# N853AE: 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: 145742
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 29, 2003
- Certificate issued: December 5, 2023
- Expires: December 31, 2030
- Mode S code: ABB282
- 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=853AE
- Page: https://openairdocs.org/aircraft/N853AE

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/N853AE/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 N853AE.

## FAA accident and incident reports

None matched to N853AE.

## Service difficulty reports (72, 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 SIMA202003065003](https://openairdocs.org/sdr/SIMA202003065003), Mar 5, 2020: LIGHT. INOPERATIVE. AFT ROW CABIN EMERGENCY LIGHT STRIP INOP-C/A-REMOVED ANS REPLACED AFT ROW CABIN EMERGENCY LIGHT STRIP IAW EMB 140 AMM 33-50-12. OPS CHECKED GOOD.
- [SDR SIMA202002132005](https://openairdocs.org/sdr/SIMA202002132005), Feb 12, 2020: HANDLE. LACK OF LUBE. EMERGENCY BRAKE VERY HARD TO ACTUATE RELEASEING BRAKE IS EASY SETTING BRAKE VERY HARD AND STICK-C/A-LUBEBRAKE HANDLE IAW AMM 324410. OPS CHECK IS GOOD
- [SDR SIMA20200212001](https://openairdocs.org/sdr/SIMA20200212001), Feb 12, 2020: HANDLE. BINDING. PARKING BRAKE HANDLE DIFFUCULT TO SET HANDLE STICKS IN OFF POSITION.-C/A-LUBRICATED ENERGENCY /PARKING BRAKE CONTROL IAW AMM 32-44-10. OPS CHECK GOOD
- [SDR SIMA202001132003](https://openairdocs.org/sdr/SIMA202001132003), Jan 12, 2020: LIGHT. MALFUNCTIONED. EMERGENCY FLOOR STRIP LIGHT ROW 16 INOP-C/A-DEFERRED EMERGENCY FLOOR STRIP ROW 16 PER MEL 33-30 AUTH #010450-C. T/S ROW 16 FLOOR PROXIMTY LIGHT AND PREFORMED EM
- [SDR SIMA20190507003](https://openairdocs.org/sdr/SIMA20190507003), May 7, 2019: OIL SYSTEM. LOW. OIL QTY DROPPED TO 5 QT ON NR 2 ENGINE AFTER START OIL QTY FLUCTUATED BETWEEN 6 QT AND 8 QT AFTER ENGINE NR 2 WAS SHUT DOWN AGAIN. C/A-SERVICED OIL ON E2 TO 12 
- [SDR SIMA20190103002](https://openairdocs.org/sdr/SIMA20190103002), Jan 3, 2019: CHARGER. INOPERATIVE. EMERGENCY LIGHTING BATTERY NR 2 WILL NOT HOLD A CHARGE. C/A-T/S EMERGENCY LIGHTING AND FOUND NR 2 EPSU CHARGER INOP. REMOVED AND REPLACED NR 2 EMERGENCY CHARGER
- [SDR SIMA201808076002](https://openairdocs.org/sdr/SIMA201808076002), Aug 6, 2018: ACCUMULATOR. UNDERSERVICED. EMERGENCY BRAKE LOW PRESSURE MESSAGE DURING FLIGHT. SERVICED THE EMERGENCY BRAKE ACCUMULATOR. 2400 PSI IAW 32-44-02, AMBIENT PRESSURE AT 84F. FIGURE 301 FOR PRE
- [SDR SIMA2018080227002](https://openairdocs.org/sdr/SIMA2018080227002), Jul 27, 2018: ISIS. FAILED. STANDBY ATTITUDE INDICATOR FLICKERS AND GOES COMPLETELY BLANK DURING CLIMB, DESCENT, DURING LANDING ROLL , AND DURING TAXI. REPEAT WRITE UP. REMOVED AND REPLACE
- [SDR SIMA20180622004](https://openairdocs.org/sdr/SIMA20180622004), Jun 22, 2018: WARNING MESSAGE. FALSE ACTIVATION. SPOILER FAIL AFTER LANDING GEAR RETRACTED, VERIFIED IT WORKED PROPERLY IN AIR, MESSAGE WENT AWAY WITH LANDING GEAR EXTENDED. PREVIOUS CMC FAULT CODE 27-SPM17. T
- [SDR SIMA2018032700002](https://openairdocs.org/sdr/SIMA2018032700002), Mar 26, 2018: LAMP. INOPERATIVE. RIGHT OVERWING EMRGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMPS IAW AMM 33-50-10. OPS CHECKED GOOD.
