# N614AE: 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: 145086
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 24, 1998
- Certificate issued: September 19, 2011
- Expires: September 30, 2027
- Mode S code: A7FD9F
- 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=614AE
- Page: https://openairdocs.org/aircraft/N614AE

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/N614AE/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 N614AE.

## FAA accident and incident reports (4)

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 20200111010289I](https://openairdocs.org/incident/20200111010289I), Jan 11, 2020: Embraer EMB-145LR (N614AE), Charlotte, NC, No damage. After aircraft landed at Charlotte international airport crew declared emergency for smoke indication in bag bay. Crew discharged bag bay fire extinguisher…
- [Incident 20130202000949I](https://openairdocs.org/incident/20130202000949I), Feb 2, 2013: Embraer EMB-145LR (N614AE), Omaha, NE, No damage. February 2, 2013, N614AE, an Embraer EMB-145LR flight no. 4350 experienced a wing anti ice problem while on approach into Eppley Airfield, Omaha, Nebraska.…
- [Incident 20040130014919I](https://openairdocs.org/incident/20040130014919I), Jan 30, 2004: Emb EMB145LR (N614AE), Wichita, KS. (-23) On January 30, 2004, flight number 3600 aircraft N614AE while enroute from ict to dfw had a malfunction. The nose landing gear would not retract after…
- [Incident 19990107016079I](https://openairdocs.org/incident/19990107016079I), Jan 7, 1999: Emb EMB145 (N614AE), Toledo, OH. (-5) Crew received low oil pressure warning indication for #1 eng. Crew declared emergency, shut down #1 engine and diverted to Toledo and landed without…

## Service difficulty reports (152, 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 HNAA2020031300096](https://openairdocs.org/sdr/HNAA2020031300096), Mar 11, 2020: FIRE BOTTLE. DEFECTIVE. EICAS BAGG EXT BTL INOP MSG DISPLAYED DURING CRUISE. RAN QRH. NO OTHER ASSOCIATED INDICATIONS ON FINAL APPROACH FIRE EXT BAGG BUTTON ILLUMINATED. RAN QRH AND PU
- [SDR HNAA2020021100051](https://openairdocs.org/sdr/HNAA2020021100051), Feb 9, 2020: INTERPHONE. MALFUNCTIONED. LOSS COMS 1 AND 2 AND INTERPHONE MID FLIGHT. PERFORMED OPS CHECK OF 1 AND 2 COMMS. OPS CHECKED IN TERPHONE SYSTEM. NO DEFECTS NOTED. INSPECTED ALL PTT SWITCHES.
- [SDR HNAA2020020300040](https://openairdocs.org/sdr/HNAA2020020300040), Jan 31, 2020: WARNING MESSAGE. FALSE ACTIVATION. FUEL 2 LOW LEVEL LIGHT DISPLAYED ON EICAS DURING TAKEOFF ROLL. ABORTED TAKEOFF. R&R FCU IAW AMM 28-41-01. OPS CHECK GOOD OK FOR SERVICE. CLEAR MEL 28-12 MEL FUE
- [SDR HNAA2020011300014](https://openairdocs.org/sdr/HNAA2020011300014), Jan 11, 2020: SMOKE WARNING. ACTIVATED. CREW DISCHARGED BAG BAY FIRE EXTINGUISHER BOTTLES DUE TO BAG BAY SMOKE INDICATION. MAINTENANCE REMOVED AND REPLACED BOTH THE HIGH-RATE AND METERING FIRE EXTINGU
- [SDR HNAA2019111500365](https://openairdocs.org/sdr/HNAA2019111500365), Nov 14, 2019: IGNITER. FAILED. #2 ENG HUNG START AT 32% N2. FOLLOWE BY ODOR IN CABIN....FIX: R&RD B IGNITOR IAW MM 74-21-10 GROUND RUN A/C, OPS CHECK GOOD.OK FOR SERVICE
- [SDR HNAA2019100700301](https://openairdocs.org/sdr/HNAA2019100700301), Oct 5, 2019: PUMP. LEAKING. NR 1 HYD LOW QTY MSG EICAS MSG IN FLIGHT. QTY CONTINUIOUSLY TRICKLED DOWN FOR WHOLE FLIGHT. R & R NR 1 ENGINE DRIVEN PUMP IAW AMM 29-10-01. PERFORMED A LEAK TES
- [SDR HNAA2019093000289](https://openairdocs.org/sdr/HNAA2019093000289), Sep 25, 2019: LIGHT. INOPERATIVE. NDIS 614 33-50 0013140 25SEP19 SBY CLOSE SERVICE DOOR EXTERNAL LIGHT IS INOP (EMERGENCY LIGHT) 27863 00 SSM FACT 25SEP19 10:34 SBY R+R SERVICE DOOR EXTERNAL LIG
- [SDR HNAA2019061400172](https://openairdocs.org/sdr/HNAA2019061400172), Jun 11, 2019: BULB. BURNED OUT. SERVICE DOOR HINGE EMERGENCY EXIT LIGHT INOP.... FIX: R&R D SERVICE DOOR HINGE EMEGENCY LIGHT LAMP IAW AMM TASK 33-50-10-000/400-801-A.
