK OF DOOR IAW AMM 52-11-00. OPS CHECK GOOD.
- [SDR SIMA20180618002](https://openairdocs.org/sdr/SIMA20180618002), Jun 18, 2018: LIGHT. INOPERATIVE. DURING PS-2 CHECK, OVERWING EMERGENCY EXIT FLOOR LIGHTING STRIP FOUND TO BE INOP. REMOVED AND REPLACED OVERWING EMERGENCY EXIT FLOOR LIGHTING STRIP IAW AMM TASK
- [SDR SIMA2018040200004](https://openairdocs.org/sdr/SIMA2018040200004), Mar 29, 2018: UNKNOWN. ODOR. FA DETECTED A STRONG ODOR IN THE CABIN GOT WORSE WITH HEAT. COMPLIED WITH ETN-EM-72-034. COMPLETED RUNS AND INSPECTION, NO DETECTABLE ODOR NOTED
- [SDR SIMA20170731001](https://openairdocs.org/sdr/SIMA20170731001), Jul 31, 2017: YOKE. CRACKED. RIGHT ENGINE FWD LOWER YOKE CRACKED. REMOVED AND INSTALLED A NEW YOKE IAW EO EM-54MR-386.
- [SDR SIMA20170731003](https://openairdocs.org/sdr/SIMA20170731003), Jul 31, 2017: SKIN. CRACKED. LEFT AFT FUSELAGE FRAME 75 SKIN CRACKED AT FASTENER BELOW STRINGER 2. REPAIRED IAW SRM 53-31-01, ITEM 11, FIGURE 219, SHEET 1, 51-20-03, AND 51-40-02.
- [SDR SIMA20170731004](https://openairdocs.org/sdr/SIMA20170731004), Jul 31, 2017: SKIN. CRACKED. RIGHT AFT FUSELAGE FRAME 75, SKIN CRACKED AT FASTENER BELOW STRINGER 2. REPAIRED IAW SRM 53-31-01, ITEM 11, FIGURE 219, SHEET 1, 51-20-03, AND 51-40-02.
- [SDR SIMA20170731002](https://openairdocs.org/sdr/SIMA20170731002), Jul 31, 2017: YOKE. CRACKED. LT ENGINE FWD LOWER YOKE CRACKED. REMOVED AND INSTALLED THE ENGINE YOKE IAW EO EM-54MR-386.
- [SDR SIMA20170730004](https://openairdocs.org/sdr/SIMA20170730004), Jul 30, 2017: SKIN. GOUGED. GOUGE FOUND ON CARGO DOOR APPROXIMATELY 10 INCHES AFT OF FORWARD END AND 24 INCHES UP FROM BOTTOM END. INSTALLED A REPAIR DOUBLER AND FILLER IAW SRM 52-30-01,IT
- [SDR SIMA20170730005](https://openairdocs.org/sdr/SIMA20170730005), Jul 30, 2017: SKIN. GOUGED. GOUGE FOUND ON CARGO DOOR APPROXIMATELY 24UP FROM THE BOTTOM AND 10 INCHES FORWARD OF AFT END. INSTALLED A DOUBLER, AND FILLER IAW SRM 52-30-01, ITEM 2, AND 51-
- [SDR ASOA20150916070](https://openairdocs.org/sdr/ASOA20150916070), Sep 16, 2015: BATTERY PACK. DISCHARGED. THE CREW REPORTED THAT THE FLOOR EMERGENCY LIGHTS WOULD NOT STAY ON. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK, OPERATIONALLY
- [SDR ASOA20150605131](https://openairdocs.org/sdr/ASOA20150605131), Jun 5, 2015: FCU. INOPERATIVE. ACFT DIVERTED FUEL 1 LO LEVEL INDICATION AND PACK 2 OVERHEAT INDICATION IN-FLIGHT. MAINTENANCE R & R FUEL CONDITIONING UNIT IAW AMM 28-41-01 AND IPC REF 28-41-0

All 124: https://openairdocs.org/aircraft/N667GB/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/N667GB/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.