# N615AE: 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: 145087
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 30, 1998
- Certificate issued: September 16, 2011
- Expires: September 30, 2027
- Mode S code: A80156
- 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=615AE
- Page: https://openairdocs.org/aircraft/N615AE

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/N615AE/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 N615AE.

## 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 20021117035419I](https://openairdocs.org/incident/20021117035419I), Nov 17, 2002: Emb EMB145LR (N615AE), Fort Wayne, IN. (-23) American eagle flight #173 declared an emergency while in cruise flight at 10,000 ft. because of a bleed air leak on number one engine, aircraft was…

## Service difficulty reports (169, 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 SIMA20221013001](https://openairdocs.org/sdr/SIMA20221013001), Oct 13, 2022: NONE. NONE. AFT EMERGENCY FLASHLIGHT CRADLE WILL NOT CHARGE. MEL 25-32 AUTH# 100080M-C REF AML PG 4913838 ITEM 2-C/A-RAR AFT FA EMERGENCY FLASHLIGHT ASSY IAW EMB 145 AMM 33
- [SDR SIMA20220923002](https://openairdocs.org/sdr/SIMA20220923002), Sep 23, 2022: LAMP. INOPERATIVE. RH OVERWING 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. NO FIX. RAR OVERWING LIGHT ASSE
- [SDR SIMA20220921001](https://openairdocs.org/sdr/SIMA20220921001), Sep 21, 2022: NONE. MISSING. EMERGENCY FLASHLIGHT MISSING IN REAR CABIN.-C/A-REPLACED EMERGENCY FLASHLIGHT AS REQUIRED IAW STANDARD MTX PRACTICES.
- [SDR SIMA20220831003](https://openairdocs.org/sdr/SIMA20220831003), Aug 31, 2022: NONE. NONE. FOUND 2EA RIVETS PULLING THROUGH SKIN AT PREVIOUSLY DEFERRED DENT ON FUSELAGE AT FR 60-61 STR 17-18L. MAJOR REPAIR.-C/A-ACCOMPLISHED MAJOR REPAIR OF FUSELAGE SK
- [SDR SIMA20220711001](https://openairdocs.org/sdr/SIMA20220711001), Jul 11, 2022: LIGHT. INOPERATIVE. ROW 12 CEILING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LAMP AT AISLE 12 CEILING EMERGENCY LIGHT IAW AMM 33-50-08. OPERATIONAL CHECK GOOD IAW AMM 33-50-00.
- [SDR SIMA20220628001](https://openairdocs.org/sdr/SIMA20220628001), Jun 28, 2022: DOOR. DIRTY. FLIGHT ATTENDENT REPORTS DIFFICULTY OPENING AND CLOSING MAIN CABIN DOOR L1-C/A-CLEANED + LUBED MAIN DOOR ROLLERS AND OPC GOOD PER EMB AMM 52-18-00
- [SDR SIMA20220618002](https://openairdocs.org/sdr/SIMA20220618002), Jun 18, 2022: RUDDER BAR. INOPERATIVE. RUDDER SYS 1-2 INOP UPON TOUCHDOWN. LOST ALL STEERING IN RUDDER PEDALS."TRANSFERRED TO NRWC 615-ORD-04966"-C/A-RAR# 2 HYDRAULIC PRESSURE SWITCH IN RUDDER IAW EM
- [SDR SIMA20220429005](https://openairdocs.org/sdr/SIMA20220429005), Apr 29, 2022: NONE. UNSERVICEABLE. RA SHOWING 25 FEET UP TO 12K AGL, GOT TOO LOW , TERRAIM AURAL WARNING FOLLOWED BY NORMAL RA INDICATIONS REMAINDER OF FLIGHT,-C/A-REMOVED AND REPLACED R/A UNIT I
- [SDR SIMA20220218005](https://openairdocs.org/sdr/SIMA20220218005), Feb 18, 2022: NONE. NONE. MEL 2532 - AUTH# 020133M-C FLASHLIGHT/HOLDER AFT EMERGENCY CABIN FLASHLIGHT LOGPAGE:<4839880 ITEM:<1 .-C/A-RAR EMERGENCY FLASHLIGHT/HOLDER AFT CABIN FLASHLIGHT 
- [SDR SIMA20220212004](https://openairdocs.org/sdr/SIMA20220212004), Feb 12, 2022: NONE. NONE. AFT CABIN EMERGENCY FLASHLIGHT CRADLE BROKEN-C/A- "TRANSFERRED TO AML PAGE 4839880 ITEM 1"
- [SDR SIMA20220212003](https://openairdocs.org/sdr/SIMA20220212003), Feb 12, 2022: NONE. NONE. SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IN REFERENCE WITH EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.
