# N931AE: 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: 14500912
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 21, 2005
- Certificate issued: September 21, 2011
- Expires: September 30, 2027
- Mode S code: ACE965
- 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=931AE
- Page: https://openairdocs.org/aircraft/N931AE

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/N931AE/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 (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 CEN11LA250](https://openairdocs.org/ntsb/CEN11LA250), Mar 26, 2011: Embraer EMB-145LR (N931AE), Kansas City, MO, no damage. Probable cause: An in-flight encounter with convectively induced turbulence associated with developing thunderstorms under the flight path during the airplane's climb to cruise flight.

## FAA accident and incident reports (1)

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

- [Accident 20110326005879A](https://openairdocs.org/incident/20110326005879A), Mar 26, 2011: Embraer EMB-145LR (N931AE), Mcpherson, KS, No damage. During climb, at approximately 32,000 feet MSL, in clear air, the aircraft hit a very small bump (light chop). It lasted a second or less. Later, the flight…

## Service difficulty reports (145, 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 HNAA2026072400604](https://openairdocs.org/sdr/HNAA2026072400604), Jul 18, 2026: FLOOR SUPPORT. CORRODED. RT OTBD FLOOR SILL AT FR 22 HAS CORROSION. REMOVED AND REPLACED WITH NEW RT OTBD FLOOR SILL AT FR 22 IAW EMB 145 SRM 51-40-02-PR
- [SDR HNAA2026072400631](https://openairdocs.org/sdr/HNAA2026072400631), Jul 14, 2026: RIB. CRACKED. RT WING, RIB 21 OB OF AILERON PCU HAS A CRACK ON UPPER FLANGE. REPAIRED RT WING RIB 21 OB OF AILERON PCU UPPER FLANGE CRACK WITH A FILLER AND DOUBLER IAW SRM 57
- [SDR HNAA2026072400630](https://openairdocs.org/sdr/HNAA2026072400630), Jul 14, 2026: RIB. CRACKED. LEFT WING, RIB 21 OB OF AILERON PCU HAS A CRACK ON UPPER FLANGE. REPAIRED LT WING RIB 21 OB AILERON PCU CRACK USING FILLER AND DOUBLER ON UPPER FLANGE IAW SRM 5
- [SDR HNAA2026072400629](https://openairdocs.org/sdr/HNAA2026072400629), Jun 24, 2026: FLOOR SUPPORT. CRACKED. FR 59 TO FR 61 LH OMEGA BEAM HAS CORROSION. COMPLIED WITH PERMANENT REPAIR OF THE L/H OMEGA BEAM BETWEEN FRAME 59 - 60 SPLICE PER EMB 145 ETD2026-145-011104 REV
- [SDR HNAA2026072400628](https://openairdocs.org/sdr/HNAA2026072400628), Jun 22, 2026: RIB. CRACKED. RIB ON RH ELEVATOR AT STA YH= 1340 HAS A CRACK. REMOVED AND REPLACED WITH NEW 1EA RIB ON RH ELEVATOR AT STA YH=1340 IAW EMB 145 SRM 51-40-02-PR.
- [SDR HNAA2026072400627](https://openairdocs.org/sdr/HNAA2026072400627), Jun 21, 2026: RIB. DAMAGED. 00361 LH INBD FLAP HAS AN ELONGATED SCREW HOLE AS MARKED. COMPLIED WITH PERMANENT REPAIR OF THE L/H IB FLAP FAIRING ATTACH RIB PER EMB 145 ETD2026-145-010947 RE
