# N815AE: 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: 145545
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 24, 2002
- Certificate issued: February 23, 2023
- Expires: February 28, 2030
- Mode S code: AB1BF4
- 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=815AE
- Page: https://openairdocs.org/aircraft/N815AE

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/N815AE/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 N815AE.

## 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 20020516009509I](https://openairdocs.org/incident/20020516009509I), May 16, 2002: Emb EMB135KL (N815AE), Oakland, CA. (-23) On approach to Oakland, the first officer was flying, the airspeed was approximately 220 knots, with flaps at 9 degrees. The first officer extended the…

## Service difficulty reports (85, 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 SIMA202003109004](https://openairdocs.org/sdr/SIMA202003109004), Mar 9, 2020: WINDOW. NOISY. ACCT LOUD SQUEAL FO WINDOW. EMER NOT DECL.INSTALLATION AND PRESSURIZATION FOR FO DV WINDOW REQUIRED REFERENCE ITEM #1 ON THIS LOG PG -C/A-INSTALLED FO COCKPIT E
- [SDR SIMA202003043001](https://openairdocs.org/sdr/SIMA202003043001), Mar 3, 2020: FLASHLIGHT. INOPERATIVE. FOUND FA FLASHLIGHT INOP-C/A-REMOVED AND REPLACED FA FLASHLIGHT IAW EMB AMM 33-50-16, OPC GOOD NO FURTHER DEFECTS NOTED
- [SDR SIMA20190313003](https://openairdocs.org/sdr/SIMA20190313003), Mar 13, 2019: WARNING SYSTEM. FALSE ACTIVATION. AFTER SUCCESSFUL ELECTRICAL AND PMEUMATIC ICE TESTS ON GROUND, RECEIVED "ICE DET 2 FAIL" IN FLIGHT DURING INITIAL CLIMB. C/A-DEFERRED ICE DET 2 PER MEL 30-25 AU
- [SDR SIMA20190111004](https://openairdocs.org/sdr/SIMA20190111004), Jan 11, 2019: CRADLE. BROKEN. CABIN AFT EMERGENCY FLASHLIGHT CRADLE IS BROKEN. C/A-REMOVED AND REPLACED CABIN AFT EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONAL CHECK GOOD.
- [SDR SIMA2018123128004](https://openairdocs.org/sdr/SIMA2018123128004), Dec 28, 2018: WARNING MESSAGE. FALSE ACTIVATION. ON APROACH WHEN SPEED BRAKE LEVER IS SELECTED TO OPEN RECIVED SPOILER FAIL ON EICAS.-C/A-T/S SPOILER FAIL EICAS MESSAGE IAW FIM TASK 27-63-00-810-802. NO ACTIVE
- [SDR SIMA201812149005](https://openairdocs.org/sdr/SIMA201812149005), Nov 29, 2018: A/C PACK. FAILED. AFTER SELECTING PACK 1 ON WE NOTICED A BURNING SMELL AND THEN RECEIVED A PACK 1 OVHT MSG. AFTER RUNNING QRH CHECKLIST PACK 1 WAS BLOWING HOT AIR IN FULL FOLD SE
- [SDR SIMA20181126001](https://openairdocs.org/sdr/SIMA20181126001), Nov 26, 2018: FLASHLIGHT ASSY. BROKEN. FWD FA FLASHLIGHT HOLDER BROKEN-C/A-REMOVED AND REPLACED FWD FA FLASHLIGHT ASSY IAW 33 50-16 POS GOOD.
- [SDR SIMA20180327004](https://openairdocs.org/sdr/SIMA20180327004), Mar 27, 2018: WIRE. BROKEN. FLOOR EMERGENCY LIGHT NR 7 HAS A BROKEN WIRE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-12.
- [SDR SIMA20180327006](https://openairdocs.org/sdr/SIMA20180327006), Mar 27, 2018: FRAME. CRACKED. FRAME 10 IS CRACKED BELOW THE COPILOTS DV WINDOW. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.
- [SDR SIMA20180327005](https://openairdocs.org/sdr/SIMA20180327005), Mar 27, 2018: WIRE. BROKEN. FLOOR EMERGENCY LIGHT NR 1 HAS A BROKEN WIRE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-12.
- [SDR SIMA20180325003](https://openairdocs.org/sdr/SIMA20180325003), Mar 25, 2018: WIRE. BROKEN. EMERGENCY LIGHT NR 8, WIRE BROKEN. REMOVED AND REPLACED THE NR 8 PROXIMITY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20180323005](https://openairdocs.org/sdr/SIMA20180323005), Mar 23, 2018: FITTING. CRACKED. LEFT PYLON FWD YOKE LOWER FWD FITTING CRACKED. REMOVED AND REPLACED THE YOKE FITTING IAW EO EM-54MR-386.
