# N610AE: 1998 Embraer EMB-145

- Status: Valid registration
- Airframe: [Embraer EMB-145](https://openairdocs.org/model/embraer-emb-145) (registry code 3260210, 55 seats)
- Engine: [Allison AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030)
- 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: 145073
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: August 19, 1998
- Certificate issued: October 14, 2011
- Expires: October 31, 2027
- Mode S code: A7EEC3
- 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=610AE
- Page: https://openairdocs.org/aircraft/N610AE

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.

## ADs that may apply (OpenAirDocs): 108 in force

### Matched by airframe (Embraer EMB-145)

- [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 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 2007-04-09](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 2006-25-07](https://openairdocs.org/ad/2006-25-07): Fuel quantity indication system (FQIS) wire harness and the direct current (DC) fuel pump wire harness · Embraer EMB-135ER, EMB-135KE, EMB-145 and 4 more. Effective Jan 16, 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
- [AD 2004-25-21](https://openairdocs.org/ad/2004-25-21): Pitch trim system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 26, 2005

### Matched by engine (Allison AE-3007A)

- [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 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 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 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 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 2005-25-04](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 2005-08-02](https://openairdocs.org/ad/2005-08-02) (historical): Electric fuel pumps · Embraer - Empresa Brasileira de Aeronautica EMB-135 Series (all) and EMB-145 Series (all). Effective May 19, 2005
- [AD 2004-09-15](https://openairdocs.org/ad/2004-09-15) (historical): Nose Landing Gear Wheel Nuts and Associated Inner and Outer Seals and Reidentify Landing Gear Strut · Embraer - Empresa Brasileira de Aeronautica EMB-135 Series (all) and EMB-145 Series (all). Effective Jun 9, 2004
- [AD 2003-09-03](https://openairdocs.org/ad/2003-09-03) (historical): Cartridge flange · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 3 more. Effective May 14, 2003
- [AD 2002-16-06](https://openairdocs.org/ad/2002-16-06) (historical): Auxiliary power unit (APU) · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 2 more. Effective Aug 27, 2002
- [AD 2002-08-21](https://openairdocs.org/ad/2002-08-21) (historical): Bonding Jumpers that Connect the Horizontal Stabilizer to the Vertical Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 2 more. Effective May 16, 2002
- [AD 2002-08-18](https://openairdocs.org/ad/2002-08-18) (historical): Actuator Clutches of the Primary and Backup Pitch Trim Systems of the Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 2 more. Effective May 16, 2002
- [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 2001-17-03](https://openairdocs.org/ad/2001-17-03) (historical): Engine Thrust Reverser Stow/Transit Switches · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Sep 5, 2001
- [AD 2001-10-15](https://openairdocs.org/ad/2001-10-15) (historical): Fire Extinguisher Bottles · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Jun 8, 2001
- [AD 2001-10-01](https://openairdocs.org/ad/2001-10-01) (historical): Airplane Flight Manuals--APU Start/Stop Switch Panel · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective May 29, 2001
- [AD 2000-19-03](https://openairdocs.org/ad/2000-19-03) (historical): Fuel System Tubing · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 1 more. Effective Oct 3, 2000
- [AD 2000-19-02](https://openairdocs.org/ad/2000-19-02) (historical): Electric Fuel Pumps · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Oct 3, 2000
- [AD 2000-13-02](https://openairdocs.org/ad/2000-13-02) (historical): Precooler Differential Pressure Switches · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Jul 3, 2000
- [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 99-11-01](https://openairdocs.org/ad/99-11-01) (historical): Bleed Air Check Valve · Embraer - Empresa Brasileira de Aeronautica EMB-145 Series (all). Effective Jun 2, 1999
- [AD 99-05-04](https://openairdocs.org/ad/99-05-04) (historical): Aileron Power Control Actuator (PCA) Rod Ends · Embraer - Empresa Brasileira de Aeronautica EMB-145 Series (all). Effective Mar 29, 1999
- [AD 99-01-12](https://openairdocs.org/ad/99-01-12) (historical): Pitch Trim System · Embraer - Empresa Brasileira de Aeronautica EMB-145 Series (all). Effective Feb 2, 1999
- [AD 98-13-34](https://openairdocs.org/ad/98-13-34) (historical): Test NLG For Extension (Free-Fall) Function · Embraer - Empresa Brasileira de Aeronautica EMB-145 Series (all). Effective Jul 9, 1998
- [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 139: https://openairdocs.org/aircraft/N610AE/ads.md

## Information bulletins (advisory) (9 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 NM-04-55](https://openairdocs.org/saib/NM-04-55): . Issued Mar 8, 2004
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N610AE.

