# N842AE: 2002 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: 145673
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 21, 2002
- Certificate issued: August 3, 2023
- Expires: August 31, 2030
- Mode S code: AB874C
- 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=842AE
- Page: https://openairdocs.org/aircraft/N842AE

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/N842AE/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 N842AE.

## FAA accident and incident reports

None matched to N842AE.

## Service difficulty reports (84, 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 SIMA20210405002](https://openairdocs.org/sdr/SIMA20210405002), Apr 5, 2021: BATTERY. MISSING. AFT CABIN EMERGENCY FLASHLIGHT MISSING BATTERY MEL 25-32 AUTH# 040011M-C REF AML PG.4689073 ITEM 1-C/A-INSTALLED BATTERY IN AFT CABIN EMERGENCY FLASHLIGHT IAW E
- [SDR SIMA20210401002](https://openairdocs.org/sdr/SIMA20210401002), Apr 1, 2021: BATTERY. MISSING. F/A REPORTED EMERGENCY FLASHLIGHT MISSING BATTERY AT AFT CABIN. C/A-DEFERRED AFT CABIN EMERGENCY FLASHLIGHT PER MEL 25-32. C/W MEL PROCEDURE.
- [SDR SIMA20210324002](https://openairdocs.org/sdr/SIMA20210324002), Mar 24, 2021: CRADLE. BROKEN. FWD FA EMEREGNCY FLASHLIGHT BRACKET BROKEN MEL 2532 AUTH# 03-330M-C AML PAGE 4720750 ITEM 1-C/A-REMOVED AND REPLACED FWD FA EMERGENCY FLASHLIGHT ASSEMBLY IAW EM
- [SDR SIMA20210323001](https://openairdocs.org/sdr/SIMA20210323001), Mar 23, 2021: CRADLE. BROKEN. FA EMERGENCY FLASHLIGHT BRACKET BROKEN-C/A-DEFFERED FWD F/A EMERGENCYFLASHLIGHT. COMPLIED WITH "M" PROCEDURE.
- [SDR SIMA202009132002](https://openairdocs.org/sdr/SIMA202009132002), Sep 12, 2020: BATTERY PACK. INOPERATIVE. EMERGENCY BATTERY NR 3 INOPERABLE. C/A REMOVED AND REPLACED NR 3 EMERGENCY BATTERY AND CHARGER ASSEMBLY, IAW AMM 33-50-04. OPERATIONAL CHECK GOOD.
- [SDR SIMA202007073001](https://openairdocs.org/sdr/SIMA202007073001), Jul 3, 2020: CHARGER. INOPERATIVE. REMOVED AND INSTALLED EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-50-04. OPS CHECKED GOOD. EMERGENCY LIGHT CHARGER.
- [SDR SIMA2020060126010](https://openairdocs.org/sdr/SIMA2020060126010), Mar 26, 2020: LIGHT. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE ON MOST FWD AND MOST AFT CABIN CEILING PANELS. REMOVED AND REPLACED LIGHT BULBS ON THE FWD AND AFT MOST CEILING PANELS IAW AMM 33-5
- [SDR SIMA202001131003](https://openairdocs.org/sdr/SIMA202001131003), Jan 11, 2020: LAMP. INOPERATIVE. RH EXTERNAL OVERWING EMERGENCY LIGHT FAILS TO ILLUMINATE.-C/A-REMOVED AND REPLACED RH OVER WING EMERGENCY LIGHT LAMP IAW AMM 33-50-01. OPS CHECK GOOD, NO FURTHE
- [SDR SIMA202001063002](https://openairdocs.org/sdr/SIMA202001063002), Jan 3, 2020: LAMP. INOPERATIVE. L/H OVER WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED L/H OVER WING EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECK GOOD
- [SDR SIMA2020010228006](https://openairdocs.org/sdr/SIMA2020010228006), Dec 28, 2019: FAN. INOPERATIVE. SMELL IN COCKPIT WHILE TAXING-C/A-UPON INSPECTION FOUND GRINDING NOISE TO BE COMING FROM RECIRC FAN. REMOVED RECIRC FAN 2 IAW EMB 140 AMM 21-24-01 AND FOUND TO 
- [SDR SIMA201912032001](https://openairdocs.org/sdr/SIMA201912032001), Dec 2, 2019: CHARGER. INOPERATIVE. AFT PAX EMERGENCY LIGHTS INCLUDING OVER WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED BATTERY POWER SUPPLY & BATTERY PACK #4 IAW AMM 33-50-04 OPS CHK GOOD.
