# N849AE: 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: 145716
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 14, 2003
- Certificate issued: June 12, 2023
- Expires: June 30, 2030
- Mode S code: ABA14D
- 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=849AE
- Page: https://openairdocs.org/aircraft/N849AE

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/N849AE/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 N849AE.

## FAA accident and incident reports

None matched to N849AE.

## Service difficulty reports (87, 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 SIMA201911143007](https://openairdocs.org/sdr/SIMA201911143007), Nov 13, 2019: LIGHT. INOPERATIVE. OVERHEAD COCKPIT EMER LIGHT INOP-C/A-REMOVED AND REPLACED OVERHEAD COCKPIT EMER LIGHT IAW AMM 33-50-05. OPS CHECK GOOD
- [SDR SIMA20190530003](https://openairdocs.org/sdr/SIMA20190530003), May 30, 2019: TUBE. NOT REPORTED. MEL 21-17 AUTH # 050951DM-C ORIGINAL LOG PAGE 4510226 ITEM 1. AUTO PRESS SYSTEM FAILED DURING CLIMB. AURAL WARNING. MANUAL PRESSURIZATION IS EXTREMLY SENSITIVE 
- [SDR SIMA201902252001](https://openairdocs.org/sdr/SIMA201902252001), Feb 22, 2019: STATIC INVERTER. FAILED. AT 16000 DESCENDING INTO SUX 115 VAC BUS OFF. WINDSHEAR INOP GPWS INOP, TERR INOP. 3 MIN LATER WARM ELECTRICAL SMELL LASTED 2 MIN THEN WENT AWAY-C/A-REMOVED AND
- [SDR SIMA201812054001](https://openairdocs.org/sdr/SIMA201812054001), Dec 4, 2018: SEAL. FOD. VERY LOUD SQUEALING AND WOOSHING NOISE COMING FROM MAIN CABIN DOOR AFTER TAKE OFF-C/A-FOUND OBJECT ON DOOR SEAL AND STICKER. REMOVED FROM MAIN CABIN DOOR SEAL A
- [SDR SIMA20181203006](https://openairdocs.org/sdr/SIMA20181203006), Dec 3, 2018: PROXIMITY SENSOR. FAILED. SPOILER FAIL MSG ON EICAS AND OPN INDICATION WHILE AT GATE AFTER STARTUP. REMOVED AND REPLACED OB RT SIDE PROXIMITY SWITCH IAW AMM 27-63-04. OPC GOOD IAW AMM 27
- [SDR SIMA201811276007](https://openairdocs.org/sdr/SIMA201811276007), Nov 26, 2018: WARNING MESSAGE. FALSE ACTIVATION. ICE CONDITION ANTI ICE INOP POSTED IN FLIGHT IN ICING CONDITIONS.-C/A-PERFORMED OPS CHECK OF ANTI ICE SYSTEM PER EMB 140 AMM 30-00-00. NO DEFECTS NOTED, NO CMC 
- [SDR SIMA201811149002](https://openairdocs.org/sdr/SIMA201811149002), Nov 9, 2018: WARNING MESSAGE. FALSE INDICATION. E2 A/ICE FAIL.-C/A-DEFERRED E2 A/ICE VALVE FAIL AS PER MEL 30-11. MTX PROCEDURES COMPLIED WITH A/C OK FOR SERVICE. PERFORMED T/S IAW EMB 140 FIM 30-80-00-810-80
- [SDR SIMA2018051706002](https://openairdocs.org/sdr/SIMA2018051706002), May 16, 2018: LIGHT. INOPERATIVE. EMERGENCY LIGHT ON MAIN DOOR DOES NOT ILLUMINATE. LIGHT WOULD ONLY COME ON WHEN HOUSING ASSEMBLY AT CONNECTOR END WAS PUSHED IN. REMOVED AND REPLACED THE EMERGE
- [SDR SIMA20180327001](https://openairdocs.org/sdr/SIMA20180327001), Mar 27, 2018: SMOKE WARNING. FALSE ACTIVATION. BAGGAGE SMOKE EICAS T GATE, CARGO DOOR CLOSED. FLIGHT ATTENDANT SAW SMOKE IN CARGO BAY. PERFORMED ETN-EM-72-034. NO SMOKE IN CARGO BAY OR CABIN. OPS CHECKED GOO
- [SDR SIMA20180306002](https://openairdocs.org/sdr/SIMA20180306002), Mar 6, 2018: LAMP. INOPERATIVE. FLASHLIGHT IN THE REAR CABIN IS INOPERATIVE. REPLACED THE LAMP IN THE FLASHLIGHT IAW CMM 25-60-11. OPS CHECKED GOOD.
