# N830AE: 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: 145615
- 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: AB585F
- 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=830AE
- Page: https://openairdocs.org/aircraft/N830AE

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/N830AE/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 N830AE.

## 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.

- [Incident 20041129029259I](https://openairdocs.org/incident/20041129029259I), Nov 29, 2004: Emb EMB135KL (N830AE), Fayetteville, AR. (-23) On November 29, 2004, at approximately 1900 CDT, Emb-135, N830AE, on a flight operated by American eagle airlines, experienced a cabin disturbance when…

## Service difficulty reports (94, 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 SIMA202001132006](https://openairdocs.org/sdr/SIMA202001132006), Jan 12, 2020: LIGHT. INOPERATIVE. MAIN DOOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED DOOR EMERGENCY LIGHT I.A.W EMB 140 AMM 33-50-10 OPS CHECK GOOD
- [SDR SIMA201911297002](https://openairdocs.org/sdr/SIMA201911297002), Nov 27, 2019: CONTROL PANEL. FAILED. PTCH TRIM BACK UP INOP DURING CRUSING. PITCH TRIM FAIL MSG. DECLARED EMERG. LANDED SAFELY-C/A-RAR PITCH TRIM CONTROL PANEL IAW EMB 140 AMM 20-13-10. OPC GOOD IA
- [SDR SIMA201910286002](https://openairdocs.org/sdr/SIMA201910286002), Oct 26, 2019: BRAKE. UNKNOWN. PARKING BRAKE IS NOT WORKING PROPERLY. DIFFICULTY SETTING IT-C/A-PERFORMED OPC OF PARKING EMERGENCY BRAKE IAW EMB 140 AMM 32-44-00. OPC GOOD. NO FURTHER DEFECTS
- [SDR SIMA201910232002](https://openairdocs.org/sdr/SIMA201910232002), Oct 22, 2019: NONE. NONE. BIRD STRIKE ON T/O ROLL ON NOSE CONE AN 2 RH WING LEADING EDGE HIGH SPEED ABORT LESS THAN 110 KT-C/A-C/W BIRD STRIKE INSPECTION WORK CARD 05-200-07 NO DAMAGE NO
- [SDR SIMA20190906001](https://openairdocs.org/sdr/SIMA20190906001), Sep 6, 2019: BATTERY. DISCHARGED. AFT FLASHLIGHT INOP. C/A-REMOVED AND REPLACED AFT FLASHLIGHT BATTERY IAW CMM 25-60-11 OPC GOOD.
- [SDR SIMA20190904002](https://openairdocs.org/sdr/SIMA20190904002), Sep 4, 2019: O-RING. DAMAGED. AT 19000 FT DURING ICE PROT PNEUMATIC TEST, BLD 2 LEAK / FA REPORTS LOUD BANG. QRH CLEARED MSG. C/A-REMOVED AND REPLACED RT BLEED JOINT NR 2 O-RING AND REASSEMB
- [SDR SIMA201908221003](https://openairdocs.org/sdr/SIMA201908221003), Aug 21, 2019: CONTROL UNIT. FAILED. FLAP FAIL ON EICAS CAUTION MESSAGE AFTER SELECTING FLAPS 9 FLAPS STAYED UP. RESET FLAPS SYSTEM IAW FIM TASK 27-51-00-810-801-A, RECEIVED FLAPS AT 9 DEGREES FOR 
- [SDR SIMA201908221004](https://openairdocs.org/sdr/SIMA201908221004), Aug 21, 2019: WARNING MESSAGE. FALSE ACTIVATION. FLAP FAIL MSF WHEN SELECTING FLAPS 22. RESET SYSTEM C/W OPERATIONAL CHECK IAW E140 AMM 27-51-00-700-801-A. NO FAULTS FOUND. A/C OK FOR SERVICE
- [SDR SIMA20190528001](https://openairdocs.org/sdr/SIMA20190528001), May 28, 2019: FLASHLIGHT. BROKEN. AFT CABIN CREW FLASHLIGHT BASE BROKEN. C/A-REMOVED AND REPLACED CABIN CREW FLASHLIGHT BASE IAW AMM 33-50-16. OPC GOOD.