- [SDR SIMA201911185002](https://openairdocs.org/sdr/SIMA201911185002), Nov 15, 2019: LAMP. INOPERATIVE. RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A OPC GOOD.
- [SDR SIMA20191101001](https://openairdocs.org/sdr/SIMA20191101001), Nov 1, 2019: POWER SUPPLY. FAILED. EMERGENCY LIGHTING BATTERY ASSY/ BATTERY CHARGER REPLACEMENT REQUIRED FOR BATTERY POWER SUPPLY #3-C/A-REMOVED AND REPLACED BATTERY POWER SUPPLY #3 IAW ENVOY W/C
- [SDR SIMA201910285003](https://openairdocs.org/sdr/SIMA201910285003), Oct 25, 2019: BULB. INOPERATIVE. L/H CENTER FAIRING EXT EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED L/H CENTER FAIRING EXT EMERGENCY LIGHT BULB IAW EMB I45 AMM 33-50-10 OPS CHECK GOOD NO FURT
- [SDR SIMA20190905001](https://openairdocs.org/sdr/SIMA20190905001), Sep 5, 2019: ROLLER. LACK OF LUBE. MAIN CABIN DOOR VERY HARD TO OPEN. C/A-LUBRICATRED MAIN AIRFRAME ROLLERS CABIN DOOR IAW AMM 53-21-02.
- [SDR SIMA201811298005](https://openairdocs.org/sdr/SIMA201811298005), Nov 28, 2018: LIGHT. INOPERATIVE. LH OVERWING LIGHT INOP-C/A-REMOVED AND REPLACED LH OVERWING LIGHT IAW EMB 140 AMM 33-50-10 OPS CK GOOD
- [SDR SIMA20181126003](https://openairdocs.org/sdr/SIMA20181126003), Nov 26, 2018: POWER SUPPLY. INOPERATIVE. CABIN EMERG LT IS ON-C/A-UPON THROUBLESHOOTING FOUND BATTERY POWER SUPPLY INOP, REMOVED AND REPLACED BATTERY POWER SUPPLY AND FOR PRECAUTIONARY PURPOSE RAR BATT
- [SDR SIMA20180815016](https://openairdocs.org/sdr/SIMA20180815016), Aug 15, 2018: LIGHT. DAMAGED. #5 LT EMERGENCY LIGHT STRIP EXTRUSION IS DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED #5 LT EMERGENCY LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE BOW301252 FOR OP
- [SDR SIMA20180815015](https://openairdocs.org/sdr/SIMA20180815015), Aug 15, 2018: LIGHT. INOPERATIVE. EXTERNAL EMERGENCY LIGHT ON LT OVERWING PANEL INOP. C/A-COMPLETE:REMOVED AND REPLACED BULB ON EXTERNAL EMERGENCY LIGHT ON LT OVERWING PANEL IAW AMM 33-50-10 OPS
- [SDR SIMA20180815014](https://openairdocs.org/sdr/SIMA20180815014), Aug 15, 2018: SKIN. CORRODED. SSI 53-20-07 FUSELAGE INTERNAL SKIN IS CORRODED BETWEEN FR 37-38 STR 21L-21R.(MARKED). C/A-COMPLETE:PERFORMED REPAIR OF FUSELAGE INTERNAL SKIN IS CORRODED BETWE
- [SDR SIMA20180815013](https://openairdocs.org/sdr/SIMA20180815013), Aug 15, 2018: SKIN. CRACKED. FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 3 FASTNERS ON FR 79 RT SIDE BELOW VERITCAL STAB. C/A-COMPLETE:REPAIRED FUSELAGE EXTERNAL SKIN CRACK ON FRAME 79 RT SIDE
- [SDR SIMA20180815012](https://openairdocs.org/sdr/SIMA20180815012), Aug 15, 2018: LIGHT. DAMAGED. #1 AND #4 FLOOR EMERGENCY LIGHT STRIPS DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED #4 #1 FLOOR EMERGENCY LIGHT STRIP IAW AMM 33-50-12. SEE BOW301252 FOR OPC.
