# N819AE: 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 AE-3007A1P](https://openairdocs.org/engine/rolls-royce-ae-3007a1p) (registry code 54571)
- 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: 145566
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 24, 2002
- Certificate issued: July 10, 2025
- Expires: July 31, 2032
- Mode S code: AB2AD0
- Registered owner: [Avi Sales & Leasing Services LLC](https://openairdocs.org/faa-owner/AVI%20SALES%20%26%20LEASING%20SERVICES%20LLC)
- Location: [Muskegon, MI](https://openairdocs.org/faa-place/MI/Muskegon)
- Owner type: LLC
- Owner's area on the map: 43.1800° N, 86.2868° W: Placed by OpenAirDocs at the center of ZIP code 49441, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=819AE
- Page: https://openairdocs.org/aircraft/N819AE

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.

## ADs that may apply (OpenAirDocs): 81 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 AE-3007A1P)

- [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 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 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 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 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 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 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 2008-19-51](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 96: https://openairdocs.org/aircraft/N819AE/ads.md

## Information bulletins (advisory) (8 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 AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N819AE.

## FAA accident and incident reports

None matched to N819AE.

## Service difficulty reports (138, 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 SIMA201910310004](https://openairdocs.org/sdr/SIMA201910310004), Oct 30, 2019: LIGHT. INOPERATIVE. MAIN PAX DOOR UPPER EMERGENCY EXIT LIGHT INOP.-C/A-REMOVED AND REPLACED PAX DOOR EXIT MARKER IAW EMB 140 AMM 33-50-13. OPS CHECK GOOD IAW EMB 140 AMM 33-50-00.
- [SDR SIMA20190610001](https://openairdocs.org/sdr/SIMA20190610001), Jun 10, 2019: FLASHLIGHT. INOPERATIVE. AFT F/A FLASHLIGHT INOP. REMOVED AND REPLACED AFT F/A FLASHLIGHT IAW AMM 33-50-16 OPS CHECK GOOD.
- [SDR SIMA20190430007](https://openairdocs.org/sdr/SIMA20190430007), Apr 30, 2019: SHUTTLE VALVE. FAILED. EMRG BRAKE LO PRESSURE. C/A-REMOVED AND REPLACED NR 4 BRAKE SHUTTLE VALVE IAW CMM CH 32-49-10 LEAK CHECK GOOD.
- [SDR SIMA201811298001](https://openairdocs.org/sdr/SIMA201811298001), Nov 28, 2018: NIPPLE. OVERHEATED. "TRANSFERRED FROM AML PAGE 4343084 ITEM 1" AFTER APU START AND OPERATING PACK 2 FOR APPROX 3 MINUTES, SMELLED ELETRICAL HEAT/BURNING SMELL WHILE AT THE GATE. F/
