# N831AE: 2002 Embraer EMB-135KL

- Status: Valid registration
- Airframe: [Embraer EMB-135KL](https://openairdocs.org/model/embraer-emb-135kl) (registry code 3260302, 37 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: 145616
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 24, 2002
- Certificate issued: November 26, 2023
- Expires: November 30, 2030
- Mode S code: AB5C16
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, 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=831AE
- Page: https://openairdocs.org/aircraft/N831AE

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): 87 in force

### Matched by airframe (Embraer EMB-135KL)

- [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 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 2008-22-19](https://openairdocs.org/ad/2008-22-19): Flight deck · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 19, 2008
- [AD 2008-17-05](https://openairdocs.org/ad/2008-17-05): Fuel tanks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 23, 2008
- [AD 2008-10-08](https://openairdocs.org/ad/2008-10-08): Reduces the compliance time for doing the modification · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective May 23, 2008
- [AD 2008-05-02](https://openairdocs.org/ad/2008-05-02): Tail section or rudder pedals · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Apr 8, 2008
- [AD 2008-03-03](https://openairdocs.org/ad/2008-03-03): Elevator control system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Feb 14, 2008
- [AD 2007-24-03](https://openairdocs.org/ad/2007-24-03): Forward fuselage right hand (RH) side skin · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jan 2, 2008
- [AD 2007-04-09](https://openairdocs.org/ad/2007-04-09): Left- and right-hand windshield temperature controllers · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 23, 2007
- [AD 2007-04-03](https://openairdocs.org/ad/2007-04-03): Pitot static heating relay K0057 · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 21, 2007
- [AD 2006-19-04](https://openairdocs.org/ad/2006-19-04): Honeywell COM unit and Mode S transponder · Bombardier BD-700-1A10, BD-700-1A11, 550 and 26 more. Effective Oct 17, 2006
- [AD 2006-16-17](https://openairdocs.org/ad/2006-16-17): Torque values of the screws that attach the seat tracks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 25, 2006
- [AD 2006-07-01](https://openairdocs.org/ad/2006-07-01): Horizontal stabilizer control unit (HSCU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective May 1, 2006
- [AD 2006-03-06](https://openairdocs.org/ad/2006-03-06): Pilot's and co-pilot's seat tracks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 13, 2006
- [AD 2005-25-17](https://openairdocs.org/ad/2005-25-17): Auxiliary power unit (APU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 18, 2006
- [AD 2005-24-11](https://openairdocs.org/ad/2005-24-11): Elevator gust lock system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 9, 2006
- [AD 2005-24-02](https://openairdocs.org/ad/2005-24-02): Airplane flight manual (AFM) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 28, 2005
- [AD 2005-23-20](https://openairdocs.org/ad/2005-23-20): Auxiliary power unit (APU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 27, 2005
- [AD 2005-23-13](https://openairdocs.org/ad/2005-23-13): Nose landing gear (NLG) wheel · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 19, 2005
- [AD 2005-22-08](https://openairdocs.org/ad/2005-22-08): Total air temperature (TAT) sensor heating system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Nov 30, 2005
- [AD 2005-20-37](https://openairdocs.org/ad/2005-20-37): Main landing gear (MLG) trailing arms and integrity of the MLG pivot axle sealant. · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Nov 16, 2005
- [AD 2005-14-02](https://openairdocs.org/ad/2005-14-02): Left and right engine fire handles · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Aug 15, 2005
- [AD 2005-14-03](https://openairdocs.org/ad/2005-14-03): Engine-driven hydraulic pump · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Aug 10, 2005
- [AD 2005-13-22](https://openairdocs.org/ad/2005-13-22): Electric fuel pumps · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jul 7, 2005
- [AD 2005-05-09](https://openairdocs.org/ad/2005-05-09): Forward upper liners · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Apr 14, 2005
- [AD 2005-04-05](https://openairdocs.org/ad/2005-04-05): Air turbine starter (ATS) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 24, 2005
- [AD 2005-01-05](https://openairdocs.org/ad/2005-01-05): Nose Landing Gear Wheel Nuts and Associated Inner and Outer Seals, and Reidentifying the Landing Gear Strut · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Feb 9, 2005
- [AD 2004-25-21](https://openairdocs.org/ad/2004-25-21): Pitch trim system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 26, 2005
- [AD 2004-25-12](https://openairdocs.org/ad/2004-25-12): Passenger service unit (PSU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 13, 2005
- [AD 2004-24-03](https://openairdocs.org/ad/2004-24-03): Internal o-ring seal · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 23 more. Effective Jan 3, 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 2006-04-02](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 2003-09-03](https://openairdocs.org/ad/2003-09-03) (historical): Cartridge flange · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 3 more. Effective May 14, 2003
- [AD 2002-16-06](https://openairdocs.org/ad/2002-16-06) (historical): Auxiliary power unit (APU) · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 2 more. Effective Aug 27, 2002
- [AD 2002-08-21](https://openairdocs.org/ad/2002-08-21) (historical): Bonding Jumpers that Connect the Horizontal Stabilizer to the Vertical Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 2 more. Effective May 16, 2002
- [AD 2002-08-18](https://openairdocs.org/ad/2002-08-18) (historical): Actuator Clutches of the Primary and Backup Pitch Trim Systems of the Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 2 more. Effective May 16, 2002
- [AD 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 104: https://openairdocs.org/aircraft/N831AE/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 N831AE.

