# N857AE: 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: 145752
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 18, 2003
- Certificate issued: April 13, 2023
- Expires: April 30, 2030
- Mode S code: ABC15E
- Registered owner: [Delux Public Charter LLC](https://openairdocs.org/faa-owner/DELUX%20PUBLIC%20CHARTER%20LLC)
- Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas)
- Owner type: LLC
- Owner's area on the map: 32.8483° N, 96.8255° W: Placed by OpenAirDocs at the center of ZIP code 75209, 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=857AE
- Page: https://openairdocs.org/aircraft/N857AE

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/N857AE/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 N857AE.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20060719016239I](https://openairdocs.org/incident/20060719016239I), Jul 19, 2006: Emb EMB135KL (N857AE), Roscoe, IL. (-23) On 07/19/2006 at approximately 0930 CDT the home of [privacy data omitted] was struck by a large piece of ice estimated to weight in excess of ten…
- [Incident 20041101027189I](https://openairdocs.org/incident/20041101027189I), Nov 1, 2004: Emb EMB135KL (N857AE), Miami, FL, Minor damage. (-23) Flight 4350, operated by American eagle from cleveland to Miami, was descending through 15,000 feet on the approach to Miami when a large bird struck the…

## Reports on N857AE not matched to an aircraft (1)

They name N857AE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19891230063089I](https://openairdocs.org/incident/19891230063089I), Dec 30, 1989: Bag JETSTM3201 (N857AE), Fort Myers, FL, Minor damage. Navigation instrument problems. Followed by a burning smell and electrical problems. Declared emergency and landed.

## Service difficulty reports (73, 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 SIMA20210728001](https://openairdocs.org/sdr/SIMA20210728001), Jul 28, 2021: DOOR. LACK OF LUBE. MAIN CABIN DOOR UNUSUALLY DIFFICULT TO OPEN.-C/A-LUBRICATED MAIN PAX CABIN DOOR IAW AMM 52-18-00 OPT CK GOOD.
- [SDR SIMA20210629001](https://openairdocs.org/sdr/SIMA20210629001), Jun 29, 2021: CONTROL VALVE. DEGRADED. MECHANICAL/BRAKE DEGRADED MESSAGE. EMERGENCY DECLARED. LANDED SAFELY - PREVIOUS CREW REPORTS BRAKE DEGRADED MSG AFTER CONFIGURING FOR LANDING"TRANSFERRED TO NRW
- [SDR SIMA20210611001](https://openairdocs.org/sdr/SIMA20210611001), Jun 11, 2021: CRADLE. INOPERATIVE. AFT CABIN EMERGENCY FLASHLIGHT HOLDER INOP-C/A-RAR AFT CABIN EMERGENCY FLASHLIGHT HOLDER PER AMM 33-50-16. OPS CK GOOD.
- [SDR SIMA20210609002](https://openairdocs.org/sdr/SIMA20210609002), Jun 9, 2021: ROLLER. LACK OF LUBE. MAIN CABIN DOOR STRUGGLES TO OPEN. MUST BE SHOOK HARD BACK AND FORTH TO OPEN-C/A-LUBED MAIN CABIN DOOR ROLLERS IAW AMM 53-21-02. OPS CHECK GOOD
- [SDR SIMA20210517002](https://openairdocs.org/sdr/SIMA20210517002), May 17, 2021: UNKNOWN. ODOR. CAPT REPORT BURNING SMELL IN THE CKPIT AT FL330. NO EMERGENCY DECALRED. REFERENCE LOG PAGE 4562659 ITEM 2 AIRCRAFT REQUIRES ADITIONAL TROUBLE SHOOTING FOR BURNI
- [SDR SIMA20210420001](https://openairdocs.org/sdr/SIMA20210420001), Apr 20, 2021: SIGN. INOPERATIVE. 3BC EMERGENCY EXIT LIGHT INOP-C/A-RAR EXIT MARKING SIGN ASSY IN FRONT OF SEAT 3B IAW EMB145 AMM 33-50-14. OPC GOOD.
