# N13989: 2000 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: 145271
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 29, 2000
- Certificate issued: August 18, 2022
- Expires: August 31, 2029
- Mode S code: A0A032
- 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=13989
- Page: https://openairdocs.org/aircraft/N13989

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/N13989/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 N13989.

## FAA accident and incident reports

None matched to N13989.

## Service difficulty reports (96, 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 ASOA2019111164060](https://openairdocs.org/sdr/ASOA2019111164060), Nov 6, 2019: WIRE. BROKEN. IAH - DURING MAINTENANCE INSPECTION THET #3 EMERGENCY LIGHT STRIP WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OP
- [SDR ASOA201909234053](https://openairdocs.org/sdr/ASOA201909234053), Sep 23, 2019: INVERTER. INOPERATIVE. IAH - FLIGHT 4155, DURING MAINTENANCE INSPECTION THE LEFT HAND OVER WING EXIT SHROUD EXIT MARKER FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE #4 I
- [SDR ASOA2019081547096](https://openairdocs.org/sdr/ASOA2019081547096), Aug 14, 2019: MOUNT. CORRODED. NR 2 ENGINE FORWARD INBOARD ACCESSORY GEARBOX MOUNT POINT CORRODED. REPAIRED AREA IN ACCORDANCE WITH TECHNICAL VARIANCE 204465 BY BLENDING OUT CORROSION AND APP
- [SDR ASOA201908017093](https://openairdocs.org/sdr/ASOA201908017093), Aug 1, 2019: SKIN. DELAMINATED. A/C IS IN C-CHECK WHEN INSPECTION FOUND THE L/H I/B FLAP WITH AREAS OF IMPACT DAMAGE ON THE LOWER SIDE. UPON FURTHER INSPECTION FOUND THE AREAS TO BE DELAMINATI
- [SDR ASOA2018062515159](https://openairdocs.org/sdr/ASOA2018062515159), Jun 21, 2018: BATTERY PACK. INOPERATIVE. DURING MX INSPECTION THE AFT EMERGENCY LIGHTS AND OVER WING LIGHTS WERE FOUND NOT TO ILLUMINATE. MX REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY. OPS CHECK
- [SDR ASOA201712217033](https://openairdocs.org/sdr/ASOA201712217033), Dec 18, 2017: BATTERY PACK. DISCHARGED. FLOOR EMERGENCY LIGHT STRIPS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 3 IAW AMM 33-50-04 AND IPC 33-50-04 ITEM 30 FIG 01. OPS CHECKED GOOD.
- [SDR ASOA201712054064](https://openairdocs.org/sdr/ASOA201712054064), Dec 5, 2017: BATTERY PACK. WEAK. IAH- DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS 3 & 4 WERE FOUND TO BE NOT HOLDING A CHANRGE. MAINTENANCE REMOVED AND REPLACED
- [SDR ASOA201712054063](https://openairdocs.org/sdr/ASOA201712054063), Dec 5, 2017: BATTERY PACK. WEAK. IAH- DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS 3 & 4 WERE FOUND TO BE NOT HOLDING A CHANRGE. MAINTENANCE REMOVED AND REPLACED
- [SDR ASOA20161005055](https://openairdocs.org/sdr/ASOA20161005055), Oct 5, 2016: INVERTER. INOPERATIVE. MAINTENANCE REPORTED THE EMERGENCY LIGHTS WERE INOPERATVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERIES NR 2, 3, AND 4 ALONG WITH INVERTER NR 6. OPS CHECKED G
- [SDR ASOA20160919049R](https://openairdocs.org/sdr/ASOA20160919049R), Sep 19, 2016: WIRE. LOOSE. THE AFT CABIN EMERGENCY EXIT OVERHEAD LIGHT INOPERATIVE. INSTALLED A LOOSE WIRE ON INTERIOR EMERGENCY LIGHT ASSY AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RET
- [SDR ASOA20160916051](https://openairdocs.org/sdr/ASOA20160916051), Sep 16, 2016: SIGN. INOPERATIVE. EXIT SIGN IN CABIN WOULD NOT ILLUMINATE IN EMERGENCY LGT MODE. MAINTNENACE REPLACED THE EXIT SIGN ASSEMBLY AND OPERATIONAL CHECKS WERE GOOD.
