# N848AE: 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: 145710
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 16, 2003
- Certificate issued: June 11, 2023
- Expires: June 30, 2030
- Mode S code: AB9D96
- 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=848AE
- Page: https://openairdocs.org/aircraft/N848AE

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/N848AE/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 N848AE.

## FAA accident and incident reports (1)

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 20120119000359I](https://openairdocs.org/incident/20120119000359I), Jan 19, 2012: Embraer EMB-135KL (N848AE), Los Angeles, CA, Minor damage. On takeoff roll in sacramento on 19 jan, 2012, American eagle flight 3015 smf-lax, an Embraer 135KL, registration # N848AE, had the left inboard (number 2)…

## Service difficulty reports (81, 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 SIMA20201013001](https://openairdocs.org/sdr/SIMA20201013001), Oct 13, 2020: LAMP. INOPERATIVE. MAIN DOOR CEILING EMERGENCY LIGHT INOPERABLE. C/A: R & R MAIN DOOR CEILING EMERGENCY LIGHT LAMP, IAW AMM TASK 33-50-06-000-801-A AND 33-50-06-400-801-A. OPERATI
- [SDR SIMA2020072616004](https://openairdocs.org/sdr/SIMA2020072616004), Jul 16, 2020: WARNING MESSAGE. FALSE ACTIVATION. BLD 1 LEAK WARNING MSG HOLD SHORT RWY AWAITING EDCT ON ENG 1 (ENG 2 & APU OFF)-C/A-PERFORMED BLEED 1 OPS CHECK IAW EMB 140 AMM 36-00-00-700-803-A. OPS CK GOOD. 
- [SDR SIMA202002265005](https://openairdocs.org/sdr/SIMA202002265005), Feb 25, 2020: CHARGER. INOPERATIVE. OVERWING EMER EXIT LIGHTS INOP-C/A-REMOVED AND REPLACED #4 EMER BATTERY AND BATTERY HOLDER ASSY IAW W/C 33-700-17 AND W/C 33-700-19 OPS CHECK GOOD. EMERGENCY LI
- [SDR SIMA202002198003](https://openairdocs.org/sdr/SIMA202002198003), Feb 18, 2020: LIGHT. INOPERATIVE. R/H OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED R/H OVER WING EMERGENCY LIGHT IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A OPC GOOD END
- [SDR SIMA202002107001](https://openairdocs.org/sdr/SIMA202002107001), Feb 7, 2020: BATTERY PACK. INOPERATIVE. L/H AND R/H HAND AFT EXTERIOR OVER WING EMERGENCY LIGHTS INOP "TRANSFERRED FROM NRWC 848-SGF-03052 ITEM 1" RWK 678084-C/A-L/H AND R/H EXTERIOR OVER WING EMERGEN
- [SDR SIMA202002076002](https://openairdocs.org/sdr/SIMA202002076002), Feb 6, 2020: CHARGER. INOPERATIVE. BOTH EXTERNAL OVERWING AFT EMERGENCY LIGHTS INOP-C/A-TROUBLE SHOT OVERWING AFT EMERGENCY LIGHTS IAW EMB WIRE MANUAL 33-50-50. FOUND #4 EMERGENCY BATTERY AND CHA
- [SDR SIMA202001164003](https://openairdocs.org/sdr/SIMA202001164003), Jan 14, 2020: CLAMP. LOOSE. PACK 1 OVRLD IN FLIGHT STRONG BURNT METALIC ODOR COMING FROM PACK 1. COMP W/ QRH LEFT PACK OFF DUE TO SMELL.-C/A-PERFORM INSPECTION ON PACK 1, FOUND CLAMPS TO B
