# N12552: 2002 Embraer EMB-145LR

- Status: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212, 55 seats)
- Engine: [Rolls-Royce AE-3007A1P](https://openairdocs.org/engine/rolls-royce-ae-3007a1p) (registry code 54571)
- 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: 145583
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 13, 2002
- Certificate issued: March 26, 2020
- Expires: March 31, 2030
- Mode S code: A06967
- Registered owner: [Corporate Flight Management Inc](https://openairdocs.org/faa-owner/CORPORATE%20FLIGHT%20MANAGEMENT%20INC)
- Location: [Smyrna, TN](https://openairdocs.org/faa-place/TN/Smyrna)
- Owner type: Corporation
- Owner's area on the map: 35.9628° N, 86.5297° W: Placed by OpenAirDocs at the center of ZIP code 37167, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12552
- Page: https://openairdocs.org/aircraft/N12552

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

## ADs that may apply (OpenAirDocs): 104 in force

### Matched by airframe (Embraer EMB-145LR)

- [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 2017-04-12](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 2012-19-06](https://openairdocs.org/ad/2012-19-06): Stabilizers · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 9 more. Effective Oct 29, 2012
- [AD 2011-21-15](https://openairdocs.org/ad/2011-21-15): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 7 more. Effective Nov 23, 2011
- [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 2008-10-08](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 2007-10-11](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 2006-19-04](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 2006-16-17](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
- [AD 2005-13-22](https://openairdocs.org/ad/2005-13-22): Electric fuel pumps · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jul 7, 2005
- [AD 2005-05-09](https://openairdocs.org/ad/2005-05-09): Forward upper liners · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Apr 14, 2005
- [AD 2005-04-05](https://openairdocs.org/ad/2005-04-05): Air turbine starter (ATS) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 24, 2005
- [AD 2005-01-05](https://openairdocs.org/ad/2005-01-05): Nose Landing Gear Wheel Nuts and Associated Inner and Outer Seals, and Reidentifying the Landing Gear Strut · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Feb 9, 2005

### Matched by engine (Rolls-Royce AE-3007A1P)

- [AD 2020-16-13](https://openairdocs.org/ad/2020-16-13): Turbine Engine Compressor Section · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Aug 14, 2020
- [AD 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018
- [AD 2015-02-08](https://openairdocs.org/ad/2015-02-08): Turbine wheels · Rolls-Royce AE 2100D2, AE 2100D2A, AE 2100D3 and 11 more. Effective Mar 11, 2015
- [AD 2013-26-06](https://openairdocs.org/ad/2013-26-06): High-pressure turbine (HPT) stage 2 wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Feb 7, 2014
- [AD 2011-22-03](https://openairdocs.org/ad/2011-22-03): Low-cycle fatigue cracks · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 4 more. Effective Nov 17, 2011
- [AD 2009-24-04](https://openairdocs.org/ad/2009-24-04): Fan spinner · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 5 more. Effective Dec 28, 2009
- [AD 2007-24-05](https://openairdocs.org/ad/2007-24-05): Engine oil temperature · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 8 more. Effective Jan 2, 2008
- [AD 2004-04-05](https://openairdocs.org/ad/2004-04-05): Engine oil system · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Mar 9, 2004
- [AD 2003-25-08](https://openairdocs.org/ad/2003-25-08): 1st and 2nd stage turbine spacers · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 3 more. Effective Jan 21, 2004
- [AD 2001-25-05](https://openairdocs.org/ad/2001-25-05): Compressor Cone Shafts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jan 23, 2002
- [AD 2000-18-06](https://openairdocs.org/ad/2000-18-06): Digital Electronic Controls · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 22, 2000
- [AD 2000-13-01](https://openairdocs.org/ad/2000-13-01): Turbine Wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 1, 2000
- [AD 2000-11-22](https://openairdocs.org/ad/2000-11-22): Critical Life-Limited Parts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Aug 7, 2000
- [AD 98-11-32](https://openairdocs.org/ad/98-11-32): Sump Magnetic Chip Collector Plug · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Jun 18, 1998

