# N810AE: 2001 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: 145525
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 1, 2001
- Certificate issued: January 24, 2023
- Expires: January 31, 2030
- Mode S code: AB0961
- 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=810AE
- Page: https://openairdocs.org/aircraft/N810AE

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/N810AE/ads.md

## Information bulletins (advisory) (10 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB AIR-20-17](https://openairdocs.org/saib/AIR-20-17): Air Conditioning - Cabin Pressure Control System. Issued Nov 3, 2020
- [SAIB NM-19-17](https://openairdocs.org/saib/NM-19-17): Ice and Rain Protection: Electrical Wiring Terminations at Pitot and TAT Relays. Issued Dec 5, 2019
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008
- [SAIB NM-08-15](https://openairdocs.org/saib/NM-08-15): Instruments: Contamination of the Attitude Heading Reference System (AHRS) Computers. Issued Mar 26, 2008
- [SAIB NM-07-40](https://openairdocs.org/saib/NM-07-40): Embraer EMB-135/145 Landing Gear Incident. Issued Jul 9, 2007
- [SAIB NM-07-20](https://openairdocs.org/saib/NM-07-20): Flight Data Recorders. Issued Mar 21, 2007
- [SAIB NE-11-22](https://openairdocs.org/saib/NE-11-22): Engine Controls. Issued Feb 23, 2011
- [SAIB CE-00-18](https://openairdocs.org/saib/CE-00-18): . Issued Mar 30, 2000
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB IAD04LA050](https://openairdocs.org/ntsb/IAD04LA050), Aug 29, 2004: Embraer EMB-135KL (N810AE), Clyde, NY, no damage. Probable cause: An unexpected encounter with clear air turbulence.

## FAA accident and incident reports (3)

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 20110525011209I](https://openairdocs.org/incident/20110525011209I), May 25, 2011: Embraer EMB-135KL (N810AE), Detroit, MI, No damage. On 5/25/11 aircraft N810AE from ord to abe, climbing out of ord at about flight level 2800, the first officer and pilot-in-command smelled a strong oder of…
- [Incident 20061027023639I](https://openairdocs.org/incident/20061027023639I), Oct 27, 2006: Emb EMB135KL (N810AE), Louisville, KY. (-23) On Friday 10/27/06 American eagle N810AE, flight 3980, departed sdf enroute to ord with 43 passengers on board, in-flight they had a thrust reverser…
- [Accident 20040829021469A](https://openairdocs.org/incident/20040829021469A), Aug 29, 2004: Emb EMB135KL (N810AE), Albany, NY. (-23) Enroute to bos from yyz, flight 4568 experienced severe turbulence which caused the flight attendant to fall and be injured by the galley cart when it…

## Service difficulty reports (98, 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 SIMA2020021231005](https://openairdocs.org/sdr/SIMA2020021231005), Jan 31, 2020: LIGHT. UNKNOWN. INSIDE MAIN CABIN THE #1 AND #2 EMERGENCY LIGHTING FLOOR PROXIMITY STRIPS DO NOT ILLUMINATE-C/A-PERFORMED OPC OF EMERGENCY LIGHTING SYSTEM IAW EMB 140 AMM 33-50
- [SDR SIMA202001164002](https://openairdocs.org/sdr/SIMA202001164002), Jan 14, 2020: SMOKE WARNING. FALSE ACTIVATION. BAGG SMOKE WARNING ON GROUND EICAS MSG ANG BAGG EXTG BUTTON ILLUMINATED-C/A-PERFORMED FIRE DETECTION TEST IAW EMB 140 AMM 26-10-00. ALL MESSAGES CLEARED. OPS CH