- [SDR SIMA20180224001](https://openairdocs.org/sdr/SIMA20180224001), Feb 24, 2018: SMOKE DETECTOR. FALSE INDICATION. CARGO SMOKE WARNING DURING TAXI IN. RAN PROCEDURE AND EXTINUISHED THE CARGO BOTTLE. CFR FOUND 1 BAG ON FIRE. INSPECTED CARGO BAY IAW AMM 25-51-01, NO DAMAGE FOU
- [SDR SIMA20180221005](https://openairdocs.org/sdr/SIMA20180221005), Feb 21, 2018: IGNITER. FAILED. DURING TAXI, TRIED TO START THE NR 2 ENGINE, HAD A HUNG START, RAN THE CHECK LIST HAD GAS FUMES , RAN CHECK LIST AND RETURNED TO GATE. REMOVED AND REPLACED THE 
- [SDR SIMA20180201006](https://openairdocs.org/sdr/SIMA20180201006), Feb 1, 2018: LIGHT. INOPERATIVE. NR 2 EMERGENCY LIGHT STRIP INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12.
- [SDR SIMA20180201005](https://openairdocs.org/sdr/SIMA20180201005), Feb 1, 2018: CONNECTOR. BROKEN. NR 1 EMERGENCY LIGHT STRIP HAS A BROKEN CONNECTOR. INSTALLED A NEW CONNECTOR AND PIN IAW SWPM 20-21-00.
- [SDR SIMA20180131003](https://openairdocs.org/sdr/SIMA20180131003), Jan 31, 2018: LIGHT. DAMAGED. L5 EMERGENCY LIGHT STRIP DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12
- [SDR SIMA20180131002](https://openairdocs.org/sdr/SIMA20180131002), Jan 31, 2018: LIGHT. DAMAGED. R3 LIGHT STRIP IS DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12.
- [SDR SIMA20180126011](https://openairdocs.org/sdr/SIMA20180126011), Jan 26, 2018: BRACE. CRACKED. NLG UPLOCK BOX AFT BRACE IS CRACKED. REMOVED AND REPLACED NLG UPLOCK BOX AFT BRACE IAW SRM 51-40-02.
- [SDR SIMA20180124002](https://openairdocs.org/sdr/SIMA20180124002), Jan 24, 2018: HINGE FITTING. ABNORMAL. RT AILERON ACTUATOR HINGE FITTING LUG HOLE WORN BUSHING LOOSE IN LUG. REMOVED AND REPLACED RT AILERON ACTUATOR HINGE FITTING IAW SRM 51-40-02, EO EM-27MR-112.
- [SDR SIMA20180124003](https://openairdocs.org/sdr/SIMA20180124003), Jan 24, 2018: FITTING. DAMAGED. RT AILERON DAMPER FITTING OUTBD LUG HOLE IS DAMAGED. REMOVED AND REPLACED RT AILERON DAMPER FITTING IAW SRM 51-40-02, EO EM-27MR-112.
- [SDR SIMA20180123017](https://openairdocs.org/sdr/SIMA20180123017), Jan 23, 2018: RIB. CRACKED. NOSE RIB ON LEFT ELEVATOR INBOARD HINGE CUTOUT INBOARD SIDE IS CRACKED. REMOVED AND REPLACED LT ELEVATOR NOSE RIB ON INBOARD HINGE CUTOUT INBOARD SIDE IAW SRM 5
- [SDR SIMA20180123016](https://openairdocs.org/sdr/SIMA20180123016), Jan 23, 2018: FRAME. CRACKED. FRAME 10 CRACKED BELOW LT DV WINDOW CUTOUT. REMOVED AND REPLACED FRAME 10 BELOW LT DV WINDOW CUTOUT IAW SRM 51-40-02.
- [SDR SIMA20180123015](https://openairdocs.org/sdr/SIMA20180123015), Jan 23, 2018: FITTING. CORRODED. SHEAR CLIP AT FRAME 65 IS CORRODED. PERFORMED REPAIR TO SHEAR CLIP AT FRAME 65 IAW SRM 53-31-04.
- [SDR SIMA20180123014](https://openairdocs.org/sdr/SIMA20180123014), Jan 23, 2018: FITTING. DAMAGED. LT AILERON DAMPNER FITTING IS CHAFFED ON INNER SURFACE. REMOVED AND REPLACED LT AILERON DAMPER FITTING IAW EO EM-27MR-112.
- [SDR SIMA20180123020](https://openairdocs.org/sdr/SIMA20180123020), Jan 23, 2018: STRINGER. CRACKED. STRINGER 6R CRACKED AT FRAME 13. REMOVED AND REPLACED STR 6R AT FR 13 IAW SRM 51-40-02.