- [SDR SIMA20150904004](https://openairdocs.org/sdr/SIMA20150904004), Sep 4, 2015: CONNECTOR. MISSING. FLOOR PROXIMITY LIGHT, WIRE LT NR 1, MISSING CONNECTOR. REPAIRED FLOOR PROXIMITY LIGHT, WIRE LT NR 1 IAW SWPM 20-21-00. FOUND DURING ACFT OPEN UP.
- [SDR SIMA20150803004](https://openairdocs.org/sdr/SIMA20150803004), Aug 3, 2015: DOOR. LACK OF LUBE. MAIN CABIN DOOR DIFFICULT TO OPEN & CLOSE. INSPECTED MAIN CABIN DOOR IAW AMM 52-10-01. DOOR CONFIRMED DIFFICULT TO OPERATE IAW AMM 52-00-00, ALL DOOR MARKINGS L
- [SDR SIMA20150801002](https://openairdocs.org/sdr/SIMA20150801002), Aug 1, 2015: DOOR. LACK OF LUBE. MAIN CABIN DOOR DIFFICULT TO OPEN & CLOSE. LUBRICATED MAIN DOOR IAW AMM 52-1-01. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150729004](https://openairdocs.org/sdr/SIMA20150729004), Jul 29, 2015: GUIDE. DEFECTIVE. FLIGHT ATTENDANT REPORTS MAIN DOOR HARD TO OPERATE. R & R LOWER RIGHT MAIN DOOR GUIDE IAW AMM 53-21-06. COMPLIED WITH PRESSURIZATION CHECK IAW AMM 21-31-00. NO 
- [SDR SIMA20150611001](https://openairdocs.org/sdr/SIMA20150611001), Jun 11, 2015: PUMP. FAILED. HYD LO QTY ON EICAS. HYD 1 FLUID LEVEL AT ZERO. R & R E1 EDP IAW AMM 29-10-03. OPERATIONS & LEAK CHECKED GOOD.
- [SDR SIMA20150604004](https://openairdocs.org/sdr/SIMA20150604004), Jun 4, 2015: ACTUATOR. FAILED. WHILE CLIMBING OUT, WE GOT A PTRIM MAIN INOPERATIVE EICAS MSG. PERFORMED AOM LIST. REPEAT WRITE UP REF LOG PAGE 3799969. TRANSFERRED TO NRWC 815-DFW-01863. R & 
- [SDR SIMA20150417003](https://openairdocs.org/sdr/SIMA20150417003), Apr 17, 2015: LIGHT. INOPERATIVE. MAIN DOOR ENTRY OVERHEAD EMER LIGHT INOPERATIVE. R & R MAIN DOOR OVERHEAD EMER LIGHT BULB IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GO
- [SDR SIMA20150304006](https://openairdocs.org/sdr/SIMA20150304006), Mar 4, 2015: LIGHT. INOPERATIVE. LEFT & RT OVERWING EMER LIGHTS ARE INOPERATIVE. R & R NR 4 EMER LIGHT CHARGER & BATTERY IAW AE WC 33-700-19. DID NOT FIX PROBLEM. R & R RT AFT OVERWING EMER LIG
- [SDR SIMA20150102004](https://openairdocs.org/sdr/SIMA20150102004), Jan 2, 2015: INVERTER. INOPERATIVE. EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT FAILS TO ILLUMINATE. R & NR 1 DC & AC INVERTER IAW AMM 33-50-11 & WM 33-50-50. OPERATIONS CHECKED GOOD IAW AMM 3
- [SDR SIMA20141108004](https://openairdocs.org/sdr/SIMA20141108004), Nov 8, 2014: LIGHT. INOPERATIVE. ROW 17 AISLE EMER LAMP INOPERATIVE. R & R ROW 17 AISLE EMER LIGHT LAMP IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD.
- [SDR SIMA20141021004](https://openairdocs.org/sdr/SIMA20141021004), Oct 21, 2014: UNKNOWN. ODOR. SMOKE ODOR IN CABIN. EMERGENCY DECLARED.
- [SDR SIMA20140921003](https://openairdocs.org/sdr/SIMA20140921003), Sep 21, 2014: ROLLER. LACK OF LUBE. MAIN CABIN DOOR HANDLE VERY DIFFICULT TO OPEN. LUBRICATED MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02. OPERATIONS TESTED GOOD, NO FURTHER NOTED.