- [SDR ASOA20160424024](https://openairdocs.org/sdr/ASOA20160424024), Apr 24, 2016: LIGHT. INOPERATIVE. THE CREW REPORTED THE EMERGENCY LIGHT MID SECTION CEILING LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EXIT ROW FORWARD EMERGENCY LIGHT. OPS CH
- [SDR ASOA20160310010R](https://openairdocs.org/sdr/ASOA20160310010R), Mar 10, 2016: LIGHT. MALFUNCTIONED. THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 18 WAS INOPERATIVE. THE SYSTEM WAS RESET AND OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150831049](https://openairdocs.org/sdr/ASOA20150831049), Aug 31, 2015: LIGHT. UNKNOWN. THE CREW REPORTED EXIT LIGHT ABOVE EXIT ROW WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPS CHECKS OF THE EMERGENCY LIGHTS. OPS CHECKS WERE GOOD.
- [SDR ASOA20150421100](https://openairdocs.org/sdr/ASOA20150421100), Apr 21, 2015: FITTING. CRACKED. DURING C-CK NR 1 ENGINE FWD LOWER YOKE FITTING CRACKED. R & R NR 1 ENGINE FWD LOWER YOKE FITTING IAW EC5450-01142. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150421099V](https://openairdocs.org/sdr/ASOA20150421099V), Apr 21, 2015: STRUCTURE. CORRODED. DURING C-CK. CARGO DOOR LOWER CUTOUT STRUCTURE IS CORRODED. R & R CARGO DOOR LOWER STRUCTURE IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150420098](https://openairdocs.org/sdr/ASOA20150420098), Apr 20, 2015: FLOOR SUPPORT. CORRODED. DURING C-CK. RT OMEGA BEAM HAS CORROSION AT FR 23. REPAIRED RT OMEGA BEAM IAW EC5320-02031. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150414097](https://openairdocs.org/sdr/ASOA20150414097), Apr 14, 2015: FRAME. CRACKED. DURING C-CHECK. FRAME 10 CRACKED UNDER RT DV WINDOW. REPAIRED FRAME 10 IAW SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140309035](https://openairdocs.org/sdr/ASOA20140309035), Mar 9, 2014: INVERTER. INOPERATIVE. DURING MX INSPECTION, THE NR 1 EMERGENCY LIGHT INVERTER WAS DISCOVERED INOPERATIVE. MX R & R NR 1 INVERTER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO 
- [SDR ASOA20130504147](https://openairdocs.org/sdr/ASOA20130504147), May 4, 2013: BEAM. CORRODED. DURING C-CHECK CARGO CUTOUT LOWER BEAM HAS CORROSION (LOCAL LEVEL 2) BETWEEN FRAMES 65-66. MX R & R CARGO LOWER CUTOUT BEAM AT FRAME 65-68 IAW SRM 51-40-02 AND 
- [SDR ASOA20130504146](https://openairdocs.org/sdr/ASOA20130504146), May 4, 2013: STRUCTURE. CORRODED. DURING C-CHECK CARGO DOOR FWD LWR INTERNAL CUTOUT CORRODED. MX PERFORMED REPAIR ON CARGO DOOR CUTOUT FWD SHEAR CLIP AT FRAME 65 IAW EC5320-01494. FOUND TO BE MA
- [SDR ASOA20130504145](https://openairdocs.org/sdr/ASOA20130504145), May 4, 2013: SKIN. DAMAGED. DURING C-CHECK FUSELAGE SKIN FRAMES 15-16 STRINGER 3R-4R HAS LIGHTNING STRIKE. MX PERFORMED REPAIR ON FUSELAGE SKIN AT FRAMES 15-16 STRINGERS 3R-4R IAW SRM 53-2
- [SDR ASOA20130504144](https://openairdocs.org/sdr/ASOA20130504144), May 4, 2013: SKIN. DAMAGED. DURING C-CHECK, FUSELAGE SKIN BETWEEN FRAMES 38-39, STRINGER 1R-3R HAS LIGHTNING STRIKE. MX PERFORMED REPAIR OF FUSELAGE SKIN BETWEEN FRAMES 38-39, STRINGER 1R-
- [SDR ASOA20130326024C](https://openairdocs.org/sdr/ASOA20130326024C), Mar 26, 2013: LIGHT. INOPERATIVE. DURING ROUTINE MX, THE EMERGENCY AISLE PATH LIGHT WAS FOUND INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT AND OPS CHECKED GOOD.
