# N12145: 2003 Embraer EMB-145XR

- Status: Valid registration
- Airframe: [Embraer EMB-145XR](https://openairdocs.org/model/embraer-emb-145xr) (registry code 3260214, 55 seats)
- Engine: [Allison AE-3007A1/3](https://openairdocs.org/engine/allison-ae-3007a1-3) (registry code 03036)
- 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: 145745
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 27, 2003
- Certificate issued: January 30, 2019
- Expires: January 31, 2029
- Mode S code: A05A6B
- 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=12145
- Page: https://openairdocs.org/aircraft/N12145

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

## ADs that may apply (OpenAirDocs): 89 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 (Allison AE-3007A1/3)

- [AD 2020-16-13](https://openairdocs.org/ad/2020-16-13): Turbine Engine Compressor Section · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Aug 14, 2020
- [AD 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018
- [AD 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 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 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 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 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 2008-19-51](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 101: https://openairdocs.org/aircraft/N12145/ads.md

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

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

## NTSB investigations

None matched to N12145.

## 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 20130204001899I](https://openairdocs.org/incident/20130204001899I), Feb 4, 2013: Embraer EMB-145XR (N12145), Chicago, IL, No damage. Flight departed ord and while climbing out of 700 feet, both pilots "noticed smoke billowing into the cockpit". Crew declared an emergency and requested an…