## FAA accident and incident reports

None matched to N831AE.

## Service difficulty reports (119, 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 SIMA20210325002](https://openairdocs.org/sdr/SIMA20210325002), Mar 25, 2021: LIGHT. INOPERATIVE. RH EXTERIOR AFT EMERGENCY LIGHT INOP-C/A-RAR RH EXTERIOR AFT EMERGENCY LIGHT IAW EMB 140 AMM 33-50-10 2. L (1) (2) (3) (4) AND 33-50-10 3. K (1) (2) (3) (4). OP
- [SDR SIMA20210301003](https://openairdocs.org/sdr/SIMA20210301003), Mar 1, 2021: WIRE. BROKEN. LH OVERWING PANEL EMERGENCY LIGHT INOP-C/A-UPON FURTHER INVESTIGATION FOUND BROKEN WIRE INSIDE LIGHT HOUSING. RAR WIRE TERMINAL ON LH OVERWING EMERGENCY LIGHT I
- [SDR SIMA20210228002](https://openairdocs.org/sdr/SIMA20210228002), Feb 28, 2021: BULB. INOPERATIVE. R/H OVER WING EMERGENCY LIGHTS NOT WORKING.-C/A-RAR LIGHT BULB R/H OVER THE WING EMEERGENCY LIGHT. OPS CHECK GOOD. IAW EMB 140 AMM 33-50-10.
- [SDR SIMA20210219001](https://openairdocs.org/sdr/SIMA20210219001), Feb 19, 2021: BATTERY PACK. INOPERATIVE. LH OVERWING EXIT IDENTIFIER, FLOOR PROX LIGHT 4, EXIT MARKER RH OVERWING, FLOOR PROX LIGHT 5, EXIT IDENTIFIER RH OVERWING, LH OVERWING LIGHT, RH OVERWING LIGHT,
- [SDR SIMA20210128001](https://openairdocs.org/sdr/SIMA20210128001), Jan 28, 2021: LIGHT. INOPERATIVE. RIGHT HAND WING EMERGENCY LIGHT INOPERABLE. C/A: R & R EMERGENCY LIGHT, IAW AMM 33-50-10. OPERATIONS CHECK OK.
- [SDR SIMA20210109005](https://openairdocs.org/sdr/SIMA20210109005), Jan 9, 2021: FLASHLIGHT. MISSING. FA EMERGENCY FLASHLIGHT MISSING, REF MEL NR 25-53 AUTH NR 010126-C. C/A: INSTALLED FA EMERGENCY FLASHLIGHT, IAW REF 33-50-16 MEL RESTORED.
- [SDR SIMA20201224001](https://openairdocs.org/sdr/SIMA20201224001), Dec 24, 2020: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT BATTERY PACK NR 3 WILL NOT HOLD CHARGE. C/A: REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK NR 3, IAW AMM 33-50-04. EMERGENCY LIGHTS OPERATIO
- [SDR SIMA20201210004](https://openairdocs.org/sdr/SIMA20201210004), Dec 10, 2020: BULB. INOPERATIVE. RT OVER WING EMERGENCY LIGHT INOPERABLE. C/A: R & R RT OVER WING EMERGENCY LIGHT BULB, IAW AMM 33-50-10. OPERATIONS CHECK GOOD.
- [SDR SIMA20201119001](https://openairdocs.org/sdr/SIMA20201119001), Nov 19, 2020: LAMP. INOPERATIVE. AISLE AFT EMERGENCY LIGHT INOPERABLE. C/A: R & R AISLE AFT EMERGENCY LIGHT LAMP, IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPERATIONS CHECK GOOD, N
