# N33182: 2005 Embraer EMB-145XR

- Status: Valid registration
- Airframe: [Embraer EMB-145XR](https://openairdocs.org/model/embraer-emb-145xr) (registry code 3260214, 55 seats)
- Engine: [Rolls-Royce AE3007 series](https://openairdocs.org/engine/rolls-royce-ae3007-series) (registry code 54582)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 14500909
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 28, 2005
- Certificate issued: June 4, 2020
- Expires: June 30, 2027
- Mode S code: A39D11
- 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=33182
- Page: https://openairdocs.org/aircraft/N33182

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/N33182/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 N33182.

## FAA accident and incident reports

None matched to N33182.

## Service difficulty reports (90, 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 JJBA20260413008](https://openairdocs.org/sdr/JJBA20260413008), Apr 10, 2026: AMPLIFIER. MALFUNCTIONED. CABIN AND CABIN EMERGENCY LIGHT ON ICU WILL NOT EXTINGUISH. RE-RACKED PA AMP. OPS CHECK OKAY AT THIS TIME. NO FAULTS NOTED.
- [SDR JJBA20260204003](https://openairdocs.org/sdr/JJBA20260204003), Feb 2, 2026: FUSE. FAILED. LH FORWARD OF WING EMERGENCY LIGHT INOPERATIVE. INSTALLED NEW BULB. DID NOT FIX. INSTALLED NEW EMERGENCY LIGHT ASSEMBLY. DID NOT FIX. PUT BACK TO ORIGINAL CONFI
- [SDR JJBA20240130063](https://openairdocs.org/sdr/JJBA20240130063), Jan 29, 2024: DOOR. LACK OF LUBE. MAIN CABIN DOOR IS BECOMING STUCK WHILE TRYING TO OPEN. LUBED AND OPS CHECK MAIN CABIN DOOR. OPS CHECK GOOD
- [SDR JJBA20231130038](https://openairdocs.org/sdr/JJBA20231130038), Nov 27, 2023: UNKNOWN. UNKNOWN. RF1 LOWER FUSELAGE, CORROSION BTW FR 61-63 LH AND AT STR 19L. LH STRINGER 19L SECTION BTW 61-66 INSTALLED AND STRINGER SPLICE COMPLETED BTW FR 65-66
- [SDR JJBA20231130037](https://openairdocs.org/sdr/JJBA20231130037), Nov 27, 2023: UNKNOWN. UNKNOWN. RF1 EXTERNAL LOWER FUSELAGE, CORROSION BTW FR 61-62A RH AND AT STR 19R. RH STRINGER 19R SECTION BTW FR 61-66 INSTALLED AND STRINGER SPLICE COMPLETED
- [SDR JJBA20231130036](https://openairdocs.org/sdr/JJBA20231130036), Nov 27, 2023: UNKNOWN. UNKNOWN. RF1 EXTERNAL LOWER FUSELAGE, CORROSION SUSPECTED BTW FR 61-63 RH AND AT STR 18R. RH STRINGER 18R SECTION BTW FR 61-66 INSTALLED AND STRINGER SPLICE COMPLETED
- [SDR JJBA20231128034](https://openairdocs.org/sdr/JJBA20231128034), Nov 24, 2023: UNKNOWN. UNKNOWN. UNRECORDED REPAIR DOUBLER FOUND ON BAGGAGE DOOR SKIN AROUND HANDLE CUT-OUT. SKIN REPAIRED WITH A DOUBLER BTW STA X22132.6-X22716.2 AND BTW HB#3-4
