# N660CL: 2003 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: 145764
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 10, 2003
- Certificate issued: September 30, 2011
- Expires: September 30, 2027
- Mode S code: A8B476
- 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=660CL
- Page: https://openairdocs.org/aircraft/N660CL

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/N660CL/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 N660CL.

## 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 20160102000209I](https://openairdocs.org/incident/20160102000209I), Jan 2, 2016: Embraer EMB-145LR (N660CL), Chicago, IL, Minor damage. At 07:40 envoy 3137, EMB-145, impacted a city of Chicago vehicle while taxiing to the gate. Impact occurred on taxiway h near A1. Right rear cab of pickup…

## Service difficulty reports (109, 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 HNAA2026072700635](https://openairdocs.org/sdr/HNAA2026072700635), Jul 26, 2026: CHECK VALVE. FAULTED. SMELL OF EXHAUST FUMES IN FLIGHT DECK FACT 26JUL26 07:22 ROA OPERATED PACK 1&2 WITH E2 BLEED AND VERIFIED NO EXHAUST SMELL COMMING FROM PACK SYSTEM. NO DEFECTS 
- [SDR HNAA2026072000597](https://openairdocs.org/sdr/HNAA2026072000597), Jul 19, 2026: CHECK VALVE. ABNORMAL. STRONG EXHAUST SMELL IN FLT DECK WHEN RUNNING APU AT THE GATE WITH PACK 1. FOUND APU BLEED VALVE INNER GASKET TO BE WORN. R&R BLEED VALVE REF TO AMM 36-12-03. N
- [SDR HNAA2026071300590](https://openairdocs.org/sdr/HNAA2026071300590), Jul 9, 2026: ACM. ODOR. BURNING SMELL IN FLIGHT DECK AND FWD GALLEY. R & R LT ACM IAW AMM 21-51-03.
- [SDR HNAA2026070300565](https://openairdocs.org/sdr/HNAA2026070300565), Jul 2, 2026: DUCT. ODOR. STRONG EXHAUST FUMES INSIDE AND OUTSIDE OF AIRCRAFT. FOUND DUCT ON HEAT EXCHANGER LEAKING. R & R HEAT EXCHANER DUCT IAW MM 21-51-00, OPS CHKD GOOD .
- [SDR HNAA2026070200564](https://openairdocs.org/sdr/HNAA2026070200564), Jul 1, 2026: CLAMP. LOOSE. EXHAUST FUMES STRONGLY SMELLED IN COCKPIT DUIRNG APU AND PACKS RUNNING AFTER LANDING. FOUND MUFFLER CLAMPS LOOSE IN APU AREA ON INTAKE AND EXHAUST TUBES, SECURE
- [SDR HNA2026F00001](https://openairdocs.org/sdr/HNA2026F00001), Jun 30, 2026: WARNING MESSAGE. FALSE ACTIVATION. IRREGULARITY REPORTED - ON TAKEOFF ROLL AT APPROX 80 KNOTS CREW REPORT MASTER WARNING FLASHED WITH NO ASSOCIATED EICAS MSGS. CREW ABORTED TAKEOFF. INSTRUCTED CR
- [SDR HNAA2026070100563](https://openairdocs.org/sdr/HNAA2026070100563), Jun 30, 2026: UNKNOWN. UNKNOWN. FLT 5802 REJECTED T/O, CONTACTED MOC, RETURNED TO GATE AND CODED 77M MX DELAY ALL FOR UNKNOWN REASON. NO FURTHER INFORMATION COLLECTED. NO WRITE UP IN LOGBOOK R
- [SDR HNAA2026070100562](https://openairdocs.org/sdr/HNAA2026070100562), Jun 30, 2026: UNKNOWN. ODOR. STRONG FUEL SMELL AT FA SEAT AND FLIGHT DECK. INSPECTED INSIDE PACK 1 AND 2 PANELS NO DEFECTS NOTED INSPECTED SPR CAP FOR LEAKS NONE NOTED PERORMED HIGH POWER R
- [SDR HNAA2026060100443](https://openairdocs.org/sdr/HNAA2026060100443), May 31, 2026: BLEED AIR SYS. ODOR. WITH APU BLEED SELECTED EXHAUST GAS SMELL IN COCKPIT AND CABIN: NOT DETECTED WITH ENGINE BLEED APU BLEED SYSTEM
- [SDR HNAA2026042700360](https://openairdocs.org/sdr/HNAA2026042700360), Apr 25, 2026: SIGNAL COND UNIT. ABNORMAL. LEFT TANK SHOWING DASHES FACT 25APR26 19:18 CLT R+R'D FUEL SIGNAL CONDITION UNIT IRT AMM 28-41-01. OPS CHECK GOOD IAW AMM 28-41-00. A/C OKAY FOR SERVICE
- [SDR HNAA2026042300354](https://openairdocs.org/sdr/HNAA2026042300354), Apr 23, 2026: APU. ODOR. STRONG CHEMICAL SMELL ENTERED COCKPIT AND CABIN WHILE APU RUNNING. R & R APU IAW WC 49-80-05, OPS CK GOOD NO ABNORMAL SMELLS NOTED. CLEAR MEL.