- [SDR SIMA20180313001](https://openairdocs.org/sdr/SIMA20180313001), Mar 13, 2018: GROUND WIRE. DISCONNECTED. AFT CABIN FLASHLIGHT NOT CHARGING RED LIGHT NOT ILLUIMINATED. TROUBLESHOT IAW AMM 33-51-00, WM 33-51-50. FOUND A GROUND WIRE DISCONNECTED. CONNECTED THE WIRE IA
- [SDR SIMA20180125007](https://openairdocs.org/sdr/SIMA20180125007), Jan 25, 2018: FRAME. CRACKED. FUSELAGE FRAME 23 IS CRACKED BETWEEN STRINGERS 15R AND 16R. REPAIRED FRAME 23 RT BETWEEN STRINGERS 15R & 16R IAW ERS-EM-53MR-3161 AND SRM FRAME REPAIR 53-00-04.
- [SDR SIMA20180125008](https://openairdocs.org/sdr/SIMA20180125008), Jan 25, 2018: STRIP. DAMAGED. EMERGENCY LIGHT STRIP EXTRUSIONS NR 1-6 AND 8 ARE DAMAGED. REMOVED AND REPLACED EMERGENCY LIGHT STRIP EXTRUSIONS 1-6 AND 8 IAW AMM 33-50-12N.
- [SDR SIMA20150125001](https://openairdocs.org/sdr/SIMA20150125001), Jan 25, 2015: SIGNAL COND UNIT. FAILED. EICAS FUEL IMBALANCE FUEL FLUX 500 - 800 LBS IN FLIGHT. R & R FCU IAW MM 28-41-01. FUEL QTY CHECKS GOOD IAW MM 28-41-00 MEL ITEM RESTORED.
- [SDR SIMA20141211003](https://openairdocs.org/sdr/SIMA20141211003), Dec 11, 2014: LIGHT. INOPERATIVE. RIGHT UPPER WING EMER LIGHT INOPERATIVE. R & R RT UPPER WING EMER LIGHT LAMP IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140522005](https://openairdocs.org/sdr/SIMA20140522005), May 22, 2014: SWITCH. MALFUNCTIONED. PTRIM BACKUP INOPERATIVE CAME ON DURING CLIMB THROUGH 13,000 FT & 270 KTS. NO TRIM SWITCH ACTIVATION, AUTO PILOT WAS OFF. R & R BACKUP CUT OUT SWITCH IAW AMM 20
- [SDR SIMA20140510004](https://openairdocs.org/sdr/SIMA20140510004), May 10, 2014: BATTERY. DEFECTIVE. FIRST OFFICER`S FLASHLIGHT NEEDS REPLACING. STRONG CHEMICAL ODOR COMING FROM BATTERIES OF FLASHLIGHT. R & R FIRST OFFICER'S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16
- [SDR SIMA20140421001](https://openairdocs.org/sdr/SIMA20140421001), Apr 21, 2014: WINDSHIELD. CRACKED. CLIMBING FL190, FIRST OFFICER`S WINDSHIELD SPONTANEOUSLY CRACKED. R & R FIRST OFFICER`S WINDSHIELD IAW AMM 56-10-01.
- [SDR SIMA20140214001](https://openairdocs.org/sdr/SIMA20140214001), Feb 14, 2014: FLASHLIGHT. INOPERATIVE. FLIGHT ATTENDANT`S FLASHLIGHT ON OVERHEAD OF JUMP SEAT IS NOT CHARGING PROPERLY. R & R FLASH LIGHT & CRADLE ASSEMBLY ON OVERHEAD OF FLIGHT ATTENDANT`S JUMP SEAT
- [SDR SIMA20140115003](https://openairdocs.org/sdr/SIMA20140115003), Jan 15, 2014: FLASHLIGHT. INOPERATIVE. FORWARD CABIN FLASHLIGHT INOPERATIVE NOT CHARGING. R & R FWD CABIN FLASHLIGHT IAW AMM 33-51-01, OPERATIONS CHECKED GOOD.
- [SDR SIMA20140106005](https://openairdocs.org/sdr/SIMA20140106005), Jan 6, 2014: FLASHLIGHT. MALFUNCTIONED. FIRST OFFICER`S FLASHLIGHT RED CHARGING LIGHT NOT COMING ON. RESET FIRST OFFICER`S FLASHLIGHT, OPERATIONS CHECKED GOOD IAW AMM CH 33-51-01.
- [SDR SIMA20131215001](https://openairdocs.org/sdr/SIMA20131215001), Dec 15, 2013: HOLDER. BROKEN. FLIGHT ATTENDANT`S REAR FLASHLIGHT HOLDER BROKEN. R & R FLIGHT ATTENDANT`S AFT FLASHLIGHT HOLDER & FLASHLIGHT IAW EMB-140 AMM 33-50-16, OPERATIONS CHECKED GOOD.
