# N18114: 2002 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: 145664
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2005
- Certificate issued: July 13, 2023
- Expires: July 31, 2030
- Mode S code: A146FB
- Registered owner: [Enterprise Aircraft Finance LLC](https://openairdocs.org/faa-owner/ENTERPRISE%20AIRCRAFT%20FINANCE%20LLC)
- Location: [Clayton, MO](https://openairdocs.org/faa-place/MO/Clayton)
- Owner type: LLC
- Owner's area on the map: 38.6443° N, 90.3281° W: Placed by OpenAirDocs at the center of ZIP code 63105, 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=18114
- Page: https://openairdocs.org/aircraft/N18114

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/N18114/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 N18114.

## FAA accident and incident reports

None matched to N18114.

## Service difficulty reports (49)

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 RAIA2019100740002](https://openairdocs.org/sdr/RAIA2019100740002), Oct 4, 2019: PUMP. LEAKING. SYSTEM 2 HYDRAULIC LOST FLUID IN FLIGHT. R & R THE NR 2 ENGINE HYD PUMP DUE TO A LEAK. LEAK AND OPS CHECKED GOOD.
- [SDR RAIA201909070001](https://openairdocs.org/sdr/RAIA201909070001), Sep 7, 2019: LIGHT. CRACKED. FLOOR PATH LIGHTING AT 4C/D IS CRACKED. REMOVED & REPLACED FLOOR PATH LIGHTING AT 4 C/D.
- [SDR RAIA201907050001](https://openairdocs.org/sdr/RAIA201907050001), Jul 5, 2019: WARNING SYSTEM. FALSE ACTIVATION. HIGH SPEED ABORT AT 90 KIAS. MASTER WARNING SPOILERS OPEN---- LOG PAGE 382906 C/W HIGH ENERGY STOP INSP NO FAULTS FOUND- LOG PAGE 382907 CLEANED AND INSP SPOILE
- [SDR RAIA201905070001](https://openairdocs.org/sdr/RAIA201905070001), May 7, 2019: GARLOCK SEAL. LEAKING. E2 SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE AND LOW QUANITY. OIL PRESSURE DROPPED TO 34 PSI AND 3 QTS. AT COMMANDED SHUT DOWN PSI INDICATED 8 PSI AND 2 QTS. R
- [SDR RAIA2019041270001](https://openairdocs.org/sdr/RAIA2019041270001), Apr 7, 2019: OXYGEN BOTTLE. LEAKING. LOW O2 EICAS MESSAGE IN FLIGHT. DIVERTED. LESS THAN 400 PSI ON OXYGEN WHEN CHECKED ON MFD BEFORE AIRCRAFT SHUTDOWN. R & R CREW OXYGEN BOTTLE. OPS CHECK GOOD.
- [SDR RAIA201903080001](https://openairdocs.org/sdr/RAIA201903080001), Mar 8, 2019: FIRE LOOP. FAILED. E1 FIRE DETECT FAIL IN FLIGHT. REMOVED AND REPLACED ENG 1 FIRE DETECTION LOOP. OPS CHECK GOOD.
- [SDR RAIA201810180002](https://openairdocs.org/sdr/RAIA201810180002), Oct 18, 2018: DOOR SILL. CRACKED. RT FLOOR SILL BETWEEN FR53 AND FR59 IS CRACKED. REMOVED AND REPLACED RT FLOOR SILL AT FR53 AND FR59.
- [SDR RAIA201810120004](https://openairdocs.org/sdr/RAIA201810120004), Oct 12, 2018: DOOR SILL. CORRODED. RT FUSELAGE FLOOR ATTACHMENT FLANGE CORRODED AT FR 40-41. REMOVE AND REPLACE RT FLOOR SILL AT FR36-41.
- [SDR RAIA201810080005](https://openairdocs.org/sdr/RAIA201810080005), Oct 8, 2018: DOOR SILL. CORRODED. LT FLOOR SILL BETWEEN FR28 AND FR29 HAS CORROSION. REMOVED AND REPLACED LT FLOOR SILL AT FR28 AND FR29.
- [SDR RAIA201810060004](https://openairdocs.org/sdr/RAIA201810060004), Oct 6, 2018: DOOR SILL. CORRODED. CORROSION ON RT FLOOR ATTACH FLANGE AT FR50 AND FR51. REMOVED AND REPLACED RT FLOOR SILL AT FR 50 AND FR51.