- [SDR SIMA202001132001](https://openairdocs.org/sdr/SIMA202001132001), Jan 12, 2020: ACM. FAILED. SMOKE IN THE CABIN & COCKPIT ON CLIMB OUT~ 13000 FEET ASSOCIATED WITH BUZZING NOISE ON RH SIDE OF AC-C/A-CW COMPLY WITH EO EM-2100-048 ON THE #1 & 2 PACK DUE TO
- [SDR SIMA2020010229006](https://openairdocs.org/sdr/SIMA2020010229006), Dec 29, 2019: ACM. FAILED. PACK 1 OVERLOAD WITH BURNING SMELL. SMELL WENT AWAY AFTER TURNING PACK 1 OFFPERFORM FIM 21-20-00 FOR BURNING SMELL IN COCKPITREF: LOGPAGE 4528695 ITEM 1-C/A-PER
- [SDR SIMA20190512004](https://openairdocs.org/sdr/SIMA20190512004), May 12, 2019: DOOR. DENTED. PAX SERVICES REPORT DENT ON MAIN CABIN DOOR AFT OF EXTERNAL HANDLE NEAR TRAILING EDGE. C/A-INSPECTED IAW SRM 52-10-01 AND FOUND DENT TO BE IN AREA B AND OUT OF 
- [SDR SIMA2018122019001](https://openairdocs.org/sdr/SIMA2018122019001), Dec 19, 2018: BATTERY. FAILED. BOTH LH AND RH AFT OVERWING EXIT LIGHTS ARE INOP.-C/A-REMOVED AND REPLACED #4 EMERGENCY LIGHT POWER SUPPLY CHARGER ASSY AND BATTERY HOLDER ASSY IAW AMM 33-50-04
- [SDR SIMA201812039003](https://openairdocs.org/sdr/SIMA201812039003), Nov 29, 2018: DAU. MALFUNCTIONED. ABORTED TAKEOFF 90 KNOTS DUE TO MASTER WARNING," TAKE OFF TRIM". ALL TRIMS WERE INDICATING GREEN-C/A-REMOVED AND REPLACED DAU#2 IAW EMB 140 AMM 31-41-01. OPS CH
- [SDR SIMA20181017002](https://openairdocs.org/sdr/SIMA20181017002), Oct 17, 2018: HOLDER. BROKEN. FWD F/A FLASHLIGHT HOLDER BOTTOM PART OF BRACKET IS BROKEN. R&R F/A FLASHLIGHT ASSY IAW AMM 33-50-16.
- [SDR SIMA2018072726002](https://openairdocs.org/sdr/SIMA2018072726002), Jul 26, 2018: LIGHT. INOPERATIVE. PAX DOOR EXTERNAL EMERGENCY LIGHT FAILS TO ILLUNINATE. R&R PAX DOOR EXTERNAL EMERGENCY LIGHT ASSY IAW AMM'S 33-50-10 AND 33-30-02. OPC GOOD IAW AMM 30-50-00-700
- [SDR SIMA201807091001](https://openairdocs.org/sdr/SIMA201807091001), Jul 7, 2018: UNKNOWN. ODOR. BURNING SMELL IN COCKPIT ON POWER UP. FOUND CIRCUIT BREAKER O/C RELAY 1, O/C RELAY 2 POPPED. PERFORMED FIM TASKS 20-21-00-810-801 UP TO STEP 5 BLOCKS 1, 26-29, 
- [SDR SIMA20180625001](https://openairdocs.org/sdr/SIMA20180625001), Jun 25, 2018: BULB. INOPERATIVE. PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-06. OPS CHECKED GOOD.
- [SDR SIMA201805254002](https://openairdocs.org/sdr/SIMA201805254002), May 24, 2018: BRAKE SYS. MALFUNCTIONED. DURING TAXI, UNDER BRAKING ONE OR MORE BRAKE WOULD RELEASE, RE-ENGAGE THEN RELEASE, EVEN UNDER LIGHT BRAKING AT ALL SPEEDS WHILE TAXIING. RAN BRAKE ANALYZER IAW
- [SDR SIMA201805187001](https://openairdocs.org/sdr/SIMA201805187001), May 17, 2018: SEAL. LEAKING. LOUD SQUEAL FROM THE MAIN CABIN DOOR, GOT LOUDER THROUGH FL 230. COMPLIED WITH A MAIN DOOR RUBBER TRIM SEAL FILLER STRIP REPAIR IAW AMM 52-00-01. DOOR OPS CHECK
- [SDR SIMA2018051706001](https://openairdocs.org/sdr/SIMA2018051706001), May 16, 2018: LIGHT. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW MM 33-50-00. OPS CHECKED GOOD.
