# N607AE: 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 AE3007C series](https://openairdocs.org/engine/allison-ae3007c-series) (registry code 03028)
- 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: 145064
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: June 27, 1998
- Certificate issued: September 30, 2011
- Expires: September 30, 2027
- Mode S code: A7E145
- 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=607AE
- Page: https://openairdocs.org/aircraft/N607AE

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 Allison AE3007C model are included.

## ADs that may apply (OpenAirDocs): 106 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 AE3007C series)

- [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 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 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 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 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 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 132: https://openairdocs.org/aircraft/N607AE/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 NM-04-55](https://openairdocs.org/saib/NM-04-55): . Issued Mar 8, 2004
- [SAIB NE-11-22](https://openairdocs.org/saib/NE-11-22): Engine Controls. Issued Feb 23, 2011
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CEN11IA369](https://openairdocs.org/ntsb/CEN11IA369), Jun 3, 2011: Embraer EMB-145 (N607AE), Chicago, IL, incident, no damage. Probable cause: The overheat and failure the brake during landing due to oxidation of the brake rotors, which went undetected by maintenance personnel. Contributing to the accident was maintenance personnel’s lack…

## FAA accident and incident reports (3)

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 20201020020109I](https://openairdocs.org/incident/20201020020109I), Oct 20, 2020: Embraer EMB-145 (N607AE), Mosinee, WI, No damage. On 10/20/2020, eny 3541 completed a stable approach (RNAV rwy 35) to kcwa, WI. Weather was 400 feet overcast, 1 mile visibility, light snow. The runway…
- [Incident 20110603009499I](https://openairdocs.org/incident/20110603009499I), Jun 3, 2011: Embraer EMB-145 (N607AE), Chicago, IL, No damage. On 06/03/11, anerican eagle airlines, inc., aircraft N607AE, operating as flight 4176 from cmh to ord, landed ord on runway 22 right at approximately 0610. The…
- [Incident 20010703015319I](https://openairdocs.org/incident/20010703015319I), Jul 3, 2001: Emb EMB145 (N607AE), Pittsburgh, PA. (-23) July 03, 2001, at 2045 EST, American eagle flight #4039, an Emb 145, landed on runway 28R after the number 2 engine was shut down for unknown reasons.…