- [SDR SIMA201910287002](https://openairdocs.org/sdr/SIMA201910287002), Oct 27, 2019: FAN. FAILED. ELECTRICAL SMELL IN FLIGHT DECK "TRANSFERRED TO NRWC 810-DFW-02773"-C/A-REMOVED AND REPLACED # 2 FWD ELECK COMPT COOLING FAN IAW AMM 21-26-02. OPCK GOOD. PERFOR
- [SDR SIMA2019100193003](https://openairdocs.org/sdr/SIMA2019100193003), Sep 30, 2019: PRECOOLER. FAILED. BLEED 2 LEAK LEAK AFTER TAKEOFF AT TAKEOFF POWER @ 500' AGL. PERFORMED BLLED AIR SYSTEM LEAK CHECK IAW WORK CARD 36-700-06, AND REPLACED ORING AT RH BLEED JOINT
- [SDR SIMA2019100193002](https://openairdocs.org/sdr/SIMA2019100193002), Sep 30, 2019: O-RING. LEAKING. BLD 2 LEAK IMMEDIATLY AFTER TAKE OFF. REMOVED AND REPLACED THE O-RINGS AT JOINT 4 AND JOIMT 20 IAW AMM 36-11-00. PERFORMED A LEAK CHECK AND FOUND SATISFACTORY I
- [SDR SIMA20190929002](https://openairdocs.org/sdr/SIMA20190929002), Sep 29, 2019: O-RING. DAMAGED. BLD 2 LEAK IMMEDIATELY AFTER TAKEOFF. WAS NOT AN OVERWEIGHT LANDING.-C/A- REMOVED AND REPLACED O-RING AT JOINT NUMBER 26 AND 4 IAW AMM 36-11-10. PERFORMED LEAK 
- [SDR SIMA20190707001](https://openairdocs.org/sdr/SIMA20190707001), Jul 7, 2019: O-RING. DAMAGED. SUPPLEMENTAL BLEED 2 LEAK WARNING. C/A-FOUND LEAKING CONNECTION AT BLEED LINE #18 JOINT. REMOVED AND REPLACED #2 SYSTEM BLEED LINE O-RINGS AT #18 CONNECTION IAW
- [SDR SIMA201906254003](https://openairdocs.org/sdr/SIMA201906254003), Jun 24, 2019: O-RING. LEAKING. BLEED 2 LEAK DURING CLIMBOUT. AFTER INSPECTION OF DUCT LINES, FOUND 12 AND 22 TO BE DAMAGED AND LEAKING IAW AMM 36-11-09. R & R THE DUCTS 12 AND 22 O-RINGS IAW 
- [SDR SIMA2019062016002](https://openairdocs.org/sdr/SIMA2019062016002), Jun 16, 2019: GPS. MALFUNCTIONED. UNRELIABLE NAV INFORMATION IN FLIGHT BETWEEN FO X CA MFD FMS AND GPS. RESET AND PERFORMED OPC CHECK OF FMS/GPS IAW AMM 34-62-00. OPC CHECK GOOD. NO FAULTS NOTED
- [SDR SIMA201906176001](https://openairdocs.org/sdr/SIMA201906176001), Jun 16, 2019: FMS. MALFUNCTIONED. UNRELIABLE NAV INFORMATION IN FLIGHT BETWEEN FO X CA MFD FMS AND GPS-C/A-RESET AND PERFORMED OPC CHECK OF FMS/GPS IAW AMM 34-62-00. OPC CHECK GOOD. NO FAULTS NO
- [SDR SIMA201906132006](https://openairdocs.org/sdr/SIMA201906132006), Jun 12, 2019: LIGHT. INOPERATIVE. EMERGENCY LIGHT STRIP INOPERATIVE AT ROWS 7-8. REMOVED AND REPLACED PROXIMITY LIGHT STRIP ON ROW 7-8 IAW AMM 33-50-122. OPS CHECKED GOOD. NO DEFECTS NOTED.
- [SDR SIMA201906132005](https://openairdocs.org/sdr/SIMA201906132005), Jun 12, 2019: FAN. FAILED. ELECTRICAL ODOR AND VISABLE HAZE IN CABIN REPORTED BY FA AND PAX. DIMINISHED ONCE RECIRC AND PACKS OFF.-C/A-PERFORMED OPERATIONAL CHECK OF THE AIR CONDITIONING 
- [SDR SIMA20190514001](https://openairdocs.org/sdr/SIMA20190514001), May 14, 2019: FLASHLIGHT. INOPERATIVE. AFT CABIN CREW FLASHLIGHT INOP. C/A-REMOVED AND REPLACED AFT CABIN CREW FLASHLIGHT IAW AMM 33-50-16 STEPS 2.I.(1) AND 3.H.(4). OPC GOOD.