- [SDR SIMA201811276006](https://openairdocs.org/sdr/SIMA201811276006), Nov 26, 2018: ACM. FAILED. SMELL OF SOMETHING HEATED ODOR AT GATE PRIOR TO PUSH BACK REPEAT WRITE UP FROM PREVIOUS 2 DAYS-C/A-REMOVED AND REPLACED R/H AIR CYCLE MACHINE IAW AMM 21-51-03. 
- [SDR SIMA20181126002](https://openairdocs.org/sdr/SIMA20181126002), Nov 26, 2018: FAN. FAILED. ELECTRICAL SMELL NOTED IN THE FRONT OF THE CABIN WHEN WE ARRIVED AT THE GATE-C/A-T/S FOUND RT RECIRCULATION FAN BURN. REMOVED AND REPLACED CABIN RECIRCULATION F
- [SDR SIMA20180716003](https://openairdocs.org/sdr/SIMA20180716003), Jul 16, 2018: PROXIMITY SWITCH. DISCONNECTED. "LG AIR/GND FAIL" EICAS MESSAGE FROM GEAR RETRACTION UNTIL PARKING. NORMAL BRAKING ON TOUCHDOWN NORMAL SPOILER DEPLOY-C/A-PERFORMED TROUBLESHOOTING PER FIM 32-6
- [SDR SIMA201805310002](https://openairdocs.org/sdr/SIMA201805310002), May 30, 2018: FUSE. INOPERATIVE. LEFT EXTERNAL WING TO FUSELAGE EMERGENCY LIGHT INOPERATIVE. R & R THE FUSE F1 ON BATTERY CHARGER NR 1 IAW CMM 25-60-03. OPS CHECKED GOOD.
- [SDR SIMA20171011005](https://openairdocs.org/sdr/SIMA20171011005), Oct 11, 2017: CRADLE. DAMAGED. FA FORWARD FLASHLIGHT LOOSE IN HOLDER AND NOT CHARGING. REMOVED AND REPLACED THE FLASHLIGHT HOLDER IAW AMM 33-50-16. OPS CHECKED GOOD.
- [SDR SIMA20170927010](https://openairdocs.org/sdr/SIMA20170927010), Sep 27, 2017: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM CORRODED AT AND AROUND THE CROSSBEAM AT FRAME 44. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-2929.
- [SDR SIMA20170927009](https://openairdocs.org/sdr/SIMA20170927009), Sep 27, 2017: STRINGER. GOUGED. STRINGER 18R GOUGED AT FRAME 23. REPAIRED THE STRINGER IAW SRM 53-00-03-RE.
- [SDR SIMA20170927008](https://openairdocs.org/sdr/SIMA20170927008), Sep 27, 2017: FRAME. CORRODED. FRAME 13 CORRODED AT STRINGER 21L AND 21R. REPAIRED THE FRAME IAW ERS-EM-53MR-2937.
- [SDR SIMA20170927007](https://openairdocs.org/sdr/SIMA20170927007), Sep 27, 2017: FRAME. CRACKED. FRAME 23 CRACKED AT STRINGER 16R. REPAIRED THE FRAME IAW EO EM-53MR-1808.
- [SDR SIMA20170922005](https://openairdocs.org/sdr/SIMA20170922005), Sep 22, 2017: FLANGE. GOUGED. OUTBOARD LOWER FLANGE OF CARGO DOOR GOUGED. REMOVED AND REPLACED THE FLANGE IAW SRM 51-40-02
- [SDR SIMA20170922004](https://openairdocs.org/sdr/SIMA20170922004), Sep 22, 2017: FRAME. CHAFED. FRAME 18 IS CHAFED AT STRINGER 2R. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-40-02.
- [SDR SIMA20170921007](https://openairdocs.org/sdr/SIMA20170921007), Sep 21, 2017: SUPPORT. CRACKED. PAX DOOR CUTOUT SUPPORT CRACKED AT FRAME 20, STRINGER 3L. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-40-02.
