# N826AE: 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: 145592
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 22, 2002
- Certificate issued: January 11, 2024
- Expires: January 31, 2031
- Mode S code: AB472A
- 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=826AE
- Page: https://openairdocs.org/aircraft/N826AE

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/N826AE/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 N826AE.

## FAA accident and incident reports

None matched to N826AE.

## Service difficulty reports (114, 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 SIMA202002106006](https://openairdocs.org/sdr/SIMA202002106006), Feb 6, 2020: COUPLING. LEAKING. BLEED 2 LEAK MESSAGE AT FL 240 FOLLOWED QRH MESSAGE CLEARED-C/A-PERFORMED INSPECTION OF AIR BLEED DUCT LINES IAW EMB 140 AMM 36-11-01. FOUND ZIP TIES MISSING (1
- [SDR SIMA202001064001](https://openairdocs.org/sdr/SIMA202001064001), Jan 4, 2020: ANTI-ICE VALVE. FAILED. BLD 2 LEAK AT FL230 IN ICING CONDITIONS-C/A-REMOVED AND REPLACED #2 WING A/I VALVE IAW EMB140 AMM 30-11-01. OPC GOOD. NO LEAKS NOTED
- [SDR SIMA201912054004](https://openairdocs.org/sdr/SIMA201912054004), Dec 4, 2019: BULB. INOPERATIVE. UPON COURTESY CHECK FOUND RH OVER WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED EMERGENCY LIGHT BULB OVER WING ON RH SIDE IAW EMB 140 AMM 33-50-10 OPC GOOD
- [SDR SIMA2019111108003](https://openairdocs.org/sdr/SIMA2019111108003), Nov 8, 2019: ACM. ODOR. MEL 21-30 AUTH 110241D-C ON TAXI OUT, BOTH PACKS RUNNING, CABIN AND COCKPIT FILLED WITH STRONG SMELL OF SMOKE. TURNED OFF PACK #1 AND SMELL WENT AWAY.REF LOG PA
- [SDR SIMA20191108001](https://openairdocs.org/sdr/SIMA20191108001), Nov 8, 2019: A/C PACK. SMOKE. ON TAXI OUT BOTH PACKS RUNING CABIN AND COCKPIT FILLED WITH STRONG SMELL OF SMOKE TURNED OFF PACK 1 AND SMELL WENT AWAY-C/A-C/W EMB-140 FIM TASK 21-20-00-810-80
- [SDR SIMA20190830003](https://openairdocs.org/sdr/SIMA20190830003), Aug 30, 2019: SKIN. DENTED. FUSELAGE DENTED AFT OF FR65 BETWEEN STR 19L-20L. C/A-C/W ERS-EM-53MR-3878.
- [SDR SIMA20190819007](https://openairdocs.org/sdr/SIMA20190819007), Aug 19, 2019: SKIN. GOUGED. DISCREPANCY: 53-10 FUSELAGEFUSELAGE MAIN, STRUCTURE - FUSELAGE SKIN GOUGED BELOW CARGO DOOR AFT OF FRAME 65 BETWEEN STRINGERS 19-20L. MAJOR REPAIR. C/A-REPAIRED
- [SDR SIMA20190324002](https://openairdocs.org/sdr/SIMA20190324002), Mar 24, 2019: ROLLER. DIRTY. MAIN CABIN DOOR HANDLE VERY HARD TO OPEN AND CLOSE. C/A-CLEAN AND LUBE DOOR ROLLERS IN REF TO AMM 52-10-01, OPC GOOD AND AMM 53-21-02.
- [SDR SIMA20190306001](https://openairdocs.org/sdr/SIMA20190306001), Mar 6, 2019: FLASHLIGHT. INOPERATIVE. SUPPLEMENTAL AFT FLASH LIGHT IS INOP. C/A-DEFERED AFT F/A FLASH LIGHT C/W MEL PROCEDURES. REMOVED AND REPLACED AFT FA FLASHLIGHT AND CRADLE OPC GOOD IAW AMM 33-
- [SDR SIMA20190227002](https://openairdocs.org/sdr/SIMA20190227002), Feb 27, 2019: LIGHT. INOPERATIVE. NR 4 FLOOR EMERGENCY LIGHT STRIP IS INOP. C/A-REMOVED AND REPLACED NR 4 FLOOR EMERGENCY LIGHT STRIP IAW AMM 30-50-12 OPS CHECK GOOD.
