# N17185: 2005 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: 14500922
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 17, 2005
- Certificate issued: July 29, 2020
- Expires: July 31, 2027
- Mode S code: A12072
- Registered owner: [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC)
- Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago)
- Owner type: Corporation
- Owner's area on the map: 41.8813° N, 87.6375° W: Placed by OpenAirDocs at the center of ZIP code 60606, 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=17185
- Page: https://openairdocs.org/aircraft/N17185

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/N17185/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 N17185.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20050808032619I](https://openairdocs.org/incident/20050808032619I), Aug 8, 2005: Emb EMB145XR (N17185), Newark, NJ, Minor damage. (-23) C2XA flt #2896, an Emb-145-XR, N17185 was parked between taxiways "w" and "y" facing north pending departure from ewr airport. Both engines were shut…

## Service difficulty reports (42)

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 JJBA20220112022](https://openairdocs.org/sdr/JJBA20220112022), Jan 12, 2022: CABLE. OUT OF LIMITS. LEFT RUDDER AP SERVO CABLE CONNECTION FOUND TO BE OUT OF LIMITS. ADJUSTED LEFT RUDDER AP SERVO CABLE. TENSION CHECK SAT.
- [SDR JJBA202201182021](https://openairdocs.org/sdr/JJBA202201182021), Jan 12, 2022: CABLE. OUT OF LIMITS. RIGHT RUDDER AP SERVO CABLE CONNECTION FOUND TO BE OUT OF LIMITS. ADJSUTED RIGHT RUDDER AP SERVO CABLE. TENSION CHECK SAT.
- [SDR JJBA20210529032](https://openairdocs.org/sdr/JJBA20210529032), May 29, 2021: BULB. INOPERATIVE. MCD AND SERVICE DOOR EXTERNAL EMERGENCY LIGHTS INOPERATIVE. R&R BULB AT SERVICE DOOR EMERGENCY LIGHT. OPS CHECK SAT. REMOVED MCD EXTERNAL EMERGENCY LIGHT HOUSIN
- [SDR ASOA2020032405011](https://openairdocs.org/sdr/ASOA2020032405011), Mar 20, 2020: FUSE. BLOWN. PILOT REPORTED EMERGENCY LIGHT NEXT TO THE GALLEY IS NOT WORKING. MX REMOVED AND REPLACED FUSE 9 AT BATTERY TRAY #1 WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVE
- [SDR ASOA201911297135](https://openairdocs.org/sdr/ASOA201911297135), Nov 29, 2019: SUPPORT PLATE. CORRODED. VENTRAL TANK FORWARD O/B SKIN FUEL LINE SHROUD SUPPORT DOUBLER CORRODED. REMOVED CORRODED BRACKET, REMOVED PREVIOUSLY INSTALLED REPAIR, CUT-OUT DAMAGED AREA ON 
- [SDR ASOA2019111907134](https://openairdocs.org/sdr/ASOA2019111907134), Nov 19, 2019: RIB. CRACKED. TYS A/C IS IN FOR A C-CHECK INSPECTION WHEN MAINTENANCE FOUND THE L/H WING AT RIB 21 CRACKED. MAINTENANCE REPAIRED THE RIB 21 IAW ETD 2019-145-153596. ALL WORK 
- [SDR ASOA201705155075](https://openairdocs.org/sdr/ASOA201705155075), May 15, 2017: MECHANISM. OUT OF ADJUST. CREW REPORTED CABIN DOOR WILL NOT OPEN FROM INSIDE. MX ADJUSTED DOOR OPEN AND CLOSE MECHANISM WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVIC
- [SDR ASOA201704123077](https://openairdocs.org/sdr/ASOA201704123077), Apr 12, 2017: FLOORBEAM. CORRODED. CENTER FUSELAGE 4 RT FLOORBEAM UNDER GUSSET CORRODED AT ANCHOR NUT LOCATION. 61 REPAIRED IAW ETD2017-145-028579. HFEC PERFORMED WITH NO FAULT FOUND.