- [SDR JJBA20231128033](https://openairdocs.org/sdr/JJBA20231128033), Nov 24, 2023: UNKNOWN. UNKNOWN. DENT FOUND ON BAGGAGE DOOR SKIN, 7 INCHES FROM FWD SKIN EDGE AND 9.5 INCHES FROM LOWER SKIN EDGE. SKIN REPAIRED WITH A DOUBLER BTW STA X22132.6-X22716.2 AND BTW
- [SDR JJBA20231128032](https://openairdocs.org/sdr/JJBA20231128032), Nov 22, 2023: UNKNOWN. UNKNOWN. CRACKS SUSPECTED (3X) ON RH SKIN AROUND FASTENERS BTW FR 77-80 & BTW STR 3R-9R. AFTER NDT INVESTIGATION, 1 CRACK FOUND, SKIN REPAIRED WITH 1 BUSHING
- [SDR JJBA20231128031](https://openairdocs.org/sdr/JJBA20231128031), Nov 21, 2023: UNKNOWN. UNKNOWN. RA #2 FWD ANTENNA BASE FOUND CORRODED. SKIN REPAIRED WITH A DOUBLER. CORROSION LEVEL 1
- [SDR JJBA20231127024](https://openairdocs.org/sdr/JJBA20231127024), Nov 20, 2023: UNKNOWN. UNKNOWN. CF1 EXTERNAL UPPER FUSELAGE SCRATCHES FOUND UNDERNEATH TOP TCAS ANTENNA. SKIN REPAIRED WITH A DOUBLER BTW FR 16-17 AND BTW STR 1L-1R UNDER TCAS ANTENNA
- [SDR JJBA20231121014](https://openairdocs.org/sdr/JJBA20231121014), Nov 17, 2023: UNKNOWN. UNKNOWN. CF1, CRACK FOUND ON ANGLE (2X) UNDER MIDDLE GUSSET BTW FR 20-22, ON FLOOR STRUCTURE AREA. REPLACED ANGLE (2X)
- [SDR JJBA20231121013](https://openairdocs.org/sdr/JJBA20231121013), Nov 17, 2023: UNKNOWN. UNKNOWN. FWD FUSE II, FRAME 10 STR 9L ANGLE FOUND CRACKED. FWD FUSE II, FR10 STR 9L ANGLE REPLACED BY NEW ANGLE
- [SDR JJBA20231127029](https://openairdocs.org/sdr/JJBA20231127029), Nov 16, 2023: UNKNOWN. UNKNOWN. IN LH ENG PYLON, LH PRECOOLER STRUCTURE FWD BRACKET IS CRACKED. REPLACED
- [SDR JJBA20231127028](https://openairdocs.org/sdr/JJBA20231127028), Nov 16, 2023: UNKNOWN. UNKNOWN. RF2, DENT FOUND ON LH AFT DUAL STRAKES INBOARD SIDE, 1" FWD OF END RIB FR 81. DENT IS ACCEPTED
- [SDR JJBA20231127027](https://openairdocs.org/sdr/JJBA20231127027), Nov 16, 2023: UNKNOWN. UNKNOWN. NLG W/WELL, CRACK FOUND ON NLG UP-LOCK AFT CROSSBEAM. REPLACED
- [SDR JJBA20231127026](https://openairdocs.org/sdr/JJBA20231127026), Oct 24, 2023: UNKNOWN. UNKNOWN. RH OUTBD FLAP SHOUD, OUTBD HINGE FOUND CRACKED. NEW PART INSTALLED
- [SDR JJBA20231127025](https://openairdocs.org/sdr/JJBA20231127025), Oct 24, 2023: UNKNOWN. UNKNOWN. CF1, CRACKS (3X) FOUND ON LH OMEGA BEAM #1 FLOOR STRUCTURE BTW FR 18-24. REPLACED
- [SDR JJBA20231127023](https://openairdocs.org/sdr/JJBA20231127023), Oct 24, 2023: UNKNOWN. UNKNOWN. CF1, CRACK FOUND ON FUEL RELAY AVIONIC BOX RH FWD SUPPORT BTW FR 15-16 AND BTW STR 7R-9R. CF1, ON FUEL RELAY AVIONIC BOX RH FWD SUPPORT BTW FR 15-16 AND BTW STR