- [SDR ASOA20120813128](https://openairdocs.org/sdr/ASOA20120813128), Aug 11, 2012: LAMP. INOPERATIVE. EMERGENCY DOME LIGHT AFT OF OVER-WING CEILING EXIT INOPERATIVE. REPLACED BULB OPS CHECK GOOD ACFT, RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20120321033](https://openairdocs.org/sdr/ASOA20120321033), Mar 21, 2012: CHARGER. INOPERATIVE. DURING ROUTINE MX, THE NR 2 EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECKS WERE GOOD.
- [SDR C2XA11IA189](https://openairdocs.org/sdr/C2XA11IA189), Aug 31, 2011: UNKNOWN. MALFUNCTIONED. STL - FLIGHT 3150, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT POWER OFF. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND ALL
- [SDR C2XA11RI143](https://openairdocs.org/sdr/C2XA11RI143), Aug 25, 2011: SMOKE DETECTOR. DEFECTIVE. FLIGHT 2517 - MHT - FLIGHT CREW REPORTED LAV SMOKE DETECT SYSTEM WOULD NOT TEST. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECK 
- [SDR C2XA11TY095](https://openairdocs.org/sdr/C2XA11TY095), Jun 27, 2011: SKIN. CORRODED. CORROSION ON INTERIOR SKIN BETWEEN FRAMES 14-15, STRINGER 21L-19R. REMOVED AND REPLACED SKIN PANEL IAW EC5330-02440.
- [SDR C2XA11TY094](https://openairdocs.org/sdr/C2XA11TY094), Jun 26, 2011: FRAME. CORRODED. AFT FUSELAGE HAS CORROSION ON FRAME 80 UNDER THE APU GENERATOR "L" BAR GROUNDING ATTACHMENT POINT. BLENDED OUT DAMAGE, PERFORMED NDT- NO DEFECTS NOTED. CONTINUE
- [SDR C2XA11TY093](https://openairdocs.org/sdr/C2XA11TY093), Jun 25, 2011: GUIDE. WORN. TYS - A/C IN FOR C-CHECK WHEN INSPECTION FOUND THE RIGHT O/B ELEVATOR CABLE AND RIGHT I/B RUDDER CABLES CHAFING AGAINST THE TEFLON GUIDE AT FR39, STR 19R-21R. M
- [SDR C2XA11TY089](https://openairdocs.org/sdr/C2XA11TY089), Jun 20, 2011: STRUCTURE. CORRODED. CARGO DOOR CORRODED ON STRUCTURE FRAME 64 ADJACENT TO CUTOUT. INSTALLED DOUBLER IAW EC5320-01479 REPAIR 3.
- [SDR C2XA11TY059](https://openairdocs.org/sdr/C2XA11TY059), May 6, 2011: SKIN. DAMAGED. LT ELEVATOR L/E SKIN HAD A TEAR/CRACK OF 9MM FOUND IN UPPER TIP SKIN AT YH=3022. CUT OUT DAMAGED AREA, INSTALLED FILLER AND DOUBLER IAW ETD2011-145/02568.
- [SDR C2XA11TY057](https://openairdocs.org/sdr/C2XA11TY057), May 4, 2011: LIGHT. INOPERATIVE. LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB IAW EMB 145AMM 33-50-10, OPS CHECK GOOD.
- [SDR C2XA10IA169](https://openairdocs.org/sdr/C2XA10IA169), Jun 7, 2010: ADC. FAULTY. FLIGHT 2734 - DURING CRUISE AT 36,000 FEET THE CAPTAIN'S AIRSPEED INDICATION STUCK AT 215 KIAS FOR 10 TO 15 MINUTES. AT THAT TIME THE STANDBY AND FIRST OFFICER'
- [SDR C2XA09CL112](https://openairdocs.org/sdr/C2XA09CL112), Sep 4, 2009: LIGHT. MALFUNCTIONED. CLE FLIGHT 2915 THE CREW REPORTED THE LEFT OVERWING EMERGENCY EXIT LIGHT BECOMES ILLUMINATED AFTER NORMAL AIRCRAFT SHUT DOWN. AFTER 7TH POWER DOWN THE LIGHT SEE
- [SDR C2XA09SH236](https://openairdocs.org/sdr/C2XA09SH236), Aug 1, 2009: CROSSBEAM. CORRODED. SHV - DURING C-CHECK CROSSBEAM BETWEEN LT AND CENTER OMEGA BEAM AT FRAME 20 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CROSSBEAM AT FRAME 20 IAW
- [SDR C2XA09SH235](https://openairdocs.org/sdr/C2XA09SH235), Aug 1, 2009: BRACKET. CORRODED. SHV - DURING C-CHECK CROSSBEAM L-BRACKET AT FRAME 23 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CROSSBEAM L-BRACKET AT FRAME 23 IAW EMB-145
- [SDR C2XA09SH234](https://openairdocs.org/sdr/C2XA09SH234), Aug 1, 2009: SILL. CORRODED. SHV - DURING C-CHECK RT FLOOR SILL FRAME 42-47 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED RT FLOOR SILL AT FRAME 42-47 IAW EMB-145 SRM 51-40-02.
