# N923AE: 2005 Embraer EMB-145LR

- Status: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212, 55 seats)
- Engine: [Rolls-Royce AE3007 series](https://openairdocs.org/engine/rolls-royce-ae3007-series) (registry code 54582)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 14500907
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 30, 2005
- Certificate issued: September 19, 2011
- Expires: September 30, 2027
- Mode S code: ACC954
- 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=923AE
- Page: https://openairdocs.org/aircraft/N923AE

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Rolls-Royce AE3007 model are included.

## ADs that may apply (OpenAirDocs): 110 in force

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

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-08-07](https://openairdocs.org/ad/2025-08-07): Flight Controls · Embraer EMB-145, EMB-145ER, EMB-145MR and 4 more. Effective Jun 26, 2025
- [AD 2024-26-07](https://openairdocs.org/ad/2024-26-07): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 11, 2025
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2021-07-14](https://openairdocs.org/ad/2021-07-14): Main landing gear · Yaborã Indústria Aeronáutica EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Apr 20, 2021
- [AD 2021-04-09](https://openairdocs.org/ad/2021-04-09): Engine fuel and control · Yaborã Indústria Aeronáutica EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Mar 30, 2021
- [AD 2019-03-30](https://openairdocs.org/ad/2019-03-30): Engine Exhaust · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 26, 2019
- [AD 2017-15-16](https://openairdocs.org/ad/2017-15-16): Flight controls · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Sep 5, 2017
- [AD 2017-12-09](https://openairdocs.org/ad/2017-12-09): Fuel · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Jul 20, 2017
- [AD 2017-04-12](https://openairdocs.org/ad/2017-04-12): Ice and rain protection · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Mar 29, 2017
- [AD 2015-02-13](https://openairdocs.org/ad/2015-02-13): Nacelles/pylons; Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 6, 2015
- [AD 2013-22-18](https://openairdocs.org/ad/2013-22-18): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Nov 20, 2013
- [AD 2012-19-06](https://openairdocs.org/ad/2012-19-06): Stabilizers · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 9 more. Effective Oct 29, 2012
- [AD 2011-21-15](https://openairdocs.org/ad/2011-21-15): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 7 more. Effective Nov 23, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2010-16-02](https://openairdocs.org/ad/2010-16-02): Airborne Auxiliary Power · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 9, 2010
- [AD 2010-16-01](https://openairdocs.org/ad/2010-16-01): Fuel · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Sep 9, 2010
- [AD 2010-12-07](https://openairdocs.org/ad/2010-12-07): Wings · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jul 22, 2010
- [AD 2010-11-01](https://openairdocs.org/ad/2010-11-01): Fuselage · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jul 6, 2010
- [AD 2010-10-11](https://openairdocs.org/ad/2010-10-11): Landing gear · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jun 21, 2010
- [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010
- [AD 2010-03-07](https://openairdocs.org/ad/2010-03-07): Landing gear · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 11, 2010
- [AD 2009-26-02](https://openairdocs.org/ad/2009-26-02): Ice and rain protection · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 19, 2010
- [AD 2009-01-05](https://openairdocs.org/ad/2009-01-05): Maximum takeoff weight (MTOW) · Embraer EMB-145, EMB-145EP, EMB-145ER and 4 more. Effective Mar 27, 2009
- [AD 2008-22-19](https://openairdocs.org/ad/2008-22-19): Flight deck · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 19, 2008
- [AD 2008-17-05](https://openairdocs.org/ad/2008-17-05): Fuel tanks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 23, 2008
- [AD 2008-10-08](https://openairdocs.org/ad/2008-10-08): Reduces the compliance time for doing the modification · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective May 23, 2008
- [AD 2008-05-02](https://openairdocs.org/ad/2008-05-02): Tail section or rudder pedals · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Apr 8, 2008
- [AD 2008-03-03](https://openairdocs.org/ad/2008-03-03): Elevator control system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Feb 14, 2008
- [AD 2007-24-03](https://openairdocs.org/ad/2007-24-03): Forward fuselage right hand (RH) side skin · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jan 2, 2008
- [AD 2007-10-11](https://openairdocs.org/ad/2007-10-11): Electrical bonding clamps · Embraer EMB-135BJ (Legacy 600), EMB-135LR, EMB-145LR and 2 more. Effective Jun 21, 2007
- [AD 2007-04-09](https://openairdocs.org/ad/2007-04-09): Left- and right-hand windshield temperature controllers · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 23, 2007
- [AD 2007-04-03](https://openairdocs.org/ad/2007-04-03): Pitot static heating relay K0057 · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 21, 2007
- [AD 2006-19-04](https://openairdocs.org/ad/2006-19-04): Honeywell COM unit and Mode S transponder · Bombardier BD-700-1A10, BD-700-1A11, 550 and 26 more. Effective Oct 17, 2006
- [AD 2006-16-17](https://openairdocs.org/ad/2006-16-17): Torque values of the screws that attach the seat tracks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 25, 2006
- [AD 2006-07-01](https://openairdocs.org/ad/2006-07-01): Horizontal stabilizer control unit (HSCU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective May 1, 2006
- [AD 2006-03-06](https://openairdocs.org/ad/2006-03-06): Pilot's and co-pilot's seat tracks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 13, 2006
- [AD 2005-25-17](https://openairdocs.org/ad/2005-25-17): Auxiliary power unit (APU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 18, 2006
- [AD 2005-24-11](https://openairdocs.org/ad/2005-24-11): Elevator gust lock system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 9, 2006
- [AD 2005-24-02](https://openairdocs.org/ad/2005-24-02): Airplane flight manual (AFM) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 28, 2005
- [AD 2005-23-20](https://openairdocs.org/ad/2005-23-20): Auxiliary power unit (APU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 27, 2005
- [AD 2005-23-13](https://openairdocs.org/ad/2005-23-13): Nose landing gear (NLG) wheel · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 19, 2005
- [AD 2005-22-08](https://openairdocs.org/ad/2005-22-08): Total air temperature (TAT) sensor heating system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Nov 30, 2005
- [AD 2005-20-37](https://openairdocs.org/ad/2005-20-37): Main landing gear (MLG) trailing arms and integrity of the MLG pivot axle sealant. · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Nov 16, 2005
- [AD 2005-14-02](https://openairdocs.org/ad/2005-14-02): Left and right engine fire handles · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Aug 15, 2005
- [AD 2005-14-03](https://openairdocs.org/ad/2005-14-03): Engine-driven hydraulic pump · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Aug 10, 2005
- [AD 2005-13-22](https://openairdocs.org/ad/2005-13-22): Electric fuel pumps · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jul 7, 2005
- [AD 2005-05-09](https://openairdocs.org/ad/2005-05-09): Forward upper liners · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Apr 14, 2005
- [AD 2005-04-05](https://openairdocs.org/ad/2005-04-05): Air turbine starter (ATS) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 24, 2005
- [AD 2005-01-05](https://openairdocs.org/ad/2005-01-05): Nose Landing Gear Wheel Nuts and Associated Inner and Outer Seals, and Reidentifying the Landing Gear Strut · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Feb 9, 2005