- [SDR HNAA2019032100076](https://openairdocs.org/sdr/HNAA2019032100076), Mar 20, 2019: ANTI-ICE SYSTEM. MALFUNCTIONED. 614 21-01 2099092 20MAR19 PHL ASSGN DURING CRUISE CREW SMELLED ODOR IN COCKPIT, SELECTED W/S HEAT OFF, ODOR DISAPPEARED. UPON TURNING W/S HEAT BACK ON, NOTICED 
- [SDR HNAA2019030600063](https://openairdocs.org/sdr/HNAA2019030600063), Mar 5, 2019: LIGHT. INOPERATIVE. NDIS 614 33-51 0008490 05MAR19 RIC CLOSE SERVICE DOOR EMERGENCY LIGHT INOP 27625 00 NGR FACT 05MAR19 11:53 RIC R/R EMERGENCY LIGHT BULB ON SERVICE_DOOR IN REF T
- [SDR HNAA2018101100246](https://openairdocs.org/sdr/HNAA2018101100246), Oct 6, 2018: LIGHT. INOPERATIVE. RT OVER WING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RT OVER WING EMERGENCY LIGHT LAMP IN REF TO AMM 33-50-10-000/400-801-A. OK FOR SERVICE.
- [SDR HNAA2018082000203](https://openairdocs.org/sdr/HNAA2018082000203), Aug 19, 2018: SIGN. INOPERATIVE. EMERGENCY EXIT SIGN BY THE MAIN DOOR WAS INOPERATIVE. R & R THE EMERGENCY EXIT SIGN, OPS CHECKED GOOD. COVER SECURED.
- [SDR HNAA2018071800158](https://openairdocs.org/sdr/HNAA2018071800158), Jul 16, 2018: A/C PACK. OUT OF ADJUST. PACK 1 O/L MESS. ADJUSTED TEMPERATURE SETTING, LIGHT EXTINGUISHED. OPERATED SYSTEM FOR 30 MINUTES, NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.
- [SDR RAIA2018042620002](https://openairdocs.org/sdr/RAIA2018042620002), Mar 30, 2018: DOOR SILL. CORRODED. CARGO DOOR SILL IS CORRODED IN SEVERAL PLACES BETWEEN FRAMES 65 AND 67. R & R THE DOOR SILL.
- [SDR RAIA201604300001](https://openairdocs.org/sdr/RAIA201604300001), Apr 30, 2016: LAMP. INOPERATIVE. EMERGENCY EXIT LIGHT IN COCKPIT CEILING, LIGHT NR 7 IS INOPERATIVE. REPLACED THE LAMP. OPS CHECKED GOOD.
- [SDR RAIA201604120001](https://openairdocs.org/sdr/RAIA201604120001), Apr 12, 2016: LIGHT. MISINSTALLED. RIGHT OUTER OVERWING EMERGENCY LIGHT IS UPSIDE DOWN. CORRECTLY REPOSITIONED RT OUTER OVERWING EMERGENCY LIGHT.
- [SDR RAIA201602190001](https://openairdocs.org/sdr/RAIA201602190001), Feb 19, 2016: BULB. INOPERATIVE. RIGHT WING OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RT WING OVERWING EMERGENCY LIGHT BULB. OPS CHECK GOOD.