- [SDR HNAA2026040300254](https://openairdocs.org/sdr/HNAA2026040300254), Apr 3, 2026: GROUND WIRE. BURNED. BURNING SMELL COMING FROM FLIGHT DECK ON GROUND. MEL`D THE AIR CONDITIONING PACKS. DISCOVERED GRD WIRE W325-0005 IB FUEL PUMP LT WING TANK BURNT AT TERMINAL END
- [SDR HNAA2026031800223](https://openairdocs.org/sdr/HNAA2026031800223), Mar 17, 2026: UNKNOWN. ODOR. EXHAUST ODOR NOTICED AFTER E2 HUNG START. HAD 3 SUCCESSFUL STARTS ON E2-A WITH BOTH PACKS ON AND NO SMELL. COULD NOT DUPLICATE. NO FURTHER DEFECTS NOTED.
- [SDR HNAA2026031100210](https://openairdocs.org/sdr/HNAA2026031100210), Mar 11, 2026: NONE. NONE. HEAVY FUEL ODOR IN AIRCRAFT WITH APU RUNNING. INSPECTED FOR DEFECTS, NONE NOTED. SUSPECT FUEL ODOR WAS CAUSED DURING REFUELING OPERATIONS. FUEL ODOR SUBSEQUENTL
- [SDR HNAA2025061700455](https://openairdocs.org/sdr/HNAA2025061700455), Jun 16, 2025: WIRE HARNESS. DAMAGED. DURING TAKE OFF CLIMB ENG 2 OIL TEMP TEMP REACHED 133 DEG C. FOLLOWED QRH AND ENG WAS SHUT DOWN. FACT 18JUN25 16:21 CLT R+R'D #2 ENG INDICATING HARNESS IAW RRMM
- [SDR HNAA2025042800224](https://openairdocs.org/sdr/HNAA2025042800224), Apr 26, 2025: RECEPTACLE. BURNED. AT APPROX 10,000 FT, FA NOTICED STRONG BURNING SMELL FROM FRONT OF CABIN FOLLOWED BY FLT DECK CREW NOTICING ON FLT DECK. REMOVED #100 LIQUID WARMER. RECEPTICAL 
- [SDR HNAA2025051200324](https://openairdocs.org/sdr/HNAA2025051200324), Mar 25, 2025: FLOORBEAM. CORRODED. F036819 LH FLOOR BEAM WEB AND LOWER FLANGE CORRODED AT FR38. ACCOMPLISHED REPAIR ON L/H FLOOR BEAM AT FR38 IAW EMB 145 SRM 53-00-10RE, FIGIRE 202, SHEET 2 AND E
- [SDR HNAA2025020600076](https://openairdocs.org/sdr/HNAA2025020600076), Feb 5, 2025: VALVE. FAULTED. HS VLV 2 FAIL MSG ON EICAS FACT 05FEB25 15:22 CLT R&R'D #2 HSV PER AMM 36-11-02-400-801A PERFORMED OPS CHECKS PER AMM 36-00-00-700-803A ALL CHECKS GOOD. OK FOR 
- [SDR HNAA2024112601133](https://openairdocs.org/sdr/HNAA2024112601133), Nov 25, 2024: EICAS. FALSE INDICATION. LOST EICAS DISPLAY DURING EVALUATION FLIGHT. EMERGENCY DECLARED. FACT 26NOV24 05:11 CLT DURING GROUND RUN EICAS REMAINED NORMAL ACFT OK FOR SERVICE
- [SDR HNAA2024110401054](https://openairdocs.org/sdr/HNAA2024110401054), Nov 1, 2024: UNKNOWN. ODOR. AIRCRAFT HAS A STRONG ODOR THROUGHOUT POSSIBLE BLEEDS. FACT 01NOV24 12:31 PHL DUMPED AND SERVICED LAV SEVERAL TIMES. RAN BOTH PACKS WITH APU. NO SMELL NOTED. RA
- [SDR HNAA2024103001038](https://openairdocs.org/sdr/HNAA2024103001038), Oct 29, 2024: O-RING. FAILED. ON TAKEOFF ROLL BLD 2 LEAK MSG DISPLAYED ON EICAS. MEL 30OCT24 13:17 AVL C30409 36-1-4 BOTH ENG BLEEDS FACT 31OCT24 01:50 AVL R+R'S BLEED 2 COUPLING O-RINGS UND