- [SDR SIMA2018042711009](https://openairdocs.org/sdr/SIMA2018042711009), Apr 11, 2018: SKIN. CRACKED. LEFT REAR FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 2L. THE SKIN WAS REPAIRED IAW SRM 53-31-01.
- [SDR SIMA2018042711008](https://openairdocs.org/sdr/SIMA2018042711008), Apr 11, 2018: SHEAR TIE. CORRODED. FWD SHEAR TIE AT FRAME 65 WAS FOUND CORRODED. THE SHEAR WAS REPAIRED IAW SRM 53-31-04.
- [SDR SIMA201804181004](https://openairdocs.org/sdr/SIMA201804181004), Apr 11, 2018: SKIN. PUNCTURED. RUDDER, RT SKIN PUNCTURED BETWEEN RIBS ZV2938.0, AND 3229. THE RUDDER SKIN WAS REPAIRED IAW SRM 55-40-01.
- [SDR SIMA2018041800002](https://openairdocs.org/sdr/SIMA2018041800002), Apr 10, 2018: SKIN. DAMAGED. DAMAGE ON THE RT SKIN, 2 INCHES FWD OF FRAME 23 AND 1.5 INCHES BELOW STRINGER 19R. REPAIRED IAW 53-21-01.
- [SDR SIMA20180405014](https://openairdocs.org/sdr/SIMA20180405014), Apr 5, 2018: WIRE. DAMAGED. DURING LT SIDE WALL INSTALLATION FOUND LT O/WING EXIT SIGN WIRES DAMAGED. LT O/WING EXIT SIGN WIRES REPAIRED IAW SPWN 20-21-00.
- [SDR SIMA20180405013](https://openairdocs.org/sdr/SIMA20180405013), Apr 5, 2018: ANTI-ICE VALVE. CORRODED. ENGINE BLEED AIR AND ANTI-ICING SYSTEMS, LT WING ANTI-ICING VALVE FOUND WITH CORROSION BEYOND ACCEPTABLE LIMITS (FILTER CAP THREADS INTO VALVE THREADS PORTIONS 
- [SDR SIMA2018101205012](https://openairdocs.org/sdr/SIMA2018101205012), Apr 5, 2018: TRIM PANEL. DAMAGED. CABIN FLOOR PROXIMITY EMERGENCY LIGHT TRIM DAMAGED. -C/A-FLOOR PROXIMITY STRIP LIGHT REPLACED IAW AMM 33-50-12 INSTALLATION COVERED BY TASK PAI715-2.
- [SDR SIMA2018101205008](https://openairdocs.org/sdr/SIMA2018101205008), Apr 5, 2018: DOOR SILL. CORRODED. LT SILL NUMBER 6 CORRODED AT SEVERALS PLACES. -C/A-LT SILL NR 6 CORRODED OUT OF LIMIT IAW SRM 53-23-10 LT SILL NR 6 REPLACED WITH NEW PART AND INSTALLED IAW SRM
- [SDR SIMA2018101205009](https://openairdocs.org/sdr/SIMA2018101205009), Apr 5, 2018: DOOR. DAMAGED. DAMAGE ON MAIN DOOR LOWER EDGE. 7.000" FROM AFT EDGE. -C/A-ON MAIN DOOR LOWER EDGE, 7" FROM AFT ADGE DAMAGE BLENDED AND REPROTECTED IAW SRM 51-10-05 ITEM 4 TYPE
- [SDR SIMA2018101205010](https://openairdocs.org/sdr/SIMA2018101205010), Apr 5, 2018: FLOOR SUPPORT. CORRODED. OMEGA BEAM LOWER FLANGE, BOTH SIDE OF WALKWAY, FOUND CORRODED BTW FR-43 TO FRM 52. -C/A-OMEGA BEAM LOWER FLANGE, BOTH SIDE OF WALKWAY CORROSION BTW FR 43 TO FR 
- [SDR SIMA2018101205011](https://openairdocs.org/sdr/SIMA2018101205011), Apr 5, 2018: BEAM. CORRODED. BAGGAGE DOOR LOWER BEAM CORRODED. -C/A-LOWER BEAM REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR SIMA2018101205007](https://openairdocs.org/sdr/SIMA2018101205007), Apr 5, 2018: FLOOR SUPPORT. CRACKED. LT OMEGA BEAM OUTBD LOWER FLANGE CRACK 6 INCH AFTER FRM-41. -C/A-LT OMEGA BEAM LOWER ANGLES REPAIRED AS PER SRM 53-23-02.