## FAA accident and incident reports

None matched to N610AE.

## Service difficulty reports (179, 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 SIMA20220815001](https://openairdocs.org/sdr/SIMA20220815001), Aug 15, 2022: LAMP. INOPERATIVE. 12C OVERWING EMERGENCY LIGHT INOP-C/A-RAR SEAT 12C OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPC GOOD.
- [SDR SIMA20220707001](https://openairdocs.org/sdr/SIMA20220707001), Jul 7, 2022: LAMP. INOPERATIVE. RH AFT OVER WING EMERGENCY EXIT LIGHT INOP-C/A-RAR AFT OVERWING EMERGENCY EXIT LIGHT LAMP IAW EMB 145 AMM 33-50-10. OPC GOOD.
- [SDR SIMA20220524006](https://openairdocs.org/sdr/SIMA20220524006), May 24, 2022: NONE. UNSERVICEABLE. ALL AFT EMERGENCY LIGHTS AND OVERWING LIGHTS INOP.-C/A-T/S ALL AFT EMERGENCY LIGHTS AND OVERWING LIGHTS INOP IAW EMB WM 33-50-50-002. FOUND #4 BATTERY AND CHARG
- [SDR SIMA20220514002](https://openairdocs.org/sdr/SIMA20220514002), May 14, 2022: NONE. NONE. MECHANICAL / DUAL SPS FAIL. EMERGENCY DECLARED. AT 16000 MSL SPS 2 INOP WARNING MSG.IN QRH WHEN SPS 2 CUT OUT WAS PRESSED,SPS 1 INOP WARNING MSG ON EICAS ASSICI
- [SDR SIMA20220509001](https://openairdocs.org/sdr/SIMA20220509001), May 9, 2022: LAMP. INOPERATIVE. MAIN DOOR INTERIOR EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR INTERIOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPC GOOD. END.
- [SDR SIMA20220502002](https://openairdocs.org/sdr/SIMA20220502002), May 2, 2022: LAMP. INOPERATIVE. MAIN DOOR ENTRY CEILING EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR ENTRY CEILING EMERGENCY LIGHT IAW EMB 145 AMM 35-50-06. OPC GOOD.
- [SDR SIMA20220304003](https://openairdocs.org/sdr/SIMA20220304003), Mar 4, 2022: NONE. NONE. MAIN DOOR CEILING EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR CEILING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPC GOOD. END.
- [SDR SIMA20220221003](https://openairdocs.org/sdr/SIMA20220221003), Feb 21, 2022: NONE. NONE. BLEED1 VALVEFAIL INTERMITTENTL Y ON EICAS../ EQP SWAP FLT CONT-C/A-RAR ENGINE BLEED VALVE ON #1 ENGINE AS PER AMM 36-11-05,OPS CHECK GOOD.
- [SDR SIMA202201187003](https://openairdocs.org/sdr/SIMA202201187003), Jan 17, 2022: LIGHT. INTERMITTENT. RH AFT OVERWING EXTERNAL EMERGENCY LIGHT INTERMITTENT-C/A-RAR RH AFT OVERWING EXTERNAL EMERGENCY LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10. OPC GOOD.
- [SDR SIMA20220111002](https://openairdocs.org/sdr/SIMA20220111002), Jan 11, 2022: NONE. NONE. RH EMERGENCY LIGHT OUT OVER WING-C/A-RAR RIGHT HAND OVERWING EMERGENCY LIGHT IAW AMM 33-50-10 OPS CHECK
- [SDR SIMA20211228002](https://openairdocs.org/sdr/SIMA20211228002), Dec 28, 2021: NONE. NONE. FA FWD FLASHLIGHT INOP.-C/A-RAR FWD FA FLASHLIGHT IAW AMM 33-50-16. OPS CHECK GOOD.
- [SDR SIMA20211012002](https://openairdocs.org/sdr/SIMA20211012002), Oct 12, 2021: NONE. NONE. LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. NO DEFECTS NOTE
- [SDR SIMA20210916002](https://openairdocs.org/sdr/SIMA20210916002), Sep 16, 2021: BATTERY PACK. INOPERATIVE. WHILE PERFORMING PS-1 INSPECTION FOUND EMERGENCY FLOOR PROXIMITY LIGHT STRIPS 4,5 INOP.-C/A-REMOVED AND REPLACED #3 BATTERY AND CHARGER IAW EMB 145 AMM 33-50-01