- [SDR RAIA201810060003](https://openairdocs.org/sdr/RAIA201810060003), Oct 6, 2018: DOOR SILL. CORRODED. LIGHT SURFACE CORROSION ON LT FLOOR ATTACH FLANGE BETWEEN FR31-32 AND FR37-38. BLENDED FLOOR SILLS FR37-38 IN LIMITS, FR31-32 OUT OF LIMITS. REMOVED AND REPLACE
- [SDR RAIA2018102460002](https://openairdocs.org/sdr/RAIA2018102460002), Oct 6, 2018: DOOR SILL. CORRODED. CORROSION ON LT FLOOR ATTACH FLANGE AT FR50. REMOVED AND REPLACED LT FLOOR SILL AT FR 50.
- [SDR RAIA2018102460001](https://openairdocs.org/sdr/RAIA2018102460001), Oct 6, 2018: DOOR SILL. CORRODED. CORROSION FOUND ON FLOOR ATTACH FLANGE RT SIDE BETWEEN FR 41 AND FR 48. REMOVED AND REPLACED FLOOR SILL ON RT SIDE BETWEEN FR41 AND FR48.
- [SDR RAIA2018102450001](https://openairdocs.org/sdr/RAIA2018102450001), Oct 5, 2018: CROSSBEAM. CRACKED. AFT AVIONICS COMP CROSSBEAM IS CRACKED. REMOVED AND REPLACED CROSSBEAM.
- [SDR RAIA2018102440002](https://openairdocs.org/sdr/RAIA2018102440002), Oct 4, 2018: FITTING. CRACKED. NR 2 ENG FWD YOKE LOWER FWD MOUNT LINKAGE FITTING INDICATION OF POSSIBLE CRACK AT UPPER INSIDE RADIUS. REMOVED AND REPLACED NR 2 ENG FWD YOKE FWD MOUNT LINKAGE 
- [SDR RAIA2018102440001](https://openairdocs.org/sdr/RAIA2018102440001), Oct 4, 2018: SUPPORT BRACKET. CRACKED. PASSENGER DOOR INTERIOR DOOR HANDLE SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED DOOR HANDLE SUPPORT BRACKET.
- [SDR RAIA2018102430006](https://openairdocs.org/sdr/RAIA2018102430006), Oct 3, 2018: DOOR SILL. CHAFED. RT FLOOR SILL IN CARGO BAY HAS CHAFE MARKS AROUND NUT PLATE HOLES BETWEEN FR61 AND FR65. REMOVED AND REPLACED RT FLOOR SILL BETWEEN FR61 AND FR65.
- [SDR RAIA2018102430005](https://openairdocs.org/sdr/RAIA2018102430005), Oct 3, 2018: SUPPORT. CRACKED. CARGO DOOR HOLD OPEN ROD SUPPORT IS CRACKED. REMOVED AND REPLACED CARGO DOOR ROD CUP SUPPORT.
- [SDR RAIA2018102430004](https://openairdocs.org/sdr/RAIA2018102430004), Oct 3, 2018: FRAME. SCRATCHED. FR 61 HAS SCRATCHES AROUND NUT PLATE HOLES. REMOVED AND REPLACED FR 61 LOWER PARTITION DOUBLED.
- [SDR RAIA2018102430003](https://openairdocs.org/sdr/RAIA2018102430003), Oct 3, 2018: FRAME. CHAFED. FR 70 CHAFED BY STRINGER 11R. BLENDED OUT DAMAGE TO FR 70 REF. ETD2018-145-105368.
- [SDR RAIA2018102430002](https://openairdocs.org/sdr/RAIA2018102430002), Oct 3, 2018: PLATE. CHAFED. RT PYLON FWD YOKE GUSSET PLATE HAS CHAFE DAMAGE. REMOVED AND REPLACED RT PYLON FWD GUSSET PLATE.
- [SDR RAIA2018102430001](https://openairdocs.org/sdr/RAIA2018102430001), Oct 3, 2018: HANDLE. CRACKED. REAR ELECTRONIC COMP DOOR HANDLE IS BENT AND POSSIBLY CRACKED. REMOVED AND REPLACED DOOR HANDLE.
- [SDR RAIA2018102420003](https://openairdocs.org/sdr/RAIA2018102420003), Oct 2, 2018: GUSSET. CORRODED. RT LAV FLOOR GUSSET HAS CORROSION AROUND FWD NUT PLATE. REMOVED AND REPLACED RT LAV FLOOR GUSSET.
- [SDR RAIA2018102420002](https://openairdocs.org/sdr/RAIA2018102420002), Oct 2, 2018: DOOR SILL. CORRODED. RT LAV FLOOR SILL HAS CORROSION AROUND AFT NUT PLATE. REMOVED AND REPLACED RT LAV FLOOR SILL.