- [SDR SIMA20211206001](https://openairdocs.org/sdr/SIMA20211206001), Dec 6, 2021: NONE. NONE. MEL 2532 - AUTH# 12-67M-C REPAIR REPAIR - POSITION AFT FA ATTENDANT EMERGENCY FLASHLIGHT/HOLDER AFT FA FLASHLIGHT BASE INOP PLACARDED -C/A-RAR F/A EMERGENCY FLA
- [SDR SIMA20210620001](https://openairdocs.org/sdr/SIMA20210620001), Jun 20, 2021: WARNING MESSAGE. ILLUMINATED. ABORTED TAKE OFF (HIGH SPEED) 90KTS DUE CGO DOOR WARNING -BAGGAGE DOOR INDICATION AFTER ADVANCING THRUST LEVERS. HIGH SPEED ABORT, VERIFIED NO BRAKE OVERHEAT MS
- [SDR SIMA20210520001](https://openairdocs.org/sdr/SIMA20210520001), May 20, 2021: CRADLE. BROKEN. FA AFT EMERGENCY FLASHLIGHT RETENTION CLAMP BROKEN AUTH#050285M-C REFERENCE LOG PAGE #4709038 ITEM #2 FOR DISCREPENCY-C/A-RAR FA AFT EMERGENCY FLASHLIGHT ASSEMB
- [SDR SIMA20210419001](https://openairdocs.org/sdr/SIMA20210419001), Apr 19, 2021: LAMP. INOPERATIVE. COCKPIT CEILING EMERGENCY LIGHT INOP-C/A-RAR COCKPIT CEILING EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-05. OPC GOOD
- [SDR SIMA20210415002](https://openairdocs.org/sdr/SIMA20210415002), Apr 15, 2021: BATTERY PACK. INOPERATIVE. EMERGENCY FLOOR STRIPS 2 AND 3 INOP-C/A-RAR #2 BATTERY POWER SUPPLY AND #2 BATTERY IAW ENVOY WC 33-700-19. OPC GOOD. END.
- [SDR SIMA20210415001](https://openairdocs.org/sdr/SIMA20210415001), Apr 15, 2021: LAMP. INOPERATIVE. MAIN DOOR EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.
