# N850AE: 2003 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: 145722
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 21, 2003
- Certificate issued: May 11, 2023
- Expires: May 31, 2030
- Mode S code: ABA75D
- 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=850AE
- Page: https://openairdocs.org/aircraft/N850AE

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/N850AE/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 N850AE.

## FAA accident and incident reports

None matched to N850AE.

## Service difficulty reports (61, 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 SIMA201912242002](https://openairdocs.org/sdr/SIMA201912242002), Dec 22, 2019: DOOR. STUCK. UNABLE TO OPEN MAIN CABIN DOOR "TRANSFERRED TO NRWC 850-DFW-03053". REMOVED AND REPLACED PAX DOOR FOLDING FLAP ACTUATING TORQUE TUBE TERMINAL IAW AMM 52-18-02. 
- [SDR SIMA2019120230001](https://openairdocs.org/sdr/SIMA2019120230001), Nov 30, 2019: SIGN. INOPERATIVE. DURING PS-1 CHECK FOUND AFT CEILING EMERGENCY EXIT SIGN LIGHT INOP-C/A-REMOVED AND REPLACED EMERGENCY CEILING LIGHT IAW AMM 33-50-15 OPC GOOD. EMERGENCY LIGHT S
- [SDR SIMA201910254001](https://openairdocs.org/sdr/SIMA201910254001), Oct 24, 2019: WARNING MESSAGE. FALSE ACTIVATION. IN ICING CONDITIONS RECIEVED WING ANTI ICE FAIL FOLLOWED BY A/I INOP WEARNING. RAN QRH PROCEDURE WORKED FOR 1 MINUTE THEN FAILED AGAIN-C/A-CMC FAULT CODE 30-1PM
- [SDR SIMA20190629002](https://openairdocs.org/sdr/SIMA20190629002), Jun 29, 2019: CONNECTOR. BROKEN. TWO EMERGENCY LIGHT STRIPS HAVE BROKEN CONNECTORS. C/A-INSTALLED NEW CONNECTORS ON 2 EMERGENCY LIGHT STRIPS IAW SWPM 20-50-00, C/W OPS CHECK OF THE EMERGENCY LI
- [SDR SIMA201906174004](https://openairdocs.org/sdr/SIMA201906174004), Jun 14, 2019: SIGN. INOPERATIVE. DURING PS-1 CHECK FOUND AFT GALLEY EXIT IDENTIFIER SIGN INOP-C/A-REMOVED AND REPLACED EXIT IDENTIFIER SIGN AFT OF GALLEY IAW EMB 140 AMM 33-50-13. OPC FAILED. F
- [SDR SIMA20190526002](https://openairdocs.org/sdr/SIMA20190526002), May 26, 2019: VALVE. FAILED. "TRANSFERRED FROM AML PAGE 4473404 ITEM 2" PACK 1 OVRLD ON TAKEOFF AND CLIMB, RESET AND FAILED AGAIN. C/A- REMOVED AND REPLACED #1 PACK VALVE IAW AMM 21-51-01 A
- [SDR SIMA20190524001](https://openairdocs.org/sdr/SIMA20190524001), May 24, 2019: ACM. DAMAGED. RETURNED TO LAND AFTER SMOKE IN THE COCKPIT AND CABIN SUSPECT PACK 1 "TRANSFERRED TO NRWC 850-DFW-02629". C/A-REF: NRWC 850-DFW-02629 - PER ETN-EM-21-062 - COMP
- [SDR SIMA20190521002](https://openairdocs.org/sdr/SIMA20190521002), May 21, 2019: ACM. FAILED. SUPPLEMENTAL SMOKE IN COCKPIT JUST AFTER GEAR UP GREY COLORED SMOKE AND STRONG FUMES. TURNED OFF PACK 1 AND BLEED 1 SMOKE AND FUMES SUBSIDED. C/A-C/W ETN-EM-72-
- [SDR SIMA201904220004](https://openairdocs.org/sdr/SIMA201904220004), Apr 20, 2019: WIRE. DISCONNECTED. EMERGENCY EXIT LIGHT ON THE AFT SIDE OF THE CENTER AISLE IS OUT. FOUND DISCONNECTED WIRE HARNESS. RESECURED CONNECTION. IAW AMM 33-50-11 OPS CHECK GOOD
- [SDR SIMA20190112002](https://openairdocs.org/sdr/SIMA20190112002), Jan 12, 2019: SIGN. INOPERATIVE. DURING PS-1 CHECK FOUND CEILING EMERGENCY SIGN INOP. C/A-REMOVED AND REPLACED AFT EMERGENCY SIGN ON CEILING PANEL IAW AMM 33-50-15. OPC GOOD.
