# N17984: 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: 145246
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 8, 2000
- Certificate issued: August 18, 2022
- Expires: August 31, 2029
- Mode S code: A13E29
- 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=17984
- Page: https://openairdocs.org/aircraft/N17984

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/N17984/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 N17984.

## FAA accident and incident reports

None matched to N17984.

## Service difficulty reports (72, 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 ASOA201909063045](https://openairdocs.org/sdr/ASOA201909063045), Sep 6, 2019: LIGHT. INOPERATIVE. THE CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHT STRIP @ ROW 10 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHT STRIP AT ROW 10.
- [SDR ASOA201905077042](https://openairdocs.org/sdr/ASOA201905077042), May 4, 2019: TRUNNION. CRACKED. RT AFT MLG TRUNNION CRACKED. REMOVED AND REPLACED RT AFT MLG TRUNNION. AIRCRAFT STILL IN C CHECK.
- [SDR ASOA201905037041](https://openairdocs.org/sdr/ASOA201905037041), May 3, 2019: STRUCTURE. GOUGED. TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE APU FIREWALL MOUNTING STRUCTURE AT THE 06:00 POSITION WITH A GOUGE AND POSSIBLE CRACK. MAINTENANCE BLENDED OUT T
- [SDR ASOA201905167047](https://openairdocs.org/sdr/ASOA201905167047), Apr 29, 2019: SKIN. CRACKED. EXTERIOR SKIN CRACKED AT FRAME 75 STRINGER 2L. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLERS. AIRCRAFT WAS IN C CHECK AND IS NOW RELEASED AND RET
- [SDR ASOA201905017040](https://openairdocs.org/sdr/ASOA201905017040), Apr 29, 2019: STRINGER. CRACKED. STRINGER 2L CRACKED AT FRAME 75. CUT OUT DAMAGED AREA AND INSTALLED J-SECTION PER ETD2019-145-055731. AIRCRAFT STILL IN C CHECK.
- [SDR ASOA201904237037](https://openairdocs.org/sdr/ASOA201904237037), Apr 23, 2019: SKIN. CRACKED. A/C IS IN C-CHECK WHEN INSPECTION FOUND THE EXTERIOR SKIN CRACKED AT FRAME 75,STRINGER 2R. MAINTENANCE REPAIRED THE SKIN AT FRAME 75 IAW EMB SRM 53-31-01 REF. F
- [SDR ASOA201808231054](https://openairdocs.org/sdr/ASOA201808231054), Aug 21, 2018: ENGINE. ODOR. THE CREW REPORTED A STRONG OIL ODOR FROM THE PACKS AFTER TAKEOFF. MAINTNENACE INSPECTED AND REPLACED THE NR 1 ENGINE IAW TASK CARD 6271001. OPS CHECKED GOOD.
- [SDR ASOA201705043132](https://openairdocs.org/sdr/ASOA201705043132), May 4, 2017: CHANNEL. CORRODED. SERVICE DOOR LOWER CHANNEL CORRODED AROUND ANCHOR NUTS. SERVICE DOOR LOWER CHANNEL REPLACED IAW SRM 51-40-02.
- [SDR ASOA201705033130](https://openairdocs.org/sdr/ASOA201705033130), May 3, 2017: BEAM. CORRODED. CARGO DOOR SURROUND STRUCTURE, LOWER BEAM FOUND CORRODED. OUT OF TOLERANCE. THE LOWER BEAM WAS REPLACED IAW SRM 51-40-02.
- [SDR ASOA201705033129](https://openairdocs.org/sdr/ASOA201705033129), May 3, 2017: DOOR FRAME. CORRODED. CORROSION ON PAX DOOR LOWER FRAME AROUND NUT PLATE HOLES. REPAIRED IAW ETD 2017-145-035391.
- [SDR ASOA201705013126](https://openairdocs.org/sdr/ASOA201705013126), May 1, 2017: CHANNEL. CRACKED. RIGHT CHANNEL CRACKED ON FORWARD PRESSURE BULKHEAD IN NOSE WHEEL WELL. THE CHANNEL WAS REPLACED IAW SRM 51-40-02.
- [SDR ASOA201705013125](https://openairdocs.org/sdr/ASOA201705013125), May 1, 2017: SUPPORT. CORRODED. SURFACE CORROSION FOUND ON WASTE DRAIN VALVE SUPPORT. WASTE DRAIN VALVE SUPPORT REPLACED IAW SRM 51-40-02.
