# N809AE: 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: 145521
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 25, 2001
- Certificate issued: August 4, 2026
- Expires: August 31, 2033
- Mode S code: AB0351
- 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=809AE
- Page: https://openairdocs.org/aircraft/N809AE

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/N809AE/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 N809AE.

## 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 20080808842779I](https://openairdocs.org/incident/20080808842779I), Aug 8, 2008: Emb EMB135KL (N809AE), Nashville, TN, Minor damage. (-23) Upon landing at the Nashville International Airport on 08/08/08, eagle flight 600, an embrer-135KL aircraft, skidded 3,289 feet before coming to a stop.…

## Service difficulty reports (127, 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 SIMA202003110005](https://openairdocs.org/sdr/SIMA202003110005), Mar 10, 2020: LIGHT. INOPERATIVE. RH OVERWING EMERGENCY LIGHT INOP. MEL # 3329 AUTH# 03-272D-C LOGPAGE # 4507659-C/A-RAR RH OVERWING EMERGENCY LIGHT IAW EMB 140 AMM 33-50-10. OPC GOOD. MEL RESTO
- [SDR SIMA202003109002](https://openairdocs.org/sdr/SIMA202003109002), Mar 9, 2020: LIGHT. INOPERATIVE. "TRANSFERRED FROM NRWC 809-CMI-04121 ITEM 1" RH OVERWING EMERGENCY LIGHT INOP-C/A-DEFERRED PER MEL 33-29. AUTH #030272D-C
- [SDR SIMA202001287004](https://openairdocs.org/sdr/SIMA202001287004), Jan 27, 2020: CONNECTOR. UNSECURE. OVERHEAD FWD FACING AISLE EMERGENCY HATCH LOCATION LIGHT INOP.-C/A-RESECURED OVERHEAD FWD FACING AISLE EMERGENCY HATCH LOCATION LIGHT ELECTRICAL CONNECTOR IAW A
- [SDR SIMA201912231001](https://openairdocs.org/sdr/SIMA201912231001), Dec 21, 2019: WIRE. DAMAGED. MAIN DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED MAIN DOOR EXTERNAL EMERGENCY LIGHT IAW EMB140 AMM 33-50-10. REPAIRED WIRE W717-0003-20 IAW EMB140 SWPM 20-2
- [SDR SIMA201912230001](https://openairdocs.org/sdr/SIMA201912230001), Dec 20, 2019: CONTROL UNIT. FAILED. FLAP FAIL WHEN FLAP LEVER MOVED TO 9, EICAS SHOWED FLAPS 0. REMOVED AND REPLACED FECU IAW EMB 140 AMM 27-53-02. OPC FAIL. REMOVED AND REPLACED FVS IAW AMM 27-51
- [SDR SIMA201912121001](https://openairdocs.org/sdr/SIMA201912121001), Dec 11, 2019: LIGHT. INOPERATIVE. 11 B/C INTERIOR OVERHEAD EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED 11 B/C INTERIOR OVERHEAD EMERGENCY LIGHT IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-
- [SDR SIMA201911210002](https://openairdocs.org/sdr/SIMA201911210002), Nov 20, 2019: LAMP. INOPERATIVE. RH OVERWING EMERGENCY LIGHT INOP.-C/A-REMOVED AND REPLACED RH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10. OPS CHECK GOOD AT THIS TIME.
- [SDR SIMA2019112019004](https://openairdocs.org/sdr/SIMA2019112019004), Nov 19, 2019: CONTROL HANDLE. LACK OF LUBE. PARKING BRAKE HARD TO RELEASE-C/A-LUBRICATED EMERGENCY PARKING BRAKE CONTROL IAW ENVOY WIC 32-600-12. OPC GOOD AT THIS TIME. NO DEFECTS NOTED.