## Service difficulty reports (174, 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 SIMA20211117003](https://openairdocs.org/sdr/SIMA20211117003), Nov 17, 2021: NONE. NONE. MAIN DOOR EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EMERGENCY LT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECK GOOD. END.
- [SDR SIMA20211027003](https://openairdocs.org/sdr/SIMA20211027003), Oct 27, 2021: FAN. FAILED. ELETRICAL BURNING ODOR ON FLT DECK DURING TURBULENCE FOR 5-10 MIN."TRANSFERRED FROM AML PAGE 4819111 ITEM 2"-C/A-RAR AVIONCS BAY EXHAUST FAN #2 IAW AMM 21-26-02
- [SDR SIMA20210918002](https://openairdocs.org/sdr/SIMA20210918002), Sep 18, 2021: LIGHT. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT IAW EMB 145 AMM 33-50-09. OPS CHECK GOOD.
- [SDR SIMA20210614004](https://openairdocs.org/sdr/SIMA20210614004), Jun 14, 2021: UNKNOWN. ODOR. ODD ODOR COMING FROM APU BLEED WHEN APU BLEED WAS SELECTED.-C/A-PERFORMED FIM 21-20-00-810-801A AND ETN-EM-72-034 R10 COULD NOT DUPLICATE DISCREPANCY. NO ODORS 
- [SDR SIMA20210607002](https://openairdocs.org/sdr/SIMA20210607002), Jun 7, 2021: A/C PACK. FAILED. DIVR LSE ACCT AC PACK 2 FAIL-PACK 2 VALVE CLOSED ADVISORY-C/A-FLIGHT CREW PLACARDED OUTFLOW VALVES M PROCEDURES C/W REF MEL 21-22 AUTH 060100DM-C MOC 680820
- [SDR SIMA20210330001](https://openairdocs.org/sdr/SIMA20210330001), Mar 30, 2021: LAMP. INOPERATIVE. AFT EMERGENCY LIGHT CEILING LIGHT INOP-C/A-RAR AFT EMERGENCY LIGHT CEILING LIGHT LAMP IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.
- [SDR SIMA20210212001](https://openairdocs.org/sdr/SIMA20210212001), Feb 12, 2021: FUEL/OIL COOLER. MALFUNCTIONED. ABORTED TAKE OFF 80KTS ACCT MECHANICAL E1 FUEL LOW TEMP MSG ON E1 OIL TEMP 26C, OIL PRESSURE 70-80 PSI. AMBIENT TEMP -29C FLIGHT CANCELED-C/A-TROUBLESHOT IAW RR
- [SDR SIMA20210124001](https://openairdocs.org/sdr/SIMA20210124001), Jan 24, 2021: LAMP. INOPERATIVE. COCKPIT ENTRY EMERGENCY LIGHT INOP-C/A-RAR COCKPIT EMERGENCY LIGHT LAMP IAW EMB AMM TASK 33-50-05-000-801-A AND TASK 33-50-05-400-801-A OPC GOOD
- [SDR SIMA20210124002](https://openairdocs.org/sdr/SIMA20210124002), Jan 24, 2021: FLASHLIGHT. INOPERATIVE. MEL 2553 - AUTH# 01-308-C AFT FLASHLIGHT INOP-C/A-RAR AFT FLASHLIGHT SYSTEM ASSEMBLY IAW 33-50-16-000-801-A AND 33-50-16-400-801-A OPS CHECK GOOD MEL RESTORED
- [SDR SIMA2020042018001](https://openairdocs.org/sdr/SIMA2020042018001), Apr 18, 2020: STRUCTURE. CRACKED. SMALL CRACK IN SHEET METAL WHERE LH NLG FORWARD HINGE ASSEMBLY PASSES THROUGH TO ATTACHMENT POINT.-C/A-REPAIRED LH NLG DOOR FORWARD HINGE ASSY PASS THROUGH POIN
- [SDR SIMA20200416002](https://openairdocs.org/sdr/SIMA20200416002), Apr 16, 2020: FRAME. CHAFED. FR 59 LH IS CHAFFED AT THE OVER HEAD BIN ATTACHMENT ARM NEAR STR. 5 LH.-C/A-REPAIRED SRM 53-00-04. CHAFE DAMAGE ASSIGNED DT-EM-53-1299.
- [SDR SIMA2020040603001](https://openairdocs.org/sdr/SIMA2020040603001), Apr 3, 2020: FLOOR SUPPORT. CORRODED. CABIN LH OMEGA BEAM HAS CORROSION ON PREVIOUS REPAIRED AREA AT FRAME 20.-C/A-DISASSEMBLED PREVIOUS REPAIR OF CABIN LH OMEGA BEAM AT FR 20. REMOVED CORROSION FRO
- [SDR SIMA2020040702007](https://openairdocs.org/sdr/SIMA2020040702007), Apr 2, 2020: RIB. DENTED. RUDDER 1 LEADING EDGE RIB BELOW CENTER HINGE FITTINGS (ZV=1897.0) IS DENTED.-C/A-REMOVED AND REPLACED RIB AT ZV=1897.0 FOR RUDDER LEADING EDGE BELOW CENTER HING
