# N14933: 1997 Embraer EMB-145EP

- Status: Valid registration
- Airframe: [Embraer EMB-145EP](https://openairdocs.org/model/embraer-emb-145ep) (registry code 3260221, 55 seats)
- Engine: [Rolls-Royce AE3007 series](https://openairdocs.org/engine/rolls-royce-ae3007-series) (registry code 54582)
- 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: 145018
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 27, 2005
- Certificate issued: July 16, 2019
- Expires: July 31, 2029
- Mode S code: A0C6FC
- Registered owner: [Spectre Air Capital LLC](https://openairdocs.org/faa-owner/SPECTRE%20AIR%20CAPITAL%20LLC)
- Location: [Horseshoe Bay, TX](https://openairdocs.org/faa-place/TX/Horseshoe%20Bay)
- Owner type: LLC
- Owner's area on the map: 30.5258° N, 98.3759° W: Placed by OpenAirDocs at the center of ZIP code 78657, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14933
- Page: https://openairdocs.org/aircraft/N14933

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 Rolls-Royce AE3007 model are included.

## ADs that may apply (OpenAirDocs): 86 in force

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

- [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 2007-04-09](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 2006-25-07](https://openairdocs.org/ad/2006-25-07): Fuel quantity indication system (FQIS) wire harness and the direct current (DC) fuel pump wire harness · Embraer EMB-135ER, EMB-135KE, EMB-145 and 4 more. Effective Jan 16, 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 (Rolls-Royce AE3007 series)

- [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 2018-17-04](https://openairdocs.org/ad/2018-17-04): Turbine section · Rolls-Royce AE 2100D2A, AE 2100D3 and AE 3007A2. Effective Sep 21, 2018
- [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 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 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 2009-04-03](https://openairdocs.org/ad/2009-04-03): 2nd stage, 3rd stage, and 4th stage compressor wheels · Rolls-Royce AE 1107C and AE 3007A1E. Effective Mar 24, 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 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 2003-25-08](https://openairdocs.org/ad/2003-25-08): 1st and 2nd stage turbine spacers · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 3 more. Effective Jan 21, 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 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 100: https://openairdocs.org/aircraft/N14933/ads.md

## Information bulletins (advisory) (10 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 CE-00-18](https://openairdocs.org/saib/CE-00-18): . Issued Mar 30, 2000
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N14933.

## FAA accident and incident reports

None matched to N14933.

