# N619AE: 1998 Embraer EMB-145LR

- Status: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212, 55 seats)
- Engine: [Allison AE3007C series](https://openairdocs.org/engine/allison-ae3007c-series) (registry code 03028)
- 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: 145101
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 23, 1998
- Certificate issued: September 6, 2011
- Expires: September 30, 2027
- Mode S code: A81032
- Registered owner: [American Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRLINES%20INC)
- Location: [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth)
- Owner type: Corporation
- Owner's area on the map: 32.8240° N, 97.0491° W: Placed by OpenAirDocs at the center of ZIP code 76155, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=619AE
- Page: https://openairdocs.org/aircraft/N619AE

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 Allison AE3007C model are included.

## ADs that may apply (OpenAirDocs): 102 in force

### Matched by airframe (Embraer EMB-145LR)

- [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 2025-08-07](https://openairdocs.org/ad/2025-08-07): Flight Controls · Embraer EMB-145, EMB-145ER, EMB-145MR and 4 more. Effective Jun 26, 2025
- [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 2009-01-05](https://openairdocs.org/ad/2009-01-05): Maximum takeoff weight (MTOW) · Embraer EMB-145, EMB-145EP, EMB-145ER and 4 more. Effective Mar 27, 2009
- [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 2007-10-11](https://openairdocs.org/ad/2007-10-11): Electrical bonding clamps · Embraer EMB-135BJ (Legacy 600), EMB-135LR, EMB-145LR and 2 more. Effective Jun 21, 2007
- [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

### Matched by engine (Allison AE3007C series)

- [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 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 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 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 2006-20-08](https://openairdocs.org/ad/2006-20-08) (historical): Rod ends of aileron power control actuator, superseding AD 99-05-04 · Embraer EMB-145, EMB-145EP, EMB-145ER and 4 more. Effective Nov 8, 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 2001-17-04](https://openairdocs.org/ad/2001-17-04) (historical): Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Sep 5, 2001
- [AD 2000-04-09](https://openairdocs.org/ad/2000-04-09) (historical): Elevator Servo Tab and Spring Tab Hinge Fittings of the Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Mar 10, 2000
- [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 113: https://openairdocs.org/aircraft/N619AE/ads.md

## Information bulletins (advisory) (9 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 AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations (2)

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 DCA20LA013](https://openairdocs.org/ntsb/DCA20LA013), Nov 11, 2019: Embraer EMB145 (N619AE), Chicago, IL, substantial damage. Probable cause: The flight crew’s inability to maintain the airplane on the runway centerline after touchdown due to the reduced braking action resulting from the deteriorating weather conditions, which caused the…
- [NTSB CEN13CA117](https://openairdocs.org/ntsb/CEN13CA117), Dec 29, 2012: Embraer EMB-145LR (N619AE), Chicago, IL, no damage. Probable cause: The presence of deice fluid on the floor, which resulted in a slip hazard and an injury to the flight attendant.

## 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.

- [Accident 20191111016409A](https://openairdocs.org/incident/20191111016409A), Nov 11, 2019: Embraer EMB-145LR (N619AE), Chicago, IL, Substantial damage. An envoy Embraer ERJ-145, registration N619AE performing flight AA-4125 from greensboro,NC to Chicago O'Hare,IL (usa) with 38 passengers and 3 crew, landed on…