- [SDR SIMA2020040602004](https://openairdocs.org/sdr/SIMA2020040602004), Apr 2, 2020: RIB. BENT. RUDDER 1 SKIN SUPPORT FLANGE (RIB) AT THE LOWER CENTER HINGE IS BENT.-C/A-REMOVED AND REPLACED RIB IAW EMB SRM 51-40-02.
- [SDR SIMA2020040602003](https://openairdocs.org/sdr/SIMA2020040602003), Apr 2, 2020: RIB. BENT. RUDDER 1 SUPPORT FLANGE SKIN AT THE UPPER CENTER HINGE IS BENT.-C/A-REMOVED AND REPLACED RIB IAW EMB SRM 51-40-02.
- [SDR SIMA2020040602005](https://openairdocs.org/sdr/SIMA2020040602005), Apr 2, 2020: RIB. DAMAGED. RUDDER 1 LEADING EDGE RIB ABOVE CENTER HINGE FITTINGS (ZV=2312.0) HAS DAMAGED FLANGE ON INTERIOR SIDE.-C/A- REMOVED AND REPLACED RIB AT ZV=2312.0 IAW EMB SRM 51
- [SDR SIMA2020040801004](https://openairdocs.org/sdr/SIMA2020040801004), Apr 1, 2020: CHANNEL. CRACKED. WEB SUPPORT IN THE AFT END OF THE NLG BAY AT FRAME 7 IS CRACKED.-C/A-RAI WEB SUPPORT (CHANNEL) IN THE AFT END OF THE NLG BAY AT FR 7 IAW SRM 51-10-02.
- [SDR SIMA2020042030004](https://openairdocs.org/sdr/SIMA2020042030004), Mar 30, 2020: SKIN. CRACKED. BAGGAGE DOOR SKIN HAS A CRACK JUST UNDER THE OPEN/CLOSE HANDLE. (CRACK APPROX 1 " LONG)-C/A-C/W ERS-EM-52MR-1073 BAGGAGE DOOR CARGO DOOR HANGLE CUTOUT CRACK PER
- [SDR SIMA2020041026004](https://openairdocs.org/sdr/SIMA2020041026004), Mar 26, 2020: DOOR SILL. CORRODED. CARGO BAY DOOR FUSELAGE SILL IS CORRODED. -C/A-REMOVED AND REPLACED CARGO BAY DOOR FUSELAGE SILL IAW SRM 51-40-02
- [SDR SIMA2020040826003](https://openairdocs.org/sdr/SIMA2020040826003), Mar 26, 2020: SUPPORT BRACKET. CRACKED. CARGO BAY DOOR HOLD OPEN ROD SUPPORT BRACKET IS CRACKED. -C/A-INSTALLED NEW BRACKET IAW EMB--145 SRM CH. 51-40-02.
- [SDR SIMA2020040826002](https://openairdocs.org/sdr/SIMA2020040826002), Mar 26, 2020: SHEAR TIE. CRACKED. SHEAR CLIP CRACKED AT FRAME 16 BETWEEN STRINGERS 1 R -2 R.-C/A-RAR SHEAR CLIP AT FR 16 IAW SRM 51-40-02.
- [SDR SIMA2020040326001](https://openairdocs.org/sdr/SIMA2020040326001), Mar 26, 2020: MOUNT BRACKET. CRACKED. CARGO DOOR ASSIST TORSION BAR MOUNT BRACKET IS CRACKED AT FR 60 RH. -C/A-REMOVED AND REPLACED BRACKET IAW SRM 51-40-02.
- [SDR SIMA2020041625008](https://openairdocs.org/sdr/SIMA2020041625008), Mar 25, 2020: SUPPORT ANGLE. CRACKED. RH WING-TO-FUSELAGE LOWER SUPPORT ANGLE #2 IS CRACKED ON THE FWD END. UP TO THE 1ST RIVET, AND IS APPROX 3/8" LONG. -C/A-C/W REPLACEMENT OF #2 RH WING TO FUSELA
- [SDR SIMA2020041625007](https://openairdocs.org/sdr/SIMA2020041625007), Mar 25, 2020: FRAME. CRACKED. CARGO BAY UNDER FLOOR FRAME IS CRACKED AT FR 72 LH AND STR.16 LH. -C/A-REPAIRED FRAME 72 IAW ERS-EM-53MR-4094.
- [SDR SIMA2020040725005](https://openairdocs.org/sdr/SIMA2020040725005), Mar 25, 2020: SUPPORT ANGLE. CRACKED. LH WING-TO-FUSELAGE UPPER SUPPORT ANGLE HAS EVIDENCE OF A CRACK BY THE RIVET. APPROX 1" LONG AT FRAME 48.-C/A-REPAIRED IAW SRM 53-23-12 ITEM #3.
- [SDR SIMA2020040625004](https://openairdocs.org/sdr/SIMA2020040625004), Mar 25, 2020: SUPPORT ANGLE. CRACKED. LH WING-TO-FUSELAGE LOWER SUPPORT ANGLE #4 IS CRACKED ON THE FWD END. AND IS APPROX 1 1/2" LONG. -C/A-REPAIRED LH WING TO FUSELAGE LOWER SUPPORT ANGLE #4 IAW ET
