# N616AE: 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 AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030)
- 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: 145092
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 21, 1998
- Certificate issued: October 4, 2011
- Expires: October 31, 2027
- Mode S code: A8050D
- 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=616AE
- Page: https://openairdocs.org/aircraft/N616AE

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): 104 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 AE-3007A)

- [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 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 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 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 2006-20-08](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 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 120: https://openairdocs.org/aircraft/N616AE/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 N616AE.

## 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 20030422017109I](https://openairdocs.org/incident/20030422017109I), Apr 22, 2003: Emb EMB145LR (N616AE), Syracuse, NY. (-23) On April 22, 2003, an Emb-145, N616AE, landed at Syracuse airport, Syracuse, NY on runway 28 after reporting a flap control problem inbound. The ARFF…

## Service difficulty reports (184, 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 SIMA20221025002](https://openairdocs.org/sdr/SIMA20221025002), Oct 25, 2022: CLAMP. UNSECURE. A/I BACK TO ORD DUE TO BLEED 1 LEAK DURING FLIGHT. EMERGENCY WAS DECLARED BUT WAS NOT OVERWEIGHT. FLT CHG EQP AND CONTINUED-C/A-PERFORMED VISUAL AND LEAK INSPEC
- [SDR SIMA20220717002](https://openairdocs.org/sdr/SIMA20220717002), Jul 17, 2022: FLASHLIGHT ASSY. BROKEN. FORWARD FLIGHT ATTENDANT FLASH LIGHT NOT CHARGING/HOLDER BROKEN-C/A-REMOVED AND REPLACED FORWARD FLIGHT ATTENDANT FLASH LIGHT ASSEMBLY IAW AMM 33-50-16. OPERATI
- [SDR SIMA20220519002](https://openairdocs.org/sdr/SIMA20220519002), May 19, 2022: NONE. NONE. E1 FIREDET FAIL IN CRUISE-C/A-PERFORMED OPERATIONAL CHECK OF E1 FIRE DET SYS OPERATION CHECK GOOD AS PER AMM 26-10-00 NO DEFECTS NOTED
- [SDR SIMA20220513003](https://openairdocs.org/sdr/SIMA20220513003), May 13, 2022: NONE. NONE. AFTER REACHING CRUISE " E1 FIRE DET FAIL" CAME ON FOR APPROX 5 MINS. ENG INDICATIONS NORMAL. NO OTHER MSGS. OR TURBULENCE.-C/A-INSP. AND FOUND FIRE LOOP HITTING
- [SDR SIMA20220323001](https://openairdocs.org/sdr/SIMA20220323001), Mar 23, 2022: NONE. NONE. E1 FIREDET FAIL CAME ON AND OFF 3 TIMES DURING FLIGHT. ALL OTHER INDICATIONS WERE NORMAL. "TRANSFERRED TO NRWC 616-DFW-04848"-C/A-RAR ENG1 FIRE DETECTOR SENSING
- [SDR SIMA20220318001](https://openairdocs.org/sdr/SIMA20220318001), Mar 18, 2022: NONE. NONE. AFT EMERGENCY FLASHLIGHT INOP MEL 2532 - AUTH# 03-253M-C-C/A-RAR AFT FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPC GOOD. MEL RE
- [SDR SIMA20220318002](https://openairdocs.org/sdr/SIMA20220318002), Mar 18, 2022: NONE. NONE. SERVICE DOOR EMERGENCY LIGHT INOP AND FOUND 2 BROKEN WIRES ON SERVICE DOOR EMERGENCY LIGHT-C/A-RAR SPLICES SP7377 AND SP7376 IAW SWPM-2430 20-21-00. OPS CHECK G
