# N806AE: 2001 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: 145503
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 22, 2001
- Certificate issued: September 6, 2023
- Expires: September 30, 2030
- Mode S code: AAF82C
- Registered owners: [Corporate Flight Management Inc DBA](https://openairdocs.org/faa-owner/CORPORATE%20FLIGHT%20MANAGEMENT%20INC%20DBA), [Contour Aviation](https://openairdocs.org/faa-owner/CONTOUR%20AVIATION)
- Location: [Smyrna, TN](https://openairdocs.org/faa-place/TN/Smyrna)
- Owner type: Corporation
- Owner's area on the map: 35.9628° N, 86.5297° W: Placed by OpenAirDocs at the center of ZIP code 37167, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=806AE
- Page: https://openairdocs.org/aircraft/N806AE

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/N806AE/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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB OPS10IA155](https://openairdocs.org/ntsb/OPS10IA155), Apr 22, 2010: Embraer EMB-135KL (N806AE), Chicago, IL, incident, no damage. Probable cause: The air traffic controller's issuance of an improper takeoff clearance to the pilot of the Embraer. Contributing to the incident was the instructor’s inadequate monitoring of the trainee local…

## FAA accident and incident reports

None matched to N806AE.

## Service difficulty reports (77, 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 SIMA20191031006](https://openairdocs.org/sdr/SIMA20191031006), Oct 31, 2019: CHARGER. FAILED. DURING OPS CHECK OF EMERGENCY LIGHTING SYSTEM FOUND LIGHTS ASSOCIATED WITH EMERGENCY BATTERY # 2 INOP-C/A-UPON INSPECTION FOUND # 2 EMERGENCY LIGHTING BATTERY N
- [SDR SIMA201910219001](https://openairdocs.org/sdr/SIMA201910219001), Oct 19, 2019: WARNING MESSAGE. FALSE ACTIVATION. EMERGENCY LIGHTS CAME ON IN FLIGHT + EICAS MESSAGE EMER LIGHT NOT ARMED & THEN WENT AWAY-C/A-PERFORMED OPS CKS OF EMER LIGHTS SYST PER EMB 140 MM 33-50-00 OPS C
- [SDR SIMA20190720004](https://openairdocs.org/sdr/SIMA20190720004), Jul 20, 2019: LIGHT. INOPERATIVE. GALLEY EXIT LIGHT OVER SERVICE DOOR INOP. C/A-REMOVED AND REPLACED GALLEY EXIT LIGHT. IAW AMM 33-50-14. OPS CK IAW AMM 33-50-00. OPS CK GOOD.
- [SDR SIMA201906254004](https://openairdocs.org/sdr/SIMA201906254004), Jun 24, 2019: LAMP. INOPERATIVE. COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R THE COCKPIT OVERHEAD EMERGENCY LIGHT LAMP IAW AMM 33-50-05-000-801 AND 33-50-05-400-801 OPS CHECKED GOOD.
- [SDR SIMA201904297001](https://openairdocs.org/sdr/SIMA201904297001), Apr 27, 2019: CHARGER. FAILED. L/H UPPER EXTERIOR EMERGENCY LIGHT WILL NOT ILLUMINATE-C/A-LH UPPER EXTERIOR EMERGENCY LIGHT ASSY REMOVED AND REPLACED IAW EMB140 AMM 33-50-10. NO. 4 BATTERY PO
- [SDR SIMA20190214001](https://openairdocs.org/sdr/SIMA20190214001), Feb 14, 2019: BRAKE CABLE. LACK OF LUBE. EMERG/PARK BRAKE DIFFICULT TO OPERATE. LUBE PARKING BRAKE CABLE IAW AMM 32-44-10. OPS CHECK GOOD.
- [SDR SIMA20190104001](https://openairdocs.org/sdr/SIMA20190104001), Jan 4, 2019: LIGHT. INOPERATIVE. AFT 2 CEILING WHITE EMERG LIGHT INOP. C/A-REMOVED AND REPLACED 2 AFT AISLE EMERGENCY LIGHT IAW AMM 33-50-08. OPS CHECK GOOD IAW AMM TASK 33-50-00.