- [SDR SIMA20170921006](https://openairdocs.org/sdr/SIMA20170921006), Sep 21, 2017: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM IS CORRODED BETWEEN FRAMES 49 AND 50. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-2925
- [SDR SIMA20170919005](https://openairdocs.org/sdr/SIMA20170919005), Sep 19, 2017: LINER. CORRODED. MAIN DOOR LOWER EDGE LINER NUTPLATE HOLES ARE CORRODED. REPAIRED IAW SRM 52-10-02, AND ETN-EM-52-041.
- [SDR SIMA20170919004](https://openairdocs.org/sdr/SIMA20170919004), Sep 19, 2017: WINDOW FRAME. CRACKED. CO-PILOT WINDSHIELD CUTOUT TOP OTBD CORNER HAS A CRACK ON LATERAL POST FRAME. REMOVED AND REPLACED THE WINDOW FRAME IAW SRM 51-40-02
- [SDR SIMA20170918005](https://openairdocs.org/sdr/SIMA20170918005), Sep 18, 2017: CHANNEL. CORRODED. SERVICE DOOR CENTER CHANNEL CORRODED. REMOVED AND REPLACED THE CHANNEL IAW SRM 51-40-02
- [SDR SIMA20170918007](https://openairdocs.org/sdr/SIMA20170918007), Sep 18, 2017: DOOR SILL. CORRODED. CARGO DOOR CUTOUT LOWER DOOR SILL CORRODED. REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02
- [SDR SIMA20170918006](https://openairdocs.org/sdr/SIMA20170918006), Sep 18, 2017: SHEAR TIE. CORRODED. CARGO DOOR CUTOUT SHEAR TIE CORRODED AT FRAME 65. REPAIRED IAW SRM 53-31-04.
- [SDR SIMA20170815007](https://openairdocs.org/sdr/SIMA20170815007), Aug 15, 2017: ANGLE. CRACKED. CENTER BEAM RT FWD TO AFT GALLEY DIGITAL SPLICE ANGLE CRACKED. REMOVED AND REPLACED THE SPLICE ANGLE IAW SRM 51-40-02.
- [SDR SIMA20170815005](https://openairdocs.org/sdr/SIMA20170815005), Aug 15, 2017: FLOOR SUPPORT. CORRODED. CENTER OMEGA BEAM CORRODED AT, AND AROUND THE CROSSBEAM BETWEEN FRAMES 57 - 59. ACCOMPLISHED A PERMENANT REPAIR IAW EO-EM-53MR-1518, PART B.
- [SDR SIMA20170815006](https://openairdocs.org/sdr/SIMA20170815006), Aug 15, 2017: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM CORRODED AT AND AROUND THE CROSSBEAM BETWEEN FRAMES 57 - 59. ACCOMPLISHED A PERMANENT REPAIR OF THE OMEGA BEAM IAW ERS-EM-53MR-2955.
- [SDR SIMA20170815008](https://openairdocs.org/sdr/SIMA20170815008), Aug 15, 2017: ANGLE. CRACKED. LEFT BEAM OTBD FWD TO AFT GALLEY DIGITAL SPLICE ANGLE CRACKED. REMOVED AND REPLACED THE SPLICE ANGLE IAW SRM 51-40-02.
- [SDR SIMA20170815009](https://openairdocs.org/sdr/SIMA20170815009), Aug 15, 2017: ANGLE. CRACKED. LEFT BEAM INBD FWD TO AFT GALLEY DIGITAL SPLICE ANGLE CRACKED. REMOVED AND REPLACED THE SPLICE ANGLE IAW SRM 51-40-02.
- [SDR SIMA20170815011](https://openairdocs.org/sdr/SIMA20170815011), Aug 15, 2017: ANGLE. CRACKED. CENTER BEAM LT FWD TO AFT GALLEY DIGITAL SPLICE ANGLE CRACKED. REMOVED AND REPLACED THE SPLICE ANGLE IAW SRM 51-40-02.
- [SDR SIMA20170815010](https://openairdocs.org/sdr/SIMA20170815010), Aug 15, 2017: CROSSBEAM. CORRODED. FRAME 20 CENTER AISLE CROSSBEAM CORRODED. R & R THE CROSSBEAM IAW SRM 51-40-02.
