# N852AE: 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: 145736
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 25, 2003
- Certificate issued: May 12, 2023
- Expires: May 31, 2030
- Mode S code: ABAECB
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=852AE
- Page: https://openairdocs.org/aircraft/N852AE

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/N852AE/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 N852AE.

## FAA accident and incident reports

None matched to N852AE.

## Service difficulty reports (101, 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 SIMA20210506001](https://openairdocs.org/sdr/SIMA20210506001), May 6, 2021: FLASHLIGHT. MISSING. AFT FA EMERGENCY FLASHLIGHT MISSING REF: LOGPAGE 4561877 ITEM 1MEL 2532 - AUTH# 050040M-C-C/A-INSTALLED MISSING AFT FA EMERGENCY FLASHLIGHT IAW EMB 145 AMM 33-5
- [SDR SIMA20210503001](https://openairdocs.org/sdr/SIMA20210503001), May 3, 2021: FLASHLIGHT. MISSING. AFT FA EMERGENCY FLASHLIGHT MISSING-C/A-FLIGHT CREW PLACARDED AFT FA FLASHLIGHT M PROCEDURE C/W AUTH# 050040M-C REF# 25-32 MOC# 206396
- [SDR SIMA20210502002](https://openairdocs.org/sdr/SIMA20210502002), May 2, 2021: CRADLE. DAMAGED. FA EMERGENCY FLASHLIGHT BRACKET DAMAGED-C/A-RAR FA FLASHLIGHT IAW EMB 140 AMM 33-50-16. OPS CHECK GOOD.
- [SDR SIMA20210324004](https://openairdocs.org/sdr/SIMA20210324004), Mar 24, 2021: CRADLE. BROKEN. FWD FA EMERGENCY FLASH LIGHT HOLDER BROKEN MEL 2532 - AUTH# 030305M-CLOGPAGE: 4643803-C/A-FWD FA EMERGENCYFLASHLIGHT ASSY RAR IAW EMB 140 AMM 33-50-16. OPS CHK 
- [SDR SIMA20210321001](https://openairdocs.org/sdr/SIMA20210321001), Mar 21, 2021: CRADLE. BROKEN. FWD FA EMRGENCY FLASH LIGHT HOLDER BROKEN-C/A-FLIGHT CREW PLACARDED PER MEL2532 AUTH030305MC MOC 135181 M PROC C/W
- [SDR SIMA20210304002](https://openairdocs.org/sdr/SIMA20210304002), Mar 4, 2021: SEAL. STICKING. PAX DOOR LOUD VIBRATION IN FLIGHT - PRESSURIZATION TEST FOR CABIN LEAKAGE REQUIRED FOR REAR ELECTRONIC COMPARTMENT DOOR REPAIR. REF NRWC 852-DFW-3500 "REAR AVIO
- [SDR SIMA202007130001](https://openairdocs.org/sdr/SIMA202007130001), Jul 10, 2020: CONNECTOR. LOOSE. UPPER SERVICE DOOR EMERGENCY EXIT PLACARD INOP. T/X IAW FIM 33-50-00-810-804-A FOUND INVERTER 2 CONNECTOR BACKSHELL LOOSE. TIGHTENED BACKSHELL IN REFERENCE WITH
- [SDR SIMA202006109002](https://openairdocs.org/sdr/SIMA202006109002), Jun 9, 2020: LIGHT. INOPERATIVE. LAST ROW FLOOR EMERGENCY LIGHT STRIP INOP. REMOVED AND REPLACED LAST ROW FLOOR EMERGENCY LIGHT STRIP IAW AMM 33-50-12 STEP 4 J2, STEP 5 I-J. ETN-EM-33-058.
- [SDR SIMA2020031710005](https://openairdocs.org/sdr/SIMA2020031710005), Feb 10, 2020: ANGLE. CRACKED. L/H OMEGA BEAM, BOTH JOINING ANGLES CRACKED (OUTBD ANGLE CRACKED BTWN FR 47-48 AND INBD ANGLE CRACKED AT FR 50-C/A-L/H OMEGA BEAM INBD ANGLE REMOVED FOR ACCESS 
- [SDR SIMA2020031710007](https://openairdocs.org/sdr/SIMA2020031710007), Feb 10, 2020: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON L/H OMEGA BEAM LOWER FLANGE, AT ANCHOR NUT LOCATION (FR23)-C/A-ON L/H OMEGA BEAM LOWER FLANGE CORROSION BLENDED OUT OF LIMITS CORRODED AREA O
