# N18120: 2003 Embraer EMB-145XR

- Status: Valid registration
- Airframe: [Embraer EMB-145XR](https://openairdocs.org/model/embraer-emb-145xr) (registry code 3260214, 55 seats)
- Engine: [Rolls-Royce AE3007 series](https://openairdocs.org/engine/rolls-royce-ae3007-series) (registry code 54582)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 145681
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2005
- Certificate issued: July 14, 2026
- Expires: July 31, 2033
- Mode S code: A1471A
- 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=18120
- Page: https://openairdocs.org/aircraft/N18120

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Rolls-Royce AE3007 model are included.

## ADs that may apply (OpenAirDocs): 95 in force

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

- [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 2017-09-09](https://openairdocs.org/ad/2017-09-09): Passenger Compartment Equipment · Boeing 717-200, MD-90-30, CL-600-2C10 (Regional Jet Series 700) and 17 more. Effective Jun 28, 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 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 2008-12-07](https://openairdocs.org/ad/2008-12-07): Fuel leakage · Embraer EMB-135BJ (Legacy 600) and EMB-145XR. Effective Jul 16, 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 2007-13-03](https://openairdocs.org/ad/2007-13-03): Ventral fuel tank · Embraer EMB-145XR. Effective Jul 25, 2007
- [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 2006-26-04](https://openairdocs.org/ad/2006-26-04): Passenger seat tracks · Embraer EMB-145XR. Effective Jan 31, 2007
- [AD 2006-21-04](https://openairdocs.org/ad/2006-21-04): Clear-ice indication lamp · Embraer EMB-135BJ (Legacy 600) and EMB-145XR. Effective Nov 17, 2006
- [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 2006-18-03](https://openairdocs.org/ad/2006-18-03): Flap system interface wiring · Embraer EMB-145XR. Effective Oct 4, 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

### Matched by engine (Rolls-Royce AE3007 series)

- [AD 2020-16-13](https://openairdocs.org/ad/2020-16-13): Turbine Engine Compressor Section · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Aug 14, 2020
- [AD 2018-17-04](https://openairdocs.org/ad/2018-17-04): Turbine section · Rolls-Royce AE 2100D2A, AE 2100D3 and AE 3007A2. Effective Sep 21, 2018
- [AD 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018
- [AD 2017-11-05](https://openairdocs.org/ad/2017-11-05): Turbine/ turboprop Engine, Turbine Section · Rolls-Royce AE 3007C and AE 3007C1. Effective Jul 18, 2017
- [AD 2015-02-08](https://openairdocs.org/ad/2015-02-08): Turbine wheels · Rolls-Royce AE 2100D2, AE 2100D2A, AE 2100D3 and 11 more. Effective Mar 11, 2015
- [AD 2013-26-06](https://openairdocs.org/ad/2013-26-06): High-pressure turbine (HPT) stage 2 wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Feb 7, 2014
- [AD 2011-22-03](https://openairdocs.org/ad/2011-22-03): Low-cycle fatigue cracks · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 4 more. Effective Nov 17, 2011
- [AD 2009-24-04](https://openairdocs.org/ad/2009-24-04): Fan spinner · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 5 more. Effective Dec 28, 2009
- [AD 2009-04-03](https://openairdocs.org/ad/2009-04-03): 2nd stage, 3rd stage, and 4th stage compressor wheels · Rolls-Royce AE 1107C and AE 3007A1E. Effective Mar 24, 2009
- [AD 2007-24-05](https://openairdocs.org/ad/2007-24-05): Engine oil temperature · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 8 more. Effective Jan 2, 2008
- [AD 2004-04-05](https://openairdocs.org/ad/2004-04-05): Engine oil system · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Mar 9, 2004
- [AD 2003-25-08](https://openairdocs.org/ad/2003-25-08): 1st and 2nd stage turbine spacers · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 3 more. Effective Jan 21, 2004
- [AD 2001-25-05](https://openairdocs.org/ad/2001-25-05): Compressor Cone Shafts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jan 23, 2002
- [AD 2001-19-03](https://openairdocs.org/ad/2001-19-03): High Pressure Turbine 1st to 2nd Stage Turbine Spacer · Rolls-Royce AE 3007A and AE 3007C. Effective Oct 29, 2001
- [AD 2001-17-31](https://openairdocs.org/ad/2001-17-31): Second Stage High Pressure Turbine Wheel · Rolls-Royce AE 2100A, AE 2100C, AE 2100D3 and 2 more. Effective Oct 5, 2001
- [AD 2000-18-06](https://openairdocs.org/ad/2000-18-06): Digital Electronic Controls · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 22, 2000
- [AD 2000-13-01](https://openairdocs.org/ad/2000-13-01): Turbine Wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 1, 2000
- [AD 2000-11-22](https://openairdocs.org/ad/2000-11-22): Critical Life-Limited Parts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Aug 7, 2000
- [AD 99-03-03](https://openairdocs.org/ad/99-03-03): Full Authority Digital Engine Control (FADEC) · Rolls-Royce AE 3007A and AE 3007A1/1. Effective Feb 16, 1999
- [AD 98-11-32](https://openairdocs.org/ad/98-11-32): Sump Magnetic Chip Collector Plug · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Jun 18, 1998