- [SDR JJBA20231127022](https://openairdocs.org/sdr/JJBA20231127022), Oct 24, 2023: UNKNOWN. UNKNOWN. LH OUTBD FLAP SHROUD, OUTB HINGE EYELET FOUND CRACKED. LH OUTBD FLAP SHROUD OUTBD HINGE REPLACED
- [SDR JJBA20231121015](https://openairdocs.org/sdr/JJBA20231121015), Oct 24, 2023: UNKNOWN. UNKNOWN. CF1, FRAME 16, RH SHEAR CLIP FOUND CRACKED BTW STR 15R-16R. ON CF1, FRAME 16, RH SHEAR CLIP REPLACED BTW STR 15R-16R
- [SDR JJBA20230710006](https://openairdocs.org/sdr/JJBA20230710006), Jul 6, 2023: UNKNOWN. UNKNOWN. MAIN CABIN DOOR HARD TO OPEN. LUBED MCD & OPS CHECKED GOOD
- [SDR JJBA20230103003](https://openairdocs.org/sdr/JJBA20230103003), Jan 3, 2023: LIGHT. DETACHED. EMERGENCY LIGHTING STRIP ON THE FLOOR BY SEAT 1A IS DETACHED. RESECURED 1A LIGHT STRIP.
- [SDR JJBA20220825027](https://openairdocs.org/sdr/JJBA20220825027), Aug 24, 2022: NONE. OUT OF ADJUST. L/G AIR GROUND FAIL AFTER TAKE OFF. UNABLE TO RETRACT L/G ADJUSTED NLG TORQUE LINK PROX SWITCH. CONDUCTED GEAR RETRACTION AND EXTENSION. OPS CHECK SAT.
- [SDR JJBA20220514025](https://openairdocs.org/sdr/JJBA20220514025), May 14, 2022: NONE. INOPERATIVE. FLAP FAIL WHEN SELECTING FLAPS 9 ON APPROACH. REMOVED AND REPLACED FECU AND FLAP DRIVE UNIT.
- [SDR JJBA20211201002](https://openairdocs.org/sdr/JJBA20211201002), Dec 1, 2021: NONE. NONE. FWD MOST EMERGENCY LIGHT STRIP UNSECURE. RESECURED FWD EMERGENCY LIGHT STRIP
- [SDR JJBA20210913032](https://openairdocs.org/sdr/JJBA20210913032), Sep 13, 2021: SKIN. CRACKED. RF 1, BTW FR 77-79 BTW STR 3R-9R, CRACK SUSPECTED AROUND FASTENERS. RF1, BTW FR77-79 BTW 3R, 9R PAINT REMOVED AROUND FASTENERS FOR INVESTIGATION CRACK CONFIRMED
- [SDR JJBA2021090830024](https://openairdocs.org/sdr/JJBA2021090830024), Aug 30, 2021: FRAME. CORRODED. CENTER FUSE IV UNDER FLOOR, FRAME 59 CORRODED. CENTER FUSE IV UNDERFLOOR FR59 HAS EXFOLIATED CORROSION AND IS OUT OF LIMITS. PERFORMED CUT OUT FRAME SECTION BTW
- [SDR JJBA2021090830023](https://openairdocs.org/sdr/JJBA2021090830023), Aug 30, 2021: YOKE. CRACKED. 2X CRACK FOUND ON PYLON YOKES UPPER FLANGE AT 2X HOLE LOCATION. INSTALLED LH AND RH BUSHINGS AND PERFORMED COLD WORK BUSHING HOLES THEN REAMED FULL SIZE AND INS
- [SDR JJBA20210116016](https://openairdocs.org/sdr/JJBA20210116016), Jan 16, 2021: CONTROL UNIT. INOPERATIVE. FLAP FAIL 0-9 DEGREES ON APPROACH. PERFORMED GVI OF INBOARD AND OUTBOARD FLAPS. FOUND DAMAGE TO ALL FLAP TRACKS. SUSPECT DAMAGE TO FLAP DRIVE SHAFTS. FOUND FECU
- [SDR JJBA20210116015](https://openairdocs.org/sdr/JJBA20210116015), Jan 16, 2021: FLAP SYSTEM. MALFUNCTIONED. FLAP FAIL 0-9 DEGREES ON APPROACH. OPERATIONAL CHECK OF FLAPS. INSPECTED FVS. NO DEFECTS NOTED.