- [SDR SIMA20190314001](https://openairdocs.org/sdr/SIMA20190314001), Mar 14, 2019: AMPLIFIER. DAMAGED. CABIN AND CABIN EMERG BUTTON LIT UP IN CRUISE FLIGHT WAS NOT ABLE TO MAKE PA'S NO CHIMES/SOUNDS WITH NO SMOKING AND SEAT BELT SIGN SWITCH BEING TOGGLED. C/A-REM
- [SDR SIMA20190205005](https://openairdocs.org/sdr/SIMA20190205005), Feb 5, 2019: PROXIMITY SENSOR. FAILED. DECLARED EMERGENCY AFTER SPOILER FAIL MESSAGE IN FLIGHT AT FL360 WENT AWAY AND BACK 5 TIMES UNTIL EMERGENCY XLIST COMPLETE AND CBS PULLED. OPEN INSCRIPTION ON E
- [SDR SIMA20181023001](https://openairdocs.org/sdr/SIMA20181023001), Oct 23, 2018: LIGHT. INOPERATIVE. RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED RT AFT OVERWING EMERGENCY EXIT LIGHT BULB IAW AMM 33-50-07. OPS CHECK GOOD.
- [SDR SIMA2018091008001](https://openairdocs.org/sdr/SIMA2018091008001), Sep 8, 2018: CHARGER. FAILED. CABIN FLOOR EMER LIGHT 1,2 & 3 INOP. R&R NR 2 BATT PACK AND CHARGER IAW AMM 33-50-04. OP CK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 84695.
- [SDR SIMA201809043002](https://openairdocs.org/sdr/SIMA201809043002), Sep 3, 2018: LIGHT. INOPERATIVE. LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT IAW AMM 33-50-07. OPS CHECK GOOD.
- [SDR SIMA2018082019005](https://openairdocs.org/sdr/SIMA2018082019005), Aug 19, 2018: LIGHT. INOPERATIVE. SECOND EMERGENCY PROXIMITY STRIP FROM MAIN ENTRANCE TO SEAT 3A INOPERATIVE. REMOVED AND REPLACED EMERGERCY LIGHT IAW AMM 33-57-12. OPS CHECKED GOOD.
- [SDR SIMA2018080131001](https://openairdocs.org/sdr/SIMA2018080131001), Jul 31, 2018: ANTENNA. FAILED. LIGHTNING STRIKE AT 16,000 FEET IN CRUISE CLEAN CONFIGURATION ARCED ACROSS NOSE OF AIRPLANE LOST COMMS 1+2 OR THE REGAINED COMM 1. COMM 2 IS RECEIVE ONLY OR WON
- [SDR SIMA201807132003](https://openairdocs.org/sdr/SIMA201807132003), Jul 12, 2018: UNKNOWN. MALFUNCTIONED. FUEL QUANTITY INDICATION ON BOTH ENGINES AND TOTAL FUEL INDICATED INCREASED AND DECREASED UP TO 900 POUNDS. THE FUEL IMBALANCE MESSAGE APPEARED AND DISAPPEARED 
- [SDR SIMA201806186001](https://openairdocs.org/sdr/SIMA201806186001), Jun 16, 2018: SWITCH. OUT OF ADJUST. ABORTED TAKEOFF BELOW V1, DUE TO A CARGO DOOR OPEN EICAS MESSAGE. ADJUSTED THE CARGO DOOR WARNING SWITCHES IAW AMM 52-76-01. OPS CHECKED GOOD.