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

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

All 109: https://openairdocs.org/aircraft/N18120/ads.md

## Information bulletins (advisory) (10 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB AIR-20-17](https://openairdocs.org/saib/AIR-20-17): Air Conditioning - Cabin Pressure Control System. Issued Nov 3, 2020
- [SAIB NM-19-17](https://openairdocs.org/saib/NM-19-17): Ice and Rain Protection: Electrical Wiring Terminations at Pitot and TAT Relays. Issued Dec 5, 2019
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008
- [SAIB NM-08-15](https://openairdocs.org/saib/NM-08-15): Instruments: Contamination of the Attitude Heading Reference System (AHRS) Computers. Issued Mar 26, 2008
- [SAIB NM-07-40](https://openairdocs.org/saib/NM-07-40): Embraer EMB-135/145 Landing Gear Incident. Issued Jul 9, 2007
- [SAIB NM-07-20](https://openairdocs.org/saib/NM-07-20): Flight Data Recorders. Issued Mar 21, 2007
- [SAIB NE-11-22](https://openairdocs.org/saib/NE-11-22): Engine Controls. Issued Feb 23, 2011
- [SAIB CE-00-18](https://openairdocs.org/saib/CE-00-18): . Issued Mar 30, 2000
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N18120.

## FAA accident and incident reports

None matched to N18120.