- [SDR ASOA201705013124](https://openairdocs.org/sdr/ASOA201705013124), May 1, 2017: FLOORBEAM. CORRODED. FLOORBEAM CORRODED UNDER GUSSET AROUND ANCHOR NUT. THE FLOORBEAM WAS REPAIRED IAW SRM 53-24-10, PAR 3, FIG 202, SHEET 3.
- [SDR ASOA201704283123](https://openairdocs.org/sdr/ASOA201704283123), Apr 28, 2017: ANGLE. CRACKED. COCKPIT LEFT FRAME 10, UPPER ANGLE CRACKED. ANGLE REPLACED IAW SRM 51-40-02.
- [SDR ASOA201704283122](https://openairdocs.org/sdr/ASOA201704283122), Apr 28, 2017: SHEAR TIE. CORRODED. CARGO DOOR SURROUND STRUCTURE SHEAR TIE CORRODED AT FRAME 65. THE SHEAR TIE WAS REPAIRED IAW SRM 53-31-04, STEP 4F.
- [SDR ASOA201704203094](https://openairdocs.org/sdr/ASOA201704203094), Apr 20, 2017: CROSSBEAM. CRACKED. NLG UPLOCK AFT CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.
- [SDR ASOA201704203093](https://openairdocs.org/sdr/ASOA201704203093), Apr 20, 2017: CROSSBEAM. CRACKED. NLG UPLOCK FORWARD CROSSBEAM CRACKED. FORWARD CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.
- [SDR ASOA20151021083H](https://openairdocs.org/sdr/ASOA20151021083H), Oct 21, 2015: FIREWALL. CRACKED. DURING MAINTENANCE INSPECTION, A CRACK WAS FOUND IN THE APU FIREWALL AT APPROXIMATELY THE 2 O'CLOCK POSITION NEAR AN EXISTING DOUBLER. MAINTENANCE REMOVED THE E
- [SDR ASOA20150421024C](https://openairdocs.org/sdr/ASOA20150421024C), Apr 21, 2015: INVERTER. INOPERATIVE. THE CREW REPORTED EMERGENCY LIGHTS ON FLOOR BETWEEN ROWS 2-8 AND EXIT SIGN BY MAIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY L
- [SDR ASOA20130901102](https://openairdocs.org/sdr/ASOA20130901102), Sep 1, 2013: COMPUTER. SHORTED. ELECTRICAL ODOR REPORTED IN COCKPIT WITH TERRAIN MESSAGE ON EICAS. MX R & R THE EGPWS COMPUTER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVIC
- [SDR ASOA20130731086](https://openairdocs.org/sdr/ASOA20130731086), Jul 31, 2013: BRACKET. UNSECURE. MX REPORTED THE MAIN CABIN DOOR WOULD NOT OPEN. MX SECURED THE MAIN DOOR HANDLE BRACKET. OPS CHECK OF THE MAIN DOOR SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO 
- [SDR ASOA20130730085](https://openairdocs.org/sdr/ASOA20130730085), Jul 30, 2013: GROUND STUD. DAMAGED. MX REPORTED THE EMERGENCY LIGHTS CAME ON WITH THE CEILING AND SIDEWALL LIGHTS ACTIVATION AND LIGHTS IN ARM POSITION. MX FOUND GROUND STUD GS8008DC TO HAVE BAD G
- [SDR ASOA20130726082](https://openairdocs.org/sdr/ASOA20130726082), Jul 26, 2013: BATTERY PACK. DISCHARGED. PILOT REPORTED EMERGENCY LIGHTS INOPERATIVE. MX R & R THE NR 3 AND NR 4 EMERGENCY LIGHT SYS BATTERY PACKS WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETUR
- [SDR ASOA20121230124](https://openairdocs.org/sdr/ASOA20121230124), Dec 30, 2012: SENSOR. FAULTY. FLIGHT DIVERTED, CREW REPORTED NR 1 ENGINE OIL PRESSURE IN FLIGHT FLUCTUATED BETWEEN 98-151 PSI. CREW SHUTDOWN ENGINE IN FLIGHT. MX R & R NR1 ENGINE OIL PRESSUR
- [SDR ASOA20121015150](https://openairdocs.org/sdr/ASOA20121015150), Oct 11, 2012: INVERTER. INOPERATIVE. EMERGENCY LIGHT FLOOR STRIPS NR 2 & 3 INOPERATIVE. R & R NR 3 INVERTER. OPS CHECK GOOD ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20120918077](https://openairdocs.org/sdr/ASOA20120918077), Sep 18, 2012: INVERTER. INOPERATIVE. DURING ROUTINE INSPECTION, MX THE FORWARD 3 EMERGENCY AILSE PATH LIGHT STRIPS WERE INOPERATIVE. MX REPLACED THE NR 2 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.
