# N664MS: 2004 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 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: 145779
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 24, 2004
- Certificate issued: October 18, 2011
- Expires: October 31, 2027
- Mode S code: A8C439
- Registered owner: [American Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRLINES%20INC)
- Location: [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth)
- Owner type: Corporation
- Owner's area on the map: 32.8240° N, 97.0491° W: Placed by OpenAirDocs at the center of ZIP code 76155, 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=664MS
- Page: https://openairdocs.org/aircraft/N664MS

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): 110 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 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 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 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 126: https://openairdocs.org/aircraft/N664MS/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 N664MS.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20070216004959I](https://openairdocs.org/incident/20070216004959I), Feb 16, 2007: Emb EMB145LR (N664MS), Middletown, PA. (-23) After takeoff, when landing gear lever was selected to the up position, the landing gear remained in the down and locked position. Aircraft returned to…

## Service difficulty reports (242, 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 HNAA2026092200883](https://openairdocs.org/sdr/HNAA2026092200883), Aug 10, 2026: SKIN. CORRODED. RT INLET HAS PITTING ON LIP SKIN. R/H INLET REMOVED AND REPLACED ON WO# H10452 S/N 00912 QUANTUM# 4600.
- [SDR HNAA2026090100852](https://openairdocs.org/sdr/HNAA2026090100852), Aug 10, 2026: SUPPORT. CORRODED. FOUND CORROSION UNDER LT OTBD SUPPORT AT FR 61-62. REMOVED AND REPLACED WITH A NEW LT OTBD PARTITION DOUBLER AT FR 61 IAW SRM 51-40-02PR, STEP 2E.
- [SDR HNAA2026092200887](https://openairdocs.org/sdr/HNAA2026092200887), Aug 7, 2026: FLOOR SUPPORT. CRACKED. FOUND RH OMEGA BEAM TO HAVE A CRACK BETWEEN FR 60 AND FR 61. PERFORMED CUTOUT WITH FILLER AND DOUBLER REPAIR ON RH OMEGA BEAM BETWEEN FR 60 AND FR 61 IAW ETD202
- [SDR HNAA2026092200886](https://openairdocs.org/sdr/HNAA2026092200886), Aug 7, 2026: FLOOR SUPPORT. CRACKED. FOUND RH OMEGA BEAM TO HAVE A CRACK AT FR 59. PERFORMED CUTOUT WITH A FILLER AND DOUBLER REPAIR ON THE RT OMEGA BEAM AT FR 59 IAW ETD2026-145-013745 AND MAJOR E
- [SDR HNAA2026090100817](https://openairdocs.org/sdr/HNAA2026090100817), Aug 7, 2026: FLOOR SUPPORT. CRACKED. UPON REMOVAL OF ONE RT OMEGA BEAM GUSSET AT FR 61, FOUND RT OMEGA BEAM TO BE CRACKED BTWN FR 60 & FR 61. PERFORMED CUTOUT WITH FILLER & DOUBLER REPAIR ON RT OME
- [SDR HNAA2026090100816](https://openairdocs.org/sdr/HNAA2026090100816), Aug 7, 2026: FLOOR SUPPORT. CORRODED. UPON REMOVAL OF ONE RT OMEGA BEAM GUSSET AT FR 61, FOUND RT OMEGA BEAM TO BE CRACKED AT FR 59. PERFORMED CUTOUT WITH A FILLER & DOUBLER REPAIR ON THE RT OMEGA B
- [SDR HNAA2026090100815](https://openairdocs.org/sdr/HNAA2026090100815), Aug 7, 2026: FLOOR SUPPORT. CRACKED. UPON REMOVAL OF ONE LT OMEGA BEAM GUSSET AT FR 61, FOUND LT OMEGA BEAM TO HAVE A CRACK AT FR 59. PERFORMED CUTOUT WITH FILLER AND DOUBLER REPAIR ON LT OMEGA BEA