- [SDR ASOA201704113076](https://openairdocs.org/sdr/ASOA201704113076), Apr 12, 2017: FRAME. CORRODED. CARGO DOOR AFT AND FWD L-SHAPE CORRODED. BAGGAGE DOOR AFT L-SHAPE REPROTECTED IAW 51-21-05/04. BAGGAGE DOOR FWD L-SHAPE CORROSION REMOVED IAW 53-31-04. HFEC PER
- [SDR ASOA201704113075](https://openairdocs.org/sdr/ASOA201704113075), Apr 11, 2017: BULKHEAD. CRACKED. LEFT WHEEL WELL AFT BULKHEAD CRACKED UPEER OUTBOARD CORNER. THE BULKHEAD UPPER OUTBOARD CORNER WAS REPAIRED IAW SRM 53-23-12 AND ETD2017-145-027457.
- [SDR ASOA201704113074](https://openairdocs.org/sdr/ASOA201704113074), Apr 11, 2017: BULKHEAD. CRACKED. R/H WHEELWELL AFT BULKHEAD CRACKED UPPER OUTBOARD CORNER. RT WHEEL WELL AFT BULKHEAD UPPER OUTBOARD CORNER REPAIRED IAW SRM 53-23-12 AND ETD2017-145-027457. HFE
- [SDR ASOA201704113073](https://openairdocs.org/sdr/ASOA201704113073), Apr 11, 2017: SUPPORT. CRACKED. WING TO BODY FAIRING ANGLE CRACKED AT RT TOP NR 1 AFT END. THE ANGLE WAS REPAIRED IAW SRM 53-21-12 AND ETD2017-145-027506.
- [SDR ASOA201704113072](https://openairdocs.org/sdr/ASOA201704113072), Apr 11, 2017: SKIN. CORRODED. CORROSION FOUND ON FUSELAGE SKIN AROUND AFT RADIO ALTIMETER AT FRAME 68. SKIN AREA UNDER AFT RADIO ALT ANTENNA REPAIRED IAW ETD2017-145-027855. AFT RADIO ALT AN
- [SDR ASOA201704113071](https://openairdocs.org/sdr/ASOA201704113071), Apr 11, 2017: SKIN. CORRODED. FUSELAGE SKIN UNDER RADIO ALTIMETER ANTENNA BASE CORRODED, BETWEEN FRAMES 65 & 66. BLENDED IAW ETD2017-145-027855. HFEC PERFORMED ON REPAIRED AREA WITH NO FAULT
- [SDR ASOA201704053068](https://openairdocs.org/sdr/ASOA201704053068), Apr 5, 2017: FLOOR SUPPORT. CORRODED. RIGHT OTBD FLOOR SUPPORT AT FRAMES 49 AND 51 CORRODED. REPLACED IAW SRM 51-40-02..
- [SDR ASOA201704053067](https://openairdocs.org/sdr/ASOA201704053067), Apr 5, 2017: FLOOR SUPPORT. CORRODED. LEFT OTBD FLOOR SUPPORT AT FRAME 51 CORRODED. REPLACED IAW SRM 51-40-02.
- [SDR ASOA20160228015H](https://openairdocs.org/sdr/ASOA20160228015H), Feb 28, 2016: BATTERY PACK. DISCHARGED. DURING MAINTENANCE INSPECTION THE RT & LT FORWARD EXTERIOR OVERWING LIGHTS AND THE FWD AISLE EMERGENCY LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE
- [SDR ASOA20160202003](https://openairdocs.org/sdr/ASOA20160202003), Feb 2, 2016: INVERTER. ABNORMAL. THE FWD SIDE EMERGENCY LIGHTS AT THE OVERWING EXIT WAS REPORTED INOPERATIVE. MAINTENANCE R & R NR 6 INVERTER FOR EMERGENCY LIGHT SYS WITH OPS CHECK GOOD. ACFT W
- [SDR ASOA20140917281](https://openairdocs.org/sdr/ASOA20140917281), Sep 17, 2014: SKIN. CRACKED. DURING C-CHECK, LT FUSELAGE SKIN IS CRACKED AROUND RIVET AT FRAME 79. LEFT FUSELAGE SKIN WAS REPAIRED IAW EC5330-02940.
- [SDR ASOA20140917280](https://openairdocs.org/sdr/ASOA20140917280), Sep 17, 2014: SKIN. CRACKED. DURING C-CHECK, RT FUSELAGE SKIN IS CRACKED AROUND RIVET AT FRAME 79. REPAIRED FUSELAGE SKIN IAW EC5330-02940. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140917279](https://openairdocs.org/sdr/ASOA20140917279), Sep 17, 2014: DOOR SILL. CORRODED. DURING A C-CHECK. CORROSION WAS FOUND ON THE SERVICE DOOR CUTOUT CENTER SILL. REPAIRED SERVICE DOOR CENTER SILL IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN T
