# N16147: 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: 145749
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 11, 2003
- Certificate issued: December 10, 2019
- Expires: December 31, 2029
- Mode S code: A0F869
- 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=16147
- Page: https://openairdocs.org/aircraft/N16147

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/N16147/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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA14CA170](https://openairdocs.org/ntsb/DCA14CA170), Sep 13, 2014: Embraer EMB 145XR (N16147), Chicago, IL, substantial damage. Probable cause: The tractor driver's failure to give way to the taxiing airplane.

## 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.

- [Accident 20140912015899A](https://openairdocs.org/incident/20140912015899A), Sep 12, 2014: Embraer EMB-145XR (N16147), O'Hare, IL, Minor damage. On September 12, 2014, at approximately 2026 CDT, express jet airlines operating as united/continental airlines, flight 4528, was impacted by a tug on the…

## Service difficulty reports (176, 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 JJBA20260813009](https://openairdocs.org/sdr/JJBA20260813009), Aug 11, 2026: LAMP. INOPERATIVE. AISLE EMERGENCY LIGHT LAMP AT ROW 18 BURNED OUT. REMOVED AND REPLACED ROW 18 AISLE EMERGENCY LIGHT LAMP. OPS CHECK SAT.
- [SDR JJBA20260518011](https://openairdocs.org/sdr/JJBA20260518011), May 14, 2026: OIL SYSTEM. OVERSERVICED. FUMES SMELLED ON TO ON OCF FROM SURFACE TO 2000 FT SIMILAR TO GASOLINE NOT JET A. INSPECTED E1/E2 INLETS. T/S USING FIM. FOUND BURNT OIL ODOR WOULD OCCUR WHEN R
- [SDR JJBA20260518008](https://openairdocs.org/sdr/JJBA20260518008), May 13, 2026: UNKNOWN. ODOR. FUMES IN COCKPIT AND CABIN ON LIFT OFF. T/S, PERFORMED ENGINES RUNS. PERFORMED PACKS OPERATION. NO ABNORMAL SMELLS OBSERVED, NO DEFECTS NOTED. FURTHER T/S INSPE
- [SDR JJBA20250731129](https://openairdocs.org/sdr/JJBA20250731129), Jul 31, 2025: DOUBLER. CORRODED. CF4, EXTERNAL POTABLE WATER DRAIN DOUBLER BTW FR 57-58 AND STR 19R-20R FOUND CORRODED. CF4 EXTERNAL POTABLE WATER DRAIN DOUBLER BTW FR 57-58 AND STR 19R-20R REM
- [SDR JJBA20250731128](https://openairdocs.org/sdr/JJBA20250731128), Jul 31, 2025: SKIN. DAMAGED. SCREWS HOLES ELONGATED ON BOTH STARKE SPLICE SKIN. STARKE SPLICE SKIN (2X) FABRICATED.
- [SDR JJBA20250731125](https://openairdocs.org/sdr/JJBA20250731125), Jul 28, 2025: SHEAR TIE. CORRODED. CF3, SHEAR CLIP AT FR 52 BTW STR 21L-21R FOUND CORRODED. CF3, SHEAR CLIP ON FR52 BTW STR 21L-21R BOTH SHEAR CLIPS BLENDED AND FOUND OUT OF LIMIT. CF3, SHEAR CLI