- [SDR SIMA201906108002](https://openairdocs.org/sdr/SIMA201906108002), Jun 8, 2019: UNKNOWN. ODOR. VERY STRONG JET FUEL SMELL IN THE COCKPIT AND CABIN AFTER E2 HUNG START WAS ABORTED. FOLLOWING FIM# 72-00-00 AND FIN#21-20-00.INSPECTED ENG.FOR LEAKS & OIL LEVE
- [SDR SIMA20190505002](https://openairdocs.org/sdr/SIMA20190505002), May 5, 2019: DRAIN LINE. CONTAMINATED. UNRELIABLE AIRSPEED. IAS MSG DISPLAYED ON BOTH PFD'S. FO AND STANBY INSTRUMENTS WERE SHOWING CONSISTENT AIRSPEED. EMERGENCY DECLARED. DIVERTED TO OKC. NOT OVERW
- [SDR SIMA2019041009005](https://openairdocs.org/sdr/SIMA2019041009005), Apr 9, 2019: CHARGER. INOPERATIVE. AFT CEILING EXIT SIGN AND LH EXIT DOOR SIGN INOP-C/A-REMOVED AND REPLACED #3 EMERG BATTERY AND POWER SUPPLY IAW AMM 33-50-04 OPS CHECK GOOD. EMERGENCY LIGHTING 
- [SDR SIMA20190319001](https://openairdocs.org/sdr/SIMA20190319001), Mar 19, 2019: CONNECTOR. UNSECURE. FWD CEILING EXIT LIGHT INOP. C/A-RESECURED CONNECTOR ON NR 6 EMERGENCY LIGHT INVERTER OPS CHECK GOOD IAW AMM 33-50-11.
- [SDR SIMA20181231003](https://openairdocs.org/sdr/SIMA20181231003), Dec 31, 2018: WIRE. BROKEN. FOUND BROKEN WIRE GOING TO SERVICE DOOR EMERGENCY EXTERNAL LIGHT. C/A-REPAIRED WIRE AT SPLICE SP7376 IAW SPWM 20-21-00.
- [SDR SIMA20181230002](https://openairdocs.org/sdr/SIMA20181230002), Dec 30, 2018: WIRE. DAMAGED. SUPPLEMENTAL SERVICE DOOR GROUND ILLUMINATION EMERGENCY LIGHT INOP-C/A- "TRANSFERRED TO AML PAGE 4420955 ITEM 2". DEFERRED PER MEL 33-29. REMOVED AND REPLACED E
- [SDR SIMA201812310001](https://openairdocs.org/sdr/SIMA201812310001), Dec 30, 2018: POWER SUPPLY. INOPERATIVE. EXIT ROW CEILING EXIT MARKER LIGHT FWD FACE DOES NOT ILLUMINATE-C/A-RAR #2 EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK IAW AMM 33-50-04. OPS CHECK GOOD
- [SDR SIMA20181213001](https://openairdocs.org/sdr/SIMA20181213001), Dec 13, 2018: ECU. FAILED. SUPPLEMENTAL FLAP FAIL EICAS MESSAGE. FLAPS FAILED AT 0 DEGREES ON APPROACH. C/A-CMC FAULT MSG RH FLAP SENSOR FAIL HAD TO RESTORE FCU TO RESET FLAPS IAW FIM 27-
- [SDR SIMA2018121211007](https://openairdocs.org/sdr/SIMA2018121211007), Dec 11, 2018: LAMP. INOPERATIVE. SERVICE DOOR HINGE COVER EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR HINGE COVER EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-09. OPC GOOD