- [SDR SIMA20140916002](https://openairdocs.org/sdr/SIMA20140916002), Sep 16, 2014: DOOR SEAL. CONTAMINATED. FLIGHT ATTENDANT SAYS MAIN DOOR HARD TO OPEN. CLEANED EXCESS GREASE OF MAIN DOOR SEAL, ROLLERS & LOCKING BLOCKS AS NEEDED. OPERATIONS CHECKED GOOD IAW AMM 52-10
- [SDR SIMA20140404004](https://openairdocs.org/sdr/SIMA20140404004), Apr 4, 2014: BATTERY. DISCHARGED. RIGHT FWD EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. R & R NR 2 EMERGENCY LIGHT BATTERY & POWER SUPPLY IAW AMM 33-50-04, OPERATION CHECKED GOOD.
- [SDR SIMA20140106003](https://openairdocs.org/sdr/SIMA20140106003), Jan 6, 2014: BATTERY. UNKNOWN. REPLACE NR 1 EPSU BATTERY CHARGER ASSEMBLY WC 33-700-19. R & R NR 1 EPSU BATTERY ASSEMBLY IAW WC 33-700-19, OPERATIONS CHECKED GOOD.
- [SDR SIMA20131222008](https://openairdocs.org/sdr/SIMA20131222008), Dec 22, 2013: LEAD. DAMAGED. EMERGENCY FLOOR STRIP LIGHT AT 7A - 8A LEADS BAD. R & R 7A - 8A EMERGENCY FLOOR STRIP LIGHT & OPERATIONS CHECKED GOOD IAW AMM 33-50-12.
- [SDR SIMA20130722004](https://openairdocs.org/sdr/SIMA20130722004), Jul 22, 2013: CONNECTOR. DIRTY. EXIT LIGHT ON FWD BULKHEAD BY MAIN DOOR INOPERATIVE. CLEANED EXIT LIGHT CONNECTOR OPC IAW AMM 33-50-00, GOOD.
- [SDR SIMA20130709009](https://openairdocs.org/sdr/SIMA20130709009), Jul 9, 2013: CRADLE. INOPERATIVE. THE CREW REPORTED THE F/O FLASHLIGHT BATTRIES WERE NOT CHARGING, VERY WEAK. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT AND CHARGING ASSY IAW AMM 33-50-16. OPS 
- [SDR SIMA20130702006](https://openairdocs.org/sdr/SIMA20130702006), Jul 2, 2013: FLOOR SUPPORT. CORRODED. DURING MX BASE VISIT, INSPECTION FOUND THE CENTER OMEGA BEAM AT FRAME 57 CORRODED AT CROSSBEAM. ACFT WAS REMOVED FROM SERVICE. REPAIRED CENTER OMEGA BEAM AT FRA
- [SDR SIMA20130702005](https://openairdocs.org/sdr/SIMA20130702005), Jul 2, 2013: FRAME. DAMAGED. DURING MX BASE VISIT INSPECTION, FOUND FRAME 68, HAS MARRED UP AREAS AROUND SCREW HOLES, FOR INTERIOR PANELS. REMOVED FROM SERVICE. REPAIRED FRAME 68 IAW EO EM-
- [SDR SIMA20130702004](https://openairdocs.org/sdr/SIMA20130702004), Jul 2, 2013: FLOOR SUPPORT. CORRODED. DURING MX BASE VISIT, INSPECTION FOUND THE CENTER OMEGA BEAM AT FRAME 57 CORRODED AT CROSSBEAM. REMOVED FROM SERVICE. REPAIRED CENTER OMEGA BEAM AT FRAME 57 IAW
- [SDR SIMA20130702003](https://openairdocs.org/sdr/SIMA20130702003), Jul 2, 2013: BUSHING. CORRODED. DURING MX BASE VISIT INSPECTION FOUND THE LT AILERON OTBD HINGE FITITNG BOTH HAT BUSHINGS PITTED. ACFT REMOVED FROM SERVICE. R & R LT AILERON OTBD HINGE FITTING
- [SDR SIMA20130702002](https://openairdocs.org/sdr/SIMA20130702002), Jul 2, 2013: SKIN. DAMAGED. DURING MX BASE VISIT INSPECTIONM, FOUND AFT COMPARTMENT DOOR 312AR ATTACH FLANGE AROUND THE AFT UPPER FASTENER HOLE, ENLARGED. ACFT REMOVED FROM SERVICE. COMPLE
- [SDR SIMA20130702001](https://openairdocs.org/sdr/SIMA20130702001), Jul 2, 2013: FRAME. GOUGED. DURING MX INSEPCTION FOUND GOUGES ON FRAME 68 BETWEEN STRINGERS 9L AND 11L. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 68 IAW EO EM-53MR-2151 R1. THE ACF
- [SDR SIMA20130616008](https://openairdocs.org/sdr/SIMA20130616008), Jun 16, 2013: WIRE. BROKEN. FLASHLIGHT ASSY HAS BROKEN WIRE AT LAVATORY PARTITION AND RT AFT STAGE ASSY. REPAIRED BROKEN WIRE IAW SWPM 20-21-00.
