# N932AE: 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: 14500915
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 26, 2005
- Certificate issued: October 17, 2011
- Expires: October 31, 2027
- Mode S code: ACED1C
- 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=932AE
- Page: https://openairdocs.org/aircraft/N932AE

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/N932AE/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 N932AE.

## FAA accident and incident reports

None matched to N932AE.

## Service difficulty reports (135, 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 HNAA2026092500911](https://openairdocs.org/sdr/HNAA2026092500911), Sep 21, 2026: STRUCTURE. DAMAGED. BIRD STRIKE TO L/H SIDE OF NOSE. PERFORMED BIRD STRIKE INSPECTION IAW AMM 05-50-08. SEE LOGPAGE 380834-3 FOR DAMAGE MAPPING.
- [SDR HNAA2026083100812](https://openairdocs.org/sdr/HNAA2026083100812), Aug 28, 2026: ELEC CONNECTOR. LOOSE. ON CLIMBOUT, MAIN PTRIM INOPERTIVE EICAS MESSAGE, EMERGENCY DECLARED & RTF. DURING TROUBLE SHOOTING, FOUND HSA CONNECTOR P1087 TO BE LOOSE, TIGHTENED AS REQUIRE
- [SDR HNAA2026062400553](https://openairdocs.org/sdr/HNAA2026062400553), Jun 23, 2026: RELAY. FAULTED. ICE CONDITION, ANTI ICE INOP, ENG REF ANTI ICE DISAG, ICE CONDITION DISPLAYED ON TAKEOFF AT 76KTS. R & R RELAYS K0264, K0532, K0531, K0323 IAW AMM 20-13-02. PER
- [SDR HNAA2026060800492](https://openairdocs.org/sdr/HNAA2026060800492), Jun 6, 2026: CONTROLLER. INTERMITTENT. W/S HEAT 2 CAUTION MSG INTERMITTENT IN FLIGHT. R & R NR 2 WS TEMP CONTROLLER IAW AMM 30-42-01 OPS CHECK GOOD. AC OK FOR SERVICE.
- [SDR HNAA2026012900105](https://openairdocs.org/sdr/HNAA2026012900105), Jan 20, 2026: SUPPORT ANGLE. CRACKED. LEFT THRUST REVERSER OTBD SKIN UPPER SUPPORT ANGLE CRACKED. R & R THE SUPPORT ANGLE IAW SRM 51-40-02
- [SDR HNAA2026012900104](https://openairdocs.org/sdr/HNAA2026012900104), Jan 15, 2026: FRAME. PUNCTURED. PUNTURED FRAME AT FR60, BTW4-5L.REPAIRED IAW ETD2025-145-934269
- [SDR HNAA2026010500003](https://openairdocs.org/sdr/HNAA2026010500003), Dec 24, 2025: SUPPORT. CORRODED. LEFT SUPPORT CORRODED AT BTW FR 60-65. R & R THE SUPPORT IAW SRM 51-40-02
- [SDR HNAA2026012300079](https://openairdocs.org/sdr/HNAA2026012300079), Dec 17, 2025: SUPPORT BRACKET. CRACKED. STALL WARNING COMPUTER SUPPORT BRACKETS CRACKED. R & R SUPPORT BRACKETS IAW SRM 51-40-02
- [SDR HNAA2026012900103](https://openairdocs.org/sdr/HNAA2026012900103), Dec 16, 2025: SHEAR TIE. CRACKED. RIGHT SHEAR TIE CRACKED AT FR 80 BTW S3-5R. R & R SHEAR TIE IAW SRM 51-40-02
- [SDR HNAA2026012800093](https://openairdocs.org/sdr/HNAA2026012800093), Dec 16, 2025: PROFILE. CRACKED. BOTTOM OF VERTICAL STAB, AFT OF REAR SPAR 3, RT PROFILE CRACKED AT LWR END. REPAIRED IAW ETD 2026-145-934573 AND EO1-55-26-0011
- [SDR HNAA2026012000017](https://openairdocs.org/sdr/HNAA2026012000017), Dec 16, 2025: SPAR. CRACKED. BTM OF VRT STA, AFT OF REAR SPAR 3, LWR LH PROFILE CRACKED IN 2 PLACES. RAR PROFILE IAW SRM 51-40-02
- [SDR HNAA2026012900102](https://openairdocs.org/sdr/HNAA2026012900102), Dec 15, 2025: DOUBLER. CORRODED. FR61 FLOOR LEVEL, FRAME DOUBLER CORRODED. REPAIRED IAW SRM 53-31-04.