- [SDR SIMA2020040125003](https://openairdocs.org/sdr/SIMA2020040125003), Mar 25, 2020: SUPPORT ANGLE. CRACKED. LH WING-TO-FUSELAGE LOWER SUPPORT ANGLE #2 IS CRACKED ON THE FWD END. UP TO THE 1ST RIVET, AND IS APPROX 3/8" LONG.-C/A-REMOVED AND REPLACED LH WING TO FUSELAGE
- [SDR SIMA2020040125002](https://openairdocs.org/sdr/SIMA2020040125002), Mar 25, 2020: SUPPORT ANGLE. CRACKED. LH WING-TO-FUSELAGE LOWER SUPPORT ANGLE #3 IS CRACKED ON THE FWD END. AND IS APPROX 1 1/2" LONG. -C/A-R EMOVED AND REPLACED LH WING TO FUSELAGE LOWER SUPPORT AN
- [SDR SIMA2020061118009](https://openairdocs.org/sdr/SIMA2020061118009), Mar 18, 2020: LIGHT. DAMAGED. EMERGENCY LIGHT NR 8 EXTRUSION DAMAGED. REMOVED AND REPLACED EMERGENCY LIGHT NR 8 EXTRUSION, IAW AMM 33-50-12. REFERENCE BOW342807 FOR INSTALLATION.
- [SDR SIMA2020061118010](https://openairdocs.org/sdr/SIMA2020061118010), Mar 18, 2020: STRUCTURE. CORRODED. COCKPIT UNDERFLOOR BETWEEN FRAMES 13 AND 14 AND STRINGERS 20R AND 18L HAS SURFACE CORROSION. C/W REPAIR IAW ERS-EM-53MR-3758 PART B. TDMI RESTORED.
- [SDR SIMA2020061118011](https://openairdocs.org/sdr/SIMA2020061118011), Mar 18, 2020: LIGHT. DAMAGED. RT EXTRUSION NR 4 DAMAGED. REMOVED AND REPLACED RT EXTRUSION NR 4, IAW AMM 33-50-12. REFERENCE BOW342807 FOR INSTALLATION.
- [SDR SIMA2020061118012](https://openairdocs.org/sdr/SIMA2020061118012), Mar 18, 2020: LIGHT. DAMAGED. RT EXTRUSION NR 7 DAMAGED. REMOVED AND REPLACED RT EXTRUSION NR 7, IAW AMM 33-50-12. REFERENCE BOW342807 FOR INSTALLATION.
- [SDR SIMA2020061118013](https://openairdocs.org/sdr/SIMA2020061118013), Mar 18, 2020: LIGHT. DAMAGED. RT EXTRUSION NR 6 DAMAGED. REMOVED AND REPLACED RT EXTRUSION NR 6, IAW AMM 33-50-12. REFERENCE BOW342807 FOR INSTALLATION.
- [SDR SIMA2020061118014](https://openairdocs.org/sdr/SIMA2020061118014), Mar 18, 2020: LIGHT. DAMAGED. EMERGENCY LIGHT NR 1 EXTRUSION DAMAGED. REMOVED AND REPLACED EMERGENCY LIGHT NR 1 EXTRUSION, IAW AMM 33-50-12. REFERENCE BOW342807 FOR INSTALLATION.
- [SDR SIMA2020061118008](https://openairdocs.org/sdr/SIMA2020061118008), Mar 18, 2020: LIGHT. DAMAGED. EMERGENCY LIGHT NR 5 EXTRUSION DAMAGED. REMOVED AND REPLACED EMERGENCY LIGHT NR 5 EXTRUSION, IAW AMM 33-50-12. REFERENCE BOW342807 FOR INSTALLATION.
- [SDR SIMA2020041618005](https://openairdocs.org/sdr/SIMA2020041618005), Mar 18, 2020: STRUCTURE. CORRODED. TDMI 607T5323 ORIGNAL LG PG 4475656/3 TRANSFERRED FROM NRTC E710113, COCKPIT UNDERFLOOR BETWEEN FRAMES 13 AND 14 AND STRINGERS 20R AND 18L HAS SURFACE CORROSION
- [SDR SIMA2020031312002](https://openairdocs.org/sdr/SIMA2020031312002), Mar 12, 2020: INVERTER. FAILED. FLOOR EMERGENCY LIGHT STRIP INOP #1-C/A-REMOVED AND REPLACED INVERTER OVER SERVICE DOOR IAW 33-50-11 OPS CHECK GOOD
- [SDR SIMA202001310003](https://openairdocs.org/sdr/SIMA202001310003), Jan 30, 2020: CRADLE. BROKEN. FWD ATTENDANT EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-REMOVED AND REPLACED FLASHLIGHT ASSY IAW EMB 145 AMM 33-50-16. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.
- [SDR SIMA201911143002](https://openairdocs.org/sdr/SIMA201911143002), Nov 13, 2019: FAN. FAILED. CLIMBING THROUGH 15000' WE HEARD AND FELT A THUD FOWLLED BY A ELEC/OZONE BURNING SMELL FOR 30 SEC IN THE COCKPIT AND GALLY THE SAME SMELL OCCURED FOR 10 SEC IN 