## Service difficulty reports (165, 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 SIMA20221114001](https://openairdocs.org/sdr/SIMA20221114001), Nov 14, 2022: CRADLE. BROKEN. FWD F/A'S EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-RAR F/A'S FLASHLIGHT BRACKET CLAMP FINGER IAW AMM 33-50-16. OPC GOOD.
- [SDR SIMA20221025001](https://openairdocs.org/sdr/SIMA20221025001), Oct 25, 2022: LAMP. INOPERATIVE. AFT CEILING LINING EMERGENCY LIGHT INOP-C/A-RAR AFT CEILING EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD. END.
- [SDR SIMA20221021003](https://openairdocs.org/sdr/SIMA20221021003), Oct 21, 2022: LAMP. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHTS OUT-C/A-RAR EMERGENCY LIGHT LAMP AS IN EMB145 AMM 33-50-09. OPS CK GOOD
- [SDR SIMA20220821002](https://openairdocs.org/sdr/SIMA20220821002), Aug 21, 2022: LAMP. INOPERATIVE. ROW 12 CEILING EMERGENCY LIGHT INOP-C/A-RAR ROW 12 CEILING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD. END.
- [SDR SIMA20220821001](https://openairdocs.org/sdr/SIMA20220821001), Aug 21, 2022: LAMP. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND33-50-09-400-801-A. NO FIX. FOUND WIRES DISCONNECT
- [SDR SIMA20220714001](https://openairdocs.org/sdr/SIMA20220714001), Jul 14, 2022: EFIS. INOPERATIVE. DESCENDING THROUGH 8,000 FT AURAL WARNING CAUTION CAME, IT WAS THE LANDING GEAR TOO LOW TERRAIN, PULL UP. THE RA WAS SHOWING 30 FT. THE FAILURE LASTED FOR ABOUT
- [SDR SIMA20220625002](https://openairdocs.org/sdr/SIMA20220625002), Jun 25, 2022: RADIO ALTIMETER. INTERMITTENT. DURING DESCENT THOUGH 6000 RADAR ALTIMETER INDICATED 25' AND RECIVED AUDIBLE "TOO LOW TERAIN AND PULL UP" REF AML PG. 4874576 ITEM 1 "TRANSFERRED TO NRWC 619-AB
- [SDR SIMA20220218002](https://openairdocs.org/sdr/SIMA20220218002), Feb 18, 2022: NONE. NONE. RH OVERWNIG EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.
- [SDR SIMA20211016001](https://openairdocs.org/sdr/SIMA20211016001), Oct 16, 2021: NONE. NONE. OVERWING EMERGENCY EXIT FORWARD CEILING LOCATOR LIGHT INOP-C/A-RAR NO. 6 EMERGENCY LIGHT AC/DC INVERTER IAW EMB 145 AMM 33-50-11. OPC GOOD.
- [SDR SIMA20210719002](https://openairdocs.org/sdr/SIMA20210719002), Jul 19, 2021: LIGHT. INOPERATIVE. DURING PS-2 CHECK FOUND RH CENTER FAIRING EXTERIOR EMERGENCY LIGHT INOP-C/A-RAR RH CENTER FAIRING EXTERIOR EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. OPS CHECK G
- [SDR SIMA20210714002](https://openairdocs.org/sdr/SIMA20210714002), Jul 14, 2021: LIGHT. BROKEN. EMERGENCY FLOOR LIGHT AT ROW 8/9 WIRE BROKEN OFF-C/A-REPLACED EMERGENCY FLOOR LIGHT STRIP AT ROW 8/9 IAW EMB 145MM 33-50-12.
- [SDR SIMA20210709003](https://openairdocs.org/sdr/SIMA20210709003), Jul 9, 2021: CLAMP. BROKEN. FA EMERGENCY FLASHLIGHT MOUNT HAS A BROKEN CLAMP-C/A-RAR FWD FA EMERGENCY FLASHLIGHT IAW EMB145 AMM 33-50-16. OPC GOOD.
