# N21130: 2003 Embraer EMB-145XR

- Status: Valid registration
- Airframe: [Embraer EMB-145XR](https://openairdocs.org/model/embraer-emb-145xr) (registry code 3260214, 55 seats)
- Engine: [Rolls-Royce AE3007 series](https://openairdocs.org/engine/rolls-royce-ae3007-series) (registry code 54582)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 145704
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2005
- Certificate issued: September 2, 2025
- Expires: September 30, 2032
- Mode S code: A1C013
- Registered owner: [Avtran LLC](https://openairdocs.org/faa-owner/AVTRAN%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=21130
- Page: https://openairdocs.org/aircraft/N21130

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/N21130/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 N21130.

## FAA accident and incident reports

None matched to N21130.

## Service difficulty reports (65, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR RAIA2020022460001](https://openairdocs.org/sdr/RAIA2020022460001), Feb 16, 2020: SKIN. GOUGED. L/H FUSELAGE SKIN HAS GOUGES INSIDE OF L/H PYLON BETWEEN FR 67-68.... REPAIRED PER ETD EO-EMB145-53-073-R1 AND ETD2020-145-005726
- [SDR RAIA201902020002](https://openairdocs.org/sdr/RAIA201902020002), Feb 2, 2019: PRESSURE SWITCH. FAILED. RUDDER SYSTEM 1-2 INOP EICAS WITH AP DISCONNECT PARTIAL REVERSIONARY LANDING. ENERGIZED THE AIRCRAFT WITH HYD POWER, SELECTED RUDDER 1 & 2 ON, CYCLED RUDDER 15 
- [SDR RAIA201901200001](https://openairdocs.org/sdr/RAIA201901200001), Jan 20, 2019: SUPPORT. CRACKED. CARGO DOOR HOLD OPEN ROD CUP SUPPORT IS CRACKED. REMOVED AND REPLACED CARGO DOOR HOLD OPEN ROD SUPORT BRACKET.
- [SDR RAIA201901170001](https://openairdocs.org/sdr/RAIA201901170001), Jan 17, 2019: BRACKET. CORRODED. LAV TOILET BRACKET HAS CORROSION AROUND HDW HOLES. REMOVED AND REPLACED LAV TOILET BRACKET.
- [SDR RAIA201901110005](https://openairdocs.org/sdr/RAIA201901110005), Jan 11, 2019: FLOOR SUPPORT. CRACKED. UNDER FLOOR BOARD 231FF RAMP-AISLE LT SIDE CRACKED THAT SUPPORTS FLOOR BOARD. REMOVED AND REPLACED RAMP ANGLE FLOOR SUPPORT ON LT SIDE.
- [SDR RAIA201901110004](https://openairdocs.org/sdr/RAIA201901110004), Jan 11, 2019: CROSSBEAM. CORRODED. SURFACE CORROSION ON DIVIDER PIECE BETWEEN FLOOR BOARDS 231FF &231GF. REMOVED AND REPLACED CROSS BEAM BETWEEN FLOOR BOARDS 231FF & 231GF.
- [SDR RAIA201901110003](https://openairdocs.org/sdr/RAIA201901110003), Jan 11, 2019: GUSSET. CORRODED. SURFACE CORROSION ON 2ND GUSSET IN FROM SERVICE DOOR SILL AFT CROSS PIECE AROUND NUT PLATE SCREW HOLES. REMOVED AND REPLACED GUSSET.
- [SDR RAIA201901110002](https://openairdocs.org/sdr/RAIA201901110002), Jan 11, 2019: GUSSET. CORRODED. SURFACE CORROSION ON O/B GUSSET UNDER FLOOR BOARD 231EF RT SIDE AFT OF PAX ENTERANCE. REMOVED AND REPLACED FLOOR SILL AT FR 20-25.
- [SDR RAIA201901110001](https://openairdocs.org/sdr/RAIA201901110001), Jan 11, 2019: DOOR SILL. CORRODED. SURFACE CORROSION AT FR 32 ON LT SIDE. REMOVED AND REPLACED LT FLOOR SILL AT FR 30-35.