- [SDR SIMA20181017004](https://openairdocs.org/sdr/SIMA20181017004), Oct 17, 2018: FLASHLIGHT. NOT REPORTED. FLASHLIGHT HOLDER OVER FLIGHT ATTENDANT STATION. FLIGHT CREW PLACARDED FWD FA FLASHLIGHT HOLDER. SUPPLEMENTAL -C/A-FLIGHT CREW PLACARDED FWD FA FLASHLIGHT HOLDE
- [SDR SIMA201808210001](https://openairdocs.org/sdr/SIMA201808210001), Aug 20, 2018: DISPLAY. FAILED. FO MFD FAILED IN FLIGHT WITH ELECTRICAL ODOR. CAPTAIN PULLED THE CIRCUIT BREAKER. RESET THE CIRCUIT BREAKER . REMOVED AND REPLACED THE FIRST OFFICER`S MFD IAW 3
- [SDR SIMA2018072320006](https://openairdocs.org/sdr/SIMA2018072320006), Jul 20, 2018: MODULE. MALFUNCTIONED. AIRCRAFT FAILNG TO PRESSURIZE NO "CABIN ALT" INDICATION NO "CABIN RATE" INDICATION EMERGNECY DECLARED. R&R CPAM IAW AMM 21-32-01. OPC GOOD. PITOT STATIC LEAK CH
- [SDR SIMA201806076007](https://openairdocs.org/sdr/SIMA201806076007), Jun 6, 2018: TIRE. FAILED. DURING TAXI IN AFTER LANDING, THE PLANE STARTED VIBRATING. PULLED OVER TO FIND TWO RIGHT MAIN TIRES FLAT. FOUND THE NR 3 MLG TIRE FLAT. REMOVED AND REPLACED THE
- [SDR SIMA20171207002](https://openairdocs.org/sdr/SIMA20171207002), Dec 7, 2017: CONNECTOR. BROKEN. EMERGENCY PATHWAY LIGHT ON SERVICE DOOR INOP-C/A-REPAIRED EMERGENCY PATHWAY LIGHT ON SERVICE DOOR WIRE TO P7198 PIN C IAW EMB 145 SWPM 20-21-00.
- [SDR SIMA20171207004](https://openairdocs.org/sdr/SIMA20171207004), Dec 7, 2017: CHARGER. INOPERATIVE. EMERGENCY FLOOR LIGHTING FROM 3A TO 6A INOP-C/A-REMOVED AND REPLACED #2 BATTERY HOLDER AND BATTERY CHARGER ASSEMBLY IAW EMB 145 AMM 33-50-04
- [SDR SIMA20171207003](https://openairdocs.org/sdr/SIMA20171207003), Dec 7, 2017: CONNECTOR. BROKEN. #2 FLOOR EMERGENCY LIGHT STRIP HAS BROKEN WIRE-C/A-REPAIRED #2 FLOOR PROXIMITY LIGHT WIRE IAW EMB 145 SWPM 20-50-00.
- [SDR SIMA20171206002](https://openairdocs.org/sdr/SIMA20171206002), Dec 6, 2017: WIRE. BROKEN. RH EMERGENCY LIGHT HAS BROKEN WIRES (WIRE# P8560) ON FUSELAGE FAIRING-C/A-REPAIRED RH 2 EMERGENCY LIGHT WIRES (WIRE# P8560) IAW EMB 140 SWPM 20-00-03 AND 20-21-
- [SDR SIMA20171204002](https://openairdocs.org/sdr/SIMA20171204002), Dec 4, 2017: SKIN. DENTED. 2 DENTS AND 1 PROTRUSION BTW FR 19-20 STR 11-12L-C/A-REPAIRED 2 DENTS AND 1 PROTRUSION BTW FR 19-0 STR 11-12L IAW ERS-EM-53MR-3029
- [SDR SIMA20171129003](https://openairdocs.org/sdr/SIMA20171129003), Nov 29, 2017: WIRE. DAMAGED. #3 EMERGENCY LIGHT STRIP WIRES DAMAGED FROM ASSEMBLY-C/A-REMOVED AND REPLACED #3 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12.