### Historical (superseded or no longer in force)

- [AD 2008-13-14](https://openairdocs.org/ad/2008-13-14) (historical): Fuel system limitations (FSL) · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jul 30, 2008
- [AD 2007-12-17](https://openairdocs.org/ad/2007-12-17) (historical): Metallic tubes enclosing the vent and pilot valve wires · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Jul 19, 2007
- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 2006-20-08](https://openairdocs.org/ad/2006-20-08) (historical): Rod ends of aileron power control actuator, superseding AD 99-05-04 · Embraer EMB-145, EMB-145EP, EMB-145ER and 4 more. Effective Nov 8, 2006
- [AD 2006-04-02](https://openairdocs.org/ad/2006-04-02) (historical): Pitot static heating relay K0057 · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Mar 31, 2006
- [AD 2005-26-15](https://openairdocs.org/ad/2005-26-15) (historical): Certain components of the elevator control system · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 8 more. Effective Feb 3, 2006
- [AD 2005-25-04](https://openairdocs.org/ad/2005-25-04) (historical): Tail section or rudder pedals · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Dec 23, 2005
- [AD 2001-17-04](https://openairdocs.org/ad/2001-17-04) (historical): Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Sep 5, 2001
- [AD 2000-04-09](https://openairdocs.org/ad/2000-04-09) (historical): Elevator Servo Tab and Spring Tab Hinge Fittings of the Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Mar 10, 2000
- [AD 2009-08-51](https://openairdocs.org/ad/2009-08-51) (historical): High-pressure turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 6 more. Effective May 27, 2009
- [AD 2008-19-51](https://openairdocs.org/ad/2008-19-51) (historical): AE 3007A, AE 3007A1, AE 3007A1E and 5 more
- [AD 2001-08-15](https://openairdocs.org/ad/2001-08-15) (historical): Oil System · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective May 14, 2001
- [AD 2000-09-05](https://openairdocs.org/ad/2000-09-05) (historical): Cone Shafts · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jul 5, 2000
- [AD 99-02-51](https://openairdocs.org/ad/99-02-51) (historical): Starter Shaft Seal · AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Apr 20, 1999

All 118: https://openairdocs.org/aircraft/N12552/ads.md

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

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

## NTSB investigations

None matched to N12552.

## FAA accident and incident reports

None matched to N12552.

