# N17138: 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: 145727
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2005
- Certificate issued: October 22, 2019
- Expires: October 31, 2029
- Mode S code: A11FC6
- 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=17138
- Page: https://openairdocs.org/aircraft/N17138

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/N17138/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 N17138.

## FAA accident and incident reports

None matched to N17138.

## Service difficulty reports (148, 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 JJBA20260728018](https://openairdocs.org/sdr/JJBA20260728018), Jul 28, 2026: LAMP. BURNED OUT. AFT AISLE EMERGENCY LIGHT BURNED OUT. REMOVED AND REPLACED AFT AISLE EMERGENCY LIGHT LAMP. OPS CHECK GOOD
- [SDR JJBA20250822045](https://openairdocs.org/sdr/JJBA20250822045), Aug 18, 2025: ELEC CONNECTOR. FAULTED. FLAP FAIL, SPS ADVANCED EICAS MESSAGE DISPLAYED AFTER MOVING FLAP HANDLE DURING APPROACH. REMOVED AND REPLACED ELECTRICAL CONNECTOR PLUG P1104. FLAPS OPS CHECK 
- [SDR JJBA20250805132](https://openairdocs.org/sdr/JJBA20250805132), Jul 31, 2025: INVERTER. INOPERATIVE. RIGHT EMERGENCY EXIT HATCH UPPER LIGHT PLACARD INOPERATIVE. REMOVED AND REPLACED INVERTER ASSEMBLY AT POSITION 5. OPS CHECK SAT.
- [SDR JJBA20250716045](https://openairdocs.org/sdr/JJBA20250716045), Jul 13, 2025: FLAP SYSTEM. FAILED. FLAP FAIL WHILE MOVING FROM 9 TO 22. FLAP SURFACES AND FSL ARE SET TO 9 DEGREES. ALSO, CONNECTORS P3683 AND P3682 ARE DISCONNECTED AND SECURED FOR FLAPS 9 FERRY
- [SDR JJBA20250609008](https://openairdocs.org/sdr/JJBA20250609008), Jun 8, 2025: PANEL. OUT OF POSITION. MCD WONT CLOSE, TOP PANEL HAS GAP AND EXTERNAL HANDLE NOT FLUSH. PERFORMED MCD ADJUSTMENT/TEST AND PERFORMED CHECK WITH THE FORCE GAUGE. LOAD IS WITHIN LIMITS, 
- [SDR JJBA20250602004](https://openairdocs.org/sdr/JJBA20250602004), Jun 1, 2025: LAMP. INOPERATIVE. MCD EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MCD EXTERNAL EMERGENCY LIGHT. OPS CHECK SAT.
- [SDR JJBA20250602003](https://openairdocs.org/sdr/JJBA20250602003), Jun 1, 2025: LAMP. INOPERATIVE. CENTER AISLE CEILING EMERGENCY LIGHT AT ROW 18 INOPERATIVE. REMOVED AND REPLACED ROW 18 CENTER AISLE CEILING EMERGENCY LIGHT. OPS CHECK SAT.
- [SDR JJBA20250512050](https://openairdocs.org/sdr/JJBA20250512050), May 11, 2025: BOLT. LOOSE. MAIN CABIN DOOR DIFFICULT TO CLOSE. FOUND INNER HANDLE BOX ATTACHMENT BOLTS TO BE LOOSE - TORQUED HANDLE BOX AND LUBRICATED DOOR. OPS CHECK SAT. NO FURTHER DEFE