## Service difficulty reports (92, 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 RAIA201907010001](https://openairdocs.org/sdr/RAIA201907010001), Jul 1, 2019: CARBON SEAL. LEAKING. HAZY IN CABIN WITH OFF SMELL. PAX COMPLAINED OF EYES BURNING. CREW BEGAN TO FEEL IT TOO. TOOK ABOUT AN HOUR TO BUILD. R&R #2 ENG 0 CARBON SEAL OPS AND LEAK CHEC
- [SDR RAIA2019060620001](https://openairdocs.org/sdr/RAIA2019060620001), Jun 2, 2019: HYDRAULIC SYSTEM. LOW. #1 HYD LOW QTY AMBER EICAS ONCE GEAR RAISED, ONCE STOWED MSG WENT OUT. ON LOWERING OF GEAR, MSG RETURNED UNTIL E-BRAKE WAS SET AND AGAIN EICAS MSG WENT AWAY. SE
- [SDR RAIA201812290001](https://openairdocs.org/sdr/RAIA201812290001), Dec 29, 2018: FITTING. CRACKED. RT FR 16 STR15-16 SHEAR CLIP CRACKED. REMOVED AND REPLACED SHEAR CLIP.
- [SDR RAIA201812250002](https://openairdocs.org/sdr/RAIA201812250002), Dec 25, 2018: GUSSET. CORRODED. LT FLOORBEAM GUSSET BETWEEN FR59 AND FR 61 IS CORRODED BEYOND LIMITS- REMOVED LT FLOORBEAM GUSSET BETWEEN FR59 AND FR61. TNSTALLED NEW LT FLOORBEAM GUSSET BETWE
- [SDR RAIA201812250001](https://openairdocs.org/sdr/RAIA201812250001), Dec 25, 2018: GUSSET. CORRODED. LT FLOORBEAM GUSSET BETWEEN FR59 AND FR 61 IS CORRODED. REMOVED AND REPLACED GUSSET.
- [SDR RAIA201812210007](https://openairdocs.org/sdr/RAIA201812210007), Dec 21, 2018: ANGLE. CRACKED. "L" ANGLE AT TOP OF "T" PROFILE AT FR 67 IS CRACKED. REMOVED AND REPLACED "L" ANGLE.
- [SDR RAIA201812210006](https://openairdocs.org/sdr/RAIA201812210006), Dec 21, 2018: SUPPORT BRACKET. CRACKED. AFT CARGO DOOR SUPPORT ROD CUP HOLDER SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED CARGO DOOR ROD CUP SUPPORT VRACKET.
- [SDR RAIA201812210005](https://openairdocs.org/sdr/RAIA201812210005), Dec 21, 2018: FITTING. CRACKED. AFT CARGO FRAME 72 SHEAR CLIP IS CRACKED AT STR 16L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 72 STR 16.
- [SDR RAIA201812210004](https://openairdocs.org/sdr/RAIA201812210004), Dec 21, 2018: GUSSET. CORRODED. CORROSION ON CTR GUSSET BETWEEN FR 19-24. REMOVED AND REPLACED CTR GUSSET BETWEEN FR 19-24.
- [SDR RAIA201812210003](https://openairdocs.org/sdr/RAIA201812210003), Dec 21, 2018: DOOR SILL. CORRODED. CORROSION ON LT FLOOR SILL BETWEEN FR19-24. REMOVED AND REPLACED LT FLOOR SILL BETWEEN FR 19-24.
- [SDR RAIA201812210002](https://openairdocs.org/sdr/RAIA201812210002), Dec 21, 2018: FITTING. CRACKED. RT FUSELAGE SHEAR CLIP AT FR15 STR 15 IS CRACKED. REMOVED AND REPLACED SHEAR CLIP AT FR 15.
- [SDR RAIA2018122410001](https://openairdocs.org/sdr/RAIA2018122410001), Dec 21, 2018: FLOOR SUPPORT. CORRODED. CORROSION ON STOP SIGN GUSSETT PLATE R/H OMEGA BEAM AT FRAME 20..........REMOVED AND REPLACED STOP SIGN GUSSETT PLATE R/H OMEGA BEAM AT FRAME 20