- [SDR SIMA20210826003](https://openairdocs.org/sdr/SIMA20210826003), Aug 26, 2021: LAMP. INOPERATIVE. EMERGENCY LIGHT ABOVE RIGHT WING INOP-C/A-SEE AML LOG PAGE4734718/3 DEFERRED EMERGENCY LIGHT PER MEL 33-22 RAR'D LAMP ASSY IAW 33-50-10. NO FIX. T/S TO LIGHT AS
- [SDR SIMA202108243001](https://openairdocs.org/sdr/SIMA202108243001), Aug 23, 2021: INVERTER. INOPERATIVE. #4 AND #5 SECTIONS OF FLOOR EMER LIGHTS INOP AND L/H AND R/H OVER WING INTERNAL LIGHTS INOP-C/A-REF TURNOVER, INSTALLED ORIGINAL #5 EMERG LIGHT INVERTER IAW AMM
- [SDR SIMA202108098001](https://openairdocs.org/sdr/SIMA202108098001), Aug 8, 2021: LAMP. INOPERATIVE. RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD. END.
- [SDR SIMA20210705003](https://openairdocs.org/sdr/SIMA20210705003), Jul 5, 2021: BULB. INOPERATIVE. RH AFT OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RH AFT OVERWING EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10-020-003-A. OP CHECKED GOOD
- [SDR SIMA20210627001](https://openairdocs.org/sdr/SIMA20210627001), Jun 27, 2021: LAMP. INOPERATIVE. RH AFT OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH AFT OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD. END.
- [SDR SIMA20210517004](https://openairdocs.org/sdr/SIMA20210517004), May 17, 2021: CONTROL MODULE. FAULTED. EMERGENCY LIGHT NOT ARMED CAUTION ON EICAS W/ EMERG LT SWITCH ARMED TRIED CYCLING MULTIPLE TIMES"TRANSFERRED TO NRWC 610-ORD-03512" GR 417418-C/A-RAR CONTROL MO
- [SDR SIMA20210409001](https://openairdocs.org/sdr/SIMA20210409001), Apr 9, 2021: LAMP. INOPERATIVE. RH OVERWING EMERGENCY LIGHT FOUND TO BE INOP PER PS-1 INSP.-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP IN REF. AMM 33-50-10. OPC GOOD IN REF TO AMM 33-50-00
- [SDR SIMA20201206004](https://openairdocs.org/sdr/SIMA20201206004), Dec 6, 2020: DUCT. LOOSE. BLEED 2 LEAK IN FLIGHT EMERGNCY DECLARED. EQUIPMENT SWAP FLT CONT. C/A: TROUBLESHOT BLEED 2 LEAK, REF FI 36-20-00-810-802A AND FOUND DUCTS TO HEAT EXCHANGER TO 
- [SDR SIMA20201130003](https://openairdocs.org/sdr/SIMA20201130003), Nov 30, 2020: LIGHT. INOPERATIVE. NR 5 FLOOR PROXIMITY EMERGENCY LIGHT STRIP IS INOPERABLE. C/A: R & R NR 5 FLOOR PROXIMITY EMERGENCY LIGHT STRIP, IAW EMB145 AMM 33-50-12. OPERATIONAL CHECK OF E
- [SDR SIMA20201103001](https://openairdocs.org/sdr/SIMA20201103001), Nov 3, 2020: BULB. INOPERATIVE. RT SIDE AFT OVERWING EMERGENCY LIGHT INOPERABLE. C/A: R & R RT SIDE AFT OVERWING EMERGENCY LIGHTBULB, IAW EMB 145 AMM 33-50-10. OPERATIONS CHECK GOOD.
- [SDR SIMA20200921001](https://openairdocs.org/sdr/SIMA20200921001), Sep 21, 2020: LAMP. INOPERATIVE. RT AFT OVERWING EMERGENCY LIGHT INOP. C/A: R & R RT AFT OVERWING EMERGENCY LAMP, IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD, IAW EMB 145 AMM 33-50-00.
- [SDR SIMA2020083129002](https://openairdocs.org/sdr/SIMA2020083129002), Aug 29, 2020: LIGHT. INOPERATIVE. RH OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RH OVERWING EMERGENCY LIGHT OPC GOOD IAW AMM 33-50-07
- [SDR SIMA202008165001](https://openairdocs.org/sdr/SIMA202008165001), Aug 15, 2020: LIGHT. INOPERATIVE. FOUND RH OVERWING EMERGENCY LIGHT TO BE INOP-C/A-REPLACED RH OVERWING EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECK GOOD