- [SDR SIMA20210320003](https://openairdocs.org/sdr/SIMA20210320003), Mar 20, 2021: SKIN. CRACKED. COCKPIT UPPER SKIN CRACKED 2 CRACKS 1.5" IN LENGTH-C/A-INSTALLED DOUBLER/ TRIPLER PER ERS-EM-53MR-4302R
- [SDR SIMA20210208001](https://openairdocs.org/sdr/SIMA20210208001), Feb 8, 2021: LANDING GEAR. MALFUNCTIONED. LANDING GEAR AIR FAIL MESSAGE UNABLE TO RETRACT IN ICING CONDITION.MESSAGE EXTINGUISHED 30 MINS. AFTER ILLUMINATED. EMERGENCY DECLARED.. THIS AIRCRAFT HAS BEEN 
- [SDR SIMA202009076001](https://openairdocs.org/sdr/SIMA202009076001), Sep 6, 2020: LAMP. INOPERATIVE. EMERGENCY EXIT AISLE CEILING LIGHT INOPERABLE. C/A RAR EMERGENCY EXIT AISLE CEILING LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPERATIONS
- [SDR SIMA2020082019004](https://openairdocs.org/sdr/SIMA2020082019004), Aug 19, 2020: WARNING MESSAGE. FALSE ACTIVATION. DURING CLIMB AROUND FL 180 PERFORMED THE PNEUMATIC ICE TEST AND RECEIVED BLEED 1 FAIL. DID NOT DECLARE EMERGENCY. SWAP A/C CONT. PERFORMED OPERATIONAL TEST OF A
- [SDR SIMA202007221003](https://openairdocs.org/sdr/SIMA202007221003), Jul 21, 2020: DOOR FRAME. CORRODED. CARGO DOOR CUTOUT AT FR 65 CORRODED AROUND NUTPLATE BETWEEN STGR 13L-14L. PERFORMED PERMANENT REPAIR ON CARGO DOOR CUTOUT AT FR 65 BETWEEN STGR 13L-14L IAW ERS-
- [SDR SIMA202007165003](https://openairdocs.org/sdr/SIMA202007165003), Jul 15, 2020: SKIN. GOUGED. EXTERNAL FUSELAGE SKIN IS GOUGED BETWEEN FRAMES 74-75 AND STR 12L-13L. PERFORMED PERMANENT REPAIR ON LT FUSELAGE EXTERNAL SKIN BETWEEN FR 74-75 AND STR 12L-13L 
- [SDR SIMA202007154003](https://openairdocs.org/sdr/SIMA202007154003), Jul 14, 2020: SHEAR TIE. CORRODED. FUSELAGE BAGGAGE DOOR LATERAL L-SHAPE AT FR 65 BETWEEN STR 16L-17L CORRODED. REMOVED AND REPLACED FR 65 SHEAR CLIP IAW SRM 53-31-04. REPLACEMENT PART: SHEAR CLI
- [SDR SIMA202007154005](https://openairdocs.org/sdr/SIMA202007154005), Jul 14, 2020: FRAME. CORRODED. FUSELAGE BAGGAGE DOOR LATERAL L-SHAPE AT FR 68 BETWEEN STGR 16L-17L CORRODED. REPAIRED FRAME 68 BETWEEN STGR 16L-17L IAW SRM 53-31-04. PART REPLACED: SHEAR CLIP
- [SDR SIMA202007154004](https://openairdocs.org/sdr/SIMA202007154004), Jul 14, 2020: DOOR SILL. CORRODED. CARGO DOOR CUTOUT LOWER SILL CORRODED IN MULTIPLE AREAS. REMOVED AND REPLACED CARGO DOOR LOWER SILL IAW SRM 51-40-02. REPLACEMENT PART: SILL PN 145-25480-603SD.
- [SDR SIMA202007162004](https://openairdocs.org/sdr/SIMA202007162004), Jul 12, 2020: SKIN. CHAFED. FUSELAGE SKIN INSIDE RT PYLON ACCESS PANEL 424DB IS CHAFFED. REPAIRED FUSELAGE SKIN CHAFE INSIDE RT PYLON ACCESS PANEL 424DB IAW ERS-EM-53MR-4134 REV ORIGINAL.
- [SDR SIMA202007132002](https://openairdocs.org/sdr/SIMA202007132002), Jul 12, 2020: RIB. CRACKED. LT WING RIB 21 IS CRACKED. REPAIRED LT WING RIB 21 CRACK IAW SRM 57-20-07, ITEM 4 REPAIR TO CRACK IN RIB 21. REPLACEMENT PARTS: FILLER: AL CLAD 2024 T3, DOUBLER
- [SDR SIMA202007131005](https://openairdocs.org/sdr/SIMA202007131005), Jul 11, 2020: PROFILE. CORRODED. RT CABIN EMERGENCY EXIT LOWER EDGE FWD AND AFT PLASTIC GUIDE BLOCKS HAVE SURFACE CORROSION ON AND AROUND SHIMS. REMOVED AND REPLACED LOWER OUTER PROFILE ON RT E
- [SDR SIMA2020072753004](https://openairdocs.org/sdr/SIMA2020072753004), May 30, 2020: HOUSING. OUT OF LIMITS. LEFT AND RIGHT SPHERICAL BEARING HOUSINGS FOUND TO BE OUT OF LIMITS IAW SRM 55-30-02. REPAIRED THE SPHERICAL BEARING HOUSINGS IAW SRM 55-30-02.