- [SDR RAIA201812200007](https://openairdocs.org/sdr/RAIA201812200007), Dec 20, 2018: SUPPORT ANGLE. CRACKED. RT LATERAL SUPPORT ANGLE IS CRACKED AT FRAME 50- CUT OUT DAMAGED AREA. FAB REPAIR PART 80% PARTIAL INSTALL. REPAIRED CRACKED SUPPORT ANGLE.
- [SDR RAIA20181220002](https://openairdocs.org/sdr/RAIA20181220002), Dec 20, 2018: SUPPORT ANGLE. CRACKED. DISCREPANCY-LT LATERAL SUPPORT ANGLE IS CRACKED AT FRAME 46 - JOB TURNOVER- REMOVED CRACKED SUPPRT ANGLE IAW SRM 51-40-02-CORR. ACTION-REMOVED AND REPAIRED ANGL
- [SDR RAIA201812200006](https://openairdocs.org/sdr/RAIA201812200006), Dec 20, 2018: SUPPORT ANGLE. CRACKED. LT LATERAL SUPPORT ANGLE IS CRACKED AT FRAME 48. REMOVED AND REPLACED SUPPORT ANGLE AT FR 48.
- [SDR RAIA201812200005](https://openairdocs.org/sdr/RAIA201812200005), Dec 20, 2018: DOOR SILL. CORRODED. LT O/B FLOOR SEAL ATTACH FLANGE CORRODED BETWEEN FR 41-48. REMOVED AND REPLACED FLOOR SILL AT FR41-48.
- [SDR RAIA201812200004](https://openairdocs.org/sdr/RAIA201812200004), Dec 20, 2018: FITTING. DAMAGED. RT UPPER SEAT TRACK FITTING IS DAMAGED AT FR 44. REMOVED AND REPLACED UPPER SEAT TRACK FITTING AT FR 44.
- [SDR RAIA201812200003](https://openairdocs.org/sdr/RAIA201812200003), Dec 20, 2018: PLATE. CORRODED. CARGO FLOOR STRUCTURE PLATE ON LT HAT BEAM BETWEEN FR 65 AND 68. REMOVED AND REPLACED HAT BEAM AT FR 65-68.
- [SDR RAIA201812200002](https://openairdocs.org/sdr/RAIA201812200002), Dec 20, 2018: SUPPORT BRACKET. CRACKED. LT BLEED DUCT SUPPORT BRACKET CRACKED AT LT AFT FUSELAGE FR69. REMOVED AND REPLACED BLEED DUCT SUPPORT BRACKED.
- [SDR RAIA201812200001](https://openairdocs.org/sdr/RAIA201812200001), Dec 20, 2018: SUPPORT ANGLE. CRACKED. LT LATERAL SUPPORT ANGLE IS CRACKED AT FRAME 49. REMOVED AND REPLACED ANGLE.
- [SDR RAIA201812190002](https://openairdocs.org/sdr/RAIA201812190002), Dec 19, 2018: REINFORCEMENT. CRACKED. REINFORCEMENT STR 3 BETWEEN FR 19-20 IS CRACKED AT FINGER. REPAIRED PER ETD.
- [SDR RAIA201812190001](https://openairdocs.org/sdr/RAIA201812190001), Dec 19, 2018: CUP. CRACKED. GPU RECEPTACLE MOUNTING CUP IS CRACKED. REMOVED AND REPLACED GPU RECEPTACLE MOUNTING CUP.
- [SDR RAIA201812180006](https://openairdocs.org/sdr/RAIA201812180006), Dec 18, 2018: FITTING. CRACKED. LT SHEAR CLIP IS CRACKED AT FR 58. REMOVED AND REPLACED SHEAR CLIP.
- [SDR RAIA201812180005](https://openairdocs.org/sdr/RAIA201812180005), Dec 18, 2018: TEE FITTING. BENT. CARGO COMP FLOOR STRUCTURE AFT "T" PROFILES ARE BENT. REMOVED AND REPLACED "T" PROFILES.
- [SDR RAIA2018122418002](https://openairdocs.org/sdr/RAIA2018122418002), Dec 18, 2018: SHEAR TIE. CRACKED. L/H SHEAR CLIP CRACKED AT FRAME26............REMOVED AND REPLACED SHEAR CLIP AT FRAME 26
- [SDR RAIA2018122418004](https://openairdocs.org/sdr/RAIA2018122418004), Dec 18, 2018: SHEAR TIE. CRACKED. R/H SHEAR CLIP CRACKED AT FRAME 25........ REMOVED AND REPLACED R/HSHEAR CLIP AT FRAME 25