- [SDR RAIA201901100003](https://openairdocs.org/sdr/RAIA201901100003), Jan 10, 2019: STRUCTURE. CORRODED. CARGO DOOR HAS CORROSION ON FWD LOWER SIDE AROUND NUT PLATES. DRILLED OUT EXISTING RIVETS, FABRICATED, LOCATED, TRIMED DOUBLER REPAIR AND SHIMS. ALODINED, PRIME
- [SDR RAIA201901100002](https://openairdocs.org/sdr/RAIA201901100002), Jan 10, 2019: SKIN. CORRODED. FABRICATED, LOCATED AND TRIMMED 3 DOUBLERS REPAIR TO DAMAGE AREAS. INSTALLED REPAIRS IAW SRM 52-30-01
- [SDR RAIA201901090001](https://openairdocs.org/sdr/RAIA201901090001), Jan 9, 2019: STRUCTURE. CORRODED. FR 61 HAS CORROSION ON LT SIDE NEAR FLOOR SILL. INSTALLED DOUBLER PIECE ON FR 61.
- [SDR RAIA201901080002](https://openairdocs.org/sdr/RAIA201901080002), Jan 8, 2019: TAB. CORRODED. LT SERVO TAB CTR ROD HDW SAFETY TAB HAS CORROSION. REMOVED AND REPLACED LT SERVO TAB CTR ROD SAFETY TAB.
- [SDR RAIA201901080001](https://openairdocs.org/sdr/RAIA201901080001), Jan 8, 2019: TAB. CORRODED. RT SERVO TAB CTR ROD HDW SAFETY TAB HAS CORROSION. REMOVED AND REPLACED RT SERVO TAB CTR ROD SAFETY TAB.
- [SDR RAIA201901040002](https://openairdocs.org/sdr/RAIA201901040002), Jan 4, 2019: CROSSBEAM. CORRODED. SURFACE CORROSION ON AFT CROSS PIECE AT AFT END OF FLOOR BOARD 231GF. REMOVED AND REPLACED CROSS BEAM AT AFT END OF FLOOR BOARD 231GF.
- [SDR RAIA2018121750001](https://openairdocs.org/sdr/RAIA2018121750001), Dec 15, 2018: POWER SUPPLY. NO TEST. LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHTS INOP #5 AND #6 - R&R #4 EMERGENCY BATTERY SUPPLY, OPS CHECK GOOD
- [SDR RAIA2018091380001](https://openairdocs.org/sdr/RAIA2018091380001), Sep 8, 2018: HOSE. CRACKED. E1 HYD PUMP FAIL. WHILE R&R E1 HYDRAULIC PUMP, DISCOVERED CRACKED HYD HOSE. R&R HOSE, LK CHK GOOD.
- [SDR RAIA2018090730001](https://openairdocs.org/sdr/RAIA2018090730001), Sep 3, 2018: OIL SYSTEM. LOW. E2 OIL LOW. SERVICED NR 2 ENGINE AFTER ENGINE CHANGE. (ENGINE CHANGE)
- [SDR RAIA2018072430001](https://openairdocs.org/sdr/RAIA2018072430001), Jul 23, 2018: ANTI-ICE VALVE. MALFUNCTIONED. E-2 A/I FAIL MESSAGE DID NOT GO AWAY WITH OVER RIDE IN ENGINE OR ALL POSITION AS PER MEL. AFTER REPLACEMENT OF E2 ANTI ICE VLV FOR DMI 70041547 COMPLIED WITH OP
- [SDR RAIA201709270001](https://openairdocs.org/sdr/RAIA201709270001), Sep 27, 2017: CLAMP. LOOSE. BLEED 1 LEAK DURING CLIMB THRU 14K. PERFORMED QRH FOR THE BLEED LEAK. EMERGENCY LANDING MADE. TIGHTENED CLAMPS ON PRECOOLER DUCTS NR 1 AND 2.
- [SDR RAIA201707170001](https://openairdocs.org/sdr/RAIA201707170001), Jul 17, 2017: LENS. CRACKED. PAX DOOR SWING ARM EMERGENCY LIGHT HAD A CRACKED LENS. R & R EMERGENCY LIGHT LENS, OPS CHECKED GOOD.
- [SDR RAIA201705150001](https://openairdocs.org/sdr/RAIA201705150001), May 15, 2017: LENS. CRACKED. PAX DOOR EMERGENCY LIGHT LENS CRACKED. R & R THE LENS, OPS CHECKED GOOD.
