# N617AE: 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: 145093
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 27, 1998
- Certificate issued: September 26, 2011
- Expires: September 30, 2027
- Mode S code: A808C4
- 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=617AE
- Page: https://openairdocs.org/aircraft/N617AE

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/N617AE/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 N617AE.

## FAA accident and incident reports

None matched to N617AE.

## Service difficulty reports (197, 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 HNAA2022082500249](https://openairdocs.org/sdr/HNAA2022082500249), Aug 24, 2022: BOLT. SHEARED. ON T/O ROLL, ENG REF A/I DISAGREE DISPLAYED. MESSAGE REMAINED ON TAXI IN ALONG WITH E2 A/I VLV FAIL DISPLAYED ON TAXI. DURING E2 A/I VLV DEACTIVATION LOCKING BO
- [SDR HNAA2022081500248](https://openairdocs.org/sdr/HNAA2022081500248), Aug 11, 2022: PROXIMITY SENSOR. MALFUNCTIONED. AFTER ROTATION NLG WILL NOT RETRACT LG LEVER DISAGREE MESSAGE DISPLAYED ON EICAS ... CMC DISPLAYS 2 OCC OF LG UP/DN PROX SW/LGUE FAIL & LG NOSE UP PROX SW FAIL.
- [SDR HNAA2022041900166](https://openairdocs.org/sdr/HNAA2022041900166), Apr 18, 2022: PROXIMITY SWITCH. FAILED. AFTER GEAR RETRACTION LOUD NOISE HEARD FROM NOSE BAY AREA. C/W QRH SPEED BELOW 250 KNOTS. GEAR INDICATED UP AS NORMAL. HYD PRESSURE NORMAL. TROUBLESHOOTING, R &
- [SDR HNAA2021081900387](https://openairdocs.org/sdr/HNAA2021081900387), Aug 18, 2021: BLEED VALVE. FAULTED. BLD 1 VALVE CLOSED MSG IN FLT AND WOULD NOT CLEAR UNTIL STARTED APPROACH. R & R BLD 1 VLV REGULATOR IAW AMM 36-11-05.NO FIX. CONTINUE T/S. R/R PANEL ASSY AIR CO
- [SDR HNAA2021061400261](https://openairdocs.org/sdr/HNAA2021061400261), Jun 13, 2021: SOLENOID VALVE. FAULTED. LOUD AIR NOISE AND VIBERATION FROM NLG AREA AFTER RETRATION OF GEAR. R&R NLG DOOR SOLENOID VALVE REF 32-33-02. LEAKS AND OP CKS GOOD OK FOR SERVICE.
- [SDR HNAA2021010500005](https://openairdocs.org/sdr/HNAA2021010500005), Jan 4, 2021: CLAMP. LOOSE. ICE CONDDITION. A/I INOPERABLE AND WING A/I FAIL MESSAGES ON EICAS WITH WING 1 AND 2 VALVE FAIL AND WING 2 A/I LEAK MESSAGES ON CMC. FOUND SERVERAL LOOSE CLAMPS
- [SDR HNAA2020090100250](https://openairdocs.org/sdr/HNAA2020090100250), Aug 31, 2020: CONNECTOR. DAMAGED. AFTER TAKEOFF, GEAR LEVER SELECTED UP, LANDING GEAR STAYED DOWN WITH AMBER INDICATIONS. CREW C/W ARH LANDING GEAR STAYED DOWN. TROUBLESHOT IAW AMM 32-32-00-700-
- [SDR HNAA2020072700233](https://openairdocs.org/sdr/HNAA2020072700233), Jul 24, 2020: UNKNOWN. ODOR. DURING TAKE OFF, AT 100KTS, A BURNING SMELL IN COCKPIT WAS NOTICED BY FO AND CAPT. REJECTED TAKE OFF. WITHIN 5 SECONDS BURNING SMELL DISSIPITATED. INSPECTED AND
- [SDR HNAA2020052310156](https://openairdocs.org/sdr/HNAA2020052310156), May 21, 2020: WARNING SYSTEM. MALFUNCTIONED. NO TAKE OFF CONFIG WARNING ON TAKE OFF. RERACKED AWU IAW AMM 31-51-01-04. OPS CHK GOOD. OKAY FOR SERVICE.