- [SDR RAIA2018102420001](https://openairdocs.org/sdr/RAIA2018102420001), Oct 2, 2018: FLOOR SUPPORT. CORRODED. BEAM AT FR 20 BETWEEN CTR AND LT OMEGA BEAMS HAS CORROSION. REMOVED AND REPLACED CTR AND LT OMEGA BEAMS AT FR 20.
- [SDR RAIA2018082830002](https://openairdocs.org/sdr/RAIA2018082830002), Aug 23, 2018: SWITCH. MALFUNCTIONED. CARGO DOOR OPEN EICAS MESSAGE. REPLACED THE CARGO DOOR WARNING SWITCH, OPS CHECKED GOOD.
- [SDR RAIA201703210002](https://openairdocs.org/sdr/RAIA201703210002), Mar 21, 2017: COUPLING. BROKEN. PACK 2 CLOSES WITH NO EICAS MESSAGE ASSOCIATED NOSE FROM CABIN FLOOR. FOUND DUCT BLOWN ON #2 PACK REPLACED COUPLING. OPS CHECK GOOD.
- [SDR RAIA201610200001](https://openairdocs.org/sdr/RAIA201610200001), Oct 20, 2016: SWITCH. FAILED. EICAS MASTER WARNING PITCH TRIM MAIN INOPERATIVE. REMOVED AND REPLACED CAPTAIN`S PITCH TRIM SWITCH AND PERFORMED OPS CHECKED GOOD ON PITCH TRIM, NO DEFECTS NOTE
- [SDR RAIA201603030001](https://openairdocs.org/sdr/RAIA201603030001), Mar 3, 2016: DUCT. LEAKING. BLEED 2 LEAK. R & R BLEED DUCT CONNECTING TO AIRSTART DUCT ON NR 2 SYSTEM. LEAK CHECK GOOD.
- [SDR RAIA201603010003](https://openairdocs.org/sdr/RAIA201603010003), Mar 1, 2016: BLEED VALVE. LEAKING. BLEED 2 LEAK. LOCKED BLEED VALVE CLOSED. PERFORMED OPS CHECK OF 2 BLEED SYS, NO DEFECTS NOTED.
- [SDR RAIA201512280002](https://openairdocs.org/sdr/RAIA201512280002), Dec 28, 2015: OUTFLOW VALVE. SLOW. SLOW CABIN DEPRESSURIZATION AT FL 230 AFTER CONFIGING TO NORMAL WITH ANTI-ICE ON. R & R PNUEMATIC OUTFLOW VALVE. OPS CHECK GOOD.
- [SDR RAIA201512280001](https://openairdocs.org/sdr/RAIA201512280001), Dec 28, 2015: WARNING MESSAGE. FALSE ACTIVATION. BLEED 2 OVERTEMP IN FLIGHT, CONDUCTED GROUND RUN OPS TEST. OPS CHECK GOOD.
- [SDR RAIA201507220001](https://openairdocs.org/sdr/RAIA201507220001), Jul 22, 2015: BOLT. LOOSE. NR 1 ENGINE LOST 7 QTS OF OIL AFTER 35 MINUTES OF FLYING. CREW COMPLETED PRECAUTIONARY NR 1 ENGINE SHUTDOWN, CONTINUED TO FOR EMERGENCY LANDING. MAINTENANCE INS
- [SDR ASOA20150114009](https://openairdocs.org/sdr/ASOA20150114009), Jan 14, 2015: DOOR SILL. CORRODED. CARGO DOOR CUTOUT CENTER SILL HAS CORROSION. R & R CARGO DOOR CUTOUT CENTER SILL IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150112007](https://openairdocs.org/sdr/ASOA20150112007), Jan 12, 2015: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM CORRODED AT FRAME 59. REPAIRED LEFT OMEGA BEAM IAW EC 5310-01473. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130228026](https://openairdocs.org/sdr/ASOA20130228026), Feb 28, 2013: INVERTER. INOPERATIVE. DURING A-CHECK INSPECTION, THE LT OVERWING EMERGENCY EXIT DOOR LOWER INTERNAL LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE NR 5 INVERTER, OPS TESTED WITH NO 
- [SDR C2XA11CL149](https://openairdocs.org/sdr/C2XA11CL149), Jun 21, 2011: WIRE HARNESS. DEFECTIVE. CLE FLT 5835 THE CREW REPORTED A ENGINE NR 1 FIRE DETECT FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE PROBLEM. REPLACED THE NR 1 ENGINE
- [SDR C2XA11CL147](https://openairdocs.org/sdr/C2XA11CL147), Jun 20, 2011: DAU. INTERMITTENT. THE CREW REPORTED A ENGINE NR 1 FIRE DETECT FAIL ON TAKEOFF. MAINTENANCE INSPECTED AND PERFORMED STEPS OF FIM 26-11-00-810-803A INCLUDING ALL ELECTRICAL STEPS L