- [SDR RAIA2018122418003](https://openairdocs.org/sdr/RAIA2018122418003), Dec 18, 2018: SHEAR TIE. CRACKED. L/H SHEAR CLIP CRACKED AT FRAME 25.........REMOVED AND REPLACED SHEAR CLIP AT FRAME 25
- [SDR RAIA201810310001](https://openairdocs.org/sdr/RAIA201810310001), Oct 31, 2018: DOOR. OUT OF ADJUST. ON POST FLIGHT, FOUND MAIN CABIN DOOR HARD TO OPEN. INSTALLED WASHERS UNDER DOOR SUPPORT LINKS. OPS CHECK GOOD.
- [SDR RAIA2018102290001](https://openairdocs.org/sdr/RAIA2018102290001), Oct 19, 2018: HYDRAULIC SYSTEM. CONTAMINATED. WHEN GEAR RETRACTED, NR 1 HYD WENT INTO AMBER WITH GEAR UP AND LOCKED. SYS NR 1 WAS FULL UPON DEPARTURE. - CORR ACTION NR 1:BLED NR 1 HYD SYS AND SVC'D NO LEAK 
- [SDR RAIA2018091370001](https://openairdocs.org/sdr/RAIA2018091370001), Sep 7, 2018: BRAKE. FAULTY. HYD 1 LOW QTY. R&R NR 2, 3 & 4 BRAKE. OPS CHECK GOOD. FAULTY VALVES, BRAKE ASSYS. ALL ARE P/N 2-71707-2, NR 2 S/N: 2775 TT:UNK TC:UNK , NR 3 S/N: 2997 TT:UNK TC
- [SDR RAIA2018052210001](https://openairdocs.org/sdr/RAIA2018052210001), May 21, 2018: MECHANISM. LACK OF LUBE. MAIN CABIN DOOR DIFFICULT TO OPEN. LUBRICATED MAIN DOOR ACTUATING & LOCKING MECHANISM. OPS CHECK GOOD
- [SDR RAIA201804100001](https://openairdocs.org/sdr/RAIA201804100001), Apr 10, 2018: ROLLER. OUT OF ADJUST. F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED MAIN DOOR SEAL AND ADJUSTED FWD ROLLER. OPS CHECK GOOD.
- [SDR RAIA201803060001](https://openairdocs.org/sdr/RAIA201803060001), Feb 28, 2018: ENGINE. MALFUNCTIONED. NR 1 ENGINE LOW PRESSURE VIBRATION HIGHER THAN NORMAL BUT NOT IN AMBER DURING DESCENT, AFTER LANDING OIL PRESSURE DECREASED STEADILY, AT 32% INDICATION TURNED R
- [SDR RAIA201802270001](https://openairdocs.org/sdr/RAIA201802270001), Feb 27, 2018: WIRE. DAMAGED. LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPAIRED THE WIRING TO THE RT OVERWING EMERGENCY LIGHT. PERFORMED AN OPS CHECK. OPS CHECKED GOOD.
- [SDR RAIA201801240001](https://openairdocs.org/sdr/RAIA201801240001), Jan 24, 2018: LIGHT. NOT REPORTED. LT AFT WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT (5). R&R LIGHT BULB ON LT AFT WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT. OPS CHECK GOOD.
- [SDR RAIA201709040001](https://openairdocs.org/sdr/RAIA201709040001), Sep 4, 2017: DOOR. OUT OF ADJUST. MAIN CABIN DOOR DIFFICULT TO OPEN. PERFORMED ADJUSTMENT OF MAIN CABIN PAX DOOR. OPS CHECK GOOD.
- [SDR RAIA201608260001](https://openairdocs.org/sdr/RAIA201608260001), Aug 26, 2016: CONTROLLER. INOPERATIVE. CABIN ALTITUDE CLIMBED ABOVE 15K. CABIN ALTITUDE WENT TO 15.000 FT DURING CLIMBOUT. ACFT HAD JUST PASSED THROUGH 10,000 FT AND PRESSURE WENT TO THE YELLOW LINE 
- [SDR RAIA201602220004](https://openairdocs.org/sdr/RAIA201602220004), Feb 22, 2016: SWITCH. INOPERATIVE. PACK 2 OVERLOAD EICAS. R & R PACK 2 OVERTEMP SWITCH. OPS CHECK GOOD.