- [SDR SIMA20201106001](https://openairdocs.org/sdr/SIMA20201106001), Nov 6, 2020: LAMP. INOPERATIVE. RT OVERWING EMERGENCY LIGHT INOPERABLE. C/A: R & R RT OVER WING EMERGENCY LIGHT LAMP, IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPERATIONS CHECK GO
- [SDR SIMA202001131001](https://openairdocs.org/sdr/SIMA202001131001), Jan 11, 2020: INVERTER. INOPERATIVE. EMERG LITE AT ROW 3 INOP-C/A-REMOVED AND REPLACED AC-DC EMERG INVERTER IAW 33-50-11 OPS CK GOOD
- [SDR SIMA2020010228003](https://openairdocs.org/sdr/SIMA2020010228003), Dec 28, 2019: LIGHT. MALFUNCTIONED. RANDOM STRIP OF EMERGENCY LIGHTS ILLUMINATED ROWS 7-11 A SIDE-C/A-PERFORMED EMERGENCY LIGHTS ADJUSTMENT/ TEST IAW AMM 33-50-00 OPC GOOD LIGHTS EXTINGUISHED
- [SDR SIMA2019111109003](https://openairdocs.org/sdr/SIMA2019111109003), Nov 9, 2019: SEAL. LEAKING. FA REPORTED MAIN DOOR WAS SQUILING, BEGAN AROUND FL20 DURING PRESSURIZATION/LEAK CHECK OF AIRCRAFT FOUND SERVICE DOOR HAS A LEAK ON BOTTOM FORWARD CORNER-C/A-RE
- [SDR SIMA20191105001](https://openairdocs.org/sdr/SIMA20191105001), Nov 5, 2019: POWER SUPPLY. FAILED. EMERG LT COME OM WHEN YOU UNARM IT TO OFF-C/A-REMOVED AND REPLACED BATTERY POWER SUPPLY 4 IAW ERJ140 AMM 33-50-04. NO FURTHER DEFECTS NOTED
- [SDR SIMA20190925002](https://openairdocs.org/sdr/SIMA20190925002), Sep 25, 2019: BATTERY. DISCHARGED. #3 EMER LIGHT BATTERY IS INOP. C/A-RAR # 3 EMER LIGHT BATTERY AND CHARGER IAW AMM 33-50-04 OPC GOOD.
- [SDR SIMA20190705001](https://openairdocs.org/sdr/SIMA20190705001), Jul 5, 2019: UNKNOWN. MALFUNCTIONED. AUTO PRESSURIZATION FAILED AFTER TAKEOFF. C/A-DEFERRED AUTO AND MANUAL PRESSURIZATION SYSTEM M PROCEDURES C/W AUTH # 070157DM-C REF # 21-19. DE-C/W M PROSSEDURE
- [SDR SIMA20190702003](https://openairdocs.org/sdr/SIMA20190702003), Jul 2, 2019: CHARGER. FAILED. EMERGENCY EXIT LIGHTS FLOOR STRIP ROW 12 INOP. C/A-REMOVED AND REPLACED #3 EMERGENCY BATTERY AND CHARGER IAW AMM 33-50-04. OP CK GOOD. EMERGENCY LIGHTING BATTER
- [SDR SIMA20190628002](https://openairdocs.org/sdr/SIMA20190628002), Jun 28, 2019: HOLDER. DEFECTIVE. EMER LIGHTS OFF POSITION, THEN BATTERIES OFF WITH GPU CONNECTED STRIP OF EMERGENCY LIGHTS ILLUMIMNATING AT ROWS 7 - 11 . F/A PANEL ALSO HAS EMERGENCY LIGHTS TUR
- [SDR SIMA201906174003](https://openairdocs.org/sdr/SIMA201906174003), Jun 14, 2019: CHARGER. FAILED. FLOOR EMERGENCY LIGHT ROWS 7 8 9 10 ILLUMINATED WITH EMER LIGHTS IN OFF POSTION-C/A-TROUBLESHOOTING EMERGENCY FLOOR LIGHTS AND FOUND #3 BATTERY POWER SUPPLY TO 