- [SDR HNAA2024091600819](https://openairdocs.org/sdr/HNAA2024091600819), Sep 15, 2024: THRUST REVERSER. WARNING MESSAGE. 784 - TEMP REPAIR IAW EO1-53-21-0254 & ETD2021-145-030320 PERFORMED AT TAT:47747 AND TAC 44977 REQUIRES REPLACE OF PART 145-21873-007 AT FRAME 73 SUPPORT BRACKE
- [SDR HNAA2024090900737](https://openairdocs.org/sdr/HNAA2024090900737), Sep 7, 2024: THRUST REVERSER. WARNING MESSAGE. APPROXIMATELY 60 KNOTS ON TAKE OFF ROLL. E1 REVERSE DISAGREE DISPLAYED ON EICAS, AND NO TAKE OFF CONFIG. C/W MEL PROCEDURE DEACT AND STOW E1 T/R IAW AMM TASK 78
- [SDR HNAA2024091700827](https://openairdocs.org/sdr/HNAA2024091700827), Aug 8, 2024: YOKE. DAMAGED. RH PYLON YOKE FWD AND AFT FASTENER HOLES REQUIRE REAMING. REPAIRED IAW EO1-54-24-0497
- [SDR HNAA2024091700828](https://openairdocs.org/sdr/HNAA2024091700828), Jul 24, 2024: SKIN. GOUGED. 00104 FUSE SKIN IS GOUGED AT FR73 STR20L. REPAIRED IAW EO1-53-24-0478
- [SDR HNAA2024042900327](https://openairdocs.org/sdr/HNAA2024042900327), Apr 17, 2024: SLEEVE. LEAKING. THE WING ANTI ICE FAILED IN ICING CONDITIONS. FACT 17APR24 00:09 CLT UPON INSPECTION FOUND SLEEVES LEAKING BLEED AIR ON Y-PIPE @DTCV REMOVED AND REPLACED SLEEVE
- [SDR HNAA2024040400282](https://openairdocs.org/sdr/HNAA2024040400282), Apr 2, 2024: RELAY. FAULTED. TAT 1 INOP. CLEARED ON ITS OWN. FOUND TAT 1 C/B POPPED OUT. PUSHED IT BACK IN. A/C OK FOR SERVICE AT THIS TIME. R/R RELAY K0064 IAW AMM 20-13-02. TAT SENSORS OP
- [SDR HNAA2023122600493](https://openairdocs.org/sdr/HNAA2023122600493), Dec 23, 2023: UNKNOWN. UNKNOWN. NEW CREW FOR A/C NOTICED STRONG FUEL SMELL IN THE GALLEY AREA, FLIGHT DECK, AND THROUGHOUT THE CABIN. SMELL WAS NOTICED WITH APU RUNNING WITH PACK 2 ON. TURNED 
- [SDR HNAA2023071900251](https://openairdocs.org/sdr/HNAA2023071900251), Jul 19, 2023: UNKNOWN. UNKNOWN. ON CLIMBOUT #2 ENGINE OIL TEMP REACHED 140C. R&R ENGINE #2 OIL TEMP/PRESSURE SENSOR IAW ROLLS-ROYCE MM 79-31-10. OPS CHECK GOOD. OK FOR SERVICE. DOWNLOADED CMC 
- [SDR HNAA2022111400305](https://openairdocs.org/sdr/HNAA2022111400305), Nov 13, 2022: RELAY. FAILED. YOKE UNLOCK WITH GUST LOCK ENGAUGED INTERMITENLY. FOUND AIR/GRND POSN RELAY K0831 FAILING INTERMITTANTLY CAUSING GUST LOCK INTERLOCK RELAY TO CYCLE. R/R'D RELAY
- [SDR HNAA2022072700244](https://openairdocs.org/sdr/HNAA2022072700244), Jul 26, 2022: UPLOCK. FAULTED. LANDING GEAR LEVER DISAGREE MSG FOR RIGHT MAIN. FOLLOWED QRH, ISSUE REMAINED. R/R RT MAIN UPLOCK BOX REF 32-33-10 AND R/R UPLOCK POSITION SWITCHES REF 32-61-01.
