# N612AE: 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: 145079
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: September 20, 1998
- Certificate issued: September 26, 2011
- Expires: September 30, 2027
- Mode S code: A7F631
- 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=612AE
- Page: https://openairdocs.org/aircraft/N612AE

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/N612AE/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 N612AE.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20151228021119I](https://openairdocs.org/incident/20151228021119I), Dec 28, 2015: Embraer EMB-145 (N612AE), Montreal, PO, Minor damage. On climb from yul encountered bird strike at 3000FT on left side of aircraft nose. Inflight evaluation of aircraft handling and performance revealed no adverse…

## Service difficulty reports (208, 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 SIMA20220613001](https://openairdocs.org/sdr/SIMA20220613001), Jun 13, 2022: LIGHT. INOPERATIVE. LH AND RH EXTERIOR OVERWING EMERGENCY LIGHTS INOP-C/A-RAR LH AND RH EXTERIOR OVERWING EMERGENCY LIGHTS IAW EMB 145 AMM 33-50-10.
- [SDR SIMA20220612001](https://openairdocs.org/sdr/SIMA20220612001), Jun 12, 2022: LIGHT. INOPERATIVE. LH AND RH OVERWING EMERGENCY LIGHTS INOP-C/A-RAR BOTH THE LH AND RH OVERWING EMERGENCY LIGHTS IAW EMB 145 AMM 33-50-07
- [SDR SIMA20220526001](https://openairdocs.org/sdr/SIMA20220526001), May 26, 2022: LAMP. INOPERATIVE. LH WING AFT OVER WING EMERGENCY LIGHT INOP-C/A-RAR LH AFT OVER WING EMERGENCY LIGHT LAMP, OPC GOOD, IAW AMM 33-50-10
- [SDR SIMA20220416003](https://openairdocs.org/sdr/SIMA20220416003), Apr 16, 2022: NONE. NONE. LH UPPER EXTERIOR EMERGENCY LIGHT INOP-C/A-RAR LH UPPER EXTERIOR EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10 OPS CHECK GOOD NO DEFECTS FOUND
- [SDR SIMA20220213002](https://openairdocs.org/sdr/SIMA20220213002), Feb 13, 2022: NONE. NONE. DURING CLIMB THROUGH 13,200 CABIN PRESSURIZATION ISSUE / DECLARED EMERGENCY NOTICED CABIN ALT WAS 9700 AND INCREASED TO 10,000. PERFORMED QRH AND DECEND TO 10,0
- [SDR SIMA20220110001](https://openairdocs.org/sdr/SIMA20220110001), Jan 10, 2022: NONE. NONE. EXTERNAL EMERGENCY LIGHT AT LH SIDE CENTER FAIRING NOT ILLUMINATING.-C/A-REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT AT LH SIDE CENTER FAIRING IAW E145 AMM 33
- [SDR SIMA20211212002](https://openairdocs.org/sdr/SIMA20211212002), Dec 12, 2021: NONE. NONE. LH AFT EXTERNAL OVERWING EVIT EMERGENCY LIGHT INOP-C/A-RAR LH AFT EXTERNAL OVERWING EXIT EMERGENCY LIGHT LAMP IAW AMM 33-50-07. OPC GOOD
- [SDR SIMA20211127003](https://openairdocs.org/sdr/SIMA20211127003), Nov 27, 2021: NONE. NONE. 1ST ROW EMERGENCY EXIT FLOOR STRIP AND LOWER SERVICE DOOR SIGN INOP-C/A-RAR #2 EMERGENCY LIGHT DC/AC INVERTER IAW EMB AMM 33-50-11-000-801-A & 33-50-11-400-801-
- [SDR SIMA20211119001](https://openairdocs.org/sdr/SIMA20211119001), Nov 19, 2021: NONE. NONE. FWD CABIN EMERGENCY FLASHLIGHT BRACKET BROKEN MEL 2532 - AUTH# 11-267M-C -C/A-RAR FWD CABIN EMERGENCY FLASHLIGHT IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400