## Service difficulty reports (101, 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 ASOA20140625144](https://openairdocs.org/sdr/ASOA20140625144), Jun 25, 2014: FRAME. CRACKED. DURING C-CHECK, FRAME 66 WAS FOUND TO BE CRACKED AT STRINGER 16R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW SRM 53-00-04. THE ACFT WAS APPROVED FOR RETURN TO S
- [SDR ASOA20140622134V](https://openairdocs.org/sdr/ASOA20140622134V), Jun 23, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 22. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10, FIGURE
- [SDR ASOA20131217220](https://openairdocs.org/sdr/ASOA20131217220), Dec 17, 2013: POWER SUPPLY. INOPERATIVE. DURING PREFLIGHT INSPECTION, CREW REPORTED THE AFT EMERGENCY EXIT LIGHT AND FLOOR PROXIMITY LIGHTS INOPERATIVE. R & R POWER SUPPLY, OPS TESTED WITH NO DEFECTS, 
- [SDR ASOA201309300178](https://openairdocs.org/sdr/ASOA201309300178), Sep 30, 2013: FLAPPER VALVE. LEAKING. THE CREW REPORTED FUEL LEAKING FROM THE RT WING. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE FLAPPER VALVE ON THE RT WING RIB 
- [SDR ASOA20130902160](https://openairdocs.org/sdr/ASOA20130902160), Sep 2, 2013: BULB. BURNED OUT. DURING MX INSP, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS, AND TH
- [SDR ASOA20130808145](https://openairdocs.org/sdr/ASOA20130808145), Aug 8, 2013: SKIN. CRACKED. DURING 2A INSPECTION THE LT SIDE FUSELAGE SKIN WAS FOUND TO BE CRACKED IN 2 PLACES AT A RIVET ON FRAME 77 BELOW STRINGER 8L. MX REMOVED THE DAMAGE AND PERFORMED
- [SDR ASOA20130808144](https://openairdocs.org/sdr/ASOA20130808144), Aug 8, 2013: SKIN. CRACKED. DURING 2A INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STR 5R. MC REMOVED THE DAMAGE, AND PERFORMED A FREEZE PLUG R
- [SDR ASOA20130808143](https://openairdocs.org/sdr/ASOA20130808143), Aug 8, 2013: SKIN. CRACKED. DURING 2A INSPECTION, LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED IN TWO PLACES AT A RIVET ON FRAME 79 BELOW STRINGER 5L. MX REMOVED THE DAMAGE AND PERFORMED A
- [SDR ASOA20130401047H](https://openairdocs.org/sdr/ASOA20130401047H), Apr 1, 2013: WIRE. BROKEN. DURING MX INSPECTION, THE NR 5 AISLE PATH LIGHT STRIP WAS FOUND TO HAVE A BROKEN WIRE. MX R & R THE AFFECTED LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACF
- [SDR ASOA20140310037](https://openairdocs.org/sdr/ASOA20140310037), Mar 10, 2013: BULB. BURNED OUT. DURING MAINTENANCE INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT BULB, OPS TESTED WITH NO D
- [SDR ASOA20120901117](https://openairdocs.org/sdr/ASOA20120901117), Sep 1, 2012: LIGHT. INOPERATIVE. DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH LIGHTING STRIP AT ROW 15A WAS INOPERATIVE. MX R & R THE AFFECTED LIGHT, OPS TESTED WITH NO 
- [SDR ASOA20120314019](https://openairdocs.org/sdr/ASOA20120314019), Mar 14, 2012: FLOOR SUPPORT. CORRODED. DURING C-CK. CENTER OMEGA BEAM CORRODED FR 18-23. R & R CENTER OMEGA BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11IA250](https://openairdocs.org/sdr/C2XA11IA250), Nov 3, 2011: ACTUATOR. INOPERATIVE. AMA - FLIGHT 4172, THE CREW REPORTED, RECEIVED A LANDING GEAR LEVER DISAGREE WARNING MESSAGE APPEARED ON CLIMBOUT. THE AIRCRAFT RETURNED TO AMA WHERE IT LANDED 
- [SDR C2XA11IA227](https://openairdocs.org/sdr/C2XA11IA227), Sep 25, 2011: LIGHT. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASS
- [SDR C2XA11IA156](https://openairdocs.org/sdr/C2XA11IA156), Jul 16, 2011: UNKNOWN. ODOR. MAF - FLIGHT 2079, THE CREW REPORTED THAT THE FLIGHT ATTENDANT SMELLED SMOKE IN FLIGHT IN THE FWD CLOSET AREA AND THE AREA OF ROW THREE WITH THE SMELL STILL PRE
- [SDR C2XA11IA111](https://openairdocs.org/sdr/C2XA11IA111), Jun 12, 2011: BALLAST. BURNED. DURING GROUND OPERATIONS THE CREW REPORTED A SMOKE SMELL NEAR THE GALLEY. MAINTENANCE FOUND THE CABIN OVERHEAD BALLAST TO BE THE SOURCE OF THE SMOKE AND REPLACE
