# N618AE: 1998 Embraer EMB-145LR

- Status: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212, 55 seats)
- Engine: [Allison AE3007C series](https://openairdocs.org/engine/allison-ae3007c-series) (registry code 03028)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 145097
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 20, 1998
- Certificate issued: September 9, 2011
- Expires: September 30, 2027
- Mode S code: A80C7B
- 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=618AE
- Page: https://openairdocs.org/aircraft/N618AE

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Allison AE3007C model are included.

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

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

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-08-07](https://openairdocs.org/ad/2025-08-07): Flight Controls · Embraer EMB-145, EMB-145ER, EMB-145MR and 4 more. Effective Jun 26, 2025
- [AD 2024-26-07](https://openairdocs.org/ad/2024-26-07): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 11, 2025
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2021-07-14](https://openairdocs.org/ad/2021-07-14): Main landing gear · Yaborã Indústria Aeronáutica EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Apr 20, 2021
- [AD 2021-04-09](https://openairdocs.org/ad/2021-04-09): Engine fuel and control · Yaborã Indústria Aeronáutica EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Mar 30, 2021
- [AD 2019-03-30](https://openairdocs.org/ad/2019-03-30): Engine Exhaust · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 26, 2019
- [AD 2017-15-16](https://openairdocs.org/ad/2017-15-16): Flight controls · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Sep 5, 2017
- [AD 2017-12-09](https://openairdocs.org/ad/2017-12-09): Fuel · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Jul 20, 2017
- [AD 2017-04-12](https://openairdocs.org/ad/2017-04-12): Ice and rain protection · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Mar 29, 2017
- [AD 2015-02-13](https://openairdocs.org/ad/2015-02-13): Nacelles/pylons; Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 6, 2015
- [AD 2013-22-18](https://openairdocs.org/ad/2013-22-18): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Nov 20, 2013
- [AD 2012-19-06](https://openairdocs.org/ad/2012-19-06): Stabilizers · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 9 more. Effective Oct 29, 2012
- [AD 2011-21-15](https://openairdocs.org/ad/2011-21-15): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 7 more. Effective Nov 23, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2010-16-02](https://openairdocs.org/ad/2010-16-02): Airborne Auxiliary Power · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 9, 2010
- [AD 2010-16-01](https://openairdocs.org/ad/2010-16-01): Fuel · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Sep 9, 2010
- [AD 2010-12-07](https://openairdocs.org/ad/2010-12-07): Wings · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jul 22, 2010
- [AD 2010-11-01](https://openairdocs.org/ad/2010-11-01): Fuselage · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jul 6, 2010
- [AD 2010-10-11](https://openairdocs.org/ad/2010-10-11): Landing gear · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jun 21, 2010
- [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010
- [AD 2010-03-07](https://openairdocs.org/ad/2010-03-07): Landing gear · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 11, 2010
- [AD 2009-26-02](https://openairdocs.org/ad/2009-26-02): Ice and rain protection · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 19, 2010
- [AD 2009-01-05](https://openairdocs.org/ad/2009-01-05): Maximum takeoff weight (MTOW) · Embraer EMB-145, EMB-145EP, EMB-145ER and 4 more. Effective Mar 27, 2009
- [AD 2008-22-19](https://openairdocs.org/ad/2008-22-19): Flight deck · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 19, 2008
- [AD 2008-17-05](https://openairdocs.org/ad/2008-17-05): Fuel tanks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 23, 2008
