# N15983: 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 AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 145239
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 24, 2000
- Certificate issued: August 18, 2022
- Expires: August 31, 2029
- Mode S code: A0EF2A
- 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=15983
- Page: https://openairdocs.org/aircraft/N15983

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

## ADs that may apply (OpenAirDocs): 104 in force

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

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

### Matched by engine (Allison AE-3007A)

- [AD 2020-16-13](https://openairdocs.org/ad/2020-16-13): Turbine Engine Compressor Section · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Aug 14, 2020
- [AD 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018
- [AD 2013-26-06](https://openairdocs.org/ad/2013-26-06): High-pressure turbine (HPT) stage 2 wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Feb 7, 2014
- [AD 2011-22-03](https://openairdocs.org/ad/2011-22-03): Low-cycle fatigue cracks · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 4 more. Effective Nov 17, 2011
- [AD 2007-24-05](https://openairdocs.org/ad/2007-24-05): Engine oil temperature · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 8 more. Effective Jan 2, 2008
- [AD 2004-04-05](https://openairdocs.org/ad/2004-04-05): Engine oil system · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Mar 9, 2004
- [AD 2001-25-05](https://openairdocs.org/ad/2001-25-05): Compressor Cone Shafts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jan 23, 2002
- [AD 2001-19-03](https://openairdocs.org/ad/2001-19-03): High Pressure Turbine 1st to 2nd Stage Turbine Spacer · Rolls-Royce AE 3007A and AE 3007C. Effective Oct 29, 2001
- [AD 2001-17-31](https://openairdocs.org/ad/2001-17-31): Second Stage High Pressure Turbine Wheel · Rolls-Royce AE 2100A, AE 2100C, AE 2100D3 and 2 more. Effective Oct 5, 2001
- [AD 2000-18-06](https://openairdocs.org/ad/2000-18-06): Digital Electronic Controls · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 22, 2000
- [AD 2000-13-01](https://openairdocs.org/ad/2000-13-01): Turbine Wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 1, 2000
- [AD 2000-11-22](https://openairdocs.org/ad/2000-11-22): Critical Life-Limited Parts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Aug 7, 2000
- [AD 99-03-03](https://openairdocs.org/ad/99-03-03): Full Authority Digital Engine Control (FADEC) · Rolls-Royce AE 3007A and AE 3007A1/1. Effective Feb 16, 1999
- [AD 98-11-32](https://openairdocs.org/ad/98-11-32): Sump Magnetic Chip Collector Plug · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Jun 18, 1998

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

- [AD 2008-13-14](https://openairdocs.org/ad/2008-13-14) (historical): Fuel system limitations (FSL) · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jul 30, 2008
- [AD 2007-12-17](https://openairdocs.org/ad/2007-12-17) (historical): Metallic tubes enclosing the vent and pilot valve wires · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Jul 19, 2007
- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 2006-20-08](https://openairdocs.org/ad/2006-20-08) (historical): Rod ends of aileron power control actuator, superseding AD 99-05-04 · Embraer EMB-145, EMB-145EP, EMB-145ER and 4 more. Effective Nov 8, 2006
- [AD 2006-04-02](https://openairdocs.org/ad/2006-04-02) (historical): Pitot static heating relay K0057 · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Mar 31, 2006
- [AD 2005-26-15](https://openairdocs.org/ad/2005-26-15) (historical): Certain components of the elevator control system · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 8 more. Effective Feb 3, 2006
- [AD 2005-25-04](https://openairdocs.org/ad/2005-25-04) (historical): Tail section or rudder pedals · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Dec 23, 2005
- [AD 2001-17-04](https://openairdocs.org/ad/2001-17-04) (historical): Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Sep 5, 2001
- [AD 2000-04-09](https://openairdocs.org/ad/2000-04-09) (historical): Elevator Servo Tab and Spring Tab Hinge Fittings of the Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Mar 10, 2000
- [AD 2010-19-01](https://openairdocs.org/ad/2010-19-01) (historical): High pressure turbine · Rolls-Royce AE 3007A. Effective Oct 27, 2010
- [AD 2009-08-51](https://openairdocs.org/ad/2009-08-51) (historical): High-pressure turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 6 more. Effective May 27, 2009
- [AD 2008-26-06](https://openairdocs.org/ad/2008-26-06) (historical): High-pressure turbine (HPT) · AE 3007A. Effective Jan 8, 2009
- [AD 2008-19-51](https://openairdocs.org/ad/2008-19-51) (historical): AE 3007A, AE 3007A1, AE 3007A1E and 5 more
- [AD 2001-08-15](https://openairdocs.org/ad/2001-08-15) (historical): Oil System · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective May 14, 2001
- [AD 2000-09-05](https://openairdocs.org/ad/2000-09-05) (historical): Cone Shafts · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jul 5, 2000
- [AD 99-02-51](https://openairdocs.org/ad/99-02-51) (historical): Starter Shaft Seal · AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Apr 20, 1999

All 120: https://openairdocs.org/aircraft/N15983/ads.md

## Information bulletins (advisory) (8 in force)

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

## NTSB investigations

None matched to N15983.