### Matched by engine (Rolls-Royce AE3007 series)

- [AD 2020-16-13](https://openairdocs.org/ad/2020-16-13): Turbine Engine Compressor Section · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Aug 14, 2020
- [AD 2018-17-04](https://openairdocs.org/ad/2018-17-04): Turbine section · Rolls-Royce AE 2100D2A, AE 2100D3 and AE 3007A2. Effective Sep 21, 2018
- [AD 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018
- [AD 2017-11-05](https://openairdocs.org/ad/2017-11-05): Turbine/ turboprop Engine, Turbine Section · Rolls-Royce AE 3007C and AE 3007C1. Effective Jul 18, 2017
- [AD 2015-02-08](https://openairdocs.org/ad/2015-02-08): Turbine wheels · Rolls-Royce AE 2100D2, AE 2100D2A, AE 2100D3 and 11 more. Effective Mar 11, 2015
- [AD 2013-26-06](https://openairdocs.org/ad/2013-26-06): High-pressure turbine (HPT) stage 2 wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Feb 7, 2014
- [AD 2011-22-03](https://openairdocs.org/ad/2011-22-03): Low-cycle fatigue cracks · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 4 more. Effective Nov 17, 2011
- [AD 2009-24-04](https://openairdocs.org/ad/2009-24-04): Fan spinner · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 5 more. Effective Dec 28, 2009
- [AD 2009-04-03](https://openairdocs.org/ad/2009-04-03): 2nd stage, 3rd stage, and 4th stage compressor wheels · Rolls-Royce AE 1107C and AE 3007A1E. Effective Mar 24, 2009
- [AD 2007-24-05](https://openairdocs.org/ad/2007-24-05): Engine oil temperature · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 8 more. Effective Jan 2, 2008
- [AD 2004-04-05](https://openairdocs.org/ad/2004-04-05): Engine oil system · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Mar 9, 2004
- [AD 2003-25-08](https://openairdocs.org/ad/2003-25-08): 1st and 2nd stage turbine spacers · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 3 more. Effective Jan 21, 2004
- [AD 2001-25-05](https://openairdocs.org/ad/2001-25-05): Compressor Cone Shafts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jan 23, 2002
- [AD 2001-19-03](https://openairdocs.org/ad/2001-19-03): High Pressure Turbine 1st to 2nd Stage Turbine Spacer · Rolls-Royce AE 3007A and AE 3007C. Effective Oct 29, 2001
- [AD 2001-17-31](https://openairdocs.org/ad/2001-17-31): Second Stage High Pressure Turbine Wheel · Rolls-Royce AE 2100A, AE 2100C, AE 2100D3 and 2 more. Effective Oct 5, 2001
- [AD 2000-18-06](https://openairdocs.org/ad/2000-18-06): Digital Electronic Controls · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 22, 2000
- [AD 2000-13-01](https://openairdocs.org/ad/2000-13-01): Turbine Wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 1, 2000
- [AD 2000-11-22](https://openairdocs.org/ad/2000-11-22): Critical Life-Limited Parts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Aug 7, 2000
- [AD 99-03-03](https://openairdocs.org/ad/99-03-03): Full Authority Digital Engine Control (FADEC) · Rolls-Royce AE 3007A and AE 3007A1/1. Effective Feb 16, 1999
- [AD 98-11-32](https://openairdocs.org/ad/98-11-32): Sump Magnetic Chip Collector Plug · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Jun 18, 1998