- [SDR ASOA20120504043](https://openairdocs.org/sdr/ASOA20120504043), May 4, 2012: FAN. ODOR. CREW REPORTED AN ELECTRICAL ODOR. INSPECTED AVIONICS BAY AND FOUND RECIRCULATION FANS INOPERATIVE. THE SYS WAS RESET AND OPS CHECKED GOOD. NO ELECTRICAL ODOR WA
- [SDR C2XA11IA160](https://openairdocs.org/sdr/C2XA11IA160), Jul 25, 2011: LIGHT. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE AFT AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERA
- [SDR C2XA11CL148](https://openairdocs.org/sdr/C2XA11CL148), Jun 20, 2011: INVERTER. FAULTY. DURING ROUTINE MAINTENANCE THE OVERHEAD EMERGENCY EXIT SIGN AT THE OVERWING ESCAPE HATCH WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT IN
- [SDR C2XA11SH073](https://openairdocs.org/sdr/C2XA11SH073), Mar 26, 2011: FITTING. LOOSE. SHV - DURING C-CHECK VERTICAL STAB SPAR 1 ATTACHMENT AT FRAME 75 SHOWS SIGNS OF MOVEMENT AT O/B AREAS (INSIDE AFT AVIONICS BAY). MAINTENANCE PERFORMED REPAIR OF
- [SDR C2XA11SH072](https://openairdocs.org/sdr/C2XA11SH072), Mar 26, 2011: STRUCTURE. DAMAGED. SHV - DURING C-CHECK CARGO DOOR INNER STRUCTURE BELOW FWD PULLEY HAS MISS DRILL DAMAGE. MAINTENANCE PERFORMED REPAIR ON CARGO DOOR INNER STRUCTURE AND RESTORED 
- [SDR C2XA11SH071](https://openairdocs.org/sdr/C2XA11SH071), Mar 26, 2011: HINGE. GOUGED. SHV - DURING C-CHECK RUDDER II LOWER CENTER HINGE HAS A GOUGE. MAINTENANCE REMOVED AND REPLACED RUDDER II LOWER CENTER HINGE IAW EC5540-01028 REV ORIG. THE AIRC
- [SDR C2XA11SH070](https://openairdocs.org/sdr/C2XA11SH070), Mar 23, 2011: DOOR FRAME. CORRODED. SHV - DURING C-CHECK SERVICE DOOR AFT CUTOUT HAS CORROSION AT LOWER NUT PLATE HOLE. REPAIRED FRAME IAW EC5310-01548. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE
- [SDR C2XA11SH069](https://openairdocs.org/sdr/C2XA11SH069), Mar 23, 2011: FRAME. CORRODED. SHV - DURING C-CHECK FRAME 65 HAS AREAS OF CORROSION. REPAIRED FRAME IAW EC5310-01505. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10CL169](https://openairdocs.org/sdr/C2XA10CL169), Nov 13, 2010: COMPUTER. FAULTY. EWR FLT 2940 THE CREW REPORTED GLIDESLOPE ISSUES GOING INTO DTW. REPORTED A 1/2 DOT DIFFERENCE BETWEEN GLIDESLOPE INDICATIONS DURING CAT II GS COMPARATIVE. THE 
- [SDR C2XA09IA272](https://openairdocs.org/sdr/C2XA09IA272), Oct 27, 2009: SEALANT. ODOR. IAH - FLIGHT 2886, THE CREW REPORTED A BURNING SMELL WHILE TAXIING IN AND WAS STRONGER IN INTENSITY AS THE PARKING BRAKE WAS SET, AND WAS FOUND TO BE STRONGER I
- [SDR C2XA09SH070](https://openairdocs.org/sdr/C2XA09SH070), Mar 1, 2009: DOOR FRAME. CORRODED. SHV - DURING C-CHECK CARGO DOOR CUTOUT LWR BEAM AREA CORRODED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED CARGO DOOR LOWER BEAM IAW EMB-145 SRM 51-40-02
- [SDR C2XA07CL093](https://openairdocs.org/sdr/C2XA07CL093), Nov 3, 2007: UPLOCK. FAULTY. CLE FLIGHT 2251 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE WARNING IN FLIGHT. THE AIRCRAFT DIVERTED TO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE I
- [SDR C2XA07RI069](https://openairdocs.org/sdr/C2XA07RI069), Aug 16, 2007: LIGHT. INOPERATIVE. RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND CEILING EMERGENCY LIGHTS AT ROW 3 AND ROW 14 INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULBS IAW EMB145 AMM 33-