- [SDR HNAA2026072400621](https://openairdocs.org/sdr/HNAA2026072400621), Jun 20, 2026: FLOOR SUPPORT. CORRODED. RIGHT OTBD FLOOR SILL FROM FR 30 TO FR 35 HAS CORROSION. REMOVED AND REPLACED RT OTBD FLOOR SILL FROM FR 30 - FR 35 PER EMB 145 SRM 51-40-02-PR.
- [SDR HNAA2026072400620](https://openairdocs.org/sdr/HNAA2026072400620), Jun 20, 2026: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM GUSSET AT FR 35 HAS CORROSION. REMOVED AND REPLACED LT OMEGA BEAM GUSSET FROM FR 30 TO FR 35 PER SRM 51-40-02 STEP 2C
- [SDR HNAA2026072400619](https://openairdocs.org/sdr/HNAA2026072400619), Jun 20, 2026: FLOOR SUPPORT. CORRODED. LEFT OTBD FLOOR SILL FROM FR 30 TO FR 35 HAS CORROSION. REMOVED AND INSTALLED NEW FROM STOCK LT OTBD FLOOR SILL FROM FR 30 TO FR 35 PER SRM 51-40-02
- [SDR HNAA2026072400618](https://openairdocs.org/sdr/HNAA2026072400618), Jun 19, 2026: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM GUSSET FROM FR 36 TO FR 41 HAS CORROSION. REMOVED AND REPLACED 1EA LT OMEGA BEAM GUSSET LOCATED BETWEEN FR 36 - FR 41 PER EMB 145 SRM 51-40-02-P
- [SDR HNAA2026072400617](https://openairdocs.org/sdr/HNAA2026072400617), Jun 19, 2026: FLOOR SUPPORT. CORRODED. LEFT OTBD FLOOR SILL FROM FR 36 TO FR 41 HAS CORROSION. COMPLIED WITH PERMANENT REINFORCING REPAIR OF THE LT OTBD FLOOR SILL FROM FR36 - FR41 PER EMB 145 ETD202
- [SDR HNAA2026072400616](https://openairdocs.org/sdr/HNAA2026072400616), Jun 19, 2026: FLOOR SUPPORT. CORRODED. RIGHT OTBD FLOOR SILL FROM FR 36 TO FR 41 HAS CORROSION. REMOVED AND REPLACED WITH NEW RT OTBD FLOOR SILL FROM FR 36 TO FR 41 IAW EMB 145 SRM 51-40-02-PR.
- [SDR HNAA2026072400615](https://openairdocs.org/sdr/HNAA2026072400615), Jun 19, 2026: FLOOR SUPPORT. CORRODED. LEFT OTBD FLOOR SILL FROM FR 43 TO FR 46 HAS CORROSION. REMOVED AND REPLACED LT OTBD FLOOR SILL FROM FR 43 TO FR 46 IAW SRM 51-40-02-PR.
- [SDR HNAA2026072400614](https://openairdocs.org/sdr/HNAA2026072400614), Jun 19, 2026: FLOOR SUPPORT. NOT REPORTED. LEFT OTBD FLOOR SILL FROM FR 47 TO FR 51 HAS CORROSION. REMOVED AND REPLACED LT OTBD FLOOR SILL FROM FR 47 TO FR 51 IAW SRM 51-40-02-PR.
- [SDR HNAA2026072400613](https://openairdocs.org/sdr/HNAA2026072400613), Jun 19, 2026: FLOOR SUPPORT. CORRODED. LEFT OTBD FLOOR SILL FROM FR 53 TO FR 57 HAS CORROSION. REMOVED AND REPLACED WITH NEW LT OTBD FLOOR SILL FROM FR 53 TO FR 57 IAW SRM 51-40-02-PR.
- [SDR HNAA2026072400612](https://openairdocs.org/sdr/HNAA2026072400612), Jun 19, 2026: FLOOR SUPPORT. CORRODED. RIGHT OTBD FLOOR SILL FROM FR 53 TO FR 57 HAS CORROSION. REMOVED AND REPLACED WITH NEW RT OTBD FLOOR SILL FROM FR 53 TO FR 57 IAW EMB 145 SRM 51-40-02-PR.
- [SDR HNAA2026072400626](https://openairdocs.org/sdr/HNAA2026072400626), Jun 18, 2026: FLOOR SUPPORT. CRACKED. ONE LT OMEGA BEAM GUSSET AT FR 28 HAS A CRACK. REMOVED AND REPLACED LH OMEGA BEAM GUSSET AT FR 28 PER EMB 145 SRM 51-40-08-PR.
- [SDR HNAA2026072400625](https://openairdocs.org/sdr/HNAA2026072400625), Jun 18, 2026: ACCESS PANEL. CRACKED. APU COWLING ACCESS PANEL CRACKED ON THE INTERIOR SIDE NEAR THE HINGE. REMOVED AND REPLACED APU COWLING ACCESS PANEL PER EMB 145 SRM 51-20-03 STEP 3