- [SDR RAIA201701020001](https://openairdocs.org/sdr/RAIA201701020001), Jan 2, 2017: POWER SUPPLY. INOPERATIVE. LEFT FORWARD EXTERIOR EMEREGNCY LIGHT INOPERATIVE. R & R NR 1 EMERGENCY POWER SUPPPLY, OPS CHECKED GOOD.
- [SDR RAIA201606270003](https://openairdocs.org/sdr/RAIA201606270003), Jun 27, 2016: LIFE VEST. UNSERVICEABLE. OBS EMERGENCY LIFE VEST BAG TORN. R & R OBS EMERGENCY LIFE VEST.
- [SDR RAIA201511060001](https://openairdocs.org/sdr/RAIA201511060001), Nov 6, 2015: BULB. INOPERATIVE. LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.
- [SDR ASOA20150513113](https://openairdocs.org/sdr/ASOA20150513113), May 13, 2015: SUPPORT. CORRODED. DURING C-CHECK THE PAX DOOR LOWER FRAME SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5210-01343. THE
- [SDR ASOA20150513112](https://openairdocs.org/sdr/ASOA20150513112), May 13, 2015: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10. THE AC
- [SDR ASOA20141110090](https://openairdocs.org/sdr/ASOA20141110090), Nov 10, 2014: YOKE. CRACKED. DURING SCHEDULED MAINTENANCE 4A INSPECTION, THE NR 2 ENGINE LOWER FORWARD YOKE FITTING WAS FOUND TO BE CRACKED APPROXIMATELY 7MM. THE YOKE WAS REPLACED IAW ETD2
- [SDR ASOA20141110089](https://openairdocs.org/sdr/ASOA20141110089), Nov 10, 2014: YOKE. CRACKED. DURING SCHEDULED MAINTENANCE 4A INSPECTION, THE NR 1 ENGINE LOWER FORWARD YOKE FITTING WAS FOUND TO BE CRACKED APPROXIMATELY 7MM. THE YOKE WAS REPLACED IAW ETD 
- [SDR ASOA20140115007R](https://openairdocs.org/sdr/ASOA20140115007R), Jan 15, 2014: CHARGER. INOPERATIVE. DURING INSPECTION THE RT FWD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. R & R BATTERY CHARGER, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130426303](https://openairdocs.org/sdr/ASOA20130426303), Apr 26, 2013: GUSSET. CORRODED. ACFT FOR A C-CHECK WHEN CORROSION WAS FOUND ON A GUSSET AT FRAME 59 AND 61Y=0.00. MX R & R THE DAMAGED PART WITH A NEW PART IAW SRM 51-40-02 AND SRM 51-20-03. A
- [SDR ASOA20130427302](https://openairdocs.org/sdr/ASOA20130427302), Apr 26, 2013: GUSSET. CORRODED. ACFT FOR A C-CHECK WHEN CORROSION WAS FOUND AT GUSSET 0.00 AT FRAME 71 NEAR SCREW HOLES. MX REMOVED DAMAGED PART, LOCATED AND DRILL NEW PART AND INSTALL REF SRM
- [SDR ASOA20130425301](https://openairdocs.org/sdr/ASOA20130425301), Apr 25, 2013: FLOOR SUPPORT. CORRODED. CORROSION AT FLOOR SUPPORT RT FRM 71 TO 73 CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R FLOOR SUPPORT
- [SDR ASOA20130425300](https://openairdocs.org/sdr/ASOA20130425300), Apr 25, 2013: FLOOR SUPPORT. CORRODED. LT FLOOR SUPPORT IN CARGO CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R FLOOR SUPPORT.
- [SDR ASOA20130425298](https://openairdocs.org/sdr/ASOA20130425298), Apr 25, 2013: SILL. CORRODED. RIGHT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.
- [SDR ASOA20130425297](https://openairdocs.org/sdr/ASOA20130425297), Apr 25, 2013: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED BEYOND LIMITS AT SCREW HOLES. R & R FLOOR SUPPORT.