- [SDR SIMA20210104001](https://openairdocs.org/sdr/SIMA20210104001), Jan 4, 2021: FLASHLIGHT ASSY. BROKEN. FA EMERGENCY FLASHLIGHT CLIP AND FLASHLIGHT BROKEN. MEL 25-53, AUTH 010001-C, LGPG 4714201, ITEM 1. C/A: REMOVED AND REPLACED F/A EMERGENCY FLASHLIGHT ASSEMBLY,
- [SDR SIMA20201204003](https://openairdocs.org/sdr/SIMA20201204003), Dec 4, 2020: LATCH. BROKEN. F/A EMERGENCY FLASHLIGHT HOLDER FWD CABIN HAS LATCH BROKE. C/A: R & R FWD EMERGENCY FLASHLIGHT, IAW EMB 145 AMM 33-50-16. OPERATIONS CHECK GOOD.
- [SDR SIMA202009076004](https://openairdocs.org/sdr/SIMA202009076004), Sep 6, 2020: CONNECTOR. LOOSE. APROX 15,000 MSL - RECEIVED ARUAL TO LOW TERRAIN WARNING BRIEFLY APPROXIMATELY 4,000 MSL. RECEIVED AURAL TOO LOW TERRAIN AND LANDING GEAR WARNING BRIEFLY. TRANS
- [SDR SIMA2020083129006](https://openairdocs.org/sdr/SIMA2020083129006), Aug 29, 2020: DRAG ANGLE. CRACKED. CRACK ON RH FWD VERTICAL TO FUSELAGE DRAG ANGLE NEAR AFT END IN RADIUS.-C/A-REMOVED AND REPLACED RH FWD VERTICAL TO FUSELAGE DRAG ANGLE IAW EMB 145 SRM 51-40-02
- [SDR SIMA2020083129005](https://openairdocs.org/sdr/SIMA2020083129005), Aug 29, 2020: SKIN. DEFORMED. SKIN DEFORMATION LOCATED AT FRAME 23 STRINGERS 16R ? 17R.-C/A-SKIN DEFORMATION LOCATED AT FRAME 23 STRINGERS 16R ? 17R. FOUND STRINGER 17R AT FR 23 TO BE BENT. 
- [SDR SIMA20200824005](https://openairdocs.org/sdr/SIMA20200824005), Aug 24, 2020: RIB. CRACKED. LEFT WING RIB 21 INSIDE PANEL 551CB IS CRACKED. REPAIRED THE LT WING RIB 21 IAW SRM 57-20-07RE ITEM 4.
- [SDR SIMA20200824002](https://openairdocs.org/sdr/SIMA20200824002), Aug 24, 2020: NUT PLATE. CORRODED. CARGO DOOR UPPER NUT PLATE HOLES HAVE CORROSION 5 EA. REMOVED AND REPLACED CARGO DOOR UPPER NUT PLATE PROFILE IAW SRM 51-40-02.
- [SDR SIMA20200824001](https://openairdocs.org/sdr/SIMA20200824001), Aug 24, 2020: WEB. CHAFED. CARGO DOOR LOWER FWD WEBBING CHAFED AT FASTENER. REPAIRED CARGO DOOR LOWER FWD WEBBING IAW SRM 52-30-01RE AND ETN-EM-52-043.
- [SDR SIMA202008242003](https://openairdocs.org/sdr/SIMA202008242003), Aug 22, 2020: NUT PLATE. CORRODED. CARGO DOOR LOWER NUT PLATE HOLES HAVE CORROSION 7 EA.-C/A-REMOVED AND REPLACED CARGO DOOR LOWER NUT PLATE PROFILE IAW EMB 145 SRM 51-40-02.
- [SDR SIMA202008210001](https://openairdocs.org/sdr/SIMA202008210001), Aug 20, 2020: YOKE. CRACKED. RH ENGINE FWD LOWER YOKE CRACKED. REMOVED AND REPLACED RH ENGINE FWD LOWER YOKE IAW ERS-EM-54MR-698.
- [SDR SIMA202008109002](https://openairdocs.org/sdr/SIMA202008109002), Aug 9, 2020: WIRE. DAMAGED. EMERGENCY LIGHT STRIP 8 HAS WIRE INSULATION PULLED OUT OF HOUSING ON BOTH WIRES. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA2020082104002](https://openairdocs.org/sdr/SIMA2020082104002), Aug 4, 2020: SKIN. DAMAGED. LEFT ELEVATOR TRAIL EDGE UPPER SKIN HAS HOLE. PERFORMED A REPAIR ON THE LT ELEVATOR TRAIL EDGE IAW ERS-EM-55MR-854.
- [SDR SIMA20200729004](https://openairdocs.org/sdr/SIMA20200729004), Jul 29, 2020: BATTERY PACK. INOPERATIVE. NR 4 EMERGENCY BATTERY INOP. C/A COMPLETE: R & R NR 4 EMERGENCY BATTERY AND BATTERY POWER SUPPLY, IAW EMB 145 AMM 33-50-04 ETN-EM-20-040 BONDING TEST GOOD. EMER