- [SDR SIMA20161215001](https://openairdocs.org/sdr/SIMA20161215001), Dec 15, 2016: LIGHT. INOPERATIVE. LAST CEILING EMERGENCY LIGHT FOUND INOPERATIVE. R & R THE EMERGENCY LIGHT IAW AMM33-50-08-04, OPS CHECKED GOOD
- [SDR SIMA20161024003](https://openairdocs.org/sdr/SIMA20161024003), Oct 24, 2016: CRADLE. BROKEN. FLASHLIGHT CRADLE BROKEN AT FWD GALLEY. REMOVED AND REPLACED THE CRADLE AND FLASHLIGHT ASSY. IAW AMM 33-50-16, OPS CHECKED GOOD
- [SDR SIMA20160831001](https://openairdocs.org/sdr/SIMA20160831001), Aug 31, 2016: ROLLER. UNKNOWN. MAIN CABIN DOOR IS HARD TO OPEN & CLOSE. SERVICED MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02. OPS CHECKED GOOD.
- [SDR SIMA20160620001](https://openairdocs.org/sdr/SIMA20160620001), Jun 20, 2016: UNKNOWN. ODOR. ON DEPARTURE, GOT BURNING RUBBER ODOR FOLLOWED BY AN SHORT ELECTRICAL ODOR. DECLARED EMERGENCY. COMPLETED FIM TASK 21-20-00-810-A AND FIM TASK 21-20-00-810-803-
- [SDR SIMA20160416001](https://openairdocs.org/sdr/SIMA20160416001), Apr 16, 2016: INVERTER. INOPERATIVE. EMERGENCY LIGHTS IN ROW 7 - 10 & LOWER EMER LIGHTS ON EMER EXIT DOORS INOPERATIVE. TROUBLE SHOT IAW FIM 33-50-00 FOUND INVERTER 5 TO BE INOPERATIVE. R & R INVER
- [SDR SIMA20151028002](https://openairdocs.org/sdr/SIMA20151028002), Oct 28, 2015: WARNING SYSTEM. FALSE ACTIVATION. SPOILER FAIL MSG ON EICAS WITH OPEN INSCRIPTION IN SPOILERS STATUS BOX. OCCURRED AT FL 360 WITH NO OBVIOUS CONTROLLABILITY ISSUES. COMPLIED WITH SPOILER OPERATI
- [SDR SIMA20151012001](https://openairdocs.org/sdr/SIMA20151012001), Oct 12, 2015: FLASHLIGHT. BROKEN. REAR CABIN FLASHLIGHT BROKEN. R & R REAR CABIN EMER FLASHLIGHT IAW AMM 25-60-0.
- [SDR SIMA20150924005](https://openairdocs.org/sdr/SIMA20150924005), Sep 24, 2015: LIGHT. INOPERATIVE. EMERGENCY LIGHTS AT ROWS 7 - 11 ARE INOPERATIVE. CHARGED EMER LIGHTS AT ROWS 7 - 11. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.
- [SDR SIMA20150813004](https://openairdocs.org/sdr/SIMA20150813004), Aug 13, 2015: LIGHT. INOPERATIVE. THE LAST FLOOR PROXIMITY STRIP LIGHT IN THE AFT CABIN IS INOPERATIVE. R & R THE LAST FLOOR PROXIMITY LIGHT STRIP IN THE AFT CABIN IAW AMM 33-50-12. OPERATIONS C
- [SDR SIMA20150807002](https://openairdocs.org/sdr/SIMA20150807002), Aug 7, 2015: LIGHT. OUT OF ADJUST. EMERGENCY CTR FLOOR LIGHTING INOPERATIVE. PERFORMED ADJUSTMENT OF EMER LIGHTING SYS IAW AMM 33-50-00. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150715004](https://openairdocs.org/sdr/SIMA20150715004), Jul 15, 2015: INVERTER. INOPERATIVE. FORWARD EMER FLOOR STRIP & SERVICE DOOR MARKER LIGHTS INOPERATIVE. R & R EMER LIGHT INVERTER NR 3 IAW AMM 33-50-11. OPERATIONAL CHECKED GOOD.