- [SDR ASOA20130425296](https://openairdocs.org/sdr/ASOA20130425296), Apr 25, 2013: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED BEYOND LIMITS AT SCREW HOLES. R & R FLOOR SUPPORT.
- [SDR ASOA20130425295](https://openairdocs.org/sdr/ASOA20130425295), Apr 25, 2013: GUSSET. CORRODED. CORROSION BEYOND LIMITS ON GUSSET AT SCREW HOLES. R & R GUSSET.
- [SDR ASOA20130425294T](https://openairdocs.org/sdr/ASOA20130425294T), Apr 24, 2013: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.
- [SDR ASOA20130425293](https://openairdocs.org/sdr/ASOA20130425293), Apr 24, 2013: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.
- [SDR ASOA20130425292](https://openairdocs.org/sdr/ASOA20130425292), Apr 24, 2013: STRAP. CORRODED. CORROSION AT NUTPLATE HOLE CORRODED BEYOND LIMITS AT FR 20 ON RT OMEGA BEAM GUSSET. R & R STRAP.
- [SDR ASOA20120503034](https://openairdocs.org/sdr/ASOA20120503034), May 3, 2012: INVERTER. INOPERATIVE. DURING SCHEDULED MX INSPECTION, THE ROW 12 OVERHEAD FORWARD EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX R & R NR 6 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11, 
- [SDR ASOA20120223017](https://openairdocs.org/sdr/ASOA20120223017), Feb 23, 2012: SIGN. INOPERATIVE. DURING SCHEDULED MX INSPECTION, THE ROW 12 CEILING EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX R & R ROW 12 CEILING EMERGENCY EXIT SIGN IAW AMM 33-50-15 WITH 
- [SDR ASOA20120129009](https://openairdocs.org/sdr/ASOA20120129009), Jan 29, 2012: SIGN. INOPERATIVE. DURING SCHEDULED MX, INSP THE FORWARD FACING EMERGENCY EXIT SIGN AT 12B WAS FOUND INOPERATIVE. MX R & R THE FORWARD FACING EMERGENCY EXIT SIGN AT 12B IAW AMM 33
- [SDR C2XA11CL248](https://openairdocs.org/sdr/C2XA11CL248), Nov 8, 2011: SIGN. INOPERATIVE. THE CREW REPORTED THE EMERGENCY SIGN OVER SEAT 12A/B/C WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT SIGN. OPERATIONAL CHECKS WERE
- [SDR C2XA11TY151](https://openairdocs.org/sdr/C2XA11TY151), Sep 26, 2011: DOOR. OUT OF ADJUST. MAIN CABIN DOOR HARD TO OPEN. RE-ADJUSTED MAIN PAX DOOR IAW EMB 145XR AMM 21-31-00. PRESSURE AND OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA11SH087](https://openairdocs.org/sdr/C2XA11SH087), May 8, 2011: BEAM. CORRODED. SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145XR SRM 51-40-02. T
- [SDR C2XA11SH086](https://openairdocs.org/sdr/C2XA11SH086), May 8, 2011: HINGE FITTING. WORN. SHV - DURING C-CHECK THE LT SPEED BRAKE CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REMOVED AND REPLACED THE WOR
- [SDR C2XA10IA349](https://openairdocs.org/sdr/C2XA10IA349), Dec 30, 2010: BLEED AIR SYS. CONTAMINATED. IAH - SMOKE IN THE LAV WAS REPORTED, MAINTENANCE PURGED THE ENGINE BLEED SYSTEM, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN 
- [SDR C2XA10IA348](https://openairdocs.org/sdr/C2XA10IA348), Dec 27, 2010: ENGINE. LEAKING. IAH - DURING TAXI THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN PRIOR TO DE-ICE WITH THE NUMBER ONE ENGINE RUNNING. THE AIRCRAFT RETURNED TO THE GATE WITHOUT