- [SDR HNAA2020052210155](https://openairdocs.org/sdr/HNAA2020052210155), May 21, 2020: PRESSURE SWITCH. FAILED. NO TAKE OFF CONFIG WARNING ON TAKEOFF. RNR PARK BRAKE PRESS SW IAW AMM 32-44-07-04. OPS CHECK GOOD OKAY FOR SERVICE.
- [SDR HNAA2020052310154](https://openairdocs.org/sdr/HNAA2020052310154), May 21, 2020: PRESSURE SWITCH. FAILED. PARKING BRAKE ON LIGHT PRESENTED INFLIGHT AND WILL NOT EXTINGUISH. RNR PARK BRAKE PRESS SWITCH IAW AMM 32-44-07-04. OPS CHECK GOOD OKAY FOR SERVICE.
- [SDR HNAA2020051800150](https://openairdocs.org/sdr/HNAA2020051800150), May 13, 2020: INVERTER. INOPERATIVE. L/H EMERGENCY DOOR MAIN EXIT LIGHT INOP (EXIT IDENT SIGN). REMOVED AND REPLACED EXIT IDENT SIGN IAW AMM 33-50-13. NO FIX TROUBLE SHOOT PER FAULT ISOLATION MANUA
- [SDR HNAA2019122700393](https://openairdocs.org/sdr/HNAA2019122700393), Nov 30, 2019: NUT PLATE. CORRODED. CORRODED NUTPLATE HOLES ON CARGO CUTOUT STRUCTURE LOWER CENTER SILL. R & R THE CARGO DOOR SILL IAW SRM 51-40-02.
- [SDR HNAA20191227001](https://openairdocs.org/sdr/HNAA20191227001), Nov 29, 2019: YOKE. CRACKED. LEFT ENGINE FWD LOWER YOKE HAS CRACK ON FWD LOWER CORNER. R & R LH FWD YOKE FITTING AND GUSSET PLATE IAW EO1-71-19-0565.
- [SDR HNAA2019122700395](https://openairdocs.org/sdr/HNAA2019122700395), Nov 27, 2019: PROFILE. CORRODED. CARGO DOOR LOWER I/B PROFILE CORRODED AROUND NUTPLATES....FIX:R&RD CARGO DOOR LWR INBD PROFILE IAW EMB145 SRM 51-40-02
- [SDR HNAA2019122700392](https://openairdocs.org/sdr/HNAA2019122700392), Nov 27, 2019: NUT PLATE. CORRODED. CARGO DOOR WEB HAS 2 AREAS AROUND NUTPLATES CORRODED. REPAIRED IAW EMB SRM 52-30-01RE AND EO1-52-19-0557
- [SDR HNAA2019122700397](https://openairdocs.org/sdr/HNAA2019122700397), Nov 26, 2019: SKIN. CRACKED. CARGO DOOR SKIN WAS CRACKED AT THE AFT END OF THE HANDLE. INSTALLED A REPAIR DOUBLER AND FILLER IAW EO1-52-19-0555.
- [SDR HNAA2019122700396](https://openairdocs.org/sdr/HNAA2019122700396), Nov 25, 2019: SKIN. GOUGED. LH WING LEADING EDGE NR 1 EXTERIOR HAD ONE GOUGE. FABRICATED AND INSTALLED A REPAIR IAW SRM 51-20-01, AND EO1-57-19-0566.