- [SDR SIMA202007187002](https://openairdocs.org/sdr/SIMA202007187002), Jul 17, 2020: CONNECTOR. DAMAGED. EMERGENCY EXIT SIGN ON AFT GALLEY WALL AT SEAT 3B INOPERATIVE. TIGHTENED UP CONNECTOR PLUG BACKSHELL IN REFERENCE WITH EMB AMM 33-50-11-000-801-A AND 33-50-11-4
- [SDR SIMA202005075002](https://openairdocs.org/sdr/SIMA202005075002), May 5, 2020: WIRE SPLICE. DEFECTIVE. L/H AFT OVERWING EMERGENCY LIGHT IS INOP.-C/A-FOUND SPLICE AT WIRE W101-8590-22 TO BE DEFECTIVE. REMOVED AND REPLACED SPLICE SP8928 IAW EMB 145 SWPM 20-21-00 . 
- [SDR SIMA2020032310007](https://openairdocs.org/sdr/SIMA2020032310007), Mar 10, 2020: PLATE. DAMAGED. RUDDER #1 HAS AREA OF CHAFEING DAMAGE-C/A-COMPLIED WITH IAW ERS-EM-55MR-830 01
- [SDR SIMA20200306002](https://openairdocs.org/sdr/SIMA20200306002), Mar 6, 2020: HINGE FITTING. UNSERVICEABLE. TRANSFERRED FROM TASK #1 OF NRTC E778170. UPPER HINGE FITTING, SRM 55-41-02 FIG 10 ITEM 140. UNSERVICEABLE AND REQUIRES REPLACEMENT. -C/A-INSTALLED NEW HINGE FI
- [SDR SIMA20200306001](https://openairdocs.org/sdr/SIMA20200306001), Mar 6, 2020: FITTING. OUT OF TOLERANCE. RUDDER 2 LOWER ROD FITTING UPPER FLANGE FAILED DIMENSIONAL CHECK, FITTING REQUIRES REPLACEMENT.-C/A-REMOVED AND REPLACED LOWER ROD FITTING ASSY IAW SRM 55-40-02
- [SDR SIMA202003094008](https://openairdocs.org/sdr/SIMA202003094008), Mar 4, 2020: ATTACH ANGLE. CRACKED. LH WING-TO-FUSELAGE UPPER ATTACHMENT ANGLE. HAS EVIDENCE OF A CRACK APPROX. 1/2" LONG. JUST BELOW A RIVET AT FRAME 50.-C/A-RAR LH WING-TO-FUSELAGE UPPER ATTACHM
- [SDR SIMA2020030426010](https://openairdocs.org/sdr/SIMA2020030426010), Feb 26, 2020: SUPPORT. CRACKED. SUPPORT CRACKED AT FR 61 BETWEEN STR 4 RT AND 5 RT-C/A-REMOVED AND REPLACED SUPPORT AT FRAME 61 BETWEEN STRINGER 4RT AND 5 RT IAW SRM 51-40-02.
- [SDR SIMA2020030426009](https://openairdocs.org/sdr/SIMA2020030426009), Feb 26, 2020: ATTACH ANGLE. CRACKED. LH WING-TO-FUSELAGE #4 LOWER ATTACHMENT ANGLE. HAS A 2" CRACK ON THE FWD END UP TO THE THIRD RIVET.-C/A-REMOVED AND REPLACED SECTION OF THE LH WING TO FUSELAGE 
- [SDR SIMA2020030426008](https://openairdocs.org/sdr/SIMA2020030426008), Feb 26, 2020: WEB. CRACKED. L/H GEAR WELL AFT WEB IS CRACKED IN 3 PLACES. -C/A-REMOVED AND REPLACED AND COMPLETED INSTALLATION OF LH GEAR WELL AFT WEB IAW SRM 51-40-02.
- [SDR SIMA202003026006](https://openairdocs.org/sdr/SIMA202003026006), Feb 26, 2020: ATTACH ANGLE. CRACKED. LH WING-TO-FUSELAGE #2 LOWER ATTACHMENT ANGLE. HAS A 3/8" CRACK ON THE FWD END UP TO THE FIRST RIVET.-C/A-REMOVED AND REPLACED LH WING TO FUSELAGE #2 LOWER ATTA
- [SDR SIMA202003026004](https://openairdocs.org/sdr/SIMA202003026004), Feb 26, 2020: ATTACH ANGLE. CRACKED. RH WING-TO-FUSELAGE LOWER ATTACHMENT ANGLE #1. HAS A 1/2" CRACK ON THE FWD END OF THE PREVIOUS REPAIR SPLICE. -C/A-REPLACED BOTH AREAS (REF TASK#1) WITH ONE REP
- [SDR SIMA202003026005](https://openairdocs.org/sdr/SIMA202003026005), Feb 26, 2020: ATTACH ANGLE. CRACKED. LH WING-TO-FUSELAGE UPPER ATTACHMENT ANGLE. HAS EVIDENCE OF A CRACK APPROX. 1/2" LONG. JUST BELOW A RIVET AT FRAME 50. -C/A-REMOVED AND REPLACED LH WING TO FUSE