- [SDR SIMA20180815011](https://openairdocs.org/sdr/SIMA20180815011), Aug 15, 2018: LIGHT. DAMAGED. #3 LT EMERGENCY LIGHT STRIP EXTRUSION IS DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED #3 LT EMERGENCY LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE BOW301252 FOR OP
- [SDR SIMA20180815010](https://openairdocs.org/sdr/SIMA20180815010), Aug 15, 2018: LIGHT. DAMAGED. #1 LT EMERGENCY LIGHT STRIP EXTRUSION IS DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED #1 LT EMERGENCY LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE BOW301252 FOR OP
- [SDR SIMA20180815009](https://openairdocs.org/sdr/SIMA20180815009), Aug 15, 2018: LIGHT. DAMAGED. #7 LT EMERGENCY LIGHT STRIP EXTRUSION IS DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED #7 LT EMERGENCY LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE BOW301252 FOR OP
- [SDR SIMA20180815008](https://openairdocs.org/sdr/SIMA20180815008), Aug 15, 2018: FLOOR SUPPORT. CRACKED. LT OMEGA BEAM FWD DIGITAL TO AFT DIGITAL INBD INTERCONNECT BRACKET IS CRACKED. C/A-COMPLETE:REMOVED AND REPLACED LT OMEGA BEAM FWD DIGITAL TO AFT DIGITAL INBD I
- [SDR SIMA20180815007](https://openairdocs.org/sdr/SIMA20180815007), Aug 15, 2018: LIGHT. DAMAGED. #4 LT EMERGENCY LIGHT STRIP EXTRUSION IS DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED #4 LT EMERGENCY LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE BOW301252 FOR OP
- [SDR SIMA20180815017](https://openairdocs.org/sdr/SIMA20180815017), Aug 15, 2018: DOOR SILL. CRACKED. FR 23 IS CRACKED AT RT OUTBD FLOOR SILL. C/A-COMPLETE:REPAIRED FR 23 AT RT OUTBD FLOOR SILL IAW EO#EM-53MR-1808 PART "A".
- [SDR SIMA20180815018](https://openairdocs.org/sdr/SIMA20180815018), Aug 15, 2018: CROSSBEAM. CORRODED. CROSSBEAM AT FR 20 IS CORRODED. C/A-COMPLETE:REMOVED AND INSTALLED SERVICEABLE CROSSBEAM AT FR 20 IAW ETN-EM-53-139 R4 AND SRM 53-21-10. NO FURTHER ACTION REQUI
- [SDR SIMA20180815019](https://openairdocs.org/sdr/SIMA20180815019), Aug 15, 2018: STRUCTURE. DAMAGED. RT FLOOR EXTRUSIONS #1 THRU #8 ARE DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED RT FLOOR ECTRUSIONS #1 THRU #8 IAW AMM 33-50-12.
- [SDR SIMA20180815020](https://openairdocs.org/sdr/SIMA20180815020), Aug 15, 2018: SUPPORT. CRACKED. RT OMEGA BEAM OTBD SUPPORT IS CRACKED BETWEEN FRAMES 47-48. C/A-COMPLETE:ACCOMPLISHED REPAIR OF RT OUTBD OMEGA BEAM SUPPORT BETWEEN FR46 AND 50 IAW SRM 53-23-02
- [SDR SIMA20180815023](https://openairdocs.org/sdr/SIMA20180815023), Aug 15, 2018: CROSSBEAM. CORRODED. CROSSBEAM BETWEEN FR 24-25 IS CORRODED. C/A-COMPLETE:REMOVED AND REPLACED ALUMINUM CROSSBEAM BETWEEN FR 24-25 IAW SRM 53-22-10 AND ETN-EM-53-139R4.
- [SDR SIMA20180815022](https://openairdocs.org/sdr/SIMA20180815022), Aug 15, 2018: SKIN. CRACKED. RT FUSELAGE UPPER SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R, CRACK ENDS MARKED, APPROX. 1/2" LONG. EASI #6581 USED. 100-500 KHZ PROBE, FREQ=400KHZ
- [SDR SIMA20180815021](https://openairdocs.org/sdr/SIMA20180815021), Aug 15, 2018: LIGHT. DAMAGED. #5 EMERGENCY LIGHT STRIP IS DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED #5 FLOOR EMERGENCY LIGHT STRIP IAW AMM 33-50-12. SEE BOW 301252 FOR OPC.
- [SDR SIMA20140528004](https://openairdocs.org/sdr/SIMA20140528004), May 28, 2014: CONTROL UNIT. FAILED. AT CRUISE ON FLIGHT 3211 CREW REPORTED WARNING MSG PITCH TRIM BACKUP INOPERATIVE. AUTOPILOT WAS ENGAGED & DECLARED EMERGENCY. THE ACFT WAS REMOVED FROM SERVICE.