- [SDR SIMA2020031710006](https://openairdocs.org/sdr/SIMA2020031710006), Feb 10, 2020: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON L/H OMEGA BEAM LOWER FLANGE, AT ANCHOR NUT LOCATION (FR23)-C/A-ON L/H OMEGA BEAM LOWER FLANGE CORROSION, BLENDED OUT OF LIMITS CORRODED AREA 
- [SDR SIMA2020031110003](https://openairdocs.org/sdr/SIMA2020031110003), Feb 10, 2020: CROSSBEAM. CORRODED. ALUMINUM CORSSBEAM AT FR 20 AND FR 24 CORRODED-C/A-ALUMINIUM CROSSBEAM AT FR 24 COVER ON WC 53-2241 AT FR 20 ALUMINIUM CROSS BEAM BLENDED OUT OF LIMIT PART REPL
- [SDR SIMA2020031110004](https://openairdocs.org/sdr/SIMA2020031110004), Feb 10, 2020: CROSSBEAM. CORRODED. ALUMINIUM CROSS BEAM BTW FR 24-25 CORRODED-C/A-BTW FR 24-25 CROSS BEAM BLENDED OUT OF LIMIT PART REPLACED (PN: EPN M53EP1284-01) AND INSTALLED AS PER ETN EM-53-
- [SDR SIMA202002076001](https://openairdocs.org/sdr/SIMA202002076001), Feb 6, 2020: INDICATOR. MALFUNCTIONED. FUEL QUANTITY AMBER DASHES WHILE ENROUTE-C/A-PERFORMED OPS CHK OF ELEC FUEL QTY, SYS. REF. AMM 28-41-00. OPS CHK GOOD NO DEFECTS NOTED
- [SDR SIMA202001232003](https://openairdocs.org/sdr/SIMA202001232003), Jan 22, 2020: HANDLE. LOOSE. MAIN PAX DOOR DIFFICULT TO OPEN.-C/A-TIGHTENED HANDLE & PERFORMED SUCCESFUL OPS CHECK OF PASSENGER DOOR REF E140 AMM 52-10-01
- [SDR SIMA201912165001](https://openairdocs.org/sdr/SIMA201912165001), Dec 15, 2019: LIGHT. UNKNOWN. GALLEY CEILING EMERGENCY EXIT SIGN INOP-C/A-PERFORMED OPC OF EMERGENCY LIGHT SYSTEM IAW EMB 140 AMM 33-50-00. OPC GOOD
- [SDR SIMA201912109001](https://openairdocs.org/sdr/SIMA201912109001), Dec 9, 2019: SCREW. LOOSE. FA'S LED FLASHLIGHT WONT CHARGE-C/A-FOUND MOUNTING SCREW TO BE PROTRUDING. RAI FLASHLIGHT BASE IAW EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-A OPC GOOD
- [SDR SIMA201911154002](https://openairdocs.org/sdr/SIMA201911154002), Nov 14, 2019: FLASHLIGHT. MISSING. ON POST FLIGHT REAR F/A FLASH LIGHT MISSING-C/A-INSTALLED NEW FLASH LIGHT AT REAR CABIN IN REF TO E140 AMM 33-50-16. OPC GOOD
- [SDR SIMA20190515005](https://openairdocs.org/sdr/SIMA20190515005), May 15, 2019: WARNING SYSTEM. FALSE ACTIVATION. DURING CLIMBOUT RECIEVED FUEL 2 LO LEVEL MESSAGE AND LOST TANK 1 INDICATING. C/A-PERFORMED FUEL QTY INDICATION OPS CHK IAW AMM 28-41-00. OPC CHK OK AT THIS TIME
- [SDR SIMA20190321004](https://openairdocs.org/sdr/SIMA20190321004), Mar 21, 2019: LIGHT. INOPERATIVE. MAIN DOOR EMERGENCY LIGHT INOP. C/A-RAR MAIN DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A OPC GOOD AT THIS TIME.END.
- [SDR SIMA20190128001](https://openairdocs.org/sdr/SIMA20190128001), Jan 28, 2019: CONNECTOR. DIRTY. ON CLIMBOUT AT 20,000 FEET NR 1 FUEL QTY INDICATOR WAS INTERMITTENT THEN WENT OUT AND FOLLOWED BY NR 2 FUEL QTY INDICATOR GOING OUT (ALL DASHES) WITH AN EICAS M
- [SDR SIMA20180922001](https://openairdocs.org/sdr/SIMA20180922001), Sep 22, 2018: ROLLER. LACK OF LUBE. MAIN DOOR HARD TO OPEN FROM OUTSIDE. LUBRICATE THE MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02. OPT GOOD.
- [SDR SIMA20180808001](https://openairdocs.org/sdr/SIMA20180808001), Aug 8, 2018: BULB. BURNED OUT. REAR CABIN FLASHLIGHT NOT WORKING. FOUND THE BULB TO BE BURNED OUT. REMOVED AND REPLACED THE AFT FLASHLIGHT ASSY, OPS CHECKED GOOD IAW AMM 33-50-16.