- [SDR SIMA20211118001](https://openairdocs.org/sdr/SIMA20211118001), Nov 18, 2021: NONE. NONE. LH EXTERIOR EMERGENCY LIGHT INOP-C/A-RAR L/H EXTERIOR EMERGENCY LIGHT ASSEMBLY IAW 33-50-10 OPS CHECK GOOD
- [SDR SIMA20211118002](https://openairdocs.org/sdr/SIMA20211118002), Nov 18, 2021: NONE. NONE. FWD CABIN EMERGENCY FLASHLIGHT BRACKET BROKEN "TRANSFERRED FROM NRWC 612-SGF-04383 ITEM 1" -C/A-DEFFERED PER MEL 25-32"M" PROCEDURES C/W
- [SDR SIMA20211016003](https://openairdocs.org/sdr/SIMA20211016003), Oct 16, 2021: NONE. NONE. ON APPROACH DUE TO DUAL GENERATOR FAIL AND APU DEFFERRED. NO GEN 1 OR GEN 4 OFF BUS EICAS MESSAGES PRESENTED QRH ABORT NO RESTORATION NO RELATED CMC MESSAGES FO
- [SDR SIMA20211008001](https://openairdocs.org/sdr/SIMA20211008001), Oct 8, 2021: NONE. NONE. LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPC GOOD. END.
- [SDR SIMA202108221003](https://openairdocs.org/sdr/SIMA202108221003), Aug 21, 2021: CHARGER. INOPERATIVE. ROW 1 EMERGENCY FLOOR STRIP LIGHTS INOP-C/A-T/S IAW FIM TASK 33-50-00-810-804-A RAR #2 BATTERY CHARGER ASSY IAW EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-
- [SDR SIMA20210611002](https://openairdocs.org/sdr/SIMA20210611002), Jun 11, 2021: UNKNOWN. MULTIPLE FAIL. ON APPROACH PHASE APROX @ 17000 FT WITH AUTOPILOT ON WE STARTED GETTING MECHANICAL MULTIPLE ALERTS GPWS WARNING " LANDING GEAR, BANK ANGLE, TOO LOW TERR, TERRAI
- [SDR SIMA20210608001](https://openairdocs.org/sdr/SIMA20210608001), Jun 8, 2021: CHARGER. INOPERATIVE. BOTH OVERWING EMERGENCY LIGHTS INOP-C/A-RAR #4 BATTERY AND CHARGER ASSEMBLY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD.
- [SDR SIMA20210523001](https://openairdocs.org/sdr/SIMA20210523001), May 23, 2021: INVERTER. FAULTED. SERVICE DOOR LOWER EMERGENCY PLACARD AND FIRST ROW EMERGENCY LIGHT STRIPS INOP-C/A-T/S IAW FIM TASK 33-50-00-810-804-A RAR #2 BATTERY POWER SUPPLY IAW EMB AMM 3
- [SDR SIMA20210510002](https://openairdocs.org/sdr/SIMA20210510002), May 10, 2021: BATTERY PACK. INOPERATIVE. OVER WING EMERGENCY LIGHTS INOP-C/A-RAR #4 EMERGENCY LIGHTING BATTERY IAW WC 33-700-19. OPC GOOD. END.
- [SDR SIMA20210417002](https://openairdocs.org/sdr/SIMA20210417002), Apr 17, 2021: FLASHLIGHT ASSY. INOPERATIVE. EMERGENCY FLASHLIGHT NEAR LAV WILL NOT CHARGE. DEFERED AFT EMERGENCY FLASHLIGHT PER MEL 25-32. AUTH # 040240M-C. M PROCEDURES COMPLIED WITH. R & R FLASHLIGHT AS
- [SDR SIMA20210320002](https://openairdocs.org/sdr/SIMA20210320002), Mar 20, 2021: WARNING SYSTEM. MALFUNCTIONED. DESCENDING THROUGH 10,000 FT MSC RECEIVED AURAL WARNINGS FOR "TERRAIN", "LANDING GEAR", BANK ANGLE"','PULL UP". BOTH MASTER WARNING AND CAUTION SOUNDED FOR MULT
- [SDR SIMA20210303004](https://openairdocs.org/sdr/SIMA20210303004), Mar 3, 2021: LIGHT. INOPERATIVE. COCKPIT STEP EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED COCKPIT STEP EXIT IDENTIFIER IAW EMB 145 AMM 33-50-13. OPERATIONAL CHECK GOOD.