- [SDR ASOA20140913277](https://openairdocs.org/sdr/ASOA20140913277), Sep 13, 2014: THRESHOLD. CORRODED. DURING C-CHECK, CARGO CUTOUT THRESHOLD CORRODED, LOCAL LEVEL 2, FRAMES 65-68. MAINTENANCE R & R CARGO CUTOUT THRESHOLD BETWEEN FRAMES 65-68 IAW SRM 51-40-02. TH
- [SDR ASOA20140913276](https://openairdocs.org/sdr/ASOA20140913276), Sep 13, 2014: VALVE. CORRODED. DURING C-CHECK, TOILET WASTE VALVE SUPPORT HAS CORROSION. MAINTENANCE R & R TOILET WASTE VALVE SUPPORT ASSY IAW SRM 51-40-02 AND IS DETERMINED TO BE MAJOR IAW S
- [SDR ASOA20140913275V](https://openairdocs.org/sdr/ASOA20140913275V), Sep 13, 2014: BUSHING. MIGRATED. DURING C-CHECK, RUDDER II UPPER CENTER HINGE HAS A MIGRATED HAT BUSHING, SECOND FROM TOP. MAINTENANCE R & R RUDDER II UPPER CENTER HINGE IAW SRM 51-40-02. THE A
- [SDR ASOA20140913274](https://openairdocs.org/sdr/ASOA20140913274), Sep 13, 2014: BUSHING. MIGRATED. DURING C-CHECK, LOWER RUDDER ACTUATOR FITTING HAT BUSHING MISSING AT RUDDER I. MAINTENANCE R & R LOWER RUDDER ACTUATOR FITTING AT RUDDER I IAW SRM 51-40-02. THE
- [SDR ASOA20131129134](https://openairdocs.org/sdr/ASOA20131129134), Nov 29, 2013: INVERTER. INOPERATIVE. PILOT REPORTED EMERGENCY LIGHT INOPERATIVE. MAINTENANCE R & R NR 1 EMERGENCY LIGHT INVERTER WITH OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140224033](https://openairdocs.org/sdr/ASOA20140224033), Feb 24, 2013: SKIN. SCRATCHED. DURING WALKAROUND INSPECTION, A SCRATCH WAS DISCOVERED IN THE AFT FUSELAGE SKIN BETWEEN FRAMES 69-70 AND EXTENDING BETWEEN STRINGERS 14L-15L. MAINTENANCE BLENDE
- [SDR ASOA20120814061](https://openairdocs.org/sdr/ASOA20120814061), Aug 14, 2012: INVERTER. INOPERATIVE. DURING MX INSP THE LT LOWER INTERIOR EMERGENCY EXIT IDENTIFIER WAS FOUND INOPERATIVE. MX R & R NR 5 INVERTER AND SIGN WITH OPS CHECKS SUCCESSFUL. ACFT WAS APPRO
- [SDR ASOA2012010900001](https://openairdocs.org/sdr/ASOA2012010900001), Jan 9, 2012: LANDING GEAR. MALFUNCTIONED. TOWER REPORTED TO DEPARTURE THAT THE LT MLG NOT FULLY RETRACTED ON T/O. THE CREW REPORTED NORMAL INDICATIONS IN THE COCKPIT WITH ALL GEAR UP AND LOCKED. THE CRE
- [SDR C2XA11RI154](https://openairdocs.org/sdr/C2XA11RI154), Sep 17, 2011: CONNECTOR. DISCONNECTED. RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND SEAT 12A LOWER EXIT EMERGENCY LIGHT INOPERATIVE. MX FOUND THE CONNECTOR FOR THE LIGHT TO BE LOOSE. MX RECONNECTED
- [SDR C2XA11IA164](https://openairdocs.org/sdr/C2XA11IA164), Jul 29, 2011: SENSOR. INOPERATIVE. IAH - FLIGHT 2053, THE CREW REPORTED A FUEL CONFIG DISAGREE MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPL
- [SDR C2XA10TY168](https://openairdocs.org/sdr/C2XA10TY168), Oct 25, 2010: SMOKE DETECTOR. DEFECTIVE. TYS - A/C JUST CAME OUT OF C-CHECK WHEN THE LAV SMOKE DETECTOR WOULDN'T TEST. MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR IAW AMM 26-14-01. OPS CHEC