- [SDR HNAA2026012700087](https://openairdocs.org/sdr/HNAA2026012700087), Dec 15, 2025: DOUBLER. CORRODED. FRAME DOUBLER CORRODED AT FR 61 LT. PERFORMED CUTOUT, FABRICATED & REINSTALLED REPAIR DOUBLER IAW SRM 53-31-04.
- [SDR HNAA2026012700086](https://openairdocs.org/sdr/HNAA2026012700086), Dec 15, 2025: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AT FR 61, S18-20R. THE SHEAR TIE REMOVED AND INSTALLED IAW SRM 51-40-02, FABRICATED NEW SHEAR TIE IAW ETD2026-415-00784, AND EO1-53-26-0033.
- [SDR HNAA2026012300080](https://openairdocs.org/sdr/HNAA2026012300080), Dec 15, 2025: GUSSET. CORRODED. CENTER GUSSET CORRODED AT BTW FR 59-61. R & R THE GUSSET IAW SRM 51-40-02
- [SDR HNAA2026010500004](https://openairdocs.org/sdr/HNAA2026010500004), Dec 15, 2025: DOUBLER. CORRODED. DOUBLER CORRODED BTW FR60-61, BTW LH SILL AND LH DOUBLER. R & R DOUBLER IAW SRM 51-40-02
- [SDR HNAA2026020300109](https://openairdocs.org/sdr/HNAA2026020300109), Dec 12, 2025: SHIELD. CORRODED. CORROSION UNDERNEATH LT THRUST REVERSER OTBD PYLON FIRESHIELD. REPAIRED IAW EO1-78-26-0009 ANS SRM 51-40-02
- [SDR HNAA2026012800092](https://openairdocs.org/sdr/HNAA2026012800092), Dec 12, 2025: FLOOR SUPPORT. CRACKED. LEFT OMEGA BEAM INBD VERTICAL FLANGE CRACKED AT FRM 34. REPAIRED IAW ETD2026-145-934095 AND EO1-53-26-0003.
- [SDR HNAA2026012800091](https://openairdocs.org/sdr/HNAA2026012800091), Dec 12, 2025: FLOOR SUPPORT. CRACKED. LEFT OMEGA BEAM INBD VERTICAL FLANGE CRACKED AT FRM 33. REPAIRED IAW ETD 2026-145-934095 AND EO1-53-26-0003.
- [SDR HNAA2026012700085](https://openairdocs.org/sdr/HNAA2026012700085), Dec 12, 2025: ANGLE. CRACKED. APU FIREWALL, THREE CRACKED ANGLES. R & R ANGLES IAW SRM M51-40-02.
- [SDR HNAA2026012200070](https://openairdocs.org/sdr/HNAA2026012200070), Dec 12, 2025: FIREWALL. CRACKED. APU FIREWALL CRACKED. REPAIRED IAW SRM 53-32-13 FIG 205
- [SDR HNAA2026012000015](https://openairdocs.org/sdr/HNAA2026012000015), Dec 12, 2025: SHEAR TIE. CRACKED. SHEAR CLIP CRACKED AT FR10 STR 9L. R & R SHEAR CLIP IAW SRM 51-40-02
- [SDR HNAA2026012000014](https://openairdocs.org/sdr/HNAA2026012000014), Dec 12, 2025: ANGLE. CRACKED. ANGLE CRACKED AT FR10 STR 9L. R & R ANGLE IAW SRM 51-40-02
- [SDR HNAA2026020900113](https://openairdocs.org/sdr/HNAA2026020900113), Dec 11, 2025: FLOOR SUPPORT. CRACKED. LEFT OMEGA BEAM OTBD ANGLE CRACKED AT BTW FR47-50. R & R ANGLE IAW SRM 51-40-02.
- [SDR HNAA2026012900106](https://openairdocs.org/sdr/HNAA2026012900106), Dec 11, 2025: SHEAR TIE. CORRODED. SHEAR CLIP CORRODED AT FR 52 BTW STR 20-21R. R & R SHEAR CLIP IAW SRM51-40-02
- [SDR HNAA2026012900101](https://openairdocs.org/sdr/HNAA2026012900101), Dec 11, 2025: SHEAR TIE. CORRODED. SHEAR TIE CORRODED AT FR51 BTW S20 - 21R. REMOVED, FABRICATED, AND INSTALLED SHEAR TIE IAW ETD2026-145-000952.