- [SDR HNAA2026072400624](https://openairdocs.org/sdr/HNAA2026072400624), Jun 18, 2026: SUPPORT BRACKET. CRACKED. FWD CARGO DOOR MECHANISM SUPPORT BRACKET CRACKED ON BOTTOM LEG. REMOVED AND REPLACED WITH NEW FWD CARGO DOOR MECHANISM SUPPORT BRACKET IAW EMB 145 SRM 51-40-02-
- [SDR HNAA2026072400623](https://openairdocs.org/sdr/HNAA2026072400623), Jun 18, 2026: FLOOR SUPPORT. CRACKED. ONE LT OMEGA BEAM AT FR 23 HAS A CRACKED. COMPLIED WITH PERMANENT REINFORCING REPAIR OF THE LT OMEGA BEAM AT FRAME 23 SPLICE IAW ETD2026-145-010691 REV. AND PIE
- [SDR HNAA2026072400622](https://openairdocs.org/sdr/HNAA2026072400622), Jun 18, 2026: PANEL. CRACKED. PANEL 191ZB RT LEADING EDGE NR 1 STRAP ASSY ( HORSE COLLAR) IS CRACKED AT THE UPPER RADIUS BY FIRST FASTENER HOLE. COMPLIED WITH REPAIR TO THE RT WING-TO -FUSEL
- [SDR HNAA2026072400611](https://openairdocs.org/sdr/HNAA2026072400611), Jun 18, 2026: GUSSET. CORRODED. ONE LT FLOOR GUSSET AT FR 59 HAS CORROSION. REMOVED AND REPLACED LT FLOOR GUSSET FROM FR 59 TO FR 61 PER SRM 51-40-02, STEP 2 C, AND 3 B
- [SDR HNAA2026072400610](https://openairdocs.org/sdr/HNAA2026072400610), Jun 18, 2026: FLOOR SUPPORT. CORRODED. RIGHT OTBD FLOOR SILL FROM FR 25 TO FR 28 HAS CORROSION. REMOVED AND REPLACED RT OTBD FLOOR SILL FROM FR 23 - FR 29 PER EMB 145 SRM 51-40-02-PR
- [SDR HNAA2026072400609](https://openairdocs.org/sdr/HNAA2026072400609), Jun 18, 2026: FLOOR SUPPORT. CORRODED. LEFT OTBD FLOOR SILL FROM FR 24 TO FR 29 HAS CORROSION. REMOVED AND REPLACED THE LT OTBD FLOOR SILL FROM FR24 - FR29 PER EMB 145 SRM 51-40-02-PR.
- [SDR HNAA2026072400608](https://openairdocs.org/sdr/HNAA2026072400608), Jun 18, 2026: FLOOR SUPPORT. CORRODED. LEFT OTB FLOOR SILL FROM FR 20 TO FR 22 HAS CORROSION. REMOVED AND REPLACED WITH NEW LT OTBD FLOOR SILL FROM FR 20 TO FR 22 IAW EMB 145 SRM 51-40-02 STEP 2 B, C
- [SDR HNAA2026072400607](https://openairdocs.org/sdr/HNAA2026072400607), Jun 18, 2026: FLOORBEAM. CORRODED. LH FLOOR CROSSBEAM AT FR 18 HAS CORROSION. REMOVED AND REPLACED WITH NEW LH FLOOR CROSSBEAM AT FR 18 IAW EMB 145 SRM 51-40-02-PR.
- [SDR HNAA2026072400606](https://openairdocs.org/sdr/HNAA2026072400606), Jun 18, 2026: DOOR FRAME. CORRODED. SERVICE DOOR CUTOUT LOWER SURROUND STRUCTURE AT FR 21 HAS CORROSION. REMOVED AND REPLACED WITH NEW SERVICE DOOR CUTOUT LOWER SURROUND STRUCTURE AT FR 21 IAW EMB
- [SDR HNAA2026072400605](https://openairdocs.org/sdr/HNAA2026072400605), Jun 18, 2026: GUSSET. CORRODED. RIGHT FLOOR GUSSET AT FR 22 HAS CORROSION. REMOVED RH FLOOR GUSSET AT FR 22.AND INSTALLED NEW GUSSET AT FR 22 PER EMB 145 SRM 51-40-02-PR
- [SDR HNAA2026072400603](https://openairdocs.org/sdr/HNAA2026072400603), Jun 18, 2026: FLOOR SUPPORT. CORRODED. 00148 1EA RH OB FLOOR SILL AT FR 20 HAS CORROSION. REMOVED AND REPLACED WITH NEW RH OB FLOOR SILL AT FR 20 IAW EMB 145 SRM 51-40-02-PR.