- [SDR SIMA20210420002](https://openairdocs.org/sdr/SIMA20210420002), Apr 20, 2021: ROLLER. LACK OF LUBE. CREW REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN-C/A-CLEANED AND LUBRICATED MAIN DOOR ROLLERS OPC GOOD IAW EMB 145 AMM 52-18-00
- [SDR SIMA20210322001](https://openairdocs.org/sdr/SIMA20210322001), Mar 22, 2021: HOLDER. BROKEN. FA FLASHLIGHT HOLDER HAS BROKEN CLAMP.-C/A-RAR FA FLASHLIGHT HOLDER IAW ETN-EM 33-059.
- [SDR SIMA202009065001](https://openairdocs.org/sdr/SIMA202009065001), Sep 5, 2020: LIGHT. INOPERATIVE. ROW 10 FLOOR EMERGENCY LIGHT STRIP DAMAGED. C/A RAR ROW 10 FLOOR EMERGENCY LIGHT STRIP IAW EMB 140 AMM 33-50-12. OPERATIONS CHECK GOOD.
- [SDR SIMA202007310004](https://openairdocs.org/sdr/SIMA202007310004), Jul 30, 2020: LIGHT. INOPERATIVE. 1ST LT EMERGENCY LIGHT STRIP INOPERATIVE. R & R THE EMERGENCY LIGHT STRIP IAW AMM 140 33-50-12. OPS CHECKED GOOD.
- [SDR SIMA2020073029001](https://openairdocs.org/sdr/SIMA2020073029001), Jul 29, 2020: LIGHT. INOPERATIVE. MAIN DOOR EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. DID NOT FIX. REP
- [SDR SIMA202006154001](https://openairdocs.org/sdr/SIMA202006154001), Jun 14, 2020: HANDLE. MALFUNCTIONED. PARKING BRAKE HANDLE CANNOT BE SET. REMOVED AND REPLACED EMERGENCY/PARKING BRAKE HANDLE IAW AMM 32-44-11. OP CHECKED GOOD.
- [SDR SIMA2020060131001](https://openairdocs.org/sdr/SIMA2020060131001), May 31, 2020: GUIDE. DIRTY. FLIGHT ATTENDANT STILL REPORTING PAX DOOR STICKY & DIFFICULT TO OPEN, 2ND WRITE UP ON ISSUE. CLEANED DOOR GUIDES AND LUBED ROLLERS, PERFORMED DOOR OPEN AND CLOS
- [SDR SIMA2020041609002](https://openairdocs.org/sdr/SIMA2020041609002), Apr 9, 2020: SKIN. DENTED. SKIN DENTED 5" AFT OF FR 19 AND 2.350" BELOW STR 1`2L.-C/A-DENTED FUSELAGE SKIN 5.000 "AFT OF FR 19 AND 2.350 BELOW STR RL 12L REPAIRED IN ACCORANCE WITH ETD 20
- [SDR SIMA2020041701005](https://openairdocs.org/sdr/SIMA2020041701005), Apr 1, 2020: STRUCTURE. CORRODED. CORROSION ON FR 80 APU SHUNT AREA-C/A-CORROSION BLENDED OUT OF LIMIT ON FR 80 APU SHUNT AREA. ON FR 80 APU SHUNT AREA REPAIR PARTS ARE FABRICATED AS PER SRM 53-
- [SDR SIMA2020041431001](https://openairdocs.org/sdr/SIMA2020041431001), Mar 31, 2020: PROFILE. CRACKED. VERT.STAB., AFT SPAR3, L/H PROFILE CRACKED ABOVE RUDDER 1 TOP CENTER HINGE FITTING.-C/A-VERT.STAB., AFT SPAR 3, L/H PROFILE ABOVE RUDDER 1 TOP CENTER HINGE FITT
- [SDR SIMA2020042026006](https://openairdocs.org/sdr/SIMA2020042026006), Mar 26, 2020: SKIN. GOUGED. GOUGE ON PAX DOOR SKIN, ON AFT EDGE AND 10.00" ABOVE LOWER EDGE.-C/A-ON PAX DOOR SKIN GOUGE AREA STRIPED FOR INVESTIGATION. GOUGE ON PAX DOOR SKIN AT AFT EDGE A