- [SDR SIMA20130626003](https://openairdocs.org/sdr/SIMA20130626003), Jun 26, 2013: CRADLE. BROKEN. DURING B INSPECTION, FOUND THE FLASHLIGHT FOR THE F/O CRADLE BROKEN. THE ACFT WAS REMOVED FROM SERVICE. R & R THE F/O FLASHLIGHT CRADLE ASSY IAW AMM 33-50-16. T
- [SDR SIMA20130528004](https://openairdocs.org/sdr/SIMA20130528004), May 28, 2013: CHECK VALVE. FAULTY. THE CREW REPORTED A STRONG METALIC ODOR AFTER TAKEOFF, SLIGHTY STRONGER IN DESCENT AFTER ON PHEUMATIC ICE TEST. THE ACFT WAS REMOVED FROM SERVICE. FOUND E2 OIL 
- [SDR SIMA20130527003](https://openairdocs.org/sdr/SIMA20130527003), May 27, 2013: FAN. FAULTY. THE CREW REPORTED THAT IMMEDIATELY AFTER TAKEOFF THEY NOTICED A STRONG ODOR, SMELL, FUMES THROUGHOUT THE ACFT. THE CREW DECLARED AN EMERGECNY AND RETURNED TO DE
- [SDR SIMA20130409001](https://openairdocs.org/sdr/SIMA20130409001), Apr 9, 2013: FRAME. CRACKED. DURING MAINTENANCE INSPECTION FOUND FRAME 23 CRACKED AT RIGHT FLOOR SILL. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR IAW AEA EO-EM-53MR-1808. THE A
- [SDR SIMA20130329008](https://openairdocs.org/sdr/SIMA20130329008), Mar 29, 2013: HOLDER. INOPERATIVE. DURING MAINTENANCE INSPECTION FOUND BATTERY HOLDER ASSEMBLY P/N 2013-1A S/N 107226 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BATTE
- [SDR SIMA20130318003](https://openairdocs.org/sdr/SIMA20130318003), Mar 18, 2013: FLASHLIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM# 33-
- [SDR SIMA20130111003](https://openairdocs.org/sdr/SIMA20130111003), Jan 11, 2013: WINDSHIELD. MALFUNCTIONED. ON FLIGHT 4359 THE CREW REPORTED THAT DURING CRUISE THEY NOTICED A STRONG ELECTRICAL SMOKE SMELL IN THE COCKPIT. THE FLIGHT ATTENDANT NOTICED IT FROM HER JUMPSE
- [SDR SIMA20121122002](https://openairdocs.org/sdr/SIMA20121122002), Nov 22, 2012: FLASHLIGHT. DEFECTIVE. ON FLIGHT 3279 THE CREW REPORTED AN ODOR IN THE COCKPIT. THE ODOR SEEMED TO BE COMING FROM THE GLARESHIELD; (LIKE DEAD ANIMAL). THE AIRCRAFT WAS REMOVED FROM SE
- [SDR SIMA20121107002](https://openairdocs.org/sdr/SIMA20121107002), Nov 7, 2012: FLASHLIGHT. INOPERATIVE. ON FLIGHT 3602 THE CREW REPORTED THE FLIGHT ATTENDANT’S AFT FLASHLIGHT DID NOT WORK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FAULTY FLASHLIGHT WITH NEW 
- [SDR SIMA20121023004](https://openairdocs.org/sdr/SIMA20121023004), Oct 23, 2012: HOLDER. BROKEN. ON FLIGHT 3135 THE CREW REPORTED THE FLASHLIGHT HOLDER BEHIND THE CAPTAIN’S SEAT WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAP
- [SDR SIMA20121009002](https://openairdocs.org/sdr/SIMA20121009002), Oct 9, 2012: BATTERY. UNSERVICEABLE. DURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHT BATTERY ASSEMBLY NEEDED TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED
- [SDR SIMA20120919004](https://openairdocs.org/sdr/SIMA20120919004), Sep 19, 2012: BATTERY. DISCHARGED. DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY EXTERIOR LIGHTS WOULD NOT WORK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY A
- [SDR SIMA20120712003](https://openairdocs.org/sdr/SIMA20120712003), Jul 12, 2012: LAMP. INOPERATIVE. DURING MAINTENANCE INSPECTION, FOUND THE RIGHT SIDE OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT SIDE OVE
- [SDR SIMA20120704002](https://openairdocs.org/sdr/SIMA20120704002), Jul 4, 2012: LIGHT. INOPERATIVE. DURING B INSPECTION FOUND THE EMERGENCY LIGHT ABOVE FLIGHT ATTENDANT SEAT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY 
- [SDR SIMA20120516004](https://openairdocs.org/sdr/SIMA20120516004), May 16, 2012: BATTERY. DISCHARGED. DURING MAINTENANCE INSPECTION FOUND THE RIGHT AND LEFT OVER THE WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NE
- [SDR SIMA20120509003](https://openairdocs.org/sdr/SIMA20120509003), May 9, 2012: BATTERY. DISCHARGED. DURING B INSPECTION FOUND THE OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY ASSEMBLY IAW AMM 33-
- [SDR SIMA20120508002](https://openairdocs.org/sdr/SIMA20120508002), May 8, 2012: LIGHT. INOPERATIVE. DURING B-INSPECTION FOUND THE OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OVERWING EMERGENCY LIGHTS IA
- [SDR SIMA20120503002](https://openairdocs.org/sdr/SIMA20120503002), May 3, 2012: LIGHT. WRONG PART. ON FLIGHT 2776 THE CREW REPORTED THEY NOTICED THE WRONG STRIP ON EMERGENCY LIGHTS ON THE FLOOR AFT OF FORWARD EXIT DOORS. THE AIRCRAFT WAS REMOVED FROM SERVICE.