- [SDR HNAA2026090100851](https://openairdocs.org/sdr/HNAA2026090100851), Aug 6, 2026: SUPPORT. CORRODED. RIGHT INBD FLAP, OTBD FLAP SHROUD SUPPORT, PITTED ON MATING SURFACE. REMOVED THE CORROSION ON RT INBD FLAP, OTBD FLAP SHROUD SUPPORT BY BLENDING. DAMAGE FOUND T
- [SDR HNAA2026092200885](https://openairdocs.org/sdr/HNAA2026092200885), Jul 30, 2026: RIB. CRACKED. RT WING, 1EA RIB 21 HAS A CRACK ON UPPER MID FLANGE. REPAIRED CRACK ON RIB 21 OF THE RT WING UPPER MID FLANGE WITH A CUTOUT FILLER AND DOUBLER IAW SRM 57-20-07-
- [SDR HNAA202609220085](https://openairdocs.org/sdr/HNAA202609220085), Jul 30, 2026: RIB. CRACKED. RT WING, 1EA RIB 21 HAS A CRACK ON UPPER MID FLANGE. REPAIRED CRACK ON RIB 21 OF THE R/H WING UPPER MID FLANGE WITH A CUTOUT FILLER AND DOUBLER PER EMB 145 SRM 
- [SDR HNAA2026090100814](https://openairdocs.org/sdr/HNAA2026090100814), Jul 30, 2026: RIB. CRACKED. RIGHT WING, ONE RIB 21 HAD A CRACK ON UPPER MID FLANGE. REPAIRED THE RIB MID FLANGE WITH A CUTOUT FILLER & DOUBLER IAW SRM 57-20-07-RE, & EO-1-57-26-0404.
- [SDR HNAA2026090100850](https://openairdocs.org/sdr/HNAA2026090100850), Jul 28, 2026: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT AT FR 49 WAS CORRODED. REMOVED AND REPLACED THE LT FLOOR SUPPORT AT FR 49 IAW SRM 51-40-02 PR , ALODINE PO 342139 & SRM CPM 51-21-04.
- [SDR HNAA2026090100849](https://openairdocs.org/sdr/HNAA2026090100849), Jul 28, 2026: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT AT FR 49 WAS CORRODED. REMOVED AND REPLACED THE RT FLOOR SUPPORT FROM FR 48 TO FR 52 IAW SRM 51-40-02, STEP 2 AND 4.
- [SDR HNAA2026090100848](https://openairdocs.org/sdr/HNAA2026090100848), Jul 28, 2026: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT FROM FR 41 TO FR 45 HAD CORROSION. REMOVED THE FLOOR SUPPORT AND INSTALLED A NEW LT FLOOR SUPPORT FROM FR 41 TO FR 45 IAW SRM 51-40-02-PR, & 
- [SDR HNAA2026090100847](https://openairdocs.org/sdr/HNAA2026090100847), Jul 28, 2026: GUSSET. CORRODED. LEFT OMEGA BEAM UPPER GUSSET FROM FR 39 TO FR 45 HAD CORROSION. REMOVED AND INSTALLED A NEW LT OMEGA BEAM UPPER GUSSET FROM FR 39 TO FR 45, SEALANT PO 342559 IA
- [SDR HNAA2026090100846](https://openairdocs.org/sdr/HNAA2026090100846), Jul 28, 2026: GUSSET. CORRODED. MID OMEGA BEAM UPPER GUSSET FROM FR 40 TO FR 43 HAD CORROSION. REMOVED AND REPLACED THE MID OMEGA BEAM UPPER GUSSET FROM FR 40 TO FR 46 IAW SRM 51-40-02 PR, STE
- [SDR HNAA2026090100845](https://openairdocs.org/sdr/HNAA2026090100845), Jul 28, 2026: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT, FR 41 TO FR 44 HAS CORROSION. REMOVED THE DAMAGED FLOOR SUPPORT & INSTALLED NEW, FR 41 TO FR 44 IAW SRM 51-40-02-PR, & SRM 51-20-01-PR.
- [SDR HNAA2026090100844](https://openairdocs.org/sdr/HNAA2026090100844), Jul 28, 2026: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT FROM FR 35 TO FR 39 HAD CORROSION. REMOVED AND REPLACED THE LT FLOOR SUPPORT FROM FR 35 TO FR 39 IAW SRM 51-20-03.
- [SDR HNAA2026090100843](https://openairdocs.org/sdr/HNAA2026090100843), Jul 28, 2026: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT FROM FR 35 TO FR 39 HAD CORROSION. REMOVED & REPLACED THE RT FLOOR SUPPORT FROM FR 36 - 42 IAW SRM 51-40-02-PR, STEPS 2 & 4.