- [SDR C2XA10CL160](https://openairdocs.org/sdr/C2XA10CL160), Oct 22, 2010: WIRE. BURNED. DURING MAINTENANCE THE APU GENERATOR WIRE WAS FOUND BURNED UNDER THE CARGO FLOOR. THE WIRE WAS BURNED AT THE MANUFACTURE SPLICE WHERE THE WIRE CHANGES FROM COPP
- [SDR C2XA10TY166](https://openairdocs.org/sdr/C2XA10TY166), Oct 21, 2010: RIB. BENT. LT ELEVATOR CLOSING-RIB CAP IS BENT APPROX 10 INCHES FROM LEADING EDGE. MAINTENANCE INDUCED DAMAGE. PERFORMED DOUBLER AND FILLER REPAIR, FABRICATION, ALODINE, P
- [SDR C2XA10CL111](https://openairdocs.org/sdr/C2XA10CL111), Jul 13, 2010: GENERATOR. FAILED. THE CREW REPORTED A GENERATOR 2 BEARING FAIL MESSAGE ON TAKEOFF ROLL. MAINTENANCE INSPECTED AND REPLACED THE NR 2 GENERATOR. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10TY037](https://openairdocs.org/sdr/C2XA10TY037), Mar 11, 2010: SKIN. DENTED. DENT ON LT SIDE OF FUSELAGE FRAME 19 & 20 JUST AFT OF MAIN DOOR STR 11L & 12L. REPAIRED DENT IAW EC 5330-02087. CUT OUT DAMAGE, INSTALLED FABRICATED FILLER, INS
- [SDR C2XA10TY036](https://openairdocs.org/sdr/C2XA10TY036), Mar 11, 2010: SKIN. DENTED. DENT ON LT SIDE OF FUSELAGE FRAME 19 & 20 JUST AFT OF MAIN DOOR STR 12L & 13L. REPAIRED DENT IAW EC 5330-02087. CUT OUT DAMAGE, INSTALLED FABRICATED FILLER, INS
- [SDR C2XA09TY222](https://openairdocs.org/sdr/C2XA09TY222), Aug 13, 2009: SKIN. DAMAGED. AIRCRAFT HAS LIGHTNING STRIKE BURN DAMAGE ON FUSELAGE SKIN AT FRM 20 STR 19L, FRM 13 STR 20L AND FRM 9 STR 18L. DRILLED DAMAGE, INSTALLED RIVET AND WASHER, PRES
- [SDR C2XA08ON109](https://openairdocs.org/sdr/C2XA08ON109), Mar 30, 2008: DUCT CLAMP. MISSING. FLT 0412 - SAN - FLIGHT CREW ABORTED T/O DUE TO NR 1 ENG EXCEEDANCE ON TAKEOFF ROLL. MX INSPECTED BLEED DUCTS AND COMPRESSOR BLEED AIR DUCTING ON ENGINE AND FOU
- [SDR C2XA07ON046](https://openairdocs.org/sdr/C2XA07ON046), Dec 27, 2007: SMOKE DETECTOR. INOPERATIVE. FLT MX - TYS - WHILE PERFORMING PLANNED MX INSPECTION THE NR 2 BAGGAGE SMOKE DETECTOR WILL NOT TEST. MX PERSONNEL REMOVED AND REPLACED NR 2 BAGGAGE SMOKE DETECT
- [SDR C2XA07ON048](https://openairdocs.org/sdr/C2XA07ON048), Dec 17, 2007: PRESSURE SWITCH. FAULTY. FLT 7652 - LAX TO LAX - FLIGHT CREW REPORTED RUDDER OVERBOOST ON CLIMBOUT OF ONT. MX PERSONNEL REMOVED AND REPLACED NR 1 RUDDER PRESSURE SWITCH. OPERATIONALLY C
- [SDR C2XA07IA220](https://openairdocs.org/sdr/C2XA07IA220), Oct 9, 2007: SMOKE WARNING. MALFUNCTIONED. IAH - FLIGHT 537, THE CREW REPORTED A BAGGAGE SMOKE INDICATION ON CLIMB. THE CARGO FIRE BOTTLES WERE DISCHARGED, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDE

## 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/N17185/stcs.md

## Earlier aircraft with N17185

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N17185 before.

- [Cancelled 1948-04-29](https://openairdocs.org/deregistered/N17185-1948-04-29): Stinson SR-9C, S/N 5303, built 1937. Owner: [Decatur Aviation Co](https://openairdocs.org/faa-owner/DECATUR%20AVIATION%20CO), [Decatur, IL](https://openairdocs.org/faa-place/IL/Decatur)

## 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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