- [SDR HNAA2019111100351](https://openairdocs.org/sdr/HNAA2019111100351), Nov 10, 2019: WARNING MESSAGE. FALSE ACTIVATION. PDIS 617 27-41 2119051 10NOV19 PHL CLOSE MAIN PITCH TRIM INOP MSG DURING FLIGHT. FACT 10NOV19 16:43 PHL T/S IN REF TO FIM TASK 27-43-00, ELECTRICAL CHECKS G OOD
- [SDR HNAA2018120500303](https://openairdocs.org/sdr/HNAA2018120500303), Nov 29, 2018: DISPLAY. MALFUNCTIONED. DIS 617 34-28 1723962 29NOV18 MHT CLOSE SITTING AT GATE WITH ELECTRICAL POWER ON. EICAS SHUT DOWN FOLLOWED BY ELECTRICAL FUMES SMELT IN COCKPIT. NO C/BS POPPED.
- [SDR HNAA2018062600128](https://openairdocs.org/sdr/HNAA2018062600128), Jun 23, 2018: SIGN. INOPERATIVE. EMERGENCY SIGN INOPERATIVE BY SEAT 12A. R & R EMERGENCY SIGN. OPS CHECKED GOOD.
- [SDR HNAA2018032600069](https://openairdocs.org/sdr/HNAA2018032600069), Mar 24, 2018: A/C PACK. SEIZED. DURING PUSHBACK STRONG RUBBER BURNING ODOR GENERATED, ODOR STOPPED ONCE PUSHBACK WAS COMPLETE. MX INSPECTED AND FOUND NR 1 PACK SEIZED. R &R THE NR 1 ACM IAW AM
- [SDR HNAA2018032100064](https://openairdocs.org/sdr/HNAA2018032100064), Mar 19, 2018: DUCT. DETACHED. WITH BOTH PACKS RUNNING ON APU, THE NR 2 PACK WAS SELECTED OFF AND NR 1 PACK MADE AN ABNORMAL NOISE, THE FLT DECK FILLED WITH SMOKE AND ODOR. INSPECTED, NO FUME
- [SDR HNAA2017092500328](https://openairdocs.org/sdr/HNAA2017092500328), Sep 20, 2017: LIGHT. INOPERATIVE. RIGHT EMERGENCY DOOR UPPER EXIT LIGHT IS INOPERATIVE. R & R THE LIGHT IAW AMM 33-50-14-000/400-801-A. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR HNAA2017073100257](https://openairdocs.org/sdr/HNAA2017073100257), Jul 31, 2017: RELAY. DAMAGED. DURING INSPECTION OF RELAY K0058 & RELAY BASE XK0058, SAID RELAY AND BASE FAIL STEP-11IN FCD1-30-165-0276. FOUND DAMAGE AND BURNED PINS ON PITOT STATIC NR 3. BO
- [SDR SIMA20170615015](https://openairdocs.org/sdr/SIMA20170615015), Jun 15, 2017: WIRE. BROKEN. LEFT NR 6 EMERGENCY LIGHT STRIP HAS BROKEN WIRES. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-12.
- [SDR SIMA20170615010](https://openairdocs.org/sdr/SIMA20170615010), Jun 15, 2017: HOLDER. CRACKED. NR 1 LT FLOOR EMERGENCY LIGHT STRIP HOLDER CRACKED. REMOVED AND REPLACED THE EMERGENCY LIGHT HOLDER IAW AMM 33-50-12.
- [SDR SIMA20170615016](https://openairdocs.org/sdr/SIMA20170615016), Jun 15, 2017: LIGHT. CRACKED. NR 1 RT EMERGENCY LIGHT STRIP CRACKED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20170615011](https://openairdocs.org/sdr/SIMA20170615011), Jun 15, 2017: LIGHT. CRACKED. LEFT NR 6 PROXIMITY LIGHT EXTRUSION CRACKED. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-12.