## FAA accident and incident reports

None matched to N15983.

## Service difficulty reports (87, 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 ASOA201902167027](https://openairdocs.org/sdr/ASOA201902167027), Feb 15, 2019: RIB. CRACKED. RT WING RIB 21 CRACKED. TRIMMED OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER. AIRCRAFT STILL IN C CHECK.
- [SDR ASOA201812067188](https://openairdocs.org/sdr/ASOA201812067188), Dec 4, 2018: SOCKET. INOPERATIVE. MAIN CABIN DOOR EMERGENCY LIGHT OUT. REMOVED AND REPLACED MAIN CABIN DOOR EMERGENCY LIGHT SOCKET IAW AMM 33-50-06.
- [SDR ASOA201705305081](https://openairdocs.org/sdr/ASOA201705305081), May 30, 2017: DISPLAY. SHORTED. MFD NR 2 WENT BLANK AT THE SAME TIME AS AN ELECTRICAL BURNING ODOR. MX REMOVED AND REPLACED NR 2 MFD WITH OPERATIONAL CHECKED GOOD. ACFT WAS APPROVED FOR RETURN
- [SDR ASOA201704083082](https://openairdocs.org/sdr/ASOA201704083082), Apr 8, 2017: LIGHT. INOPERATIVE. THE CREW REPORTED FORWARD FLOOR EMERGENCY LIGHT INOPERATIVE.
- [SDR ASOA201704083070](https://openairdocs.org/sdr/ASOA201704083070), Apr 8, 2017: BATTERY. INOPERATIVE. THE CREW REPORTED FORWARD FLOOR EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.
- [SDR ASOA20160427013](https://openairdocs.org/sdr/ASOA20160427013), Apr 25, 2016: SKIN. DENTED. DENT LOCATED BETWEEN FRAME 19 AND FRAME 20 AT STR 15L AND 16L. CUTOUT DAMAGED SECTION FABRICATED FILLER AND DOUBLER, INSTALLED AND REFINISHED. ACFT RELEASED AND
- [SDR ASOA20151030063](https://openairdocs.org/sdr/ASOA20151030063), Oct 30, 2015: SKIN. DENTED. GROUND PERSONAL REPORTED DENT DAMAGE AROUND RT REAR AREA OF ACFT FUSELAGE BETWEEN STRINGERS 18R & 19R AND FRAMES 62 & 63A. MAINTENANCE INSPECTED AND PERFORMED R
- [SDR ASOA20141105318](https://openairdocs.org/sdr/ASOA20141105318), Nov 5, 2014: PROFILE. CORRODED. DURING C-CHECK, CARGO DOOR INNER L PROFILE IS CORRODED AROUND NUTPLATES. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW SRM 51-40-02 A.
- [SDR ASOA20141105317](https://openairdocs.org/sdr/ASOA20141105317), Nov 5, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, LT OMEGA BEAM FLANGE CORRODED AT FRAME 23. REPAIRED IAW EC5320-01984. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140922107](https://openairdocs.org/sdr/ASOA20140922107), Sep 22, 2014: SMOKE DETECTOR. FAULTY. PILOT REPORTED A LAV SMOKE MASTER WARNING ON THE EICAS DURING FLIGHT. OCCURED TWICE FOR APPOXIMATELY 10 SECONDS EACH TIME. MX R & R THE LAVATORY SMOKE SENSOR, O
- [SDR ASOA20140612069](https://openairdocs.org/sdr/ASOA20140612069), Jun 12, 2014: UNKNOWN. ODOR. CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE FLIGHT DECK AND TOWARDS REAR OF ACFT DURING ARRIVAL. ALSO NOTED THE ACFT WAS VERY WARM WITH THE PACKS TO FULL CO
- [SDR ASOA20140518042](https://openairdocs.org/sdr/ASOA20140518042), May 18, 2014: BRAKE ASSY. WORN. THE CREW REPORTED BRAKES COULD NOT BE APPLIED FULL, GRAB HARD AND RELEASE AND PULL LEFT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BRAKE ASSEMBLY. OPS CHECKED
- [SDR ASOA20140502039](https://openairdocs.org/sdr/ASOA20140502039), May 2, 2014: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE THE AFT AISLE PATH EMERGENCY LIGHT STRIP WOULD NOT TEST. MAINTENANCE REPLACED THE LIGHT STRIP AND OPS CHECKS WERE GOOD.