- [SDR SIMA2020042218007](https://openairdocs.org/sdr/SIMA2020042218007), Mar 18, 2020: SKIN. DAMAGED. CHERRY MAX FOUND ON SKIN AT FR 28 AND STR 17 LH.-C/A-PAINT STRIPPED SKIN AT FR 28 AND STR 17 L/H AS PER 51-21-01. AIR CONDITIONING DUCTS BETWEEN WINDOW L/H #4-5
- [SDR SIMA2020042118006](https://openairdocs.org/sdr/SIMA2020042118006), Mar 18, 2020: SKIN. DAMAGED. CHERRY MAX FOUND ON SKIN AT FR 25 BTW FR 18-19LH.-C/A-PAINT STRIPPED SKIN AT FR 75 BTW FR 18-19 L/H AS PER CPM 51-21-01. CHERRY MAX REMOVED AND CUT OUT PERFORME
- [SDR SIMA202003097003](https://openairdocs.org/sdr/SIMA202003097003), Mar 7, 2020: TIRE. VIBRATION. EXCESSIVE NLG SHIMMY VIBRATION BETWEEN 20-40 KNOTS WITH STEERING CNTERED. NO VIBRATION OFF CENTER-C/A-REMOVED AND REPLACED LEFT NLG TIRE IAW WC 32-700-17
- [SDR SIMA202003029002](https://openairdocs.org/sdr/SIMA202003029002), Feb 29, 2020: LIGHT. INOPERATIVE. FWD CABIN EMERGENCY EXIT SIGN AT SEAT 3BC LIGHT INOP-C/A-REMOVED AND REPLACED FWD CABING EMERGENCY EXIT SIGN LIGHT AT SEAT 3BC IAW EMB 140 AMM 33-50-13. OPS CHE
- [SDR SIMA201912065002](https://openairdocs.org/sdr/SIMA201912065002), Dec 5, 2019: CONTROL MODULE. FAILED. EMERG LT NOT ARMED CAUTION MSG ON TAKE OFF AT APPROX 100 KIAS. THEN INTERMITTENTLY APPROX EVERY 3 MIN IN FLIGHT.-C/A-UPON FUTHER INSPECTION FOUND C/P FOR COCKPI
- [SDR SIMA20190926003](https://openairdocs.org/sdr/SIMA20190926003), Sep 26, 2019: WARNING SYSTEM. ACTIVATED. DURING FLIGHT IN ICING CONDITIONS STAB A/ICE FAIL MESSAGE APPEARED, FOLLOWED BY ICE-COND - A/I INOP WARNING-C/A-CMC FAULT CODE 30-IPM75. FLIGHT CREW PLACARDED S
- [SDR SIMA20190316002](https://openairdocs.org/sdr/SIMA20190316002), Mar 16, 2019: ROLLER. LACK OF LUBE. MAIN CABIN DOOR IS DIFFICULT TO OPEN. C/A-PERFORMED GVI OF MAIN DOOR FOUND TWO AFT ROLLERS NOT MOVING CLEAN AND LUB ROLLERS AS PER AMM 53-21-02 OPC GOOD.
- [SDR SIMA201812073008](https://openairdocs.org/sdr/SIMA201812073008), Dec 3, 2018: SKIN. DENTED. TRANSFERRED FROM AML 4424546 ITEM 3, FOUND LARGE DENT WITH GAUGE BETWEEN STGR 12R & 14R AND BETWEEN FR 22A & 23. W=4.875IN, L=9.125IN, DEPTH=0.218IN. THIS IS A 
- [SDR SIMA201812073007](https://openairdocs.org/sdr/SIMA201812073007), Dec 3, 2018: STRINGER. CRACKED. STR 13R IS CRACKED BETWEEN FR 22A-23.-C/A-REMOVED AND REPLACED STR 13R BETWEEN FR 22A-23 IAW SRM 51-40-02
- [SDR SIMA2018043029002](https://openairdocs.org/sdr/SIMA2018043029002), Apr 29, 2018: LIGHT. INOPERATIVE. FLOOR EMERGENCY LIGHT BETWEEN ROWS 7 AND 8 FOUND INOPERATIVE.
