# N13975: 1999 Embraer EMB-145LR

- Status: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212, 55 seats)
- Engine: [Allison AE3007C series](https://openairdocs.org/engine/allison-ae3007c-series) (registry code 03028)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 145163
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 25, 1999
- Certificate issued: August 18, 2022
- Expires: August 31, 2029
- Mode S code: A0A00B
- 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=13975
- Page: https://openairdocs.org/aircraft/N13975

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

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

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

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

### Matched by engine (Allison AE3007C series)

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

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

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

All 113: https://openairdocs.org/aircraft/N13975/ads.md

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

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

## NTSB investigations

None matched to N13975.

## FAA accident and incident reports

None matched to N13975.

## Service difficulty reports (75, 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 ASOA2019082324047](https://openairdocs.org/sdr/ASOA2019082324047), Aug 22, 2019: SKIN. CRACKED. DURING A-CHECK INSPECTION, THE CROWN SKIN AT THE UPPER AFT CORNER OF THE F/O'S DV WINDOW WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE CRACK AREA AND PERFORM
- [SDR ASOA2018101624053](https://openairdocs.org/sdr/ASOA2018101624053), Oct 12, 2018: CHARGER. INOPERATIVE. IAH - THE CREW REPORTED AN OVERHEAD EMERGENCY LIGHT AT ROW THREE TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY CHARGE
- [SDR ASOA201808127147](https://openairdocs.org/sdr/ASOA201808127147), Aug 12, 2018: WINDOW POST. CRACKED. LEFT COCKPIT WINDSHIELD LATERAL POST WAS CRACKED. REPAIRED THE POST IAW SB 145-53-0029.
- [SDR ASOA201807277143](https://openairdocs.org/sdr/ASOA201807277143), Jul 27, 2018: DOOR SILL. CORRODED. TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND THE LT FLOOR SILL AT FRAME 32 AND 33 WITH CORROSION. MAINTENANCE R&R THE ENTIRE SILL IAW SRM 51-40-02. ALL WOR
- [SDR ASOA201802117012](https://openairdocs.org/sdr/ASOA201802117012), Jan 27, 2018: RIB. CRACKED. LT WING RIB 5 CRACKED. REMOVED AND REPLACED LT RIB 5 IAW ECTC ETD2017-145-104919. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA201703254012](https://openairdocs.org/sdr/ASOA201703254012), Mar 25, 2017: BATTERY PACK. DISCHARGED. MAINTENANCE REPORTED THAT THE NR 1 & 2 OVERWING EMERGENCY LIGHTS AND AFT INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACE
- [SDR ASOA201703254011](https://openairdocs.org/sdr/ASOA201703254011), Mar 25, 2017: POWER SUPPLY. INOPERATIVE. MAINTENANCE REPORTED THAT THE NR 1 & 2 OVERWING EMERGENCY LIGHTS AND AFT INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACE
- [SDR ASOA20150913069](https://openairdocs.org/sdr/ASOA20150913069), Sep 13, 2015: BATTERY PACK. DISCHARGED. DURING MAINTENANCE INSPECTION, THE NR 4 EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED BATTERY PACK, OPERATIONALLY TES
- [SDR ASOA20150830047](https://openairdocs.org/sdr/ASOA20150830047), Aug 30, 2015: CHARGER. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE AFT SECTION OF EMERGENCY FLOOR PATH LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT SYSTEM BATTERY 
