# N846AE: 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: 145692
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 20, 2003
- Certificate issued: December 11, 2024
- Expires: December 31, 2031
- Mode S code: AB9628
- Registered owners: [Corporate Flight Management Inc DBA](https://openairdocs.org/faa-owner/CORPORATE%20FLIGHT%20MANAGEMENT%20INC%20DBA), [Contour Aviation](https://openairdocs.org/faa-owner/CONTOUR%20AVIATION)
- Location: [Smyrna, TN](https://openairdocs.org/faa-place/TN/Smyrna)
- Owner type: Corporation
- Owner's area on the map: 35.9628° N, 86.5297° W: Placed by OpenAirDocs at the center of ZIP code 37167, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=846AE
- Page: https://openairdocs.org/aircraft/N846AE

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/N846AE/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 N846AE.

## FAA accident and incident reports

None matched to N846AE.

## Reports on N846AE not matched to an aircraft (2)

They name N846AE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19930705026099I](https://openairdocs.org/incident/19930705026099I), Jul 5, 1993: Bag JETSTM3201 (N846AE), Raleigh-Durham, NC. Left engine torque and EGT increased on final. Shut engine down. Landed safely. Fuel control unit had malfunctioned
- [Incident 19900519037409I](https://openairdocs.org/incident/19900519037409I), May 19, 1990: Bag JETSTM3201 (N846AE), Freeport, Bahamas, Minor damage. NR1 engine power deteriorated. Landed safely. Inspection revealed turbine wheel failure.

## Service difficulty reports (91, 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 SIMA202001098001](https://openairdocs.org/sdr/SIMA202001098001), Jan 8, 2020: CONNECTOR. MISSING. PRESS. FAIL DURING CLIMB OUT-C/A-FLIGHT CREW PLACARDED PER MEL2122 AUTH010305DMC MOC 135181 M PROC C/W. FOUND FLAP TYPE GROUND CONNECTION VALVE MISSING. REMOVED
- [SDR SIMA201911154001](https://openairdocs.org/sdr/SIMA201911154001), Nov 14, 2019: ROLLER. LACK OF LUBE. MAIN CABIN DOOR VERY DIFFICULT TO OPEN. FA WAS UNABLE TO OPEN. FO OPENED DOOR-C/A-LUBRICATED MAIN CABIN DOOR ROLLERS IAW EMB 140 AMM 53-21-02-600-801-A STEP 2J3
- [SDR SIMA201911143003](https://openairdocs.org/sdr/SIMA201911143003), Nov 13, 2019: DOOR. BINDING. MAIN CABIN DOOR VERY DIFFICULT FOR FA TO OPEN & CLOSE.-C/A-PERFORMED GVI OF DOOR AND SEALS. PERFORMED OPS CK OF OPEN & CLOSE FUNCTION OF DOOR IAW EMB 145MM 52-1
- [SDR SIMA20190722002](https://openairdocs.org/sdr/SIMA20190722002), Jul 22, 2019: LIGHT. INOPERATIVE. GALLEY OVERHEAD EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED GALLEY OVERHEAD EMERGENCY LIGHT LAMP IAW AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECK
- [SDR SIMA20190628004](https://openairdocs.org/sdr/SIMA20190628004), Jun 28, 2019: BUTTON. DEFECTIVE. CABIN CHIME WOULD NOT STOP DINGING IN FLIGHT. COULD NOT HEAR ATC AND CREW COULD NOT ESTABLISH COMM BETWEEN THE TWO OF US. RETURNED BACK TO BTR AS A RESULT. C/A-
- [SDR SIMA201906110002](https://openairdocs.org/sdr/SIMA201906110002), Jun 10, 2019: CONNECTOR. DAMAGED. SECOND TO LAST EMERGENCY LIGHT FLOOR STRIP INOP. EVALUATED AND FOUND 4 EA DAMAGED WIRE CONNECTORS FOR LAST AND ALSO SECOND TO LAST EMERGENCY LIGHT FLOOR STRIP. 