- [SDR SIMA20190507004](https://openairdocs.org/sdr/SIMA20190507004), May 7, 2019: BRAKE ASSY. DEFECTIVE. SUPPLEMENTAL EMERGENCY BRAKE LO PRES AFTER PARKING. C/A-DEFFERED AS PER MEL 32-5 C/W (M) PROCEDURES. SERVICED EMERGENCY BRAKE ACCUMULATER TDMI 831T3278 IAW AMM 
- [SDR SIMA20190501002](https://openairdocs.org/sdr/SIMA20190501002), May 1, 2019: BATTERY. FAILED. OVERWING UPPER AND LOWER INTERIOR EMERGENCY EXIT LIGHTS INOP AND EMERGERNCY LIGHT FLOOR STRIPS 4 AND 5 INOP. C/A-FOUND NR 3 EPSU BATTERY WOULD NOT HOLD A CHARGE
- [SDR SIMA201904254002](https://openairdocs.org/sdr/SIMA201904254002), Apr 24, 2019: LAMP. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOP-C/A-REMOVED AND RELAMPED IAW EMB 140 AMM 33-50-09. OPS CHECK GOOD AT THIS TIME
- [SDR SIMA201904153001](https://openairdocs.org/sdr/SIMA201904153001), Apr 13, 2019: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT AT STRIP 4 AND 5,SIDE EXIT LIGHT IN THE EMERGENCY DOORS INOP-C/A-REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY #3 IAW AMM 33-50-04,OPS CHECK
- [SDR SIMA2019040142003](https://openairdocs.org/sdr/SIMA2019040142003), Apr 1, 2019: UNKNOWN. UNKNOWN. FLOOR EMERGENCY LIGHTS SECTION 9A-11A AND BOTH OVERWING EXIT SIGNS ILLUMINATED AFTER ENGINE SHUTDOWN. CYCLED POWER AND PERFORMED OPC CHECK IAW AMM 33-50-00 AND 
- [SDR SIMA20190212001](https://openairdocs.org/sdr/SIMA20190212001), Feb 12, 2019: MECHANISM. DIRTY. MAIN CABIN DOOR HARD TO OPEN AND CLOSE, FLAP ON TOP OF THE DOOR NOT CLOSING FULLY. PERFORMED INSPECTION, CLEANED & LUBED LOCKING MECHANISM IAW AMM 52-11-00 AND 
- [SDR SIMA201902110001](https://openairdocs.org/sdr/SIMA201902110001), Feb 10, 2019: SEAL. DEBONDED. DURING CLIMB THE AIRCRAFT FAILED TO PRESSURIZE. CREW COMPLIED WITH QRH AND RETURNED TO BNA. CA DV WINDO NOT SEALING PROPERLY AT TOP -C/A-INSP CA DV WINDOW AND F
- [SDR SIMA2019021108002](https://openairdocs.org/sdr/SIMA2019021108002), Feb 8, 2019: CONTROL VALVE. DAMAGED. CABIN WOULD NOT PRESSURIZE CLIMBING THROU 10,000 FT.NOTED THAT A/C WAS NOT PRESSURIZED BUT CABIN ALTITUDE INCREASING-C/A-PERFORMED INSPECTION/CHECK OF PACK 2 DU
- [SDR SIMA20190119003](https://openairdocs.org/sdr/SIMA20190119003), Jan 19, 2019: CONNECTOR. SEVERED. RT FWD EMERGENCY LIGHT CONNECTOR SEVERED. C/A-REPAIR EMERGENCY LIGHT RT FWD PLUG CONNECTOR IAW SWPM 20-50-00 OPS CHECK GOOD.
- [SDR SIMA20181215005](https://openairdocs.org/sdr/SIMA20181215005), Dec 15, 2018: FITTING. CORRODED. BAGGAGE DOOR SHEAR CLIP CORRODED AT FR 65 AND STR 15L. C/A-INSTALLED SERVICABLE SHEAR CLIP AT FR 65 IAW SRM 53-31-04.