- [SDR HNAA2026090100842](https://openairdocs.org/sdr/HNAA2026090100842), Jul 28, 2026: GUSSET. CORRODED. MID OMEGA BEAM UPPER GUSSET FROM FR 35 TO FR 38 HAD CORROSION. REMOVED AND REPLACED THE LT OMEGA BEAM MID UPPER GUSSET AT FR 35 TO 38 IAW SRM 51-40-02-PR, STEP 
- [SDR HNAA2026090100841](https://openairdocs.org/sdr/HNAA2026090100841), Jul 28, 2026: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT FROM FR 29 TO FR 35 WAS CORRODED. REMOVED AND REPLACED THE LT FLOOR SUPPORT FROM FR 29 TO FR 35 IAW SRM 51-40-02-PR, STEP 2.B AND 3.B.
- [SDR HNAA2026090100840](https://openairdocs.org/sdr/HNAA2026090100840), Jul 28, 2026: GUSSET. CORRODED. LEFT OMEGA BEAM UPPER GUSSET FROM FR 29 TO FR 35 HAD CORROSION. REMOVED AND REPLACED THE LT OMEGA BEAM GUSSET FROM FR 29 TO FR 35 IAW SRM 51-40-02-PR.
- [SDR HNAA2026090100839](https://openairdocs.org/sdr/HNAA2026090100839), Jul 28, 2026: GUSSET. CORRODED. MID OMEGA BEAM UPPER GUSSET FROM FR 29 TO FR 35 HAD CORROSION. REMOVED AND REPLACED THE MID OMEGA BEAM GUSSET FROM FR 29 TO FR 35 IAW SRM 51-40-02-PR, & SRM 51-
- [SDR HNAA2026090100838](https://openairdocs.org/sdr/HNAA2026090100838), Jul 28, 2026: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT FROM FR 31 TO FR 35 HAD CORROSION. REMOVED AND REPLACED RT FLOOR SUPPORT FROM FR 29 TO FR 35 IAW SRM 51-40-02PR, STEP 2 B & C.
- [SDR HNAA2026090100833](https://openairdocs.org/sdr/HNAA2026090100833), Jul 27, 2026: FLOORBEAM. CORRODED. MID FLOORBEAM AT FR 25 HAS CORROSION. REMOVED AND REPLACED WITH A NEW MID FLOORBEAM AT FR 25 IAW SRM 51-40-02-PR.
- [SDR HNAA202609010233](https://openairdocs.org/sdr/HNAA202609010233), Jul 27, 2026: FLOORBEAM. CORRODED. MID FLOORBEAM AT FR 25 HAD CORROSION. REMOVED AND REPLACED WITH A NEW FLOORBEAM AT FR 25 IAW SRM 51-40-02-PR.
- [SDR HNAA2026090100837](https://openairdocs.org/sdr/HNAA2026090100837), Jul 27, 2026: GUSSET. CORRODED. MID OMEGA BEAM UPPER GUSSET FROM FR 25 TO FR 29 HAD CORROSION. REMOVED AND REPLACED THE MID OMEGA BEAM UPPER GUSSET FROM FR 25 TO FR 29 IAW SRM 51-40-02-PR, & S
- [SDR HNAA2026090100836](https://openairdocs.org/sdr/HNAA2026090100836), Jul 27, 2026: GUSSET. CORRODED. OMEGA BEAM UPPER GUSSET FROM FR 25 TO FR 28, LT, HAD CORROSION. REMOVED AND REPLACED THE LT OMEGA BEAM GUSSET AT FR23 TO FR29 IAW SRM 51-40-02PR STEP 2C, & SRM 
- [SDR HNAA2026090100835](https://openairdocs.org/sdr/HNAA2026090100835), Jul 27, 2026: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT FROM FR 23 TO FR 29, LT, HAD CORROSION. REMOVED AND REPLACED THE LT FLOOR SUPPORT FROM FR 23 TO FR 29 IAW SRM 51-40-02-PR.