- [SDR JJBA20250509045](https://openairdocs.org/sdr/JJBA20250509045), May 7, 2025: HANDLE. FAULTED. MCD EXTERIOR DOOR HANDLE NOT FULLY FLUSH. FA REPORTED LOUDER THAN NORMAL WHISTLING SOUNDS. RE-SEALED LOOSED FRAME SEAL. PERFORMED PRESSURIZATION CHECK. OPS CHEC
- [SDR JJBA20250221030](https://openairdocs.org/sdr/JJBA20250221030), Feb 18, 2025: DRIVE UNIT. FAILED. FLAP FAIL MESSAGE ON EICAS. NO FLAP CHANGE WHEN MOVING FLAP LEVER. REMOVED AND REPLACED FPDU. OPS CHECK GOOD.
- [SDR JJBA20230605001](https://openairdocs.org/sdr/JJBA20230605001), Jun 1, 2023: UNKNOWN. UNKNOWN. MAIN CABIN DOOR UNLOCKING HANDLE LOWER ROLL PIN PULLED OUT RESECURED MAIN CABIN DOOR UNLOCKING HANDLE LOWER ROLL PIN.
- [SDR JJBA20230303019](https://openairdocs.org/sdr/JJBA20230303019), Feb 27, 2023: NONE. NONE. PHOTO LUMINESCENT LIGHT STRIP LOOSE AT 3A. RESECURED EMERGENCY LIGHT STRIP AT 3A
- [SDR JJBA20221227026](https://openairdocs.org/sdr/JJBA20221227026), Dec 26, 2022: CHARGER. INOPERATIVE. LH FWD WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECK SAT.
- [SDR JJBA20220912007](https://openairdocs.org/sdr/JJBA20220912007), Sep 9, 2022: LAMP. INOPERATIVE. MCD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MCD EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT
- [SDR JJBA20220721023](https://openairdocs.org/sdr/JJBA20220721023), Jul 18, 2022: LIGHT. INOPERATIVE. RH EXTERNAL LOWER EMERGENCY LIGHT RETAINER ASSY NOT FLUSH WITH FUSELAGE AND IS MISSING SEALANT. R&R EXTERNAL LOWER EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.
- [SDR JJBA20220613010](https://openairdocs.org/sdr/JJBA20220613010), Jun 13, 2022: NONE. INOPERATIVE. AC CABIN ALT RAPIDLY CLIMBED TO 8400 THEN 9000 FEET, CAB RATE CONTINUED TO -150. CAB ALT CONTINUED TO RISE. DID A RAPID DECENT AND EMERGENCY DECLARED. OPENED BO
- [SDR JJBA20220519036](https://openairdocs.org/sdr/JJBA20220519036), May 19, 2022: NONE. LEAKING. BRAKE DEGRADED CAUTION MESSAGE ON FINAL APPROACH. ALL WHEEL SPEED SENSORS CHECKED AND FOUND SATISFACTORY. AIRCRAFT TAXIED OUT AND FOUND #2 BRAKES ON MFD HOTTER 
- [SDR JJBA20220515027](https://openairdocs.org/sdr/JJBA20220515027), May 15, 2022: LAMP. INOPERATIVE. COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT LAMP. OPS CHECK SAT.
- [SDR JJBA20220515026](https://openairdocs.org/sdr/JJBA20220515026), May 15, 2022: BATTERY PACK. INOPERATIVE. LH FWD WTF FAIRING EMERGENCY LIGHT INOPERATIVE. FOUND MULTIPLE EMERGENCY LIGHTS INOPERATIVE ON THE SAME CIRCUIT. REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY
- [SDR JJBA20211001004](https://openairdocs.org/sdr/JJBA20211001004), Oct 1, 2021: NONE. NONE. COCKPIT ENTRY FLOOR BEAM HAS SIGNS OF CORROSION, TOOLING MARKS AND INCORRECT NUT PLATE INSTALLED. REMOVED AND REPLACED DAMAGE PROFILE REINFORCEMENT AT COCKPIT E
- [SDR JJBA20211001003](https://openairdocs.org/sdr/JJBA20211001003), Oct 1, 2021: NONE. NONE. COPILOT SIDE SEAT TRACKS (INBD/OUTBD) FLOOR BEAMS SHOW SIGNS OF CORROSION. REMOVED CORROSION AND EVALUATED AREA FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOU
- [SDR JJBA20210930007](https://openairdocs.org/sdr/JJBA20210930007), Sep 30, 2021: NONE. NONE. PILOT SIDE INBD AND OUTBD SEAT TRACK FLOOR BEAMS SHOW SIGNS OF CORROSION (FS9-FS10 4WD LBL12 AND LBL24). BLENDED AREA FOUND TO BE OUT OF LIMITS IN RIGHT SIDE IN
- [SDR JJBA20210926002](https://openairdocs.org/sdr/JJBA20210926002), Sep 26, 2021: NONE. NONE. AFT FUSELAGE, UNDER TOILET AREA, RH GUSSET BEAMS, FROM FR 61 TO 59, BOTH HAT BEAMS HAS SIGNS OF CORROSION AT BOLT HOLES 4 EACH. BLENDED OUT CORROSION AND EVALUA
- [SDR JJBA20210924010](https://openairdocs.org/sdr/JJBA20210924010), Sep 24, 2021: NONE. NONE. M/D CABIN RH SIDE, AT FRAME 53 - 34 FR SIGNS OF CORROSION ALONG FLOOR SILL. REMOVED AND REPLACED FLOOR SILL ON MID CABIN RH SIDE FR 56-41 AND FR 48-52. PERFORME
- [SDR JJBA20210923006](https://openairdocs.org/sdr/JJBA20210923006), Sep 23, 2021: NONE. NONE. HAT BEAM RH AFT OF FR 59 FOUND TO HAVE CORRODED AREA AT NUT PLATE AREA. CUTOUT DAMAGE AREA. FABRICATED REPAIR DOUBLER. APPLIED ALODINE, PRIMER, TOP COAT AND INS
- [SDR JJBA20210921033](https://openairdocs.org/sdr/JJBA20210921033), Sep 21, 2021: NONE. NONE. LH FUSELAGE AT FR60 SILL AREA, SMALL PLATE FOR WATER SUPPLY HAS A CRACK AT NUT PLATE. INSTALLED EWIS PROTECTION ON LH FUSELAGE AT FR60 TO FR 59. REMOVED CABLE A
- [SDR JJBA20210919027](https://openairdocs.org/sdr/JJBA20210919027), Sep 19, 2021: NONE. NONE. RH FR19, Y=479 SUSPECT CORROSION ON HAT-BEAM. REMOVED AND REPLACED HAT BEAM AT Y=479 RH FR19 CORROSION LEVEL 2
- [SDR JJBA20210821003](https://openairdocs.org/sdr/JJBA20210821003), Aug 21, 2021: RIB. CORRODED. LH AILERON INBD RIB SHOWS SIGNS OF CORROSION. FABRICATED AND REPLACED LH AILERON INBD RIB.
- [SDR JJBA20210818048](https://openairdocs.org/sdr/JJBA20210818048), Aug 18, 2021: PANEL. CORRODED. VERTICAL STAB INSIDE PANEL 325CL THE UPPER RUDDER ACTUATOR CONNECTING HARDWARE IS CORRODED. REMOVED & REPLACED UPPER RUDDER ACTUATOR BOLT & HARDWARE
- [SDR JJBA20210719021](https://openairdocs.org/sdr/JJBA20210719021), Jul 19, 2021: TARGET. OUT OF ADJUST. LG AIR/GROUND FAIL CAUTION MESSAGE RIGHT AFTER ROTATION FOLLOWED BY ENG 1-2 REV DISAGREE. ADJUSTED NLG DOWNLOCK PROX SWITCH TARGET. OPS CHECK SAT. PERFORMED OPE