- [SDR C2XA09SH233](https://openairdocs.org/sdr/C2XA09SH233), Aug 1, 2009: SILL. CORRODED. SHV - DURING C-CHECK SERVICE DOOR CENTER SILL HAS CORRODED NUT PLATES AT FRAMES 20-22. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR CENTER SILL NUT PLATES IAW 
- [SDR C2XA09SH232](https://openairdocs.org/sdr/C2XA09SH232), Aug 1, 2009: SILL. CORRODED. SHV - DURING C-CHECK SERVICE DOOR FORWARD SILL HAS CORROSION (LEVEL 2 WIDESPREAD). MAINTENANCE PERFORMED REPAIR OF SERVICE DOOR FORWARD SILL IAW SRM 51-10-03 AN
- [SDR C2XA09SH231](https://openairdocs.org/sdr/C2XA09SH231), Aug 1, 2009: PLATE. CORRODED. SHV - DURING C-CHECK SHELL PLATE AT FRAME 22 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED SHELL PLATE AT FRAME 22 IAW EMB-145 SRM 51-40-02. THE AI
- [SDR C2XA09SH230](https://openairdocs.org/sdr/C2XA09SH230), Aug 1, 2009: PLATE. CORRODED. SHV - DURING C-CHECK SHELL PLATE AT FRAME 20 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED SHELL PLATE AT FRAME 20 IAW EMB-145 SRM 51-40-02. THE AI
- [SDR C2XA09SH229](https://openairdocs.org/sdr/C2XA09SH229), Aug 1, 2009: BUTTSTRAP. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM BUTTSTRAP FRAMES 20-22 HAS CORROSION (LEVEL 2 WIDESPREAD). MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM BUTTSTRAP A
- [SDR C2XA09SH228](https://openairdocs.org/sdr/C2XA09SH228), Aug 1, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM BUTTSTRAP HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 71. MAINTENANCE COMPLETED THE REMOVAL AND INSTALLATION OF NEW CENTER OME
- [SDR C2XA09SH227](https://openairdocs.org/sdr/C2XA09SH227), Aug 1, 2009: BEAM. CORRODED. SHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT BEAM CORRODED (LEVEL 2 WIDESPREAD) IN SEVERAL AREAS. MAINTENANCE PERFORMED AND COMPLETED INSTALLATION OF CARGO DOOR
- [SDR C2XA09SH226](https://openairdocs.org/sdr/C2XA09SH226), Aug 1, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK RT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAME 23. MAINTENANCE PERFORMED REPAIR IAW EMB-145 SRM 51-10-03 AND CPM 51-20-06. THE AIRCRAFT WA
- [SDR C2XA09SH225](https://openairdocs.org/sdr/C2XA09SH225), Aug 1, 2009: FRAME. CORRODED. SHV - DURING C-CHECK RT CARGO FRAME 61 CORRODED (LEVEL 2 LOCAL) AT 15R BEHIND CARBON BEAM. MAINTENANCE PERFORMED REPAIR IAW IC2009-145/05601. THE AIRCRAFT WAS R
- [SDR C2XA09SH224](https://openairdocs.org/sdr/C2XA09SH224), Aug 1, 2009: SILL. CORRODED. SHV - DURING C-CHECK RT FLOOR SILL AT FRAME 69-73 HAS VARIOUS AREAS OF CORROSION (LEVEL 2 WIDESPREAD). MAINTENANCE REMOVED AND REPLACED NUT PLATES AND COMPLETED
- [SDR C2XA09SH223](https://openairdocs.org/sdr/C2XA09SH223), Aug 1, 2009: SILL. CORRODED. SHV - DURING C-CHECK RT FLOOR SILL AT FRAME 61-66 HAS CORROSION (LEVEL 2 WIDESPREAD) ON SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED NUT PLATES AND COMPLETED

All 96: https://openairdocs.org/aircraft/N13989/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/N13989/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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