## Service difficulty reports (73, 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 ASOA201805250134](https://openairdocs.org/sdr/ASOA201805250134), May 21, 2018: CONTROL PANEL. FAULTY. CREW REPORTED THE EMERGENCY LIGHTS TURNED ON WHEN BRIGHT/DIM SWITCH WAS PRESSED ON THE FA PANEL. MX REMOVED AND REPLACED FLIGHT ATTENDANT CONTROL PANEL ASSEMBLY
- [SDR ASOA201708065098](https://openairdocs.org/sdr/ASOA201708065098), Aug 6, 2017: TRANSDUCER. INTERMITTENT. PILOT REPORTED: AT TAXI SPEED WHEN THE PLANE HITS A BUMP IN THE PAVEMENT, ALSO RANDOMLY WITHOUT PRESSURE CHANGES ON THE BRAKE PEDALS THE PLANE SEEMS TO REDUCE T
- [SDR ASOA20160511030](https://openairdocs.org/sdr/ASOA20160511030), May 11, 2016: BLEED VALVE. FAULTY. THE CREW REPORTED ODOR OF JET FUEL COMING THROUGH THE VENTS WHILE APU POWERING THE PACKS. MAINTENANCE INSPECTED AND REPLACED APU BLEED VALVE. OPS CHECKS WERE GO
- [SDR ASOA20150906050RS](https://openairdocs.org/sdr/ASOA20150906050RS), Sep 6, 2015: WIRE HARNESS. ARCED. CREW REPORTED A BURNING ODOR FROM ROW 6 AND LIGHT PUFF OF SMOKE. MAINTENANCE R & R THE CABIN LIGHT ASSY AND HARNESS AT ROW 6. ACFT APPROVED FOR RETURN TO SERVIC
- [SDR ASOA20150906050R](https://openairdocs.org/sdr/ASOA20150906050R), Sep 6, 2015: LIGHT. SMOKE. CREW REPORTED A BURNING ODOR FROM ROW 6 AND LIGHT PUFF OF SMOKE.
- [SDR ASOA20150905052](https://openairdocs.org/sdr/ASOA20150905052), Sep 5, 2015: LIGHT. SMOKE. THE CREW REPORTED A BURNING ODOR FROM ROW 6 AND LIGHT PUFF OF SMOKE. MAINTENANCE RELEASED ACFT IAW 33-20-00-2. SUPPLEMENT TO FOLLOW.
- [SDR ASOA20141027087C](https://openairdocs.org/sdr/ASOA20141027087C), Oct 27, 2014: WIRE. CHAFED. THE CREW REPORTED ELECTRICAL BURNING ODOR COMING FROM THE CEILING AROUND THE COURTESY LIGHT AND COCKPIT. MAINTENANCE INSPECTED AND REPAIRED CHAFED WIRES. OPS CH
- [SDR ASOA20140618072](https://openairdocs.org/sdr/ASOA20140618072), Jun 18, 2014: LIGHT. NO TEST. PILOT REPORTED THE EMERGENCY LIGHT BETWEEN ROWS 18 & 20 DID NOT ILLUMINATE DURING TEST. MX R & R EMERGENCY LIGHT SECTION AND OPS CHECKED GOOD. ACFT WAS APPROVED
- [SDR ASOA201404140350](https://openairdocs.org/sdr/ASOA201404140350), Apr 14, 2014: COFFEEMAKER. FAILED. CREW REPORTED COFFEE POTS WERE NOT WARMING AND A BURNING ODOR. ODOR DISSIPATED WHEN THEY WERE TURNED OFF. MAINTENANCE INSPECTED AND REPLACED THE COFFEE BREWER L
- [SDR ASOA20140413081](https://openairdocs.org/sdr/ASOA20140413081), Apr 12, 2014: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AT FRAME 24, STRINGERS 16 AND 17R. R & R SHEAR TIE.
- [SDR ASOA20140413080](https://openairdocs.org/sdr/ASOA20140413080), Apr 12, 2014: FLOOR SUPPORT. CORRODED. CORROSION BEYOND LIMITS AROUND FASTENERS IN RT OTBD FLOOR SUPPORT AT FRAME 20. R & R FLOOR SUPPORT.
- [SDR ASOA20140411079](https://openairdocs.org/sdr/ASOA20140411079), Apr 10, 2014: PROFILE. CORRODED. CORROSION AROUND NUTPLATES ON BOTTOM OF PAX DOOR IS OUT OF LIMITS. R & R PROFILE.
- [SDR ASOA20140411078](https://openairdocs.org/sdr/ASOA20140411078), Apr 10, 2014: FLOOR SUPPORT. CRACKED. CRACK IN INBD SPLICE ANGLE UNDER FLOOR SUPPORT AT LT OMEGA BEAM BETWEEN FRAMES 16-17. R & R CRACKED SPLICE ANGLE.
- [SDR ASOA20140411076](https://openairdocs.org/sdr/ASOA20140411076), Apr 10, 2014: SEAT TRACK. CORRODED. CORROSION IN MULTIPLE AREAS ALONG LT SIDEWALL SEAT TRACK SUPPORT. CORROSION OUT OF LIMITS AFTER BLEND-OUT. R & R SUPPORT.
- [SDR ASOA20140410075](https://openairdocs.org/sdr/ASOA20140410075), Apr 9, 2014: FLOOR SUPPORT. CRACKED. CRACK IN OTBD SPLICE ANGLE UNDER FLOOR SUPPORT AT LT OMEGA BEAM BETWEEN FRAMES 16-17. R & R CRACKED SPLICE ANGLE.
- [SDR ASOA20140410074](https://openairdocs.org/sdr/ASOA20140410074), Apr 9, 2014: FLOOR SUPPORT. CORRODED. CORROSION BEYOND LIMITS ON RAMP ANGLE UNDER LATERAL FLOOR SUPPORT. R & R RAMP ANGLE.
- [SDR ASOA20140410073](https://openairdocs.org/sdr/ASOA20140410073), Apr 9, 2014: FLOOR SUPPORT. CORRODED. CORROSION BEYOND LIMITS ALONG LT OTBD FLOOR SUPPORT BETWEEN FRAMES 19-23. R & R FLOOR SUPPORT.