- [SDR HNAA2026012900100](https://openairdocs.org/sdr/HNAA2026012900100), Dec 11, 2025: STRINGER. CORRODED. STRINGER 21R CORRODED AT BTW FR 50-53. R & R THE STRINGER BETWEEN FRMS 50-53 IAW SRM 51-40-02.
- [SDR HNAA2026012900099](https://openairdocs.org/sdr/HNAA2026012900099), Dec 11, 2025: SUPPORT. CRACKED. LEFT OMEGA BEAM CRACKED AT FR36. REPAIRED IAW ETD 2025-145-934098 AND EO1-53-26-0001.
- [SDR HNAA2026012800090](https://openairdocs.org/sdr/HNAA2026012800090), Dec 11, 2025: SUPPORT ANGLE. CRACKED. CARGO DOOR LIFTING MECHANISM SUPPORT ANGLE CRACKED AT FR 62 BTW S4 - 5R. R & R THE SUPPORT ANGLE IAW SRM 51-40-02.
- [SDR HNAA2026012700084](https://openairdocs.org/sdr/HNAA2026012700084), Dec 11, 2025: ANGLE. CRACKED. RIGHT OVERWING PANEL 194ER, NR 1 LWR ANGLE CRACKED, YA-1085, RIB1A. REMOVED, FARICATED, AND INSTALLED A NEW ANGLE IAW SRM 57-20-01RE.
- [SDR HNAA2026012300078](https://openairdocs.org/sdr/HNAA2026012300078), Dec 11, 2025: FLOOR SUPPORT. CRACKED. LEFT OMEGA BEAM INBD ANGLE CRACKED AT BTW FR47-50. R & R ANGLE IAW SRM 51-40-02
- [SDR HNAA2026012300077](https://openairdocs.org/sdr/HNAA2026012300077), Dec 11, 2025: FLOOR SUPPORT. CRACKED. 53-2132 RH OMEGA BEAM IB ANGLE CRACKED AT BTW FR48-50. R & R ANGLE IAW SRM 51-40-02
- [SDR HNAA2026012300076](https://openairdocs.org/sdr/HNAA2026012300076), Dec 11, 2025: FLOOR SUPPORT. CRACKED. 53-2131 RH OMEGA BEAM OB ANGLE CRACKED AT BTW FR48-50. RAR ANGLE IAW SRM 51-40-02
- [SDR HNAA2026012100051](https://openairdocs.org/sdr/HNAA2026012100051), Dec 11, 2025: SUPPORT. CRACKED. CARGO DOOR LIFTING MECHANISM UPPER SUPPORT CRACKED AT BTW FR 67-68 STR4R. RAR SUPPORT IAW SRM 51-40-02
- [SDR HNAA2026012000016](https://openairdocs.org/sdr/HNAA2026012000016), Dec 11, 2025: SUPPORT. CRACKED. CARGO DOOR LIFTING MECHANISM SUPPORT CRACKED AT BTW FR61-62 BTW STR4-5R. RAR SUPPORT IAW SRM 51-40-02
- [SDR HNAA2026012000013](https://openairdocs.org/sdr/HNAA2026012000013), Dec 11, 2025: SUPPORT. CORRODED. RIGHT SILL CORRODED AT BTW FR 71-73. R & R SILL IAW SRM 51-40-02
- [SDR HNAA2025121900862](https://openairdocs.org/sdr/HNAA2025121900862), Dec 11, 2025: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AT FR 58 BTW S15-16L. R & R SHEAR TIE IAW SRM 51-40-02.
- [SDR HNAA2026012900098](https://openairdocs.org/sdr/HNAA2026012900098), Dec 10, 2025: SUPPORT. CRACKED. LEFT OMEGA BEAM INBD VERTICAL FLANGE CRACKED AT FR23. REPAIRED IAW ETD2025-145-93466 AND EO 1-53-26-0001.
- [SDR HNAA2026012900097](https://openairdocs.org/sdr/HNAA2026012900097), Dec 10, 2025: SUPPORT. CRACKED. LEFT OMEGA BEAM INBD VERTICAL FLANGE CRACKED AROUND RIVET HEAD AT FR22. REPAIRED IAW ETD 2025-145-934066 AND EO1-53-26-0001.