- [SDR JJBA20210523025](https://openairdocs.org/sdr/JJBA20210523025), May 23, 2021: NONE. NONE. FUEL LEAK COMING FROM PANEL 651CB. REMOVED PANEL 651 CB. FOUND FUEL IN THE DRY BAY OUTSIDE OF RIB 20. AILERON PCA`S HAD FUEL ON THEM, THE HYDRAULIC LINE CLOTH C
- [SDR JJBA20210402007](https://openairdocs.org/sdr/JJBA20210402007), Apr 2, 2021: SEAT FRAME. CRACKED. CRACKED AISLE SIDE FRAMES ON SEATS 4A, 10A, 19A, AND 22A. R&R SEATS 4A, 10A, 19A, AND 22A.
- [SDR JJBA20201213026](https://openairdocs.org/sdr/JJBA20201213026), Dec 13, 2020: BATTERY PACK. NO TEST. DURING OPERATIONS CHECKS OF EMERGENCY LIGHT FOUND SERVICE DOOR. EXIT IDENTIFIER, EXIT MARKER, EXIT LOCATOR ALL LOCATED IN GALLEY AREA INOPERATIVE. REMOVED AND I
- [SDR JJBA20201209023](https://openairdocs.org/sdr/JJBA20201209023), Dec 9, 2020: SEAT TRACK. CORRODED. LEFT AISLE UNDER SEAT TRACK NR 29 FLOOR BEAM HAS CORROSION. REMOVED AND REPLACED LEFT AISLE UNDER SEAT TRACK NR 29 FLOOR BEAM.
- [SDR JJBA20201207017](https://openairdocs.org/sdr/JJBA20201207017), Dec 7, 2020: STRINGER. DAMAGED. STRINGER HAS GROOVE CUT IN THE BOTTOM SIDE, AT FR 17X+10.562 AND STGR 15R. REMOVED DAMAGED SECTION OF STRINGER 15R BETWEEN FRAMES 15 AND 16 ENDING AT FRAME 20 A
- [SDR JJBA20201204025](https://openairdocs.org/sdr/JJBA20201204025), Dec 4, 2020: SEAT TRACK. CORRODED. LEFT AISLE, UNDER SEAT TRACK NR 31 FLOOR BEAM HAS CORROSION. REMOVED AND REPLACED LEFT AISLE UNDER SEAT TRACK NR 31 FLOOR BEAM.
- [SDR JJBA20201204024](https://openairdocs.org/sdr/JJBA20201204024), Dec 4, 2020: SEAT TRACK. CORRODED. LEFT AISLE, UNDER SEAT TRACK NR 30 FLOOR BEAM HAS CORROSION. REMOVED AND REPLACED LEFT AISLE UNDER SEAT TRACK NR 30 FLOOR BEAM.
- [SDR JJBA20201204022](https://openairdocs.org/sdr/JJBA20201204022), Dec 4, 2020: BUTTSTRAP. CORRODED. LT FLOOR STRUCTURE UNDER SEAT 1A CORROSION ON BUTT STRAP IN 2 LOCATIONS. REMOVED AND REPLACED BUTT STRAP FLOOR STRUCTURE UNDER SEAT 1A.
- [SDR JJBA20201125021](https://openairdocs.org/sdr/JJBA20201125021), Nov 25, 2020: FRAME. CORRODED. RIGHT ENGINE, FORWARD FRAME AFT FLANGE TO COMPOSITE OUTER BYPASS DUCT HAS MULTIPLE LOCATIONS OF CORROSION AROUND CIRCUMFERENCE APPROXIMATELY 60 PERCENT OF THE C
- [SDR RAIA2019121080001](https://openairdocs.org/sdr/RAIA2019121080001), Dec 8, 2019: FLAP SYSTEM. UNKNOWN. FLAP FAIL ON APPROACH AT 0 DEGREE---PERFORMED GVI OF FLAP SYSTEM AND RAN OPS CHECKS OF FLAPS,OPS CHECK GOOD ACFT OK FOR SERVICE
- [SDR RAIA201909230002](https://openairdocs.org/sdr/RAIA201909230002), Sep 23, 2019: CONTROL UNIT. INOPERATIVE. PITCH TRIM MAIN INOP FOLLOWED BY PITCH TRIM BACKUP INOP. RETURNED FROM FLIGHT AND DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. R&R HSCU AND MAIN PITCH TRIM CUTO