- [SDR SIMA20220315001](https://openairdocs.org/sdr/SIMA20220315001), Mar 15, 2022: FLASHLIGHT. INOPERATIVE. AFT EMERGENCY FLASHLIGHT INOP-C/A-FLIGHT CREW PLACARDED AFT EMERGENCY FLASHLIGHT M PROCEDURES C/W MEL 25-32 AUTH 030253M-C MOC 607038
- [SDR SIMA20220217001](https://openairdocs.org/sdr/SIMA20220217001), Feb 17, 2022: NONE. NONE. FLIGHT ATTENDANT FORWARD EMEERGENCY FLASHLIGHT INOP-C/A-REPLACED FWD FA EMERGENCY FLASHLIGHT OPS CHECK GOOD PE 25-60-11
- [SDR SIMA20220124002](https://openairdocs.org/sdr/SIMA20220124002), Jan 24, 2022: NONE. NONE. EMERGENCY LIGHT ON SERVICE DOOR NOT ILLUMINATING AND WIRE BROKE OFF AT BULB.-C/A-REMOVED AND REPLACED SERVICE DOOR EXTERNAL EMERGENCY LIGHT ASSY IAW EMB 145 AMM
- [SDR SIMA20211119002](https://openairdocs.org/sdr/SIMA20211119002), Nov 19, 2021: NONE. NONE. FWD FA EMERGENCYFLASHLIGHT IS MISSING-C/A-RAR FWD FA EMERGENCY FLASHLIGHT. IAW E145 AMM 33-50-16
- [SDR SIMA20211103003](https://openairdocs.org/sdr/SIMA20211103003), Nov 3, 2021: NONE. NONE. AFT EMERGENCY FLASHLIGHT MISSING MEL 25-32. AUTH #110026M-C. REF LOG PG 4676473/1.-C/A-RAR AFT EMEREGENCY FLASHLIGHT ASSY ON TOILET FWD PARTITION, BEHIND LAST D
- [SDR SIMA20210416003](https://openairdocs.org/sdr/SIMA20210416003), Apr 16, 2021: WARNING MESSAGE. FALSE ACTIVATION. BLEED 1 LEAK EICAS MSG IN AIR. HAPPENED AFTER OR DIRECTLY AFTER ENTERING ICING DID NOT DECLARE EMERGENCY-C/A-PERFORMED DUCT LINE INSPECTION AND CHECK IAW EMB 14
- [SDR SIMA20210226002](https://openairdocs.org/sdr/SIMA20210226002), Feb 26, 2021: FLASHLIGHT. MISSING. REAR CABIN EMERGENCY FLASHLIGHT MISSING-C/A-REPLACED CABIN CABIN FLASHLIGHT IAW ETN-EM-33-034 OPC GOOD NO FUTHER DEFECTS NOTED
- [SDR SIMA20210221003](https://openairdocs.org/sdr/SIMA20210221003), Feb 21, 2021: BATTERY PACK. INOPERATIVE. LEFT FWD WING TO FUSELAGE FAIRING EMERGENCY LIGHT INOPERATIVE. C/A-REMOVED AND REPLACED NR 1 EMERGENCY BATTERY AND NR 1 EMERGENCY CHARGER ASSY IAW WORK CARD 33-
- [SDR SIMA20210106001](https://openairdocs.org/sdr/SIMA20210106001), Jan 6, 2021: LAMP. INOPERATIVE. RT OVERWING EMERGENCY LIGHT INOPERABLE. C/A: R & R RT OVERWING EMERGENCY LIGHT LAMP, IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPERATIONS CHECK GOO
- [SDR SIMA20200825001](https://openairdocs.org/sdr/SIMA20200825001), Aug 25, 2020: ROLLER. LACK OF LUBE. MAIN CABIN DOOR WOULDN'T OPEN FROM THE INSIDE.-C/A-LUB. THE MAIN DOOR FRAME ROLLERS AS REQUIRED.OPS. CHECK GOOD.NO DEFECTS NOTED AT THIS TIME.
- [SDR SIMA202005197008](https://openairdocs.org/sdr/SIMA202005197008), May 17, 2020: DOOR FRAME. CORRODED. CARGO DOOR FWD SIDE EDGE NUTPLATE HOLE CORRODED OUT OF LIMITS-C/A-REPAIRED CARGO DOOR FWD FRAME CENTER HOLE IAW EMB 145 SRM 52-30-04RE
- [SDR SIMA202005187004](https://openairdocs.org/sdr/SIMA202005187004), May 17, 2020: DOOR SILL. CORRODED. SERVICE DOOR LOWER CENTER FLOOR SILL CORRODED-C/A-REPAIRED MIDDLE AND FWD NUTPLATE HOLES OF SERVICE DOOR CENTER SILL, IAW EMB 145 SRM 53-21-02.