- [SDR ASOA20140410072T](https://openairdocs.org/sdr/ASOA20140410072T), Apr 9, 2014: STRAP. CORRODED. CORROSION AROUND NUTPLATE IN GUSSET AT RT OMEGA BEAM, CORRODED BEYOND LIMITS. R & R GUSSET.
- [SDR ASOA20140312037](https://openairdocs.org/sdr/ASOA20140312037), Mar 12, 2014: CHARGER. INOPERATIVE. DURING MAINTENANCE INSPECTION THE FWD OVERWING EMERGENCY LIGHTS WERE DISCOVERED INOPERATIVE. MAINTENANCE R & R THE NR 1 EMERGENCY LIGHT BATTERY CHARGER ASSY WIT
- [SDR ASOA20140202012](https://openairdocs.org/sdr/ASOA20140202012), Feb 2, 2014: POWER SUPPLY. INOPERATIVE. DURING ROUTINE MAINTENANCE, THE ENTRY OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. OPS CHECKED GOOD.
- [SDR ASOA20140128009](https://openairdocs.org/sdr/ASOA20140128009), Jan 28, 2014: POWER SUPPLY. INOPERATIVE. DURING ROUTINE MAINTENANCE, FORWARD CABIN CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT POWER SUPPLY. OPS CHECKED GOOD.
- [SDR ASOA20130923112](https://openairdocs.org/sdr/ASOA20130923112), Sep 23, 2013: BALLAST. OVERHEATED. CREW REPORTED A BURNING ELECTRICAL ODOR LIKE A SOLDERING IRON OR HAIR CURLER, ABOVE SEAT 1A. DETERMINED THE ODOR TO BE COMING FROM THE SEAT 1A BALLAST. R & R CE
- [SDR ASOA20130805344](https://openairdocs.org/sdr/ASOA20130805344), Aug 5, 2013: LAMP. INOPERATIVE. RT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LIGHT BULB. OPS CK GOOD.
- [SDR ASOA20130426032](https://openairdocs.org/sdr/ASOA20130426032), Apr 26, 2013: FLAPPER VALVE. LEAKING. THE CREW REPORTED A FUEL LEAK FROM RT WING AFTER TAKEOFF. FUEL QTY DROPPED 300LBS AND THEN FUEL LEAK STOPPED. MX INSPECTED AN REPLACED THE RT WING FLAP VALVE. O
- [SDR ASOA20120728056R](https://openairdocs.org/sdr/ASOA20120728056R), Jul 28, 2012: CHARGER. INOPERATIVE. DURING MX INSPECTION, THE LT AFT EXTERIOR, ROW 12, AND 2 AFT CEILING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MX R & R BATTERY CHARGER AND BATTERY PACK. O
- [SDR ASOA20120612045](https://openairdocs.org/sdr/ASOA20120612045), Jun 12, 2012: SUPPORT. CORRODED. DURING C-CHECK, EXTERNAL WASTE VALVE SUPPORT CORRODED AROUND WASTE VALVE. MX R & R WASTE DRAIN VALVE DUMP ASSY IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETUR
- [SDR ASOA20120612044](https://openairdocs.org/sdr/ASOA20120612044), Jun 12, 2012: SILL. CORRODED. DURING C-CHECK, CARGO DOOR CUTOUT CENTER SILL CORRODED. MX R & R CARGO DOOR CUTOUT CENTER SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120608042](https://openairdocs.org/sdr/ASOA20120608042), Jun 8, 2012: MOUNT. CRACKED. DURING C-CHECK, NR 1 ENGINE FWD LOWER MOUNT FITTING CRACKED. R & R FITTING IAW EC5450-01028. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20111231002](https://openairdocs.org/sdr/ASOA20111231002), Dec 31, 2011: FLAPPER VALVE. LEAKING. RT WING LEAKING FUEL DURING CLIMB. CREW DECLARED AN EMERGENCY, RETUNED AND LANDED WITHOUT INCIDENT. MX INSPECTED AND CLEANED THE FLAPPER VALVE ON THE RT WING. O
- [SDR ASOA20111218016](https://openairdocs.org/sdr/ASOA20111218016), Dec 18, 2011: VALVE. LEAKING. DURING FLIGHT IT WAS NOTED THAT FUEL WAS VENTING FROM THE RT WING. THE CREW ELECTED TO DIVERT, WHERE THE ACFT LANDED WITHOUT INCIDENT. MX REPLACED THE RT WING T
- [SDR ASOA20111218011](https://openairdocs.org/sdr/ASOA20111218011), Dec 18, 2011: VALVE. LEAKING. FUEL LEAK NR 2 TANK. R & R RT WING VENT VALVE IAW AMM 28-23-04. OPS AND LEAK CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA11CL238](https://openairdocs.org/sdr/C2XA11CL238), Oct 27, 2011: SWITCH. FAULTY. ORD FLT 6092 THE CREW REPORTED A BLEED 1 VALVE CLOSED MESSAGE AFTER TAKEOFF. MESSAGE DID NOT CLEAR. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MA
- [SDR C2XA11RI122](https://openairdocs.org/sdr/C2XA11RI122), Jul 5, 2011: BATTERY. OVERTEMP. FLIGHT 6124 - IAD - FLIGHT CREW REPORTED NR 1 MAIN BATTERY OVERTEMP DURING LANDING. IAD MX REMOVED AND REPLACED NR 1 AND PERFORMED OPERATIONAL CHECK SUCCESSFULL