- [SDR HNAA2022041300163](https://openairdocs.org/sdr/HNAA2022041300163), Apr 7, 2022: NONE. NONE. E911537 - LH ELEVATOR LWR INBD SKIN HAS AN OIL CANNED DENT BTW RIB 73.0% AND TRAILING EDGE, BTW RIB YH=-1595.0 AND RIB YH=-1880.0 .... REPAIRED LH ELEVATOR LWR 
- [SDR HNAA2022041300162](https://openairdocs.org/sdr/HNAA2022041300162), Apr 7, 2022: NONE. NONE. E909508 - LH ELEVATOR LOWER INBD AFT SKIN IS CRACKED .... REMOVED AND REPLACED LH ELEVATOR LOWER INBOARD AFT SKIN IAW PIEDMONT EO1-55-22-0067.
- [SDR HNAA2022041300161](https://openairdocs.org/sdr/HNAA2022041300161), Mar 31, 2022: NONE. NONE. E908787 - LH FWD ENGINE PYLON SPAR II YOKE UPPER AFT JO-BOLT HOLE HAS INTERNAL DAMAGE .... REAMED LH FWD ENGINE PYLON UPPER AFT JO-BOLT HOLE TO 1ST OVERSIZE TO 
- [SDR HNAA2022041300155](https://openairdocs.org/sdr/HNAA2022041300155), Mar 31, 2022: NONE. NONE. E907210 - EVIDENCE OF CRACK AT TWO FASTENERS ON THE LH SIDE AT FRAME 78 .... INSTALLED SKIN BUSHING (1 LOCATION) ON THE LH SKIN AT FRAME 78 AT LOWER FASTENER LO
- [SDR HNAA2022041300154](https://openairdocs.org/sdr/HNAA2022041300154), Mar 31, 2022: NONE. NONE. E907209 - EVIDENCE OF CRACK AT TWO FASTENERS ON THE LH SIDE AT FRAME 77 .... INSTALLED 2 SKIN BUSHINGS ON LH SKIN AT FRAME 77 AT 2 FASTENER HOLE LOCATIONS IAW E
- [SDR HNAA2022041300157](https://openairdocs.org/sdr/HNAA2022041300157), Mar 29, 2022: NONE. NONE. E907791 - SSI 53-20-13 SERVICE DOOR CENTER SILL CORRODED AROUND NUT PLATES HOLES .... RAR SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2022041300156](https://openairdocs.org/sdr/HNAA2022041300156), Mar 23, 2022: NONE. NONE. E907711 - POSSIBLE CRACK ON FRAME 66 AT STRINGER 16R .... REMOVED AND REPLACED FR66 (LOWER FRAME SECTION) IAW EMB145 SRM 51-40-02
- [SDR HNAA2022041300153](https://openairdocs.org/sdr/HNAA2022041300153), Mar 23, 2022: NONE. NONE. E907197 - SSI 53-20-29 EVIDENCE OF CORROSION ON THE LAV BUCKET AT THE WASTE DRAIN HANDLE .... RAR LAV BUCKET STIFFENERS AND LAV BUCKET IAW EMB 145 SRM 51-20-03,
- [SDR HNAA2022041300159](https://openairdocs.org/sdr/HNAA2022041300159), Mar 16, 2022: NONE. NONE. E907833 - LEFT-HAND UPPER SEAT TRACK CORRODED BETWEEN FRAME 20 AND 21 .... REMOVED AND REPLACED LEFT-HAND #1 UPPER SEAT TRACK IAW EMB 145 AMM 53-01-06
- [SDR HNAA2022041300158](https://openairdocs.org/sdr/HNAA2022041300158), Mar 16, 2022: NONE. NONE. E907832 - LEFT HAND LOWER SEAT TRACK CORRODED BETWEEN FRAME 18 TO 23 .... REMOVED AND REPLACED LEFT HAND LOWER #1 SEAT TRACK IAW EMB 145 AMM 53-01-06.