- [SDR SIMA20180123012](https://openairdocs.org/sdr/SIMA20180123012), Jan 23, 2018: DOOR SILL. CORRODED. CARGO DOOR SILL IS CORRODED. REMOVED AND REPLACED THE CARGO DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA20180123018](https://openairdocs.org/sdr/SIMA20180123018), Jan 23, 2018: DOOR SILL. CORRODED. SERVICE DOOR CUTOUT LOWER CENTER SILL CORRODED. REMOVED AND REPLACED SERVICE DOOR CUTOUT LOWER CENTER SILL IAW SRM 51-40-02.
- [SDR SIMA20180123019](https://openairdocs.org/sdr/SIMA20180123019), Jan 23, 2018: FRAME. CRACKED. FRAME 10 CRACKED BELOW RT DV WINDOW CUTOUT. REMOVED AND REPLACED FRAME 10 BELOW RT DV WINDOW CUTOUT IAW SRM 51-40-02
- [SDR SIMA20180123013](https://openairdocs.org/sdr/SIMA20180123013), Jan 23, 2018: FRAME. CRACKED. FRAME 23 CRACKED BETWEEN STR 15R AND 16R. ACCOMPLISHED REPAIR OF FR 23 BETWEEN STR 15R-16R IAW SRM 53-00-04 ITEM 3 AND 51-40-02.
- [SDR SIMA20180105004](https://openairdocs.org/sdr/SIMA20180105004), Jan 5, 2018: STRUCTURE. ERODED. THE RT NR 2 LEADING EDGE ERODED, AND IS OUT OF LIMITS IN ONE AREA AT ZONE NR 2. REPAIRED DAMAGE IAW ERS EM-55MR-574
- [SDR SIMA20171220007](https://openairdocs.org/sdr/SIMA20171220007), Dec 20, 2017: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT HAS CORROSION BETWEEN FRAMES 23 AND 24. REPAIR THE FLOOR SUPPORT.
- [SDR SIMA20171220008](https://openairdocs.org/sdr/SIMA20171220008), Dec 20, 2017: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT HAS CORROSION BETWEEN FRAMES 25 AND 26. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR SIMA20171220006](https://openairdocs.org/sdr/SIMA20171220006), Dec 20, 2017: CROSSBEAM. CRACKED. CENTER AISLE CARBON CROSSBEAM AT FRAME 27 IS CRACKED. REMOVED AND REPLACED THE CROSSBEAM CENTER AISLE IAW SRM 51-40-02.
- [SDR SIMA20171220003](https://openairdocs.org/sdr/SIMA20171220003), Dec 20, 2017: FLOOR SUPPORT. CRACKED. GALLEY LEFT FLOOR SUPPORT LT ANGLE BETWEEN FRAMES 16 AND 17 CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT ANGLE BETWEEN FRAMES 16 AND 17 IAW SRM 51-40-02.
- [SDR SIMA20171220004](https://openairdocs.org/sdr/SIMA20171220004), Dec 20, 2017: FLOORBEAM. CORRODED. GALLEY CENTER AISLE FLOORBEAM AT FRAME 20 CORRODED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 53-21-10, AND ETN-EM-53-139R4.
- [SDR SIMA20171220005](https://openairdocs.org/sdr/SIMA20171220005), Dec 20, 2017: FLOOR SUPPORT. CRACKED. GALLEY CENTER FLOOR SUPPORT LT ANGLE BETWEEN FRAMES 16 AND 17 CRACKED. REMOVED AND REPLACEMENT THE FLOOR SUPPORT ANGLE IAW SRM 51-40-02.
- [SDR SIMA20150222002](https://openairdocs.org/sdr/SIMA20150222002), Feb 22, 2015: BRACKET. BROKEN. REENTER MEL 25 - 53, AFT FLASHLIGHT BRACKET BROKEN. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD. MEL 25-53 RESTORED.
- [SDR SIMA20141228006](https://openairdocs.org/sdr/SIMA20141228006), Dec 28, 2014: CRADLE. BROKEN. CAPTAIN`S FLASHLIGHT CLIP ON THE MOUNT IS BROKEN. R & R CAPTAIN`S FLASHLIGHT CRADLE. OPERATIONS CHECKED GOOD IAW AMM 33-50-16.
- [SDR SIMA20141201001](https://openairdocs.org/sdr/SIMA20141201001), Dec 1, 2014: CONTROLLER. FAULTY. COUPLED TO FIRST OFFICER`S SIDE, DURING CLIMB OUT SPEED SELECTOR KNOB WOULD NOT CHANGE SPEED INITIALLY. AFTER 2 MIN SPEED WAS ABLE TO BE CHANGED INTERMITTENTLY.