- [SDR SIMA20171128008](https://openairdocs.org/sdr/SIMA20171128008), Nov 28, 2017: SKIN. NICKED. SKIN NICKED FWD OF FR 14 BTW STR 20-21L-C/A-PERFORMED REPAIR TO SKIN FWD OF FR 14 BTW STR 20-21L IAW EMB 140 SRM 53-21-01 FIG. 206
- [SDR SIMA20171127006](https://openairdocs.org/sdr/SIMA20171127006), Nov 27, 2017: DOOR SILL. CORRODED. CARGO DOOR SILL IS CORRODED-C/A-RAR CARGO DOOR SILL IAW EMB 145 SRM 51-40-02
- [SDR SIMA20171127004](https://openairdocs.org/sdr/SIMA20171127004), Nov 27, 2017: FRAME. CRACKED. CO PILOT'S SIDE FRAME 10 CRACKED BELOW DV WINDOW TRACK-C/A-REMOVED AND REPLACED CO PILOT'S SIDE FRAME 10 IAW EMB 145 SRM 51-40-02
- [SDR SIMA20171127005](https://openairdocs.org/sdr/SIMA20171127005), Nov 27, 2017: FRAME. CRACKED. PILOT'S SIDE FRAME 10 CRACKED BELOW DV WINDOW TRACK-C/A-REMOVED AND REPLACED PILOT'S SIDE FRAME 10 IAW EMB 145 SRM 51-40-02
- [SDR SIMA20171127003](https://openairdocs.org/sdr/SIMA20171127003), Nov 27, 2017: FRAME. CRACKED. CRACKS AROUND RIVETS ON L/H FRAME 78. REPAIRED CRACKS AROUND RIVETS ON LH FRAME 78 IAW ERS-EM-53MR-3020
- [SDR SIMA20171126004](https://openairdocs.org/sdr/SIMA20171126004), Nov 26, 2017: FITTING. CRACKED. MACHINED FITTING BETWEEN FRAMES 19 AND 20 AT STRINGER 3L CRACKED-C/A-REMOVED AND REPLACED MACHINED FITTING BETWEEN FRAMES 19 AND 20 AT STRINGER 3L CRACKED IAW E
- [SDR SIMA20171124003](https://openairdocs.org/sdr/SIMA20171124003), Nov 24, 2017: FRAME. CRACKED. FRAME 23 CRACKED AT RH OTBD FLOOR SUPPORT-C/A-REPAIRED FRAME 23 CRACK BETWEEN STRINGERS 15R - 16R AT RH OTBD FLOOR SUPPORT IAW EM-53MR-1808
- [SDR SIMA20171122004](https://openairdocs.org/sdr/SIMA20171122004), Nov 22, 2017: FITTING. CRACKED. L/H PYLON LOWER FWD ENGINE YOKE FITTING CRACKED-C/A-REMOVED AND REPLACED L/H PYLON LOWER FWD ENGINE YOKE FITTING IAW EO EM-54MR-386.
- [SDR SIMA20171121004](https://openairdocs.org/sdr/SIMA20171121004), Nov 21, 2017: SUPPORT. CORRODED. SSI 53-20-29; LAV EXTERNAL WASTE VALVE SUPPORT IS CORRODED-C/A-REMOVED AND REPLACED LAV EXTERNAL WASTE VALVE SUPPORT IAW EMB 140-SRM 51-40-02
- [SDR SIMA20171121005](https://openairdocs.org/sdr/SIMA20171121005), Nov 21, 2017: FLOOR SUPPORT. CORRODED. SSI 53-20-11; LEFT OMEGA BEAM IS CORRODED AT FR 38-C/A-REPAIRED LEFT OMEGA BEAM AT FR 38 IAW EMB 140 SRM 53-00-10, FIG 202 SHEET II
- [SDR SIMA20171121003](https://openairdocs.org/sdr/SIMA20171121003), Nov 21, 2017: FLOOR SUPPORT. CORRODED. SSI; 53-20-11 LEFT OMEGA BEAM IS CORRODED BTW FR 57-59-C/A-REPAIRED LEFT OMEGA BEAM BTW FR 57-59 IAW EO-EM-53MR-1518 REV 3
- [SDR SIMA20171117004](https://openairdocs.org/sdr/SIMA20171117004), Nov 17, 2017: WIRE. BROKEN. LH #2 CABIN FLOOR PROXIMITY LIGHT WIRE BROKEN-C/A-REMOVED AND REPLACED LH #2 CABIN FLOOR PROXIMITY LIGHT IAW EMB 140 AMM 33-50-12-04
- [SDR SIMA20171004011](https://openairdocs.org/sdr/SIMA20171004011), Oct 4, 2017: WIRE. DAMAGED. EMERGENCY LIGHT HAD WIRE INSULATION DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20171004012](https://openairdocs.org/sdr/SIMA20171004012), Oct 4, 2017: LIGHT. DAMAGED. LEFT CABIN FLOOR, FIVE EMERGENCY LIGHT EXTRUSIONS CRACKED. R & R THE LIGHTS IAW AMM 33-50-12-04.