- [SDR HNAA2022041300160](https://openairdocs.org/sdr/HNAA2022041300160), Mar 10, 2022: NONE. NONE. E908064 - RIGHT HAND LAVATORY GUSSET CORRODED AT FORWARD AND AFT NUTPLATES AND AT POTABLE WATER OVERFLOW NIPPLE ..... REMOVED AND REPLACED RIGHT HAND LAVATORY G
- [SDR HNAA2022022300083](https://openairdocs.org/sdr/HNAA2022022300083), Feb 20, 2022: NOT REPORTED. NOT REPORTED. NDIS 660 33-50 0039670 20FEB22 SBY CLOSE SERVICE DOOR EMERGENCY LIGHT IS INOP. FACT 20FEB22 09:45 SBY R&R'D LAMP. NO FIX. LIGHT LEASE COVER IS REMOVED. REPAIRED
- [SDR HNAA2020051800151](https://openairdocs.org/sdr/HNAA2020051800151), May 14, 2020: POTENTIOMETER. OUT OF ADJUST. A/C PULLS HARD LEFT WITH STEERING ON. ADJUSTED NOSE WHEEL STEERING FEEDBACK POT IAW EMB 145 AMM 32-50-00. OPS CHECK SAT. OK FOR SERVICE AT THIS TIME.
- [SDR HNAA2020070900189](https://openairdocs.org/sdr/HNAA2020070900189), May 3, 2020: INVERTER. INOPERATIVE. FOUND DURING RON, CEILING EXIT SIGN ASSY AT ROW 12 FACING AFT INOP. R&R EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECK GOOD.
- [SDR HNAA2019120900378](https://openairdocs.org/sdr/HNAA2019120900378), Dec 6, 2019: HANDLE. OUT OF ADJUST. MAIN CABIN DOOR WOULD NOT OPEN FROM INSIDE THE CABIN. FIX ADJUSTED PAX DOOR INNER HANDLE IAW EMB 145 AMM 52-18-00 OPTS CHECK GOOD AT THIS TIME OK FOR SERVICE.
- [SDR HNAA2019090900265](https://openairdocs.org/sdr/HNAA2019090900265), Sep 8, 2019: WARNING SYSTEM. FALSE ACTIVATION. RTO DUE NO T/O CONFIG BRAKE WARNING AT 60KTS. NO EMERGENCY. CREW/PAX OKAY. MESSAGE CLEARED AND A/C IS GOOD TO GO BY MAINTENANCE.
- [SDR HNAA2019090900258](https://openairdocs.org/sdr/HNAA2019090900258), Sep 7, 2019: UNKNOWN. MALFUNCTIONED. PDIS 660 31-40 2006861 07SEP19 PHL CLOSE FO'S PFD SHOWED NO AIRSPEED INDICATION DURING TAKEOFF ROLL FACT 07SEP19 23:57 PHL PERFORMED ADC OPS CHECK IAW AMM 34-15
- [SDR HNAA2019080800222](https://openairdocs.org/sdr/HNAA2019080800222), Jul 13, 2019: SKIN. CRACKED. FUSELAGE UPPER SKIN CRACKED 2 PLACES,SKIN CRACK 1:ON FRAME 75 AT PREVIOUS REPAIR ON FIRST FASTENER BELOW STR 2L. SKIN CRACK 2: ON STR 2L JUST AFT OF FRAME 75...
- [SDR HNAA2019080800221](https://openairdocs.org/sdr/HNAA2019080800221), Jul 13, 2019: BRACKET. CORRODED. CARGO DR LWR FWD CUTOUT CORRODED AT FRAME 65L PROFILE BRACKET. R&RD CARGO DR LWR FWD CUTOUT AT FRAME 65L PROFILE BRACKET IAW EMB SRM 53-31-04 AND EO1-53-19-0328

All 109: https://openairdocs.org/aircraft/N660CL/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/N660CL/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.