- [SDR SIMA202005187003](https://openairdocs.org/sdr/SIMA202005187003), May 17, 2020: DOOR FRAME. CORRODED. CARGO DOOR LWR SIDE EDGE 4 NUTPLATE HOLES CORRODED-C/A-REMOVED AND REPLACED CARGO DOOR LWR INBD FRAME IAW EMB 145 SRM 51-40-02
- [SDR SIMA202005187007](https://openairdocs.org/sdr/SIMA202005187007), May 17, 2020: DOOR FRAME. GOUGED. CARGO DOOR LWR OTBD FRAME FWD CORNER GOUGED-C/A-REMOVED AND REPLACED CARGO DOOR OTBD FRAME IAW EMB 145 SRM 51-40-02
- [SDR SIMA202005187006](https://openairdocs.org/sdr/SIMA202005187006), May 17, 2020: PROFILE. BENT. CARGO DOOR LOWER PROFILE IS BENT NEAR FORWARD ROLLER-C/A-REMOVED AND REPLACED CARGO DOOR LOWER PROFILE IAW EMB 145 SRM 51-40-02
- [SDR SIMA202005187005](https://openairdocs.org/sdr/SIMA202005187005), May 17, 2020: FRAME. DENTED. FRAME 72 BETWEEN STRINGERS 15R AND 17R HAS A DENT-C/A-REMOVED AND REPLACED FRAME 72 IAW EMB 145 SRM 51-40-02
- [SDR SIMA202001221004](https://openairdocs.org/sdr/SIMA202001221004), Jan 21, 2020: CONNECTOR. DIRTY. MAIN DOOR EMERGENCY LIGHT INOP"TRANSFERRED TO NRWC 616-ORD-03398"-C/A-DEFERRED PER MEL 33-29. CLEANED MAIN DOOR EMERGENCY LIGHT ASSY ELECTRICAL CONNECTIONS IAW 
- [SDR SIMA201911086001](https://openairdocs.org/sdr/SIMA201911086001), Nov 6, 2019: LAMP. INOPERATIVE. ROW 12 B/C OVERHEAD EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED 12 B/C OVERHEAD EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-07-04. OPS CHECK GOOD.
- [SDR SIMA201910076001](https://openairdocs.org/sdr/SIMA201910076001), Oct 6, 2019: SMOKE DETECTOR. FALSE ACTIVATION. ON TAXI RECIEVED BAGG SMOKE INDICATION. REMOVED AND REPLACED FWD CARGO SMOKE DETECTOR IAW AMM 26-15-01 OPC GOOD
- [SDR SIMA201908231007](https://openairdocs.org/sdr/SIMA201908231007), Aug 21, 2019: ENGINE. FAILED. POSSIBLE APU FIRE, SMOKE COMING FROM APU INTAKE. REMOVED AND REPLACED APU IAW W/C 49-800-05. OPS CHECK GOOD LEAK CHECK GOOD.
- [SDR SIMA20190709003](https://openairdocs.org/sdr/SIMA20190709003), Jul 9, 2019: CONTROL VALVE. FAILED. ON FINAL APPROCH WHEN LANDING REAR EXTENDED BRAKE DEGRADED MASTER CAUTION INDICATION APPEARED DID GO AROUND CAUTION DISAPPEARED WHEN LANDING GEAR RETRACTED + RE
- [SDR SIMA20190524002](https://openairdocs.org/sdr/SIMA20190524002), May 24, 2019: VALVE. FAILED. PAC 1 VALVE FAIL IN FLIGHT; PAC 1 & 2 OVLD IN FLIGHT; BURNING SMELL IN COCKPIT. SMELLED LIKE BURNT PLASTIC. NO COMPLAINTS OF BURNING SMELL IN CABIN. NO SMOKE OB
- [SDR SIMA20190517002](https://openairdocs.org/sdr/SIMA20190517002), May 17, 2019: CRADLE. BROKEN. AFT CABIN FLASHLIGHT CRADLE BROKEN. C/A-REMOVED AND REPLACED AFT FLASHLIGHT CRADLE IAW AMM TASK 33-50-16-000-801-A AND 33-50-16-400-801-A.