- [SDR SIMA20180830003](https://openairdocs.org/sdr/SIMA20180830003), Aug 30, 2018: CHARGER. INOPERATIVE. CENTER AFT EMERGENCY EXIT SIGN AND LT WALL MOUNTED EMERGENCY SIGN INOP. C/A-REMOVED AND REPLACED NR 3 EMERGENCY BATTERY AND CHARGER IAW AMM 33-50-04 OP'S CHECK 
- [SDR SIMA201807132001](https://openairdocs.org/sdr/SIMA201807132001), Jul 12, 2018: CONNECTOR. DIRTY. EMERGENCY EXIT LOCATING SIGN ON MID CEILING PANEL, AFT SIDE IS INOP. CLEANED WIRING HARNESS CONNECTION FOR EMERGENCY EXIT LOCATING SIGN NR 3 IAW SWPM 20-21-00. 
- [SDR SIMA20180115004](https://openairdocs.org/sdr/SIMA20180115004), Jan 15, 2018: BULB. INOPERATIVE. RIGHT OVERWING FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-10. OPS CHECKED GOOD.
- [SDR SIMA20171005001](https://openairdocs.org/sdr/SIMA20171005001), Oct 5, 2017: SKIN. CRACKED. LEFT UPPER FUSELAGE SKIN CRACKED AT STRINGER 2L JUST AFT OF FRAME 75. REPAIRED THE SKIN IAW SRM 53-31-01.
- [SDR SIMA20170930005](https://openairdocs.org/sdr/SIMA20170930005), Sep 30, 2017: SKIN. GOUGED. PAX DOOR EXTERNAL SKIN IS GOUGED AT THE AFT LOWER END. REPAIRED THE DOOR SKIN IAW ERS-EM-52MR-808.
- [SDR SIMA20170929005](https://openairdocs.org/sdr/SIMA20170929005), Sep 29, 2017: WIRE. CHAFED. NR 3 EMERGENCY LIGHT WIRE CHAFED. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20170929003](https://openairdocs.org/sdr/SIMA20170929003), Sep 29, 2017: WIRE. TORN. NR 4 EMERGENCY LIGHT STRIP WIRE TORN. REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12.
- [SDR SIMA20170929004](https://openairdocs.org/sdr/SIMA20170929004), Sep 29, 2017: DOOR SILL. CORRODED. SERVICE DOOR SILL CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA20170928006](https://openairdocs.org/sdr/SIMA20170928006), Sep 28, 2017: FRAME. CRACKED. FRAME 10 CRACKED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.
- [SDR SIMA20170922006](https://openairdocs.org/sdr/SIMA20170922006), Sep 22, 2017: DOOR SILL. CORRODED. CARGO DOOR SILL CORRODED. REMOVED AND REPLACED THE LOWER DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA20170823003](https://openairdocs.org/sdr/SIMA20170823003), Aug 23, 2017: CROSSBEAM. CORRODED. CROSSBEAM BETWEEN FR 24-25 IS CORRODED. REMOVED AND REPLACED CROSSBEAM BETWEEN FR 24-25 IAW SRM 53-22-10, ETN-EM-53-139.
- [SDR SIMA20170823002](https://openairdocs.org/sdr/SIMA20170823002), Aug 23, 2017: FLASHLIGHT. INOPERATIVE. AFT EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.
- [SDR SIMA20150102007](https://openairdocs.org/sdr/SIMA20150102007), Jan 2, 2015: INVERTER. INOPERATIVE. AFT EMER EXIT SIGN INOPERATIVE. R & R AFT EMER EXIT SIGN LIGHT INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150102005](https://openairdocs.org/sdr/SIMA20150102005), Jan 2, 2015: LIGHT. INOPERATIVE. RIGHT FWD EMER LIGHT INOPERATIVE. R & R INOPERATIVE RT FWD EMER LIGHT IAW 33-50-10. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140908006](https://openairdocs.org/sdr/SIMA20140908006), Sep 8, 2014: FLASHLIGHT. BROKEN. REAR PAX CABIN EMER FLASHLIGHT BROKEN. R & R REAR PAX CABIN EMER FLASHLIGHT AS REQUIRED.
