# N928AE: 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: 14500911
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 19, 2005
- Certificate issued: September 29, 2011
- Expires: September 30, 2027
- Mode S code: ACDBE7
- 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=928AE
- Page: https://openairdocs.org/aircraft/N928AE

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/N928AE/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 N928AE.

## FAA accident and incident reports

None matched to N928AE.

## Service difficulty reports (162, 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 HNAA2026082600789](https://openairdocs.org/sdr/HNAA2026082600789), Aug 25, 2026: UNKNOWN. ODOR. FLIGHT ATTENDANT REPORTED STRONG EXHAUST ODOR AFTER LANDING. INSPECTED PACK 2 AREA. NO DEFECTS NOTED. RAN PACKS 1 AND 2 OFF APU BLEED. NO ODOR PRESENT IN CABIN.
- [SDR HNAA2026071300595](https://openairdocs.org/sdr/HNAA2026071300595), Jul 13, 2026: A/C PACK. ODOR. UPON ARRIVING TO A/C OIL FUME SMELL NOTED IN FLIGHT DECK AND CABIN ON APU BLEED WITH BOTH PACKS RUNNING. RAN PACKS IAW AMM 21-51-00 DETERMINED OZONE/HUMIDITY SM
- [SDR HNAA2026071400595](https://openairdocs.org/sdr/HNAA2026071400595), Jul 13, 2026: A/C PACK. ODOR. UPON ARRIVING TO ACFT OIL FUME ODOR NOTED IN FLIGHT DECK AND CABIN ON APU BLEED WITH BOTH PACKS RUNNING. RAN PACKS IAW AMM 21-51-00 DETERMINED OZONE/HUMIDITY SM
- [SDR HNAA2026041500285](https://openairdocs.org/sdr/HNAA2026041500285), Apr 15, 2026: APU. ODOR. STRONG ODOR IN COCKPIT, NO REPORT FROM PREVIOUS CREW. NEW CREW REPORTED CHEMICAL ODOR WHEN ARRIVING TO THE A/C 1M MIN LATER. PLACED APU ON MEL 49-1.
- [SDR HNAA2026022400152](https://openairdocs.org/sdr/HNAA2026022400152), Feb 22, 2026: PRESSURE SWITCH. FAULTED. HS VLV 2 FAIL ON TAKEOFF ROLL. REJECTED TAKEOFF AT 50 TO 60 KNOTS. FACT 23FEB26 12:10 PHF R & R HIGH STAGE PRESSURE SWITCH IRT AMM TASK 36-11-07-000/400-801-A. 
- [SDR HNAA2025102200722](https://openairdocs.org/sdr/HNAA2025102200722), Oct 21, 2025: BATTERY. INOPERATIVE. CIELING AT ROW 5 AND MAIN DOOR, ALONG WITH MAIN DOOR EMERGENCY LIGHTS INOP. R & R BATTERY NR 1 IAW AMM 33-50-04.
- [SDR HNAA2025081800571](https://openairdocs.org/sdr/HNAA2025081800571), Aug 16, 2025: ACM. ODOR. BRIEFSMOKE/ODOR IN THE COCKPIT IN FLIGHT. F.A. REPORTED A "POP" NOISE NEAR ROW 12. AIR CONDITIONING PACKS. R&R LT ACM EXUAST DUCT ASSY AND GRATE ASSY IRW EMB AM
- [SDR HNAA2025022400092](https://openairdocs.org/sdr/HNAA2025022400092), Feb 23, 2025: OIL SYSTEM. LOW. FAINT OIL LIKE ODOR IN FLIGHT DECK WHILE ON ENGINE BLEEDS DURING DESECENT LAST APPROX 30SECS FACT 23FEB25 13:56 PHL E1 1QT LOW. SERVICED E1 WITH 1QT AS REQUIRED