- [SDR C2XA10IA221](https://openairdocs.org/sdr/C2XA10IA221), Aug 9, 2010: BATTERY. OVERHEATED. IAH - FLIGHT 2735 THE CREW REPORTED A NUMBER TWO BATTERY OVERTEMP INDICATION ON DESCENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED A
- [SDR C2XA10IA097](https://openairdocs.org/sdr/C2XA10IA097), Mar 13, 2010: BALLAST. OVERHEATED. IAH - FLIGHT 3027, THE CREW REPORTED AN ELECTRICAL BURNING SMELL AROUND ROW 2A. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOV
- [SDR C2XA09IA323](https://openairdocs.org/sdr/C2XA09IA323), Dec 20, 2009: GROUND WIRE. DEFECTIVE. IAH - FLIGHT 2963, THE CREW REPORTED A SPOILER FAIL AND SPOILER OPEN INDICATION IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECT
- [SDR C2XA09IA291](https://openairdocs.org/sdr/C2XA09IA291), Nov 18, 2009: REVEAL. LOOSE. CRP - FLIGHT 2820, THE CREW REPORTED THAT THE WINDOW REVEAL AT ROW 18A WAS FOUND TO BE LOOSE. THE AIRCRAFT DIVERTED TO CRP WHERE IT LANDED WITHOUT INCIDENT. MAI
- [SDR C2XA09IA275](https://openairdocs.org/sdr/C2XA09IA275), Oct 28, 2009: STARTER GEN. MALFUNCTIONED. IAH - FLIGHT 3020, THE CREW REPORTED A BURNING SMELL AFTER ENGINE 1 START. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND DETERM
- [SDR C2XA09TY214](https://openairdocs.org/sdr/C2XA09TY214), Aug 7, 2009: DOOR FRAME. CORRODED. TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND CORROSION AT FRAME 22 AT THE SERVICE DOOR CUTOUT. MAINTENANCE CUT OUT THE DAMAGE SECTION AND REPLACED. COLD
- [SDR C2XA09TY213](https://openairdocs.org/sdr/C2XA09TY213), Aug 7, 2009: SILL. CORRODED. TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE SERVICE DOOR SILL CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB 135/145 SRM 51-40-0
- [SDR C2XA09TY212](https://openairdocs.org/sdr/C2XA09TY212), Aug 4, 2009: FIREWALL. CRACKED. TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND A CRACK IN THE APU FIREWALL. MAINTENANCE REMOVED AND REPLACED THE FIREWALL IAW EMB 145 SRM 51-40-02 AND IC 
- [SDR C2XA09TY211](https://openairdocs.org/sdr/C2XA09TY211), Aug 3, 2009: ANGLE. CRACKED. GALLEY CENTER AISLE LT RAMP ANGLE CRACKED. REMOVED AND REPLACED RAMP ANGLE.
- [SDR C2XA09TY210](https://openairdocs.org/sdr/C2XA09TY210), Aug 2, 2009: FITTING. CRACKED. SHEAR CLIP CRACKED AT FRM 77 STR 1R. REMOVED AND REPLACED CRACKED SHEAR CLIP.
- [SDR C2XA09TY209](https://openairdocs.org/sdr/C2XA09TY209), Jul 31, 2009: BRACKET. CRACKED. BRACKET CRACKED AT FRM 81 TO STR 8R. REMOVED AND REPLACED SHEAR CLIP.
- [SDR C2XA09TY208](https://openairdocs.org/sdr/C2XA09TY208), Jul 31, 2009: FITTING. CRACKED. SHEAR CLIP CRACKED AT FRM 81 TO STR 8L. REMOVED AND REPLACED SHEAR CLIP.
- [SDR C2XA09TY207](https://openairdocs.org/sdr/C2XA09TY207), Jul 31, 2009: FLOOR SUPPORT. CORRODED. GALLEY AREA CENTER OMEGA BEAM TOP CAP HAS SMALL AREAS OF CORROSION. CENTER TOP CAP WAS REMOVED AND REPLACED.
- [SDR C2XA09TY199](https://openairdocs.org/sdr/C2XA09TY199), Jul 30, 2009: SILL. CORRODED. TYS - A/C IN C-CHECK WHEN INSPECTION FOUND THE LEFT FLOOR SILL CORRODED FROM FRAME 23 TO FRAME 29 (SSI 53-20-11). MAINTENANCE REMOVED AND REPLACED THE FLOOR SIL
- [SDR C2XA09TY197](https://openairdocs.org/sdr/C2XA09TY197), Jul 30, 2009: BEARING CAP. CORRODED. TYS - A/C CURRENTLY IN C-CHECK AND INSPECTION FOUND CORROSION ON THE RIGHT FORWARD MAIN LANDING GEAR BEARING CAP WITH DEEP PITTING. MAINTENANCE REMOVED AND REPL
- [SDR C2XA09TY206](https://openairdocs.org/sdr/C2XA09TY206), Jul 29, 2009: BEARING CAP. CORRODED. RIGHT AFT MAIN LANDING GEAR BEARING CAP HAS DEEP PITTING CORROSION. REMOVED AND REPLACED CAP.
- [SDR C2XA09TY203](https://openairdocs.org/sdr/C2XA09TY203), Jul 29, 2009: ANGLE. CORRODED. GALLEY CENTER AISLE RT RAMP ANGLE CORRODED BEYOND LIMITS AT CARBON CROSS BEAM. REMOVED AND REPLACED RAMP ANGLE.
- [SDR C2XA09TY201](https://openairdocs.org/sdr/C2XA09TY201), Jul 29, 2009: CASE. CORRODED. NR 2 ENG FAN CASE FWD FLANGE HAS CORROSION IN BOLT HOLES. REMOVED CORROSION FROM 12 HOLES BY REAMING IAW EC 7220-01066.