- [SDR SIMA201910076006](https://openairdocs.org/sdr/SIMA201910076006), Oct 6, 2019: BATTERY PACK. FAILED. #2 EMERGENCY BATTERY INOP-C/A-REMOVED AND REPLACED #2 EMERGENCY LIGHT BATTERY ASSEMBLY AND CHARGER ASSEMBLY IAW AMMK 33-50-04.OPS CHECK GOOD. BATTEERY CHARGER A
- [SDR SIMA201910076005](https://openairdocs.org/sdr/SIMA201910076005), Oct 6, 2019: BATTERY PACK. FAILED. #3 EMERGENCY BATTERY INOP-C/A-REMOVED AND REPLACED #3 EMERGENCY LIGHT BATTERY ASSEMBLY AND CHARGER ASSEMBLY IAW AMM 33-50-=04.OPS CHECK GOOD. BATTERY CHARGER AS
- [SDR SIMA201910076004](https://openairdocs.org/sdr/SIMA201910076004), Oct 6, 2019: BATTERY PACK. FAILED. #4 EMERGENCY BATTERY INOP-C/A-REMOVED AND REPLACED #4 EMERGENCY LIGHT BATTERY ASSEMBLY AND CHARGER ASSEMBLY IAW AMM 33-50-04.OPS CHECK GOOD.
- [SDR SIMA201910076007](https://openairdocs.org/sdr/SIMA201910076007), Oct 6, 2019: CHARGER. FAILED. #1 EMERGENCY BATTERY INOP-C/A-REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSEMBLY AND CHARGER ASSEMBLY #1 IAW AMM 33-50-04 OPS CHECK GOOD. EMERGENCY LIGHTING 
- [SDR SIMA20190913002](https://openairdocs.org/sdr/SIMA20190913002), Sep 13, 2019: FLASHLIGHT. DAMAGED. FWD FLIGHT ATTENDANT FLASHLIGHT FOUND DAMAGED. C/A-REMOVED AND REPLACED FWD FLIGHT ATTENDANT FLASHLIGHT IAW AMM 33-50-16. OPS CHECK GOOD.
- [SDR SIMA201908219005](https://openairdocs.org/sdr/SIMA201908219005), Aug 19, 2019: BATTERY PACK. INOPERATIVE. FA FWD FLASHLIGHT NOT WORKING. REMOVED AND REPLACED FLASHLIGHT BATTERY AS REQUIRED OPC GOOD.
- [SDR SIMA201908164002](https://openairdocs.org/sdr/SIMA201908164002), Aug 14, 2019: MODULE. FAILED. CABIN LIGHTS WILL NOT TURN OFF. BURNING SMELL FROM LIGHT BULB NEAR FA CONTROL PANEL AND FORWARD WINDOW. REMOVED AND REPLACED CABIN LIGHTS MODULE CONTROL ASSY IA
- [SDR SIMA201908121005](https://openairdocs.org/sdr/SIMA201908121005), Aug 11, 2019: FAN. INOPERATIVE. OIL SMELL IN THE COCKPIT, INSPECTED NR 1 & 2 PACK RECIRCULATION SYSTEMS AND FOUND NR 2 RECIRCULATING FAN INOPERATIVE, REMOVED AND REPLACED THE NR 2 RECIRCULATIO
- [SDR SIMA20190729001](https://openairdocs.org/sdr/SIMA20190729001), Jul 29, 2019: WIRE. BROKEN. FOUND EMERGENCY LIGHT STRIP WIRE BROKEN IN ROW 16A. C/A-REMOVED AND REPLACED EMERGENCY FLOOR STRIP LIGHT IAW AMM 33-50-12 OPS CHECK GOOD.
- [SDR SIMA20190702004](https://openairdocs.org/sdr/SIMA20190702004), Jul 2, 2019: DOOR SEAL. TORN. PASSENGER DOOR SEAL ON DOOR SIDE IS TORN (MAIN DOOR DIFFICULT TO OPEN/CLOSE). -C/A-REMOVED AND REPLACED PAX DOOR SEAL IAW AMM 52-18-04, REFER TO 607-MQT-02445 F
- [SDR SIMA20190701003](https://openairdocs.org/sdr/SIMA20190701003), Jul 1, 2019: DOOR. OUT OF ADJUST. SUPPLEMENTAL MAIN DOOR DIFFICULT TO OPEN/CLOSE "TRANSFERRED TO NRWC 607-ORD-02433". C/A-REF NRWC # 607-ORD-02433 REF AML # 4532148 ITEM #1 AND #3 FOR CORRECTIVE

All 174: https://openairdocs.org/aircraft/N607AE/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/N607AE/stcs.md

## Related

- Other Embraer EMB-145 aircraft: https://openairdocs.org/model/embraer-emb-145/aircraft.md
- The Allison AE3007C series engine: https://openairdocs.org/engine/allison-ae3007c-series.md

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