- [SDR JJBA20250730109](https://openairdocs.org/sdr/JJBA20250730109), Jul 28, 2025: ANGLE. CRACKED. RH WING TO BODY FAIRING, ANGLE #3 FOUND CRACKED. RH WING TO BODY FAIRING, ANGLE #3 REPLACED.
- [SDR JJBA20250728102](https://openairdocs.org/sdr/JJBA20250728102), Jul 28, 2025: RACK. CRACKED. REAR FUSELAGE I AVIONIC COMPARTMENT, AT FR 75 AND STR 14R SUPPORT ON ELECTRIC RACK CRACKED. REAR FUSE I AVIONIC COMPARTMENT AT FR 75 AND STR 14R SUPPORT ON ELEC
- [SDR JJBA20250728099](https://openairdocs.org/sdr/JJBA20250728099), Jul 28, 2025: SHEAR TIE. CRACKED. LH FR 72 BTW STR 16L-17L SHEAR CLIP FOUND CRACKED. AT FR72 BTW STR 16L-17L SHEAR CLIP REMOVED FOR REPLACEMENT. AT FR72 BTW STR 16L-17L INSTALLED.
- [SDR JJBA20250731130](https://openairdocs.org/sdr/JJBA20250731130), Jul 25, 2025: STRINGER. CORRODED. STRINGER 21R BTW FR 53-54 FOUND CORRODED. S21R BTW FR 53-54 CORROSION BLENDED AND STRINGER FOUND TO BE OUT OF LIMIT. S21R CUTOUT PERFORMED. S21L REPAIR PERFORME
- [SDR JJBA20250731127](https://openairdocs.org/sdr/JJBA20250731127), Jul 25, 2025: SPAR. CRACKED. RIGHT WING FRONT SPAR LOWER FLANGE CRACKED AT ONE HOLE. RT WING FRONT SPAR LOWER FLANGE REPAIRED WITH A DOUBLER.
- [SDR JJBA20250730118](https://openairdocs.org/sdr/JJBA20250730118), Jul 25, 2025: FLOOR SUPPORT. CORRODED. CF1, RH OMEGA BEAM FOUND CORRODED AT FR20 AND AT FR23. AFTER INVESTIGATION, NO CORROSION FOUND AT FR20, ONLY CORROSION FOUND AT FR23. AT CF1 FR23 RH OMEGA BEAM 
- [SDR JJBA20250730112](https://openairdocs.org/sdr/JJBA20250730112), Jul 23, 2025: HINGE FITTING. DAMAGED. INBD HINGE FITTING #1 NICKED ON LH AILERON. BUSHING REPAIRS AND ALTERNATE FASTENERS ON LH AILERON INBD FITTING.
- [SDR JJBA20250728100](https://openairdocs.org/sdr/JJBA20250728100), Jul 23, 2025: SHEAR TIE. CRACKED. LH FR 71 BTW STR 5L-6L SHEAR CLIP FOUND CRACKED. SHEAR CLIP FABRICATED AND INSTALLED
- [SDR JJBA20250730113](https://openairdocs.org/sdr/JJBA20250730113), Jul 22, 2025: FRAME. CRACKED. FR 59 LH FOUND CRACKED BTW STR 15L-16L. FR59 LH SPLICE REMOVED BTW STR15L-16L FOR REPAIR ACCESS. FR 59 LH BTW STR 15-16 REPAIRED
- [SDR JJBA20250728101](https://openairdocs.org/sdr/JJBA20250728101), Jul 22, 2025: SKIN. DENTED. DENT ON LH FWD FUSE I SKIN, BTW FR 6-7 AND ABOVE STR 15L, UNDER GPU ACCESS DOOR. ON LH FWD FUSE I SKIN, BTW FR 6-7 AND ABOVE STR 15L UNDER GPU ACCESS DOOR REPAI
- [SDR JJBA20250728098](https://openairdocs.org/sdr/JJBA20250728098), Jul 22, 2025: ANGLE. CRACKED. AT FR 59 LH ANGLE BTW FR 59 AND OMEGA BEAM FOUND CRACKED. AT FR59 LH ANGLE BTW FR 59 AND OMEGA BEAM REMOVED. AT FR59 LH ANGLE BTW FR 59 AND OMEGA BEAM REPLACED
- [SDR JJBA20250728095](https://openairdocs.org/sdr/JJBA20250728095), Jul 22, 2025: SHEAR TIE. CRACKED. SHEAR CLIP AT FR 59 AND BTW STR 15L-16L FOUND CRACKED. SHEAR CLIP AT FR 59 BTW STR 15L-16L REMOVED AND REPLACED