- [SDR SIMA20141125010](https://openairdocs.org/sdr/SIMA20141125010), Nov 25, 2014: CIRCUIT CARD. FAILED. UPON DEPARTURE ALT SPD & HDG SELECTORS BECAME INOPERATIVE. THE SELECTORS REMAINED INOPERATIVE UNTIL SHORT FINAL. DEFERRED IAW MEL 33-02. R & R NR 1 IC 600 IAW A
- [SDR SIMA20141004001](https://openairdocs.org/sdr/SIMA20141004001), Oct 4, 2014: SIGN. FADED. EMERGENCY EXIT SIGN ON MAIN CABIN DOOR FADED & ILLEGIBLE. R & R IAW AMM 11-00-01.
- [SDR SIMA20141002006](https://openairdocs.org/sdr/SIMA20141002006), Oct 2, 2014: VALVE. FAILED. DURING CLIMB THROUGH 12,000 FEET, NR 2 PACK VALVE FAILED MESSAGE. R & R NR 2 PACK VALVE IAW AMM 21-51-01. OPS CHECKED GOOD. LEAK CHECKED GOOD.
- [SDR SIMA20140615001](https://openairdocs.org/sdr/SIMA20140615001), Jun 15, 2014: FLASHLIGHT. INOPERATIVE. AFT CABIN FLASHLIGHT INOPERATIVE. R & R AFT CABIN FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.
- [SDR SIMA20140430002](https://openairdocs.org/sdr/SIMA20140430002), Apr 30, 2014: FLASHLIGHT. BROKEN. FIRST OFFICER'S EMERGENCY FLASHLIGHT IS BROKEN. R & R FIRST OFFICER'S EMERGENCY FLASHLIGHT IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.
- [SDR SIMA20140430004](https://openairdocs.org/sdr/SIMA20140430004), Apr 30, 2014: CRADLE. DAMAGED. FORWARD PAX CABIN EMERGENCY LIGHT CRADLE STRUCTURE HAS EVIDENCE OF OVERHEATING. R & R FWD EMERGENCY LIGHT CHARGER CRADLE IAW AMM 33-50-16, OPERATIONS CHECKED GO
- [SDR SIMA20140430003](https://openairdocs.org/sdr/SIMA20140430003), Apr 30, 2014: LIGHT. MALFUNCTIONED. AFT PAX CABIN EMERGENCY LIGHT CRADLE STRUCTURE HAS EVIDENCE OF OVERHEATING. R & R AFT PAX EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.
- [SDR SIMA20140404002](https://openairdocs.org/sdr/SIMA20140404002), Apr 4, 2014: WHEEL. FAILED. JUST AFTER V1 NOSE SHIMMY THEN BUMP, BUMP, BUMP & THEN AIRBORNE. R & R LT NLG WHEEL ASSEMBLY IAW WC 32-700-17, OPERATIONS CHECKED GOOD.
- [SDR SIMA20140112009](https://openairdocs.org/sdr/SIMA20140112009), Jan 12, 2014: FLASHLIGHT. INOPERATIVE. FLIGHT ATTENDANT`S FLASHLIGHT INOPERATIVE. R & R FLIGHT ATTENDANT`S FLASHLIGHT IAW AMM 33-51-01. OPERATIONS CHECKED GOOD, NO FURTHER DEFECTS NOTED.
- [SDR SIMA20130921002](https://openairdocs.org/sdr/SIMA20130921002), Sep 21, 2013: BULB. BROKEN. CAPTAIN`S FLASHLIGHT BULB BROKEN. R & R FLASHLIGHT ASSY IAW AMM 33-50-00, OPS CHECKED GOOD.
- [SDR SIMA20130726002](https://openairdocs.org/sdr/SIMA20130726002), Jul 26, 2013: BATTERY. INOPERATIVE. DURING MX INSPECTION, FOUND THE CAPTAIN’S FLASHLIGHT, RED LED TO CHARGING STATUS INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R CAPTAIN’S FLASHLIGHT BATTERY IAW 
- [SDR SIMA20130721003](https://openairdocs.org/sdr/SIMA20130721003), Jul 21, 2013: CRADLE. INOPERATIVE. AFT CABIN FLASHLIGHT CHARGING CRADLE INOPERATIVE. R & R AFT FLASHLIGHT CRADLE WITH SERVICEABLE ONE IAW AMM 33-50-16. NO OTHER DEFECTS NOTED AT THIS TIME.

All 87: https://openairdocs.org/aircraft/N849AE/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/N849AE/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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