- [SDR SIMA201805018010](https://openairdocs.org/sdr/SIMA201805018010), Apr 28, 2018: PUMP. FAILED. NR 1 ENGINE HYD PUMP FAILED. REMOVED AND REPLACED THE HYD PUMP IAW AMM 29-10-03.
- [SDR SIMA20180306001](https://openairdocs.org/sdr/SIMA20180306001), Mar 6, 2018: UPLOCK. FAILED. DURING RETRACTION, LEFT MLG DID NOT INDICATE UP INDICATION FOLLOWED BY LG LEVER DISAGREE WARNING MESSAGE REMOVED AND REPLACED LT MLG UPLOCK BOX IAW AMM 32-33-10
- [SDR SIMA20180225002](https://openairdocs.org/sdr/SIMA20180225002), Feb 25, 2018: ANTI-ICE VALVE. FAILED. NR 1 ENGINE ANTI-ICE VALVE CYCLING OPEN & CLOSED. SHOULD REMAIN OPEN. EICAS MESSAGES WOULD COME AND GO AS WELL. PUTTING ICE DETECTION KNOB TO ENGINE OR ALL E1 S
- [SDR SIMA20180203001](https://openairdocs.org/sdr/SIMA20180203001), Feb 3, 2018: DAU. FAILED. DAU NR 1A FAILED. TROUBLESHOOT IAW FIM 31-41-00. REMOVED AND REPLACED THE NR 1 DAU IAW AMM 31-41-00, OPS CHECKED GOOD, NO DFECTS NOTED.
- [SDR SIMA20180117006](https://openairdocs.org/sdr/SIMA20180117006), Jan 17, 2018: INVERTER. INOPERATIVE. COCKPIT STEP EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11 OPC GOOD.
- [SDR SIMA20171004007](https://openairdocs.org/sdr/SIMA20171004007), Oct 4, 2017: WIRE. BROKEN. EMERGENCY LIGHT NR 6 HAS A BROKEN WIRE. R & R THE EMERGENCY LIGHT CONNECTOR IAW SWPM 20-21-00. OPS CHECKED GOOD.
- [SDR SIMA20171004010](https://openairdocs.org/sdr/SIMA20171004010), Oct 4, 2017: WIRE. BROKEN. LT NR 1 EMERGENCY LIGHT HAS BROKEN WIRES. R & R THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD.
- [SDR SIMA20171004005](https://openairdocs.org/sdr/SIMA20171004005), Oct 4, 2017: DOOR FRAME. CORRODED. CARGO DOOR FWD FRAME CORRODED AT 4 NUTPLATE HOLES. REPAIRED THE DOOR FRAME IAW ERS EM-52MR-822.
- [SDR SIMA20171004009](https://openairdocs.org/sdr/SIMA20171004009), Oct 4, 2017: WIRE. BROKEN. LEFT NR 3 EMERGENCY LIGHT HAS BROKEN WIRES. R & R THE WIRES IAW AMM 33-50-12. OPS CHECKED GOOD.
- [SDR SIMA20171004006](https://openairdocs.org/sdr/SIMA20171004006), Oct 4, 2017: WIRE. BROKEN. LH FORWARD LOWER FAIRING EMERGENCY LIGHT HAS A BROKEN WIRE. REPAIRED THE WIRE IAW SWPM 20-21-00.