- [SDR SIMA20140803002](https://openairdocs.org/sdr/SIMA20140803002), Aug 3, 2014: CRADLE. BROKEN. FIRST OFFICERS EMER FLASHLIGHT CRADLE BROKEN. R & R FIRST OFFICERS EMER FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GO
- [SDR SIMA20140727005](https://openairdocs.org/sdr/SIMA20140727005), Jul 27, 2014: LIGHT. INOPERATIVE. LEFT AFT EMER LIGHT OVERWING IS INOPERATIVE. R & R LT AFT EMER EXTERNAL LIGHT BULB OVERWING IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140717002](https://openairdocs.org/sdr/SIMA20140717002), Jul 17, 2014: LIGHT. INOPERATIVE. RIGHT WING FWD EMER LIGHT INOPERATIVE. R & R RT WING FWD EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140616001](https://openairdocs.org/sdr/SIMA20140616001), Jun 16, 2014: LIGHT. INOPERATIVE. RIGHT EXTERNAL OVERWING EMER LIGHT INOPERATIVE. R & R LIGHT LAMP IN LT EXTERNAL OVERWING EMER LIGHT IAW AMM 33-50-07-000-801-A & 33-50-07-400-801-A. OPERATIONS 
- [SDR SIMA20140601003](https://openairdocs.org/sdr/SIMA20140601003), Jun 1, 2014: LIGHT. INOPERATIVE. RIGHT FWD EMER LIGHT INOPERATIVE. R & R RT EMER LIGHT FAIRING IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.
- [SDR SIMA20140407001](https://openairdocs.org/sdr/SIMA20140407001), Apr 7, 2014: SUPPORT. DAMAGED. DURING FLIGHT WHEN INCREASING AIRSPEED ABOVE 225KNTS UNKNOWN SOUND & VIBRATION. FLIGHT ATTENDANT REPORTED VIBRATION IN FLOOR AROUND ROW 4 & 5. INSPECTION FOUND 
- [SDR SIMA20140212006](https://openairdocs.org/sdr/SIMA20140212006), Feb 12, 2014: SUMP. COKED. WHILE CLIMBING THROUGH FL 330 E1 ITT WAS NOTED TO BE FLUCTUATING BETWEEN 600 - 800. N2 WAS FLUCTUATING +- 5%. N1 DROPPED BELOW 45% NO ENG LIMITATIONS WERE SEEN 
- [SDR SIMA20140205001](https://openairdocs.org/sdr/SIMA20140205001), Feb 5, 2014: BRACKET. DEFECTIVE. FLIGHT ATTENDANT`S REAR FLASHLIGHT HOLDER WILL NOT HOLD FLASHLIGHT. R & R WITH SERVICEABLE AFT FLASHLIGHT BRACKET IAW AMM 333 50 16, OPERATIONS CHECKED OK.
- [SDR SIMA20140112007](https://openairdocs.org/sdr/SIMA20140112007), Jan 12, 2014: LIGHT. INOPERATIVE. RIGHT FWD OVERWING EMERGENCY LIGHT IS INOPERATIVE. R & R LAMP ON RT FWD OVERWING EMERGENCY LIGHT IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.
- [SDR SIMA20130923003](https://openairdocs.org/sdr/SIMA20130923003), Sep 23, 2013: LAMP. INOPERATIVE. EMERGENCY LIGHT ON RT FWD BELLY FAIRING INOP. R & R EMERGENCY LIGHT BULB ON RT FWD BELLY FAIRING IAW AMM 33-50-10. OPS CHECKED GOOD.
- [SDR SIMA20130920009](https://openairdocs.org/sdr/SIMA20130920009), Sep 20, 2013: LIGHT. INOPERATIVE. RIGHT FWD EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R RT EMERGENCY LIGHT ASSY IAW AMM 33-50-07. OPS CHECKED GOOD.
- [SDR SIMA20130910004](https://openairdocs.org/sdr/SIMA20130910004), Sep 10, 2013: CRADLE. BROKEN. LEFT SIDE OF FLASHLIGHT CRADLE BEHIND CAPTAIN'S SEAT IS BROKEN. R & R CRADLE IAW CMM 25-60-11.