- [SDR SIMA2019042416006](https://openairdocs.org/sdr/SIMA2019042416006), Apr 16, 2019: CRADLE. INOPERATIVE. FLASHLIGHT ON RH AFT STOWAGE CLOSET LED CHARGE LIGHT INOP.-C/A-REMOVED AND REPLACED FLASHLIGHT CHARGER ASSY IAW EMB-140 AMM 33-50-16. OPS CHECK GOOD.
- [SDR SIMA2019042416005](https://openairdocs.org/sdr/SIMA2019042416005), Apr 16, 2019: TERMINAL. DAMAGED. EMERGENCY EXIT LIGHT STRIP WIRES UNDER 251GF HAVE BROKEN TERMINAL ENDS.-C/A-WIRE TERMINAL ENDS FOR THE EMERGENCY EXIT LIGHT STRIP UNDER 251GF WHERE REPAIRED IAW
- [SDR SIMA2019042216003](https://openairdocs.org/sdr/SIMA2019042216003), Apr 16, 2019: WIRE. BROKEN. LH FLOOR EDGE EMERGENCY LIGHTING STRIP BETWEEN FRAMES 25 - 27 HAS BROKEN WIRE.-C/A-INSTALLED NEW LH EMERGENCY LIGHTING STRIP IAW AMM 23-50-12. REF: NRWC 846-MQT
- [SDR SIMA2019042216002](https://openairdocs.org/sdr/SIMA2019042216002), Apr 16, 2019: FLOORBOARD. CRACKED. CABIN FLOOR BOARD 231EF IS CRACKED IN HALF-C/A-REMOVED AND REPLACED 231EF IAW AMM TASK 53-01-02.
- [SDR SIMA20190414002](https://openairdocs.org/sdr/SIMA20190414002), Apr 14, 2019: LIGHT. INOPERATIVE. EMERGENCY LIGHT STRIP ROW 11 INOP-C/A-DEFERRED EMERGENCY LIGHT STRIP ROW 11 REF: MEL 33-30 AUTH: 040506-C. BROKEN OFF WIRE TERMINAL ENDS UNDER FLOOR PANEL 251GF
- [SDR SIMA2019042414003](https://openairdocs.org/sdr/SIMA2019042414003), Apr 14, 2019: WIRE. DAMAGED. EMERGENCY LIGHT STRIP INOP ON ROW 11 AND 12-C/A-BROKEN OFF WIRE TERMINAL ENDS UNDER FLOOR PANEL 251GF WHERE FOUND AND REPAIRED IAW SPWM 20-21-00 AND C/W OPERATI
- [SDR SIMA201904164002](https://openairdocs.org/sdr/SIMA201904164002), Apr 14, 2019: LIGHT. INOPERATIVE. EMERGENCY LIGHT STRIP ROW 11 INOP. DEFERRED EMERGENCY LIGHT STRIP ROW 11 REF: MEL 33-30 AUTH: 040506-C
- [SDR SIMA20190307002](https://openairdocs.org/sdr/SIMA20190307002), Mar 7, 2019: ROLLER. LACK OF LUBE. MAIN CABIN DOOR IS HARD TO OPEN. C/A-LUBRICATED MAIN CABIN DOOR ROLLERS AND GUIDES AS PER AMM 52-10-00,OPS CHECK GOOD.