All 65: https://openairdocs.org/aircraft/N21130/reports.md

## STCs that may be installed (OpenAirDocs) (56, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Embraer EMB-145XR)

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST02176AT-D](https://openairdocs.org/stc/ST02176AT-D): Installation of a Teledyne Mini Flight Data Acquistion Unit. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST02310AT](https://openairdocs.org/stc/ST02310AT): Installation of SAF-T-GLO photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST01409LA](https://openairdocs.org/stc/ST01409LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC ST01984LA-D](https://openairdocs.org/stc/ST01984LA-D): Modification and installation of passenger seats, passenger service units and filler panels, seat track covers, and seat row placards. Safran Cabin Inc
- [STC ST04219NY](https://openairdocs.org/stc/ST04219NY): Installation of SpaceX Starlink Aviation System. Aerospace Design & Compliance LLC
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST00640DE](https://openairdocs.org/stc/ST00640DE): Installation of Tropospheric Airborne Meteorolocigal Data Reporting System (TAMDAR). FLYHT Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC ST04177NY](https://openairdocs.org/stc/ST04177NY): Installation of ALI LED Cabin Lighting, Cabin and Crew AC Power Outlets, LH Fwd Closet and Misc Cabin Mods. C & L STC Holdings LLC
- [STC ST01983WI](https://openairdocs.org/stc/ST01983WI): Installation of a folding stair in the main entrance for models equipped with a side-hinged main door. Worldwide Aviation Engineering LLC
- [STC ST04212NY](https://openairdocs.org/stc/ST04212NY): Installation of Universal UNS-1Lw Flight Management System. C&L Engineering Services, LLC
- [STC ST04213NY](https://openairdocs.org/stc/ST04213NY): PAX Social Distance Floorplan Reconfiguration. C&L Engineering Services LLC
- [STC ST04281AT](https://openairdocs.org/stc/ST04281AT): Installation for the Upgrade of the NZ-2000 FMS computer for software version NZ6. Chippewa Aerospace Inc
- [STC ST03158CH-D](https://openairdocs.org/stc/ST03158CH-D): Installation of a Reconfiguration of a Cabin Floorplan. Standard Aero Business Aviation Services LLC
- [STC SA9087SC-D](https://openairdocs.org/stc/SA9087SC-D): RECORE® Hamilton Sundstrand heat exchanger, P/N 816630-1 / -2 in accordance with Honeywell LORI Sealed Drawing List SDL3869-1 Rev. A, dated June 7, 2005 or later FAA approved revision. Honeywell International Inc
- [STC ST00818DE](https://openairdocs.org/stc/ST00818DE): Installation of Honeywell Control Display Unit (CDU) model CD-830. Premier Air Center LLC d/b/a West Star Aviation
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST09858SC](https://openairdocs.org/stc/ST09858SC): Installation of cabin automatic coffee brewing system. Safran Cabin Germany Gmbh
- [STC ST03420NY](https://openairdocs.org/stc/ST03420NY): Installation of a Cabin Interior. Delta Engineering Corporation
- [STC ST02327LA](https://openairdocs.org/stc/ST02327LA): Installation of replacement proximity sensor harness assembly part numbers used on the nose and main landing gears. Safran Electrical Components USA Inc
- [STC ST10550SC](https://openairdocs.org/stc/ST10550SC): Installation of a WeatherMASTER X-Band Fuselage Nose Radome Assembly. The NORDAM Group LLC
- [STC ST04316CH](https://openairdocs.org/stc/ST04316CH): Installation of a Smartsky System in accordance with StandardAero Master Data List 1034570, Revision (C), dated March 23, 2019 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST03177NY](https://openairdocs.org/stc/ST03177NY): Installation of a Honeywell ADS-B (Out), EHS and FreeFlight GPS. Delta Engineering Corporation