- [SDR SIMA20130410007](https://openairdocs.org/sdr/SIMA20130410007), Apr 10, 2013: LIGHT. INOPERATIVE. DURING B INSPECTION FOUND THE RIGHT EMERGENCY LIGHT ON THE FORWARD BELLY PANEL INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT
- [SDR SIMA20130305003](https://openairdocs.org/sdr/SIMA20130305003), Mar 5, 2013: BATTERY. DISCHARGED. DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY NR 4 BATTERY AND BATTERY CHARGER NEEDS TO BE REPLACED IAW WC 33-700-19. THE AIRCRAFT WAS REMOVED FROM SERVICE.
- [SDR SIMA20130224006](https://openairdocs.org/sdr/SIMA20130224006), Feb 24, 2013: UNKNOWN. SMOKE. DURING MAINTENANCE INSPECTION FOUND THE NUMBER 1 MAIN GEAR GREEN INDICATION ON MFD THE BRAKE TEMP. 10 MIN AFTER BLOCK IN NUMBER 1 MAIN GEAR TIRE HAD LIGHT SMOKE
- [SDR SIMA20130218005](https://openairdocs.org/sdr/SIMA20130218005), Feb 18, 2013: BATTERY. INOPERATIVE. DURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY BATTERY INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY BATTER
- [SDR SIMA20130110009](https://openairdocs.org/sdr/SIMA20130110009), Jan 10, 2013: GUSSET. CORRODED. DURING B INSPECTION FOUND THE LAV RIGHT BEAM GUSSET CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAV RIGHT BEAM GUSSET IAW EMB SRM 
- [SDR SIMA20130110008](https://openairdocs.org/sdr/SIMA20130110008), Jan 10, 2013: GUSSET. CORRODED. DURING B INSPECTION FOUND THE LAV CENTER BEAM GUSSET CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAV CENTER BEAM GUSSET IAW EMB SR
- [SDR SIMA20130110007](https://openairdocs.org/sdr/SIMA20130110007), Jan 10, 2013: LIGHT. INOPERATIVE. DURING B INSPECTION FOUND THE RIGHT EMERGENCY EXIT LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT ABOVE RIGHT
- [SDR SIMA20130110005](https://openairdocs.org/sdr/SIMA20130110005), Jan 10, 2013: STRIP. MISSING. DURING B INSPECTION FOUND THE FLOOR EMERGENCY LIGHT STRIP MISSING INFILL STRIP ON AFT END. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED FLOOR EMERGENCY LIGH
- [SDR SIMA20130110004](https://openairdocs.org/sdr/SIMA20130110004), Jan 10, 2013: HANDLE. LOOSE. DURING B INSPECTION FOUND THE LEFT EMERGENCY EXIT DOOR UPPER GRAB HANDLE LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TIGHTENED HARDWARE ON THE LEFT EMERGENCY 
- [SDR SIMA20121231007](https://openairdocs.org/sdr/SIMA20121231007), Dec 31, 2012: ECU. MALFUNCTIONED. ON FLIGHT 2997 THE CREW REPORTED THEY RECEIVED A FLAP FAIL EICAS MESSAGE WITH FLAPS NOT MOVING. THE AIRCRAFT WAS REMOVED FROM SERVICE. MEL 27-09 WAS ISSUED PRIO
- [SDR SIMA20120923004](https://openairdocs.org/sdr/SIMA20120923004), Sep 23, 2012: CLAMP. LOOSE. ON FLIGHT 3071 THE CREW REPORTED THAT WHILE PERFORMING THE AFTER LANDING CHECKLIST, THE BAGGAGE EXTINGUISHER BUTTON ILLUMINATED WITH NO ASSOCIATED FIREBELL OR W
- [SDR SIMA2012045001](https://openairdocs.org/sdr/SIMA2012045001), Feb 13, 2012: SMOKE DETECTOR. MALFUNCTIONED. ON FLIGHT 3046 THE FLIGHT ATTENDANT ADVISED THE GREEN LIGHT ON THE GALLEY SMOKE DETECTOR DID NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OP
- [SDR SIMA201122206](https://openairdocs.org/sdr/SIMA201122206), Aug 7, 2011: INVERTER. INOPERATIVE. MID CABIN CEILING PANEL FWD EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. DURING ROUTINE PS-2 INSPECTION FOUND EMERGENCY LIGHT DID NOT ILLUMINATE. REMOVED AND REPLA

All 61: https://openairdocs.org/aircraft/N850AE/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/N850AE/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.