- [SDR SIMA201806185006](https://openairdocs.org/sdr/SIMA201806185006), Jun 15, 2018: HYDRAULIC SYSTEM. LEAKING. HYD SYS 1 LOW QTY TICKED DOWN TO BOTTOM OF AMBER RANGE. TRANFERED HYD FLUID FROM SYTEM 2 TO SYSTEM 1 IAW ETN-EM-29-023 AND SERVICED IAW AMM 12-13-01-600-801-A .
- [SDR SIMA2018052118003](https://openairdocs.org/sdr/SIMA2018052118003), May 18, 2018: WARNING MESSAGE. FALSE ACTIVATION. CARGO DOOR SHOWS OPEN WHEN CLOSED. TESTED THE CARGO DOOR WARNING SWITCHES IAW AMM 52-76-01. OPS CHECKED GOOD. NO DEFECTS NOTED.
- [SDR SIMA2018041600011](https://openairdocs.org/sdr/SIMA2018041600011), Apr 13, 2018: UNKNOWN. ODOR. ON LANDING, A FAINT ODOR OF OIL FROM PACKS. SWITCHED TO APU AFTER SHUTTING OFF BOTH PACKS. NO ODOR ON APU BLEED. PERFORMED ZERO CARBON SEAL LEAK CHECK AND ENGIN
- [SDR SIMA20180311001](https://openairdocs.org/sdr/SIMA20180311001), Mar 11, 2018: FLASHLIGHT. INOPERATIVE. FWD CABIN FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT AT FWD CABIN IN REFERENCE WITH AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. NO FURTHER DISCREPANCIE
- [SDR SIMA20180308003](https://openairdocs.org/sdr/SIMA20180308003), Mar 8, 2018: CONTROL PANEL. FAILED. DURING DESCENT, RECEIVED A LAVATORY SMOKE WARNING, FOLLOWED AOM 1 PROCEDURES. FLIGHT ATTENDENT SAID THERE WAS NO FIRE OR SMOKE BUT AN UNUSUAL ODOR. THE WARNING 
- [SDR SIMA20180123008](https://openairdocs.org/sdr/SIMA20180123008), Jan 23, 2018: CRADLE. BROKEN. FA EMERGENCY FLASHLIGHT HOLDER ASSEMBLY BROKEN. REMOVED AND REPLACED THE FLASHLIGHT & HOLDER IAW AMM 33-50-16-000-801-A, AND 33-50-16-400-801-A. NO FURTHER DEFE
- [SDR SIMA20171231003](https://openairdocs.org/sdr/SIMA20171231003), Dec 31, 2017: BULB. INOPERATIVE. RIGHT OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW 33-50-10.
- [SDR SIMA20171227002](https://openairdocs.org/sdr/SIMA20171227002), Dec 27, 2017: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM BETWEEN FRAMES 27 AND 29 HAS CORROSION. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-3052.
- [SDR SIMA20171222005](https://openairdocs.org/sdr/SIMA20171222005), Dec 22, 2017: CONNECTOR. DAMAGED. NR 8 CABIN EMERGENCY LIGHT STRIP CONNECTOR DAMAGED. REMOVED AND REPLACED THE CONNECTOR IAW SWPM 20-21-00.
- [SDR SIMA20171222004](https://openairdocs.org/sdr/SIMA20171222004), Dec 22, 2017: CONNECTOR. MISSING. NR 2 CABIN EMERGENCY LIGHT STRIP MISSING A CONNECTOR. INSTALLED THE CONNECTOR IAW SWPM 20-21-00.
- [SDR SIMA20171222006](https://openairdocs.org/sdr/SIMA20171222006), Dec 22, 2017: CONNECTOR. DAMAGED. NR 7 CABIN EMERGENCY LIGHT STRIP CONNECTOR DAMAGED. REMOVED AND REPLACED THE CONNECTOR IAW SWPM 20-21-00.
- [SDR SIMA20171217004](https://openairdocs.org/sdr/SIMA20171217004), Dec 17, 2017: LIGHT. INOPERATIVE. NR 1 PROXIMITY LIGHT STRIP IS INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-12.
- [SDR SIMA20171216003](https://openairdocs.org/sdr/SIMA20171216003), Dec 16, 2017: RIB. CRACKED. RIGHT ELEVATOR INBD HINGE INBD LEADING EDGE RIB CRACKED. REMOVED AND REPLACED THE RIB IAW SRM 51-40-02.
- [SDR SIMA20171215014](https://openairdocs.org/sdr/SIMA20171215014), Dec 15, 2017: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM SIDEWALL CORRODED BETWEEN FRAMES 44 - 45. ACCOMPLISHED A REPAIR ON THE OMEGA BEAM IAW SRM 53-00-10.