- [SDR HNAA2025021000081](https://openairdocs.org/sdr/HNAA2025021000081), Feb 9, 2025: NONE. NONE. BIRD STRIKE ON LEFT SIDE AIRCRAFT ON TAKE OFF ROLL FACT 09FEB25 04:13 ROA CLEANED AND INSPECTED IAW AMM 05-50-08 NO DEFECTS NOTED
- [SDR HNAA2024080900656](https://openairdocs.org/sdr/HNAA2024080900656), Jul 21, 2024: CHANNEL. CORRODED. E046877 FOUND CORROSION ON CENTER HAT BEAM AROUND NUT PLATE HOLE AT FR59. CUT OUT DAMAGE, INSTALLED DOUBLER AND FILLER FOR REPAIR OF LAV CENTER HAT BEAM AT NUT-
- [SDR HNAA2024080900655](https://openairdocs.org/sdr/HNAA2024080900655), Jul 19, 2024: DRAG BRACE. CORRODED. E046631 NLG DRAG BRACE LH BEARING CAP IS CORRODED. RAR NLG DRAG BRACE LH BEARING CAP IAW EMB 145 AMM 32-20-02
- [SDR HNAA2024080900654](https://openairdocs.org/sdr/HNAA2024080900654), Jul 18, 2024: DOOR SILL. CORRODED. E046499 SERVICE DOOR CENTER SILL CORRODED AROUND NUT PLATE HOLES. BLENDED OUT CORROSION ON SERVICE DOOR CUTOUT CENTER SILL AROUND 3 NUT PLATE HOLES IAW EMB145 S
- [SDR HNAA2024080900653](https://openairdocs.org/sdr/HNAA2024080900653), Jul 18, 2024: FLOOR SUPPORT. CORRODED. E046457 LH #1 FLOOR SILL CORRODED. RAR LH #1 FLOOR SILL IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024080900652](https://openairdocs.org/sdr/HNAA2024080900652), Jul 18, 2024: FLOOR SUPPORT. CORRODED. E046425 PAX DOOR CUT-OUT AFT FLOOR BOARD SUPPORT CORRODED AROUND NUTT PLATES. RAR PAX DOOR CUT-OUT AFT FLOOR BOARD SUPPORT IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024080900651](https://openairdocs.org/sdr/HNAA2024080900651), Jul 18, 2024: FLOOR SUPPORT. CORRODED. E046388 RH #1 OMEGA BEAM FLOOR SUPPORT CORRODED IN MULTIPLE AREAS. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE R/H #1 OMEGA BEAM SUPPORT IAW EMB 145 SRM 51-
- [SDR HNAA2024080900650](https://openairdocs.org/sdr/HNAA2024080900650), Jul 18, 2024: FLOOR SUPPORT. CORRODED. E046384 RH #1 FLOOR SILL HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED RH #1 FLOOR SILL IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024080900649](https://openairdocs.org/sdr/HNAA2024080900649), Jul 18, 2024: FLOOR SUPPORT. CORRODED. RH #2 FLOOR SILL HAS CORROSION IN MULTIPLE AREAS. RAR R/H # 2 FLOOR SILL IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024080900648](https://openairdocs.org/sdr/HNAA2024080900648), Jul 18, 2024: FLOOR SUPPORT. CORRODED. LH #3 OMEGA BEAM FLOOR SUPPORT CORRODED IN MULTIPLE AREAS. REMOVED AND REPLACED LH #3 OMEGA BEAM FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024080900647](https://openairdocs.org/sdr/HNAA2024080900647), Jul 18, 2024: FLOOR SUPPORT. CORRODED. LH #2 FLOOR SILL HAS CORROSION IN MULTIPLE AREAS BETWEEN FRAMES 24 TO 35. REMOVED AND REPLACED LH #2 FLOOR SILL IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024080900646](https://openairdocs.org/sdr/HNAA2024080900646), Jul 16, 2024: GUSSET. CORRODED. LAV CENTER FLOOR GUSSET CORRODED AROUND NUT PLATE HOLES. REMOVED AND REPLACED LAV CENTER FLOOR GUSSET IAW EMB145 SRM 51-40-02.