- [SDR JJBA20210111009](https://openairdocs.org/sdr/JJBA20210111009), Jan 11, 2021: WARNING MESSAGE. FALSE ACTIVATION. EICAS FLAP FAIL ON FINAL APPROACH. FLAP POS SHOWING 1. CHECKED ELEC CONNECTORS ON FECU, VEL SENSORS, AND FPRU. PERFORMED GVI ON FLAP MECH LINE. OPERATIONS CHECK
- [SDR JJBA201912164002](https://openairdocs.org/sdr/JJBA201912164002), Dec 14, 2019: TERMINAL. LOOSE. SERVICE DOOR EXTERNAL EMERGENCY LIGHT FLICKERS. R&R BROKEN SERVICE DOOR BONDING JUMPER AND RESECURED GROUND TERMINAL OF THE SERVICE DOOR EMERGENCY LIGHT LAMP. O
- [SDR JJBA201910075004](https://openairdocs.org/sdr/JJBA201910075004), Oct 5, 2019: LIGHT. INOPERATIVE. MAIN DOOR HINGE EMERGENCY LIGHT INOPERATIVE. R&R MAIN DOOR HINGE EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.
- [SDR JJBA20190919005](https://openairdocs.org/sdr/JJBA20190919005), Sep 19, 2019: SKIN. DENTED. FUSELAGE CF1 14" AFT OF MAIN CABIN DOOR HAS DENT/GOUGE IN AREA OF PREVIOUS DENT. PERMANENT REPAIR IS DUE WITHIN 50 CYCLES.
- [SDR JJBA20190521010](https://openairdocs.org/sdr/JJBA20190521010), May 21, 2019: CONTROLLER. INOPERATIVE. LOST PRESSURIZATION AT 30,000 FT IN AUTOMATIC MODE. AS DESCENDING TO 30,000 FEET AND AFTER LEVELING OFF, PRESSURIZATION BEGAN A SLOW CLIMB TO ABOUT 14,000 USING
- [SDR JJBA2019021309009](https://openairdocs.org/sdr/JJBA2019021309009), Feb 9, 2019: LIGHT. DAMAGED. AFT RIGHT HAND EMERGENCY FLOOR LIGHTING IS DAMAGED. ALSO, ALL PLASTIC COVERS NEED TO BE CLEANED OR REPLACED PER CUSTOMER. REMOVED AND REPLACED AFT RIGHT HAND EM
- [SDR JJBA2019021309008](https://openairdocs.org/sdr/JJBA2019021309008), Feb 9, 2019: FLOOR SUPPORT. CORRODED. OMEGA BEAM AT Y=0 AND FR 20 CORRODED. REMOVED AND REPLACED ENTIRE OMEGA BEAM AT Y=0 AND FR 20
- [SDR JJBA2019021307007](https://openairdocs.org/sdr/JJBA2019021307007), Feb 7, 2019: FLOOR SUPPORT. CORRODED. OMEGA BEAM REPAIR AT -Y=479.0 AND FR 20 CORRODED. INSTALLED NEW REPAIR PARTS EXTERNAL ANGLE, FILLER AND 2 EA SHIMS.
- [SDR JJBA2019021304006](https://openairdocs.org/sdr/JJBA2019021304006), Feb 4, 2019: DOOR FRAME. CORRODED. CORROSION ON LOWER SERVICE DOOR FRAME CHANNEL AROUND 3 EA FASTENER HOLES (MARKED). REMOVED AND REPLACED SERVICE DOOR LOWER BEAM.
- [SDR JJBA2019021304005](https://openairdocs.org/sdr/JJBA2019021304005), Feb 4, 2019: SKIN. DENTED. FUSELAGE DENTED BETWEEN FR 73 AND FR 74, STR 18R - 21R MARKED WITH GREEN DOT. COMPLIED WITH ETD 2019-145-012414 FOR PERMANENT ACCEPTANCE/REPAIR OF DENT/DAMAGE O