- [SDR SIMA20181115002](https://openairdocs.org/sdr/SIMA20181115002), Nov 15, 2018: ACCUMULATOR. LOW. EMG BRAKE LO PRESS MSG. DRFERRED EMG BRAKE LOW PRESSURE MSG M PROC. C/W MEL 32-5 AUTH 110522M-C. SERVICED EMERGENCY/PARKING BRAKE ACCUMULATOR IAW EMB 140 AMM 32
- [SDR SIMA201808232003](https://openairdocs.org/sdr/SIMA201808232003), Aug 22, 2018: UNKNOWN. UNKNOWN. EMERGENCY EXIT SIGN ABOVE SERVICE DOOR WILL NOT COME ON. T/S IAW FIM 33-50-00-810-804-A, EMERGENCY EXIT SIGN ABOVE SERVICE DOOR OPERATIONAL TESTED GOOD IAW AMM 
- [SDR SIMA2018052119009](https://openairdocs.org/sdr/SIMA2018052119009), May 19, 2018: LIGHT. INOPERATIVE. PAX DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 25-23-04. OPS CHECKED GOOD.
- [SDR SIMA20180425001](https://openairdocs.org/sdr/SIMA20180425001), Apr 25, 2018: FRAME. CRACKED. FRAME 23 WAS FOUND CRACKED AT THE CABIN RT NR 1 FLOOR SUPPORT. REPAIRED THE FRAME IAW EO EM-53MR-1808.
- [SDR SIMA2018042500009](https://openairdocs.org/sdr/SIMA2018042500009), Apr 19, 2018: WIRE. BROKEN. EMERGENCY LIGHT STRIP HAS A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT CONNECTOR IAW SWPM 20-50-01.
- [SDR SIMA2018042500003](https://openairdocs.org/sdr/SIMA2018042500003), Apr 15, 2018: SKIN. CRACKED. RIGHT UPPER AFT FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R APPROXIMATELY 3/8 INCH LONG. INSTALLED A REPAIR DOUBLER, FILLER, SHIM, REPAIR A
- [SDR SIMA2018042500004](https://openairdocs.org/sdr/SIMA2018042500004), Apr 15, 2018: SKIN. CRACKED. LEFT UPPER AFT FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L APPROXIMATELY 3/4 INCH LONG. INSTALLED A REPAIR DOUBLER, FILLER, SHIM, REPAIR AN
- [SDR SIMA2018042500013](https://openairdocs.org/sdr/SIMA2018042500013), Apr 13, 2018: LIGHT. BROKEN. LEFT NR 1, 6, AND 8 EMERGENCY LIGHTS BROKEN. REMOVED AND REPLACED THE EMERGENCY LIGHTS IAW AMM 33-50-12.
- [SDR SIMA2018042504001](https://openairdocs.org/sdr/SIMA2018042504001), Apr 4, 2018: DOOR SILL. CORRODED. CARGO DOOR LOWER SILL CORRODED. REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA2018042550003](https://openairdocs.org/sdr/SIMA2018042550003), Apr 4, 2018: CHANNEL. CORRODED. SERVICE DOOR CENTER SILL CORRODED. REMOVED AND INSTALLED A SERVICEABLE SERVICE DOOR CENTER SILL IAW SRM 51-40-02.
- [SDR SIMA20180404002](https://openairdocs.org/sdr/SIMA20180404002), Apr 4, 2018: SKIN. DENTED. RIVET ROW JUST FORWARD OF FRAME 10 BETWEEN STRINGERS 13R AND 15R HAS A PROTRUSION AT RIVET SECOND FROM TOP. REPAIRED IAW ERS-EM-53MR-3229.