- [AD 2008-10-08](https://openairdocs.org/ad/2008-10-08): Reduces the compliance time for doing the modification · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective May 23, 2008
- [AD 2008-05-02](https://openairdocs.org/ad/2008-05-02): Tail section or rudder pedals · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Apr 8, 2008
- [AD 2008-03-03](https://openairdocs.org/ad/2008-03-03): Elevator control system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Feb 14, 2008
- [AD 2007-24-03](https://openairdocs.org/ad/2007-24-03): Forward fuselage right hand (RH) side skin · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jan 2, 2008
- [AD 2007-10-11](https://openairdocs.org/ad/2007-10-11): Electrical bonding clamps · Embraer EMB-135BJ (Legacy 600), EMB-135LR, EMB-145LR and 2 more. Effective Jun 21, 2007
- [AD 2007-04-09](https://openairdocs.org/ad/2007-04-09): Left- and right-hand windshield temperature controllers · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 23, 2007
- [AD 2007-04-03](https://openairdocs.org/ad/2007-04-03): Pitot static heating relay K0057 · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 21, 2007
- [AD 2006-19-04](https://openairdocs.org/ad/2006-19-04): Honeywell COM unit and Mode S transponder · Bombardier BD-700-1A10, BD-700-1A11, 550 and 26 more. Effective Oct 17, 2006
- [AD 2006-16-17](https://openairdocs.org/ad/2006-16-17): Torque values of the screws that attach the seat tracks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 25, 2006
- [AD 2006-07-01](https://openairdocs.org/ad/2006-07-01): Horizontal stabilizer control unit (HSCU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective May 1, 2006
- [AD 2006-03-06](https://openairdocs.org/ad/2006-03-06): Pilot's and co-pilot's seat tracks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 13, 2006
- [AD 2005-25-17](https://openairdocs.org/ad/2005-25-17): Auxiliary power unit (APU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 18, 2006
- [AD 2005-24-11](https://openairdocs.org/ad/2005-24-11): Elevator gust lock system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 9, 2006
- [AD 2005-24-02](https://openairdocs.org/ad/2005-24-02): Airplane flight manual (AFM) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 28, 2005
- [AD 2005-23-20](https://openairdocs.org/ad/2005-23-20): Auxiliary power unit (APU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 27, 2005
- [AD 2005-23-13](https://openairdocs.org/ad/2005-23-13): Nose landing gear (NLG) wheel · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 19, 2005
- [AD 2005-22-08](https://openairdocs.org/ad/2005-22-08): Total air temperature (TAT) sensor heating system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Nov 30, 2005
- [AD 2005-20-37](https://openairdocs.org/ad/2005-20-37): Main landing gear (MLG) trailing arms and integrity of the MLG pivot axle sealant. · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Nov 16, 2005
- [AD 2005-14-02](https://openairdocs.org/ad/2005-14-02): Left and right engine fire handles · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Aug 15, 2005
- [AD 2005-14-03](https://openairdocs.org/ad/2005-14-03): Engine-driven hydraulic pump · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Aug 10, 2005
- [AD 2005-13-22](https://openairdocs.org/ad/2005-13-22): Electric fuel pumps · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jul 7, 2005
- [AD 2005-05-09](https://openairdocs.org/ad/2005-05-09): Forward upper liners · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Apr 14, 2005
- [AD 2005-04-05](https://openairdocs.org/ad/2005-04-05): Air turbine starter (ATS) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 24, 2005
- [AD 2005-01-05](https://openairdocs.org/ad/2005-01-05): Nose Landing Gear Wheel Nuts and Associated Inner and Outer Seals, and Reidentifying the Landing Gear Strut · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Feb 9, 2005