- [SDR RAIA201602130001](https://openairdocs.org/sdr/RAIA201602130001), Feb 13, 2016: POWER SUPPLY. INOPERATIVE. RT WING FORWARD EMERGENCY FLOOD LIGHT NR 1 INOPERATIVE. R & R BATTERY SUPPLY IN POSITION NR 2. OPS CHECK GOOD.
- [SDR RAIA201512270002](https://openairdocs.org/sdr/RAIA201512270002), Dec 27, 2015: BATTERY PACK. INOPERATIVE. CEILING EMERGENCY EXIT LIGHT AT ROW 8, LIGHT NR 16B, IS INOPERATIVE INSPECTED AND FOUND BATTERY SUPPLY UNIT NR 2 TO BE FAULTY. R & R BATTERY SUPPLY UNIT NR 2. O
- [SDR RAIA201510040001](https://openairdocs.org/sdr/RAIA201510040001), Oct 4, 2015: OIL SYSTEM. LEAKING. NR 1 ENGINE OIL LEVEL WENT FROM 11 QTS TO 2 QTS DURING CLIMB TO 17,000, RETURNED TO DEPARTURE. MAINTENANCE INSPECTED AND FOUND INTERNAL LEAK, REPLACED THE NR 1 
- [SDR RAIA201509080005](https://openairdocs.org/sdr/RAIA201509080005), Sep 8, 2015: BATTERY. INOPERATIVE. NR 4 EMERGENCY BACKUP BATTERY INOPERATIVE. MAINTENANCE REPLACED NR 4 EMERGENCY BACKUP BATTERY, OPS CHECK GOOD.
- [SDR RAIA201509080004](https://openairdocs.org/sdr/RAIA201509080004), Sep 8, 2015: BATTERY. INOPERATIVE. NR 3 EMERGENCY BACKUP BATTERY INOPERATIVE. MAINTENANCE REPLACED NR 3 EMERGENCY BACKUP BATTERY, OPS CHECK GOOD.
- [SDR RAIA201509080003](https://openairdocs.org/sdr/RAIA201509080003), Sep 8, 2015: BATTERY. INOPERATIVE. NR 2 EMERGENCY BACKUP BATTERY INOPERATIVE. MAINTENANCE REPLACED NR 2 BACKUP BATTERY, OPS CHECKED GOOD.
- [SDR RAIA201509080002](https://openairdocs.org/sdr/RAIA201509080002), Sep 8, 2015: BATTERY. INOPERATIVE. NR 1 EMERGENCY BACKUP BATTERY INOPERATIVE. MAINTENANCE REPLACED NR 1 BACKUP BATTERY, OPS CHECK GOOD.
- [SDR ASOA20150611133](https://openairdocs.org/sdr/ASOA20150611133), Jun 11, 2015: MOUNT. CRACKED. DURING C-CHECK THE LT ENGINE FORWARD LOWER MOUNT YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FITTING IAW EC5450-01152. THE ACFT WAS APPROVED FOR
- [SDR ASOA20150611132](https://openairdocs.org/sdr/ASOA20150611132), Jun 11, 2015: DRAG ANGLE. CRACKED. DURING C-CHECK, THE LT FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED BETWEEN FRAMES 75-76. MAINTENANCE R & R THE ANGLE IAW SRM 51-40-02. TH
- [SDR ASOA20141106114](https://openairdocs.org/sdr/ASOA20141106114), Nov 5, 2014: LIGHT. INOPERATIVE. FWD LT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY ASSY OPS CHECK GOOD ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20140911100](https://openairdocs.org/sdr/ASOA20140911100), Sep 11, 2014: INVERTER. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE LT AFT INTERIOR OVERWING EMERGENCY EXIT SIGN WAS INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT SYS INVERTER WITH OPS CHECK G
- [SDR ASOA20140803102](https://openairdocs.org/sdr/ASOA20140803102), Aug 3, 2014: LIGHT. INOPERATIVE. DURING PREFLIGHT, CREW REPORTED THAT THE EMERGENCY EXIT SIGN FACING SEAT 3CD WAS NOT FUNCTIONING. MAINTENNACE INSPECTED THE LIGHT ASSY, R & R THE LIGHT, OPERATI