## 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 JJBA20260520024](https://openairdocs.org/sdr/JJBA20260520024), May 18, 2026: HOSE. CUT. #1 HYD LOW QTY FOLLOWED BY HYD SYSTEM 1 FAIL ON CLIMB OUT. #1 HYD LOW QTY MESSAGE CAME ON DURING CLIMB OUT OF IAH/ QTY WAS SHOWING AMBER. SAW THE CARROTS WERE S
- [SDR JJBA20260501033](https://openairdocs.org/sdr/JJBA20260501033), Apr 30, 2026: BATTERY PACK. INOPERATIVE. EXTERIOR EMERGENCY LIGHT - WING FUSELAGE FRONT FAIRING LT - INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY #1. OPS CHECK SAT. NO FURTHER DEFECTS NOTED.
- [SDR JJBA20251224030](https://openairdocs.org/sdr/JJBA20251224030), Dec 22, 2025: BATTERY PACK. INOPERATIVE. NUMBER 4 EMERGENCY LIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD.
- [SDR JJBA20251208015](https://openairdocs.org/sdr/JJBA20251208015), Dec 7, 2025: BATTERY PACK. INOPERATIVE. INTERIOR EXIT ROW EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BPS #3. OPS CHECK SAT.
- [SDR JJBA20231120012](https://openairdocs.org/sdr/JJBA20231120012), Nov 18, 2023: PUMP. INOPERATIVE. HYD SYS 1 FAIL. FOUND ENGINE DRIVEN PUMP AT FAULT, REMOVED AND INSPECTED PRESSURE AND CASE DRAIN FILTERS. OPS AND LEAK CHECK SAT. NO DEFECTS NOTED. REMOVED AND 
- [SDR JJBA20230717018](https://openairdocs.org/sdr/JJBA20230717018), Jul 16, 2023: MODULE. INOPERATIVE. EMERGENCY LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED ICU PANEL. OPS CHECK SAT.
- [SDR JJBA20210207018](https://openairdocs.org/sdr/JJBA20210207018), Feb 7, 2022: NOT REPORTED. NOT REPORTED. CNTR OMEGA BEAM - FR 46 THRU FR 53 BL "0" I/B LWR FLANGE - HAS CORROSION MULTIPLE LOCATIONS. REMOVED AND REPLACED CENTER OMEGA BEAM AT FRAME 46 THRU FR 53
- [SDR JJBA20220207017](https://openairdocs.org/sdr/JJBA20220207017), Feb 7, 2022: NOT REPORTED. NOT REPORTED. LH OMEGA BEAM FR 38 + 5 THRU FR 46 I/B LWR FLANGE HAS CORROSION MULTIPLE LOCATIONS. REMOVED AND REPLACED LH OMEGA BEAM AT FRAME 38 + 5 TO FRAME 46
- [SDR JJBA20210808026](https://openairdocs.org/sdr/JJBA20210808026), Aug 8, 2021: RELAY. FAILED. SMOKE IN THE GALLEY AND BEHIND THE F/O SEAT ON SHORT FINAL. FOUND RELAYS K0055, AND K0054 AND THEIR SOCKETS TO BE DAMAGED. ALSO, NOTED DAMAGE TO WIRES GOING TO 
- [SDR JJBA20210704005](https://openairdocs.org/sdr/JJBA20210704005), Jul 4, 2021: LIGHT. INOPERATIVE. SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R SERVICE DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK SAT.
- [SDR JJBA20210311036](https://openairdocs.org/sdr/JJBA20210311036), Mar 11, 2021: DOUBLER. NOT REPORTED. RH ELEVATOR REPAIR DOUBLER FOUND ON HORN UPPER SKIN BTW RIB YH 3222-8233 AND BTW L/E & SPAR 73.0%. REPAIR DOUBLER REWORKED.
- [SDR RAIA2019021340003](https://openairdocs.org/sdr/RAIA2019021340003), Feb 4, 2019: TEE FITTING. CORRODED. AFT CARGO BAY DOOR CUTOUT FWD T CLIP HAS CORROSION. REMOVED AND REPLACED CARGO BAY DOOR CUTOUT FWD T CLIP
- [SDR RAIA2019021300001](https://openairdocs.org/sdr/RAIA2019021300001), Feb 4, 2019: ANGLE. CORRODED. AFT CARGO BAY DOOR CUTOUT Z ANGLE HAS CORROSION. REMOVED AND REPLACED AFT CARGO BAY DOOR CUTOUT Z ANGLE