- [SDR SIMA201902254002](https://openairdocs.org/sdr/SIMA201902254002), Feb 24, 2019: ROLLER. LACK OF LUBE. MAIN CABIN DOOR DIFFICULT TO OPERATE OPEN AND CLOSE-C/A-LUBED FRAME ROLLERS AND RESECURED STOPS,PERFORMED MAIN DOOR OPEN/CLOSE IAW AMM 52-18-00, OPC GOOD
- [SDR SIMA201812038006](https://openairdocs.org/sdr/SIMA201812038006), Nov 28, 2018: WHEEL. OUT OF LIMITS. UPON PS-1 CHECK FOUND # 4 TIRE WORN OUT OF LIMIT-C/A-REMOVED AND REPLACED # 4 TIRE IAW ENVOY MAIN LANDING GEAR WHEEL ASSY REMOVAL AND INSTALLATION W/C 37-700-11
- [SDR SIMA201810198002](https://openairdocs.org/sdr/SIMA201810198002), Oct 18, 2018: ELECTRONIC UNIT. FAILED. LG FAILED TO RETRACT AFTER TAKEOFF. ENGINE WOULD NOT GO TO CLB OR CRZ MODE.WERE IN ALT T/O-1 FOR @ 15 MIN. GUST LOCK WONT LOCK -C/A-T/S LG FAIL TO RETRACT PER F
- [SDR SIMA201809177002](https://openairdocs.org/sdr/SIMA201809177002), Sep 17, 2018: ADC. FAILED. RED X ON AIRSPEED- ALT- AND VERTICAL SPEED DURING BEGINING OF APPROACH. BROKE OFF APPROACH AND DIVERTED TO ABI- VFR CONDITIONS. RED X'S OCCURED ON MULTIPLE OCCA
- [SDR SIMA20180830001](https://openairdocs.org/sdr/SIMA20180830001), Aug 30, 2018: DOOR. LACK OF LUBE. FA REPORTS MAIN CABIN DOOR RED LEVEL IS VERY HARD TO MOVE OPEN AND CLOSE.-C/A-AT THIS TIME LUBE MAIN CABIN DOOR HANDLE PER STANDAR PRACTICE. OPS CK GOOD PER AMM
- [SDR SIMA201804020001](https://openairdocs.org/sdr/SIMA201804020001), Mar 30, 2018: CONTROL VALVE. FAILED. BRAKE DEGRADED MESSAGE PRESENTED ON EICAS IN FLIGHT AND ON THE GROUND AFTER LANDING. LT INBD FAILED PRESSURE TEST AND SHOWS EXCESSIVE PRESSURE, WITHOUT BRAKES A
- [SDR SIMA20180119004](https://openairdocs.org/sdr/SIMA20180119004), Jan 19, 2018: CONNECTOR. DAMAGED. NR 5 FLOOR EMERGENCY LIGHT INOPERATIVE. R & R THE CONNECTOR IAW SWPM 20-50-01. OPS CHECKED GOOD.
- [SDR SIMA20180118003](https://openairdocs.org/sdr/SIMA20180118003), Jan 18, 2018: CONTROL UNIT. FAILED. PITCH TRIM BACKUP INOPERATIVE, WHEN AUTO PILOT ENGAED. PERFORMED TROUBLESHOOTING IAW FIM. R & R THE HORIZONTAL STABILIZER CONTROL UNIT IAW AMM 27-43-02. OPS CHE
- [SDR SIMA20180115005](https://openairdocs.org/sdr/SIMA20180115005), Jan 15, 2018: ATTACH FITTING. GOUGED. LEFT AILERON DAMPER ATTACH FITTING HINGE IS GOUGED. REMOVED AND REPLACED THE ATTACH FITTING IAW EO EM-27MR-112.
- [SDR SIMA20180115006](https://openairdocs.org/sdr/SIMA20180115006), Jan 15, 2018: ATTACH FITTING. GOUGED. RIGHT AILERON DAMPER ATTACH FITTING HINGE IS GOUGED. REMOVED AND REPLACED THE AILERON DAMPER ATTACH FITTING IAW EO EM-27MR-112.
- [SDR SIMA20171230002](https://openairdocs.org/sdr/SIMA20171230002), Dec 30, 2017: SKIN. CRACKED. RIGHT AFT FUSELAGE SKIN AT FRAME 75 CRACKED ABOVE STRINGER 2R. REPAIRED THE SKIN IAW SRM 53-31-01, FIG 219, SHEET 2.
- [SDR SIMA20171223001](https://openairdocs.org/sdr/SIMA20171223001), Dec 23, 2017: DOOR SILL. CORRODED. CARGO DOOR LOWER SILL IS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA20171223002](https://openairdocs.org/sdr/SIMA20171223002), Dec 23, 2017: DOOR SILL. CORRODED. CARGO DOOR LOWER SILL IS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02
- [SDR SIMA20171219005](https://openairdocs.org/sdr/SIMA20171219005), Dec 19, 2017: FRAME. CRACKED. FRAME 23 CRACKED AT STRINGER 16R. REPAIRED THE FRAME IAW SRM 53-00-04, ITEM 3.