- [SDR HNAA2024080900645](https://openairdocs.org/sdr/HNAA2024080900645), Jul 16, 2024: GUSSET. CORRODED. LAV LH CENTER FLOOR GUSSET CORRODED AROUND NUT PLATE HOLES. REMOVED AND REPLACED LAV L/H CENTER FLOOR GUSSET IAW EMB145 SRM 51-40-02.
- [SDR HNAA2024080900644](https://openairdocs.org/sdr/HNAA2024080900644), Jul 16, 2024: FLOOR SUPPORT. CORRODED. LAV LH FLOOR SUPPORT CORRODED BETWEEN FR 59/60. BLENDED TO REMOVE CORROSION ON LAV L/H FLOOR SUPPORT BETWEEN FR59/-60 IAW EMB145 SRM 51-10-03.
- [SDR HNAA2024080900661](https://openairdocs.org/sdr/HNAA2024080900661), Jul 15, 2024: BEAM. CRACKED. E045789 L/H EMERGENCY EXIT DOOR BEAM #3 HAS A POSSIBLE CRACK. PERFORMED DOUBLER REPAIR ON L/H EMERGENCY EXIT DOOR BEAM #3 CRACK IAW ETD2024-145-020373 AND EO1-5
- [SDR HNAA2024080900660](https://openairdocs.org/sdr/HNAA2024080900660), Jul 15, 2024: DOOR FRAME. CHAFED. E045844 PAX DOOR AFT FRAME IS CHAFED AROUND NUT-PLATES HOLES. BLENDED TOTAL OF 7 CHAFED AREAS AROUND PAX DOOR AFT FRAME NUT-PLATE HOLES IAW EMB 145 SRM 51-10-03
- [SDR HNAA2024080900659](https://openairdocs.org/sdr/HNAA2024080900659), Jul 15, 2024: WEB. CHAFED. E045806 CARGO DOOR INTERNAL WEB IS CHAFED IN MULTIPLE AREAS. FURTHER INVESTIGATION OF CARGO DOOR INTERNAL WEB CHAFES IN MULTIPLE AREAS SHOWS TO BE TOTAL OF 2 CH
- [SDR HNAA2024080900658](https://openairdocs.org/sdr/HNAA2024080900658), Jul 15, 2024: DOUBLER. CORRODED. E045597 FUSELAGE SKIN INTERNAL DOUBLER BETWEEN FRAME 60 AND FRAME 61 AND STRINGERS 19L AND 20L HAS CORROSION. REMOVED UNSERVICEABLE INTERNAL FUSELAGE SKIN DOUBL
- [SDR HNAA2024080900643](https://openairdocs.org/sdr/HNAA2024080900643), Jul 15, 2024: ANGLE. CORRODED. PAX DOOR LWR AFT PROFILE HAS CORROSION AROUND NUT-PLATES HOLES. REMOVED PAX DOOR LWR AFT PROFILE WITH CORROSION AROUND NUT-PLATES HOLES, INSTALLED SERVICEABLE P
- [SDR HNAA2024080900642](https://openairdocs.org/sdr/HNAA2024080900642), Jul 15, 2024: ANGLE. CORRODED. PAX DOOR LWR FWD PROFILE HAS CORROSION AROUND NUT-PLATES HOLES. REMOVED PAX DOOR LWR FWD PROFILE THAT IS CORRODED AROUND NUT-PLATES HOLES, PREPPED AND INSTALLED
- [SDR HNAA2024080900641](https://openairdocs.org/sdr/HNAA2024080900641), Jul 15, 2024: ANGLE. CORRODED. CARGO DOOR INTERNAL LWR FRAME L SHAPE ANGLE HAS CORROSION AROUND NUTPLATES HOLES. REMOVED AND REPLACED CARGO DOOR INTERNAL LWR FRAME L SHAPE ANGLE (L-PROFILE) I