- [SDR RAIA201902040001](https://openairdocs.org/sdr/RAIA201902040001), Feb 4, 2019: DOOR SILL. CORRODED. SERVICE DOOR AFT SILL AT FRAME 22 HAS CORROSION. REMOVED CORRODED SECTION FABRICATED DOUBLER AND INSTALLED AT FRAME 22.
- [SDR RAIA201902010003](https://openairdocs.org/sdr/RAIA201902010003), Feb 1, 2019: GUSSET. CORRODED. LT LAV FLOOR GUSSET AT FRAME 61 HAS SURFACE CORROSION. REMOVED AND REPLACED LT LAV FLOOR GUSSET AT FRAME 61.
- [SDR RAIA201902010002](https://openairdocs.org/sdr/RAIA201902010002), Feb 1, 2019: GUSSET. CORRODED. MID LAV FLOOR GUSSET AT FRAME 61 HAS SURFACE CORROSION. REMOVED AND REPLACED MID LAV FLOOR GUSSET AT FRAME 61.
- [SDR RAIA201810100003](https://openairdocs.org/sdr/RAIA201810100003), Oct 10, 2018: CLAMP. LOOSE. BLEED 2 LEAK. R2 ENGINE BLEED VALVE AND BOTH CLAMPS. TIGHTENED CLAMP JUST AFT OF NR 2 PRECOOLER AND ADJUSTED PNEUMATIC DUCTS. PERFORMED OPS/LEAK TEST. NO DEFECT
- [SDR RAIA201808270001](https://openairdocs.org/sdr/RAIA201808270001), Aug 27, 2018: CLAMP. UNSECURE. BLEED 2 LEAK AT 20,000 FT IN ICING CONDITIONS. CHECKED SECURITY OF ALL BLEED 2 COUPLINGS. NO FURTHER LEAKS NOTED AT JOINTS 18, 20, 22, OR 24. SECURED 3 CLAMPS I
- [SDR RAIA201803250001](https://openairdocs.org/sdr/RAIA201803250001), Mar 25, 2018: SUPPORT. OUT OF ADJUST. MAIN CABIN DOOR WILL NOT CLOSE FROM THE INSIDE. ADJUSTED FWD UPPER ROLLER SUPPORT. OPSC CHECK GOOD AT THIS TIME.
- [SDR RAIA201610230001](https://openairdocs.org/sdr/RAIA201610230001), Oct 23, 2016: LIGHT. WORN. EMERGENCY LIGHT STRIP WORN BY 1A. R & R THE EMERGENCY LIGHT STRIP.
- [SDR RAIA201609290001](https://openairdocs.org/sdr/RAIA201609290001), Sep 24, 2016: ARMREST. DAMAGED. INBOARD ARMREST WILL NOT LOCK AT 18A. INBOARD ARMREST AT 18A PLACED ON DMI# 7009152 ON LOG PAGE 156769, ON 09/24/16. ON 09/25/16: R & R INBOARD ARMREST AT 18A, 
- [SDR RAIA20160304001](https://openairdocs.org/sdr/RAIA20160304001), Mar 4, 2016: LAMP. INOPERATIVE. EMERGENCY LIGHT LT FWD WING TO FUSELAGE FAIRING EC, EXTERIOR FLOOD LIGHT NR 3 INOPERATIVE. REPLACED THE LAMP EXTERIOR EMERGENCY FLOOD LIGHT NR 3. OPS CHECK GOOD
- [SDR RAIA201601250002](https://openairdocs.org/sdr/RAIA201601250002), Jan 25, 2016: FLASHLIGHT. INOPERATIVE. F/A FLASHLIGHT WILL NOT CHARGE. R & R THE FLASHLIGHT. OPS CHECK GOOD.
- [SDR ASOA20140829074](https://openairdocs.org/sdr/ASOA20140829074), Aug 29, 2014: MOUNT. CRACKED. DURING ROUTINE MAINTENANCE 5A INSPECTION, THE NR 1 ENGINE LOWER FORWARD MOUNT YOKE FITTING WAS FOUND CRACKED. MAINTENANCE REPLACED THE YOKE FITTING IAW SB 145-5
- [SDR ASOA20130819097](https://openairdocs.org/sdr/ASOA20130819097), Aug 19, 2013: BULB. INOPERATIVE. DURING MX INSPECTION THE AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. R & R BULB, OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130719189](https://openairdocs.org/sdr/ASOA20130719189), Jul 19, 2013: FRAME. CORRODED. DURING C-CHECK THE PAX DOOR LOWER FRAME WAS FOUND TO BE CORRODED AROUND THE NUTPLATE HOLES FOR THE DOOR LINER FASTENERS. MX REMOVED THE CORROSION AND PERFORMED 