- [SDR C2XA07IA131](https://openairdocs.org/sdr/C2XA07IA131), Jun 5, 2007: PROXIMITY SWITCH. INOPERATIVE. IAH - FLIGHT 2598, THE CREW REPORTED A LOUD NOISE AND VIBRATION IN THE NOSE ARE DURING CRUISE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REM
- [SDR C2XA07IA120](https://openairdocs.org/sdr/C2XA07IA120), May 18, 2007: BRAKE ASSY. MALFUNCTIONED. IAH - FLIGHT 2528, THE CREW REPORTED A -BRK OUTBD- MESSAGE ON EICAS ON FINAL APPROACH, AND THAT THE OUTBOARD BRAKES DID NOT WORK ON ROLLOUT. MAINTENANCE INSPECT
- [SDR C2A07SH028](https://openairdocs.org/sdr/C2A07SH028), May 13, 2007: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CORROSION ON CENTER OMEGA BEAM FROM FR 20 TO 23. MX REMOVED AND REPLACED CENTER OMEGA BEAM FROM FR 18-23 IAW EMB 145 SRM 51-40-02. THE AIRC
- [SDR C2XA06CL063](https://openairdocs.org/sdr/C2XA06CL063), Jun 27, 2006: PROXIMITY SWITCH. FAULTY. CLE FLIGHT 3245 THE CREW REPORTED LOUD NOISE FROM NOSE GEAR AREA DURING CLIMBOUT ABOVE 1700 AND DURING FLIGHT. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOO
- [SDR C2XA05RI017](https://openairdocs.org/sdr/C2XA05RI017), Aug 8, 2005: WIRE HARNESS. BURNED. FLT 2969 - RIC - PRE-FLIGHT - DURING PRE-FLIGHT INSPECTION, SIDE WALL LIGHT AT SEAT 2A WAS SMOKING. RIC MAINTANACE REMOVED AND REPLACED LAMP HARNESS ASSY AND PE
- [SDR C2XA05SH041](https://openairdocs.org/sdr/C2XA05SH041), May 23, 2005: FLOOR SUPPORT. CORRODED. DURING C CHECK, PREVIOUS REPAIR TO LT OMEGA BEAM AT FS 20 WAS FOUND TO BE CORRODED. MX REMOVED DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 51-40
- [SDR C2XA05SH042](https://openairdocs.org/sdr/C2XA05SH042), May 23, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE RT OMEGA BEAM NUT PLATE IS CORRODED JUST AFT OF FRAME 23. MAINTENANCE INSTALLED HAT BEAM REPAIR ON RT OMEGA BEAM AT NUT PLATE HOLE AFT 
- [SDR C2XA05RI001](https://openairdocs.org/sdr/C2XA05RI001), Jan 13, 2005: LIGHT. BURNED OUT. RIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY LIGHT FLOOR STRIP, BY SEAT 6A, INOP. MAINTENANCE REMOVED AND REPLACED STRIP. OPERATIONAL CHECK WAS 
- [SDR C2XA04BT091](https://openairdocs.org/sdr/C2XA04BT091), Aug 15, 2004: ODOR. DETECTED. CREW REPORTED, (STRONG FUEL ODOR IN AIRCRAFT WHILE APU IS RUNNING.) MAINTENANCE TROUBLESHOT NO DEFECTS FOUND AND PLACED THE AIRCRAFT ON MEL FOR FURTHER FOLLOWUP
- [SDR C2XA03TY073](https://openairdocs.org/sdr/C2XA03TY073), May 20, 2003: ANGLE. CORRODED. DURING A SCHEDULED INSPECTION THE LOWER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE LOWER RAMP ANGLE 
- [SDR C2XA03TY072](https://openairdocs.org/sdr/C2XA03TY072), May 20, 2003: ANGLE. CORRODED. DURING A SCHEDULED INSPECTION THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE CENTER RAMP A

All 72: https://openairdocs.org/aircraft/N17984/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/N17984/stcs.md

## Earlier aircraft with N17984

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N17984 before.

- [Cancelled 1951-11-02](https://openairdocs.org/deregistered/N17984-1951-11-02): Piper J-2, S/N 1584, built 1937. Owner: [Hall A W](https://openairdocs.org/faa-owner/HALL%20A%20W), [Asheville, NC](https://openairdocs.org/faa-place/NC/Asheville)

## 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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