### Matched by engine (Allison AE3007C series)

- [AD 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018
- [AD 2017-11-05](https://openairdocs.org/ad/2017-11-05): Turbine/ turboprop Engine, Turbine Section · Rolls-Royce AE 3007C and AE 3007C1. Effective Jul 18, 2017
- [AD 2015-02-08](https://openairdocs.org/ad/2015-02-08): Turbine wheels · Rolls-Royce AE 2100D2, AE 2100D2A, AE 2100D3 and 11 more. Effective Mar 11, 2015
- [AD 2009-24-04](https://openairdocs.org/ad/2009-24-04): Fan spinner · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 5 more. Effective Dec 28, 2009
- [AD 2007-24-05](https://openairdocs.org/ad/2007-24-05): Engine oil temperature · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 8 more. Effective Jan 2, 2008
- [AD 2001-25-05](https://openairdocs.org/ad/2001-25-05): Compressor Cone Shafts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jan 23, 2002
- [AD 2001-19-03](https://openairdocs.org/ad/2001-19-03): High Pressure Turbine 1st to 2nd Stage Turbine Spacer · Rolls-Royce AE 3007A and AE 3007C. Effective Oct 29, 2001
- [AD 2001-17-31](https://openairdocs.org/ad/2001-17-31): Second Stage High Pressure Turbine Wheel · Rolls-Royce AE 2100A, AE 2100C, AE 2100D3 and 2 more. Effective Oct 5, 2001
- [AD 2000-18-06](https://openairdocs.org/ad/2000-18-06): Digital Electronic Controls · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 22, 2000
- [AD 2000-13-01](https://openairdocs.org/ad/2000-13-01): Turbine Wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 1, 2000
- [AD 2000-11-22](https://openairdocs.org/ad/2000-11-22): Critical Life-Limited Parts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Aug 7, 2000
- [AD 98-11-32](https://openairdocs.org/ad/98-11-32): Sump Magnetic Chip Collector Plug · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Jun 18, 1998

### Historical (superseded or no longer in force)

- [AD 2008-13-14](https://openairdocs.org/ad/2008-13-14) (historical): Fuel system limitations (FSL) · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jul 30, 2008
- [AD 2007-12-17](https://openairdocs.org/ad/2007-12-17) (historical): Metallic tubes enclosing the vent and pilot valve wires · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Jul 19, 2007
- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 2006-20-08](https://openairdocs.org/ad/2006-20-08) (historical): Rod ends of aileron power control actuator, superseding AD 99-05-04 · Embraer EMB-145, EMB-145EP, EMB-145ER and 4 more. Effective Nov 8, 2006
- [AD 2006-04-02](https://openairdocs.org/ad/2006-04-02) (historical): Pitot static heating relay K0057 · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Mar 31, 2006
- [AD 2005-26-15](https://openairdocs.org/ad/2005-26-15) (historical): Certain components of the elevator control system · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 8 more. Effective Feb 3, 2006
- [AD 2005-25-04](https://openairdocs.org/ad/2005-25-04) (historical): Tail section or rudder pedals · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Dec 23, 2005
- [AD 2001-17-04](https://openairdocs.org/ad/2001-17-04) (historical): Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Sep 5, 2001
- [AD 2000-04-09](https://openairdocs.org/ad/2000-04-09) (historical): Elevator Servo Tab and Spring Tab Hinge Fittings of the Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Mar 10, 2000
- [AD 2000-09-05](https://openairdocs.org/ad/2000-09-05) (historical): Cone Shafts · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jul 5, 2000
- [AD 99-02-51](https://openairdocs.org/ad/99-02-51) (historical): Starter Shaft Seal · AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Apr 20, 1999

All 113: https://openairdocs.org/aircraft/N618AE/ads.md

## Information bulletins (advisory) (9 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB AIR-20-17](https://openairdocs.org/saib/AIR-20-17): Air Conditioning - Cabin Pressure Control System. Issued Nov 3, 2020
- [SAIB NM-19-17](https://openairdocs.org/saib/NM-19-17): Ice and Rain Protection: Electrical Wiring Terminations at Pitot and TAT Relays. Issued Dec 5, 2019
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008
- [SAIB NM-08-15](https://openairdocs.org/saib/NM-08-15): Instruments: Contamination of the Attitude Heading Reference System (AHRS) Computers. Issued Mar 26, 2008
- [SAIB NM-07-40](https://openairdocs.org/saib/NM-07-40): Embraer EMB-135/145 Landing Gear Incident. Issued Jul 9, 2007
- [SAIB NM-07-20](https://openairdocs.org/saib/NM-07-20): Flight Data Recorders. Issued Mar 21, 2007
- [SAIB NE-11-22](https://openairdocs.org/saib/NE-11-22): Engine Controls. Issued Feb 23, 2011
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N618AE.