- [SDR SIMA20150621003](https://openairdocs.org/sdr/SIMA20150621003), Jun 21, 2015: INVERTER. INOPERATIVE. FIRST FLOOR EMER LIGHT STRIP IN PAX CABIN & SERVICE DOOR LOWER EXIT MARKER DID NOT ILLUMINATE. R & R NR 2 DC & AC INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED 
- [SDR SIMA20150506001](https://openairdocs.org/sdr/SIMA20150506001), May 6, 2015: BATTERY. DISCHARGED. DURING PS 1 CHECK, FOUND NR 3 & 4 FLOOR PROXIMITY LIGHT STRIPS INOPERATIVE. R & R NR 3 EMER LIGHTING BATTERY & CHARGER IAW WC 33-700-19. OPERATIONS CHECKED IAW 
- [SDR SIMA20150407001](https://openairdocs.org/sdr/SIMA20150407001), Apr 7, 2015: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS FOR FLIGHT COMPARTMENT CEILING, LT FWD FAIRING & AISLE CEILING PANEL NR 1 INOPERATIVE. R & R NR 1 EMER LIGHTS BATTERY POWER SUPPLY & BATTERY PA
- [SDR SIMA20150313008](https://openairdocs.org/sdr/SIMA20150313008), Mar 13, 2015: WIRE. BROKEN. EMERGENCY LIGHT STRIP NR 2 HAS BROKEN WIRES. R & R EMER LIGHT STRIP NR 2 IAW AMM 33-50-12. SEE BOW 181199 FOR OPERATIONS CHECK.
- [SDR SIMA20150313007](https://openairdocs.org/sdr/SIMA20150313007), Mar 13, 2015: CONNECTOR. BROKEN. LEFT NR 5 EMER LIGHT STRIP BROKEN AT CONNECTOR, LIGHT STRIP SIDE. R & R LT EMER LIGHT STRIP NR 5 IAW AMM 33-50-12. SEE BOW 181199 FOR OPERATIONS CHECK.
- [SDR SIMA20150313010](https://openairdocs.org/sdr/SIMA20150313010), Mar 13, 2015: WIRE. BROKEN. EMERGENCY LIGHT STRIP NR 8 HAS A BROKEN WIRE ON THE ACFT SIDE. INSTALLED NEW CONNECTOR AT EMER LIGHT STRIP NR 8 IAW SWPM 20-00-03,20-21-00 & WM 91-10-02.
- [SDR SIMA20150313005](https://openairdocs.org/sdr/SIMA20150313005), Mar 13, 2015: WIRE. BROKEN. EMERGENCY LIGHT STRIP NR 7 HAS BROKEN WIRES. R & R EMER LIGHT STRIP NR 7 IAW AMM 33-50-12. SEE BOW 181199 FOR OPERATIONS CHECK.
- [SDR SIMA20150313009](https://openairdocs.org/sdr/SIMA20150313009), Mar 13, 2015: LIGHT. INOPERATIVE. NUMBER 1 FLOOR PROXIMITY EMER LIGHT STRIP INOPERATIVE. R & R NR 1 EMER FLOOR PROXIMITY LIGHT IAW AMM 33-50-12. SEE BOW 181199 FOR OPERATIONAL CHECK OF EMER LIGH
- [SDR SIMA20150313006](https://openairdocs.org/sdr/SIMA20150313006), Mar 13, 2015: WIRE. BROKEN. EMERGENCY LIGHT WIRE AT FRAME 25 BROKEN. FOUND BROKEN WIRES AT FRAME 27 & NOT FRAME 25. REPAIRED WIRES W192-8900-22 & W192-8901-22 FOR EMERGENCY LIGHT WIRES IAW
- [SDR SIMA20150311006](https://openairdocs.org/sdr/SIMA20150311006), Mar 11, 2015: FLOOR SUPPORT. CORRODED. LAVATORY LT OMEGA BEAM IS CORRODED. REPAIRED IAW ERS-EM-53MR-1133.

All 138: https://openairdocs.org/aircraft/N819AE/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/N819AE/stcs.md

## Related

- Other Embraer EMB-135KL aircraft: https://openairdocs.org/model/embraer-emb-135kl/aircraft.md
- The Rolls-Royce AE-3007A1P engine: https://openairdocs.org/engine/rolls-royce-ae-3007a1p.md

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