### Historical (superseded or no longer in force)

- [AD 2008-13-14](https://openairdocs.org/ad/2008-13-14) (historical): Fuel system limitations (FSL) · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jul 30, 2008
- [AD 2007-12-17](https://openairdocs.org/ad/2007-12-17) (historical): Metallic tubes enclosing the vent and pilot valve wires · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Jul 19, 2007
- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 2006-20-08](https://openairdocs.org/ad/2006-20-08) (historical): Rod ends of aileron power control actuator, superseding AD 99-05-04 · Embraer EMB-145, EMB-145EP, EMB-145ER and 4 more. Effective Nov 8, 2006
- [AD 2006-04-02](https://openairdocs.org/ad/2006-04-02) (historical): Pitot static heating relay K0057 · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Mar 31, 2006
- [AD 2005-26-15](https://openairdocs.org/ad/2005-26-15) (historical): Certain components of the elevator control system · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 8 more. Effective Feb 3, 2006
- [AD 2005-25-04](https://openairdocs.org/ad/2005-25-04) (historical): Tail section or rudder pedals · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Dec 23, 2005
- [AD 2001-17-04](https://openairdocs.org/ad/2001-17-04) (historical): Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Sep 5, 2001
- [AD 2000-04-09](https://openairdocs.org/ad/2000-04-09) (historical): Elevator Servo Tab and Spring Tab Hinge Fittings of the Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Mar 10, 2000
- [AD 2010-19-01](https://openairdocs.org/ad/2010-19-01) (historical): High pressure turbine · Rolls-Royce AE 3007A. Effective Oct 27, 2010
- [AD 2009-08-51](https://openairdocs.org/ad/2009-08-51) (historical): High-pressure turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 6 more. Effective May 27, 2009
- [AD 2008-26-06](https://openairdocs.org/ad/2008-26-06) (historical): High-pressure turbine (HPT) · AE 3007A. Effective Jan 8, 2009
- [AD 2008-19-51](https://openairdocs.org/ad/2008-19-51) (historical): AE 3007A, AE 3007A1, AE 3007A1E and 5 more
- [AD 2001-08-15](https://openairdocs.org/ad/2001-08-15) (historical): Oil System · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective May 14, 2001
- [AD 2000-09-05](https://openairdocs.org/ad/2000-09-05) (historical): Cone Shafts · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jul 5, 2000
- [AD 99-02-51](https://openairdocs.org/ad/99-02-51) (historical): Starter Shaft Seal · AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Apr 20, 1999

All 126: https://openairdocs.org/aircraft/N923AE/ads.md

## Information bulletins (advisory) (10 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB AIR-20-17](https://openairdocs.org/saib/AIR-20-17): Air Conditioning - Cabin Pressure Control System. Issued Nov 3, 2020
- [SAIB NM-19-17](https://openairdocs.org/saib/NM-19-17): Ice and Rain Protection: Electrical Wiring Terminations at Pitot and TAT Relays. Issued Dec 5, 2019
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008
- [SAIB NM-08-15](https://openairdocs.org/saib/NM-08-15): Instruments: Contamination of the Attitude Heading Reference System (AHRS) Computers. Issued Mar 26, 2008
- [SAIB NM-07-40](https://openairdocs.org/saib/NM-07-40): Embraer EMB-135/145 Landing Gear Incident. Issued Jul 9, 2007
- [SAIB NM-07-20](https://openairdocs.org/saib/NM-07-20): Flight Data Recorders. Issued Mar 21, 2007
- [SAIB NE-11-22](https://openairdocs.org/saib/NE-11-22): Engine Controls. Issued Feb 23, 2011
- [SAIB CE-00-18](https://openairdocs.org/saib/CE-00-18): . Issued Mar 30, 2000
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N923AE.

## FAA accident and incident reports

None matched to N923AE.