- [SDR RAIA201602080002](https://openairdocs.org/sdr/RAIA201602080002), Feb 8, 2016: LAMP. INOPERATIVE. RIGHT AFT WING FUSELAGE FAIRING EXTERIOR FLOOD LIGHT IS INOPERATIVE. REPLACED THE LAMP RT AFT WING FUSELAGE FAIRING EXTERIOR FLOOD LIGHT. OPS CHECK GOOD.
- [SDR RAIA201602080001](https://openairdocs.org/sdr/RAIA201602080001), Feb 8, 2016: LIGHT. INOPERATIVE. SERVICE DOOR EXTERIOR FLOOD LIGHT IS INOPERATIVE. R & R SERVICE DOOR EMERGENCY LIGHT. OPS CHECKED GOOD.
- [SDR SIMA20151008003](https://openairdocs.org/sdr/SIMA20151008003), Oct 8, 2015: SKIN. CRACKED. LEFT UPPER FUSELAGE SKIN CRACKED AT FIRST FASTENER BELOW STRINGER 2L ON FRAME 75. ACCOMPLISHED REPAIR OF LT REAR FUSELAGE I SKIN IAW ERS-EM-53MR-1689.
- [SDR SIMA20151008006](https://openairdocs.org/sdr/SIMA20151008006), Oct 8, 2015: INVERTER. INOPERATIVE. EMERGENCY FLOOR LIGHT STRIPS NR 2 & 3 INOPERATIVE. R & R NR 3 EMER ACFT INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.
- [SDR SIMA20151008005](https://openairdocs.org/sdr/SIMA20151008005), Oct 8, 2015: SKIN. DAMAGED. EXTERNAL SKIN OF FUSELAGE HAS A LIGHTNING STRIKE AFT FRAME 19, BETWEEN STRINGER 18R & 19R. PERFORMED REPAIR TO EXTERNAL SKIN AFT FRAME 19, STRINGER 18R - 19R IA
- [SDR SIMA20151008004](https://openairdocs.org/sdr/SIMA20151008004), Oct 8, 2015: SKIN. CRACKED. RIGHT UPPER FUSELAGE SKIN CRACKED FIRST FASTENER BELOW STRINGER 2R. REPAIRED FRAME 75 IAW ERS-EM-53MR-1688.
- [SDR SIMA20151008002](https://openairdocs.org/sdr/SIMA20151008002), Oct 8, 2015: GUSSET. DAMAGED. LEFT FLOOR GUSSET UNDER COCKPIT FLOOR PANEL 221GF, FASTENER HOLE DAMAGED. REPAIRED LT FLOOR GUSSET UNDER COCKPIT FLOOR WHERE DAMAGED FASTENER HOLE WAS IAW ERS-E
- [SDR SIMA20151008001](https://openairdocs.org/sdr/SIMA20151008001), Oct 8, 2015: LEAD. BROKEN. NUMBER 8 EMER LIGHT STRIP HAS BROKEN LEAD. R & R NR 8 EMER LIGHT FLOOR STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150923003](https://openairdocs.org/sdr/SIMA20150923003), Sep 23, 2015: FRAME. CRACKED. FRAME 68, Z FRAME CRACKED UNDER CARGO DOOR HOLD OPEN ROD CUP BRACKET. PERFORMED REPAIR OF FRAME 68, Z FRAME IAW ERS-EM-53MR-16821.
- [SDR SIMA20150922006](https://openairdocs.org/sdr/SIMA20150922006), Sep 22, 2015: STOP FITTING. GOUGED. CARGO DOOR AFT CONTINUOUS STOP IS GOUGED. R & R CARGO DOOR AFT CONTINUOUS STOP IAW ERS-EM-5200-440 & SRM 51-40-02.
- [SDR SIMA20150910007](https://openairdocs.org/sdr/SIMA20150910007), Sep 10, 2015: SKIN. CRACKED. RIGHT UPPER FUSELAGE SKIN CRACKED AT 1ST FASTENER BELOW STRINGER 2R ON FRAME 75, APPROX 1/2" LONG. REPAIRED RT UPPER FUSELAGE SKIN AT 1ST FASTENER BELOW STRINGE
- [SDR SIMA20150910008](https://openairdocs.org/sdr/SIMA20150910008), Sep 10, 2015: LEAD. BROKEN. EMERGENCY LIGHT STRIP NR 8 HAS BROKEN LEADS. INSTALLED EMER LIGHT STRIPS NR 8 IAW AMM 33-50-12. SEE BOW 202054 FOR OPERATIONS CHECK.
