# N14916: 2001 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: 145415
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 21, 2001
- Certificate issued: August 18, 2022
- Expires: August 31, 2029
- Mode S code: A0C6B9
- Registered owner: [Delux Public Charter LLC](https://openairdocs.org/faa-owner/DELUX%20PUBLIC%20CHARTER%20LLC)
- Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas)
- Owner type: LLC
- Owner's area on the map: 32.8483° N, 96.8255° W: Placed by OpenAirDocs at the center of ZIP code 75209, 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=14916
- Page: https://openairdocs.org/aircraft/N14916

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/N14916/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 N14916.

## FAA accident and incident reports

None matched to N14916.

## Service difficulty reports (59, 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 ASOA201904247039](https://openairdocs.org/sdr/ASOA201904247039), Apr 24, 2019: SKIN. CRACKED. TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND THE RIGHT ENGINE PYLON/B SIDE SKIN CRACKED IN TWO PLACES. MAINTENANCE REPAIRED THE CRACK AT THE PYLON FIREWALL
- [SDR ASOA201904237038](https://openairdocs.org/sdr/ASOA201904237038), Apr 23, 2019: SKIN. CHAFED. A/C IS IN C-CHECK WHEN INSPECTION FOUND A CHAFE AT FRAME 70 BETWEEN STRINGER12R AND 13R. MAINTENANCE PERFORMED REPAIR PROCEDURES IAW ECTC ETD2019-145-048747.ALL
- [SDR ASOA201905167048](https://openairdocs.org/sdr/ASOA201905167048), Apr 22, 2019: DOOR FRAME. CORRODED. SERVICE DOOR CUT-OUT CORRODED BELOW AFT LOWER STOP. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER. AIRCRAFT WAS IN C CHECK BUT IS NOW RELEASED AND RETURNED
- [SDR ASOA201811247185](https://openairdocs.org/sdr/ASOA201811247185), Nov 23, 2018: FCU. FAULTY. HEAVY EXHAUST GAS SMELL AFTER STARTING THE APU. REMOVED AND REPLACED THE APU FUEL SOLENOID VALVE IAW HSMM 49-31-02 AND FCU IAW HSMM 49-32-01. OPS AND LEAK CHECK
- [SDR ASOA201808304045](https://openairdocs.org/sdr/ASOA201808304045), Aug 30, 2018: CONNECTOR. BROKEN. SHV - FLIGHT 4309 THE CREW REPORTED SMOKE IN THE FLIGHT DECK AND DIVERTED TO SHV. THE AIRCRAFT LANDED IN SHV WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AI
- [SDR ASOA201803284018](https://openairdocs.org/sdr/ASOA201803284018), Mar 30, 2018: BATTERY PACK. DISCHARGED. THE AISLE EMERGENCY LIGHTING BETWEEN SEATS 8 - 18 WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY PACK, OPS TESTED WITH NO D
- [SDR ASOA20160912050C](https://openairdocs.org/sdr/ASOA20160912050C), Sep 12, 2016: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT STRIP BY ROW 9 AND 10 WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT STRIP AND OPS CHECKS WERE G
- [SDR ASOA20160410034](https://openairdocs.org/sdr/ASOA20160410034), Apr 10, 2016: BULB. BURNED. THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE CABIN. THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE LIGHT BULB AT SEAT 8A, OPERATIONALLY TESTED W
- [SDR ASOA20140718225](https://openairdocs.org/sdr/ASOA20140718225), Jul 18, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 43-44. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-019
- [SDR ASOA20140718224V](https://openairdocs.org/sdr/ASOA20140718224V), Jul 18, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10. THE A
- [SDR ASOA20140718223V](https://openairdocs.org/sdr/ASOA20140718223V), Jul 18, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 29. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10. THE AC
- [SDR ASOA20140718222](https://openairdocs.org/sdr/ASOA20140718222), Jul 18, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, THE LT OMEGA BEAM AT FRAME 33-34 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10. TH
- [SDR ASOA20140718221](https://openairdocs.org/sdr/ASOA20140718221), Jul 18, 2014: BEAM. CORRODED. DURING C-CHECK, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERV
- [SDR ASOA20130416029](https://openairdocs.org/sdr/ASOA20130416029), Apr 16, 2013: LIGHT. INOPERATIVE. DURING ROUTINE MX, THE EMERGENCY LIGHT STRIP BY SEATS 1A/ 2A WOULD NOT TURN ON. MX REPLACED THE AISLE PATH LIGHT STRIP. OPS CHECKS WERE GOOD.