- [SDR SIMA2020030425009](https://openairdocs.org/sdr/SIMA2020030425009), Feb 25, 2020: FLOOR SUPPORT. CORRODED. CENTER OMEGA BEAM HAS SIDE CORROSION PITTING NEAR THE CROSSBEAM AT FR. 38. -C/A-COMPLETED REPAIR ON THE CENTER OMEGA BEAM AT FRAME 38 IAW SRM 53-00-10 AND 51-40
- [SDR SIMA202003025008](https://openairdocs.org/sdr/SIMA202003025008), Feb 25, 2020: FLOOR SUPPORT. CORRODED. LH OMEGA BEAM HAS SIDE CORROSION PITTING NEAR THE CROSSBEAM AT FR. 38. -C/A-REPAIRED LH OMEGA BEAM NEAR THE CROSSBEAM AT FR 38 IAW SRM 53-00-10.
- [SDR SIMA2020031224002](https://openairdocs.org/sdr/SIMA2020031224002), Feb 24, 2020: FLOOR SUPPORT. CORRODED. CENTER OMEGA BEAM HAS SIDE CORROSION PITTING NEAR THE CROSSBEAM AT FR. 50. -C/A-REPAIRED IAW ERS-EM-53MR-4062
- [SDR SIMA2020040617005](https://openairdocs.org/sdr/SIMA2020040617005), Feb 17, 2020: CROSSBEAM. CORRODED. CABIN CROSSBEAM BETWEEN FRAMES 24-25 HAS CORROSION.-C/A-COMPLETE:REMOVED AND REPLACED CABIN CROSSBEAM BETWEEN FRAMES 24-25 IAW ETN-EM-53-139
- [SDR SIMA2020040617009](https://openairdocs.org/sdr/SIMA2020040617009), Feb 17, 2020: LIGHT. DAMAGED. LH FLOOR EMERGENCY LIGHT STRIP EXTRUSIONS #3,AND #8 ARE DAMAGED-C/A-COMPLETE:REPLACED LH FLOOR EMERGENCY LIGHT STRIP EXTRUSIONS #3,AND #8 IAW AMM 33-50-12
- [SDR SIMA2020040617007](https://openairdocs.org/sdr/SIMA2020040617007), Feb 17, 2020: LIGHT. INOPERATIVE. LH FLOOR EMERGENCY LIGHT STRIP #8 EXTRUSION ARE DAMAGED-C/A-COMPLETE:REPLACED #8 LH FLOOR EMERGENCY LIGHT STRIP EXTRUSION IAW AMM 33-50-12.
- [SDR SIMA2020040617004](https://openairdocs.org/sdr/SIMA2020040617004), Feb 17, 2020: SPLICE. INOPERATIVE. RH LATERAL WING-TO-FUSELAGE 194BR ACCESS PANEL EXTERNAL EMERGENCY LIGHT WILL NOT ILLUMINATE.-C/A-COMPLETE:REPLACED SPLICE 8930, OVERWING EMERGENCY LIGHT TEST GO
- [SDR SIMA2020040617006](https://openairdocs.org/sdr/SIMA2020040617006), Feb 17, 2020: LIGHT. DAMAGED. EMERGENCY FLOOR LIGHTING LH EXTRUSION FOR RAMP PANEL IS DAMAGED.-C/A-COMPLETE:REMOVED AND REPLACED EMERGENCY FLOOR LIGHTING LH EXTRUSION FOR RAMP PANEL IAW AMM 
- [SDR SIMA2020040617008](https://openairdocs.org/sdr/SIMA2020040617008), Feb 17, 2020: LIGHT. CORRODED. FORWARD BELLY FAIRING, LH EXTERIOR EMERGENCY LIGHT CORRODED.-C/A-COMPLETE:RRMOVED AND REPLACED RETAINER RING IAW SRM 51-40-02
- [SDR SIMA201912198002](https://openairdocs.org/sdr/SIMA201912198002), Dec 18, 2019: RIVET. SHEARED. RIVETS SHEARED OFF FROM THE RH ANGLE OF THE NLG UPLOCK BOX SUPPORT WEB ON THE RH SIDE OF THE WEB. MOVEMENT OF THIS WEB HAS ALSO CAUSED A LARGE CRACK IN THE FWD 
- [SDR SIMA201911186002](https://openairdocs.org/sdr/SIMA201911186002), Nov 16, 2019: PROXIMITY SWITCH. MALFUNCTIONED. AFTER T.O. NOSE GEAR DID NOT GO UP, GOT LG/LEVER DISAGREE WARNING RAN QRH PROCEDURE, FIXED BUT MADE A VERY LOUD UNCOMFORTABLE BANG WHEN CLOSED. "TRANSFERRED TO 
- [SDR SIMA201911185004](https://openairdocs.org/sdr/SIMA201911185004), Nov 15, 2019: LIGHT. INOPERATIVE. DURING PS-2 FOUND EXTERIOR RH FWD EMERGENCY LIGHT INOP-C/A-RAR EXTERIOR RH FWD EMERGENCY LIGHT IAW 145 AMM 33-50-10 OPS-CHECK GOOD NO FURTHER DEFECTS NOTED