- [SDR SIMA201809054001](https://openairdocs.org/sdr/SIMA201809054001), Sep 4, 2018: BLEED VALVE. MALFUNCTIONED. ADVISORY MESSAGE BLD 2 VLV CLOSED. REMOVED AND REPLACED ENGINE BLEED 2 VALVE IAW AMM 36-11-05. REMOVED AND REPLACED BLEED AIR NR 2 PUSHBUTTON IAW AMM 20-13-04. 
- [SDR SIMA20180628002](https://openairdocs.org/sdr/SIMA20180628002), Jun 28, 2018: HYDRAULIC LINE. FAILED. HYDRAULIC SYSTEM 1 LOW QUANTITY FOLLOWED BY A RAPID LOSS OF HYDRAULIC FLUID. TRANSFERRED HYDRAULIC FLUID FROM SYS 2 TO SYS 1 IAW ETN-EM-29-023R2. FOUND LT AND R
- [SDR SIMA2018061108008](https://openairdocs.org/sdr/SIMA2018061108008), Jun 8, 2018: SELECTOR. FAILED. FLAP INDICATION WHEN SET IN ANY POSITION. COMPLETED A FLAP FAIL CHECKLIST AND PERFORMED NO FLAP LANING. AFTER LANDING FLAPS INDICATED 0 IN FLAPS 22 POSITION. FL
- [SDR SIMA20180130007](https://openairdocs.org/sdr/SIMA20180130007), Jan 30, 2018: WIRE. BROKEN. EMERGENCY LIGHT CONNECTOR HAS A BROKEN WIRE. REPAIRED THE WIRE IAW SWPM 20-00-03, AND 20-21-00.
- [SDR SIMA20180130004](https://openairdocs.org/sdr/SIMA20180130004), Jan 30, 2018: SKIN. CRACKED. FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 6 FASTENERS ON FR 78 RT SIDE BELOW VERTICAL STAB. REPAIRED FUSELAGE SKIN CRACKS ON 6 FASTENERS ON FR78 IAW ERS-EM-53MR-
- [SDR SIMA20180130002](https://openairdocs.org/sdr/SIMA20180130002), Jan 30, 2018: FRAME. DENTED. DENT ON RT FWD FUSELAGE STRINGER 14R AFT OF RADOME. REPAIRED DENT ON RT FWD FUSELAGE STRINGER 14R AFT OF RADOME IAW ERS-EM-53MR-3107.
- [SDR SIMA20180123011](https://openairdocs.org/sdr/SIMA20180123011), Jan 23, 2018: SUPPORT. CRACKED. LT OMEGA BEAM OUTBOARD SUPPORT IS CRACKED BETWEEN FRAMES 47-48. REPAIRED LEFT OMEGA BEAM OUTBOARD SUPPORT BETWEEN FRAMES 47-48 IAW SRM 53-23-10.
- [SDR SIMA20180122001](https://openairdocs.org/sdr/SIMA20180122001), Jan 22, 2018: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM IS CORRODED AT FRAME 59. REPAIRED THE OMEGA BEAM IAW EO-EM-53MR-1518, REV 3.
- [SDR SIMA20180122003](https://openairdocs.org/sdr/SIMA20180122003), Jan 22, 2018: FLOOR SUPPORT. CORRODED. CENTER OMEGA BEAM IS CORRODED AT FRAME 59. REPAIRED THE OMEGA BEAM IAW EO-EM-53MR-1518, REV 3.
- [SDR SIMA20180122002](https://openairdocs.org/sdr/SIMA20180122002), Jan 22, 2018: STOP FITTING. CRACKED. SERVICE DOOR FORWARD LOWER STOP BRACKET IS CRACKED. REMOVED AND REPLACED THE SERVICE DOOR FORWARD LOWER STOP BRACKET IAW SRM 51-40-02.