- [SDR JJBA20250730117](https://openairdocs.org/sdr/JJBA20250730117), Jul 21, 2025: CUP. CORRODED. CF4, TOILET WASTE CUP EXTERNAL SIDE FOUND CORRODED. CF4 TOILET WASTE CUP BLENDED OUT OF LIMITS. TOILET WASTE CUP REMOVED AND REPLACED
- [SDR JJBA20250723089](https://openairdocs.org/sdr/JJBA20250723089), Jul 21, 2025: PARTITION. CORRODED. RIGHT FR 61 FRAME PARTITION FOUND CORRODED AT FLOOR LEVEL. RT FR 61 FRAME PARTITION BLENDED, FOUND OUT OF LIMIT. RT FR 61 FRAME PARTITION REMOVED AND REPLACED.
- [SDR JJBA20250723086](https://openairdocs.org/sdr/JJBA20250723086), Jul 17, 2025: GUSSET. CORRODED. LH GUSSET BTW FR 59-61 FOUND CORRODED. LH GUSSET BTW FR 59-61 FOUND CORRODED OUT OF LIMIT. LH GUSSET BTW FR 59-61 REMOVED AND REPLACED
- [SDR JJBA20250723085](https://openairdocs.org/sdr/JJBA20250723085), Jul 17, 2025: SHEAR TIE. CORRODED. SHEAR CLIP AT FR 58 AND BTW STR 20R-21R FOUND CORRODED. SHEAR CLIP AT FR 58 AND BTW STR 20R-21R REMOVED AND REPLACED
- [SDR JJBA20250730116](https://openairdocs.org/sdr/JJBA20250730116), Jul 16, 2025: FLOOR SUPPORT. CRACKED. LH OMEGA BEAM AT FR 59-61 FOUND CRACKED AT 2 ANCHOR NUT LOCATION. LH OMEGA BEAM AT FR 59-61 CUTOUT AT 2 ANCHOR NUT LOCATION. LH OMEGA BEAM BTW FR 59-61 REPAIRED
- [SDR JJBA20250728103](https://openairdocs.org/sdr/JJBA20250728103), Jul 16, 2025: STRINGER. CORRODED. STR 20 RH AT FR 58 FOUND CORRODED. STR 20R CORROSION FOUND ON STRINGER AT FR 59 ALSO. STR 20R, BLENDED AND FOUND OUT OF LIMIT. STR 20R BTW FR 57-60 REMOVED AND 
- [SDR JJBA20250716057](https://openairdocs.org/sdr/JJBA20250716057), Jul 16, 2025: DOOR FRAME. CORRODED. CARGO DOOR CUT-OUT BTW FR 65-68 LOWER BEAM FOUND CORRODED. ON CARGO DOOR CUT-OUT BTW FR 65-68 LOWER BEAM REMOVED AND REPLACED
- [SDR JJBA20250723090](https://openairdocs.org/sdr/JJBA20250723090), Jul 15, 2025: PARTITION. CORRODED. LEFT FR 61 FRAME PARTITION FOUND CORRODED AT FLOOR LEVEL. LT FR 61 FRAME, PARTITION REMOVED AND REPLACED.
- [SDR JJBA20250723084](https://openairdocs.org/sdr/JJBA20250723084), Jul 15, 2025: SHEAR TIE. CORRODED. SHEAR CLIP AT FR 59 AND BTW STR 20R-21R FOUND CORRODED. SHEAR CLIP AT FR 59 AND BTW STR 20R-21R BLEND OUT OF LIMITS. SHEAR CLIP REMOVED AND REPLACED.
- [SDR JJBA20250721069](https://openairdocs.org/sdr/JJBA20250721069), Jul 15, 2025: SHEAR TIE. CORRODED. SHEAR CLIP AT FR 59 AND BTW STR 19R-20R FOUND CORRODED. SHEAR CLIP AT FR59 AND BTW STR 19R-20R REMOVED AND INSTALLED
- [SDR JJBA20250721066](https://openairdocs.org/sdr/JJBA20250721066), Jul 15, 2025: SHEAR TIE. CRACKED. RH FR 73 BTW STR 8R-10R SHEAR CLIP FOUND CRACKED. CRACKED SHEAR CLIP AT RH FR 73 BTW STR 8R-10R REMOVED AND REPLACED