- [SDR SIMA20181215006](https://openairdocs.org/sdr/SIMA20181215006), Dec 15, 2018: DOOR SILL. CORRODED. SERVICE DOOR CUTOUT FLOOR CENTER SILL CORRODED. C/A-REPAIRED SERVICE DOOR CUTOUT LOWER CENTER SILL IAW SRM 51-40-02, AND 51-20-03.
- [SDR SIMA20181215004](https://openairdocs.org/sdr/SIMA20181215004), Dec 15, 2018: DOOR SILL. CORRODED. BAGGAGE DOOR SILL CORRODED. C/A-INSTALLED SERVICABLE CARGO DOOR SILL IAW SRM 52-40-02.
- [SDR SIMA20181209010](https://openairdocs.org/sdr/SIMA20181209010), Dec 9, 2018: CROSSBEAM. CORRODED. ISLE CROSS BEAM AT FRAME 25 CORRODED. C/A-COMPLETE: REMOVED AND REPLACED ISLE CROSS BEAM AT FRAME 25 IAW SRM 53-21-10 FIG-1, 10, 10A, 10B, 10C, 10D. ETN-EM-53-1
- [SDR SIMA20181209009](https://openairdocs.org/sdr/SIMA20181209009), Dec 9, 2018: WIRE HARNESS. DAMAGED. WIRE BUNDLE BELOW CARGO FLOOR ON LT SIDE BETWEEN FRAMES 65 AND 66 HAS BURN MARKS (TAGGED). C/A-COMPLETE: REPAIRED WIRE BUNDLE BETWEEN FR 65 66 LT IAW SWPM 20-21
- [SDR SIMA20181209008](https://openairdocs.org/sdr/SIMA20181209008), Dec 9, 2018: SUPPORT BRACKET. NOT REPORTED. TRANSFERRED FROM LOG PAGE 4411161 ITEM 1 "TDMI 831T5346 - REF LOG PAGE 4064237 ITEM 2 - ONETIME REPAIR - POSITION LT WING - WING TO FUSELAGE FAIRING SUPPORT L/H
- [SDR SIMA20181209005](https://openairdocs.org/sdr/SIMA20181209005), Dec 9, 2018: LIGHT. DAMAGED. RT FLOOR EXTRUSIONS NR 1 AND 2 ARE DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED RT ISLE EXTRUSIONS NR 1, 2 IAW AMM 33-50-12.
- [SDR SIMA20181209006](https://openairdocs.org/sdr/SIMA20181209006), Dec 9, 2018: WIRE. OUT OF POSITION. EMERGENCY LIGHT STRIP WIRING ROUTED INCORRECTLY AT FLOOR PANEL 231GF. (TAGGED) C/A-COMPLETE:REPAIRED AND REROUTED EMERGENCY LIGHT STRIP WIRING AT 231GF IAW SWPM
- [SDR SIMA20181209007](https://openairdocs.org/sdr/SIMA20181209007), Dec 9, 2018: LIGHT. DIM. PAX DOOR EMERGENCY LIGHT DIM. C/A-COMPLETE:REMOVED AND REPLACED PAX DOOR EMERGENCY LIGHT ASSY. IAW AMM 33-50-10.
- [SDR SIMA20181209004](https://openairdocs.org/sdr/SIMA20181209004), Dec 9, 2018: LIGHT. DAMAGED. EMERGENCY LIGHT EXTRUSIONS ARE DAMAGED NR 1, 2 ,3 AND 8. C/A-COMPLETE:REMOVED AND REPLACED LT ISLE EXTRUSIONS NR 1, 2 ,3 AND 8. IAW AMM 33-50-12.
- [SDR SIMA201812076001](https://openairdocs.org/sdr/SIMA201812076001), Dec 6, 2018: SENSOR. FAILED. DURNING ICE TEST PNEUMATIC WING A/ICE FAIL CAUTION MESSAGE IN FLIGHT ALL FOUR ANTI ICE LIGHTS WERE ILLUMANATED OPEN NON ICING CONDITION AND ICE DETECTOR OVERRID
- [SDR SIMA20181021003](https://openairdocs.org/sdr/SIMA20181021003), Oct 21, 2018: TAPE. MISSING. ON CLIMB OUT OF DFW WE HEARD A LOUD BANG NOISE COMING FROM CAPTAIN SIDE SPEEDTAPE WAS PEELING OFF. C/W VISUAL INSP FWD AREA OF AIRCRAFT. FOUND SPEED TAPE DAMAGE