All 179: https://openairdocs.org/aircraft/N610AE/reports.md

## STCs that may be installed (OpenAirDocs) (68, 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-145)

- [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 ST02310AT](https://openairdocs.org/stc/ST02310AT): Installation of SAF-T-GLO photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [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 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 ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [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 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 ST04551AT](https://openairdocs.org/stc/ST04551AT): Installation of the Universal UNS-ILW FMS/GPS. Chippewa Aerospace Inc
- [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 ST00818DE](https://openairdocs.org/stc/ST00818DE): Installation of Honeywell Control Display Unit (CDU) model CD-830. Premier Air Center LLC d/b/a West Star Aviation
- [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 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 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 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
- [STC ST04282AT](https://openairdocs.org/stc/ST04282AT): Installation of the Honeywell DU-875 LCD Flight Display. Chippewa Aerospace Inc
- [STC ST04015AT](https://openairdocs.org/stc/ST04015AT): Installation of the Honeywell NZ-2000 FMS/GPS System with or without WAAS/LPV. Chippewa Aerospace Inc
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC ST09859AC](https://openairdocs.org/stc/ST09859AC): Installation of a SkyTender Beverage Trolley. ASIG LLC
- [STC ST04263AT](https://openairdocs.org/stc/ST04263AT): Modification of Interior Arrangement Configuration from 50 to 30 Passenger Seats (All Tourist Class). VIA Airlines Inc
- [STC ST03390AT](https://openairdocs.org/stc/ST03390AT): Installation of a LIVE TV XM Satellite Radio System. Thales Avionics Inc
- [STC ST04191AT](https://openairdocs.org/stc/ST04191AT): Installation of the Honeywell Sky Connect Tracker Iridium Satcom System. Chippewa Aerospace Inc
- [STC ST02524LA](https://openairdocs.org/stc/ST02524LA): Installation of TCAS version 7.0. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST01754WI](https://openairdocs.org/stc/ST01754WI): Replacement of lighted No Smoking Signs with No Smoking Placards. Georgian Aerospace Group Inc
- [STC ST03483AT](https://openairdocs.org/stc/ST03483AT): Installation of a Portable Beverage Dispensing System, P/N B43-FA-001. Dynamo Beverage Company, USA, L.L.C
- [STC ST04149AT](https://openairdocs.org/stc/ST04149AT): Installation of a Constant Friction Mount, Cradle and Integrated Power Supply on Embraer 145 series aircraft and associated hardware. Avionics Support Group Inc

All 68: https://openairdocs.org/aircraft/N610AE/stcs.md

## Related

- Other Embraer EMB-145 aircraft: https://openairdocs.org/model/embraer-emb-145/aircraft.md
- The Allison AE-3007A engine: https://openairdocs.org/engine/allison-ae-3007a.md

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