- [SDR C2XA11RI031](https://openairdocs.org/sdr/C2XA11RI031), Feb 24, 2011: CONTROLLER. INOPERATIVE. FLIGHT 2865 - EWR - FLIGHT CREW REPORTED THAT ON DESCENT PRESSURIZATION CABIN ALT STOPPED AT 5800FT AT 16000FT, FOLLOWING QRH IN MANUAL MODE THE CABIN CLIMBED T
- [SDR C2XA11RI030](https://openairdocs.org/sdr/C2XA11RI030), Feb 24, 2011: MODULE. INOPERATIVE. FLIGHT 2865 - EWR - FLIGHT CREW REPORTED THAT ON DESCENT PRESSURIZATION CABIN ALT STOPPED AT 5800FT AT 16000FT, FOLLOWING QRH IN MANUAL MODE THE CABIN CLIMBED T
- [SDR C2XA11CL046](https://openairdocs.org/sdr/C2XA11CL046), Feb 11, 2011: CONTROLLER. FAULTY. THE CREW REPORTED THE CABIN PRESSURIZATION DID NOT DESCEND ON SCHEDULE AFTER ENCOUNTERING ICING CONDITIONS IN AUTO MODE. MAINTENANCE INSPECTED AND REPLACED THE 
- [SDR C2XA11CL042](https://openairdocs.org/sdr/C2XA11CL042), Feb 10, 2011: PRESSURE SWITCH. FAULTY. THE CREW REPORTED THE CABIN PRESSURIZATION DID NOT DESCEND ON SCHEDULE. MAINTENANCE INSPECTED AND REPLACED THE HIGH STAGE VALVE PRESSURE SWITCH AND CONNECTOR P1
- [SDR C2XA10IA188](https://openairdocs.org/sdr/C2XA10IA188), Jul 1, 2010: LIGHT. MALFUNCTIONED. TAM - DURING TAXI THE CREW REPORTED THAT THE EMERGENCY LIGHTS REMAINED ON CONTINUOUSLY. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE RESET THE ELECTRICAL
- [SDR C2XA10SH193](https://openairdocs.org/sdr/C2XA10SH193), Jun 6, 2010: BEAM. CORRODED. SHV - DURING C CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE
- [SDR C2XA10SH192](https://openairdocs.org/sdr/C2XA10SH192), Jun 6, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24-25. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE A
- [SDR C2XA10SH191](https://openairdocs.org/sdr/C2XA10SH191), Jun 6, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 37. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB145 SRM 53-00-10. THE AIRCRAFT WAS AP
- [SDR C2XA10SH190](https://openairdocs.org/sdr/C2XA10SH190), Jun 6, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24-25. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCR
- [SDR C2XA10SH187](https://openairdocs.org/sdr/C2XA10SH187), Jun 2, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C CHECK THE LT OMEGA BEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53
- [SDR C2XA10IA106](https://openairdocs.org/sdr/C2XA10IA106), Mar 25, 2010: FLAPPER VALVE. LEAKING. SDF - FLIGHT 2815, DURING CLIMBOUT OF SDF, THE CREW REPORTED FUEL LEAKING FROM THE LEFT WING. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAI
- [SDR C2XA09CL040](https://openairdocs.org/sdr/C2XA09CL040), Apr 10, 2009: PUMP. LEAKING. CLE - FLIGHT 2690 THE CREW REPORTED, LOST ALL NR 2 HYDRAULIC SYSTEM FLUID IN FLIGHT. THE AIRCRAFT LANDED IN CLE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED 
- [SDR C2XA09CL011](https://openairdocs.org/sdr/C2XA09CL011), Jan 22, 2009: LIGHT. INOPERATIVE. CREW REPORTED AISLE PATH EMERGENCY LIGHTS INOPERATIVE AT ROWS 9 AND 15. MX INSP AND REPLACED THE AISLE PATH LIGHT STRIPS. OPS CHECKS WERE GOOD.
- [SDR C2XA08CL127](https://openairdocs.org/sdr/C2XA08CL127), Dec 4, 2008: RELAY. FAULTY. CLE - FLIGHT 2006 - THE CREW REPORTED A WING ANTI-ICE AND A PACK 1 VALVE FAIL MESSAGE ON THE EICAS DURING CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITH
- [SDR C2XA08SH066](https://openairdocs.org/sdr/C2XA08SH066), Apr 13, 2008: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM CORRODED UNDER LOWER LT RAMP ANGLE FR 20. MX REPAIRED LT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPRO
- [SDR C2XA08SH065](https://openairdocs.org/sdr/C2XA08SH065), Apr 13, 2008: DOOR FRAME. CRACKED. SHV - DURING C-CHECK MINOR CRACK AT FWD LOWER CORNER OF CARGO DOOR. MX REMOVED AND REPLACED FWD FRAME ON CARGO DOOR IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS A
- [SDR C2XA08SH064](https://openairdocs.org/sdr/C2XA08SH064), Apr 13, 2008: FRAME. DAMAGED. SHV - DURING C-CHECK FR 15 DAMAGE AT STR 2R FROM COCKPIT DOOR HINGE PIN. MX REPAIRED FR 15 AT STR 2R IAW EMB 145 SRM 53-00-04 FIG 206. THE AIRCRAFT WAS APPROVED