- [SDR ASOA20130107208](https://openairdocs.org/sdr/ASOA20130107208), Jan 6, 2013: LIGHT. INOPERATIVE. MAIN PAX DOOR EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT ASSY. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20120530050](https://openairdocs.org/sdr/ASOA20120530050), May 30, 2012: SIGN. INOPERATIVE. DURING ROUTINE MX, THE LT SIDEWALL EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX REPLACED THE LT SIDEWALL EMERGENCY EXIT SIGN. OPS CHECKED GOOD.
- [SDR ASOA20120314023](https://openairdocs.org/sdr/ASOA20120314023), Mar 14, 2012: CHECK VALVE. TORN. FLT 4566. DURING TAKEOFF, A SMALL FUEL LEAK WAS REPORTED FROM THE LT WING. CREW PERFORMED AIR RETURN BACK AS PRECAUTION WITHOUT INCIDENT. MX FOUND DEBRIS AND TH
- [SDR C2XA11IA167](https://openairdocs.org/sdr/C2XA11IA167), Jul 27, 2011: BATTERY. DISCHARGED. MCI - DURING MAINTENANCE INSPECTION THE NUMBER TWO EMERGENCY LIGHT BATTERY WAS FOUND TO BE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY
- [SDR C2XA11RI027](https://openairdocs.org/sdr/C2XA11RI027), Feb 20, 2011: LIGHT. INOPERATIVE. RIC - DURING ROUTINE MAINTENANCE, INSPECTION FOUND EMERGENCY LIGHT FLOOR STRIP AT EMERGENCY EXIT (ROW 12) INOPERATIVE. RIC MX REMOVED AND REPLACED LIGHT STRIP A
- [SDR C2XA10CL200](https://openairdocs.org/sdr/C2XA10CL200), Dec 15, 2010: UNKNOWN. SMOKE. MCI FLT 3088 THE CREW REPORTED SMOKE IN THE CABIN DURING PACK 2 OPERATION.MAINTENANCE PERFORMED ENGINE 1 AND 2 RUNS WITH BLEED 1 AND 2 OPEN AND BOTH PACKS OPERA
- [SDR C2XA10IA332](https://openairdocs.org/sdr/C2XA10IA332), Dec 15, 2010: ENGINE. LEAKING. IAH - FLIGHT 2496, THE CREW REPORTED AN ACRID BURNING SMELL LIKE TIRES OR GUNPOWDER DESCENDING THROUGH FL270 THAT ONLY LASTED A FEW SECONDS, WITH NOTHING NOTICE
- [SDR C2XA10IA331](https://openairdocs.org/sdr/C2XA10IA331), Dec 15, 2010: UNKNOWN. SMOKE. MCI - FLIGHT 3088, DURING TAXI THE CREW REPORTED SMOKE IN THE CABIN DURING PACK 2 OPERATION, THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE A
- [SDR C2XA10SH420](https://openairdocs.org/sdr/C2XA10SH420), Dec 5, 2010: RIVET. LOOSE. SHV - DURING C-CHECK RT FUSELAGE HAS WORKING RIVETS BETWEEN FRAMES 75-80 (38 RIVETS). MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN RT SIDE FRAMES 75-80 IAW EMB
- [SDR C2XA10SH419](https://openairdocs.org/sdr/C2XA10SH419), Dec 5, 2010: RIVET. LOOSE. SHV - DURING C-CHECK LT FUSELAGE HAS WORKING RIVETS BETWEEN FRAMES 76-80 (23 RIVETS). MAINTENANCE PERFORMED REPAIR ON LT FUSELAGE SKIN FRAMES 76-80 IAW EC5330-0
- [SDR C2XA10SH418](https://openairdocs.org/sdr/C2XA10SH418), Dec 5, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK RT OMEGA BEAM IS CORRODED AT FRAME 23. MAINTENANCE PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 23 IAW EMB-145 EC5320-01443 REV C AND IAW EMB
- [SDR C2XA10SH417](https://openairdocs.org/sdr/C2XA10SH417), Dec 5, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM IS CORRODED (PNL 231FF) AND RAMP ANGLE AT FRAME 20. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AND REMOVED AND REPLACED LT
- [SDR C2XA10SH416](https://openairdocs.org/sdr/C2XA10SH416), Dec 5, 2010: FITTING. CORRODED. SHV - DURING C-CHECK FUSELAGE FITTING-TO-VERTICAL STABILIZER SPAR ATTACHMENT BETWEEN FRAME 75 HAS INDICATION OF CORROSION AT TOP SKIN INTERFACE. MAINTENANCE REM