- [SDR SIMA2018100503003](https://openairdocs.org/sdr/SIMA2018100503003), Oct 3, 2018: BRAKE SYS. CONTAMINATED. WHEN APPLYING LIGHT BRAKE PRESSURE, BRAKES WOULD GRAB EXTREMELY HARD. THIS OCCURRED ON BOTH THE CA & FO SIDE BRAKES. AT TIME OCCURRENCE, BRAKE TEMPERATURES WERE
- [SDR SIMA201809264006](https://openairdocs.org/sdr/SIMA201809264006), Sep 24, 2018: ALTIMETER. MALFUNCTIONED. IN CRUISE AT FL360 STANDBY ALTIMETER INDICATED 450 FT TO 500 FT LOWER THAN CAPTAINS AND F/O'S ALTIMETERS. DIFFERENCE NORMALIZED DURING DESCENT.-C/A-RAR ISIS IAW
- [SDR SIMA201806186003](https://openairdocs.org/sdr/SIMA201806186003), Jun 16, 2018: SEAL. OUT OF ADJUST. MAIN CABIN DOOR SQUEALING DURING CLIMB, UNTIL APPROX 5.5 PSI CABIN PRESSURE, ALSO CONTINUED DURING DECENT. THE MAIN DOOR RUBBER TRIM SEAL ADJUSTED IAW AMM 52-00
- [SDR SIMA20171026002](https://openairdocs.org/sdr/SIMA20171026002), Oct 26, 2017: LIGHT. INOPERATIVE. PAX DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECKED GOOD.
- [SDR SIMA20170103001](https://openairdocs.org/sdr/SIMA20170103001), Jan 3, 2017: ICU. FAILED. TCAS FAILED ON BOTH PFDS IN ENROUTE. REMOVED AND REPLACED 1 ICU IAW AMM 23-00-01. OPS CHECKED GOOD IAW AMM 34-43-00 .
- [SDR SIMA20161218002](https://openairdocs.org/sdr/SIMA20161218002), Dec 18, 2016: FCU. MALFUNCTIONED. LOST FLAP INDICATIONS ON EICAS AND RMU, USED MARKS ON FLAPS TO DETERMINE POSITION OF FLAPS UP TO 22, 22-45 NOT VISIBLE. REMOVED AND REPLACED FECU IAW AMM 27-53-
- [SDR SIMA20160922001](https://openairdocs.org/sdr/SIMA20160922001), Sep 22, 2016: FLASHLIGHT ASSY. INOPERATIVE. OVER F/A JUMPSEAT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW CHECKLIST. OPS CHECKED GOOD.
- [SDR SIMA20160902001](https://openairdocs.org/sdr/SIMA20160902001), Sep 2, 2016: SMOKE WARNING. FALSE ACTIVATION. BAGGAGE SMOKE INDICATION IN FLIGHT. INSPECTED BAGGAGE BAY SMOKE DETECTORS IAW FIM 26-15-00-810-805-A. NO DEFECTS NOTED. R & R BOTH BAGGAGE BAY FIRE BOTTLES IAW 
- [SDR SIMA20160731002](https://openairdocs.org/sdr/SIMA20160731002), Jul 31, 2016: FLASHLIGHT. BROKEN. F/O FLASHLIGHT ON/OFF SWITCH BROKEN, REPLACED F/O FLASHLIGHT IAW AMM TASK 33-50-16. OPS CHECK GOOD.
- [SDR SIMA20160717002](https://openairdocs.org/sdr/SIMA20160717002), Jul 17, 2016: POWER SUPPLY. INOPERATIVE. NR 4 & 5 EMRGENCY LIGHTS, EXIT MARKER, AND EXIT IDENTTIFIER INOPERATIVE. R & R NR 3 EMERGENCY LIGHTING SYSTEM POWER SUPPLY IAW W/C 33-700-19. OPS CHECKED GOOD I