- [SDR HNAA2026012800088](https://openairdocs.org/sdr/HNAA2026012800088), Dec 10, 2025: FLOOR SUPPORT. CRACKED. LEFT OMEGA BEAM INBD VERTICAL FLANGE CRACKED AROUND RIVET AT FR 21. REPAIRED IAW ETD2025-145-934066 AND EO1-53-26-0001.
- [SDR HNAA2025121900861](https://openairdocs.org/sdr/HNAA2025121900861), Dec 10, 2025: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AT FR26 BTW S15-16L. R & R SHEAR TIE IAW SRM 51-40-02.
- [SDR HNAA2025061600453](https://openairdocs.org/sdr/HNAA2025061600453), Jun 15, 2025: UNKNOWN. FUMES. SMELLED POSSIBLE FUEL FUMES IN CLOCKPIT DURING APU START FACT 15JUN25 18:20 CLT STARTED APU AT GATE NO FUEL SMELL IN FLIGHT DECK OR CABIN. OK FOR SERVICE
- [SDR HNAA2025052000357](https://openairdocs.org/sdr/HNAA2025052000357), May 19, 2025: CONTACTOR. LOOSE. WHILE DEPLANING SMELLED FUMES IN FLIGHT DECK DETECTED SMOKE AT L/H DISTROBUTION BOX BEHIND CAPTAIN SEAT. REMOVED EBC1 IAW AMM 24-60-03.(842286) R&R'D #100 EBC1 
- [SDR HNAA2024111801101](https://openairdocs.org/sdr/HNAA2024111801101), Nov 17, 2024: CONTACTOR. OVERHEATED. ODOR ON FLIGHT DECK ON DECENT, BECAMRE STRONGER WHEN APU SELCTED. INSPECTED AND FOUND ODOR TO BE OF A BURNT ELECTRICAL SMELL, VISUALLY INSPECTED LH DISTRIBUTION
- [SDR HNAA2024111801100](https://openairdocs.org/sdr/HNAA2024111801100), Nov 16, 2024: UNKNOWN. ODOR. OZONE SMELL ON DECENT IN CABIN AND FLIGHT DECK UPON TOUCHDOWN WITH APU BLEED SELECTED SMELL BECAME STRONG UPON GAT EARRIVAL WHEN DOOR OPEN SMELL PERSIST. FACT 1
- [SDR HNAA2024053100481](https://openairdocs.org/sdr/HNAA2024053100481), May 30, 2024: UNKNOWN. VIBRATION. SUDDEN VIBRATION AND LOUD NOISE DURING CLIMB, DESCENT AND TURNS THAT LASTED APPROX 5 SECONDS WITH GEAR UP AND LOCKED. NOISE OBSERVED FROM NOSE OF A/C. FACT 31MA
- [SDR HNAA2024053000479](https://openairdocs.org/sdr/HNAA2024053000479), May 29, 2024: INVERTER. INOPERATIVE. RH EMERGENCY EXIT DOOR IDENTIFIER SIGN IS OUT. RAR #5 INVERTER IAW AMM 33-50-11-400-801-A
- [SDR HNAA2024022700165](https://openairdocs.org/sdr/HNAA2024022700165), Feb 26, 2024: WIRE. FRAYED. EMERGENCY FLOOR STRIP LIGHT WIRES ARE FRAYED AT ROW 8 TO9. R&R'D EMERGENCY FLOOR LIGHT ASSY AT ROW 8-9 IAW AMM33-50-12
- [SDR HNAA2023092400247](https://openairdocs.org/sdr/HNAA2023092400247), Sep 24, 2023: UNKNOWN. UNKNOWN. NO.2 ENG SHUT DOWN INFLIGHT AND WOULD NOT RESTART. R/R #200 ENGINE IRT WORKCARD 71-00-00
- [SDR HNAA2023061900193](https://openairdocs.org/sdr/HNAA2023061900193), May 17, 2023: UNKNOWN. UNKNOWN. E975872 SSI 53-30-48, CARGO DOOR LOWER SILL FWD EDGE HAS LEVEL 2 CORROSION. : BLENDED CORROSION ON CARGO DOOR LOWER SILL FWD EDGE IAW EMB 145 SRM 51-10-03. HASN

All 135: https://openairdocs.org/aircraft/N932AE/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/N932AE/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

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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.