- [SDR SIMA20201231002](https://openairdocs.org/sdr/SIMA20201231002), Dec 31, 2020: FLASHLIGHT. INOPERATIVE. FWD FA EMERGENCY FLASHLIGHT INOPERABLE, SWAPPED WITH AFT FLASHLIGHT, MEL 2553-AUTH 120356-C. C/A: SWAPPED FWD FA EMERGENCY FLASHLIGHT ASSEMBLY BACK TO THE AFT F
- [SDR SIMA202008030005](https://openairdocs.org/sdr/SIMA202008030005), Jul 30, 2020: CRADLE. BROKEN. AFT FLASHLIGHT BASE BROKE. R & R AFT FLASHLIGHT BASE IAW AMM 33-50-16. OPS CHECK GOOD
- [SDR SIMA202006232002](https://openairdocs.org/sdr/SIMA202006232002), Jun 22, 2020: LAMP. INOPERATIVE. PSU FILLER EMERGENCY LIGHT AT SEAT 12A INOPERATIVE. REMOVED AND REPLACED PSU FILLER EMERGENCY LIGHT LAMP IAW AMM 33-50-07. OPS CHECKED GOOD.
- [SDR SIMA2020060130002](https://openairdocs.org/sdr/SIMA2020060130002), May 30, 2020: SUPPORT. CORRODED. DURING MBV INSPECTION, QC FOUND THE TOILET WASTE VALVE SUPPORT CORRODED. REMOVED AND REPLACED THE TOILET WASTE VALVE SUPPORT IAW SRM 51-40-02.
- [SDR SIMA2020060130001](https://openairdocs.org/sdr/SIMA2020060130001), May 30, 2020: SPAR. CRACKED. DURING MBV INSPECTION, QC FOUND THE RT WING SPAR 1 CRACKED AT A PREVIOUS REPAIR AT RIB 9. REPAIRED RT WING SPAR 1 AT RIB 9 IAW SRM 57-20-05-RE ITEM 3.
- [SDR SIMA202005298001](https://openairdocs.org/sdr/SIMA202005298001), May 28, 2020: FLOOR SUPPORT. CORRODED. DURING MBV INSPECTION, QC FOUND THE LAV CENTER OMEGA BEAM CORRODED AT NUT PLATE HOLE JUST AFT OF FR 59. REPAIRED LAV CENTER OMEGA BEAM NUT PLATE HOLE JUST AFT O
- [SDR SIMA202005298002](https://openairdocs.org/sdr/SIMA202005298002), May 28, 2020: FRAME. CHAFED. DURING MBV INSPECTION, QC FOUND FR 19 CHAFED AT STRINGER 3R. REPAIRED FR 19 CHAFE AT STRINGER 3R IAW SRM 53-00-04RE ITEM 14.
- [SDR SIMA2020061128004](https://openairdocs.org/sdr/SIMA2020061128004), Mar 28, 2020: FIXTURE. BROKEN. SERVICE DOOR EMERGENCY LIGHT FIXTURE BROKEN. REMOVED AND REPLACED THE SERVICE DOOR EMERGENCY LIGHT FIXTURE IAW AMM 33-50-10. OP CHECKS GOOD.
- [SDR SIMA2020061128005](https://openairdocs.org/sdr/SIMA2020061128005), Mar 28, 2020: LIGHT. CRACKED. NR 1 RT EMERGENCY LIGHT STRIP IS CRACKED. REMOVED AND REPLACED NR 1 RT EMERGENCY LIGHT STRIP IAW AMM 33-50-12. SEE BOW344658 FOR INSTALLATION ON AIRCRAFT.