- [SDR ASOA20130719188](https://openairdocs.org/sdr/ASOA20130719188), Jul 19, 2013: YOKE. CRACKED. DURING C-CHECK THE RT ENGINE FWD LOWER MOUNT YOKE WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MX R & R THE YOKE IAW EC5450-01073. THE ACFT WAS APPRO
- [SDR ASOA20130706183](https://openairdocs.org/sdr/ASOA20130706183), Jul 6, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10. THE ACFT WAS AP
- [SDR ASOA20130204008C](https://openairdocs.org/sdr/ASOA20130204008C), Feb 4, 2013: UNKNOWN. SMOKE. THE CREW REPORTED AT 800 FT. SMOKE BEGAN BILLOWING INTO THE COCKPIT AND CABIN THEN HAD APU FAIL MESSAGE. MX INSPECTED AND NOTICED STRONG ODOR OF DEICE FLUID WHE
- [SDR ASOA20120804067C](https://openairdocs.org/sdr/ASOA20120804067C), Aug 4, 2012: TIRE. FAILED. THE CREW REPORTED NR 3 TIRE BLEW ON TAKEOFF. PERFORMED EMERGENCY LANDING. MX REPLACED THE NR 3 AND NR 4 MAIN WHEEL ASSEMBLIES. THE ACFT WAS RELEASED FOR SERVICE
- [SDR C2XA11RI158](https://openairdocs.org/sdr/C2XA11RI158), Sep 28, 2011: SHOCK ABSORBER. DEFECTIVE. FLT 2494 EWR-MCI CREW REPORTED 3 BANGS DURING GEAR RETRACTION AFTER TAKEOFF. CREW PERFORMED AIR RETURN BACK TO EWR UNEVENTFULLY. EWR MX REMOVED AND REPLACED THE
- [SDR C2XA11CL214](https://openairdocs.org/sdr/C2XA11CL214), Sep 25, 2011: CONTROL UNIT. MALFUNCTIONED. CLE FLT 2354 THE CREW REPORTED A BANGING NOISE DURING GEAR RETRACTION. THE CREW SEEMED TO THINK IT WAS ASSOCIATED WITH THE WHEELS SPINNING. THE AIRCRAFT RETURNE
- [SDR C2XA11CL173](https://openairdocs.org/sdr/C2XA11CL173), Jul 24, 2011: WARNING SYSTEM. MALFUNCTIONED. CLE FLT 2250 THE CREW REPORTED AN APU FIRE DETECT FAIL MESSAGE ON THE EICAS DURING TAXI. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED PLACED THE APU
- [SDR C2XA11TY115](https://openairdocs.org/sdr/C2XA11TY115), Jul 19, 2011: INVERTER. INOPERATIVE. EMERGENCY LIGHT INVERTER NR 4 INOP. REMOVED AND REPLACED NR 4 INVERTER IAW EMB 145XR AMM33-50-11, OPS CHECK GOOD.
- [SDR C2XA11RI050](https://openairdocs.org/sdr/C2XA11RI050), Mar 18, 2011: SOLENOID VALVE. INOPERATIVE. FLIGHT 2909 - DCA - FLIGHT CREW REPORTED THAT UPON GEAR RETRACTION WIND NOISE HEARD FROM NOSE AREA. EWR MX REMOVED AND REPLACED NOSE GEAR DOOR SOLENOID VALVE AN
- [SDR C2XA11CL036](https://openairdocs.org/sdr/C2XA11CL036), Feb 4, 2011: PRESSURE SWITCH. FAULTY. IAH - FLT 2548 THE CREW REPORTED A NR 1 ENGINE LOW OIL PRESSURE WARNING IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPE
- [SDR C2XA10SH091](https://openairdocs.org/sdr/C2XA10SH091), Mar 7, 2010: SKIN. CRACKED. SHV - DURING C-CHECK FUSELAGE SKIN HAS CRACKS AROUND RIVETS AT FR 79 ON RT SIDE. REPAIRED SKIN IAW EC5310-02080. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH090](https://openairdocs.org/sdr/C2XA10SH090), Mar 7, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 23-30. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH088](https://openairdocs.org/sdr/C2XA10SH088), Mar 7, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK RT OMEGA BEAM BETWEEN FRAME 60-61 HAS CORROSION (LEVEL 2 LOCAL) AT NUT PLATE HOLE. MAINTENANCE PERFORMED REPAIR ON RT OMEGA BEAM BETWEEN FR
- [SDR C2XA10SH087](https://openairdocs.org/sdr/C2XA10SH087), Mar 7, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION (LEVEL 2 LOCAL) FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM BETWEEN FRAMES 16-24 IAW EMB-1