- [STC ST01520WI](https://openairdocs.org/stc/ST01520WI): Installation of the Concorde RG-442 VRSLA Battery and Temperature Sensor in place of the original Nickel-Cadmium Battery. Concorde Battery Corporation
- [STC ST00361BO](https://openairdocs.org/stc/ST00361BO): Installation of a Honeywell Primus II (XS-852) ADS-B Out System. Pro Star Aviation, LLC
- [STC ST04282CH](https://openairdocs.org/stc/ST04282CH): Installation of Honeywell CD-830 Control Display Unit (CDU). Nextant Aerospace
- [STC ST01702WI](https://openairdocs.org/stc/ST01702WI): Change seating configuration to 30 passengers by removal of seats. Worldwide Aircraft Engineering LLC
- [STC ST04108CH](https://openairdocs.org/stc/ST04108CH): Installation of Gogo Business Aviation ATG-8000 High Speed Internet with Wireless Local Area Network (WLAN). Nextant Aerospace
- [STC ST04367AT](https://openairdocs.org/stc/ST04367AT): Removal of the Existing Honeywell DL-900 or DL-950 Data Loader and Installation of the Honeywell DL-1000 Data Loader. Chippewa Aerospace Inc
- [STC ST04190AT](https://openairdocs.org/stc/ST04190AT): Installation of an ADS-B Out. Chippewa Aerospace Inc
- [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST04282AT](https://openairdocs.org/stc/ST04282AT): Installation of the Honeywell DU-875 LCD Flight Display. Chippewa Aerospace Inc
- [STC ST04015AT](https://openairdocs.org/stc/ST04015AT): Installation of the Honeywell NZ-2000 FMS/GPS System with or without WAAS/LPV. Chippewa Aerospace Inc
- [STC ST09859AC](https://openairdocs.org/stc/ST09859AC): Installation of a SkyTender Beverage Trolley. ASIG LLC
- [STC ST04263AT](https://openairdocs.org/stc/ST04263AT): Modification of Interior Arrangement Configuration from 50 to 30 Passenger Seats (All Tourist Class). VIA Airlines Inc
- [STC ST04191AT](https://openairdocs.org/stc/ST04191AT): Installation of the Honeywell Sky Connect Tracker Iridium Satcom System. Chippewa Aerospace Inc
- [STC ST02524LA](https://openairdocs.org/stc/ST02524LA): Installation of TCAS version 7.0. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST03483AT](https://openairdocs.org/stc/ST03483AT): Installation of a Portable Beverage Dispensing System, P/N B43-FA-001. Dynamo Beverage Company, USA, L.L.C
- [STC ST03999AT](https://openairdocs.org/stc/ST03999AT): Installation of a Single Honeywell HF-1050 HF Communication System. Chippewa Aerospace Inc
- [STC ST01619CH](https://openairdocs.org/stc/ST01619CH): Installation of a Lavatory Service Shutoff Valve. AeroControlex Group TransDigm Inc
- [STC ST03994AT](https://openairdocs.org/stc/ST03994AT): Installation of Bleed Air Coupling Sleeve Kit. Seal Dynamics
- [STC ST02638AT](https://openairdocs.org/stc/ST02638AT): Installation of an improved aircraft toilet rinse/fill shutoff valve and asociated hardware. Parker Hannifin Corporation, Parker Aerospace
- [STC ST03890AT](https://openairdocs.org/stc/ST03890AT): Installation of an L-3 Communications Micro Quick Access Recorder (MQAR). Chippewa Aerospace, Inc
- [STC ST02882CH-D](https://openairdocs.org/stc/ST02882CH-D): Installation of a Honeywell Flight Management System (FMS #2). Standard Aero
- [STC ST02803CH-D](https://openairdocs.org/stc/ST02803CH-D): Installation of a Honeywell KHF-1050 system. Standard Aero

All 56: https://openairdocs.org/aircraft/N21130/stcs.md

## Earlier aircraft with N21130

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N21130 before.

- [Cancelled 1976-08-03](https://openairdocs.org/deregistered/N21130-1976-08-03): Cessna 182P, S/N 18261435. Exported to Canada. Owner: [Lingenfelter Michael I](https://openairdocs.org/faa-owner/LINGENFELTER%20MICHAEL%20I), [State College, PA](https://openairdocs.org/faa-place/PA/State%20College)

## 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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