- [SDR SIMA20170615014](https://openairdocs.org/sdr/SIMA20170615014), Jun 15, 2017: HOLDER. CRACKED. NR 2 LT FLOOR LIGHT STRIP HOLDER CRACKED. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT HOLDER IAW AMM 33-50-12.
- [SDR SIMA20170615013](https://openairdocs.org/sdr/SIMA20170615013), Jun 15, 2017: SKIN. BENT. RIGHT EMERGENCY EXIT EXTERNAL SKIN UPPER EDGE BENT. CONTOURED BENDED IAW SRM 51-10-08.
- [SDR SIMA20170615012](https://openairdocs.org/sdr/SIMA20170615012), Jun 15, 2017: STIFFENER. CRACKED. FOUND APU COWLING PROFILE 17D CRACKED APPROX 28 INCHES FROM FWD EDGE. COMPLETE:REPAIRED THE APU COWLING INTERNAL STIFFENER IAW SRM 53-32-17.
- [SDR SIMA20170615009](https://openairdocs.org/sdr/SIMA20170615009), Jun 15, 2017: BRACKET. CORRODED. CORROSION ON RT EMERGENCY ESCAPE HATCH INTERNAL LOWER BRACKET. REMOVED AND REPLACED RT EMERGENCY EXIT LOWER BRACKET IAW SRM 51-40-02.
- [SDR SIMA20170615008](https://openairdocs.org/sdr/SIMA20170615008), Jun 15, 2017: BRACKET. CRACKED. BRACKET IS CRACKED ON INTERNAL FUSELAGE AT FRAME 20 STRINGERS 3L. REMOVED AND REPLACED BRACKET ON INTERNAL FUSELAGE AT FRAME 20 STRINGERS 3L IAW SRM 51-40-02.
- [SDR SIMA20170615007](https://openairdocs.org/sdr/SIMA20170615007), Jun 15, 2017: DOOR SILL. CORRODED. CARGO DOOR CENTER SILL IS CORRODED ON FWD END. REMOVED AND REPLACED CARGO DOOR CENTER SILL WITH NEW SERVICEABLE SILL IAW SRM 51-40-02.
- [SDR SIMA20170615006](https://openairdocs.org/sdr/SIMA20170615006), Jun 15, 2017: CONNECTOR. DISCONNECTED. EMERGENCY EXIT LIGHT IN 233ALC IS INOP. UPON FURTHER INVESTIGATION FOUND ELECTRICAL CONNECTOR ABOVE MAIN DOOR REGION CEILING PANEL DISCONNECTED. RECONNECTED ELE
- [SDR SIMA20170615005](https://openairdocs.org/sdr/SIMA20170615005), Jun 15, 2017: CONNECTOR. DISCONNECTED. LT COCKPIT BULKHEAD EMERGENCY EXIT LIGHT INOP. UPON FURTHER INVESTIGATION FOUND ELECTRICAL CONNECTOR ABOVE MAIN DOOR REGION CEILING PANEL DISCONNECTED. RECONNEC
- [SDR SIMA20170611001](https://openairdocs.org/sdr/SIMA20170611001), Jun 11, 2017: CONNECTOR. DISCONNECTED. LEFT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. FOUND EMERGENCY LIGHT BATTERY CHARGER NR 1 CONNECTOR REMOVED FROM CHARGER. SECURED THE CONNECTOR, OPS CHECKED GOO
- [SDR SIMA20170601001](https://openairdocs.org/sdr/SIMA20170601001), Jun 1, 2017: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE EXIT LIGHT IAW AMM 33-50-14, OPS CHECKED GOOD.
- [SDR SIMA20170419001](https://openairdocs.org/sdr/SIMA20170419001), Apr 19, 2017: WARNING MESSAGE. ILLUMINATED. HIGH SPEED ABORT FOR MASTER WARNING SPS 1-2 INOPERATIVE, AT 120 KTS. NORMAL BRAKING AND NO OVERHEATING ON BRAKES. -TIGHTENED SPC MOUNTING TRAY KNOBS AS NEEDED. 