- [SDR SIMA201810165001](https://openairdocs.org/sdr/SIMA201810165001), Oct 15, 2018: SWITCH. FAULTY. PK 1 OVL CAUTION MESSAGE LOST CABIN PRESS AT FL240 DECLARE EMR PK 2 CLSD ADVISORY. -C/A-FOUND CMC MESSAGES PACK NR 1 OVERPRESSURE AND HAD CB NR 2 PACK TRIPPING 
- [SDR SIMA201809065004](https://openairdocs.org/sdr/SIMA201809065004), Sep 5, 2018: DISPLAY. FAILED. ON FINAL FO PFD FAILED AND NOTICED BURNING SMELL IN CKPT. PULLED PFD 2 CB AS SAFETY PRECAUTION. UPON FURTHER INSP FOUND PFD TO BE THE BURNING SMELL C/W M FUNCTI
- [SDR SIMA201808221007](https://openairdocs.org/sdr/SIMA201808221007), Aug 21, 2018: BULB. INOPERATIVE. NR 2 CEILING EMERGENCY LIGHT INOPERATIVE. R & R THE NR 2 CEILING EMERGENCY LIGHT BULB IAW AMM 33-50-08. OPS CHECKED GOOD.
- [SDR SIMA20180622001](https://openairdocs.org/sdr/SIMA20180622001), Jun 22, 2018: LIGHT. INOPERATIVE. MAIN PAX DOOR EMERGENCY LIGHT DOES NOT COME ON. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY. OP TESTED OK. IAW AMM 33-30-02 AND AMM 33-50-10.
- [SDR SIMA2018060403002](https://openairdocs.org/sdr/SIMA2018060403002), Jun 3, 2018: LIGHT. INOPERATIVE. EMERGENCY LIGHT STRIPS AT ROWS 7 & 8 WERE INOPERATIVE. R & R THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD. NO DEFECTS NOTED.
- [SDR SIMA2018060131004](https://openairdocs.org/sdr/SIMA2018060131004), May 31, 2018: LIGHT. INOPERATIVE. EMERGENCY LIGHT AT ROWS 7 & 8 WERE INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. NO DEFECTS NOTED.
- [SDR SIMA2018052220005](https://openairdocs.org/sdr/SIMA2018052220005), May 20, 2018: WARNING MESSAGE. FALSE ACTIVATION. NR 2 BLEED LEAK OCCURED AT APPROX 500FT. PERFORMED AN OPS CHECK OF THE BLEED SYSTEM IAW AMM 36-11-10, AND AMM 36-00-00. OPS CHECKED GOOD.
- [SDR SIMA20180323001](https://openairdocs.org/sdr/SIMA20180323001), Mar 23, 2018: SHEAR TIE. CRACKED. CRACKED SHEAR TIE, FRAME 80, BETWEEN STRINGERS 6R AND 7R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-05, AND 51-21-06.
- [SDR SIMA20180323002](https://openairdocs.org/sdr/SIMA20180323002), Mar 23, 2018: BEAM. CORRODED. CORROSION ON THE CARGO DOOR THRESHOLD BEAM AT FRAME 65. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-31-15, REMOVED THE THRESHOLD BEAM IAW AMM 53-31-
- [SDR SIMA20180318001](https://openairdocs.org/sdr/SIMA20180318001), Mar 18, 2018: SKIN. GOUGED. GOUGE IN THE SKIN AT FRAME 25 BETWEEN STRINGERS 21L AND 21R. CUT OUT THE DAMAGED AREA IAW SRM 53-22-01, REPAIR TYPE A, PERFORMED HFEC INSPECTION, NO DEFECTS NOT
- [SDR SIMA20180824009](https://openairdocs.org/sdr/SIMA20180824009), Mar 14, 2018: FRAME. CRACKED. CRACK IN FRAME 23 BETWEEN STRINGERS 14 R AND 15 R-C/A-INSTALLED EWIS PROTECTION IAW SWMP 20-21-00, REMOVED OMEGA BEAM STANTION TO FOM IAW EMB 145 SRM 51-40-02, 
- [SDR SIMA20180314004](https://openairdocs.org/sdr/SIMA20180314004), Mar 14, 2018: FITTING. CRACKED. CRACK IN SHEAR CLIP AT FRAME 25 BETWEEN STRINGERS 15R AND 16 R. REMOVED CRACKED SHEAR CLIP, LOCATED, DRILLED ALODINED AND INSTALLED NEW SHEAR CLIP IAW SRM 51-40
- [SDR SIMA20180314003](https://openairdocs.org/sdr/SIMA20180314003), Mar 14, 2018: FITTING. CRACKED. CRACK IN SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 16 R AND 17 R. REMOVED CRACKED SHEAR CLIP, LOCATED DRILLED AND APPLIED ALODINE TO NEW SHEAR CLIP AND INSTALLED
- [SDR SIMA20180314005](https://openairdocs.org/sdr/SIMA20180314005), Mar 14, 2018: FITTING. CRACKED. CRACK IN SHEAR CLIP AT FRAME 67 BETWEEN STRINGERS 6L AND 7L. REMOVED CRACKED SHEAR CLIP, LOCATED DRILLED AND APPLIED ALODINE TO NEW SHEAR CLIP AND INSTALLED IAW