- [SDR ASOA20120917105V](https://openairdocs.org/sdr/ASOA20120917105V), Sep 17, 2012: SILL. CORRODED. DURING C-CHECK CARGO DOOR CUTOUT LOWER SILL CORRODED FR 65-66. MX R & R CARGO DOOR CUTOUT LOWER SILL BETWEEN FRAME 65-68 IAW SRM 51-40-02. THE ACFT WAS APPROVED
- [SDR ASOA201112120017](https://openairdocs.org/sdr/ASOA201112120017), Dec 12, 2011: UNKNOWN. ODOR. THE CREW REPORTED A STRONG JET FUEL ODOR DURING APU START. MX PERFORMED APU OPS CHECKS AND NO FUEL ODOR WAS NOTED. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR C2XA10IA269](https://openairdocs.org/sdr/C2XA10IA269), Oct 18, 2010: CONNECTOR. DIRTY. IAH - FLIGHT 2093, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE SERVICE DOOR EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE CL
- [SDR C2XA10IA254](https://openairdocs.org/sdr/C2XA10IA254), Sep 15, 2010: FMU. DEFECTIVE. IAH - FLIGHT 3151, THE CREW REPORTED A LOW N1 MASTER WARNING ON TAKEOFF ROLE. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANC
- [SDR C2XA10SH290](https://openairdocs.org/sdr/C2XA10SH290), Sep 8, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK RT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAME 23. MAINTENANCE PERFORMED REPAIR AND INSTALLED A DOUBLER ON RT OMEGA BEAM AT FRAME 23 IAW E
- [SDR C2XA10SH289](https://openairdocs.org/sdr/C2XA10SH289), Sep 8, 2010: STRUCTURE. CORRODED. SHV - DURING C-CHECK SERVICE DOOR BOTTOM NUT PLATE HOLES CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED CORROSION FROM AFFECTED AREA OF SERVICE DOOR BOTTOM NUT P
- [SDR C2XA10SH288](https://openairdocs.org/sdr/C2XA10SH288), Sep 8, 2010: STRUCTURE. CORRODED. SHV - DURING C-CHECK PAX DOOR BOTTOM 4 NUT PLATE HOLES FOR MAIN LINER CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED CORROSION FOR AFFECTED AREA OF PAX DOORS NUT
- [SDR C2XA10SH287](https://openairdocs.org/sdr/C2XA10SH287), Sep 8, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK RT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAME 22. MAINTENANCE PERFORMED REPAIR AT RT OMEGA BEAM AT FRAME 22 IAW EMB-145 SRM 53-21-10. THE
- [SDR C2XA10SH286](https://openairdocs.org/sdr/C2XA10SH286), Sep 8, 2010: SKIN. DAMAGED. SHV - DURING C-CHECK 10 WORKING RIVETS FRM 77 BETWEEN STR'S 3L-8L. MAINTENANCE PERFORMED REPAIR OF WORKING RIVETS AT FRM 77 BETWEEN STR'S 3L-8L IAW EC5330-02224
- [SDR C2XA10SH285](https://openairdocs.org/sdr/C2XA10SH285), Sep 8, 2010: SKIN. DAMAGED. SHV - DURING C-CHECK 2 WORKING RIVETS FRM 78 BETWEEN STR'S 5L-6L. MAINTENANCE PERFORMED REPAIR AT FRM 78 BETWEEN STR'S 5L-6L WORKING RIVETS IAW EC5330-02224. TH
- [SDR C2XA10SH284](https://openairdocs.org/sdr/C2XA10SH284), Sep 8, 2010: SKIN. DAMAGED. SHV - DURING C-CHECK 4 WORKING RIVETS FRM 79 BETWEEN STR'S 3L-8L. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN WORKING RIVETS AT FRM 79 STR'S 3L-8L IAW EMB-145
- [SDR C2XA10SH283](https://openairdocs.org/sdr/C2XA10SH283), Sep 8, 2010: SKIN. DAMAGED. SHV - DURING C-CHECK 7 WORKING RIVETS FRM 79 BETWEEN STR'S 3R-7R. MAINTENANCE PERFORMED REPAIR TO FUSELAGE SKIN FRM 79 STR'S 3R-7R IAW EMB-145 EC5330-02224. THE