- [SDR SIMA20160519002](https://openairdocs.org/sdr/SIMA20160519002), May 19, 2016: SIGN. INOPERATIVE. EXIT MARKER SIGN ON LT EMER EXIT DOOR INOPERATIVE. R & R EXIT MARKER SIGN IAW AMM 33-50-14. OPERATIONS CHECKED GOOD.
- [SDR SIMA20160427001](https://openairdocs.org/sdr/SIMA20160427001), Apr 27, 2016: HYDRAULIC LINE. NOT REPORTED. DURING FLIGHTS NOTICED HYD 1 LO QTY, AFTER LG EXTENSION, 3 DOWN, GOT ENG 1 HYD PUMP FAIL. COMPLIED WITH CHECKLIST. TRANSFERRED TO NRWC 809-DFW-02349. R & R LT M
- [SDR SIMA20160120002](https://openairdocs.org/sdr/SIMA20160120002), Jan 20, 2016: DISPLAY. FAILED. STRONG ELEC ODOR IN COCKPIT. REPLACED CAPTAINS MFD IAW AMM 34-22-01. OPERATIONS CHECKED GOOD.
- [SDR SIMA20151215003](https://openairdocs.org/sdr/SIMA20151215003), Dec 15, 2015: BATTERY. DISCHARGED. EMERGENCY LIGHTS ON FLOOR MID-WAY IN CABIN INOPERATIVE. R & R NR 3 EMER LIGHT BATTERY CHARGER & BATTERY IAW WC 33-700-17 & 33-700-19. OPERATIONS CHECKED GOOD. C
- [SDR SIMA20151023002](https://openairdocs.org/sdr/SIMA20151023002), Oct 23, 2015: CHARGER. FAILED. EMERGENCY LIGHTS, FWD AISLE STRIP, GALLEY SERVICE DOOR & FWD EXTERNAL RT EMER LIGHT FLICKERS OFF AFTER ABOUT A SECOND AFTER BEING TURNED ON. ALL ARE POWERED BY 
- [SDR SIMA20150611002](https://openairdocs.org/sdr/SIMA20150611002), Jun 11, 2015: LIGHT. INOPERATIVE. SERVICE DOOR EMER LIGHT INOPERATIVE. R & R LAMP WITH NEW. OPERATIONS CHECKED GOOD IAW MM CH 33-50-10.
- [SDR SIMA20150524003](https://openairdocs.org/sdr/SIMA20150524003), May 24, 2015: UNIVERSAL. MALFUNCTIONED. UNABLE TO CONTROL TEMP IN COCKPIT. TEMP CLIMBING THROUGH FL 190 DROPPED TO +7C IN COCKPIT. R & R NR 1 DIGITAL TEMP CONTROLLER IAW AMM-21-60-04. DID NOT FIX, SEE
- [SDR SIMA20150519007](https://openairdocs.org/sdr/SIMA20150519007), May 19, 2015: FCU. FAILED. ON TAKEOFF ROLL, RECEIVED FUEL 1 - 2 LO LEVEL WARNING & BOTH FUEL QTY GAUGES SHOWED DASHES, TAKEOFF ABORTED. R & R FCU IAW AMM 28-41-01. OPERATIONS CHECK FOUND 
- [SDR SIMA20150328002](https://openairdocs.org/sdr/SIMA20150328002), Mar 28, 2015: PRESSURE SWITCH. INOPERATIVE. AT ALT 240 RECEIVED YD & AP FAIL FOLLOWED BY RUDDER SYS 1 - 2 INOPERATIVE. EXAMINED AFCS EVENT CODES, CODE 271 PREVIOUS FLIGHT & LAST NIGHT, RUDDER HYD MON. AFC

All 127: https://openairdocs.org/aircraft/N809AE/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/N809AE/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.