## Service difficulty reports (190, 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 HNAA2026070300569](https://openairdocs.org/sdr/HNAA2026070300569), Jun 4, 2026: SKIN. GOUGED. LT CENTER I LOWER FUSELAGE EXTERIOR SKIN GOUGED BTW FR 19-20 AND BTW STRINGERS 16L-17L. PERFORMED DOUBLER AND FILLER REPAIR ON LT CENTER 1 LOWER FUSELAGE SKIN B
- [SDR HNAA2026070300571](https://openairdocs.org/sdr/HNAA2026070300571), Jun 3, 2026: FLOORBEAM. CORRODED. WARDROBE FLOORBEAM ANGLE AT FRAME 18 HAS CORROSION. REMOVED AND REPLACED WARDROBE FLOORBEAM ANGLE AT FRAME 18 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026070300568](https://openairdocs.org/sdr/HNAA2026070300568), May 31, 2026: SKIN. DAMAGED. LEFT ELEVATOR LOWER SURFACE HAS LIGHTNING STRIKE DAMAGE, MELTED METAL AT THE OUTBD AFT CORNER. PERFORMED PERMANENT REPAIR OH LT ELEVATOR LOWER SURFACE AT THE OT
- [SDR HNAA2026070300567](https://openairdocs.org/sdr/HNAA2026070300567), May 31, 2026: SKIN. CRACKED. REAR FUSELAGE 2 HAS A POSSIBLE CRACK AT RT SIDE FR 77 JUST BELOW S8R. PERFORMED (.500") CUTOUT ON THE SKIN TO REMOVE THE CRACKED AND INSTALLED BUSHING ON REAR F
- [SDR HNAA2026070300566](https://openairdocs.org/sdr/HNAA2026070300566), May 28, 2026: SPAR. CRACKED. THE LEFT WING SPAR 1 AT RIB 9 SHOWS A RELEVANT INDICATION OF A CRACK AT THE FWD LOWER FLANGE. PERFORMED PERMANENT REPAIR OF THE LT SPAR I AT RIB 9 IAW SRM 57-20
- [SDR HNAA2026070300570](https://openairdocs.org/sdr/HNAA2026070300570), May 28, 2026: DOOR SILL. CORRODED. CARGO DOOR CUTOUT LOWER SILL CORRODED ON FORWARD END. R & R CARGO DOOR CUTOUT LOWER SILL IAW SRM 51-40-02.
- [SDR HNAA2025062400458](https://openairdocs.org/sdr/HNAA2025062400458), Jun 22, 2025: UNKNOWN. ODOR. SMELL OF BURNING RUBBER AROUND 18K. RAN ENGINES W APU ON AIR GROUNDS OPEN HYDRAULICS AND PACKS RUNNING INSPECTED MAIN BATT 1,2 & BACKUP RELAY BOX. INSPECTED RIG
- [SDR HNAA2025052300363](https://openairdocs.org/sdr/HNAA2025052300363), May 22, 2025: CONTACTOR. BURNED. FA REPORTS ELECTRICAL BURNING SMEILL FOR 10MIN IN FWD CABIN DURING APPROACH STARTING AT 8000FT, PREV HISTORY FOR FUMES WITH BURNED CONTACTOR SUPPORT IN LH DIST 
- [SDR HNAA2025050500301](https://openairdocs.org/sdr/HNAA2025050500301), May 3, 2025: CONTROLLER. ABNORMAL. WINDSHIELD HEAT #2 FAILED IN FLIGHT, CMC MESSAGE W/S HEATING INOP, MOMENTARY IN ICING. R+R WINDSHIELD HEAT TEMP CONTROLLER IAW 30-42-01. PERFORMED OPS CHECK IAW
- [SDR HNAA2025041000198](https://openairdocs.org/sdr/HNAA2025041000198), Apr 10, 2025: UNKNOWN. ODOR. AFTER POSSIBLE LIGHTNING STRIKE SMELLED FAINT BURNING SMELL THAT DISIPATED.
- [SDR HNAA2025041000197](https://openairdocs.org/sdr/HNAA2025041000197), Apr 10, 2025: UNKNOWN. ODOR. AFTER POSSIBLE LIGHTNING STRIKE SMELLED FAINT BURNING SMELL THAT DISSIPATED.
- [SDR HNAA2025012400070](https://openairdocs.org/sdr/HNAA2025012400070), Jan 23, 2025: UNKNOWN. SMOKE. AFTER E-1 START, SMOKE IN FLIGHT DECK AND CABIN. PULLED BOTH "T" HANDLES,(DID NOT BLOW BOTTLES), AND EVACUATED THROUGH PAX DOOR AND GALLEY DOOR. NO ABNORMAL ENG