- [SDR SIMA20141208003](https://openairdocs.org/sdr/SIMA20141208003), Dec 8, 2014: BATTERY. DISCHARGED. COCKPIT STEP EMER LIGHT INOPERATIVE. R & R NR 1 EMER BATTERY & CHARGER IAW WC 33-700-19. REF ITEM 2 THIS NRWC FOR OPERATIONS CHECK. EMER LIGHTING BATTERY PN 201
- [SDR SIMA20141001001](https://openairdocs.org/sdr/SIMA20141001001), Oct 1, 2014: CRADLE. BROKEN. FIRST OFFICER`S EMER FLASHLIGHT CRADLE BROKEN. R & R IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR SIMA20140804006](https://openairdocs.org/sdr/SIMA20140804006), Aug 4, 2014: UNKNOWN. ODOR. STRONG SMELL OF JET FUEL IN COCKPIT & CABIN WHILE TAXIING IN WITH ENGS SUPPLYING PACKS. SMELL WENT AWAY WITH APU RUNNING & SUPPLYING PACKS. COMPLIED WITH AE ETN
- [SDR SIMA20140603002](https://openairdocs.org/sdr/SIMA20140603002), Jun 3, 2014: CRADLE. BROKEN. EMERGENCY FLASHLIGHT CRADLE ABOVE FLIGHT ATTENDANT SEAT BROKEN. R & R FLIGHT ATTENDANT FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A, OPERAT
- [SDR SIMA20140323011](https://openairdocs.org/sdr/SIMA20140323011), Mar 23, 2014: FLASHLIGHT. INOPERATIVE. FLIGHT ATTENDANT FLASHLIGHT WAS DISCOVERED IN LAVATORY & INOPERATIVE. DEFERRED IAW MEL 25-53. INSTALLED FLIGHT ATTENDANT FLASHLIGHT IAW CMM 25-60-11. OPERATIONA
- [SDR SIMA20140323004](https://openairdocs.org/sdr/SIMA20140323004), Mar 23, 2014: CRADLE. BROKEN. COCKPIT FLASHLIGHT CRADLE BROKEN, CAPTAIN`S SIDE. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140323003](https://openairdocs.org/sdr/SIMA20140323003), Mar 23, 2014: HANDLE. OUT OF POSITION. MAIN CABIN DOOR VERY DIFFICULT TO OPEN. REPOSITIONED HANDLE BACK ON SPLINE IAW AMM 52-18-05. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140321005](https://openairdocs.org/sdr/SIMA20140321005), Mar 21, 2014: FLASHLIGHT. INOPERATIVE. FLIGHT ATTENDANT FWD JUMP SEAT FLASHLIGHT IS INOPERATIVE. REPLACED FLASHLIGHT IAW CMM 25-60-11.
- [SDR SIMA20131118006](https://openairdocs.org/sdr/SIMA20131118006), Nov 18, 2013: LIGHT. INOPERATIVE. LEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. C/A R & R LT AFT OVERWING EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-07, OPERATIONS CHECKED GOOD.
- [SDR SIMA20130826005](https://openairdocs.org/sdr/SIMA20130826005), Aug 26, 2013: LINE. LEAKING. FUEL ODOR IN FLIGHT DECK AFTER APU & NR 1 ENGINE START. RETURNED TO GATE, R & R APU "OUT" FUEL LINE AT FUEL CONTROL, REF AMM 49-32-01. OPS CHECKED GOOD, NO LEAK
- [SDR SIMA20130728005](https://openairdocs.org/sdr/SIMA20130728005), Jul 28, 2013: ACM. ODOR. INTERMITTENT OIL ODOR AT VARIOUS TIMES DURING PACK OPERATION. ODOR WOULD OCCUR THEN VERY QUICKLY DISSIPATE. R & R LT ACM, OPS CHECKED GOOD IAW AMM 21-51-03 AND 
- [SDR SIMA20130728006](https://openairdocs.org/sdr/SIMA20130728006), Jul 28, 2013: ACM. ODOR. SITTING AT GATE WITH PCA CONNECTED, STARTED TO SMELL EXTREMELY STRONG OIL ODOR. MX STARTED APU, DISCONNETED PCA, TURNED NR 2 AND SAME ODOR RETURNED IN COCKPIT N
- [SDR SIMA20130722003](https://openairdocs.org/sdr/SIMA20130722003), Jul 22, 2013: ENGINE. FAILED. DURING CRUISE FL 330, NOTICED OIL LEVEL WAS 7 QTS ON NR 1 ENGINE. NR 1 ENGINE ITT WENT INTO CAUTION SO THEY PULLED TL BACK HALFWAY. ITT CAME DOWN THEN SHOT INTO

All 73: https://openairdocs.org/aircraft/N857AE/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/N857AE/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.