- [SDR ASOA20150610032](https://openairdocs.org/sdr/ASOA20150610032), Jun 10, 2015: SIGN. INOPERATIVE. DURING ROUTINE MAINTENANCE THE MAIN DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE SIGN ASSY AND OPS CHECKS WERE GOOD.
- [SDR ASOA20140118009](https://openairdocs.org/sdr/ASOA20140118009), Jan 18, 2014: CHARGER. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE MAIN CABIN DOOR EXTERIOR AND CEILING LIGHTS WERE FOUND INOPERATIVE. R & R THE NR 1 EMERGENCY LIGHT SYS BATTERY POWER SUPPLY W
- [SDR ASOA20131001114](https://openairdocs.org/sdr/ASOA20131001114), Oct 1, 2013: CONTROL PANEL. FAULTY. PILOT REPORTED LAVATORY SMOKE WARNING ON EICAS IN FLIGHT BUT NO SMOKE OBSERVED IN CABIN OR LAVATORY. MX R & R THE LAVATORY SMOKE DETECTOR PANEL OPS CHECKED GOOD
- [SDR ASOA20130909104](https://openairdocs.org/sdr/ASOA20130909104), Sep 9, 2013: LIGHT. INOPERATIVE. DURING SCHEDULED MX INSPECTION THE NR 1 FLOOR PROXIMITY EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MX R & R THE NR 1 FLOOR PROXIMITY LIGHT STRIP WITH OP
- [SDR ASOA20120820062](https://openairdocs.org/sdr/ASOA20120820062), Aug 20, 2012: CONTROLLER. FAULTY. CREW REPORTED LOST AUTO PRESSURIZATION. CABIN PRESSURE CLIMBED TO 8400FT, NO EICAS MESSAGE PRESENT. CREW PERFORMED AIR RETURN. MX R & R DIGITAL PRESSURE CONTROL
- [SDR ASOA20120813130](https://openairdocs.org/sdr/ASOA20120813130), Aug 13, 2012: SEAT TRACK. CORRODED. DURING C-CHECK, FOUND THE RT WALL SEAT TRACK SUPPORT AT FRAME 50 CORRODED. MX BLENDED OUT THE CORROSION IAW SRM 51-10-03. FOUND AREA TO BE WITHIN LIMITS IAW 53-
- [SDR ASOA20120813127](https://openairdocs.org/sdr/ASOA20120813127), Aug 10, 2012: SKIN. CORRODED. CORROSION OUT OF LIMITS ON INNER SKIN BAYS BETWEEN STR 20R & 21L & 22L AT FRM 13 & 14. CUTOUT CORRODED AREAS, FABRICATED 2 FILLERS AND ONE DOUBLER. ACFT STILL I
- [SDR C2XA11CL114](https://openairdocs.org/sdr/C2XA11CL114), Apr 30, 2011: CONTROLLER. FAULTY. ORD FLT 5999 THE CREW REPORTED CABIN ALTITUDE BEGAN TO CLIMB AT A HIGH RATE UNTIL IT REACHED 10,500. THE AIRCRAFT WAS AT 34,000. BEGAN A RAPID DESCENT TO 10,500
- [SDR C2XA10RI106](https://openairdocs.org/sdr/C2XA10RI106), Aug 26, 2010: COFFEEMAKER. DEFECTIVE. FLIGHT 2699 - FLIGHT CREW REPORTED LT COFFEEMAKER SMOKING. EWR MX REMOVED AND REPLACED LT COFFEEMAKER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APP
- [SDR C2XA10CL136](https://openairdocs.org/sdr/C2XA10CL136), Aug 24, 2010: BUTTON. FAULTY. CLE - FLT 2339 - THE CREW REPORTED THE BAG EXTINGUISHER PUSH BUTTON DID NOT ILLUMINATE DURING FIRE DETECTION TEST. MAINTENANCE INSPECTED AND REPLACED THE BAG EX
- [SDR C2XA10TY113](https://openairdocs.org/sdr/C2XA10TY113), Aug 15, 2010: CAP. CORRODED. RIGHT LAV TOP CAP HAS SURFACE CORROSION AT CARBON CROSS BEAM. REMOVED AND REPLACED RT TOP CAP IAW EMB SRM 51-40-09.
- [SDR C2XA10IA200](https://openairdocs.org/sdr/C2XA10IA200), Jul 12, 2010: LIGHT. MALFUNCTIONED. IAH - FLIGHT 2804, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN EMERGENCY EXIT SIGN TO BE INOPERATIVE. MAINTENANCE RESET THE ELECTRICAL SYSTEM, OPERATIONALL
- [SDR C2XA10RI054](https://openairdocs.org/sdr/C2XA10RI054), Apr 15, 2010: INVERTER. INOPERATIVE. FLIGHT 2074 - EWR - FLIGHT CREW REPORTED NR 1 FLOOR EMERGENCY LIGHT STRIP AND SERVICE DOOR EXIT LIGHT INOPERATIVE. EWR MX REMOVED AND REPLACED NR 2 EMERGENCY LI