- [SDR JJBA201902131052](https://openairdocs.org/sdr/JJBA201902131052), Jan 31, 2019: SKIN. DENTED. FUSELAGE SKIN DENTED BELOW STGR 11L BETWEEN FR 19 AND 20. EVALUATED (2 EACH) SKIN DENTS BELOW STGR 11L BETWEEN FR 19 & 20. DENT (1) LOCATED AT FR 19 + 11" HAS A
- [SDR JJBA201902131051](https://openairdocs.org/sdr/JJBA201902131051), Jan 31, 2019: SKIN. DENTED. FUSELAGE SKIN HAS A PROTRUDING DENT BETWEEN STGR 17R & 18R; BETWEEN FR 22 & 23. EVALUATED PROTRUDING DENT BETWEEN STGR 17R & 18R AND FR 22 & 23. AREA = .048"L X
- [SDR JJBA2018061907001](https://openairdocs.org/sdr/JJBA2018061907001), May 7, 2018: UNKNOWN. SMOKE. SMOKE AND FUMES IN THE CABIN, FUMES IN COCKPIT SHORTLY AFTER TAKEOFF. R & R THE NR 1 HEAT EXCHANGER. OPS CHECKED GOOD. LEAK CHECK GOOD. FOUND GRATE ASSEMBLY DAM
- [SDR JJBA201804295008](https://openairdocs.org/sdr/JJBA201804295008), Apr 25, 2018: COUPLING. DAMAGED. DURING CLIMB, BETWEEN FL200 FL280, AN EICAS WARNING MESSAGE FOR ICE CON A/I INOPERATIVE. WHILE RUNNING THE CHECKLIST, THE MESSAGE DISAPPEARED. A FEW SECONDS LAT
- [SDR JJBA20171216011](https://openairdocs.org/sdr/JJBA20171216011), Dec 16, 2017: BATTERY PACK. DISCHARGED. THREE CABIN EMERGENCY LIGHTS INOPERATIVE. CHARGED THE BATTERIES AND PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM. OPS CHECK GOOD.
- [SDR JJBA20171208009](https://openairdocs.org/sdr/JJBA20171208009), Dec 8, 2017: RECEPTACLE. DAMAGED. DAMAGE TO EXTERNAL POWER RECEPTACLE AND SURROUNDING STRUCTURE. REMOVED EXTERNAL POWER RECEPTACLE IAW EMB 145 AMM 24-40-01. REMOVED EXTERNAL POWER RECEPTACLE HOU
- [SDR JJBA20171206003](https://openairdocs.org/sdr/JJBA20171206003), Dec 6, 2017: LIGHT. INOPERATIVE. ENTRY DOOR EMERGENCY LIGHT INOP. R&R LIGHT BULB. OPS CHECK SAT.
- [SDR JJBA20170925033](https://openairdocs.org/sdr/JJBA20170925033), Sep 25, 2017: BULB. INOPERATIVE. AFT CEILING EMERGENCY LIGHT INOPERATIVE. R & R THE BULB, OPS CHECKED GOOD.
- [SDR JJBA20170320012](https://openairdocs.org/sdr/JJBA20170320012), Mar 20, 2017: BULB. INOPERATIVE. GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.

All 90: https://openairdocs.org/aircraft/N33182/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/N33182/stcs.md

## Earlier aircraft with N33182

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N33182 before.

- [Cancelled 1991-08-08](https://openairdocs.org/deregistered/N33182-1991-08-08): Cessna TU206F, S/N U20602657. Exported to Mexico. Owner: [Eddora Inc](https://openairdocs.org/faa-owner/EDDORA%20INC), [Sedona, AZ](https://openairdocs.org/faa-place/AZ/Sedona)

## 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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