## 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 20050707013449I](https://openairdocs.org/incident/20050707013449I), Jul 7, 2005: Emb EMB145LR (N618AE), Grand Rapids, MI. (-23) On July 07, 2005, at 1633, Emb-145-LR, N618AE, registered to simmons airline, #1 engine low oil light came on, and pilot noticed oil quantity drop to 5…

## Service difficulty reports (178, 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 SIMA202210043001](https://openairdocs.org/sdr/SIMA202210043001), Oct 3, 2022: LAMP. INOPERATIVE. RH OVERWING EMERGENCY LT INOP-C/A-RAR OVERWING EMERGENCY LIKGHT LAMP IAW EMB 145 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.
- [SDR SIMA20220716001](https://openairdocs.org/sdr/SIMA20220716001), Jul 16, 2022: LIGHT. INOPERATIVE. LH OVER-WING EMERGENCY LIGHT INOP-C/A-RAR LH OVER-WING EMERGENCY LIGHT LAMP IAW AMM 33-50-07. OPS TEST GOOD AT THIS TIME
- [SDR SIMA20220410003](https://openairdocs.org/sdr/SIMA20220410003), Apr 10, 2022: NONE. INOPERATIVE. EMERGENCY FLOOR LIGHT PROXIMITY STRIP INOP NEAR ROW 8A. ORIG LOGPAGE 4593164 ITEM 3 MEL 3323 - AUTH# 04-128-C .-C/A-REMOVED AND REPLACED PROXIMITY FLOOR STRIP 8
- [SDR SIMA20220409003](https://openairdocs.org/sdr/SIMA20220409003), Apr 9, 2022: BATTERY. UNSERVICEABLE. EMERGENCY LIGHT STRIP AT SEAT 8A AND 9A INOP SUSPECT #3 EMERGENCY POWER SUPPLY NEED REPLACEMENT-C/A-RAR #3 EMERGENCY POWER SUPPLY IAW AMM 33-50-04. OPERATIONAL 
- [SDR SIMA20220409002](https://openairdocs.org/sdr/SIMA20220409002), Apr 9, 2022: LAMP. INOPERATIVE. L/H OVER WING EMERGENCY LIGHT INOP-C/A-RAR L/H OVER WING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPERATIONAL CHECK GOOD.
- [SDR SIMA20220404002](https://openairdocs.org/sdr/SIMA20220404002), Apr 4, 2022: NONE. NONE. RH AILERON O/B PCA ATTACHMENT TO AILERON FITTING, BUSHING IS MIGRATED AND LOOSE.(MAJOR REPAIR)-C/A-RAR RH AILERON PCA FITTING ASSY IAW EO-EM-27MR-112
- [SDR SIMA20220329001](https://openairdocs.org/sdr/SIMA20220329001), Mar 29, 2022: LAMP. INOPERATIVE. RH OVER WING EMERGENCY LIGHT INOP-C/A-RAR RH OVER WING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. NO FIX. RAR RH OVER WING EMER
- [SDR SIMA20220322001](https://openairdocs.org/sdr/SIMA20220322001), Mar 22, 2022: NONE. NONE. PACK #1 + PACK #2 CLOSED EICAS MESSAGE IN FLIGHT RAN QRH AND AIRCRAFT DID NOT PRESSURIZE.DECLARED EMG TROUBLE WITH CABIN PRESSURE PACK #1 + PACK #2 CLOSED EICAS
- [SDR SIMA20211124002](https://openairdocs.org/sdr/SIMA20211124002), Nov 24, 2021: NONE. NONE. FA AFT EMERGENCY FLASHLIGHT MISSING-C/A-FLIGHT CREW PLACARDED AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AUTH 110346M-C REF 25-32 MOC 630997