- [SDR HNAA2026072400602](https://openairdocs.org/sdr/HNAA2026072400602), Jun 18, 2026: PAINT. FLAKING. PANEL 191HL HAS CORROSION UNDER PAINT AND PAINT IS FLAKING OFF. REMOVED CORROSION FOUND ON PANEL 191HL, LOWEST REMAINING THICKNESS FOUND TO BE AT .06995 PARTS F
- [SDR HNAA2026072400601](https://openairdocs.org/sdr/HNAA2026072400601), Jun 17, 2026: CUP. CORRODED. CORROSION AROUND THE WASTE DRAIN VALVE. REMOVED AND REPLACED WITH NEW WASTE DISCHARGE CUP ASSY PER EMB 145 SRM 51-40-02-PR STEP 4B.
- [SDR HNAA2026061600500](https://openairdocs.org/sdr/HNAA2026061600500), Jun 14, 2026: UNKNOWN. ODOR. IN FLT FUMES AND ODOR IN COCKPIT- BURNING ELEC SMELL. OPS CHECKED APU BOTH ENGINES, BOTH PACKS, BOTH WIPERS, WINDSHIELD HEAT. OPS CHECK GOOD. INSPECTED BOTH DIS
- [SDR HNAA2026032300229](https://openairdocs.org/sdr/HNAA2026032300229), Mar 22, 2026: PIPE. BROKEN. WITH E1 ON, ON TAXI OUT BURNING SMELL IN FLT DECK AND CABIN WITH EITHER PACK ON. INSPECTED PACK 1 AND PACK 2. FOUND BROKEN SECTION OF PIPE. SUSPECT BROKEN SECTI
- [SDR HNAA2025120300847](https://openairdocs.org/sdr/HNAA2025120300847), Dec 2, 2025: WARNING MESSAGE. FALSE ACTIVATION. BLEED 1 LEAK DISPLAYED IN FLIGHT. INSPECTED FOR BLEED 1 LEAK/ NO DEFECTS NOTED. OPS CHECKED IAW AMM 36-00-00. OPS CHECKED GOOD. COULD NOT DUPLICATE. AC OK FOR S
- [SDR HNAA2025092300638](https://openairdocs.org/sdr/HNAA2025092300638), Sep 22, 2025: BLEED VALVE. FAILED. BLEED 1 VALVE FAILED MESSAGE ON TO ROLL. R & R THE BLEED VALVE IAW AMM 36-11-05. OPS CHECKED GOOD IRT AMM 36-00-00-700-803-A. GROUND RAN AIRCRAFT. NO LEAKS NOTE
- [SDR HNAA2025031000145](https://openairdocs.org/sdr/HNAA2025031000145), Mar 8, 2025: BLEED VALVE. ACTIVATION ERROR. ON TAKEOFF ENGINE BLEED VALVE FAIL ON EICAS, GOING 20 KNOTS AND REFKECTED TAKEOFF. FACT 08MAR25 18:48 CLT REMOVED AND REPLACED ENGINE BLEED AIR VALVE IRW AMM 36
- [SDR HNAA2024060700488](https://openairdocs.org/sdr/HNAA2024060700488), Jun 6, 2024: COMPUTER. FAULTED. SPS 2 INOP DISPLAYED IN FLT FACT 06JUN24 20:04 PHL REMOVED AND REPLACED STALL PROTECT COMPUTER IAW AMM 27-36-02. PREFORMED OPS CHECK IAW AMM 27-36-00. OPS CHECK
- [SDR HNAA2024053000478](https://openairdocs.org/sdr/HNAA2024053000478), May 29, 2024: UNKNOWN. ODOR. BURNING SMELL DURING TAXI. CLEARED WITH PACK 1 SELECTED OFF FACT 29MAY24 19:10 CLT INSPECTED BOTH PACKS FOR DEFECTS. NONE NOTED AT THIS TIME. PERFORMED OPS CHEC
- [SDR HNAA2024042900328](https://openairdocs.org/sdr/HNAA2024042900328), Apr 16, 2024: BOOT. DAMAGED. IN CLIMB OUT SLOW TO RAPID DEPRESSURIZATION AT FL 290.BEGAN TO STABALIZE AT FL 230 IN AUTO MODE. FACT 16APR24 20:05 PHL INSPECTED PACK 1 AREA AND FOUND DAMAGED 
- [SDR HNAA2024040100245](https://openairdocs.org/sdr/HNAA2024040100245), Mar 15, 2024: FLOOR SUPPORT. CORRODED. 00210 LH Y-479 FLOOR BEAM CAP IS CORRODED BETWEEN FRM48 AND FRM50. REMOVED AND REPLACED LH Y-479 FLOOR BEAM CAP BETWEEN FRM46 AND FRM53 IAW EMB-145 SRM 51-40-02