- [SDR C2XA10RI018](https://openairdocs.org/sdr/C2XA10RI018), Jan 31, 2010: DISPLAY. MALFUNCTIONED. FLIGHT 2899 - EWR - FLIGHT CREW REPORTED EICAS WENT BLANK IN FLIGHT, ACCOMPANIED BY ELECTRICAL ODOR. EWR MX REMOVED AND REPLACED EICAS DISPLAY UNIT AND PERFORME
- [SDR C2XA09CL045](https://openairdocs.org/sdr/C2XA09CL045), Apr 18, 2009: ENGINE. MALFUNCTIONED. MAINTENANCE REPORTED HAZE AND SMOKE DURING ENGINE RUNS OF THE NR 1 ENGINE WITH THE LEFT OR RIGHT COOLING PACKS ON. THE ENGINE WAS REPLACED AND OPERATIONAL CHECK
- [SDR C2XA08IA188](https://openairdocs.org/sdr/C2XA08IA188), Aug 4, 2008: PROXIMITY SENSOR. INOPERATIVE. IAH - FLIGHT 2352 - CREW REPORTED, AFTER TAKEOFF THE LANDING GEAR DID NOT INITIALLY RETRACT, AND HAD THE ASSOCIATED DISAGREE MESSAGE ON EICAS. THE ACFT LANDED A
- [SDR C2XA08IA187](https://openairdocs.org/sdr/C2XA08IA187), Aug 4, 2008: CONTROL HANDLE. INOPERATIVE. IAH-FLIGHT 2352 - THE CREW REPORTED THAT AFTER TAKEOFF THE LANDING GEAR DID NOT INITIALLY RETRACT, AND HAD THE ASSOCIATED DISAGREE MESSAGE ON EICAS. THE ACFT LA
- [SDR C2XA06TY069](https://openairdocs.org/sdr/C2XA06TY069), Oct 18, 2006: SILL. CORRODED. AIRCRAFT IN FOR 2C CHECK 602 058223 - BAGGAGE DOOR SILL FWD EDGE CORRODED. REMOVED AND REPLACED LOWER SILL IAW EMB145 SRM 51-40-02 AND AMM 21-31-00.
- [SDR C2XA06TY063](https://openairdocs.org/sdr/C2XA06TY063), Oct 12, 2006: HINGE. WORN. TYS DURING A 2C INSPECTION THE RT VERTICAL STAB SPHERICAL BEARING WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REAMED THE HOLE TO THE FIRST OVERSIZE IAW EC 5510-0
- [SDR C2XA06IA084](https://openairdocs.org/sdr/C2XA06IA084), May 27, 2006: POWER SUPPLY. DISCHARGED. IAH - FLIGHT 3170, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE ROW 12 TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, 
- [SDR C2XA06IA083](https://openairdocs.org/sdr/C2XA06IA083), May 27, 2006: BATTERY PACK. ACTIVATED. IAH - FLIGHT 3170, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE ROW 12 TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, 
- [SDR C2XA05IA115](https://openairdocs.org/sdr/C2XA05IA115), Oct 18, 2005: CONTROL VALVE. INOPERATIVE. IAH - FLIGHT 2955, CREW REPORTED A OILY BURNING ODOR IN THE COCKPIT AND FORWARD CABIN DURING DESCENT WITH A PAX OVERLOAD INDICATION IN AUTO. THE AIRCRAFT LANDED

## 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/N12145/stcs.md

## Earlier aircraft with N12145

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N12145 before.

- [Cancelled 1975-03-27](https://openairdocs.org/deregistered/N12145-1975-03-27): Cessna 172M, S/N 17261841, built 1973. Exported to Canada. Owner: [George Wm Potter Flight Training](https://openairdocs.org/faa-owner/GEORGE%20WM%20POTTER%20FLIGHT%20TRAINING), [Fulton, NY](https://openairdocs.org/faa-place/NY/Fulton)

## Related

- Other Embraer EMB-145XR aircraft: https://openairdocs.org/model/embraer-emb-145xr/aircraft.md
- The Allison AE-3007A1/3 engine: https://openairdocs.org/engine/allison-ae-3007a1-3.md

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