- [SDR SIMA20180314006](https://openairdocs.org/sdr/SIMA20180314006), Mar 14, 2018: FITTING. CRACKED. CRACK IN SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L. REMOVED CRACKED SHEAR CLIP, LOCATED DRILLED AND APPLIED ALODINE TO NEW SHEAR CLIP AND INSTALLED IAW
- [SDR SIMA20180313006](https://openairdocs.org/sdr/SIMA20180313006), Mar 13, 2018: FLOOR SUPPORT. CORRODED. CORROSION ON THE CENTER OMEGA BEAM, FRAME 27. REMOVED CORROSION IAW SRM 51-40-02, 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 53-22-10, CUT OUT THE DAMAGED AREA
- [SDR SIMA20180313005](https://openairdocs.org/sdr/SIMA20180313005), Mar 13, 2018: SHEAR TIE. CRACKED. CRACK IN SHEAR TIE AT FRAME 73, BETWEEN STRINGERS 8R AND 10R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, 51-20-03, CPM 51-21-04, AND 51-21-05
- [SDR SIMA20180313004](https://openairdocs.org/sdr/SIMA20180313004), Mar 13, 2018: SHEAR TIE. CRACKED. CRACKED SHEAR TIE, FRAME 65 BETWEEN STRINGERS 18L AND 19L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-20-02, 51-20-03, AND CPM 51-21-04.
- [SDR SIMA20180313003](https://openairdocs.org/sdr/SIMA20180313003), Mar 13, 2018: SHEAR TIE. CRACKED. CRACK IN SHEAR TIE, FRAME 61 BETWEEN STRINGER 6 - 7L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02 , 51-20-03, AND CPM 51-21-04.
- [SDR SIMA20180313002](https://openairdocs.org/sdr/SIMA20180313002), Mar 13, 2018: SUPPORT. CRACKED. CRACK IN RT OMEGA BEAM INBORED SUPPORT BETWEEN FRAMES 47 AND 48. REMOVED, LOCATED, DRILLED, AND ALODINED NEW SUPPORTS IAW SRM 51-40-02, 51-20-03, AND CPM 51-21-
- [SDR SIMA20150904006](https://openairdocs.org/sdr/SIMA20150904006), Sep 4, 2015: CONNECTOR. BROKEN. NUMBER 1 CABIN FLOOR PROXIMITY LIGHT WIRE CONNECTOR BROKEN. R & R NR 1 CABIN FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12. SEE NRWC 826-ABI-02103 FOR OPERATIONA
- [SDR SIMA20150904005](https://openairdocs.org/sdr/SIMA20150904005), Sep 4, 2015: WIRE. BROKEN. LEFT NR 5 PROXIMITY LIGHT HAS BROKEN WIRE AT BASE OF LIGHT. R & R LT NR 5 PROXIMITY LIGHT STRIP IAW AMM 33-50-12. OPERATIONAL CHECKED GOOD.
- [SDR SIMA20150621001](https://openairdocs.org/sdr/SIMA20150621001), Jun 21, 2015: LIGHT. INOPERATIVE. EXTERIOR RT WING TO FUSELAGE EMER LIGHT INOPERATIVE. R & R RT EXTERIOR EMER LIGHT BULB ON WING TO FUSELAGE FAIRING IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150529005](https://openairdocs.org/sdr/SIMA20150529005), May 29, 2015: INDICATOR. FAILED. STANDBY EHSI SCREEN INOPERATIVE, 1/2 OF SCREEN HAS LINE GOING THROUGH IT. R & R ISIS INDICATOR IAW AMM 34-01-01. LEAK & FNC GOOD IAW AMM 34-13-00 & 34-01-01.
- [SDR SIMA20150418002](https://openairdocs.org/sdr/SIMA20150418002), Apr 18, 2015: DUCT. BROKEN. AIR CONDITIONING PACKS COULD NOT SUPPLY ENOUGH AIR FOR AIR CONDITIONING OR PRESSURIZATION. COULD NOT MAINTAIN REQUIRED CABIN ALTITUDE. TRANSFERRED TO NRWC 826-D
- [SDR SIMA20141017005](https://openairdocs.org/sdr/SIMA20141017005), Oct 17, 2014: CARBON SEAL. DEFECTIVE. SMOKE COMING FROM E1 AFTER BEING SHUTDOWN 15 PLUS MINUTES. COMPLIED WITH ETN-79--15 UP TO STEP 12 TDMI 826T7221 SCHEDULE A 50 FLIGHT HOURS. R & R LPT SHAFT PLUG
- [SDR SIMA20140624001](https://openairdocs.org/sdr/SIMA20140624001), Jun 24, 2014: VALVE. FAILED. DURING TAXI OUT, HS VLV 2 FAIL ON EICAS WITH BOTH ENGS RUNNING. R & R HS VLV 2 IAW AMM 36-11-02. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140603004](https://openairdocs.org/sdr/SIMA20140603004), Jun 3, 2014: ISIS. MALFUNCTIONED. ISIS ONLY SHOWS RT HALF OF DISPLAY LT HALF IS BLANK. R & R ISIS IAW AMM 34-01-01. OPERATIONS & LEAK CHECKED GOOD.