- [SDR SIMA20180405006](https://openairdocs.org/sdr/SIMA20180405006), Apr 5, 2018: DOOR SILL. CORRODED. RT SILL NUMBER 4 CORRODED AT SEVERAL PLACES. RT SILL NUMBER 4 FOUND BEYOND LIMITS CORRODED AT SEVERAL PLACES IAW SRM 53-23-10 RT SILL NUMBER 4 REPLACED WITH NEW
- [SDR SIMA20180405005](https://openairdocs.org/sdr/SIMA20180405005), Apr 5, 2018: DOOR SILL. CORRODED. RT SILL NUMBER 3 CORRODED AT SEVERAL PLACES. RT SILL NR 3 CORRODED OUT OF LIMIT IAW SRM 53-23-10. RT SILL REPLACED WITH NEW PART AND INSTALLED IAW SRM 51-40-02.
- [SDR SIMA2018100105004](https://openairdocs.org/sdr/SIMA2018100105004), Apr 5, 2018: SKIN. CRACKED. LT REAR FUSELAGE SKIN CRACKED AT FRAME 75 AT STR 2L-C/A-LT REAR FUSELAGE SKIN AT FRAME 75 STR 2L REPAIRED IAW SRM 53-31-01 FIG 219 SHEET 2
- [SDR SIMA2018082805003](https://openairdocs.org/sdr/SIMA2018082805003), Apr 5, 2018: STRUCTURE. CORRODED. BAGGAGE DOOR FWD L-SHAPE CORRODED AT FR 65-C/A-IN RF1 AT FR65, FWD L-SHAPE BLENDED, OUT OF LIMITS IAW ETN EM-53-272 AND OLD SEGMENT REMOVED IAW SRM 53-31-04. IN
- [SDR SIMA20150415005](https://openairdocs.org/sdr/SIMA20150415005), Apr 15, 2015: WIRE. DAMAGED. SERVICE DOOR EMER LIGHT INOPERATIVE. SEE IPC 33-50-10-40 FOR LOCATION. REPAIRED WIRE W716-0008-20 IAW WM 20-21-00. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150402003](https://openairdocs.org/sdr/SIMA20150402003), Apr 2, 2015: HOLDER. BROKEN. CAPTAINS FLASHLIGHT HOLDER BROKEN. R & R FLASHLIGHT HOLDER IAW AMM 33-50-16. OPERATIONS CHECKED GOOD. NO FURTHER DEFECT NOTED.
- [SDR SIMA20150329002](https://openairdocs.org/sdr/SIMA20150329002), Mar 29, 2015: FLASHLIGHT. INOPERATIVE. FLIGHT ATTENDANT EMER FLASHLIGHT RED LED INDICATOR INOPERATIVE. R & R FLIGHT ATTENDANT EMER FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150224005](https://openairdocs.org/sdr/SIMA20150224005), Feb 24, 2015: DUCT. CRACKED. NUMBER 2 ENG 14TH STAGE DUCT FROM CUSTOMER SERVICE PANEL CRACKED AT ANTI-ICE VLV END. R & R 14TH STAGE DUCT AT NR 2 ENG CUSTOMER SERVICE PANEL TO ANTI-ICE VLV I
- [SDR SIMA20150204002](https://openairdocs.org/sdr/SIMA20150204002), Feb 4, 2015: ENGINE. FAILED. LAVATORY SMOKE AFTER TAKEOFF, AOM 1 PROCEDURE COMPLIED WITH. FLIGHT ATTENDANT REPORTS SMOKE & FUMES IN CABIN. R & R NR 2 ENGINE IAW WC 71-000-00. OPERATIONS CHE
- [SDR SIMA20150202001](https://openairdocs.org/sdr/SIMA20150202001), Feb 2, 2015: FLASHLIGHT. INOPERATIVE. THE CAPTAIN'S SIDE COCKPIT FLASHLIGHT HAS NO CHARGE. R & R CAPTAIN`S FLASHLIGHT IAW AMM 33-50-16. FOUND GOOD AT THIS TIME.