- [SDR SIMA20150910006](https://openairdocs.org/sdr/SIMA20150910006), Sep 10, 2015: SKIN. CRACKED. RIGHT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 & ABOVE STRINGER 2R, APPROX 3/8" LONG. CRACK ON RT REAR FUSELAGE 1 EXTERNAL SKIN AFT OF FRAME 75 ABOVE STRINGE
- [SDR SIMA20150910005](https://openairdocs.org/sdr/SIMA20150910005), Sep 10, 2015: FRAME. CRACKED. FRAME 68, Z FRAME CRACKED UNDER CARGO DOOR HOLD OPEN ROD CUP BRACKET. PERFORMED REPAIR TO FRAME 68, Z FRAME UNDER CARGO DOOR HOLD OPEN ROD CUP BRACKET IAW ERS-E
- [SDR SIMA20150910004](https://openairdocs.org/sdr/SIMA20150910004), Sep 10, 2015: SKIN. CRACKED. LEFT UPPER FUSELAGE SKIN CRACKED AT 1ST FASTENER BELOW STRINGER 2L ON FRAME 75, APPROX 3/8" LONG. EASI 8071 USED, 100-500 KHZ PROBE, FREQ=400, V-GAIN=78.5, H-GA
- [SDR SIMA20150910003](https://openairdocs.org/sdr/SIMA20150910003), Sep 10, 2015: WIRE. BROKEN. BROKEN WIRE, W192-8630-22, ON EMER FLOOR LIGHT STRIP 1. REPAIRED WIRE, W192-8630-22, ON EMER FLOOR LIGHT STRIP 1 IAW SWPM 20-21-00. SEE BOW 202054 FOR OPERATION
- [SDR SIMA20150910002](https://openairdocs.org/sdr/SIMA20150910002), Sep 10, 2015: INVERTER. INOPERATIVE. EMERGENCY FLOOR LIGHT STRIPS NR 2 & 3 INOPERATIVE. R & R NR 3 EMER ACFT INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150822002](https://openairdocs.org/sdr/SIMA20150822002), Aug 22, 2015: LIGHT. INOPERATIVE. RIGHT OVERWING EMER LIGHT INOPERATIVE. R & R RT OVERWING EMER LIGHT LAMP. OPERATIONS CHECKED GOOD IAW AMM 33-50-10.
- [SDR SIMA20150803005](https://openairdocs.org/sdr/SIMA20150803005), Aug 3, 2015: WIRE. BROKEN. AFT EMERGENCY LIGHT STRIP BROKEN WIRE ON AIRCRAFT SIDE OF STRIP, IN FRONT OF LAVATORY. REPAIRED FLOOR STRIP WIRE IAW SWPM 20-21-00.
- [SDR SIMA20150723003](https://openairdocs.org/sdr/SIMA20150723003), Jul 23, 2015: LIGHT. INOPERATIVE. RIGHT EMER LIGHT OVERWING INOPERATIVE. R & R RT EMER LIGHT OVERWING. OPERATIONS CHECKED GOOD IAW AMM 33-50-01.