- [SDR SIMA20211117001](https://openairdocs.org/sdr/SIMA20211117001), Nov 17, 2021: NONE. NONE. RH EXTERIOR OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH EXTERIOR OVERWING EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10, NO FIX. RAR #4 EMERGENCY BATTERY PACK AND 
- [SDR SIMA20211006001](https://openairdocs.org/sdr/SIMA20211006001), Oct 6, 2021: NONE. NONE. MEL 2532 - AUTH# 100085M-C FA FWD FLASHLIGHT INOP LOGPAGE: 4715664-C/A-RAR FA FWD FLASHLIGHT ASSY IAW EMB145 AMM 33-50-16. OPC GOOD. MEL 25-32 AUTH# 100085M-C R
- [SDR SIMA202109054001](https://openairdocs.org/sdr/SIMA202109054001), Sep 4, 2021: LIGHT. INOPERATIVE. SEAT 12A OVERWING EMERGENCY LIGHT INOP-C/A-RAR SEAT 12A OVERWING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-07. OPS CHECK GOOD.
- [SDR SIMA20210516004](https://openairdocs.org/sdr/SIMA20210516004), May 16, 2021: CONTACTOR. BURNED. STRONG ELEC FUME SMELL WHILE DECENDING THROUGH FL240 CAME AND WENT FOR THE REMAINDEROF FLIGHT.-C/A- FOUND LH RECIRCULATION FAN CONTACTOR BURNED . RAR RECIRCULAT
- [SDR SIMA20201106002](https://openairdocs.org/sdr/SIMA20201106002), Nov 6, 2020: STRINGER. CORRODED. CORROSION ON STR 17R BETWEEN FR 19A AND FR 20. C/A: REMOVED AND REPLACED DAMAGED PORTION OF STRINGER 17R BETWEEN FR 16-24, IAW EMB 145 SRM 53-00-03 ITEM 7.
- [SDR SIMA20201101003](https://openairdocs.org/sdr/SIMA20201101003), Nov 1, 2020: VALVE. CORRODED. SSI 53-20-29 TOILET WASTE VALVE BUCKET IS CORRODED. C/A: REMOVED AND REPLACED WASTE VALVE CUP (BUCKET), IAW EMB 145 SRM 51-40-02 AND EMB 145 SRM 51-20-03.
- [SDR SIMA20201031003](https://openairdocs.org/sdr/SIMA20201031003), Oct 31, 2020: PROFILE. CORRODED. SSI 52-21-06 CORROSION ON LT PASSENGER ESCAPE HATCH LOWER L PROFILE. C/A: REMOVED AND REPLACED LT PASSENGER ESCAPE HATCH LOWER L PROFILE, IAW EMB145 SRM 51-20-0
- [SDR SIMA20201028002](https://openairdocs.org/sdr/SIMA20201028002), Oct 28, 2020: DOOR SILL. CORRODED. SSI 53-30-48: AIRCRAFT STRUCTURE CARGO DOOR LOWER CUTOUT CORRODED, MARKED. C/A: REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT (SILL), IAW EMB 145 SRM 51-40-02.
- [SDR SIMA20201028001](https://openairdocs.org/sdr/SIMA20201028001), Oct 28, 2020: DOOR SILL. CRACKED. FRAME 66 CRACKED AT CARGO DOOR SILL ON T BRACKET. C/A: REMOVED AND REPLACED FR 66 LOWER SECTION, IAW EMB 145 SRM 51-40-02.
- [SDR SIMA20201026004](https://openairdocs.org/sdr/SIMA20201026004), Oct 26, 2020: SKIN. DAMAGED. EXTERNAL FUSELAGE SKIN HAS A CREASE BETWEEN FR 73-74 AND STGR 12L-13L. C/A: PERFORMED A TYPE A SKIN DOUBLER REPAIR AT CEASE BETWEEN FR 73-74 STGR 12L-13L, IAW E