- [SDR SIMA20180122004](https://openairdocs.org/sdr/SIMA20180122004), Jan 22, 2018: SKIN. CRACKED. FUSELAGE SKIN CRACKED, FRAME 77 AND 78. REPAIRED THE SKIN IAW ERS-EM-53MR-3709.
- [SDR SIMA20180117005](https://openairdocs.org/sdr/SIMA20180117005), Jan 17, 2018: STRINGER. DAMAGED. STRINGER 13L DAMAGED BETWEEN FRAMES 48 AND 50. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-02, AND 51-20-01
- [SDR SIMA20180117004](https://openairdocs.org/sdr/SIMA20180117004), Jan 17, 2018: DOOR SILL. CORRODED. CARGO DOOR SILL IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02
- [SDR SIMA20180117002](https://openairdocs.org/sdr/SIMA20180117002), Jan 17, 2018: SKIN. CRACKED. FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R. REPAIRED THE SKIN IAW SRM 53-31-01
- [SDR SIMA20180117001](https://openairdocs.org/sdr/SIMA20180117001), Jan 17, 2018: RIB. CRACKED. LEFT ELEVATOR NOSE RIB ON INBOARD HINGE CUTOUT INBOARD SIDE CRACKED. REMOVED AND REPLACED THE RIB IAW SRM 51-40-02
- [SDR SIMA20171212008](https://openairdocs.org/sdr/SIMA20171212008), Dec 12, 2017: SUPPORT. CRACKED. RIGHT OMEGA BEAM INBD SUPPORT IS CRACKED BETWEEN FRAMES 47 - 48. REMOVED AND REPLACED THE SUPPORT IAW SRM 53-23-02.
- [SDR SIMA20171212009](https://openairdocs.org/sdr/SIMA20171212009), Dec 12, 2017: CROSSMEMBER. CORRODED. CENTER AISLE CROSSMEMBER CORRODED BETWEEN FRAMES 33-34. REMOVED AND REPLACED THE CROSSMEMBER IAW SRM 51-40-02, SRM 51-20-01, AND ETN-EM-53-241.
- [SDR SIMA20171212010](https://openairdocs.org/sdr/SIMA20171212010), Dec 12, 2017: CROSSMEMBER. CORRODED. CENTER AISLE CROSSMEMBER CORRODED BETWEEN FRAMES 24-25. REMOVED AND REPLACED THE CENTER AISLE CROSSMEMBER IAW SRM 51-40-02, SRM 51-20-01, AND ETN-EM-53-241.
- [SDR SIMA20160629006](https://openairdocs.org/sdr/SIMA20160629006), Jun 29, 2016: HOLDER. BROKEN. F/O'S FLASHLIGHT HOLDER BROKEN. REMOVED AND INSTALLED F/O'S FLASHLIGHT CRADLE IAW AMM 33-50-16.
- [SDR SIMA20160620003](https://openairdocs.org/sdr/SIMA20160620003), Jun 20, 2016: LEVER. DEFECTIVE. BAGGAGE DOOR WARNING SYS MFD/EICAS, BAGGAGE DOOR WARNING ILLUMINATED AFTER TAKEOFF AND EXTINGUISHED AFTER LANDING. RESTORATION OF MEL ITEMS REVIEW THE MEL AND E
- [SDR SIMA20160402001](https://openairdocs.org/sdr/SIMA20160402001), Apr 2, 2016: LEVER. DEFECTIVE. ON ROLL OUT AT 80KTS, RECEIVED ADVISORY CARGO DOOR OPEN. TAKEOFF ABORTED. RETURNED TO GATE. GND PERSONNEL REVISED DOOR. DOOR INDICATION ON MFD FLICKERING GREEN 
- [SDR SIMA20160211003](https://openairdocs.org/sdr/SIMA20160211003), Feb 11, 2016: SMOKE DETECTOR. FAILED. BAGGAGE COMPARTMENT SMOKE DETECTOR FAILS FIRE TEST. R & R BAGGAGE COMPARTMENT FWD SMOKE DETECTOR IAW AMM 26-15-01. OPERATIONAL CHECKED GOOD.