- [SDR HNAA2025010300014](https://openairdocs.org/sdr/HNAA2025010300014), Jan 2, 2025: SENSOR. FAULTED. REJECTED TAKE OFF AT 50 KNOTS DUE TO SPS ADVANCED AND FLAP LOW SPEED ON EICAS. FOUND "FLAP FEEDBACK POS FAIL" ON CMC. R&R FPTU IAW AMM 27-53-05. OPS CHECK GOOD.
- [SDR HNAA2024050900345](https://openairdocs.org/sdr/HNAA2024050900345), May 8, 2024: ANTI-ICE VALVE. FAULTED. ON T/O ROLL AT 60 KNTS ICE COND-A/I INOP, NO T/O CONFIG AND E2 A/ICE FAIL DISPLAYED. E2 A/ICE FAIL REMAINS DISPLAYED. FACT 08MAY24 19:00 TRI PERFORMED A/ICE VAL
- [SDR HNAA2024050900344](https://openairdocs.org/sdr/HNAA2024050900344), May 8, 2024: UNKNOWN. ODOR. FUEL LIKE SMELL AROUND ROW 12 FACT 08MAY24 23:55 CLT INSPECTED PACK SYSTEMS AND FUEL SYS AT WING STUB. NO LEAKS FOUND. TAXI'D A/C. PERFORMED 4 HIGH PWR RUNS, NO
- [SDR HNAA2024022700140](https://openairdocs.org/sdr/HNAA2024022700140), Feb 16, 2024: BULKHEAD. CRACKED. E022752 NLG WHEEL WELL RH BULKHEAD CRACKED INSIDE NOSE HYDRAULIC COMPARTMENT, AT AFT UPPER END OF BULKHEAD. PERFORMED REPAIR ON NLG WHEEL WELL R/H BULKHEAD INSI
- [SDR HNAA2024022700141](https://openairdocs.org/sdr/HNAA2024022700141), Feb 14, 2024: RIB. CRACKED. E017252 POSSIBLE CRACKS ON RH WING RIB 21. FABRICATED AND DRILLED DOUBLER, FILLER, AND SHIM AND INSTALLED REPAIR OF R/H WING RIB 21 IAW EMB 145 SRM 57-50-07 ITE
- [SDR HNAA2024022700152](https://openairdocs.org/sdr/HNAA2024022700152), Feb 12, 2024: BEARING RACE. CORRODED. E021954 NLG LEG RH TRUNNION BEARING RACE PITTED. REMOVED AND REPLACED NLG RH TRUNNION IAW EMB SRM 51-40-02
- [SDR HNAA2024022700139](https://openairdocs.org/sdr/HNAA2024022700139), Feb 7, 2024: SKIN. DAMAGED. E020843 BURN MARK ON FR26 BETWEEN STRINGERS 18R - 19R. REPAIRED BURN MARK AT FR26 BETWEEN STRINGERS 18R - 19R IAW EMB ETD2024-145-003973 REV. A AND EO1-53-24-01
- [SDR HNAA2024022700138](https://openairdocs.org/sdr/HNAA2024022700138), Feb 7, 2024: SKIN. DAMAGED. E020842 BURN MARK ON SKIN AT FR14 BETWEEN STRINGERS 20R - 21R. REPAIRED BURN MARK ON EXTERNAL SKIN AT FR14 BETWEEN STRINGERS 20R-21R IAW EMBRAER ETD2024-145-004
- [SDR HNAA2024022700137](https://openairdocs.org/sdr/HNAA2024022700137), Feb 7, 2024: SKIN. DAMAGED. E020841 BURN MARK ON FR22 BETWEEN STRINGERS 18R - 19R. PERFORMED THE CUT OUT OF THE DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER ON BURN MARK AT FR
- [SDR HNAA2024022700164](https://openairdocs.org/sdr/HNAA2024022700164), Feb 4, 2024: FLOOR SUPPORT. CORRODED. E020502 LH CENTER FLOOR SILL IS CORRODED AT FRAME 49. REMOVED AND INSTALLED LH CENTER FLOOR SILL AT FRAME 49. IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024022700163](https://openairdocs.org/sdr/HNAA2024022700163), Feb 4, 2024: SEAT TRACK. CORRODED. E020488 RH UPPER SEAT TRACK #3 IS GOUGED AND CORRODED. RAR RH UPPER SEAT TRACK #3 IAW EMB 145 AMM 53-01-06