- [SDR SIMA20171212007](https://openairdocs.org/sdr/SIMA20171212007), Dec 12, 2017: DOOR SILL. CORRODED. SERVICE DOOR CENTER SILL IS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02, AND 51-20-01.
- [SDR SIMA20171208004](https://openairdocs.org/sdr/SIMA20171208004), Dec 8, 2017: SHEAR TIE. CORRODED. FRAME 65 SHEAR TIE CORRODED. REPAIRED THE SHEAR TIE IAW SRM 53-31-04, FIGURE 213.
- [SDR SIMA20171208005](https://openairdocs.org/sdr/SIMA20171208005), Dec 8, 2017: DOOR SILL. CORRODED. CARGO DOOR LOWER SILL IS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA20171208002](https://openairdocs.org/sdr/SIMA20171208002), Dec 8, 2017: SKIN. DENTED. DENT FOUND BELOW GPU DOOR. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-12-01 .
- [SDR SIMA20171208003](https://openairdocs.org/sdr/SIMA20171208003), Dec 8, 2017: STRUCTURE. CORRODED. MAIN DOOR CORRODED AROUND LOWER NUTPLATE HOLES. REMOVED AND REPLACED THE MAIN DOOR LOWER AFT SECTION IAW SRM 51-40-02, 51-20-03, AND 51-40-09.
- [SDR SIMA20171116008](https://openairdocs.org/sdr/SIMA20171116008), Nov 16, 2017: CROSSBEAM. CORRODED. CROSSBEAM AT FR 20 IS CORRODED. REMOVED AND INSTALLED SERVICEABLE CROSSBEAM AT FRAME 20 IAW SRM 51-40-02.
- [SDR SIMA20171116007](https://openairdocs.org/sdr/SIMA20171116007), Nov 16, 2017: PROFILE. CRACKED. RIGHT OVERWING EMERGENCY EXIT FWD PROFILE CRACKED IN THE UPPER BAY. REMOVED AND REPLACED THE RT OVERWING EMERGENCY EXIT DOOR IAW AMM 52-21-00.
- [SDR SIMA20171116006](https://openairdocs.org/sdr/SIMA20171116006), Nov 16, 2017: LIGHT. DAMAGED. LEFT PROXIMITY LIGHT AT SIDEWALLS NR 1 THRU 8 ARE DAMAGED. REMOVED AND REPLACED THE LIGHT STRIP IAW AMM 33-50-12.
- [SDR SIMA20171116005](https://openairdocs.org/sdr/SIMA20171116005), Nov 16, 2017: BULB. INOPERATIVE. RIGHT OVERWING EXIT EXTERNAL AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-10. OPS CHECKED GOOD.
- [SDR SIMA20141109004](https://openairdocs.org/sdr/SIMA20141109004), Nov 9, 2014: LIGHT. INOPERATIVE. SERVICE DOOR EXTERNAL EMER LAMP INOPERATIVE. R & R IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR SIMA20140807002](https://openairdocs.org/sdr/SIMA20140807002), Aug 7, 2014: UNKNOWN. ODOR. IN FLIGHT GETTING ACRID SMELL IN COCKPIT & CABIN, NO SMOKE WAS PRESENT, ODOR WAS NOT OVERPOWERING WITH RECENT ENG JUST NEEDS ADDRESSING NOTABLE ON CLIMB & CRUIS
- [SDR SIMA20140724005](https://openairdocs.org/sdr/SIMA20140724005), Jul 24, 2014: UNKNOWN. ODOR. STRONG ENG OIL SMELL IN MAIN CABIN THRU NR 2 PACK, COCKPIT OK & NO SMELL. SUSPECT NR 2 ENG. DETERMINED PROBABLE CAUSE OF SMELL TO BE FROM NEW NR 2 HEAT EXCHANGE
- [SDR SIMA20140716006](https://openairdocs.org/sdr/SIMA20140716006), Jul 16, 2014: PUMP. FAILED. NUMBER 1 HYD QTY LOW. GEAR DEPLOYED WITH FREE FALL HANDLE. GEAR PINS INSTALLED. R & R NR 1 ENG HYD PUMP IAW AMM 29-10-03. OPERATIONS CHECKED GOOD. LEAK CHECKED 

All 101: https://openairdocs.org/aircraft/N852AE/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/N852AE/stcs.md

## Related

- Other Embraer EMB-135KL aircraft: https://openairdocs.org/model/embraer-emb-135kl/aircraft.md
- The Rolls-Royce AE3007 series engine: https://openairdocs.org/engine/rolls-royce-ae3007-series.md

---
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