- [SDR SIMA20171218005](https://openairdocs.org/sdr/SIMA20171218005), Dec 18, 2017: SHEAR TIE. CORRODED. FRAME 68 SHEAR TIE IS CORRODED AT CARGO DOOR LOWER SILL AREA. REPAIRED THE SHEAR TIE IAW SRM 53-31-04
- [SDR SIMA20171217005](https://openairdocs.org/sdr/SIMA20171217005), Dec 17, 2017: SHEAR TIE. CORRODED. FRAME 65 SHEAR TIE CORRODED AT THE CARGO DOOR LOWER SILL. REPAIRED THE SHEAR TIE IAW SRM 53-31-04.
- [SDR SIMA20171202006](https://openairdocs.org/sdr/SIMA20171202006), Dec 2, 2017: SIGN. INOPERATIVE. ROW 11 CEILING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT SIGN IAW AMM 33-50-13. OPS CHECKED GOOD.
- [SDR SIMA20171202007](https://openairdocs.org/sdr/SIMA20171202007), Dec 2, 2017: INVERTER. FAILED. EMERGENCY LIGHT LOCATED AT THE AFT OF EMERGENCY EXIT ARE NOT FUNCTIONAL. REMOVED AND REPLACED THE NR 6 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECKED GO
- [SDR SIMA20171202008](https://openairdocs.org/sdr/SIMA20171202008), Dec 2, 2017: SIDEWALL SUPPORT. CORRODED. LEFT OMEGA BEAM SIDEWALL IS CORRODED BETWEEN FRAMES 49-50. REPAIRED THE OMEGA BEAM SIDEWALL IAW ERS-EM-53MR-3067.
- [SDR SIMA20140808003](https://openairdocs.org/sdr/SIMA20140808003), Aug 8, 2014: ROLLER. LACK OF LUBE. MAIN CABIN DOOR VERY HARD TO OPEN. PERFORMED MAIN DOOR INTERNAL ACTUATING HANDLE TEST IAW AMM 52-10-01. LUBRICATED MAIN DOOR ROLLERS. LOAD FALLS WITHIN ALLOWABL
- [SDR SIMA20140804007](https://openairdocs.org/sdr/SIMA20140804007), Aug 4, 2014: BRACKET. CRACKED. BRACKET SUPPORTING RT WING REFUEL TUBE INSIDE ACCESS PANEL 631AB IS CRACKED AT NUT PLATE FOR CLAMP. REPAIRED BRACKET IAW ETN 51-150, INSTALLED IAW SRM 51-40-09.
- [SDR SIMA20140725004](https://openairdocs.org/sdr/SIMA20140725004), Jul 25, 2014: DOOR. OBSTRUCTED. FLIGHT ATTENDANT REPORTED THAT MAIN DOOR IS VERY HARD TO OPEN & CLOSE. FOUND COURTAIN STRAP GETTING BETWEEN PAX DOOR AND DOOR STOP. REPOSITIONED STRAP AND COMPL
- [SDR SIMA20140721013](https://openairdocs.org/sdr/SIMA20140721013), Jul 21, 2014: NUT PLATE. BROKEN. LEFT FWD EMER LIGHT HOUSING HAS BROKEN NUTPLATE. R & R LT FWD EMER LIGHT HOUSING IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140721012](https://openairdocs.org/sdr/SIMA20140721012), Jul 21, 2014: FUSE. BLOWN. LEFT FWD EXTERIOR EMER LIGHT INOPERATIVE. R & R FUSE IN NR 1 EMER LIGHT BATTERY CHARGER IAW CMM 25-60-03. OPERATIONS CHECKED IAW AMM 33-50-04. OPERATIONS CHECKE
- [SDR SIMA20140711003](https://openairdocs.org/sdr/SIMA20140711003), Jul 11, 2014: POWER SUPPLY. DEFECTIVE. FLOOR PROXIMITY STRIP POWERED BY NR 3 EMER BATTERY COMES ON & GOES OFF AFTER FEW SECONDS. R & R NR 3 POWER SUPPLY & BATTERY IAW AMM 33-50-04. OPERATIONS CHECKED