- [SDR HNAA2024022700162](https://openairdocs.org/sdr/HNAA2024022700162), Feb 4, 2024: FLOOR SUPPORT. CORRODED. E020486 RH CENTER FLOOR SILL HAS CORROSION BETWEEN FRAMES 30-33. : RAR R/H CENTER FLOOR SILL BETWEEN FRAMES 30-33 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024022700161](https://openairdocs.org/sdr/HNAA2024022700161), Feb 4, 2024: FLOOR SUPPORT. CORRODED. E020483 LH CENTER FLOOR SILL HAS CORROSION AT FRAME 24. REMOVED AND INSTALLED SERVICEABLE LH CENTER FLOOR SILL AT FRAME 24 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024022700160](https://openairdocs.org/sdr/HNAA2024022700160), Feb 4, 2024: FLOOR SUPPORT. CORRODED. E020482 RH OUTBD FLOOR SILL #1 HAS CORROSION. REMOVED AND REPLACED WITH SERVICEABLE RH OUTBD FLOOR SILL #1 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024022700159](https://openairdocs.org/sdr/HNAA2024022700159), Feb 4, 2024: FLOOR SUPPORT. CORRODED. E020481 LH OUTBD FLOOR SILL #5 HAS CORROSION. REMOVED AND REPLACED LH OUTBD FLOOR SILL #5 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024022700158](https://openairdocs.org/sdr/HNAA2024022700158), Feb 4, 2024: FLOOR SUPPORT. CORRODED. E020480 LH OUTBD FLOOR SILL #4 HAS CORROSION. REMOVED AND REPLACED WITH SERVICEABLE LH OUTBD FLOOR SILL #4 IAW EMB145 SRM 51-40-02.
- [SDR HNAA2024022700157](https://openairdocs.org/sdr/HNAA2024022700157), Feb 4, 2024: FLOOR SUPPORT. CORRODED. E020479 LH OUTBD FLOOR SILL #3 HAS CORROSION. REMOVED AND REPLACED LH OUTBD FLOOR SILL #3 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024022700156](https://openairdocs.org/sdr/HNAA2024022700156), Feb 4, 2024: FLOOR SUPPORT. CORRODED. E020478 LH OUTBD FLOOR SILL #2 HAS CORROSION. REMOVED AND REPLACED LH OUTBD FLOOR SILL #2 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024022700155](https://openairdocs.org/sdr/HNAA2024022700155), Feb 4, 2024: FLOOR SUPPORT. CORRODED. E020471 RH FLOOR SILL #6 CORRODED ON MULTIPLE AREAS. REMOVED AND INSTALLED SERVICEABLE RH FLOOR SILL #6 IAW EMB 145 SRM 51-40-02,
- [SDR HNAA2024022700151](https://openairdocs.org/sdr/HNAA2024022700151), Feb 4, 2024: DOOR SILL. CORRODED. E020579 AFT SERVICE DOOR SILL CORRODED AROUND NUT PLATE HOLE. REMOVED AND REPLACED WITH NEW SERVICEABLE AFT SERVICE DOOR SILL IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024022700150](https://openairdocs.org/sdr/HNAA2024022700150), Feb 4, 2024: SHEAR TIE. CORRODED. E020549 SHEAR CLIP AT FR 62 BETWEEN STGR19R / 20R CORRODED. RAR SHEAR CLIP AT FR 62 BETWEEN STGR19R / 20R IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024022700149](https://openairdocs.org/sdr/HNAA2024022700149), Feb 4, 2024: SEAT TRACK. CORRODED. E020513 LH UPPER SEAT TRACK #5 IS CORRODED. RAR LH UPPER SEAT TRACK #5 IAW EMB 145 AMM 53-01-06.
- [SDR HNAA2024022700148](https://openairdocs.org/sdr/HNAA2024022700148), Feb 4, 2024: SEAT TRACK. CORRODED. E020512 LH UPPER SEAT TRACK #4 IS CORRODED. RAR NEW LH UPPER SEAT TRACK #4 IAW EMB 145 AMM 53-01-06.
- [SDR HNAA2024022700147](https://openairdocs.org/sdr/HNAA2024022700147), Feb 4, 2024: FLOOR SUPPORT. CORRODED. E020510 LH CENTER FLOOR SILL HAS CORROSION AT FRAME 38. RAR L/H CENTER FLOOR SILL IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024022700146](https://openairdocs.org/sdr/HNAA2024022700146), Feb 4, 2024: FLOOR SUPPORT. CORRODED. E020508 LH CENTER FLOOR SILL HAS CORROSION AT FRAME 40. RAR LH CENTER FLOOR SILL AT FRAME 40 IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024022700136](https://openairdocs.org/sdr/HNAA2024022700136), Feb 4, 2024: SUPPORT PLATE. DAMAGED. E020609 PILOT SIDE AFT BULKHEAD OTBD GUIDE PIN HOLE SUPPORT PLATE ELONGATED. FABRICATED, DRILLED UP REPAIR DOUBLER AND SACRIFICIAL PLATE TO FIT AND INSTALLED PI