- [SDR SIMA20150710003](https://openairdocs.org/sdr/SIMA20150710003), Jul 10, 2015: LIGHT. INOPERATIVE. RIGHT EXTERIOR OVERWING EMER LAMP INOPERATIVE. R & R RT EXTERIOR OVERWING EMER LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD AT 
- [SDR SIMA20150331007](https://openairdocs.org/sdr/SIMA20150331007), Mar 31, 2015: SKIN. DENTED. REPLACE RT STAB UPPER SKIN. R & R RT STAB UPPER SKIN IAW SRM 55-10-01 SI, 51-40-02, 51-20-03, 51-40-06, CPM 51-21-04, 51-21--05, 51-21-06, ETN-EM-55-073R2, ETN-
- [SDR SIMA20150327007](https://openairdocs.org/sdr/SIMA20150327007), Mar 27, 2015: SKIN. DENTED. REPLACE RT STAB UPPER SKIN. R & R RT STAB UPPER SKIN IAW SRM 55-10-01 SI, 51-40-02, 51-20-03, 51-40-06 & CPM 51-21-04, 51-21--05, 51-21-06, ETN-EM-55-073R2, ETN
- [SDR SIMA20150327006](https://openairdocs.org/sdr/SIMA20150327006), Mar 27, 2015: SKIN. DENTED. HAIL DAMAGE EVENT. REPLACE LT STAB UPPER SKIN. R & R LT STAB UPPER SKIN IAW SRM 55-10-01SI, 51-20-01, 51-20-03, 51-40-02, 51-40-06, ETN-EM-55-074 & ETN-EM-51-11
- [SDR SIMA20150315001](https://openairdocs.org/sdr/SIMA20150315001), Mar 15, 2015: LIGHT. INOPERATIVE. SECOND FROM THE REAR AISLE EMER LIGHT INOPERATIVE. R & R AISLE EMER LIGHT LAMP IAW AMM 33-50-08. OPERATIONS CHECKED OK.
- [SDR SIMA20150131003](https://openairdocs.org/sdr/SIMA20150131003), Jan 31, 2015: LIGHT. INOPERATIVE. RIGHT EXTERIOR OVERWING EMER LAMP INOPERATIVE. R & R RT EXTERIOR OVERWING EMER LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GO
- [SDR SIMA20141223008](https://openairdocs.org/sdr/SIMA20141223008), Dec 23, 2014: WIRE HARNESS. DAMAGED. AFTER LANDING GEAR RETRACTION, THE NOSE GEAR DOORS DIDN`T FULLY CLOSE, CYCLED GEAR DOWN THEN UP, DID NOT FIX THE PROBLEM. RETURNED TO DEPARTURE. R & R WIRING HA
- [SDR SIMA20141216004](https://openairdocs.org/sdr/SIMA20141216004), Dec 16, 2014: LIGHT. INOPERATIVE. OVERWING EMER LIGHT RT WING INOPERATIVE. R & R OVERWING EMER LIGHT RT WING LAMP. OPERATIONS CHECKED GOOD IAW AMM 33-50-07.
- [SDR SIMA20141128004](https://openairdocs.org/sdr/SIMA20141128004), Nov 28, 2014: UNKNOWN. ODOR. DURING TAXI, AFTER STARTING NR 1 ENG, STRONG ELEC BURNING SMELL IN COCKPIT & GALLEY AREA. BOTH ENGS RUNNING WITH APU FEEDING THE PACKS NO SMOKE OR FIRE VISIBLE.
- [SDR SIMA20141128005](https://openairdocs.org/sdr/SIMA20141128005), Nov 28, 2014: ELECTRICAL BOX. MALFUNCTIONED. IAW NR 1 OF THIS LOG PAGE AFTER START ENG 1, DURING TAXI, STRONG ELEC BURNING SMELL IN COCKPIT & GALLEY AREA. PERFORMED GVI INSPECTION FOR SMOKE SMELL & BURNT E
- [SDR SIMA20141029004](https://openairdocs.org/sdr/SIMA20141029004), Oct 29, 2014: LIGHT. INOPERATIVE. RIGHT EXTERIOR AFT OVERWING EMER LIGHT IS INOPERATIVE. LAMPED THE RT EXTERIOR AFT OVERWING EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
- [SDR SIMA20141029003](https://openairdocs.org/sdr/SIMA20141029003), Oct 29, 2014: INVERTER. INOPERATIVE. CABIN EMER LIGHTS INOPERATIVE. FLOOR PROXIMITY 4 & 5 LT EXIT IDENTIFIER & RT EXIT IDENTIFIER. R & R INVERTER NR 5 IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140922005](https://openairdocs.org/sdr/SIMA20140922005), Sep 22, 2014: FLASHLIGHT. BROKEN. FIRST OFFICER`S FLASHLIGHT ON & OFF SWITCH IS BROKEN. THE SWITCH FELL OFF THE LIGHT. R & R FIRST OFFICER'S FLASHLIGHT. OPERATIONS CHECKED GOOD IAW AMM CH 33-51-

All 152: https://openairdocs.org/aircraft/N614AE/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/N614AE/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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