- [SDR SIMA2020072753005](https://openairdocs.org/sdr/SIMA2020072753005), May 30, 2020: CONNECTOR. BROKEN. EMERGENCY LIGHT STRIP #2 HAS BROKEN CONNECTOR. R & R THE CONNECTOR IAW SWPM 20-21-00, AND 20-50-00.
- [SDR SIMA2020072753006](https://openairdocs.org/sdr/SIMA2020072753006), May 30, 2020: CONNECTOR. BROKEN. EMERGENCY LIGHT STRIP 3 HAS BROKEN CONNECTOR. R & R THE CONNECTOR IAW SWPM 20-21-00, AND 20-50-00.
- [SDR SIMA202002121001](https://openairdocs.org/sdr/SIMA202002121001), Feb 11, 2020: LIGHT. INOPERATIVE. GALLEY EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED GALLEY EMERGENCY LIGHT IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A OPC GOOD END
- [SDR SIMA202002065001](https://openairdocs.org/sdr/SIMA202002065001), Feb 5, 2020: ENGINE. FAILED. 10,00'',300KTS OVER CHICAGO. NUMBER 1 ENGINE NOISE,EICAS E1 SHUT DOWN,OIL QTY ENGINE 1 IN AMBER AND 4QTS,RAN EPC CHECLIST.SMOKE IN CABIN AND COCKPIT,CFD INSPECT
- [SDR SIMA202001064009](https://openairdocs.org/sdr/SIMA202001064009), Jan 4, 2020: LIGHT. INOPERATIVE. DURING PS-2 CHECK FOUND COURTESY LIGHT INOP AT GALLEY.-C/A-REMOVED AND REPLACED COURTESY LIGHT IAW EMB 145 AMM 33-26-05 OPS CHECK GOOD
- [SDR SIMA201912109004](https://openairdocs.org/sdr/SIMA201912109004), Dec 9, 2019: LAMP. INOPERATIVE. LH DOOR FWD EMERGENCY EXIT LIGHT INOP-C/A-RAR LH DOOR FWD EMERGENCY EXIT LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD.
- [SDR SIMA20190911005](https://openairdocs.org/sdr/SIMA20190911005), Sep 11, 2019: LIGHT. INOPERATIVE. DURING PS-1 CHK FOUND RT OVERWING EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHK GOOD.
- [SDR SIMA20190902003](https://openairdocs.org/sdr/SIMA20190902003), Sep 2, 2019: ACM. FAILED. PACK 1 OVERLOAD PACK 1 OVERHEAT HAPPENED ON GROUND THERE WAS A BURNING SMELL THAT WAS THERE FOR A SHORT TIME AT 2K FEET NO MESSAGES APPEARED. "TRANSFERRED TO NR
- [SDR SIMA201908265002](https://openairdocs.org/sdr/SIMA201908265002), Aug 25, 2019: WIRE. BROKEN. EMER. LIGHT WIRES BROKEN AT PANEL 251BF. SECURED WIRING CONNECTORS ON FLOOR PROXIMITY LIGHTS AT ROW 5/6 IAW AMM 33-50-12 OPS CHECK GOOD.
- [SDR SIMA201908064004](https://openairdocs.org/sdr/SIMA201908064004), Aug 4, 2019: SHUNT. FAILED. APU FAILED ON START ATTEMPT, DURING TAXI IN WITH BOTH ENG RUNNING. REPAIRED APU SHUNT MOUNT IAW ERS-EM-53MR-3849. OPS CHECKED GOOD.