- [SDR HNAA2024022700135](https://openairdocs.org/sdr/HNAA2024022700135), Feb 4, 2024: DOOR SILL. CORRODED. E020578 SERVICE DOOR CENTER SILL CORRODED AROUND NUT PLATE HOLES. BLENDED OUT CORROSION ON SERVICE DOOR CENTER SILL AROUND NUTPLATE HOLES, FOUND THE AFT NUPLATE
- [SDR HNAA2024022700134](https://openairdocs.org/sdr/HNAA2024022700134), Feb 4, 2024: FLOOR SUPPORT. CORRODED. E020497 LH OMEGA BEAM HAS CORROSION BETWEEN FRAMES 45-50. PERFORMED REAPIRS TO LH OMEGA BEAM HAS CORROSION BETWEEN FRAMES 45-50 IAW ETD2024-145-003653 AND EO1-5
- [SDR HNAA2024022700154](https://openairdocs.org/sdr/HNAA2024022700154), Feb 3, 2024: MOUNT. CORRODED. E020403 RH LOWER APU COWLING MOUNT FITTING IS CORRODED, INSIDE 312AR AT FWD SIDE OF FIREWALL. REMOVED AND REPLACED RH LOWER APU COWLING MOUNT FITTING IN IAW EMB
- [SDR HNAA2024022700153](https://openairdocs.org/sdr/HNAA2024022700153), Feb 2, 2024: FLOOR SUPPORT. CORRODED. E020342 CARGO RH FLOOR BOARD SUPPORT BETWEEN FR 71 / 73 CORRODED. RAR CARGO RH FLOOR BOARD SUPPORT BETWEEN FR 71 / 73 IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024022700145](https://openairdocs.org/sdr/HNAA2024022700145), Feb 2, 2024: FRAME. GOUGED. E020365 Z FRAME NUT PLATE HOLES GOUGED AT FR 65 BETWEEN STRGS 16L-11L. REMOVED AND REPLACED Z FRAME AT FR65 IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024022700144](https://openairdocs.org/sdr/HNAA2024022700144), Feb 2, 2024: DOOR SILL. CORRODED. E020332 CARGO DOOR CUT-OUT CENTER SILL CORRODED IN NUMEROUS AREAS REMOVED AND REPLACED WITH SERVICEABLE CARGO DOOR CUT-OUT CENTER SILL IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024022700143](https://openairdocs.org/sdr/HNAA2024022700143), Feb 1, 2024: FRAME. GOUGED. E020167 BAGGAGE DOOR AFT LATERAL FRAME IS GOUGE AROUND NUTPLATE HOLE. PERFORMED CUTOUT ON BAGGAGE DOOR AFT LATERAL FRAME TO REMOVE DAMAGE, FABRICATED AND INSTAL
- [SDR HNAA2024022700142](https://openairdocs.org/sdr/HNAA2024022700142), Feb 1, 2024: WEB. CRACKED. E020163 BAGGAGE DOOR INTERNAL LWR WEB HAS A HOLE AT HB4 BETWEEN VB3 AND VB4. REMOVED DAMAGED & REPLACED WITH NEW & SERVICEABLE BAGGAGE DOOR INTERNAL LWR WEB (SK
- [SDR SIMA20230417003](https://openairdocs.org/sdr/SIMA20230417003), Apr 17, 2023: UNKNOWN. UNKNOWN. SERVICE DOOR EMERGENCY LT INOP-C/A-RAR SERVICE DOOR EMERGENCY LT IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. END.
- [SDR SIMA20230318001](https://openairdocs.org/sdr/SIMA20230318001), Mar 18, 2023: LAMP. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR ERMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD. END.
- [SDR SIMA2023013029001](https://openairdocs.org/sdr/SIMA2023013029001), Jan 29, 2023: LAMP. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOP. R & R SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECK GOOD. END.
- [SDR SIMA20230120003](https://openairdocs.org/sdr/SIMA20230120003), Jan 20, 2023: LAMP. INOPERATIVE. AFT AISLE CEILING EMERGENCY LIGHT INOPERATIVE. -R & R AFT AISLE CEILING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD.