- [SDR SIMA2020061128006](https://openairdocs.org/sdr/SIMA2020061128006), Mar 28, 2020: LIGHT. CRACKED. RT EMERGENCY LIGHT STRIPS CRACKED (5EA). REMOVED ANDREPLACED (5EA) RT EMERGENCY LIGHT STRIPS IAW AMM 33-50-12. SEE BOW344658 FOR INSTALLATION ON AIRCRAFT.
- [SDR SIMA20200114001](https://openairdocs.org/sdr/SIMA20200114001), Jan 14, 2020: DUCT. PUNCTURED. WITH ENGINE PNEUMATIC SET AT CLIMB THRUST. RECEIVED ENG 1 BLEED LEAK ANNUNCIATION. ANNUNCIATION EXTINGUISHED AFTER APPLYING ABNORMAL CHECKLIST.-C/A-FOUND HOLE I
- [SDR SIMA202001131002](https://openairdocs.org/sdr/SIMA202001131002), Jan 11, 2020: LIGHT. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. NO FURTHER 
- [SDR SIMA201908141006](https://openairdocs.org/sdr/SIMA201908141006), Aug 11, 2019: FAN. FAILED. DURING TAXI STRONG RUBBER BURNING SMELL IN THE COCKPIT AND CABING. AFTER TURNING OFF RECIRCULATING FAN, SMELL DISSIPATED.-C/A-REMOVED AND REPLACED BOTH RECIRCUL
- [SDR SIMA20190519003](https://openairdocs.org/sdr/SIMA20190519003), May 19, 2019: INVERTER. INOPERATIVE. AFT 3 EMERGENCY FLOOR STRIPS INOP. C/A-REMOVED AND REPLACED NR 6 INVERTER IAW AMM 33-50-11 OPS CHECK GOOD.
- [SDR SIMA20190507002](https://openairdocs.org/sdr/SIMA20190507002), May 7, 2019: MODULE. INOPERATIVE. SUPPLEMENTAL DECOMPRESSION ABOVE 250, SLOW CABIN CLIMB, OX MASK DEPLOYED AS PER EMER CHECKLIST. C/A-REFER AML #4475082 DECOMPRESSION ABOVE 250, SLOW CABIN CLIMB
- [SDR SIMA201904243002](https://openairdocs.org/sdr/SIMA201904243002), Apr 23, 2019: BRAKE. WEAK. WHILE TAXIING WHEN BRAKES WERE APPLIED "BRAKE DEGRADED" EICAS APPEARED EACH TIME WE TRIED TO COME TO A STOP. WHEN RETURNING TO GATE BRAKES SEEMED TO NEED MORE A
- [SDR SIMA201904154001](https://openairdocs.org/sdr/SIMA201904154001), Apr 14, 2019: LIGHT. INOPERATIVE. FLOOR PROXIMITY STRIP LIGHT INOP. REMOVED AND REPLACED THE FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-50-12
- [SDR SIMA20190316001](https://openairdocs.org/sdr/SIMA20190316001), Mar 16, 2019: CONTROL UNIT. FAILED. PUT GEAR DOWN ON FINAL INTO SHV BRAKE DEGRADED EICAS MSG. C/A-INTEREGRATED CMC, NO MSG FOUND. REMOVED AND REPLACED BCU IAW AMM, 32-41-02.OPS GOOD. PERFORMED HIG
- [SDR SIMA20190303001](https://openairdocs.org/sdr/SIMA20190303001), Mar 3, 2019: OUTFLOW VALVE. FAILED. SUPPLEMENATL CABIN DEPRESSURIZATION AT FL 340. LOUD WHISTLE FROM MAIN CABIN DOOR. EMERGENCY DESCENT ACCCOMP. HIGHEST CABIN ALT WAS 11800 FT. C/A-C/W MANUAL PRES
- [SDR SIMA201902254001](https://openairdocs.org/sdr/SIMA201902254001), Feb 24, 2019: CABIN PRESSURE. MALFUNCTIONED. FL 360 CABIN ALTITUDE WAS UNCONTROLLABLE IN AUTO OR MANUAL MODE FOLLOWED QRH PROCEDURES. PERFORM FIM TASK 21-31-00-810-808-A TO STEP 8 NO DEFECT NOTED, NO MORE 
- [SDR SIMA20190215003](https://openairdocs.org/sdr/SIMA20190215003), Feb 15, 2019: UNKNOWN. ODOR. STALE ODOR FROM PACK 1 DURING TAKEOFF AND IN CLOUDS DURING CRUISE. PERFORMED ETN-EM-72-034 ENG ODOR EVENT T/S. NO ODOR EVENT NOTED. PERFORMED OPS CHECK OF PACK 
- [SDR SIMA20190201002](https://openairdocs.org/sdr/SIMA20190201002), Feb 1, 2019: SKIN. CRACKED. POSSIBLE CRACKED ON CARGO DOOR CUT OUT AS MARKED. MAJOR REPAIR. COMPLIED WITH ERS-EM-52MR-953 CARGO DOOR OUTER SKIN AT HANDLE CUTOUT CRACK PERMANENT REPAIR.