- [SDR SIMA20200729003](https://openairdocs.org/sdr/SIMA20200729003), Jul 29, 2020: LIGHT. CRACKED. LT EMERGENCY LIGHT STRIP PANELS AT POSITIONS 2, 3, 5, AND 8 ARE CRACKED/BROKEN. C/A COMPLETE: REMOVED AND REPLACED LT EMERGENCY LIGHT STRIP COVER PANELS AT POSI
- [SDR SIMA20200729002](https://openairdocs.org/sdr/SIMA20200729002), Jul 29, 2020: BATTERY PACK. NOT REPORTED. A3265 OPS A. REMOVE AND REPLACE EMERGENCY LIGHTING BATTERY ASSY/BATTERY CHARGER EMB WC 33-700-19 CRJ WC 33-002 ETN-EM-25-385 PN 2013-1A SN 10484 POS 3. C/A COMP
- [SDR SIMA202006291004](https://openairdocs.org/sdr/SIMA202006291004), Jun 21, 2020: OUTFLOW VALVE. FAILED. CABIN ALT REACHED 9600FT @ AT FL190 AFTER DESCENDING TO 10000FT CABIN SLOWLY REPRESSURIZED TO 400 FT (DELTA)P 4.4 NORMAL FOR THAT ALTITUDE-C/A-FOUND PNEUMATIC O
- [SDR SIMA202006198002](https://openairdocs.org/sdr/SIMA202006198002), Jun 18, 2020: SUPPORT. DAMAGED. SUPPLEMENTAL MAIN PAX ENTRY DOOR VERY HARD TO OPEN.-C/A-WHILE T/S HARD TO OPEN AND INSPECTION SUPPORT ASSY BOLTS IAW ETN-EM-52-052 FOUND DAMAGE TO THE BEARING S
- [SDR SIMA202006176001](https://openairdocs.org/sdr/SIMA202006176001), Jun 16, 2020: LOCK. LACK OF LUBE. FA REPORTS ENTRY DOOR IS EXTREMELY HARD TO UNLOCK + WILL UNLOCK HALFWAY THEN GOT STUCK. ONCE UNLOCKED IT IS HARD TO PUSH OPEN.-C/A-LUBRICATED PAX DOOR ROLLERS I
- [SDR SIMA202002110001](https://openairdocs.org/sdr/SIMA202002110001), Feb 10, 2020: DRIVE UNIT. DAMAGED. FLAP FAIL UPON ACCD ALT ON TAKEOFF-C/A-T/S FLAP FAIL MSG IAW FIM 27-51-00-810-801-A REMOVED AND REPLACED FPDU IAW EMB 145 AMM 27-53-04 NO FIX REMOVED AND REPLAC
- [SDR SIMA2020020411008](https://openairdocs.org/sdr/SIMA2020020411008), Nov 11, 2019: CHARGER. FAILED. GALLEY EMERGENCY LIGHTS NOT PASSING FUNCTIONAL CHECK-C/A-REMOVED AND REOLACED NUMBER 2 EMERGENCY BATTERY POWER SUPPLY ASSY IAW EMB AMM 33-50-04. EMERGENCY LIGHT
- [SDR SIMA202002061108](https://openairdocs.org/sdr/SIMA202002061108), Nov 10, 2019: WING. DAMAGED. WX-DMG / A/C LANDED SLID OFF RWY INTO TERRAIN. NO INJ TO CREW/PAX. ALL PAX TRANSPORTED TO TERMINAL BY BUS. EMERGENCY DECLARED.-C/A-PENDING CORRECTIVE ACTIONS. R
- [SDR SIMA2019100198011](https://openairdocs.org/sdr/SIMA2019100198011), Sep 28, 2019: LAMP. INOPERATIVE. ROW 17 AISLE EMERGENCY LIGHT INOPERATIVE. R & R ROW 17 AISLE EMERGENCY LIGHT LAMP IAW AMM 33-50-08. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.
- [SDR SIMA20190711003](https://openairdocs.org/sdr/SIMA20190711003), Jul 11, 2019: WARNING SYSTEM. FALSE ACTIVATION. BLD 2 LEAK WARNING MSG. C/A-PERFORMED INSPECTION AND LEAK CHECK OF BLEED 2 AIR SYSTEM AS PER AMM 36-11-09. WITH ENGINE RUNNING FOR 25 MINS. NO LEAKS OR FAULTS N
- [SDR SIMA20190320006](https://openairdocs.org/sdr/SIMA20190320006), Mar 20, 2019: LIGHT. INOPERATIVE. MAIN-DOOR EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED MAIN-DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A AND AMM 33-50-06-400-801-A. OPS CHECK GOOD. N