- [SDR HNAA2024040100244](https://openairdocs.org/sdr/HNAA2024040100244), Mar 15, 2024: FLOORBEAM. CORRODED. 00207 LH Y-479 FLOOR BEAM CAP IS CORRODED BETWEEN X13200 AND X15125. INSTALLED NEW SERVICEABLE FLOOR BEAM CAP (GUSSET) PN: 145-30634-005 IAW EMB-145 SRM 51-40-0
- [SDR HNAA2024040100243](https://openairdocs.org/sdr/HNAA2024040100243), Mar 15, 2024: FLOOR SUPPORT. CORRODED. 00206 CENTER Y 0 FLOOR BEAM CAP IS CORRODED BETWEEN X11990 AND X13200. : INSTALLED NEW SERVICEABLE CENTER Y 0 FLOOR BEAM CAP BETWEEN X11990 AND 13200 IAW EMB145
- [SDR HNAA2024040100242](https://openairdocs.org/sdr/HNAA2024040100242), Mar 15, 2024: SEAT TRACK. CORRODED. 00203 CENTER Y 0 FLOOR SEAT TRACK IS CORRODED BETWEEN FRM37 AND FRM38. INSTALLED CENTER Y 0 FLOOR SEAT TRACK BETWEEN FRM36 TO FRM46 IAW EMB145 AMM 53-01-06-400-
- [SDR HNAA2024040100238](https://openairdocs.org/sdr/HNAA2024040100238), Mar 15, 2024: FLOORBEAM. CORRODED. 00178 RH FLOOR BEAM CAP AT FRM22 AND Y+479 IS CORRODED. REMOVED AND REPLACED WITH NEW RH FLOOR BEAM CAP (P/N: 145-22461-011) IAW EMB145LR SRM 51-40-02
- [SDR HNAA2024240100240](https://openairdocs.org/sdr/HNAA2024240100240), Mar 14, 2024: STRAP. CORRODED. LH FLOOR SUPPORT SRTRAP AT X7578 BETWEEN Y-479 AND Y 0 IS CORRODED. REMOVED AND REPLACED STRAP IAW EMB145 SRM 51-40-02.
- [SDR HNAA2024040100241](https://openairdocs.org/sdr/HNAA2024040100241), Mar 14, 2024: FLOOR SUPPORT. CORRODED. 00192 CENTER Y 0 FLOOR BEAM LH FLANGE IS CORRODED BETWEEN FRM28 AND FRM29. REPAIRED CENTER Y 0 FLOOR BEAM LH FLANGE IS CORROSION BETWEEN FRM28 AND FRM29 IAW EMB
- [SDR HNAA2024040100240](https://openairdocs.org/sdr/HNAA2024040100240), Mar 14, 2024: STRAP. CORRODED. 00182 LH FLOOR SUPPORT STRAP AT X7578 BETWEEN Y-479 AND Y 0 IS CORRODED.
- [SDR HNAA2024040100239](https://openairdocs.org/sdr/HNAA2024040100239), Mar 14, 2024: FLOORBEAM. CORRODED. 00179 CENTER Y 0 FLOOR BEAM CAP IS CORRODED BETWEEN FRM20 AND X7038. INSTALLED NEW CENTER Y 0 FLOOR BEAM CAP PN# 145-22460-013 BETWEEN FRM20 AND X7038 IAW EMB 1
- [SDR HNAA2023103000369](https://openairdocs.org/sdr/HNAA2023103000369), Oct 28, 2023: UNKNOWN. UNKNOWN. LEFT I/B MAIN TIRE DAMAGED (TREAD CAME OFF). R&R #200 MLG TIRE IAW EMB AMM 32-49-02-000-801-A/32-49-02-400-801-A INSPECTED AND FOUND ADDITIONAL DAMAGE SEE SEQ 2
- [SDR SIMA20230319001](https://openairdocs.org/sdr/SIMA20230319001), Mar 19, 2023: FLASHLIGHT. INOPERATIVE. AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT NOT CHARGING-C/A-RAR AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY. OPC GOOD PER EMB AMM 33-51-01

All 145: https://openairdocs.org/aircraft/N931AE/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/N931AE/stcs.md

## Earlier aircraft with N931AE

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N931AE before.

- [Cancelled 1999-07-26](https://openairdocs.org/deregistered/N931AE-1999-07-26): British Aerospace BAE JETSTREAM 3201, S/N 931. 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

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