- [SDR SIMA201908052002](https://openairdocs.org/sdr/SIMA201908052002), Aug 2, 2019: LAMP. INOPERATIVE. MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPAIRED MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A.
- [SDR SIMA201906110003](https://openairdocs.org/sdr/SIMA201906110003), Jun 10, 2019: LIGHT. INOPERATIVE. FLOOR PROX LIGHT STRIP BETWEEN SEAT 8 AND 9 INOP.-C/A-DEFERRED FLOOR PROX LGHT STRIP BETWEEN SEAT 8 AND 9. REMOVED AND REPLACED THE FLOOR PROX STRIP IAW EMB 145
- [SDR SIMA201906103006](https://openairdocs.org/sdr/SIMA201906103006), Jun 3, 2019: LINE. LEAKING. CABIN HAD FUMES OF STINKY SOCKS AFTER LANDING PEOPLE EXITED THE AIRCRAFT COUGHING-C/A- INSPECTED FOUND HYDRAULIC LEAK IN EMERGENCY PARKING BRAKE LINE BETWEEN FR
- [SDR SIMA20190508004](https://openairdocs.org/sdr/SIMA20190508004), May 8, 2019: NOT REPORTED. DAMAGED. RT SIDE RVSM CRITICAL AREA, 1" CREASE LEFT OF CENTER. "TRANSFERRED TO NRWC 615-ORD-02843". C/A- C/W ERS-EM-5300-3770. AC IS GOOD FOR RETURN TO SERVICE.
- [SDR SIMA201904220001](https://openairdocs.org/sdr/SIMA201904220001), Apr 20, 2019: FLASHLIGHT. INOPERATIVE. REAR FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED AFT CABIN EMERGENCY FLASH LIGHT IAW AMM 33-51-01. OPS CHECK GOOD.
- [SDR SIMA2019042219001](https://openairdocs.org/sdr/SIMA2019042219001), Apr 19, 2019: CONTROLLER. FAILED. AIRCRAFT BEGAN TO LOOSE PRESSURAZATION DURING CLIMB CABIN ALTITTUDE CONTINUED TO INCREASE UNTIL CLIMB STOPPED DESCENT BEGAN-C/A-DEFERRED AUTO AND MANUAL PRESSUR
- [SDR SIMA20190302001](https://openairdocs.org/sdr/SIMA20190302001), Mar 2, 2019: CONTROL UNIT. FAILED. MAIN PTRIM INOP WARNING MESSAGE AFTER T/O TRYING TO TRIM NOSE DOWN. C/A-INTERROGATED CMC FOUND CORRELATED HSCU FAILURE MSG. REMOVED AND REPLACED HSCU IAW AMM 27
- [SDR SIMA2018111305002](https://openairdocs.org/sdr/SIMA2018111305002), Nov 5, 2018: FITTING. EXCESS PLAY. LEFT HAND AILERON HAS PLAY AT PCA ATTACH POINT.-C/A-REMOVED AND REPLACED AILERON PCA/ACTUATOR FITTING IAW EO EM-27MR-112.
- [SDR RAIA201803040001](https://openairdocs.org/sdr/RAIA201803040001), Mar 4, 2018: BLANKING PLATE. LEAKING. LOSS OF PRESSURIZATION AT ABOUT 19000 FT. REINSTALLED CLAMP AND BLANKING PLATE FOR THE NR 2 CONDENSER MIXER. PERFORMED AN OPS CHECK OF PRESSURIZATION CONTROL SY
- [SDR RAIA201710310001](https://openairdocs.org/sdr/RAIA201710310001), Oct 31, 2017: DOOR SILL. CORRODED. SSI 53-30-07 CORROSION ON FRAMES AND SKIN AT LOWER FORWARD CARGO DOOR. R & R CARGO DOOR SILL AND SHEAR CLIP. SUPPORTING DOCUMENTS HAVE BEEN SENT TO 9-AMC-SDR-PR

All 169: https://openairdocs.org/aircraft/N615AE/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/N615AE/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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