- [SDR C2XA11CL146](https://openairdocs.org/sdr/C2XA11CL146), Jun 18, 2011: CONTROL MODULE. FAULTY. ORD FLT 5887 THE CREW REPORTED A ENGINE NR 1 FIRE DETECT FAIL MESSAGE ON CLIMBOUT. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACE
- [SDR C2XA10CL034](https://openairdocs.org/sdr/C2XA10CL034), Feb 23, 2010: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LAMP ON THE RIGHT OVERWING EMERGENCY
- [SDR C2XA09IA287](https://openairdocs.org/sdr/C2XA09IA287), Nov 10, 2009: ACTUATOR. INOPERATIVE. IAH - FLIGHT 2116, THE CREW REPORTED A PITCH TRIM MAIN INOP EICAS MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AN
- [SDR C2XA09RI186](https://openairdocs.org/sdr/C2XA09RI186), Oct 30, 2009: WIRE HARNESS. DAMAGED. FLIGHT 2807 - EWR - FLIGHT CREW REPORTED NR 1 BRAKE TEMP INDICATION IN RED AT TAKE OFF. FLIGHT CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX RE
- [SDR C2XA07IA207](https://openairdocs.org/sdr/C2XA07IA207), Sep 15, 2007: PANEL. INOPERATIVE. IAH - FLIGHT 2163, THE CREW REPORTED LANDING GEAR LEVER, BACKLIGHTING PANEL, UP POSITION WILL NOT ILUMINATE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOU
- [SDR C2XA06TY025](https://openairdocs.org/sdr/C2XA06TY025), Apr 30, 2006: FLOOR SUPPORT. CORRODED. CENTER OMEGA BEAM IN GALLEY FROM FRAME 18-23 IS CORRODED. REMOVED AND REPLACED CENTER OMEGA BEAM IN GALLEY IAW EMB145 XR SRM 57-40-02.
- [SDR C2XA05SD019](https://openairdocs.org/sdr/C2XA05SD019), Apr 29, 2005: FLASHLIGHT. INOPERATIVE. SDF - F/O'S EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA03BT109](https://openairdocs.org/sdr/C2XA03BT109), Nov 19, 2003: CONNECTOR. FIRE. CREW REPORTED, GPU CAUGHT FIRE AT CONNECTOR END AND BURNED AIRCRAFT AT GPU RECEPTICAL (GPU WAS ARCHING WHEN GPU CORD WAS PULLED). MAINTENANCE INSPECTED FUSELAGE
- [SDR C2XA03IA052](https://openairdocs.org/sdr/C2XA03IA052), May 20, 2003: INVERTER. INOPERATIVE. DURING POSTFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHT ON ROW SEAT TWELVE (12) FORWARD EXIT FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGE
- [SDR C2XA03IA004](https://openairdocs.org/sdr/C2XA03IA004), Jan 11, 2003: CONTROLLER. INOPERATIVE. DURING CLIMBOUT THE CREW NOTED THAT THE AIRCRAFT WOULD NOT PRESSURIZE. THE CREW DECLARED EMERGENCY, RETURNED TO IAH AND LANDED WITHOUT INCIDENT. IAH- MAINTENANC
- [SDR C2XA02IA250](https://openairdocs.org/sdr/C2XA02IA250), Dec 14, 2002: LIGHT. DISCONNECTED. DURING PREFLIGHT THE CREW NOTED THAT THE SERVICE DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE. MAINTENANCE CONNECTED THE EMERGENCY LIGHT TO THE CONNECTOR, PERFORME

## 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/N18114/stcs.md

## Earlier aircraft with N18114

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N18114 before.

- [Cancelled 1991-07-22](https://openairdocs.org/deregistered/N18114-1991-07-22): Cessna 177B, S/N 17702528. Exported to Netherlands. Owner: [Snyder D Jay](https://openairdocs.org/faa-owner/SNYDER%20D%20JAY), [Londonderry, VT](https://openairdocs.org/faa-place/VT/Londonderry)

## 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

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