- [SDR SIMA20190205003](https://openairdocs.org/sdr/SIMA20190205003), Feb 5, 2019: LIGHT. INOPERATIVE. FWD CEILING EMERGENCY LIGHT INOP. R&R EMERGENCY LIGHT IAW AMM 33-50-08. OPC GOOD.
- [SDR SIMA20180930005](https://openairdocs.org/sdr/SIMA20180930005), Sep 30, 2018: HINGE FITTING. WORN. RIGHT AILERON OUTBOARD HINGE FITTING HAS A MIGRATING BUSHING. REMOVED AND REPLACED RT AILERON OB HINGE FITTING/BUSHING ASSY IAW EO EM-27MR-112.
- [SDR SIMA20180926001](https://openairdocs.org/sdr/SIMA20180926001), Sep 26, 2018: STRUCTURE. UNKNOWN. EM-52MR-236 PTB COCKPIT UNDERFLOOR ACCESS HATCH FRAME REPAIR-C/A-C/W EO# EM-52MR-236 PART B
- [SDR RAIA2018080620001](https://openairdocs.org/sdr/RAIA2018080620001), Aug 2, 2018: BRACKET. LOOSE. LDG AIR/GND FAILED, INSPECTED AND FOUND A LOOSE BRACKET HOLDING THE WOW SWITCH ON THE LT AFT LANDING GEAR, PERFORMED AN OPS CHECK OF ALL 5 WOW SWITCHES INDIVIDU
- [SDR RAIA201803310002](https://openairdocs.org/sdr/RAIA201803310002), Mar 31, 2018: WARNING MESSAGE. ILLUMINATED. NR 2 PACK OVERLOAD. R & R THE SLEEVE, OPS CHECKED GOOD.
- [SDR RAIA2018042610001](https://openairdocs.org/sdr/RAIA2018042610001), Mar 30, 2018: SHEAR TIE. CORRODED. FRAME 65 SHEAR TIE CORRODED ON THE LOWER END BY CARGO DOOR SILL. REPAIRED THE SHEAR TIE.
- [SDR RAIA201801310002](https://openairdocs.org/sdr/RAIA201801310002), Jan 31, 2018: CLAMP. LOOSE. BLEED 2 LEAK ON CLIMB OUT FOUND HIGH STAGE VLV CLAMP LOOSE AND TIGHTENED. FOUND BLEED VALVE NR 2 CLAMP LOOSE AND TIGHTENED. RAN THE LEAK CHECK AT 90%. NO LEAKS 
- [SDR RAIA201801300002](https://openairdocs.org/sdr/RAIA201801300002), Jan 30, 2018: SENSOR. LOOSE. NR 2 BLEED LEAK IN FLT, WHILE CLIMBING THROUGH 13,000 FEET. QRH PERFORMED, NO CHANGE. SECURED A LOOSE TEMP SENSOR ON THE DUCT FORWARD OF THE NR 2 PRE COOLER. OP
- [SDR RAIA201801280001](https://openairdocs.org/sdr/RAIA201801280001), Jan 28, 2018: O-RING. LEAKING. NR 2 BLEED LEAK WARNING IN FLIGHT. FOUND A BROKEN O-RING AT DUCT JOINT 14. R & R O-RING. OPS CHECKED GOOD.
- [SDR RAIA201801220001](https://openairdocs.org/sdr/RAIA201801220001), Jan 22, 2018: SMOKE DETECTOR. FALSE ACTIVATION. EICAS WARNING BAGG SMOKE DURING PUSH. BAGGAGE FIRE EXT BUTTON PRESSED. REMOVED AND REPLACED FWD CARGO BAY SMOKE DETECTOR. OPS CHECK GOOD.
- [SDR RAIA201801050002](https://openairdocs.org/sdr/RAIA201801050002), Jan 5, 2018: SKIN. GOUGED. SKIN REPAIR DOUBLER AT FRAME 75, STRINGER 2R GOUGED. REPAIRED THE SKIN DOUBLER.
- [SDR RAIA201712260003](https://openairdocs.org/sdr/RAIA201712260003), Dec 26, 2017: FRAME. CRACKED. FRAME 73 CRACKED JUST BELOW THE RT AFT FLOOR SILL. R & R THE FRAME LOWER SECTION.
- [SDR RAIA201712060002](https://openairdocs.org/sdr/RAIA201712060002), Dec 26, 2017: FRAME. CRACKED. FRAME 66 CRACKED AT STRINGER 16R. REPAIRED THE FRAME.
- [SDR RAIA201712260001](https://openairdocs.org/sdr/RAIA201712260001), Dec 26, 2017: SHEAR TIE. CORRODED. FRAME 65 SHEAR TIE CORRODED IN THE CARGO DOOR CUTOUT, LOWER CORNER. REPAIRED THE SHEAR TIE.