All 92: https://openairdocs.org/aircraft/N18120/reports.md

## STCs that may be installed (OpenAirDocs) (56, 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-145XR)

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST02176AT-D](https://openairdocs.org/stc/ST02176AT-D): Installation of a Teledyne Mini Flight Data Acquistion Unit. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST02310AT](https://openairdocs.org/stc/ST02310AT): Installation of SAF-T-GLO photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST01409LA](https://openairdocs.org/stc/ST01409LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC 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 ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC 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 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 ST00818DE](https://openairdocs.org/stc/ST00818DE): Installation of Honeywell Control Display Unit (CDU) model CD-830. Premier Air Center LLC d/b/a West Star Aviation
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST09858SC](https://openairdocs.org/stc/ST09858SC): Installation of cabin automatic coffee brewing system. Safran Cabin Germany Gmbh
- [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 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 ST03177NY](https://openairdocs.org/stc/ST03177NY): Installation of a Honeywell ADS-B (Out), EHS and FreeFlight GPS. Delta Engineering Corporation
- [STC ST01520WI](https://openairdocs.org/stc/ST01520WI): Installation of the Concorde RG-442 VRSLA Battery and Temperature Sensor in place of the original Nickel-Cadmium Battery. Concorde Battery Corporation
- [STC ST00361BO](https://openairdocs.org/stc/ST00361BO): Installation of a Honeywell Primus II (XS-852) ADS-B Out System. Pro Star Aviation, LLC
- [STC ST04282CH](https://openairdocs.org/stc/ST04282CH): Installation of Honeywell CD-830 Control Display Unit (CDU). Nextant Aerospace
- [STC ST01702WI](https://openairdocs.org/stc/ST01702WI): Change seating configuration to 30 passengers by removal of seats. Worldwide Aircraft Engineering LLC
- [STC ST04108CH](https://openairdocs.org/stc/ST04108CH): Installation of Gogo Business Aviation ATG-8000 High Speed Internet with Wireless Local Area Network (WLAN). Nextant Aerospace
- [STC ST04367AT](https://openairdocs.org/stc/ST04367AT): Removal of the Existing Honeywell DL-900 or DL-950 Data Loader and Installation of the Honeywell DL-1000 Data Loader. Chippewa Aerospace Inc
- [STC ST04190AT](https://openairdocs.org/stc/ST04190AT): Installation of an ADS-B Out. Chippewa Aerospace Inc
- [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST04282AT](https://openairdocs.org/stc/ST04282AT): Installation of the Honeywell DU-875 LCD Flight Display. Chippewa Aerospace Inc
- [STC ST04015AT](https://openairdocs.org/stc/ST04015AT): Installation of the Honeywell NZ-2000 FMS/GPS System with or without WAAS/LPV. Chippewa Aerospace Inc
- [STC ST09859AC](https://openairdocs.org/stc/ST09859AC): Installation of a SkyTender Beverage Trolley. ASIG LLC
- [STC ST04263AT](https://openairdocs.org/stc/ST04263AT): Modification of Interior Arrangement Configuration from 50 to 30 Passenger Seats (All Tourist Class). VIA Airlines Inc
- [STC ST04191AT](https://openairdocs.org/stc/ST04191AT): Installation of the Honeywell Sky Connect Tracker Iridium Satcom System. Chippewa Aerospace Inc
- [STC ST02524LA](https://openairdocs.org/stc/ST02524LA): Installation of TCAS version 7.0. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST03483AT](https://openairdocs.org/stc/ST03483AT): Installation of a Portable Beverage Dispensing System, P/N B43-FA-001. Dynamo Beverage Company, USA, L.L.C
- [STC ST03999AT](https://openairdocs.org/stc/ST03999AT): Installation of a Single Honeywell HF-1050 HF Communication System. Chippewa Aerospace Inc
- [STC ST01619CH](https://openairdocs.org/stc/ST01619CH): Installation of a Lavatory Service Shutoff Valve. AeroControlex Group TransDigm Inc
- [STC ST03994AT](https://openairdocs.org/stc/ST03994AT): Installation of Bleed Air Coupling Sleeve Kit. Seal Dynamics
- [STC ST02638AT](https://openairdocs.org/stc/ST02638AT): Installation of an improved aircraft toilet rinse/fill shutoff valve and asociated hardware. Parker Hannifin Corporation, Parker Aerospace
- [STC ST03890AT](https://openairdocs.org/stc/ST03890AT): Installation of an L-3 Communications Micro Quick Access Recorder (MQAR). Chippewa Aerospace, Inc
- [STC ST02882CH-D](https://openairdocs.org/stc/ST02882CH-D): Installation of a Honeywell Flight Management System (FMS #2). Standard Aero
- [STC ST02803CH-D](https://openairdocs.org/stc/ST02803CH-D): Installation of a Honeywell KHF-1050 system. Standard Aero

All 56: https://openairdocs.org/aircraft/N18120/stcs.md

## Earlier aircraft with N18120

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N18120 before.

- [Cancelled 1983-05-05](https://openairdocs.org/deregistered/N18120-1983-05-05): Cessna 150L, S/N 15073800. Administratively canceled. Owner: [Ferris Bonnie J](https://openairdocs.org/faa-owner/FERRIS%20BONNIE%20J), [Dillon, MT](https://openairdocs.org/faa-place/MT/Dillon)

## Related

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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.