- [SDR HNAA2026090100834](https://openairdocs.org/sdr/HNAA2026090100834), Jul 27, 2026: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AT FR 23, LT, HAD CORROSION. REMOVED AND REPLACED WITH A NEW LT FLOOR SUPPORT AT FR 23 IAW SRM 51-40-02-PR.
- [SDR HNAA2026090100234](https://openairdocs.org/sdr/HNAA2026090100234), Jul 27, 2026: FLOORBEAM. CORRODED. MID FLOORBEAM AT FR 25 HAD CORROSION. REMOVED AND REPLACED WITH A NEW MID FLOORBEAM AT FR 25 IAW SRM 51-40-02-PR.
- [SDR HNAA2026090100832](https://openairdocs.org/sdr/HNAA2026090100832), Jul 27, 2026: SUPPORT. CORRODED. PAX DOOR CUTOUT LOWER AFT SCUFF PLATE SUPPORT AT FR 17 HAD CORROSION. REMOVED AND REPLACED THE PAX DOOR CUTOUT LOWER AFT SCUFF PLATE SUPPORT AT FR 17 IAW SRM 51
- [SDR HNAA2026090100831](https://openairdocs.org/sdr/HNAA2026090100831), Jul 27, 2026: SUPPORT. CORRODED. PAX DOOR CUTOUT LOWER FWD SCUFF PLATE SUPPORT AT FR 16 HAD CORROSION. REMOVED AND REPLACED WITH NEW PAX DOOR CUTOUT LOWER FWD SCUFF PLATE SUPPORT AT FR 16 IAW S
- [SDR HNAA2026090100830](https://openairdocs.org/sdr/HNAA2026090100830), Jul 27, 2026: GUSSET. CORRODED. LEFT OMEGA BEAM GUSSET AT FR 17 HAD CORROSION. REMOVED AND REPLACED LT OMEGA BEAM GUSSET IAW SRM 51-40-02-PR.
- [SDR HNAA2026090100829](https://openairdocs.org/sdr/HNAA2026090100829), Jul 27, 2026: FLOORBEAM. CORRODED. LEFT FLOORBEAM AT FR 18 HAD CORROSION. REMOVED AND REPLACED WITH A NEW LT FLOORBEAM AT FR 18 IAW SRM 51-40-02-PR.
- [SDR HNAA2026090100828](https://openairdocs.org/sdr/HNAA2026090100828), Jul 27, 2026: FLOORBEAM. CORRODED. LEFT FLOORBEAM AT FR 20 HAD CORROSION. REMOVED AND INSTALLED A NEW LT FLOORBEAM AT FR 20 IAW SRM 51-40-02-PR, & SRM 51-20-01-PR.
- [SDR HNAA2026090100827](https://openairdocs.org/sdr/HNAA2026090100827), Jul 27, 2026: FLOOR SUPPORT. CORRODED. RIGHT OMEGA BEAM AT FR 23 HAD CORROSION. COMPLIED WITH CNTR FUSELAGE I - FLOOR STRUCTURE - RT OMEGA BEAM AT FRAME 23 - PERMANENT REPAIR IAW ETD2026-145-013232, 
- [SDR HNAA2026090100826](https://openairdocs.org/sdr/HNAA2026090100826), Jul 27, 2026: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AT FR 22, RT, HAD CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT AT FR 22 AND COMPLIED WITH CNTR FUSELAGE I FLOOR STRUCTURE PROFILE T PERMANENT
- [SDR HNAA2026090100825](https://openairdocs.org/sdr/HNAA2026090100825), Jul 27, 2026: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AT FR 18, RT, HAD CORROSION. PERFORMED REPAIR OF THE RT FLOOR SUPPORT AT FR 18 IAW SRM 53-21-10-RE, STEP 4, & ETD2026-145-014004. SEE EO EO1-05-25
- [SDR HNAA2026090100824](https://openairdocs.org/sdr/HNAA2026090100824), Jul 25, 2026: GUSSET. CORRODED. LEFT OMEGA BEAM UPPER GUSSET AT FR 53 HAD CORROSION. REMOVED AND REPLACED THE LT OMEGA BEAM UPPER GUSSET AT FR 53 - 59 IAW SRM 51-40-02-PR, STEP 2.B AND 3.B.