- [SDR SIMA20180301002](https://openairdocs.org/sdr/SIMA20180301002), Mar 1, 2018: WIRE. BROKEN. FLOOR EMERGENCY LIGHT STRIP ASSEMBLY AT 261BF HAS A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20180227003](https://openairdocs.org/sdr/SIMA20180227003), Feb 27, 2018: SKIN. DAMAGED. DOOR EXTERNAL SKIN HAS 1 DENT APPROX. 2 INCHES, FRONT FWD EDGE AND 6 INCHES FROM UPPER EDGE. SKIN IS BENT AND KNIFE EDGED APPROXIMATELY 8 INCHES FROM UPPER EDGE
- [SDR SIMA20180219004](https://openairdocs.org/sdr/SIMA20180219004), Feb 19, 2018: DOOR SILL. CORRODED. CARGO DOOR SILL IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE CARGO DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA20180219003](https://openairdocs.org/sdr/SIMA20180219003), Feb 19, 2018: DOOR SILL. CORRODED. SERVICE DOOR SILL IS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA20180218005](https://openairdocs.org/sdr/SIMA20180218005), Feb 18, 2018: WIRE. BROKEN. LEFT NR 3 EMERGENCY LIGHT STRIP HAS A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20180218006](https://openairdocs.org/sdr/SIMA20180218006), Feb 18, 2018: FRAME. CRACKED. RIGHT FRAME 10 CRACKED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.
- [SDR SIMA20180218007](https://openairdocs.org/sdr/SIMA20180218007), Feb 18, 2018: FRAME. CRACKED. LEFT FRAME 10 CRACKED. REMOVED AND REPLACED THE FRAMEIAW SRM 51-40-02.
- [SDR SIMA20180218004](https://openairdocs.org/sdr/SIMA20180218004), Feb 18, 2018: WIRE. BROKEN. LEFT NR 7 EMERGENCY LIGHT HAS A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20180217015](https://openairdocs.org/sdr/SIMA20180217015), Feb 17, 2018: WEB. CHAFED. LEFT OVERWING EMERGENCY EXIT INTERNAL WEB CHAFED ABOVE WINDOW CUTOUT. REPAIRED IAW ERS-EM-52MR-854
- [SDR SIMA20180214004](https://openairdocs.org/sdr/SIMA20180214004), Feb 14, 2018: FRAME. CRACKED. FRAME 23 IS CRACKED BETWEEN STRINGERS 16R - 15R. REPAIRED THE FRAME IAW EM-53MR-1808.
- [SDR SIMA20180124006](https://openairdocs.org/sdr/SIMA20180124006), Jan 24, 2018: DOOR FRAME. CORRODED. PASSENGER DOOR LOWER FRAME CORRODED AT 2 NUTPLATE HOLES. REPAIRED DOOR FRAME IAW ERS-EM-52MR-858.
- [SDR SIMA20180124005](https://openairdocs.org/sdr/SIMA20180124005), Jan 24, 2018: FLOOR SUPPORT. CORRODED. LEFT CENTER OMEGA BEAM CORRODED UNDER THE CARBON CROSS MEMBER AT FRAME 44. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-3147.
- [SDR SIMA20140612002](https://openairdocs.org/sdr/SIMA20140612002), Jun 12, 2014: FLASHLIGHT. DIM. CAPTAIN`S SIDE FLASHLIGHT VERY DIM. R & R FLASHLIGHT IAW ETN-EM-33-034, OPS CHECKED GOOD.
- [SDR SIMA20140423003](https://openairdocs.org/sdr/SIMA20140423003), Apr 23, 2014: WIRE HARNESS. DAMAGED. FLIGHT ATTENDANT REPORTS STRONG ODOR OF BURNING SMELL WHEN SHE TURNED LIGHTS ON AFTER LANDING. SMELL IS IN FWD PART OF CABIN. TRANSFERRED TO NRWC 810-ORD-01663.
- [SDR SIMA20140331002](https://openairdocs.org/sdr/SIMA20140331002), Mar 31, 2014: WIRE. FAILED. FLIGHT ATTENDANT REPORTED THAT AFTER LANDING GEAR EXTENSION, A MEDIUM STRENGTH ODOR OF BURNING RUBBER LASTING 1 TO 3 MINUTES IN THE FWD GALLEY AREA & FWD ENTRY 
- [SDR SIMA20140222002](https://openairdocs.org/sdr/SIMA20140222002), Feb 22, 2014: CHARGER. FAILED. PASSENGER DOOR & OVERHEAD ENTRY EMERGENCY LIGHT BULBS INOPERATIVE, 0 VOLTS. R & R NR 1 EMERGENCY BATTERY CHARGER & OPERATIONS CHECKED GOOD IAW AMM 33-50-04.