- [SDR HNAA2024080900640](https://openairdocs.org/sdr/HNAA2024080900640), Jul 15, 2024: DOOR SILL. CORRODED. CARGO DOOR CUTOUT LOWER SILL HAS CORROSION. REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024080900657](https://openairdocs.org/sdr/HNAA2024080900657), Jul 12, 2024: DOUBLER. CORRODED. E044964 CENTER FUSELAGE 4, THE POTABLE WATER SERVICING PORT DOUBLER HAS CORROSION. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE CENTER FUSELAGE 4, THE POTABL
- [SDR SIMA20230220002](https://openairdocs.org/sdr/SIMA20230220002), Feb 20, 2023: LAMP. INOPERATIVE. MAIN DOOR EXT EMERGENCY DOOR LIGHT INOP-C/A-RAR MAIN DOOR EXT EMERGENCY DOOR LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECK GOOD. E
- [SDR SIMA202301154001](https://openairdocs.org/sdr/SIMA202301154001), Jan 14, 2023: LAMP. INOPERATIVE. DURING PS-1 CHECK FOUND INTERIOR EMERGENCY EXIT CEILING LIGHT INOP-C/A-REPLACED LAMP IAW 33-50-08. OPC GOOD.
- [SDR SIMA20221120001](https://openairdocs.org/sdr/SIMA20221120001), Nov 20, 2022: LAMP. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD
- [SDR SIMA20221024002](https://openairdocs.org/sdr/SIMA20221024002), Oct 24, 2022: NONE. NONE. AFT CARGO DOOR FRAME 65 GUSSET IS CORRODED.(LEVEL 2 CORROSION) (MAJOR REPAIR)-C/A-FRAME 65 REPAIRED IAW ERS-EM-53MR-4660.
- [SDR SIMA20220722001](https://openairdocs.org/sdr/SIMA20220722001), Jul 22, 2022: FLASHLIGHT ASSY. BROKEN. FA EMERGENCY FLASHLIGHT BRACKET IS BROKEN-C/A-ACCOMPLISHED REPLACEMENT OF FA EMERGENCY FLASHLIGHT BRACKET CLAMP IAW EMB 145 CMM TASK 25-60-14. OPC GOOD NO DEFEC
- [SDR SIMA20220721002](https://openairdocs.org/sdr/SIMA20220721002), Jul 21, 2022: ACM. FUMES. STRONG SMELL OF FUEL FUMES ON DECENT STARTING AT FL250 THROUGH 14000 FT FOLLOWED BY BURNING SMELL TILL 5000FT-C/A-C/W ETN-72-034R10 NO DEFECTS NOTED. C/W TECH S
- [SDR SIMA20220618001](https://openairdocs.org/sdr/SIMA20220618001), Jun 18, 2022: INVERTER. INOPERATIVE. FWD EMERGENCY EXIT PLACARD INOP-C/A-T/S IAW W/M 33-50-50 FOUND INVERTER 1 AT FAULT. RAR INVERTER 1 IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A OPS CHE
- [SDR SIMA20220529002](https://openairdocs.org/sdr/SIMA20220529002), May 29, 2022: LAMP. INOPERATIVE. MAIN DOOR EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPC GOOD. END.
- [SDR SIMA20220325004](https://openairdocs.org/sdr/SIMA20220325004), Mar 25, 2022: NONE. NONE. AISLE EMERGENCY LIGHT AT 16CB INOP-C/A-RAR AISLE EMERGENCY LIGHT LAMP OPC GOOD IAW AMM 33-50-08
- [SDR SIMA202108221001](https://openairdocs.org/sdr/SIMA202108221001), Aug 21, 2021: CRADLE. BROKEN. AFT FLASHLIGHT CRADLE BROKEN-C/A-RAR AFT FLASHLIGHT CRADE IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPC GOOD. END.