- [SDR C2XA10SH415](https://openairdocs.org/sdr/C2XA10SH415), Dec 5, 2010: SILL. CORRODED. SHV - DURING C-CHECK CARGO DOOR SILL HAS CORROSION. REMOVED AND REPLACED CARGO DOOR SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH414](https://openairdocs.org/sdr/C2XA10SH414), Dec 5, 2010: SILL. CORRODED. SHV - DURING C-CHECK SERVICE DOOR CENTER SILL HAS CORROSION REPAIRED SERVICE DOOR CENTER SILL IAW EMB 145 SRM 53-21-03. AIRCRAFT WAS APPROVED FOR RETURN TO SERV
- [SDR C2XA10SH413](https://openairdocs.org/sdr/C2XA10SH413), Dec 5, 2010: ATTACH FITTING. WORN. SHV - DURING C-CHECK RT GROUND SPOILER O/B ATTACHMENT FITTING HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT FITTING IAW EMB 145 SRM 51-20-03. AIRCRA
- [SDR C2XA10SH412](https://openairdocs.org/sdr/C2XA10SH412), Dec 5, 2010: ATTACH FITTING. WORN. SHV - DURING C-CHECK RT GROUND SPOILER I/B ATTACHMENT FITTING HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT FITTING IAW EMB 145 SRM 51-20-03. AIRCRA
- [SDR C2XA10SH411](https://openairdocs.org/sdr/C2XA10SH411), Dec 5, 2010: FLOOR SUPPORT. CORRODED. DURING C-CK. LT OMEGA BEAM HAS CORROSION AT FR 38. REPAIRED OMEGA BEAM IAW SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH410](https://openairdocs.org/sdr/C2XA10SH410), Dec 5, 2010: FLOOR SUPPORT. CORRODED. DURING C-CK. LT OMEGA BEAM HAS CORROSION AT FR 29. REPAIRED OMEGA BEAM IAW SRM 53-22-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH409](https://openairdocs.org/sdr/C2XA10SH409), Dec 5, 2010: FLOOR SUPPORT. CORRODED. DURING C-CK. LT OMEGA BEAM HAS CORROSION AT FR 24. REPAIRED OMEGA BEAM IAW SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH408](https://openairdocs.org/sdr/C2XA10SH408), Dec 5, 2010: FLOOR SUPPORT. CORRODED. DURING C-CK, CTR OMEGA BEAM HAS CORROSION AT FR 34. REPAIRED OMEGA BEAM IAW SRM 53-22-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH407](https://openairdocs.org/sdr/C2XA10SH407), Dec 5, 2010: FLOOR SUPPORT. CORRODED. DURING C-CK. CTR OMEGA BEAM HAS CORROSION AT FR 20. R & R OMEGA BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH402](https://openairdocs.org/sdr/C2XA10SH402), Nov 27, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 36-41. REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH399](https://openairdocs.org/sdr/C2XA10SH399), Nov 17, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK RT OMEGA BEAM IS CORRODED (LEVEL 2 LOCAL) AT FRAME 23. MAINTENANCE PERFORMED REPAIR OF RT OMEGA BEAM AT FRAME 23 IAW EMB-145 EC5320-01443 R
- [SDR C2XA10CL128](https://openairdocs.org/sdr/C2XA10CL128), Aug 6, 2010: CONNECTOR. LOOSE. CLE FLT 2537 THE CREW REPORTED A APU FIRE DETECT FAIL MESSAGE ON TAKEOFF ROLL. MAINTENANCE INSPECTED THE APU FIRE DETECTOR WIRE HARNESS AND SECURED A LOOSE CONN
- [SDR C2XA10IA209](https://openairdocs.org/sdr/C2XA10IA209), Jul 25, 2010: WIRE. CHAFED. SAV - FLIGHT 2312, THE CREW REPORTED ELECTRICAL SMOKE IN THE COCKPIT AND CABIN, AND ON SHORT FINAL AUTO PILOT FAILED, SECONDARY PITCH TRIM FAIL, THEN CA,& F/O M
- [SDR C2XA10IA208](https://openairdocs.org/sdr/C2XA10IA208), Jul 24, 2010: ICU. INOPERATIVE. SAV - FLIGHT 2312, THE CREW REPORTED ELECTRICAL SMOKE IN THE COCKPIT AND CABIN, AND ON SHORT FINAL AUTO PILOT FAILED, SECONDARY PITCH TRIM FAIL, THEN CA, & F/O 
