# N693AE: 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: 14500868
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 12, 2004
- Certificate issued: September 16, 2011
- Expires: September 30, 2027
- Mode S code: A935E0
- 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=693AE
- Page: https://openairdocs.org/aircraft/N693AE

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/N693AE/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 N693AE.

## FAA accident and incident reports

None matched to N693AE.

## Service difficulty reports (179, 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 HNAA2026100500945](https://openairdocs.org/sdr/HNAA2026100500945), Oct 3, 2026: SHROUD. UNSECURE. FLAP FAIL AT 11 DEGREES DURING GO-AROUND. INSP'D FLAPS & FOUND L/H INBD FLAP SHROUD OTBD ROLLER MISSING & FLAP JAMMED INTO SHROUD, REMOVED L/H INBD FLAP, INSTAL
- [SDR HNAA2025060400379](https://openairdocs.org/sdr/HNAA2025060400379), Jun 3, 2025: VALVE. MALFUNCTIONED. DURING CLIMBOUT PACK 1 AND 2 VLVS KEPT CLOSING. GND RAN BOTH PACKS OPS CHECK GOOD. PERFORM PRESSURIZATION OPS IAW AMM 21-31-00 OPS CHECK GOOD OK FOR SERVICE
- [SDR HNAA2024122401244](https://openairdocs.org/sdr/HNAA2024122401244), Nov 27, 2024: FLOOR SUPPORT. CRACKED. F012133 LH OMEGA BEAM SIDE WALL CRACKED AT FR31. PERFORMED REPAIR OF CRACK ON LH OMEGA BEAM SIDE WALL AT FR31 IAW ETD2024-145-032466 AND EO1-53-24-0728.
- [SDR HNAA2024122401243](https://openairdocs.org/sdr/HNAA2024122401243), Nov 27, 2024: FLOOR SUPPORT. CRACKED. F012102 LH OMEGA BEAM CRACKED ON SIDE WALL AT FR29. REMOVED DAMAGE AND PERFORMED DOUBLER FILLER REPAIR IAW ETD2024-145-032096 AND EO-1-53-24-0724.
- [SDR HNAA2024122401242](https://openairdocs.org/sdr/HNAA2024122401242), Nov 23, 2024: FLOOR SUPPORT. CRACKED. F011503 L/H OMEGA BEAM FR-22 HAS CRACK. REPAIRED THE LH OMEGA BEAM AT FR22 IAW EMB ETD2024-145-032094 AND EO1-53-24-0726
- [SDR HNAA2024122401241](https://openairdocs.org/sdr/HNAA2024122401241), Nov 23, 2024: FLOOR SUPPORT. CRACKED. F011500 L/H OMEGA BEAM AT FR-21 HAS CRACK. PERFORMED CUT OUT, DOUBLER AND FILLER REPAIR ON L/H OMEGA BEAM AT FR-21 IAW ETD2024-145-032095 AND EO1-53-24-0723
- [SDR HNAA2024122401257](https://openairdocs.org/sdr/HNAA2024122401257), Nov 22, 2024: FLOOR SUPPORT. CORRODED. F011194 L/H OMEGA GUSSET #2 HAS CORROSION IN MULTIPLES AREAS. RAR L/H OMEGA GUSSET #2 IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024122401256](https://openairdocs.org/sdr/HNAA2024122401256), Nov 22, 2024: FLOOR SUPPORT. CORRODED. F011193 CENTER OMEGA BEAM GUSSET #1 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED CENTER OMEGA BEAM GUSSET #1 IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024122401255](https://openairdocs.org/sdr/HNAA2024122401255), Nov 22, 2024: FLOOR SUPPORT. CORRODED. F011176 L/H FLOOR SILL #3 HAS CORROSION AT MULTIPLES AREAS. REMOVED AND REPLACED L/H FLOOR SILL #3 IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024122401254](https://openairdocs.org/sdr/HNAA2024122401254), Nov 22, 2024: FLOOR SUPPORT. CORRODED. F011175 L/H OMEGA GUSSET #3 HAS CORROSION IN MULTIPLES AREAS. RAR L/H OMEGA GUSSET #3 IAW EMB-145 SRM 51-40-02
- [SDR HNAA2024122401253](https://openairdocs.org/sdr/HNAA2024122401253), Nov 22, 2024: FLOOR SUPPORT. CORRODED. F011174 CENTER OMEGA BEAM GUSSET #2 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED CENTER OMEGA BEAM GUSSET #2 IAW EMB145 SRM 51-40-02.