- [SDR SIMA2018042500005](https://openairdocs.org/sdr/SIMA2018042500005), Apr 4, 2018: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM CORRODED IN RADIUS AT FRAME 38. REPAIRED IAW SRM 53-00-10, FIGURE 202, SHEET 1.
- [SDR SIMA20180404004](https://openairdocs.org/sdr/SIMA20180404004), Apr 4, 2018: FLOOR SUPPORT. CORRODED. CENTER OMEGA BEAM CORRODED IN RADIUS AT FR 38. REPAIRED IAW SRM 53-00-10, FIG 203, SHEET 1.
- [SDR SIMA20150929002](https://openairdocs.org/sdr/SIMA20150929002), Sep 29, 2015: INVERTER. INOPERATIVE. EMERGENCY FLOOR PROXIMITY LIGHTING STRIPS FROM ROW 11 - 16 INOPERATIVE. R & R NR 6 EMER LIGHT DC & AC INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150924003](https://openairdocs.org/sdr/SIMA20150924003), Sep 24, 2015: TIRE. SEPARATED. ENGINE DAMAGE FOUND, DUE TO LOST NR 3 TIRE TREAD SEPARATED FROM RT INBD. R & R NR 3 & 4 MLG TIRE WHEEL ASSEMBLY IAW WC 32-700-11. PERFORMED INSPECTION, AFTER ML
- [SDR SIMA20150308004](https://openairdocs.org/sdr/SIMA20150308004), Mar 8, 2015: BATTERY. DISCHARGED. THE LT & RT AFT EXTERIOR EMER LIGHTS ARE INOPERATIVE. R & R THE NR 4 EPSU BATTERY & CHARGER ASSEMBLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. EMER LIGHTING BA
- [SDR SIMA20150211006](https://openairdocs.org/sdr/SIMA20150211006), Feb 11, 2015: FLASHLIGHT. BROKEN. CAPTAIN`S FLASHLIGHT NEEDS ON OFF SWITCH, BROKEN. REPLACED CAPTAIN'S FLASHLIGHT ASSEMBLY 25 60 11.
- [SDR SIMA20150210001](https://openairdocs.org/sdr/SIMA20150210001), Feb 10, 2015: HOT WATER POT. DEFECTIVE. BURNING SMELL IN GALLEY ORIGINATING FROM HOT JUG LOCATION. FOUND LOOSE PIN ON BACK OF HOT JUG. REMOVED & DEFERRED IAW MEL 25-50 M PROCEDURE COMPLIED WITH.
- [SDR SIMA20150119004](https://openairdocs.org/sdr/SIMA20150119004), Jan 19, 2015: LIGHT. INOPERATIVE. PASSENGER CABIN CEILING EMER LIGHT AT ROW 3 INOPERATIVE. R & R LAMP IAW AMM 33-50-08. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.
- [SDR SIMA20141126002](https://openairdocs.org/sdr/SIMA20141126002), Nov 26, 2014: LIGHT. INOPERATIVE. LEFT EMER EXIT PSU EMER LIGHT IDENTIFIER SIGN IS INOPERATIVE. R & R LT EMER EXIT PSU EMER LIGHT IDENTIFIER LAMP IAW CMM 25-28-23. OPERATIONAL CHECKED GOOD.
- [SDR SIMA20141120002](https://openairdocs.org/sdr/SIMA20141120002), Nov 20, 2014: PUMP. LEAKING. FUEL LEAKING BOTTOM OF NR 1 ENG COWLING & FUEL SMELL IN CABIN WITH APU AIR ON. NOTE SEE ITEM NR 4 THIS AML PG FOR FUEL SMELL RAD 367347. R & R NR 1 ENG FPMU IAW
- [SDR SIMA20140322003](https://openairdocs.org/sdr/SIMA20140322003), Mar 22, 2014: LIGHT. INOPERATIVE. RT FWD EMERGENCY LIGHT INOPERATIVE. R & R RT FWD EMERGENCY LIGHT IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.