- [SDR RAIA2019083029001](https://openairdocs.org/sdr/RAIA2019083029001), Aug 29, 2019: FRAME. CORRODED. LOWER FRAME ON CARGO DOOR HAS CORROSION AROUND NUTPLATE HOLES. R&R LOWER FR ON CARGO DOOR.
- [SDR RAIA2019083027003](https://openairdocs.org/sdr/RAIA2019083027003), Aug 27, 2019: GUSSET. CORRODED. LH OMEGA BEAM UPPER DIGITAL SUPPORT HAS CORROSION AT FRAME 59. REMOVED & REPLACED LH OMEGA BEAM GUSSET, NUT PLATES STILL NEED TO BE INSTALLED. INSTALLED NUT PLA
- [SDR RAIA2019082970002](https://openairdocs.org/sdr/RAIA2019082970002), Aug 27, 2019: FRAME. CRACKED. COCKPIT FRAME 10 RH SIDE IS CRACKED AT UPPER END- R & R FR 10 RH.
- [SDR RAIA2019082970001](https://openairdocs.org/sdr/RAIA2019082970001), Aug 27, 2019: FRAME. CRACKED. COCKPIT FRAME 10 LH SIDE IS CRACKED AT UPPER END. R & R FRAME 10 LH.
- [SDR RAIA201908260001](https://openairdocs.org/sdr/RAIA201908260001), Aug 26, 2019: WEB. CRACKED. LT WW REAR WEB IS CRACKED AT LOWER O/B CORNER. R&R LT WW REAR WEB.
- [SDR RAIA201908200008](https://openairdocs.org/sdr/RAIA201908200008), Aug 20, 2019: SHEAR TIE. CRACKED. RT SHEAR CLIP AT FR 80 BETWEEN STR 5&6 IS CRACKED. REMOVED CRACKED SHEAR CLIP AT FRAME 80 BETWEEN STRINGERS 5&6 AND INSTALLED NEW SHEAR CLIP.
- [SDR RAIA201908200007](https://openairdocs.org/sdr/RAIA201908200007), Aug 20, 2019: SHEAR TIE. CRACKED. LT SHEAR CLIP AT FR 80 BETWEEN STR 5&6 IS CRACKED. REMOVED LT SHEAR CLIP AT FRAME 80 RT BETWEEN STRINGERS 5 & 6 AND INSTALLED HI-LOKS INTO NEW PART, AIRCRAFT RI
- [SDR RAIA2019083020006](https://openairdocs.org/sdr/RAIA2019083020006), Aug 20, 2019: FLOOR SUPPORT. CORRODED. LH FLOOR SILL HAS LIGHT CORROSION ON UPPER SURFACE BETWEEN FRAME 54 & 55 LH. REMOVED AND STARTED INSTALLING LH FLOOR SILL AT FR 54-55. FINISHED INSTALLING LH FL
- [SDR RAIA2019083020005](https://openairdocs.org/sdr/RAIA2019083020005), Aug 20, 2019: GUSSET. CORRODED. AFT LAV CENTER OMEGA BEAM UPPER DIGITAL SUPPORT HAVE CORROSION AROUND NUTPLATE HOLE AT FRAME 59. REMOVED & REPLACED AFT LAV CENTER OMEGA BEAM GUSSET, NUTPLATES 

All 148: https://openairdocs.org/aircraft/N17138/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/N17138/stcs.md

## Earlier aircraft with N17138

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N17138 before.

- [Cancelled 1990-04-03](https://openairdocs.org/deregistered/N17138-1990-04-03): Stinson SR-9E, S/N 5209. N-number assigned, not yet registered

## 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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