- [SDR SIMA20160118003](https://openairdocs.org/sdr/SIMA20160118003), Jan 18, 2016: LIGHT. INOPERATIVE. LEFT OVERWING EMER LIGHT INOPERATIVE. R & R LT OVERWING EMER LIGHT LAMP IAW AMM 33-50-07. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150726001](https://openairdocs.org/sdr/SIMA20150726001), Jul 26, 2015: PROXIMITY SENSOR. FAILED. SPOILER FAIL MSG PRESENTED. SPOILERS SHOWED OPEN INTERMITTENTLY. RAN INADVERTENT SPOILER OPEN IN FLIGHT CHECKLIST. FLIGHT ATTENDANT DID NOT OBSERVE OPEN SPOILER
- [SDR SIMA20150623004](https://openairdocs.org/sdr/SIMA20150623004), Jun 23, 2015: WARNING SYSTEM. ACTIVATED. HYDRAULIC SYS 1 LO LEVEL IN FLIGHT. LEVEL 3/4 FULL ON GND & AT CRUSE. DECREASED INTO AMBER. HYD LO LEVEL ON EICAS, SUSPECT LEAK. TRANSFERRED HYD FLUID IAW ETN E
- [SDR SIMA20150426001](https://openairdocs.org/sdr/SIMA20150426001), Apr 26, 2015: LIGHT. INOPERATIVE. IAW PS1 CHECK, RT EXTERNAL EMER LIGHT IS INOPERATIVE. REMOVED & INSTALLED RT EXTERNAL EMER LIGHT IAW AMM 33-50-10.
- [SDR SIMA20150408005](https://openairdocs.org/sdr/SIMA20150408005), Apr 8, 2015: WIRE. PULLED. LAST EMER LIGHT PROXIMITY STRIP AFT WIRES PULLED FROM SPLICES. R & R SPLICES SP 9502 & SP 9503 IAW SWPM 20-21-00. EMER LIGHT STRIP OPERATIONS CHECKED GOOD IAW A
- [SDR SIMA20140815001](https://openairdocs.org/sdr/SIMA20140815001), Aug 15, 2014: DOOR. LACK OF LUBE. FLIGHT ATTENDANT REPORTS CABIN ENTRY DOOR IS HARDER TO OPERATE WHEN OPENING. CLEAN & LUBED MAIN CABIN DOOR. OPERATIONS CHECKED GOOD IAW SP.
- [SDR SIMA20140724004](https://openairdocs.org/sdr/SIMA20140724004), Jul 24, 2014: CONTROL MODULE. FAULTY. ON TAXI GOT APU FIRE EICAS WHILE APU WAS OFF. PRESSED APU EXT BUTTON IAW CHECK LIST. MSG EXTINGUISHED THEN REAPPEARED & EXTINGUISHED AGAIN. R & R APU FIRE DETEC
- [SDR SIMA20140718001](https://openairdocs.org/sdr/SIMA20140718001), Jul 18, 2014: SKIN. CRACKED. DURING IMBV INSPECTION, QA FOUND LT AFT FUSELAGE FASTENER HOLE CRACKED AT FRAME 75 STRINGER 2 AREA. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE 
- [SDR SIMA20140714005](https://openairdocs.org/sdr/SIMA20140714005), Jul 14, 2014: FRAME. CRACKED. DURING IMBV INSPECTION, QA FOUND FRAME 23 CRACKED BETWEEN STRINGER 15R - 16R. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AF
- [SDR SIMA20140628017](https://openairdocs.org/sdr/SIMA20140628017), Jun 28, 2014: WIRE. BROKEN. ONE PROX LIGHT WITH ARROWS & ONE PROX LIGHT WITHOUT ARROWS HAVE BROKEN WIRES AT PROX LIGHT. R & R IAW AMM 33-50-12. SEE NRTC BOW 159263 FOR FINAL INSTALL & OPER
- [SDR SIMA20140628011](https://openairdocs.org/sdr/SIMA20140628011), Jun 28, 2014: SKIN. CRACKED. AFT UPPER LT EXTERNAL FUSELAGE SKIN CRACKED AT RIVET FRAME 77. REPAIRED DAMAGE BY INSTALL BUSHING & FILET SEALED IAW ERS-EM-5300-562. SEE TURNOVER FOR DETAILS.