- [SDR SIMA201902041001](https://openairdocs.org/sdr/SIMA201902041001), Feb 1, 2019: MOUNT. CORRODED. REF AML 4372209 MEL 01-936DM-C APU FAILS TO CRANK "TRANSFERRED TO NRWC 612-ABI-02544" MAJOR REPAIR-C/A-ACCOMPLISHED ERS-EM-53MR-3643 PART A REAR FUSELAGE II FRA
- [SDR SIMA20190129002](https://openairdocs.org/sdr/SIMA20190129002), Jan 29, 2019: SWITCH. OBSTRUCTED. BAGGAGE DOOR OPEN CAUTION MSG DURING TAKEOFF. REJECTED TAKEOFF AT 85-90 KTS. DEFERRED BAGGAGE DOOR WARNING INDICATION PERL MEL 52-05. INSPECTED AIRCRAFT FOR DAM
- [SDR SIMA20190119001](https://openairdocs.org/sdr/SIMA20190119001), Jan 19, 2019: CONTROLLER. FAILED. SUPPLEMENTAL CABIN DEPRESSURIZED IN CRZ AT FL 370 WHILE IN AUTO MODE. C/A-DEFERREED PRESSURE CONTROL SYSTEM AUTOMATIC MODE M PROCEDURES C/W VERIFIED AUTAMATIC M
- [SDR SIMA201812187001](https://openairdocs.org/sdr/SIMA201812187001), Dec 17, 2018: SEAL. LEAKING. RAPID DECOMPRESSION @ FL < CABIN ALT SHOWED AND MASTER WARNING SOUNDED> O@ MASKS DEPLOYED FA NOTED SQUEALING NOISE FROM SERVICE DOOR.-C/A-DEFERRED PRESSURIZATIO
- [SDR SIMA20181212003](https://openairdocs.org/sdr/SIMA20181212003), Dec 12, 2018: NOT REPORTED. MALFUNCTIONED. AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKE OFF. ON DESCENT COMING THROUGH 10,000 FEET AIRCRAFT APPEARED TO BEGIN PRESSURIZING NORMALLY. PERFORMED FUNCTIONAL TEST 
- [SDR RAIA201802100001](https://openairdocs.org/sdr/RAIA201802100001), Feb 10, 2018: MECHANISM. LACK OF LUBE. MAIN CABIN DOOR HARD TO OPEN. LUBRICATED THE MAIN DOOR ACTUATING AND LOCKING MECHANISM. OPS CHECKED GOOD.
- [SDR RAIA201709230001](https://openairdocs.org/sdr/RAIA201709230001), Sep 23, 2017: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM CORRODED AT CENTER AISLE CROSSBEAM AT FRAME 54. REPAIRED THE LT OMEGA BEAM.

All 208: https://openairdocs.org/aircraft/N612AE/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/N612AE/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

---
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.