- [SDR SIMA20201026003](https://openairdocs.org/sdr/SIMA20201026003), Oct 26, 2020: PROFILE. CORRODED. CORROSION ON CARGO DOOR LOWER LT PROFILE. C/A: R & R CARGO DOOR LOWER LT PROFILE, IAW EMB 145 SRM 51-20-03 AND SRM 51-40-02.
- [SDR SIMA20201025004](https://openairdocs.org/sdr/SIMA20201025004), Oct 25, 2020: PROFILE. CORRODED. CORROSION ON RT PASSENGER ESCAPE HATCH LOWER LT PROFILE. C/A: R & R RT PASSENGER ESCAPE HATCH LOWER LT PROFILE, IAW EMB 145 SRM 51-20-03, 51-40-02, AND 51-20-01
- [SDR SIMA20201025003](https://openairdocs.org/sdr/SIMA20201025003), Oct 25, 2020: SKIN. GOUGED. CARGO DOOR INNER WEBBING (SKIN) HAS 3 GOUGES AT PREVIOUS REPAIR. C/A: RE-ACCOMPLISHED 2 EACH REPAIRS ON THE CARGO DOOR INNER LOWER SKIN, IAW EMB 145 SRM 52-30-0
- [SDR SIMA20201025002](https://openairdocs.org/sdr/SIMA20201025002), Oct 25, 2020: DOOR FRAME. CORRODED. RT OVER WING HATCH LOWER FRAME IS CORRODED AROUND 2 FASTENER HOLES ON AFT END. C/A: R & R RT PASSENGER ESCAPE HATCH LOWER LT PROFILE BEAM, IAW EMB 145 SRM 51-20
- [SDR SIMA20201023004](https://openairdocs.org/sdr/SIMA20201023004), Oct 23, 2020: SHEAR TIE. CORRODED. CARGO DOOR CUTOUT FR 65 SHEAR CLIP CORRODED. C/A: R & R CARGO DOOR CUTOUT FR 65 SHEAR CLIP, IAW EMB 145 SRM 53-31-04.
- [SDR SIMA20201023003](https://openairdocs.org/sdr/SIMA20201023003), Oct 23, 2020: BRACKET. CORRODED. FR 65 T BRACKET CORRODED. C/A: R & R FR 65 T BRACKET, IAW EMB 145 SRM 51-40-02.
- [SDR SIMA20201020003](https://openairdocs.org/sdr/SIMA20201020003), Oct 20, 2020: YOKE. CRACKED. RT ENGINE FWD YOKE STRUCTURE, FWD OUTBOARD LOWER SIDE IS CRACKED. C/A: R & R RT ENGINE FWD LOWER YOKE FITTING, IAW ERS-EM-54MR-698.
- [SDR SIMA20201007001](https://openairdocs.org/sdr/SIMA20201007001), Oct 7, 2020: RIB. CRACKED. LT WING RIB 21 IS CRACKED INSIDE THE PCA PANEL. C/A: PERFORMED REPAIR AT LT WING RIB 21 INSIDE THE PCA PANEL, IAW EMB 145 SRM 57-50-07 ITEM 4 FIGURE 203.
- [SDR SIMA20201002006](https://openairdocs.org/sdr/SIMA20201002006), Oct 2, 2020: BULB. INOPERATIVE. EMERGENCY LIGHT ON RIGHT WING OVERHEAD PANEL INOPERABLE. C/A COMPLETE: R & R EMERGENCY LIGHT BULB ON RIGHT WING OVERHEAD PANEL, IAW EMB 145 AMM 33-50-10. OPERAT
- [SDR SIMA20201002007](https://openairdocs.org/sdr/SIMA20201002007), Oct 2, 2020: CONNECTOR. MISSING. NR 1 AND NR 2 EMERGENCY FLOOR LIGHT STRIPS ARE MISSING CONNECTORS ON A/C SIDE. C/A COMPLETE: INSTALLED NEW AND SERVICEABLE CONNECTORS AT NR 1 AND NR 2 EMERGENCY
- [SDR SIMA20201002005](https://openairdocs.org/sdr/SIMA20201002005), Oct 2, 2020: CONNECTOR. BROKEN. NR 1 EMERGENCY LIGHT STRIP CONNECTOR ON A/C SIDE IS BROKEN. C/A COMPLETE: R & R NR 1 EMERGENCY LIGHT STRIP CONNECTOR ON A/C SIDE, IAW EMB 145 SWPM 20-21-00. INS