- [SDR SIMA20140321003](https://openairdocs.org/sdr/SIMA20140321003), Mar 21, 2014: SMOKE DETECTOR. INOPERATIVE. WHILE PERFORMING WORK CARD NR 26-200-06 AFT CARGO SMOKE DETECTOR MX LED FAILED TO ILLUMINATE. REMOVED & INSTALLED SERVICEABLE AFT CARGO SMOKE DETECTOR IAW AMM 2
- [SDR SIMA20131228004](https://openairdocs.org/sdr/SIMA20131228004), Dec 28, 2013: SMOKE DETECTOR. FAILED. FIRE DETECTION TEST FAILED BAGGAGE WARNING LIGHT DOES NOT ILLUMINATE DURING TEST, STAYS ILLUMINATED AFTER TEST. R & R NR 2 BAGGAGE COMPARTMENT SMOKE DETECTOR IA
- [SDR SIMA20131026003](https://openairdocs.org/sdr/SIMA20131026003), Oct 26, 2013: FLASHLIGHT ASSY. INOPERATIVE. EMERGENCY FLASHLIGHT NR 3 INOPERATIVE. R & R FLASHLIGHT AND HOLDER ASSY IAW AMM 33-50-16. OPS CHECKED GOOD.
- [SDR SIMA20131006004](https://openairdocs.org/sdr/SIMA20131006004), Oct 6, 2013: INVERTER. INOPERATIVE. DURING EMERGENCY LIGHT TEST FOUND FLOOR LIGHT STRIPS 6, 7, 8 INOPERATIVE. R & R INVERTER ASSY NR 6 IAW AMM 33-50-11. PERFORMED OPS CHECKED IAW AMM 33-50-00. OPS
- [SDR SIMA20130926003](https://openairdocs.org/sdr/SIMA20130926003), Sep 26, 2013: UNKNOWN. ODOR. COCKPIT SMELLS STRONGLY OF A FISH. CLEANED COCKPIT IAW AMM 25-00-00.
- [SDR SIMA20130817002](https://openairdocs.org/sdr/SIMA20130817002), Aug 17, 2013: CRADLE. WORN. FLASHLIGHT IS NOT CHARGING PROPERLY, VIBRATION CAUSE CHARGE LIGHT TO GO OUT. R & R FLASHLIGHT CRADLE ASSY IAW AMM 33-50-16, OPS CHECKED GOOD AT THIS TIME.
- [SDR SIMA20130710012](https://openairdocs.org/sdr/SIMA20130710012), Jul 10, 2013: LIGHT. INOPERATIVE. COCKPIT CEILING EMERGENCY LIGHT AT DOOR INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 32-50-05. OPS CHECKED GOOD
- [SDR SIMA20130710013](https://openairdocs.org/sdr/SIMA20130710013), Jul 10, 2013: LIGHT. DAMAGED. THE LT NR 8 EMERGENCY LIGHT DAMAGED. R & R EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20130710014](https://openairdocs.org/sdr/SIMA20130710014), Jul 10, 2013: LIGHT. DAMAGED. THE LT NR 2 EMERGENCY LIGHT DAMAGED. R & R EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20130710011](https://openairdocs.org/sdr/SIMA20130710011), Jul 10, 2013: LIGHT. DAMAGED. THE LT NR 6 EMERGENCY LIGHT DAMAGED. R & R EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20130710010](https://openairdocs.org/sdr/SIMA20130710010), Jul 10, 2013: LIGHT. DAMAGED. THE LEFT NR 1 EMERGENCY LIGHT DAMAGED. R & R THE EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20130610004](https://openairdocs.org/sdr/SIMA20130610004), Jun 10, 2013: PITOT SYSTEM. CONTAMINATED. THE CREW REPORTED THAT UPON DESCENT THE NR 2 ALTIMITER DISPLAYED A RED X. THE CREW RAN THE APPROPRIATE CHECKLIST AND DECLARED AN EMERGENCY. THE ACFT LANDED WITH

All 114: https://openairdocs.org/aircraft/N826AE/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/N826AE/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.