- [SDR SIMA20140206003](https://openairdocs.org/sdr/SIMA20140206003), Feb 6, 2014: WIRE. BROKEN. CABIN EMERGENCY EXIT FLOOR PROXIMITY STRIP LIGHT AT ENTRY TO LAVATORY HAS BROKEN WIRES. R & R CABIN EMERGENCY EXIT FLOOR PROXIMITY STRIP LIGHT AT ENTRY TO LAVAT
- [SDR SIMA20140112006](https://openairdocs.org/sdr/SIMA20140112006), Jan 12, 2014: HOLDER. DEFECTIVE. BRACKET THAT HOLDS FLIGHT ATTENDANT`S FWD FLASHLIGHT IS VERY LOOSE. R & R FWD FLASHLIGHT HOLDER IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.
- [SDR SIMA20131212007](https://openairdocs.org/sdr/SIMA20131212007), Dec 12, 2013: CONNECTOR. DISCONNECTED. LEFT FWD EXTERNAL OVERWING EMERGENCY LIGHT INOPERATIVE. FOUND NR 1 EMERGENCY POWER SUPPLY CONNECTOR NOT TO BE CONNECTED. RECONNECTED AS REQUIRED, OPERATIONS CHE
- [SDR SIMA20131210002](https://openairdocs.org/sdr/SIMA20131210002), Dec 10, 2013: CHARGER. INOPERATIVE. DURING MAINTENANCE INSPECTION ON FLIGHT 3718 FOUND LT FWD EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R NR 4 BATTERY CHARGER. OPERATIONS 
- [SDR SIMA20130924006](https://openairdocs.org/sdr/SIMA20130924006), Sep 24, 2013: COMPRESSOR. STALLED. CREW REPORTED THAT ON INTIAL CLIMB, NR 2 ENGINE HP VIBRATIONS MAXED CLIMBING THROUGH 2000 FT. FELT COMPRESSOR STALL. IMMEDIATELY BROUGHT ENGINE TO IDLE AND INDI
- [SDR SIMA20130831002](https://openairdocs.org/sdr/SIMA20130831002), Aug 31, 2013: CRADLE. UNSECURE. CAPTAIN'S EMERGENCY FLASHLIGHT HOLDER, LOOSE. SECURED FLASHLIGHT HOLDER IN REF WITH AMM TASK 33-50-16-400-801-A END.
- [SDR SIMA20130430006](https://openairdocs.org/sdr/SIMA20130430006), Apr 30, 2013: FRAME. CRACKED. DURING MAINTENANCE INSPECTION FOUND FRAME 23 CRACKED BETWEEN STRINGERS 15R AND 16R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CRACKED SECTION OF FRAME, FAB
- [SDR SIMA20130420012](https://openairdocs.org/sdr/SIMA20130420012), Apr 20, 2013: ANGLE. CRACKED. RT FWD VERTICAL TO FUSELAGE ANGLE CRACKED. REPAIRED ANGLE IAW AEA EM-53MR-1281.