- [SDR SIMA20120304001](https://openairdocs.org/sdr/SIMA20120304001), Mar 4, 2012: RETAINING RING. MISSING. DURING MAINTENANCE INSPECTION FOUND THE MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE. HANDLE STICKS AT 10:00 POSITION. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND
- [SDR SIMA2012058016](https://openairdocs.org/sdr/SIMA2012058016), Feb 26, 2012: FLASHLIGHT. OUT OF POSITION. DURING MTX INSPECTION CREW MEMBER FOUND FLASHLIGHT MISSING. RESTORATION OF MEL ITEMS. FOUND FLASHLIGHT AND REINSTALLED IAW EMB 140 MM CHAPTER 33-50-16. OPERATIO
- [SDR SIMA2012016005](https://openairdocs.org/sdr/SIMA2012016005), Jan 12, 2012: SOLENOID VALVE. INOPERATIVE. FOR FLIGHT 3017 THE CREW REPORTED THAT DURING APU START ATTEMPT APU ROTATION STOPS AT 29% EICAS MESSAGE "APU FAIL" PRESENTED. SMOKE REPORTED BY GROUND CREW COMI
- [SDR SIMA2011353009](https://openairdocs.org/sdr/SIMA2011353009), Dec 18, 2011: LAMP. INOPERATIVE. DURING MAINTENANCE BASE VISIT FOUND THE RIGHT SIDE CENTER FAIRING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RI
- [SDR SIMA2011350001](https://openairdocs.org/sdr/SIMA2011350001), Dec 15, 2011: FLASHLIGHT. MALFUNCTIONED. FOR FLIGHT 3074 THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL SMOKE ODOR COMING FROM THE GALLEY AREA. PACK 2 WAS ON POWERED BY APU, NO ENGS RUNNING. THE AIRCRAFT 
- [SDR SIMA201109404](https://openairdocs.org/sdr/SIMA201109404), Mar 31, 2011: BEAM. CORRODED. DURING MAINTENANCE BASE VISIT FOUND THE LEFT CENTER AISLE BEAM RUNNING ALONG Y=-479, VERTICAL SIDE TO HAVE CORROSION AT APPROXIMATELY AFT OF FRAME 49 ABOVE CARB
- [SDR SIMA201109403](https://openairdocs.org/sdr/SIMA201109403), Mar 31, 2011: BRACKET. CRACKED. DURING MAINTENANCE BASE VISIT FOUND PASSENGER MAIN DOOR HANDLE BRACKET CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BRACKET IAW AEAI EO 
- [SDR SIMA201109102](https://openairdocs.org/sdr/SIMA201109102), Mar 31, 2011: FRAME. CRACKED. DURING MAINTENANCE BASE VISIT INSPECTION FOUND FRAME 23 CRACKED AT FLOOR LEVEL. THE AIRCRAFT WAS REMOVED FROM SERVICE. CRACK AT FLOOR LEVEL ON FRAME 23 HAS BEEN
- [SDR SIMA201109101](https://openairdocs.org/sdr/SIMA201109101), Mar 31, 2011: BRACKET. CRACKED. DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE PASSENGER MAIN DOOR HANDLE BRACKET CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BRACK
- [SDR SIMA201032202](https://openairdocs.org/sdr/SIMA201032202), Nov 18, 2010: BATTERY. DISCHARGED. DURING MAINTENANCE BASE CHECK FOUND THE REAR EMERGENCY LIGHTS WOULD NOT TURN ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 BATTERY AND CH

All 72: https://openairdocs.org/aircraft/N853AE/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/N853AE/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.