- [SDR SIMA20200917004](https://openairdocs.org/sdr/SIMA20200917004), Sep 17, 2020: LIGHT. INOPERATIVE. DURING PS-1 CHECK, FOUND LT ABOVE WING EXTERIOR EMERGENCY LIGHT INOP. C/A: R & R EXTERIOR EMERGENCY LIGHT ASSEMBLY, IAW AMM 33-50-10. OPERATIONAL CHECK GOOD. NO
- [SDR SIMA202008164001](https://openairdocs.org/sdr/SIMA202008164001), Aug 14, 2020: BULB. INOPERATIVE. DURING PS-1 CHECK FOUND R/H O/W EMERGENCY LIGHT INOP-C/A-RAR R/H O/W EMERGENCY LIGHT BULB IAW EMB-145 AMM 33-50-10
- [SDR SIMA202007232003](https://openairdocs.org/sdr/SIMA202007232003), Jul 22, 2020: CONNECTOR. DETACHED. LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R LT EXTERIROR OVERWING EMERGENCY EXIT LIGHT BULB IAW AMM 33-50-10. OPS CHECK FAILED. REMOVED ACESS
- [SDR SIMA202006109003](https://openairdocs.org/sdr/SIMA202006109003), Jun 9, 2020: FLAPPER VALVE. FAULTY. SUPPLEMENTAL LOST PRESSURIZATION AT APPROX 13,500 COULD CABIN ALT (2000) FEET WAS THE BEST. DEFER AUTO PRES M PROCEDURES C/W MANUAL PRESS OPS CHECK GOOD IAW AMM
- [SDR SIMA2020060129003](https://openairdocs.org/sdr/SIMA2020060129003), May 29, 2020: BATTERY. DISCHARGED. LEFT EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY INVERTER IAW AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. NO FIX, REMOVED AN
- [SDR SIMA2020060129001](https://openairdocs.org/sdr/SIMA2020060129001), May 29, 2020: LIGHT. INOPERATIVE. LEFT AFT OVERWING EMERGENCY LIGHT. REMOVED AND REPLACED LT AFT OVERWING EMERGENCY LIGHT IAW AMM 33-50-07-000-801-A AND 33-50-07-400-801-A, NO FIX.. REMOVED AND 
- [SDR SIMA2020060129002](https://openairdocs.org/sdr/SIMA2020060129002), May 29, 2020: BATTERY. DISCHARGED. RIGHT EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY INVERTER IAW AMM 33-50-11-000-801-A AND 33-50-11-400-801-A, NO FIX. REMOVED A
- [SDR SIMA202005186001](https://openairdocs.org/sdr/SIMA202005186001), May 16, 2020: CHARGER. INOPERATIVE. INTERIOR RH EXIT EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED #2 BATTERY CHARGER ASSEMBLY, IAW AMM 33-50-04, OPERATIONS CHECK GOOD. BATTERY CHARGER ASSY P/N 11
- [SDR SIMA202003254001](https://openairdocs.org/sdr/SIMA202003254001), Mar 24, 2020: LIGHT. INOPERATIVE. RIGHT HAND OVERWING EXIT LIGHT INOP-C/A-REMOVED AND REPLACED LAMP FOR THE RH OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-50-07. OPS CHECK GOOD
- [SDR SIMA202003097001](https://openairdocs.org/sdr/SIMA202003097001), Mar 7, 2020: BATTERY. DISCHARGED. LH AND RH OVER WING EMERGENCY LIGHTS WILL NOT ILLUMINATE-C/A-RE-LAMPED RH OVER WING EMERGENCY LIGHT NO FIX. RAR BATTERY AND CHARGER #4 IAW WC 33-700-19 OPC CHEC