- [SDR HNAA2026090100823](https://openairdocs.org/sdr/HNAA2026090100823), Jul 25, 2026: GUSSET. CORRODED. MID OMEGA BEAM UPPER GUSSET FROM FR 54 TO FR 56 HAS CORROSION. REMOVED AND REPLACED MID OMEGA BEAM UPPER GUSSET FROM FR 54 TO FR 56 PER SRM 51-40-02-PR, STEP 2.
- [SDR HNAA2026090100822](https://openairdocs.org/sdr/HNAA2026090100822), Jul 25, 2026: FLOOR SUPPORT. CORRODED. RIGHT OTBD FLOOR SUPPROT FROM FR 56 TO FR 59 HAD CORROSION. REMOVE THE FLOOR SUPPORT & INSTALLED A NEW RT OTBD FLOOR SUPPORT FR 53-FR 59 IAW SRM 51-40-02.
- [SDR HNAA2026090100821](https://openairdocs.org/sdr/HNAA2026090100821), Jul 25, 2026: FLOOR SUPPORT. CORRODED. LEFT OTBD FLOOR SUPPORT AT FR 61 HAD CORROSION. REMOVED & REPLACED WITH A NEW LT OTBD FLOOR SUPPORT AT FR 61 IAW SRM 51-40-02-PR.
- [SDR HNAA2026090100820](https://openairdocs.org/sdr/HNAA2026090100820), Jul 25, 2026: GUSSET. CORRODED. LEFT OMEGA BEAM GUSSET AT FR 61 HAD CORROSION. REMOVED AND REPLACED WITH A NEW LT OMEGA BEAM GUSSET AT FR 61 IAW SRM 51-40-02PR, STEP 2C.
- [SDR HNAA2026090100819](https://openairdocs.org/sdr/HNAA2026090100819), Jul 25, 2026: GUSSET. CRACKED. ONE RT OMEGA BEAM GUSSET AT FR 59 HAD CORROSION. REMOVED AND REPLACED WITH A NEW RT OMEGA BEAM GUSSET AT FR 59 IAW SRM 51-40-02PR.
- [SDR HNAA2026092200884](https://openairdocs.org/sdr/HNAA2026092200884), Jul 23, 2026: SKIN. CORRODED. FUSELAGE EXTERNAL SKIN AT , LT, AT FR 61, STR 19L HAS CORROSION. REMOVED CORROSION BY BLENDING ON FUSELAGE EXTERNAL SKIN AT, LT, AT FR 61, STR 19L. FOUND TO BE 
- [SDR HNAA2026090100818](https://openairdocs.org/sdr/HNAA2026090100818), Jul 23, 2026: SUPPORT. CORRODED. TOILET WASTE VALVE SUPPORT EXTERNAL STRUCTURE HAS CORROSION. REMOVED AND REPLACED WITH A NEW TOILET WASTE VALVE SUPPORT EXTERNAL STRUCTURE IAW SRM 51-40-02-PR.
- [SDR HNAA2026090100813](https://openairdocs.org/sdr/HNAA2026090100813), Jul 23, 2026: SKIN. CORRODED. FUSELAGE EXTERNAL SKIN AT FR 61, STRINGER 19L HAD CORROSION. REMOVED CORROSION BY BLENDING ON SKIN AT FR 61, STR 19L. FOUND TO BE WITHIN LIMITS. IAW SRM 53-21-0
- [SDR HNAA2025043000293](https://openairdocs.org/sdr/HNAA2025043000293), Apr 29, 2025: VALVE. ABNORMAL. HS VALVE 1 FAIL ON T/O ROLL FACT 29APR25 02:31 PHL R/R H/S VALVE 1 IAW AMM 36-11-02. OPS CHECK GOOD. A/C OKAY FOR SERVICE AT THIS TIME.
- [SDR HNAA2024111101058](https://openairdocs.org/sdr/HNAA2024111101058), Nov 8, 2024: PIVOT ASSY. OUT OF ADJUST. ON TAKEOFF ROLL AROUND 60 KNOTS GOT ENG 2 REV DISAGREE. REJECTED TAKEOFF FACT 10NOV24 04:45 MDT T/S IRT FIM TASK 78-30-00-810-821A. PRFORMED PIVOT DOOR OVERSTOW

All 242: https://openairdocs.org/aircraft/N664MS/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/N664MS/stcs.md

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/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.