All 165: https://openairdocs.org/aircraft/N619AE/reports.md

## STCs that may be installed (OpenAirDocs) (75, 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-145LR)

- [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 ST02216AT-D](https://openairdocs.org/stc/ST02216AT-D): Installation of Teledyne Mini Flight Data Acquisition Unit in a Provisioned EMB-135/145. 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 ST01984LA-D](https://openairdocs.org/stc/ST01984LA-D): Modification and installation of passenger seats, passenger service units and filler panels, seat track covers, and seat row placards. 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 ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [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 ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST04213NY](https://openairdocs.org/stc/ST04213NY): PAX Social Distance Floorplan Reconfiguration. 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 SA9087SC-D](https://openairdocs.org/stc/SA9087SC-D): RECORE® Hamilton Sundstrand heat exchanger, P/N 816630-1 / -2 in accordance with Honeywell LORI Sealed Drawing List SDL3869-1 Rev. A, dated June 7, 2005 or later FAA approved revision. Honeywell International Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST01039DE](https://openairdocs.org/stc/ST01039DE): Passenger seating arrangement for 30 or less passengers. Deluxe Public Charter LLC
- [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 ST04423NY](https://openairdocs.org/stc/ST04423NY): Installation of ADS-B Out. FTI Engineering Nework GmbH
- [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 ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST04333NY](https://openairdocs.org/stc/ST04333NY): Installation of sat: Tglo® Photolumincsccnt Aisle Path Marking System. STG Aerospace Ltd
- [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 ST01702WI](https://openairdocs.org/stc/ST01702WI): Change seating configuration to 30 passengers by removal of seats. Worldwide Aircraft Engineering LLC
- [STC ST04108CH](https://openairdocs.org/stc/ST04108CH): Installation of Gogo Business Aviation ATG-8000 High Speed Internet with Wireless Local Area Network (WLAN). 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

All 75: https://openairdocs.org/aircraft/N619AE/stcs.md

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/aircraft.md
- The Allison AE3007C series engine: https://openairdocs.org/engine/allison-ae3007c-series.md

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