All 73: https://openairdocs.org/aircraft/N12552/reports.md

## STCs that may be installed (OpenAirDocs) (75, 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-145LR)

- [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 ST02216AT-D](https://openairdocs.org/stc/ST02216AT-D): Installation of Teledyne Mini Flight Data Acquisition Unit in a Provisioned EMB-135/145. 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 ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [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 ST04527CH](https://openairdocs.org/stc/ST04527CH): Installation of a 16 passenger configuration. C&L STC Holdings 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 ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [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 ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST01039DE](https://openairdocs.org/stc/ST01039DE): Passenger seating arrangement for 30 or less passengers. Deluxe Public Charter LLC
- [STC ST04537NY](https://openairdocs.org/stc/ST04537NY): Installation of Air Filtration. Kilroy Aviation LLC
- [STC ST09858SC](https://openairdocs.org/stc/ST09858SC): Installation of cabin automatic coffee brewing system. Safran Cabin Germany Gmbh
- [STC ST04255CH](https://openairdocs.org/stc/ST04255CH): Installation of an Automatic Dependent Surveillance-Broadcast (ADS-B Out) System. ENVOY AIR
- [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 ST04423NY](https://openairdocs.org/stc/ST04423NY): Installation of ADS-B Out. FTI Engineering Nework GmbH
- [STC ST00015IB](https://openairdocs.org/stc/ST00015IB): Installation of a Honeywell HF Communication System, model KHF 1050, with provisions for a dual installation. Embraer Engineering & Technology Center - USA Inc
- [STC ST00014IB](https://openairdocs.org/stc/ST00014IB): Installation of a second Honeywell HF Communication System, model KHF 1050. Embraer Engineering & Technology Center - USA Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST04333NY](https://openairdocs.org/stc/ST04333NY): Installation of sat: Tglo® Photolumincsccnt Aisle Path Marking System. STG Aerospace Ltd
- [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 ST000081B](https://openairdocs.org/stc/ST000081B): Installation of a second SELCAL channel. EMBRAER - Empresa Brasileira de Aeronautica
- [STC ST00008IB](https://openairdocs.org/stc/ST00008IB): Installation of a second SELCAL channel. EMBRAER - Empresa Brasileira de Aeronautica
- [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

All 75: https://openairdocs.org/aircraft/N12552/stcs.md

## Earlier aircraft with N12552

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N12552 before.

- [Cancelled 1991-03-27](https://openairdocs.org/deregistered/N12552-1991-03-27): Cessna 172M, S/N 17262066. Triennial form not returned. Owner: [Tradewinds Aviation Inc](https://openairdocs.org/faa-owner/TRADEWINDS%20AVIATION%20INC), [Lantana, FL](https://openairdocs.org/faa-place/FL/Lantana)

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/aircraft.md
- The Rolls-Royce AE-3007A1P engine: https://openairdocs.org/engine/rolls-royce-ae-3007a1p.md

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