- [SDR C2XA09TY193](https://openairdocs.org/sdr/C2XA09TY193), Jul 28, 2009: FITTING. WORN. RT SPEED BRAKE ACTUATOR BRACKET LOWER ATTACHMENT HAT BUSHING BORE OUT OF LIMITS. REMOVED AND REPLACED FITTING.
- [SDR C2XA09TY187](https://openairdocs.org/sdr/C2XA09TY187), Jul 28, 2009: BUSHING. WORN. TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RIGHT GROUND SPOILER, CENTER HINGE BRACKET HAT BUSHING RACE OUT OF MFG'S LIMITS. MAINTENANCE REMOVED AN
- [SDR C2XA09TY180](https://openairdocs.org/sdr/C2XA09TY180), Jul 24, 2009: SPAR CAP. CORRODED. TYS - SURFACE CORROSION WAS FOUND ON THE LEFT WING SPAR ONE I/B CAP. MAINTENANCE REMOVED THE LITE CORROSION IAW EMB 135/145 SRM 57-20-01. ALL WORK ACCOMPLISHED 
- [SDR C2XA09TY173A](https://openairdocs.org/sdr/C2XA09TY173A), Jul 21, 2009: HINGE. CORRODED. LEFT AND RIGHT HORZ STAB HINGE PINS PITTED AND HAVE CORROSION. REPLACED HINGE PINS.
- [SDR C2XA08IA246](https://openairdocs.org/sdr/C2XA08IA246), Nov 25, 2008: LIGHT. INOPERATIVE. IAH - FLIGHT 2819 - DURING POST FLIGHT INSPECTION THE CREW REPORTED THE 3RD AISLE PATH EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE A
- [SDR C2XA08IA237](https://openairdocs.org/sdr/C2XA08IA237), Nov 12, 2008: UNKNOWN. ODOR. IAH - FLIGHT 3059 THE CREW REPORTED A BURNING SMELL IN THE GALLEY DURING TAXI. THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIR
- [SDR C2XA08IA223](https://openairdocs.org/sdr/C2XA08IA223), Oct 6, 2008: UNKNOWN. UNKNOWN. IAH FLIGHT 3123 THE CREW REPORTED A LOUD THUMPING NOISE 3 OR 4 TIMES AFTER GEAR RETRACTION. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX INSPEC
- [SDR C2XA08RI036](https://openairdocs.org/sdr/C2XA08RI036), Mar 3, 2008: UPLOCK. DEFECTIVE. FLIGHT 2400 - EWR - CREW REPORTED NOSE LANDING GEAR MADE CONTINUOUS BANGING SOUND AFTER RETRACTION. CREW DIVERTED FLIGHT TO EWR AND LANDED AIRCRAFT UNEVENTFULLY
- [SDR C2XA07CL021](https://openairdocs.org/sdr/C2XA07CL021), Feb 7, 2007: CONTROL UNIT. FAULTY. CLE FLIGHT 2727 THE CREW REPORTED LOUD NOISE AND VIBRATION FROM FRONT OF AIRPLANE. THE GEAR WAS RECYCLED AND THE NOISE WENT AWAY. MAINTENANCE INSPECTED AND FOUN
- [SDR C2XA06RI002](https://openairdocs.org/sdr/C2XA06RI002), Aug 21, 2006: LIGHT. INOPERATIVE. RIC - MX DURING ACFT ROUTINE INSPECTION, MX FOUND NR 7 FLOOR PROXIMITY EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED PROXIMITY LIGHT ASSY. OPERATIONAL TEST PERF
- [SDR C2XA06CL052](https://openairdocs.org/sdr/C2XA06CL052), May 24, 2006: SOLENOID VALVE. STICKING. CLE FLIGHT 2236 THE CREW REPORTED THE NOSE GEAR DOORS STAYED OPEN AFTER GEAR RETRACTION. EVENTUALLY SLAMMED SHUT. MAINTENANCE INSPECTED AND REPLACED THE NOSE LA
- [SDR C2XA05BT044](https://openairdocs.org/sdr/C2XA05BT044), Jun 23, 2005: DUCT. FAILED. BNA/EWR---CO2882, DURING PREFLIGHT INSPECTION CREW REPORTED, SMOKE FROM VENTS, ELECTRICAL IN NATURE FROM PACK NR 2. NASHVILLE MAINTENANCE INSPECTED AIRCRAFT AND
- [SDR C2XA05CL050](https://openairdocs.org/sdr/C2XA05CL050), Jun 19, 2005: APU. ODOR. DURING ROUTINE MAINTENANCE, OIL ODOR IN CABIN WAS NOTED WHEN APU BLEED WAS SELECTED. MX RELEASED ACFT IAW MEL 49-00-00. MX REPLACED APU. OPS CHECKS WERE GOOD.
- [SDR C2XA05CL049](https://openairdocs.org/sdr/C2XA05CL049), Jun 16, 2005: SMOKE DETECTOR. INTERMITTENT. CREW REPORTED INTERMITTENT LAVATORY SMOKE WARNING ON GROUND AND INFLIGHT. MX INSP AND REPLACED LAVATORY SMOKE DETECTOR. OPS CHECKS GOOD.
- [SDR C2XA05RI002](https://openairdocs.org/sdr/C2XA05RI002), Mar 2, 2005: BULB. LOOSE. RIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND SERVICE DOOR OVERHEAD EMERGENCY LIGHT (ONE BULB) NOT WORKING. MAINTENANCE REPOSITION BULB AND PERFORMED OPERA
- [SDR C2XA05BT009](https://openairdocs.org/sdr/C2XA05BT009), Jan 28, 2005: LIGHT. FAULTY. EWR---CO2383, CREW REPORTED RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGH

All 101: https://openairdocs.org/aircraft/N14933/reports.md

## STCs that may be installed (OpenAirDocs) (66, 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-145EP)

- [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 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 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 ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [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 ST00818DE](https://openairdocs.org/stc/ST00818DE): Installation of Honeywell Control Display Unit (CDU) model CD-830. Premier Air Center LLC d/b/a West Star Aviation
- [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 ST09858SC](https://openairdocs.org/stc/ST09858SC): Installation of cabin automatic coffee brewing system. Safran Cabin Germany Gmbh
- [STC ST01270WI-D](https://openairdocs.org/stc/ST01270WI-D): Installation of Honeywell MK V and MK VII EGPWS Runway Awareness and Advisory System (RAAS). This approval is limited to specifically idenitfied aircraft. Duncan Aviation Inc
- [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
- [STC ST04282AT](https://openairdocs.org/stc/ST04282AT): Installation of the Honeywell DU-875 LCD Flight Display. Chippewa Aerospace Inc
- [STC ST04015AT](https://openairdocs.org/stc/ST04015AT): Installation of the Honeywell NZ-2000 FMS/GPS System with or without WAAS/LPV. Chippewa Aerospace Inc
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS

All 66: https://openairdocs.org/aircraft/N14933/stcs.md

## Related

- Other Embraer EMB-145EP aircraft: https://openairdocs.org/model/embraer-emb-145ep/aircraft.md
- The Rolls-Royce AE3007 series engine: https://openairdocs.org/engine/rolls-royce-ae3007-series.md

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