- [SDR SIMA20190512002](https://openairdocs.org/sdr/SIMA20190512002), May 12, 2019: LIGHT. INOPERATIVE. FLOOR EMERGENCY LIGHT STRIP AT ROWS 6A/7A INOP. C/A-REMOVED AND REPLACED EMERGENCY LIGHT STRIP IAW AMM 33-50-12 OPS TEST GOOD.
- [SDR SIMA20190503001](https://openairdocs.org/sdr/SIMA20190503001), May 3, 2019: BATTERY. DISCHARGED. DURING PS-2 FOUND LH EXT EMERGENCY LIGHT BURNED OUT. C/A-REMOVED AND REPLACED LT FWD EXT EMERGENCY LIGHT ASSY IAW 33-50-10. EMERGENCY LIGHTS OPS CHECK GOOD IAW 
- [SDR SIMA20181106004](https://openairdocs.org/sdr/SIMA20181106004), Nov 6, 2018: CONNECTOR. MISSING. THE EMERGENCY LIGHT STRIP CONNECTOR THAT CONNECTS TO THE EMERGENCY LIGHT STRIP AT FLOOR PANEL 251BF HAS MISSING CONNECTOR. INSTALLED SERVICEABLE CONNECTOR ON EM
- [SDR RAIA20180829004](https://openairdocs.org/sdr/RAIA20180829004), Aug 23, 2018: FUSE. BLOWN. NR 1 EMERGENGY LIGHT BATTERY HAD LOW VOLTAGE. R & R THE BATTERY, OPS CHECKED GOOD. THE BATTERY HAD A BLOWN FUSE.
- [SDR RAIA201802010001](https://openairdocs.org/sdr/RAIA201802010001), Feb 1, 2018: VALVE. DEFECTIVE. A/C WOULD NOT PRESSURIZE AFTER TAKE OFF. R & R GROUND CONNECTION VALVE. PERFORMED OPS CHK OF PRESSURIZATION OPS CHECK GOOD.
- [SDR RAIA201801310001](https://openairdocs.org/sdr/RAIA201801310001), Jan 31, 2018: VALVE. DEFECTIVE. UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKE OFF. R&R GROUND CONNECTION VALVE PERFORMED OPS CHECK OF PRESSURIZATION, OPS CHECK GOOD.
- [SDR RAIA201801220002](https://openairdocs.org/sdr/RAIA201801220002), Jan 22, 2018: WINDSHIELD. CRACKED. F/O WINDSHIELD OUTER PLY SHATTERED. R & R F/O WINDSHIELD OPS CHECK GOOD.
- [SDR RAIA201711190001](https://openairdocs.org/sdr/RAIA201711190001), Nov 19, 2017: CONNECTOR. DIRTY. UNCOMMANDED STEERING SWERVED ON GROUND. REMOVED AND CLEANED FEEDBBACK POT CONNECTOR. RECONNECTED AND HAD CREW PERFORM TAXI OPS CHECK OF STEERING. NO DEFECT NOTE
- [SDR RAIA201711110002](https://openairdocs.org/sdr/RAIA201711110002), Nov 11, 2017: SKIN. CRACKED. RIGHT FUSELAGE EXTERIOR SKIN AT FR 75 HAS 3 POSSIBLE CRACKS - MARKED. PERFORMED REPAIR ON RH FUSELAGE EXTERIOR SKIN AT FR 75.
- [SDR RAIA201605240001](https://openairdocs.org/sdr/RAIA201605240001), May 24, 2016: LINE. FAILED. ON TAKEOFF, RECEIVED A LANDING GEAR DISAGREE MESSAGE AND HYD SYS 1 FAIL AND HYDRAULIC SYS 1 LOW QTY. INSPECTED AND FOUND LT MLG ACTUATOR HYDRAULIC LINE FAILED. 