- [SDR C2XA10RI045](https://openairdocs.org/sdr/C2XA10RI045), Mar 22, 2010: CONNECTOR. LOOSE. FLIGHT 2612 - EWR - FLIGHT CREW REPORTED APU FIRE DETECTION SYSTEM FAIL MESSAGE ON EICAS. EWR MX RE-SECURED LOOSE CONNECTOR ON APU FIRE LOOP AND PERFORMED OPERA
- [SDR C2XA10RI012](https://openairdocs.org/sdr/C2XA10RI012), Jan 12, 2010: INVERTER. INOPERATIVE. EWR - DURING ROUTINE MAINTENANCE, EWR MX FOUND EMERGENCY LIGHT OVER RIGHT WING EXIT DOOR INOPERATIVE. MX REMOVED AND REPLACED INVERTER AND PERFORMED OPERATIONAL
- [SDR C2XA09RI182](https://openairdocs.org/sdr/C2XA09RI182), Oct 23, 2009: HYDRAULIC SYSTEM. LOW. FLIGHT 2138 - RIC - FLIGHT CREW DIVERTED FLIGHT TO RIC DUE TO HYDRAULIC 1 QUANTITY LOW MESSAGE AND FLUID LEVEL DECREASING. CREW LANDED ACFT UNEVENTFULLY. RIC MX
- [SDR C2XA09CL126](https://openairdocs.org/sdr/C2XA09CL126), Oct 1, 2009: WINDSHIELD. CRACKED. CLE FLT 2995 - THE CREW REPORTED THE CAPTAINS WINDSHIELD WAS CRACKED IN THE LOWER LEFT CORNER ABOUT 3-4 INCHES LONG. MAINTENANCE INSPECTED AND REPLACED THE WIND
- [SDR C2XA09CL005](https://openairdocs.org/sdr/C2XA09CL005), Jan 11, 2009: ECU. FAULTY. CLE FLIGHT NR 2841 THE CREW REPORTED A FLAP FAIL MSG ON THE EICAS ATTEMPTING TO RAISE THE FLAPS TO O AFTER TAKEOFF. INDICATION WAS 9 DEGRESS AND THE FLAP HANDLE
- [SDR C2XA09RI005](https://openairdocs.org/sdr/C2XA09RI005), Jan 5, 2009: CHARGER. INOPERATIVE. EWR MX - DURING ROUTINE MX, EWR MX FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE. MX R&R NR 1 EMERGENCY LIGHT BATTERY CHARGER AND PERFORMED OPS TEST SUCCESSFULLY. 
- [SDR C2XA09RI004](https://openairdocs.org/sdr/C2XA09RI004), Jan 5, 2009: CHARGER. INOPERATIVE. EWR MX - DURING ROUTINE MX, EWR MX FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE. MX R&R NR 2 EMERGENCY LIGHT BATTERY CHARGER AND PERFORMED OPS TEST SUCCESSFULLY. 
- [SDR C2XA09RI003](https://openairdocs.org/sdr/C2XA09RI003), Jan 5, 2009: BATTERY PACK. INOPERATIVE. DURING ROUTINE MX, MX FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE. MX REMOVED AND REPLACED NR2 EMERGENCY LIGHT BATTERY AND PERFORMED OPS TEST SUCCESSFULLY. ACFT 
- [SDR C2XA07IA225](https://openairdocs.org/sdr/C2XA07IA225), Oct 18, 2007: INVERTER. INOPERATIVE. IAH - FLIGHT 2455, THE CREW REPORTED THAT THE FORWARD CEILING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT I
- [SDR C2XA07RI017](https://openairdocs.org/sdr/C2XA07RI017), Apr 15, 2007: FLEX DUCT. DAMAGED. FLT 2987 - EWR - FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN COMING FROM FLOOR VENT BETWEEN ROWS 9-11. EWR MX FOUND NR 1 PACK DUCT TO BE OFF RECIRCULATE FAN AN

All 87: https://openairdocs.org/aircraft/N15983/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/N15983/stcs.md

## Earlier aircraft with N15983

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N15983 before.

- [Cancelled 1979-03-26](https://openairdocs.org/deregistered/N15983-1979-03-26): Piper PA-34-200, S/N 34-7350115, built 1973. Exported to Canada. Owner: [Aerosmith Denton Inc](https://openairdocs.org/faa-owner/AEROSMITH%20DENTON%20INC), [Denton, TX](https://openairdocs.org/faa-place/TX/Denton)

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/aircraft.md
- The Allison AE-3007A engine: https://openairdocs.org/engine/allison-ae-3007a.md

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