All 119: https://openairdocs.org/aircraft/N831AE/reports.md

## STCs that may be installed (OpenAirDocs) (55, 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-135KL)

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST02176AT-D](https://openairdocs.org/stc/ST02176AT-D): Installation of a Teledyne Mini Flight Data Acquistion Unit. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST02310AT](https://openairdocs.org/stc/ST02310AT): Installation of SAF-T-GLO photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC 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 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 ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC 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 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 ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [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 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 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 ST04367AT](https://openairdocs.org/stc/ST04367AT): Removal of the Existing Honeywell DL-900 or DL-950 Data Loader and Installation of the Honeywell DL-1000 Data Loader. Chippewa Aerospace Inc
- [STC ST04190AT](https://openairdocs.org/stc/ST04190AT): Installation of an ADS-B Out. Chippewa Aerospace Inc
- [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST04282AT](https://openairdocs.org/stc/ST04282AT): Installation of the Honeywell DU-875 LCD Flight Display. Chippewa Aerospace Inc
- [STC ST04015AT](https://openairdocs.org/stc/ST04015AT): Installation of the Honeywell NZ-2000 FMS/GPS System with or without WAAS/LPV. Chippewa Aerospace Inc
- [STC ST04191AT](https://openairdocs.org/stc/ST04191AT): Installation of the Honeywell Sky Connect Tracker Iridium Satcom System. Chippewa Aerospace Inc
- [STC ST02524LA](https://openairdocs.org/stc/ST02524LA): Installation of TCAS version 7.0. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST03483AT](https://openairdocs.org/stc/ST03483AT): Installation of a Portable Beverage Dispensing System, P/N B43-FA-001. Dynamo Beverage Company, USA, L.L.C
- [STC ST03999AT](https://openairdocs.org/stc/ST03999AT): Installation of a Single Honeywell HF-1050 HF Communication System. Chippewa Aerospace Inc
- [STC ST01619CH](https://openairdocs.org/stc/ST01619CH): Installation of a Lavatory Service Shutoff Valve. AeroControlex Group TransDigm Inc
- [STC ST03994AT](https://openairdocs.org/stc/ST03994AT): Installation of Bleed Air Coupling Sleeve Kit. Seal Dynamics
- [STC ST02638AT](https://openairdocs.org/stc/ST02638AT): Installation of an improved aircraft toilet rinse/fill shutoff valve and asociated hardware. Parker Hannifin Corporation, Parker Aerospace
- [STC ST03890AT](https://openairdocs.org/stc/ST03890AT): Installation of an L-3 Communications Micro Quick Access Recorder (MQAR). Chippewa Aerospace, Inc
- [STC ST02882CH-D](https://openairdocs.org/stc/ST02882CH-D): Installation of a Honeywell Flight Management System (FMS #2). Standard Aero
- [STC ST02803CH-D](https://openairdocs.org/stc/ST02803CH-D): Installation of a Honeywell KHF-1050 system. Standard Aero
- [STC ST01008LA-D](https://openairdocs.org/stc/ST01008LA-D): Installation of Hollingsead International Sentry One Cabin Mounted Video Camera System. Audio International

All 55: https://openairdocs.org/aircraft/N831AE/stcs.md

## Related

- Other Embraer EMB-135KL aircraft: https://openairdocs.org/model/embraer-emb-135kl/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.