- [SDR SIMA20161023001](https://openairdocs.org/sdr/SIMA20161023001), Oct 23, 2016: LIGHT. INOPERATIVE. EMERGENCY LIGHTS STRIP INOPERATIVE SEATS 7-11.
- [SDR SIMA20161023002](https://openairdocs.org/sdr/SIMA20161023002), Oct 23, 2016: CHARGER. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE AT SEATS 7-11. REMOVED AND REPLACED THE NR 3 EMERGENCY POWER SUPPLY AND BATTERY PACK IAW AMM 33-50-04. OPS CHECKED GOOD.
- [SDR SIMA20160509003](https://openairdocs.org/sdr/SIMA20160509003), May 9, 2016: LIGHT. INOPERATIVE. LEFT EMER LIGHT FWD OF WING INOPERATIVE. R & R EMER LIGHT FWD OF WING IAW AMM 33-50-10-000-801 & 33-50-10-400-801. OPERATIONS CHECKED GOOD.
- [SDR SIMA20160331001](https://openairdocs.org/sdr/SIMA20160331001), Mar 31, 2016: ROD. DEFECTIVE. MAIN CABIN DOOR WILL NOT OPEN. DEPLANED VIA SERVICE DOOR. R&R ROD CONNECTED TO CAM ASSEMBLY FOR PAX DOOR FLAP ASSEMBLY IAW AMM 52-18-02. OPERATIONS CHECKED GOOD
- [SDR SIMA20160208003](https://openairdocs.org/sdr/SIMA20160208003), Feb 8, 2016: STRINGER. DENTED. DENT & SCRATCH AT FRAME & STRINGER 8R WITH 1 MISS-DRILLED HOLE IN STRINGER 8R. PERFORMED PERMANENT REPAIR OF DENT, SCRATCH & MISS-DRILLED HOLE ON FRAME 75, STRI
- [SDR SIMA20160205003](https://openairdocs.org/sdr/SIMA20160205003), Feb 5, 2016: WIRE. BROKEN. EXIT SIGN ON COCKPIT HAS A BROKEN WIRE. PERFORMED SPLICE REPAIR TO WIRE W762-8044-20 IAW SWPM 20-21-00.
- [SDR SIMA20160205004](https://openairdocs.org/sdr/SIMA20160205004), Feb 5, 2016: CONNECTOR. MISSING. EMERGENCY LIGHT STRIP NR 8 CONNECTOR AT FLOOR PANEL 261BF MISSING, ACFT SIDE. INSTALLED MISSING CONNECTORS SP9212 WIRE W192-8832-22 & SP9213 WIRE W192-8833-22 I
- [SDR SIMA20160202004](https://openairdocs.org/sdr/SIMA20160202004), Feb 2, 2016: SKIN. CRACKED. LEFT UPPER FUSELAGE SKIN HAS 2 CRACKS. ONE ABOVE STRINGER 2L, & ONE BELOW STRINGER 2L. PERFORMED PERMANENT REPAIR OF LT UPPER SKIN AT FRAME 75 ABOVE & BELOW STR
- [SDR SIMA20160202002](https://openairdocs.org/sdr/SIMA20160202002), Feb 2, 2016: WIRE. BROKEN. LEFT NR 5 FLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRE AT BASE OF LIGHT. R & R NR 5 PROXIMITY LIGHT STRIP IAW AMM 33-50-12.
- [SDR SIMA20160128004](https://openairdocs.org/sdr/SIMA20160128004), Jan 28, 2016: SUPPORT. CORRODED. LAVATORY WASTE BUCKET HAS CORROSION. FABRICATED & INSTALLED DOUBLER ON LAVATORY TOILET WASTES VLV SUPPORT IAW 145 SRM 53-31-02.

All 197: https://openairdocs.org/aircraft/N617AE/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/N617AE/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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