- [SDR C2XA10CL033](https://openairdocs.org/sdr/C2XA10CL033), Feb 21, 2010: INVERTER. INOPERATIVE. DURING ROUTINE MAINTENANCE THE NR 4 AND 5 EMERGENCY AISLE PATH LIGHT STRIPS WERE FOUND INOPERATIVE. THE NR 5 EMERGENCY LIGHT INVERTER WAS REPLACED AND OPERATION
- [SDR C2XA10CL030](https://openairdocs.org/sdr/C2XA10CL030), Jan 24, 2010: CONNECTOR. LOOSE. CLE FLT 2866 THE CREW REPORTED THE LANDING GEAR HANDLE AND GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE INSPECTED AND RESECURED THE NOSE LANDING GEAR PROXI
- [SDR C2XA10TY008](https://openairdocs.org/sdr/C2XA10TY008), Jan 9, 2010: BATTERY. DEFECTIVE. EMERGENCY LIGHT CIRCUIT BREAKER POPPING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY NR 1, MOUNT TRAY AND CONNECTOR IAW EMB145 AMM 33-50-04, 20-13-07 AND 20-50
- [SDR C2XA09RI164](https://openairdocs.org/sdr/C2XA09RI164), Sep 19, 2009: LIGHT. INOPERATIVE. RIC MX - DURING ROUTINE INSPECTION, MX FOUND EMERGENCY LIGHT STRIP BY SEATS 1A AND 2A INOPERATIVE. RIC MX REMOVED AND REPLACED EMERGENCY LIGHT STRIP AND PERFORM
- [SDR C2XA09TY039](https://openairdocs.org/sdr/C2XA09TY039), Mar 1, 2009: LIGHT. INOPERATIVE. AIRCRAFT IN FOR A OVERNIGHT INSPECTION WHEN THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 
- [SDR C2XA09IA010](https://openairdocs.org/sdr/C2XA09IA010), Jan 1, 2009: CONNECTOR. DIRTY. ON TAKEOFF ROLL THE CREW REPORTED RELAYS CLICKING, AND AFTER TAKEOFF CLICKED AGAIN VERY LOUD AND A JOLT WAS FELT THROUGH THE YOLK AND RUDDER PEDALS. AT 12000 FT
- [SDR C2XA08RI141](https://openairdocs.org/sdr/C2XA08RI141), Sep 26, 2008: WIRE. LOOSE. RIC - MX - DURING ROUTINE MAINTENANCE RIC MX FOUND FORWARD EMERGENCY LIGHT STRIP NOT ILLUMINATING. MX RECONNECTED LOOSE WIRING AND PERFORMED OPERATIONAL CHECK S
- [SDR C2XA08RI142](https://openairdocs.org/sdr/C2XA08RI142), Sep 26, 2008: WIRE. DISCONNECTED. RIC - MX - DURING ROUTINE MAINTENANCE RIC MX FOUND SERVICE DOOR EMERGENCY LIGHT NOT ILLUMINATING. MX FOUND ONE WIRE DISCONNECTED FROM THE SPLICE. MX RECONNECTED
- [SDR C2XA08SH101](https://openairdocs.org/sdr/C2XA08SH101), Aug 9, 2008: FIREWALL. CRACKED. SHV - DURING C-CHECK IT WAS FOUND THAT THE APU FIREWALL WAS CRACKED AROUND RIVETS AT 3 O`CLOCK POSITION. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EXPRESSJET E
- [SDR C2XA07IA251](https://openairdocs.org/sdr/C2XA07IA251), Dec 19, 2007: UNKNOWN. ODOR. FLIGHT 2875 IAH-MFE, THE CREW REPORTED A BURNING ELECTRICAL SMELL IN THE COCKPIT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORME
- [SDR C2XA07RI098](https://openairdocs.org/sdr/C2XA07RI098), Nov 11, 2007: WIRE. BROKEN. FLT 3035 - EWR - CREW REPORTED 3 AFT EMERGENCY LIGHT STRIPS INOPERATIVE. EWR MX FOUND BROKEN WIRE AT EMERGENCY LIGHT NR 8. ME REPAIRED WIRING AND PERFORMED OPER
- [SDR C2XA07IA169](https://openairdocs.org/sdr/C2XA07IA169), Jul 9, 2007: BATTERY PACK. INOPERATIVE. BAN - DURING MAINTENANCE INSPECTION THE NUMBER 4 EMERGENCY LIGHT BATTERY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LI
- [SDR C2XA06CL075](https://openairdocs.org/sdr/C2XA06CL075), Sep 21, 2006: LIGHT. INOPERATIVE. CLE FLIGHT NR 2351 - THE CREW REPORTED THE AISLE PATH EMERGENCY LIGHT STRIP AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT ST
- [SDR C2XA06SH087](https://openairdocs.org/sdr/C2XA06SH087), Sep 1, 2006: STRINGER. CORRODED. SHV - DURING C-CHECK STR 21L HAS CORROSION BETWEEN FR12-13. MAINTENANCE REMOVED AND REPLACED STR 21 FR 8-13 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED 