- [SDR RAIA201605090001](https://openairdocs.org/sdr/RAIA201605090001), May 9, 2016: BUTTON. INOPERATIVE. THRUST RATING PANEL CLIMB BUTTON WOULD NOT ENGAGE. R & R THRUST RATING PBA. OPS CHECK GOOD.
- [SDR RAIA201506250003](https://openairdocs.org/sdr/RAIA201506250003), Jun 25, 2015: LIGHT. INOPERATIVE. SERVICE DOOR, NR 2 SHROUDED EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT, OPS CHECKED GOOD.
- [SDR RAIA201506250002](https://openairdocs.org/sdr/RAIA201506250002), Jun 25, 2015: LIGHT. INOPERATIVE. COCKPIT STEP EXIT IDENTIFIER LIGHT NR 9 DOES NOT ILLUMINATE. MAINTENANCE REPLACED LIGHT, OPS CHECKED GOOD.
- [SDR RAIA201506250001](https://openairdocs.org/sdr/RAIA201506250001), Jun 25, 2015: LIGHT. OUT OF POSITION. MAIN DOOR EMERGENCY FLOOD LIGHT NR 13 SWITCHED WITH COURTESY LIGHT. MAINTENANCE SWITCHED LIGHTS TO THE CORRECT POSITION, OPS CHECK GOOD.
- [SDR SIMA20150519008](https://openairdocs.org/sdr/SIMA20150519008), May 19, 2015: BATTERY. DISCHARGED. FLOOR PROXIMITY EMER EXIT LIGHTS FROM EMER EXIT ROW TO THE FRONT DO NOT ILLUMINATE. OPERATED APU TO CHARGE EMER BATTERIES. TURNED ON EMER LIGHTS. PERFORMED OPER
- [SDR SIMA20150519006](https://openairdocs.org/sdr/SIMA20150519006), May 19, 2015: WARNING SYSTEM. FALSE ACTIVATION. FLAP LOW SPEED ADVISORY APPEARED ON EICAS DURING CLIMB OUT. REINSTALLED FLAP DRIVE MOTORS IN ORIGINAL LOCATIONS IAW AMM 27-53-01. PERFORMED TAKEOFF FLAPS OPERAT
- [SDR SIMA20150510001](https://openairdocs.org/sdr/SIMA20150510001), May 10, 2015: DOUBLER. CORRODED. LOWER RT PARTITION DOUBLER ON FRAME 61 IS CORRODED BEYOND LIMITS. COMPLETED REPAIR TO RT PARTITION DOUBLER ON FRAME 61 IAW ERS-EM-53MR-1291.
- [SDR SIMA20150503002](https://openairdocs.org/sdr/SIMA20150503002), May 3, 2015: BEARING. DISLODGED. RUDDER 1 LOWER CONTROL ROD BEARING ON VERTICAL STAB RETAINER RING IS DISLODGED. R & R RUDDER 1 LOWER HINGE FITTING ASSEMBLY IAW SRM 51-40-02.
- [SDR SIMA20150503003](https://openairdocs.org/sdr/SIMA20150503003), May 3, 2015: HINGE. RATCHETING. RUDDER 1 UPPER CONTROL ROD. BEARING ON VERTICAL STAB IS RACHETING. R & R RUDDER 1 UPPER CTR HINGE FITTING ASSEMBLY IAW SRM 51-40-02.
- [SDR SIMA20150503001](https://openairdocs.org/sdr/SIMA20150503001), May 3, 2015: HINGE. DAMAGED. VERTICAL STAB TO RUDDER 1 LOWER HINGE SHACKLE HAS PLAY. INSTALLED NEW HINGE FITTING ASSEMBLY IAW SRM 51-40-02 & ERS-EM-5500-287.

All 184: https://openairdocs.org/aircraft/N616AE/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/N616AE/stcs.md

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/aircraft.md
- The Allison AE-3007A engine: https://openairdocs.org/engine/allison-ae-3007a.md

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