- [SDR SIMA202001275002](https://openairdocs.org/sdr/SIMA202001275002), Jan 25, 2020: BRAKE. LACK OF LUBE. PARKING BRAKE HARD TO SET.-C/A-CLEANED AND LUBRICATED PARKING BRAKE IAW EMB 145MM 32-44-10. OPS CK GOOD.
- [SDR SIMA2020012019004](https://openairdocs.org/sdr/SIMA2020012019004), Jan 19, 2020: SMOKE DETECTOR. FALSE INDICATION. CARGO SMOKE INDICATION AT PARKING BRAKE SET CFR RESPONDED. NO EVIDENCE OF SMOKE DETECTED. R & R THE SMOKE DETECTORS NR 1 AND 2 IAW AMM 26-15-01. OPS CHECKED GOO
- [SDR SIMA202001198001](https://openairdocs.org/sdr/SIMA202001198001), Jan 18, 2020: CRADLE. BROKEN. REAR FLASHLIGHT HOLDER IN CABIN BROKEN. REMOVED AND REPLACED AFT FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECKED GOOD.
- [SDR SIMA201912164001](https://openairdocs.org/sdr/SIMA201912164001), Dec 14, 2019: LINE. DAMAGED. HYD SYS 1 LO QTY RETURNED TO BASE TRANSFER TO NRWC# 618-MIA-03437-C/A-REPAIRED HYD RETURNED LINE ITEM#1 FIG 17 ON IPC 29-11-00 LEAK CHECK GOOD NO DISCREPANCIES 
- [SDR SIMA20190914004](https://openairdocs.org/sdr/SIMA20190914004), Sep 14, 2019: INVERTER. INOPERATIVE. RT UPPER EMERGENCY EXIT LIGHT AT ROW 12C INOP. C/A-REMOVED AND R EPLACED EMERGENCY LIGHT DC/AC INVERTER IAW AMM 33-50-11 OPC GOOD.
- [SDR SIMA201906173004](https://openairdocs.org/sdr/SIMA201906173004), Jun 13, 2019: CONTROL MODULE. ODOR. FA REPORTS PANGENT SMELL COMING FROM SERVICE DOOR BACK TO ROW 6-C/A-FOUND CABIN LIGHT CONTROL MODULE TO BE THE SOCRCE REMOVED AND REPLACED CONTROL MODULE ASSEMB
- [SDR SIMA2019040104](https://openairdocs.org/sdr/SIMA2019040104), Mar 27, 2019: CONNECTOR. BROKEN. DURING INSTALLATION OF FLOOR PANEL 261BF FOUND FLOOR PROXIMITY STRIP LIGHT WIRE CONNECTOR BROKEN.-C/A-INSTALLED MISSING SPLICE MALE CONNECTOR IN FLOOR PROXIMITY
- [SDR SIMA20190220001](https://openairdocs.org/sdr/SIMA20190220001), Feb 20, 2019: LIGHT. INOPERATIVE. LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A AND AMM 33-50-10-400-801-A. OPS CHECK GOOD. NO M
- [SDR SIMA201812065001](https://openairdocs.org/sdr/SIMA201812065001), Dec 5, 2018: LAMP. INOPERATIVE. LH EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH EMERGENCY LIGHT IAW AMM 33-50-10 OPS CHECK GOOD.
- [SDR SIMA201811196001](https://openairdocs.org/sdr/SIMA201811196001), Nov 16, 2018: WARNING LIGHT. FALSE ACTIVATION. FLAP LOW SPEED ADVISORYIN CRUISE AT FL 370 NO FLAPS SELECTED LEVER NOT MOVED MECH FLAP WARNING AT ALTITUDE AND POSS AIRSPEED UNRELIABLE EMERGENCY DECLARED.-C/A-

All 178: https://openairdocs.org/aircraft/N618AE/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/N618AE/stcs.md

## Related

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

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