- [SDR SIMA20130616009](https://openairdocs.org/sdr/SIMA20130616009), Jun 16, 2013: LIGHT. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R SERVICE DOOR EMERGENCY LIGHT ASSY IAW AMM 33-50-10. OPS CHECKED GOOD.
- [SDR SIMA20130616010](https://openairdocs.org/sdr/SIMA20130616010), Jun 16, 2013: BATTERY PACK. INOPERATIVE. REAR CABIN EMERGENCY LIGHTS DO NOT ILLUMINATE. FOUND BATTERIES AT THE LEFT EMERGENCY EXIT AND AFT CABIN CEILING POSTION TO HAVE NO CHARGE. R & R BOTH BATTERIES 
- [SDR SIMA20130616007](https://openairdocs.org/sdr/SIMA20130616007), Jun 16, 2013: SILL. CORRODED. SERVICE DOOR FWD SILL CORRODED. COMPLETE: REMOVED CORRODED SERVICE DOOR FWD SILL IAW SRM 51-20-03 AND INSTALLED NEW SILL IAW SRM 51-40-02.
- [SDR SIMA20130616006](https://openairdocs.org/sdr/SIMA20130616006), Jun 16, 2013: LIGHT. INOPERATIVE. AFT LEFT EMERGENCY LIGHT ON FWD FUSELAGE BELLY PANEL IS INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECKED GOOD.
- [SDR SIMA20130616005](https://openairdocs.org/sdr/SIMA20130616005), Jun 16, 2013: BATTERY PACK. DISCHARGED. DURING MX INSPECTION FOUND TWO BATTERIES HAD NO CHARGE. ACFT REMOVED FROM SERVICE. R & R THE BATTERIES. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.
- [SDR SIMA20130503005](https://openairdocs.org/sdr/SIMA20130503005), May 3, 2013: RETAINER. BROKEN. DURING B INSPECTION FOUND THE FORWARD CABIN EMERGENCY FLASHLIGHT CHARGER RETAINER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWAR
- [SDR SIMA20130430004](https://openairdocs.org/sdr/SIMA20130430004), Apr 30, 2013: FLASHLIGHT. INTERMITTENT. DURING B INSPECTION FOUND THE CAPTAIN’S EMERGENCY FLASHLIGHT WORKING INTERMITTENTLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S E
- [SDR SIMA20130401001](https://openairdocs.org/sdr/SIMA20130401001), Apr 1, 2013: HANDLE. UNSECURE. ON FLIGHT 4257 THE CREW REPORTED THEY COULD NOT OPEN THE MAIN CABIN DOOR FROM INSIDE THE CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESECURED MAIN DOOR HANDL
- [SDR SIMA20130102001](https://openairdocs.org/sdr/SIMA20130102001), Jan 2, 2013: PDU. MALFUNCTIONED. ON FLIGHT 4016 THE CREW REPORTED THEY RECEIVED A FLAP FAIL CAUTION MESSAGE AT CRUISE AT ALTITUDE 230. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT
- [SDR SIMA20120510019](https://openairdocs.org/sdr/SIMA20120510019), May 10, 2012: LIGHT. INOPERATIVE. DURING B INSPECTION FOUND THE SERVICE DOOR MOUNTED EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT L
- [SDR SIMA20120420004](https://openairdocs.org/sdr/SIMA20120420004), Apr 20, 2012: CRADLE. BROKEN. DURING B-INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT CRADEL BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIG
- [SDR SIMA2011313002](https://openairdocs.org/sdr/SIMA2011313002), Nov 7, 2011: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION FOUND THE ELECT CONNECTOR TO EMERGENCY FLOOR LIGHT AT SEATS 7A/B/C AND 8A/B/C BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOV
- [SDR SIMA201128306](https://openairdocs.org/sdr/SIMA201128306), Oct 9, 2011: SLEEVE. LEAKING. ON FLIGHT 2726 THE CREW REPORTED AN ELECTRICAL ODOR IN THE COCKPIT THAT SMELLED LIKE BURNING PLASTIC. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DFW. THE AI

All 85: https://openairdocs.org/aircraft/N815AE/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/N815AE/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.