- [SDR SIMA20130420011](https://openairdocs.org/sdr/SIMA20130420011), Apr 20, 2013: GUSSET. CORRODED. DURING B INSPECTION, FOUND THE LAV RT BEAM GUSSET CORRODED. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LAV RT BEAM GUSSET IAW SRM 51-40-02. THE ACFT WAS RETUR
- [SDR SIMA20130420010](https://openairdocs.org/sdr/SIMA20130420010), Apr 20, 2013: COVER. DAMAGED. DURING B INSPECTION, FOUND THE FOUR PROXIMITY LIGHT STRIP COVER PANELS DAMAGED. THE ACFT WAS REMOVED FROM SERVICE. R & R THE FOUR EMERGENCY LIGHT PROXIMITY STRI
- [SDR SIMA20130420009](https://openairdocs.org/sdr/SIMA20130420009), Apr 20, 2013: LIGHT. DAMAGED. DURING B INSPECTION, FOUND THE NR 4, NR 5, NR 7 PROXIMITY LIGHT STRIPS DAMAGED. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 4, NR 5, AND NR 7 PROXIMITY LIGH
- [SDR SIMA20130420008](https://openairdocs.org/sdr/SIMA20130420008), Apr 20, 2013: WIRE. BROKEN. DURING B INSPECTION, FOUND THE NR 3 EMERGENCY LIGHT STRIP WIRES BROKEN. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 3 EMERGENCY LIGHT STRIP IAW AMM 33-50-12
- [SDR SIMA20130420007](https://openairdocs.org/sdr/SIMA20130420007), Apr 20, 2013: GUSSET. CORRODED. DURING B INSPECTION, FOUND GUSSET ON RT BEAM CORRODED AT FRAME 20. ACFT REMOVED FROM SERVICE. R & R THE GUSSET IAW SRM 51-40-02, 51-20-03 AND 51-40-06. ACFT RET
- [SDR SIMA20130401004](https://openairdocs.org/sdr/SIMA20130401004), Apr 1, 2013: BATTERY. DISCHARGED. DURING MAINTENANCE INSPECTION FOUND THE ELT BATTERY FAILED TEST. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BATTERY IAW AE WC 25-
- [SDR SIMA20130131012](https://openairdocs.org/sdr/SIMA20130131012), Jan 31, 2013: ACM. FAILED. FLIGHT 4245. AT FLIGHT LEVEL 250, COCKPIT HAZY WITH SMOKE AND FLIGHT ATTENDANT CONFIRMED SMOKE IN CABIN. PERFORMED EPC AND SMOKE DISSIPATED. DECLARED AN EMERGEN
- [SDR SIMA20120827002](https://openairdocs.org/sdr/SIMA20120827002), Aug 27, 2012: FIREWALL. CRACKED. FOUND APU FIREWALL TO HAVE FOUR CRACKS. REMOVED AND REPLACED APU FIREWALL WITH NEW IAW EO EM-53AD-1883. AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA20120803003](https://openairdocs.org/sdr/SIMA20120803003), Aug 3, 2012: LIGHT. MALFUNCTIONED. FLIGHT 4113, CREW REPORTED THAT UPON ENTERING THE AIRCRAFT, EMERGENCY LIGHTS WERE ON BETWEEN ROWS 7 TO 11. AIRCRAFT REMOVED FROM SERVICE. CYCLED POWER. OPS CHEC
- [SDR SIMA20120707004](https://openairdocs.org/sdr/SIMA20120707004), Jul 6, 2012: LIGHT. INOPERATIVE. ON FLIGHT 2717 THE CREW REPORTED THE FLIGHT ATTENDANT’S FLASHLIGHT WOULD NOT TURN ON. REMOVED AND REPLACED THE LIGHT BULB IAW DME -CORP-CMM 25-60-11. THE OPERAT
- [SDR SIMA20120509002](https://openairdocs.org/sdr/SIMA20120509002), May 9, 2012: TRIM SWITCH. DEFECTIVE. ON FLIGHT 3211 AFTER TAKEOFF THE CREW RECEIVED A PITCH TRIM MAIN INOP MASTER WARNING MESSAGE ON EICAS. BOTH PITCH TRIM ON YOKE INOPERABLE. THE CREW DECLARED AN 
- [SDR SIMA20120430009](https://openairdocs.org/sdr/SIMA20120430009), Apr 30, 2012: SKIN. DAMAGED. ON FLIGHT 2834 THE CREW REPORTED MULTIPLE LIGHTNING STRIKES EN ROUTE. ON POST FLT FOUND DAMAGE TO BOTH WING TIPS, STATIC WICK ON LEFT LOOSE, LANDING GEAR WAS UP
- [SDR SIMA20120315001](https://openairdocs.org/sdr/SIMA20120315001), Mar 15, 2012: LIGHT. BROKEN. DURING MAINTENANCE INSPECTION THE CLEANERS FOUND AFT EMERGENCY LIGHT STRIP BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLOOR EME

All 77: https://openairdocs.org/aircraft/N806AE/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/N806AE/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.