- [SDR JJBA20250721064](https://openairdocs.org/sdr/JJBA20250721064), Jul 14, 2025: SHEAR TIE. CRACKED. IN REAR COMPARTMENT, BULKHEAD 80, LH SHEAR CLIP CRACKED BETWEEN STRINGER 9 AND STRINGER 11. IN REAR COMPARTMENT BULKHEAD 80 LH SHEAR CLIP BTW STRINGER 9 AND STR
- [SDR JJBA20250716056](https://openairdocs.org/sdr/JJBA20250716056), Jul 14, 2025: WINDOW FRAME. CRACKED. LOWER SIDE WINDOW CUT-OUT AREA, RH FR10 ANGLE FOUND CRACKED. AT LOWER SIDE WINDOW CUT-OUT AREA, RH FR10 ANGLE REMOVED AND REPLACED.
- [SDR JJBA20250711039](https://openairdocs.org/sdr/JJBA20250711039), Jul 11, 2025: SUPPORT. CRACKED. CF1 BTW FR 15-16 AND BTW 7R-9R SUPPORT ASSY CRACKED. CF1 BTW FR 15-16 INBD BTW STR 7R-9R SUPPORT ASSY REMOVED AND REPLACED
- [SDR JJBA20250731126](https://openairdocs.org/sdr/JJBA20250731126), Jul 10, 2025: SHEAR TIE. CORRODED. CF4, SHEAR CLIP AT FR54 BTW STR 21L-21R FOUND CORRODED. SHEAR CLIP FABRICATED AND INSTALLED.
- [SDR JJBA20250731123](https://openairdocs.org/sdr/JJBA20250731123), Jul 10, 2025: SKIN. CORRODED. INT SKIN BTW FR 61-62A AND STR 21L-19R FOUND CORRODED. REPAIR DOUBLER PERFORMED ON REAR FUSELAGE I RH LOWER SKIN AT FR62 AND BTW STR 19R-20R.
- [SDR JJBA20250731122](https://openairdocs.org/sdr/JJBA20250731122), Jul 10, 2025: FRAME. CRACKED. CF2, FR25 BTW STR 15R-16R FOUND CRACKED. CF2 FR 25 BTW STR 15R-16R CUT OUT PERFORMED. FR25 BTW STR 15R-16R PART FABRICATED. CF2 FR25 BTW STR 15R-16R REPAIRED.
- [SDR JJBA20250721067](https://openairdocs.org/sdr/JJBA20250721067), Jul 10, 2025: GUSSET. CORRODED. CENTER GUSSET BTW FR 59-61 FOUND CORRODED. CENTER GUSSET BTW FR 59-61 FOUND CORRODED OUT OF LIMIT. CENTER GUSSET BTW FR 59-61 HAS BEEN REMOVED AND REPLACED
- [SDR JJBA20250716054](https://openairdocs.org/sdr/JJBA20250716054), Jul 10, 2025: SHEAR TIE. CORRODED. SHEAR CLIP FR 65 BTW STR 17L-16L CRACKED. SHEAR CLIP AT FR65 BTW STR 17L-16L REMOVED AND INSTALLED
- [SDR JJBA20250716051](https://openairdocs.org/sdr/JJBA20250716051), Jul 10, 2025: BRACKET. CORRODED. CARGO DOOR CUT-OUT STRUCTURE, LH FR 65 AT FLOOR LEVEL BRACKET FOUND CORRODED. ON CARGO DOOR CUT-OUT STRUCTURE, LH FR 65 AT FLOOR LEVEL BRACKET REMOVED AND INSTA
- [SDR JJBA20250729106](https://openairdocs.org/sdr/JJBA20250729106), Jul 9, 2025: INLET. DAMAGED. RH ENGINE AIR INTAKE, BLENDED SPOT TO BE INVESTIGATED. REPAIR DOUBLER ON RH NACELLE AIR INLET MODULE INNER SKIN.
- [SDR JJBA20250714047](https://openairdocs.org/sdr/JJBA20250714047), Jul 9, 2025: SHEAR TIE. CRACKED. CF2 LH SHEAR CLIP FR 28 BTW STR 15L-16L CRACKED. CF2 LH SHEAR CLIP FR28 BTW STR 15L-16L REMOVED AND REPLACED
- [SDR JJBA20250730114](https://openairdocs.org/sdr/JJBA20250730114), Jul 8, 2025: SKIN. CRACKED. RF1 FUSE SKIN AT FR75 AND AT STR 2L CRACKED. SKIN AT FR75 AND AT STR 2L PAINT STRIPPED. CUT-OUT AT FR75 CRACKED LOCATION PERFORMED. SKIN AT FR75 AND AT STR 2L R