- [SDR SIMA202108176001](https://openairdocs.org/sdr/SIMA202108176001), Aug 16, 2021: CRADLE. BROKEN. AFT FA EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-FLIGHT CREW PLACARDED AFT FA EMERGENCY FLASHLIGHT HOLDER. M PROCEDURES C/W. MEL AUTH# 080225M-C REF# 25-32 MOC# 62
- [SDR SIMA202108065001](https://openairdocs.org/sdr/SIMA202108065001), Aug 5, 2021: CONNECTOR. DIRTY. MAIN PAX DOOR EMERGENCY EXIT SIGN INOP-C/A-CLEANED MAIN PAX DOOR EMERGENCY EXIT SIGN ELECTRICAL CONNECTORS IAW SWPM 20-50-00 OPS CHECK GOOD
- [SDR SIMA20210519001](https://openairdocs.org/sdr/SIMA20210519001), May 19, 2021: LIGHT. DIM. MEL 33-23 AUTH # 050266-C "FLOOR EMERGENCY LIGHTING STRIP #6 AND STRIP #8 DIM" REF AML PAGE 4761264 ITEM 1.-C/A-RAR FLOOR PROXIMITY STRIP LIGHTS #6 AND #8 REF A
- [SDR SIMA20210518001](https://openairdocs.org/sdr/SIMA20210518001), May 18, 2021: LIGHT. DIM. FLOOR EMERGENCY LIGHTING STRIP #6 AND STRIP #8 DIM-C/A- "TRANSFERRED TO AML PAGE 4761264 ITEM 1"
- [SDR SIMA20210517003](https://openairdocs.org/sdr/SIMA20210517003), May 17, 2021: O-RING. LEAKING. BLEED 1 LEAK CLIMBING THROUGH 8000. PERFOMED ARH STILL INDICATED LEAK. LOSS OF CABIN PRSSURE EMERGENCY DECLARED.SWAP A/C CONT -C/A-T/S IAW FIM 36-20-00-810-801-
- [SDR SIMA20210301004](https://openairdocs.org/sdr/SIMA20210301004), Mar 1, 2021: FITTING. GOUGED. R/H AILERON DAMPER FITTING IS GOUGED ON THE AILERON.-C/A-COMPLETE RAR R/H AILERON DAMPER FITTING IAW ENVOY EO EM-27MR-112.
- [SDR SIMA20210217001](https://openairdocs.org/sdr/SIMA20210217001), Feb 17, 2021: HINGE. EXCESS PLAY. VERTICAL STABILIZER UPPER RUDDER ATTACH POINT FITTING HAS PLAY. C/A-REPLACE VERTICAL STAB UPPER RUDDER HINGE ASSY IAW EMB145 SRM 51-40-02.
- [SDR SIMA20210217002](https://openairdocs.org/sdr/SIMA20210217002), Feb 17, 2021: BUSHING. MIGRATED. RIGHT AILERON PCU ATTACH FITTING HAS MIGRATING BUSHINGS ON THE INBD AND OUTBD LUG. C/A-R & R RT AILERON PCU ATTACH FITTING IAW EO-EM-27MR-112.
- [SDR SIMA20210217003](https://openairdocs.org/sdr/SIMA20210217003), Feb 17, 2021: BUSHING. MIGRATED. LEFT AILERON PCU ATTACH FITTING HAS MIGRATING BUSHINGS ON THE INBD AND OUTBD LUG. C/A-R & R LT AILERON PCA FITTING IAW EO-EM-27MR-112.

All 162: https://openairdocs.org/aircraft/N928AE/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/N928AE/stcs.md

## Earlier aircraft with N928AE

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N928AE before.

- [Cancelled 1999-09-22](https://openairdocs.org/deregistered/N928AE-1999-09-22): British Aerospace BAE JETSTREAM 3201, S/N 928. Exported to Argentina. Owner: [First Security Bank Na Trustee](https://openairdocs.org/faa-owner/FIRST%20SECURITY%20BANK%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)

## 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.