- [SDR SIMA20150124003](https://openairdocs.org/sdr/SIMA20150124003), Jan 24, 2015: DRAIN LINE. CRACKED. LOW SPEED ABORT APPROX 60 KTS. MX NOT REQUIRED, CONDITIONS NOT MET FOR HIGH ENERGY STOP INSPECTION 05-50-16-200-801-A. REFERENCE NRWC 848-CMI-01730 ERRONEOUS AI
- [SDR SIMA20150123003](https://openairdocs.org/sdr/SIMA20150123003), Jan 23, 2015: LIGHT. INOPERATIVE. SERVICE DOOR EXTERNAL EMER LAMP INOPERATIVE. R & R SERVICE DOOR EMER LIGHT LAMP IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A. OPERATIONS CHECKED GOOD.
- [SDR SIMA20141228003](https://openairdocs.org/sdr/SIMA20141228003), Dec 28, 2014: PITOT SYSTEM. CONTAMINATED. FLASHING IAS AMBER LIGHT ON PFD A/S ON STBY & FIRST OFFICER SIDE SAME ADC 2 SELCETED. PROBLEM CORRECTED, A/S WAS INCREASING ON CA SIDE. DRAINED WATER FROM PITOT
- [SDR SIMA20140824008](https://openairdocs.org/sdr/SIMA20140824008), Aug 24, 2014: LIGHT. NOT SEATED. SERVICE DOOR EMER LIGHT INOPERATIVE. FOUND SERVICE DOOR EMER LIGHT BULB UNSEATED. RESEATED BULB IAW AMM 33-50-10 STEPS 3 J 1 - 3. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140413004](https://openairdocs.org/sdr/SIMA20140413004), Apr 13, 2014: COMPUTER. FAILED. SHORTLY AFTER TAKEOFF AHRS 1 FAIL. ASSOCIATED ATT & HDG FAIL. R & R AHRS IAW AMM 34--21 01, OPERATIONS CHECKED GOOD.
- [SDR SIMA20140329007](https://openairdocs.org/sdr/SIMA20140329007), Mar 29, 2014: FLASHLIGHT. INOPERATIVE. FLASHLIGHT DOESN'T HOLD CHARGE. R & R WHOLE ASSEMBLY IAW AMM 33-50-16, OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR SIMA20131219001](https://openairdocs.org/sdr/SIMA20131219001), Dec 19, 2013: STALL WARNING. FALSE ACTIVATION. FLIGHT 2848 AFTER SHUTDOWN, WITH BOTH ENGINES OFF APU ON, GPU OFF, SPS1 INOP, SPS ADVANCED ALERTS ON EICAS & AOA COMPARATOR LIGHT ON PFD1 APPEARED. MASTER WARNI
- [SDR SIMA20130422001](https://openairdocs.org/sdr/SIMA20130422001), Apr 21, 2013: FLOOR SUPPORT. CORRODED. DURING MAINTENANCE INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 25 AND 28. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR IAW EMBRAER S
- [SDR SIMA20130421002](https://openairdocs.org/sdr/SIMA20130421002), Apr 21, 2013: FITTING. GOUGED. DURING MAINTENANCE INSPECTION FOUND THE RIGHT AILERON BRACKET WHERE DAMPER ATTACHES GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DAMPER F

All 81: https://openairdocs.org/aircraft/N848AE/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/N848AE/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.