All 190: https://openairdocs.org/aircraft/N923AE/reports.md

## STCs that may be installed (OpenAirDocs) (75, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Embraer EMB-145LR)

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST02176AT-D](https://openairdocs.org/stc/ST02176AT-D): Installation of a Teledyne Mini Flight Data Acquistion Unit. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST02216AT-D](https://openairdocs.org/stc/ST02216AT-D): Installation of Teledyne Mini Flight Data Acquisition Unit in a Provisioned EMB-135/145. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST02310AT](https://openairdocs.org/stc/ST02310AT): Installation of SAF-T-GLO photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST01409LA](https://openairdocs.org/stc/ST01409LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC ST01984LA-D](https://openairdocs.org/stc/ST01984LA-D): Modification and installation of passenger seats, passenger service units and filler panels, seat track covers, and seat row placards. Safran Cabin Inc
- [STC ST04219NY](https://openairdocs.org/stc/ST04219NY): Installation of SpaceX Starlink Aviation System. Aerospace Design & Compliance LLC
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST00640DE](https://openairdocs.org/stc/ST00640DE): Installation of Tropospheric Airborne Meteorolocigal Data Reporting System (TAMDAR). FLYHT Inc
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC ST04527CH](https://openairdocs.org/stc/ST04527CH): Installation of a 16 passenger configuration. C&L STC Holdings LLC
- [STC ST04177NY](https://openairdocs.org/stc/ST04177NY): Installation of ALI LED Cabin Lighting, Cabin and Crew AC Power Outlets, LH Fwd Closet and Misc Cabin Mods. C & L STC Holdings LLC
- [STC ST01983WI](https://openairdocs.org/stc/ST01983WI): Installation of a folding stair in the main entrance for models equipped with a side-hinged main door. Worldwide Aviation Engineering LLC
- [STC ST04212NY](https://openairdocs.org/stc/ST04212NY): Installation of Universal UNS-1Lw Flight Management System. C&L Engineering Services, LLC
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST04213NY](https://openairdocs.org/stc/ST04213NY): PAX Social Distance Floorplan Reconfiguration. C&L Engineering Services LLC
- [STC ST04281AT](https://openairdocs.org/stc/ST04281AT): Installation for the Upgrade of the NZ-2000 FMS computer for software version NZ6. Chippewa Aerospace Inc
- [STC ST03158CH-D](https://openairdocs.org/stc/ST03158CH-D): Installation of a Reconfiguration of a Cabin Floorplan. Standard Aero Business Aviation Services LLC
- [STC SA9087SC-D](https://openairdocs.org/stc/SA9087SC-D): RECORE® Hamilton Sundstrand heat exchanger, P/N 816630-1 / -2 in accordance with Honeywell LORI Sealed Drawing List SDL3869-1 Rev. A, dated June 7, 2005 or later FAA approved revision. Honeywell International Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST01039DE](https://openairdocs.org/stc/ST01039DE): Passenger seating arrangement for 30 or less passengers. Deluxe Public Charter LLC
- [STC ST04537NY](https://openairdocs.org/stc/ST04537NY): Installation of Air Filtration. Kilroy Aviation LLC
- [STC ST09858SC](https://openairdocs.org/stc/ST09858SC): Installation of cabin automatic coffee brewing system. Safran Cabin Germany Gmbh
- [STC ST04255CH](https://openairdocs.org/stc/ST04255CH): Installation of an Automatic Dependent Surveillance-Broadcast (ADS-B Out) System. ENVOY AIR
- [STC ST03420NY](https://openairdocs.org/stc/ST03420NY): Installation of a Cabin Interior. Delta Engineering Corporation
- [STC ST02327LA](https://openairdocs.org/stc/ST02327LA): Installation of replacement proximity sensor harness assembly part numbers used on the nose and main landing gears. Safran Electrical Components USA Inc
- [STC ST04423NY](https://openairdocs.org/stc/ST04423NY): Installation of ADS-B Out. FTI Engineering Nework GmbH
- [STC ST00015IB](https://openairdocs.org/stc/ST00015IB): Installation of a Honeywell HF Communication System, model KHF 1050, with provisions for a dual installation. Embraer Engineering & Technology Center - USA Inc
- [STC ST00014IB](https://openairdocs.org/stc/ST00014IB): Installation of a second Honeywell HF Communication System, model KHF 1050. Embraer Engineering & Technology Center - USA Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST04333NY](https://openairdocs.org/stc/ST04333NY): Installation of sat: Tglo® Photolumincsccnt Aisle Path Marking System. STG Aerospace Ltd
- [STC ST10550SC](https://openairdocs.org/stc/ST10550SC): Installation of a WeatherMASTER X-Band Fuselage Nose Radome Assembly. The NORDAM Group LLC
- [STC ST04316CH](https://openairdocs.org/stc/ST04316CH): Installation of a Smartsky System in accordance with StandardAero Master Data List 1034570, Revision (C), dated March 23, 2019 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST000081B](https://openairdocs.org/stc/ST000081B): Installation of a second SELCAL channel. EMBRAER - Empresa Brasileira de Aeronautica
- [STC ST00008IB](https://openairdocs.org/stc/ST00008IB): Installation of a second SELCAL channel. EMBRAER - Empresa Brasileira de Aeronautica
- [STC ST03177NY](https://openairdocs.org/stc/ST03177NY): Installation of a Honeywell ADS-B (Out), EHS and FreeFlight GPS. Delta Engineering Corporation
- [STC ST01520WI](https://openairdocs.org/stc/ST01520WI): Installation of the Concorde RG-442 VRSLA Battery and Temperature Sensor in place of the original Nickel-Cadmium Battery. Concorde Battery Corporation
- [STC ST00361BO](https://openairdocs.org/stc/ST00361BO): Installation of a Honeywell Primus II (XS-852) ADS-B Out System. Pro Star Aviation, LLC
- [STC ST04282CH](https://openairdocs.org/stc/ST04282CH): Installation of Honeywell CD-830 Control Display Unit (CDU). Nextant Aerospace
- [STC ST01702WI](https://openairdocs.org/stc/ST01702WI): Change seating configuration to 30 passengers by removal of seats. Worldwide Aircraft Engineering LLC
- [STC ST04108CH](https://openairdocs.org/stc/ST04108CH): Installation of Gogo Business Aviation ATG-8000 High Speed Internet with Wireless Local Area Network (WLAN). Nextant Aerospace
- [STC ST04367AT](https://openairdocs.org/stc/ST04367AT): Removal of the Existing Honeywell DL-900 or DL-950 Data Loader and Installation of the Honeywell DL-1000 Data Loader. Chippewa Aerospace Inc
- [STC ST04190AT](https://openairdocs.org/stc/ST04190AT): Installation of an ADS-B Out. Chippewa Aerospace Inc
- [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC

All 75: https://openairdocs.org/aircraft/N923AE/stcs.md

## Related

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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.