- [SDR SIMA20140120003](https://openairdocs.org/sdr/SIMA20140120003), Jan 20, 2014: DISPLAY. FAILED. AT INITIAL POWER UP CAPTAIN'S MFD DID NOT COME ON ASSOCIATED WITH A STRONG ODOR. MFD 1 CB FOUND POPPED. R & R NR 1 MFD IAW AMM 31-41-02, OPERATIONS CHECKED GOOD
- [SDR SIMA20130710003](https://openairdocs.org/sdr/SIMA20130710003), Jul 10, 2013: INVERTER. INOPERATIVE. DURING B INSPECTION, FOUND FORWARD LEFT EMERGENCY LIGHTING AND SERVICE DOOR LOWER EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R NR 2 EMERGENCY L
- [SDR SIMA20130710002](https://openairdocs.org/sdr/SIMA20130710002), Jul 10, 2013: FLASHLIGHT. INOPERATIVE. DURING B INSPECTION, FOUND THE FWD CABIN EMERGENCY FLASHLIGHT INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE FORWARD CABIN EMERGENCY FLASHLIGHT IAW W
- [SDR SIMA20130505004](https://openairdocs.org/sdr/SIMA20130505004), May 5, 2013: WIRE. BROKEN. DURING B INSPECTION FOUND THE AFT LEFT EMERGENCY LIGHT STRIP HAD A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHTI
- [SDR SIMA20130220004](https://openairdocs.org/sdr/SIMA20130220004), Feb 20, 2013: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION FOUND THE LEFT FORWARD OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT F
- [SDR SIMA20130211005](https://openairdocs.org/sdr/SIMA20130211005), Feb 11, 2013: CONNECTOR. UNSERVICEABLE. ON FLIGHT 3866 THE CREW REPORTED THAT DURING CRUISE FLIGHT LEVEL 360 A BRAKE LIGHT CAME ON AND REMAINED ON TO THE GATE. THE CREW DECLARED AN EMERGENCY. THE FLIG
- [SDR SIMA20130127002](https://openairdocs.org/sdr/SIMA20130127002), Jan 27, 2013: UNKNOWN. FUMES. DURING MAINTENANCE INSPECTION WHEN APU WAS STARTED FUEL FUMES WERE NOTICED IN THE COCKPIT WITH THE ENGINE RUNNING. THE AIRCRAFT WAS REMOVED FROM SERVICE. RAN BO
- [SDR SIMA20121129003](https://openairdocs.org/sdr/SIMA20121129003), Nov 29, 2012: ANGLE. CRACKED. DURING MAINTENANCE INSPECTION FOUND THE RIGHT VERTICAL STABILIZER TO FUSELAGE ANGLE AT FRAME 76 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO 
- [SDR SIMA20121129002](https://openairdocs.org/sdr/SIMA20121129002), Nov 29, 2012: FITTING. DAMAGED. DURING MAINTENANCE INSPECTION FOUND THE RIGHT AILERON DAMPER FITTING OUTBOARD LUG SCORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DAMPER 
- [SDR SIMA20121128012](https://openairdocs.org/sdr/SIMA20121128012), Nov 28, 2012: FLOOR SUPPORT. DENTED. DURING HEAVY CHECK INSPECTION FOUND THE RIGHT OMEGA BEAM BETWEEN FRAME 71 AND 72 HAS A LARGE DENT ON UPPER SURFACE. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPL
- [SDR SIMA20121205001](https://openairdocs.org/sdr/SIMA20121205001), Nov 28, 2012: SKIN. CRACKED. DURING HEAVY CHECK INSPECTION FOUND REAR ELECTRONICS COMPARTMENT DOOR 272DR HAS 2 EACH CRACKS UNDER THE ATTACHMENT HOOK. THE AIRCRAFT WAS REMOVED FROM SERVICE. 
- [SDR SIMA20121128009](https://openairdocs.org/sdr/SIMA20121128009), Nov 28, 2012: SKIN. CRACKED. DURING MAINTENANCE INSPECTION FOUND THE RIGHT FUSELAGE SKIN HAS A CRACK 3/8" LONG AT FRAME 75 AND STRINGER 2R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED R

All 98: https://openairdocs.org/aircraft/N810AE/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/N810AE/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.