- [SDR SIMA20140419002](https://openairdocs.org/sdr/SIMA20140419002), Apr 19, 2014: VALVE. FAILED. BLEED 2 OVERTEMP CAME ON FOR 2 OR 3 SECONDS THEN WENT OFF. BLEED 2 TEMP WAS IN RED BELOW 10,000 FT MAX CLIMB THRUST. R & R RT FAN AIR VLV IAW AMM 36-11-03. OPER
- [SDR SIMA20140418002](https://openairdocs.org/sdr/SIMA20140418002), Apr 18, 2014: SWITCH. FAULTY. E2 ANTI-ICE FAIL MSG, NR 2 BLEED TEMP IN THE RED, E2 ANTI-ICE VLV OPEN INDICATION, AFTER FEW MINUTES EICAS MSG & OPEN INDICATION EXTINGUISHED. HOWEVER BLEED TEM
- [SDR SIMA20140308003](https://openairdocs.org/sdr/SIMA20140308003), Mar 8, 2014: FLASHLIGHT. BROKEN. FLIGHTDECK FLASHLIGHT ON & OFF SWITCH BROKE OFF. DEFERRED CAPTAIN`S FLASHLIGHT IAW MEL 25-53 AUTH 030374-C. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16, CHECKED 
- [SDR SIMA20140225003](https://openairdocs.org/sdr/SIMA20140225003), Feb 25, 2014: ROLLER. LACK OF LUBE. MAIN CABIN DOOR HARD TO OPEN. CLEANED & LUBED MAIN CABIN DOOR ROLLER PINS IAW AMM 53-21-02, OPERATIONS CHECKED GOOD.
- [SDR SIMA20131012007](https://openairdocs.org/sdr/SIMA20131012007), Oct 12, 2013: INVERTER. INOPERATIVE. FWD EMERGENCY EXIT SIGN BELOW COCKPIT DOOR INOPERATIVE. R & R NR 1 EMERG POWER INVERTER IAW AMM 33-50-11, OPC GOOD.
- [SDR SIMA20131012006](https://openairdocs.org/sdr/SIMA20131012006), Oct 12, 2013: INVERTER. INOPERATIVE. FWD CEILING EMERGENCY EXIT SIGN INOPERATIVE. R & R NR 1 INVERTER, OPS CHECKED GOOD IAW AMM 33-50-11.
- [SDR SIMA20130811001](https://openairdocs.org/sdr/SIMA20130811001), Aug 11, 2013: ROLLER. LACK OF LUBE. F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED MAIN DOOR FRAME ROLLERS IAW 52-21-02.
- [SDR SIMA20130721004](https://openairdocs.org/sdr/SIMA20130721004), Jul 21, 2013: CHECK VALVE. INOPERATIVE. THE CREW REPORTED A BLEED TWO LEAK INDICATION AFTER TAKEOFF AT 900 FT AGL. THE CREW PERFORMED EMERGENCY PROCEDURES. BLEED 2 LEAK INDICATION EXTINGUISHED AFTER A
- [SDR SIMA20130610006](https://openairdocs.org/sdr/SIMA20130610006), Jun 10, 2013: ECU. FAILED. DURING CRUISE, RECEIVED AN EICAS FLAP LOW SPEED AND SPS ADVANCED MESSAGES. COMPLIED WITH AOM, VOL 1 PROCEDURES. ON APPROACH EICAS FLAP FAIL MESSAGE RECEIVED. DE
- [SDR SIMA20130511004](https://openairdocs.org/sdr/SIMA20130511004), May 11, 2013: LIGHT. LOOSE. DURING B INSPECTION FOUND THE PASSENGER DOOR EMERGENCY LIGHT ON PIVOT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED LENS, REMOVED LIGHT BULB, ROTAT
- [SDR SIMA20130422003](https://openairdocs.org/sdr/SIMA20130422003), Apr 22, 2013: HANDLE. MALFUNCTIONED. FLIGHT 3370. MAIN CABIN DOOR WAS DIFFICULT TO OPEN & CLOSE. REMOVED MAIN DOOR HANDLE, RETORQUED PIVOT BUSHING BOLT IAW AMM 20-10-01. RETORQUED BOLTS ON INNER HA

All 91: https://openairdocs.org/aircraft/N846AE/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/N846AE/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.