- [SDR SIMA20140323006](https://openairdocs.org/sdr/SIMA20140323006), Mar 23, 2014: LIGHT. INOPERATIVE. LEFT EXTERIOR OVERWING EMERGENCY LAMP INOPERATIVE. R & R LT EXTERIOR OVERWING EMERGENCY LIGHT LAMPS IAW AMM TASK 33-50-10-000-801-A & 33-50-10-400-801-A. OPERAT
- [SDR SIMA20140319002](https://openairdocs.org/sdr/SIMA20140319002), Mar 19, 2014: LIGHT. INOPERATIVE. LT AFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R LAMP AT LT AFT EXTERNAL EMERGENCY LIGHT IAW AMM 33-50-10 & SMP, OPERATIONS CHECKED GOOD.
- [SDR SIMA20140304001](https://openairdocs.org/sdr/SIMA20140304001), Mar 4, 2014: LIGHT. INOPERATIVE. ROW 14 EMERGENCY LIGHT INOPERATIVE. R & R ELECTROLUMINESCENT STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140115004](https://openairdocs.org/sdr/SIMA20140115004), Jan 15, 2014: INVERTER. INOPERATIVE. COCKPIT STEP EMERGENCY SIGN INOPERATIVE. R & R NR 1 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11 & OPERATIONS CHECKED GOOD.
- [SDR SIMA20140106004](https://openairdocs.org/sdr/SIMA20140106004), Jan 6, 2014: HOLDER. BROKEN. FIRST OFFICER`S FLASHLIGHT HOLDER BROKEN. R & R FLASH LIGHT HOLDER IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.
- [SDR SIMA20131226004](https://openairdocs.org/sdr/SIMA20131226004), Dec 26, 2013: NUT. BENT. BUTTERFLY NUT THAT HOLDS CRASH AXE CLAMP CLOSED IS BENT OVER 90 DEGREES. UNABLE TO STOW OR USE CRASH AXE. INSTALLED IAW STANDARD PRACTICE.
- [SDR SIMA20131006005](https://openairdocs.org/sdr/SIMA20131006005), Oct 6, 2013: INVERTER. INOPERATIVE. EMERGENCY LIGHT ABOVE F/A SEAT INOPERATIVE. REPLACED INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.
- [SDR SIMA20130827001](https://openairdocs.org/sdr/SIMA20130827001), Aug 27, 2013: DISPLAY. FAILED. AFTER DISCONNECTING GPU, DETECTED SMOKE IN COCKPIT, NOTICED EICAS BLANK AND MFD DISPLAYED AN AMBER "CHECK EICAS" MESSAGE. R & R EICAS DISPLAY UNIT IAW AMM 34-22
- [SDR SIMA20130826003](https://openairdocs.org/sdr/SIMA20130826003), Aug 26, 2013: WIRE HARNESS. FAILED. CREW REPORTED THAT DURING TAKEOFF, RECEIVED AN AIR GROUND FAIL MESSAGE WITH ASSOCIATED REV DISAGREE MESSAGE ON EICAS. DECLARED EMERGENCY, RETURNED AND LANDED WI
- [SDR SIMA20130824004](https://openairdocs.org/sdr/SIMA20130824004), Aug 24, 2013: PROXIMITY SENSOR. INOPERATIVE. THE CREW REPORTED THAT DURING TAKEOFF THEY FELT A VIBRATION FROM THE NOSE GEAR AND HEARD A THUMP AFTER ROTATION. THE TOWER CONFIRMED RUBBER ON THE RUNWAY. THE C
- [SDR SIMA20130812001](https://openairdocs.org/sdr/SIMA20130812001), Aug 12, 2013: BULB. INOPERATIVE. LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-50-07. OPS CHECKED GOOD.
- [SDR SIMA20130706002](https://openairdocs.org/sdr/SIMA20130706002), Jul 6, 2013: BATTERY PACK. INOPERATIVE. DURING MX INSPECTION, FOUND EMERGENCY POWER BATTERY UNIT NR 3 INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R BATTERY UNIT. OPS CHECKED GOOD. ACFT RETURNED TO SER
- [SDR SIMA20130607009](https://openairdocs.org/sdr/SIMA20130607009), Jun 7, 2013: LIGHT. INOPERATIVE. DURING B INSPECTION, FOUND THE LT OVER WING EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE BULB IN OVER WING EMERGENCY LIGHT IAW AMM 3
- [SDR SIMA20130530002](https://openairdocs.org/sdr/SIMA20130530002), May 30, 2013: LIGHT. INOPERATIVE. DURING B INSPECTION, FOUND THE LT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LT AFT OVERWING EMERGENCY LIGHT IAW AMM 
- [SDR SIMA20130425007](https://openairdocs.org/sdr/SIMA20130425007), Apr 25, 2013: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION FOUND THE LEFT OVER WING AFT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB FOR 

All 84: https://openairdocs.org/aircraft/N842AE/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/N842AE/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.