- [SDR JJBA20250730120](https://openairdocs.org/sdr/JJBA20250730120), Jul 8, 2025: SHEAR TIE. CORRODED. CF4, SHEAR CLIP AT FR 53 BTW STR 21L-21R FOUND CORRODED. CF4, SHEAR CLIPS ON FR53 BTW STR 21L-21R, BOTH SHEAR CLIPS BLENDED AND FOUND OUT OF LIMIT. AT CF4, BOTH
- [SDR JJBA20250714046](https://openairdocs.org/sdr/JJBA20250714046), Jul 8, 2025: ANGLE. CRACKED. RH INTERNAL STRUCTURE BTW FR 61-62 AND STR 4R-5R, ANGLE FOUND CRACKED. RH INTERNAL STRUCTURE BTW FR 61-62 AND STR 4R-5R ANGLE REMOVED AND REPLACED.
- [SDR JJBA20250711043](https://openairdocs.org/sdr/JJBA20250711043), Jul 8, 2025: SHEAR TIE. CRACKED. LH FR 67 BTW STR 6L-7L SHEAR CLIP FOUND CRACKED. LH SHEAR CLIP AT FR67 BTW STR 6L-7L REMOVED AND REPLACED.
- [SDR JJBA20250711041](https://openairdocs.org/sdr/JJBA20250711041), Jul 8, 2025: ANGLE. CRACKED. RH INTERNAL STRUCTURE BTW FR 67-68 AND STR 4R-5R. CARGO DOOR MECHANISM MIDDLE ANGLE FOUND CRACKED. RH INTERNAL STRUCTURE BTW FR 67-68 AND STR 4R-5R CARGO DOOR M
- [SDR JJBA20250730115](https://openairdocs.org/sdr/JJBA20250730115), Jul 7, 2025: DOUBLER. MISINSTALLED. CTR FUSELAGE I, UNRECORDED REPAIR DOUBLER FOUND ON UPPER SKIN PANEL BTW FR16-17 AND STR 3R-4R. CTR FUSELAGE, UNRECORDED REPAIR DOUBLER REMOVED. CTR FUSELAGE 1 P
- [SDR JJBA20250711008](https://openairdocs.org/sdr/JJBA20250711008), Jul 7, 2025: SHEAR TIE. CRACKED. CF2 RH SHEAR CLIP FR24 BTW STR 15R-16R CRACKED. CF2 RH SHEAR CLIP FR24 BTW STR 15R-16R REMOVED AND INSTALLED
- [SDR JJBA20250716055](https://openairdocs.org/sdr/JJBA20250716055), Jul 4, 2025: SHEAR TIE. CRACKED. SHEAR CLIP AT FR58 AND BTW STR 15L-16L FOUND CRACKED. SHEAR CLIP AT FR58 AND BTW STR 15L-16L REMOVED AND INSTALLED
- [SDR JJBA20250711006](https://openairdocs.org/sdr/JJBA20250711006), Jul 4, 2025: SHEAR TIE. CRACKED. CF2 RH SHEAR CLIP FR25 BTW STR 15R-16R CRACKED. CF2 RH SHEAR CLIP FR25 BTW STR 15R-16R REMOVED AND INSTALLED.
- [SDR JJBA20250711005](https://openairdocs.org/sdr/JJBA20250711005), Jul 4, 2025: SHEAR TIE. CRACKED. CF2 RH SHEAR CLIP FR25 BTW STR 16R-17R CRACKED. CF2 RH SHEAR CLIP FR 25 BTW STR 16R-17R REMOVED AND REPLACED.

All 176: https://openairdocs.org/aircraft/N16147/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/N16147/stcs.md

## Earlier aircraft with N16147

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N16147 before.

- [Cancelled 1937-12-17](https://openairdocs.org/deregistered/N16147-1937-12-17): Stinson SR-8A, S/N 9716. Owner: [Vaughan George Jr](https://openairdocs.org/faa-owner/VAUGHAN%20GEORGE%20JR), [Philadelphia, PA](https://openairdocs.org/faa-place/PA/Philadelphia)

## 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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