- [SDR C2XA06SH085](https://openairdocs.org/sdr/C2XA06SH085), Sep 1, 2006: STRINGER. CORRODED. SHV - DURING C-CHECK STR 21R HAS CORROSION BETWEEN FR 12-13. MAINTENANCE REMOVED DAMAGE STR & SPLICED IN NEW SECTION 21R FR 10-13 IAW EMB 145 SRM 53-00-03 ITEM 
- [SDR C2XA06SH084](https://openairdocs.org/sdr/C2XA06SH084), Aug 22, 2006: TIE CLIP. CORRODED. SHV - DURING C-CHECK THE SHEAR CLIP ON FRAME 65 BETWEEN STRINGERS 15 AND 16 L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOU
- [SDR C2XA06CL037](https://openairdocs.org/sdr/C2XA06CL037), Apr 3, 2006: DOOR. BROKEN. CLE FLIGHT NR 2541, CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE. AIR RETURN. MAINTENANCE INSPECTED FOUND AIR SERVICE CHECK VALVE DOOR BROKEN. DOOR ASSEMBLY REMO
- [SDR C2XA06IA050](https://openairdocs.org/sdr/C2XA06IA050), Mar 25, 2006: LIGHT. INOPERATIVE. CRP - DURING MAINTENANCE INSPECTION, THE AISLE PATH LIGHTING STRIP AT SEAT 14A WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT 
- [SDR C2XA05CL098](https://openairdocs.org/sdr/C2XA05CL098), Dec 13, 2005: BALLAST. BURNED. DURING ROUTINE MAINTENANCE THE GALLEY HAD A BURNING ODOR. MAINTENANCE INSPECTED AND FOUND THE GALLEY LIGHT BALLAST BURNED. THE BALLAST WAS REPLACED AND OPERATIO
- [SDR C2XA05BT054](https://openairdocs.org/sdr/C2XA05BT054), Aug 2, 2005: ODOR. DETECTED. CREW REPORTED, ODOR OF BURNING PLASTIC OCCURRED IN CRUISE, TURNED OFF RECIRCULATING FAN, ODOR WENT AWAY. ODOR ONLY IN COCKPIT. INSPECTED CABIN AND COCKPIT FOR B
- [SDR C2XA04IA145](https://openairdocs.org/sdr/C2XA04IA145), Nov 20, 2004: WIRE. BROKEN. IAH - FLIGHT 2890, DURING THE PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE GALLEY EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND R
- [SDR C2XA04SH474](https://openairdocs.org/sdr/C2XA04SH474), Aug 1, 2004: FLOORBEAM. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT THE CROSSBEAM BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORME
- [SDR C2XA04SH472](https://openairdocs.org/sdr/C2XA04SH472), Jul 30, 2004: FLOORBEAM. CORRODED. SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPA
- [SDR C2XA04SH468](https://openairdocs.org/sdr/C2XA04SH468), Jul 27, 2004: FLOORBEAM. CORRODED. SHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02
- [SDR C2XA04SH466](https://openairdocs.org/sdr/C2XA04SH466), Jul 22, 2004: BATTERY. DISCHARGED. DURING C-CHECK THE NR 4 EMERGENCY LIGHT BATTERY WAS FOUND TO BE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY, THE ENSUUING 
- [SDR C2XA03CL044](https://openairdocs.org/sdr/C2XA03CL044), Feb 18, 2003: HARNESS. SHORTED. LIT FLIGHT#2474 THE CREW REPORTED THE CABIN LIGHT AT ROW 6A SHORTED OUT CAUSING SPARKS AND ELECTRICAL SMELL IN THE CABIN.MAINTENANCE INSPECTED AND REPLACED THE 
- [SDR C2XA02TY167](https://openairdocs.org/sdr/C2XA02TY167), Nov 8, 2002: FITTING. BENT. TYS. During a scheduled inspection, the left aileron PCA fitting attach lug was found bent. Maintenance removed and replaced the fitting. I/A/W-EC5750-01177. Th
- [SDR C2XA02TY166](https://openairdocs.org/sdr/C2XA02TY166), Nov 6, 2002: INTAKE. DAMAGED. DURING A SCHEDULED 2-C INSPECTION, THE NR 1 ENGINE INLET INNER SKIN WAS FOUND PROTRUDING ON AFT SIDE OF SKIN AT 4:00 AND 10:00 O`CLOCK POSITIONS. MAINT. MEASURE

All 75: https://openairdocs.org/aircraft/N13975/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/N13975/stcs.md

## Related

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

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