- [SDR C2XA10SH282](https://openairdocs.org/sdr/C2XA10SH282), Sep 8, 2010: SKIN. CRACKED. SHV - DURING C-CHECK FOUND CRACK ON APU FIREWALL AROUND 3 O'CLOCK POSITION. MAINTENANCE REPAIRED CRACKS ON APU FIREWALL 3 O'CLOCK POSITION IAW EMB-145 EC5330-02
- [SDR C2XA10SH281](https://openairdocs.org/sdr/C2XA10SH281), Sep 8, 2010: SKIN. CRACKED. SHV - DURING C-CHECK APU FIREWALL (EXT SKIN) HAS CRACKS FROM RT UPPER MOUNT AT STIFFENER ENDS AND FROM RIVET HEADS TO RT LOWER MOUNT, AND (2) EACH ON LT SIDE AT
- [SDR C2XA10SH280](https://openairdocs.org/sdr/C2XA10SH280), Sep 8, 2010: SILL. CRACKED. SHV - DURING C-CHECK SERVICE DOOR CENTER SILL CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF SERVICE DOOR CENTER SILL IAW EMB-145 SRM 51-40-02 AND AP
- [SDR C2XA10SH279](https://openairdocs.org/sdr/C2XA10SH279), Sep 8, 2010: BEAM. CRACKED. SHV - DURING C-CHECK CARGO DOOR CUTOUT LWR BEAM HAS CORROSION (LEVEL 2 LOCAL) FRM 65-68. MAINTENANCE PERFORMED REPAIR ON CARGO DOOR CUTOUT LWR BEAM FRM 65-68 AN
- [SDR C2XA10SH278](https://openairdocs.org/sdr/C2XA10SH278), Sep 8, 2010: FRAME. CRACKED. SHV - DURING C-CHECK FRAME 10 STR 10R-9R CRACKED. MAINTENANCE REMOVED AND REPLACED FRM 10 BETWEEN STR 9R-13R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED
- [SDR C2XA10SH277](https://openairdocs.org/sdr/C2XA10SH277), Sep 8, 2010: SILL. CORRODED. SHV - DURING C-CHECK SERVICE DOOR CENTER SILL CORRODED (LEVEL 2 LOCAL). MAINTENANCE REPAIRED SERVICE DOOR CENTER SILL IAW EMB-145 SRM 51-40-02 AND APPLIED SEALA
- [SDR C2XA10RI109](https://openairdocs.org/sdr/C2XA10RI109), Aug 21, 2010: O-RING. DEFECTIVE. FLIGHT 3085 - EWR - FLIGHT CREW REPORTED SMOKE IN CABIN / BLEED NR 1 LEAK WITH APU RUNNING. EWR MX REMOVED AND REPLACED O-RINGS AT JOINTS 25 AND 23. MX PERFORME
- [SDR C2XA10RI047](https://openairdocs.org/sdr/C2XA10RI047), Mar 27, 2010: CONTROL UNIT. INOPERATIVE. FLIGHT 2961 - EWR - FLIGHT CREW REPORTED MAIN AND BACK UP PITCH TRIM INOPERATIVE ON CLIMBOUT. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REM
- [SDR C2XA09RI193](https://openairdocs.org/sdr/C2XA09RI193), Nov 17, 2009: LIGHT. INOPERATIVE. FLIGHT 2543 - EWR - FLIGHT CREW REPORTED EMERGENCY AISLE PATH LIGHT OVERWING EXIT INOPERATIVE. MX REMOVED AND REPLACED AISLE PATH LIGHT AND PERFORMED OPERATIONA
- [SDR C2XA09CL070](https://openairdocs.org/sdr/C2XA09CL070), May 16, 2009: LIGHT. MALFUNCTIONED. YYZ - FLIGHT 3117 - THE CREW REPORTED THE EMERGENCY LIGHTS DID NOT WORK. THE CREW RESET AND OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA09CL065](https://openairdocs.org/sdr/C2XA09CL065), May 16, 2009: CHARGER. INOPERATIVE. FLIGHT NR 3117, THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE. MX INSPECTED AND REPLACED THE NR3 EMERGENCY LIGHT BATTERY AND CHARGER. OPS 
- [SDR C2XA09RI019](https://openairdocs.org/sdr/C2XA09RI019), Jan 27, 2009: INVERTER. INOPERATIVE. RIC - DURING ROUTINE MX, RIC MX FOUND EMERGENCY LIGHT EXIT SIGN AFT GALLEY BULKHEAD INOPERATIVE. MX R&R NR 3 INVERTER AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT
- [SDR C2XA08CL137](https://openairdocs.org/sdr/C2XA08CL137), Dec 26, 2008: CONTROL UNIT. FAULTY. CLE FLT 2345 - THE CREW REPORTED A PITCH TRIM MAIN INOP MESSAGE IN FLIGHT. THE CREW RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLA
- [SDR C2XA08TY138](https://openairdocs.org/sdr/C2XA08TY138), Dec 9, 2008: LIGHT. INOPERATIVE. EMERGENCY LIGHT FLOOR PROXIMITY STRIP INOP. R&R LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPS CK GOOD. ACFT RELEASED AND RETURNED TO SERVICE
- [SDR C2X2008F00017](https://openairdocs.org/sdr/C2X2008F00017), Aug 4, 2008: SKIN. GOUGED. ACFT CURRENTLY IN A C-CHECK STATUS AND THE LT FUSELAGE WAS FOUND GOUGED AND DENTED AT FR19. MAINTENANCE CUT OUT THE AREA AND FABRICATED A NEW REPAIR IAW EC5330-
- [SDR C2XA07IA214](https://openairdocs.org/sdr/C2XA07IA214), Oct 1, 2007: CONTROL UNIT. INOPERATIVE. IAH - FLIGHT 2802, DURING TAXI THE CREW REPORTED A BRAKE OUTBOARD MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE
- [SDR C2XA07TY032](https://openairdocs.org/sdr/C2XA07TY032), Jun 28, 2007: CONTROL LEVER. INOPERATIVE. BNA - FLIGHT NR 2175 - AFTER TAKEOFF, LANDING GEAR DID NOT RETRACT AND CYCLE PROCEDURE PER QRC DID NOT WORK AND A/C DIVERTED INTO TYS. TYS REMOVED AND REPLACED 
- [SDR C2XA05IA062](https://openairdocs.org/sdr/C2XA05IA062), Apr 22, 2005: LIGHT. INOPERATIVE. IAH - FLIGHT 2690, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE CABIN INTERPHONE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A
- [SDR C2XA03BT067](https://openairdocs.org/sdr/C2XA03BT067), Jun 15, 2003: BULB. BURNED OUT. DURING ROUTINE INSPECTION, MAINTENANCE FOUND PASSENGER DOOR EMERGENCY LIGHT AND THE COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY
- [SDR C2XA03BT027](https://openairdocs.org/sdr/C2XA03BT027), Feb 7, 2003: LIGHT. FAULTY. BTV---CO2002, DURING 2A INSPECTION, MAINTENANCE FOUND FLOOR EMERGENCY LIGHT STRIP 2ND FROM THE REAR TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED #7 FLOOR
- [SDR C2XA02IA253](https://openairdocs.org/sdr/C2XA02IA253), Dec 29, 2002: BATTERY. DISCHARGED. BNA- DURING MAINTENANCE THE MECHANIC NOTED THAT THE #1 EMERGENCY LIGHT BATTERY WOULD NOT HOLD CHARGE. BNA- MAINTENANCE REMOVED AND REPLACED THE #1 EMERGENCY LIG
- [SDR C2XA02SH138](https://openairdocs.org/sdr/C2XA02SH138), Dec 6, 2002: BEAM. CORRODED. DURING C CHECK, THE LT HAND OMEGA BEAM AT FRAME 20 INBOARD SIDE WAS FOUND TO HAVE CORROSION. MAITENACE REMOVED DAMAGED AREA AND PERFORMED A SPLICE REPAIR IAW EM
- [SDR C2A02SH136](https://openairdocs.org/sdr/C2A02SH136), Dec 6, 2002: BUTT STRAP. CORRODED. SHV- DURING C CHECK THE CENTER OMEGA BEAM BUTTSTRAP BETWEEN FRAMES 16 AND 17 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AREA AND REPLACED AFFECTED 
- [SDR C2XA02SH139](https://openairdocs.org/sdr/C2XA02SH139), Dec 6, 2002: PLATE. GOUGED. SHV-DURING C CHECK, NR 1 ENGINE, FOWARD PYLON YOKE GUSSET PLATE WAS FOUND TO HAVE A GOUGE BY LOWER ENGINE MOUNT. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTE

All 59: https://openairdocs.org/aircraft/N14916/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/N14916/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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