- [SDR SIMA20140628008](https://openairdocs.org/sdr/SIMA20140628008), Jun 28, 2014: LIGHT. INOPERATIVE. NUMBER 1 AISLE EMER LIGHT STRIP NOT WORKING. R & R NR 1 AISLE EMER FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12. SEE BOW 159263 TASK NR 1 FOR OPERATIONAL CHECK.
- [SDR SIMA20140628009](https://openairdocs.org/sdr/SIMA20140628009), Jun 28, 2014: WIRE. BROKEN. FORWARD PROXIMITY LIGHT STRIP WIRE BROKEN AT SPLICE CONNECTOR. REPAIRED FWD PROXIMITY LIGHT STRIP WIRE AT SPLICE CONNECTOR IAW SWPM 20-21-00 STEP 6.
- [SDR SIMA20140628015](https://openairdocs.org/sdr/SIMA20140628015), Jun 28, 2014: FLANGE. CORRODED. RIGHT LE NR 2 OTBD MACHINED FLANGE IS CORRODED. REPAIRED IAW ERS-EM-5700-182. SEE TURNOVER FOR DETAILS.
- [SDR SIMA20140628014](https://openairdocs.org/sdr/SIMA20140628014), Jun 28, 2014: SUPPORT. CRACKED. CABIN RT FLOORBEAM OTBD SUPPORT CRACKED AT WING BOX BETWEEN FRAME 47 & 48. REMOVED RT CABIN OMEGA BEAM TO WING BOX OTBD SUPPORT ANGLE & DRILLED FASTENER HOLES I
- [SDR SIMA20140628013](https://openairdocs.org/sdr/SIMA20140628013), Jun 28, 2014: SKIN. CRACKED. AFT UPPER RT EXTERNAL FUSELAGE SKIN CRACKED AT RIVET FRAME 78. REPAIRED DAMAGE BY INSTALLING BUSHING IAW ERS-EM-5300-563. SEE TURNOVER FOR DETAILS.
- [SDR SIMA20140628012](https://openairdocs.org/sdr/SIMA20140628012), Jun 28, 2014: SPLICE PLATE. CRACKED. GALLEY UNDERFLOOR FWD TO AFT DIGITAL SPLICE REINFORCEMENT CRACKED AT LT FLOORBEAM. R & R SPLICE PLATE IAW SRM 51-30-01, 51-40-02 & GPM 17-13. SEE WIPS & TASKS F
- [SDR SIMA20140628016](https://openairdocs.org/sdr/SIMA20140628016), Jun 28, 2014: FRAME. CRACKED. RIGHT AFT FUSELAGE FRAME 75 FASTENER HOLE CRACKED STRINGER 3 AREA MARKED. REPAIRED DAMAGE AT RT AFT FUSELAGE BY INSTALLING BUSHING IAW ERS-EM-5300-575. SEE TURN
- [SDR SIMA20140628010](https://openairdocs.org/sdr/SIMA20140628010), Jun 28, 2014: SKIN. CRACKED. AFT UPPER RT EXTERNAL FUSELAGE SKIN CRACKED AT RIVET FRAME 79 MARKED. REAMED FASTENER HOLE ON AFT UPPER RT EXTERNAL FUSELAGE SKIN AT FRAME 79 BETWEEN STRINGER 3

All 94: https://openairdocs.org/aircraft/N830AE/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/N830AE/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

---
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