- [SDR HNAA2024122401240](https://openairdocs.org/sdr/HNAA2024122401240), Nov 22, 2024: FLOOR SUPPORT. CORRODED. F011310 SERVICE DOOR LOWER CENTER FLOOR SILL HAVE CORROSION. REMOVED CORROSION AT CENTER HOLE OF THE SERVICE DOOR LOWER CENTER FLOOR SILL AND FOUND IT WITHIN AL
- [SDR HNAA2024122401259](https://openairdocs.org/sdr/HNAA2024122401259), Nov 21, 2024: FLOOR SUPPORT. CORRODED. F010813 CABIN LH CENTER FLOOR GUSSET CORRODED BETWEEN FR 45 / 53. R A R CABIN L/H FLOOR GUSSET FR 45/53 IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024122401258](https://openairdocs.org/sdr/HNAA2024122401258), Nov 21, 2024: FLOOR SUPPORT. CORRODED. F010812 CABIN RH CENTER FLOOR GUSSET CORRODED BETWEEN FR 45 / 53. REMOVED AND REPLACED RH CENTER FLOOR GUSSET BETWEEN FR 45 / 53 IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024122401252](https://openairdocs.org/sdr/HNAA2024122401252), Nov 21, 2024: FLOOR SUPPORT. CORRODED. F010835 LH #4 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED LH #4 FLOOR SUPPORT IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024122401251](https://openairdocs.org/sdr/HNAA2024122401251), Nov 21, 2024: FLOOR SUPPORT. CORRODED. F010824 RH CENTER FLOOR GUSSET CORRODED BETWEEN FR 35 / 39. RAR R/H CENTER FLOOR GUSSET FR 35/39 IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024122401250](https://openairdocs.org/sdr/HNAA2024122401250), Nov 21, 2024: FLOOR SUPPORT. CORRODED. F010822 RH CENTER FLOOR GUSSET CORRODED BETWEEN FR 38 / 45. REMOVED AND REPLACED RH CENTER FLOOR GUSSET BETWEEN FR 38 / 45 IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024122401249](https://openairdocs.org/sdr/HNAA2024122401249), Nov 20, 2024: DOOR FRAME. CHAFED. F010194 CARGO DOOR FRAME LOWER EDGE CHAFED. REMOVED AND REPLACED CARGO DOOR FRAME LOWER EDGE PROFILE IAW EMB 145 SRM 51-20-01 AND 51-40-02
- [SDR HNAA2024122401239](https://openairdocs.org/sdr/HNAA2024122401239), Nov 20, 2024: SHEAR TIE. CRACKED. F010566 CARGO UNDER FLOOR SHEAR CLIP AT FR 73 BETWEEN STGR 16L / 17L CRACKED. REMOVED AND REPLACED CARGO UNDER FLOOR SHEAR CLIP AT FR 73 BETWEEN STGR 16L / 17L 
- [SDR HNAA2024122401238](https://openairdocs.org/sdr/HNAA2024122401238), Nov 20, 2024: FRAME. CRACKED. CARGO FR 73 CRACKED BETWEEN STGR 16R/17R. RAR CARGO FR73 IAW EMB 145 SRM 51-40-02
- [SDR HNAA2024122401237](https://openairdocs.org/sdr/HNAA2024122401237), Nov 20, 2024: SHEAR TIE. CRACKED. CARGO SHEAR CLIP AT FR66 BETWEEN STGR 6L / 7L CRACKED. REMOVED AND REPLACED SHEAR CLIP AT FR66 BETWEEN STGR 6L / 7L IAW EMB-145 SRM 51-40-02.
- [SDR HNAA2024122401248](https://openairdocs.org/sdr/HNAA2024122401248), Nov 18, 2024: RIB. CRACKED. F009621 RH WING RIB 21 IS CRACKED AT FWD AND AFT END. PERFORMED PERMANENT REPAIR OF RH WING RIB 21 AFT END IAW EMB 145 ETD2024-145-033676 AND EO1-57-24-0730. ND
- [SDR HNAA2024122401247](https://openairdocs.org/sdr/HNAA2024122401247), Nov 18, 2024: RIB. CRACKED. F009620 LH WING RIB 21 IS CRACKED AT AFT END. PERFORMED REPAIR OF LH WING RIB 21 AT AFT END IAW EMB 145 ETD2024-145-031113 AND EO1-57-24-0727
- [SDR HNAA2024122401246](https://openairdocs.org/sdr/HNAA2024122401246), Nov 16, 2024: SKIN. CRACKED. F008527 THE EXTERNAL SKIN OF THE FUSELAGE IS CRACKED AT FRAME 75 BETWEEN STRINGERS 1L AND 2L. PERFORMED REPAIR ON EXTERNAL SKIN OF THE FUSELAGE AT FRAME 75 BETW
- [SDR HNAA202412241245](https://openairdocs.org/sdr/HNAA202412241245), Nov 16, 2024: SKIN. CORRODED. F008493 LAVATORY BUCKET EXTERNAL SKIN AROUND WASTE VALVE CORRODED. REMOVED AND REPLACED LAVATORY BUCKET IAW EMB145 SRM 51-40-02
- [SDR SIMA20221029002](https://openairdocs.org/sdr/SIMA20221029002), Oct 29, 2022: NONE. INOPERATIVE. FA FORWARD FLASHLIGHT INOP-C/A-SPARE FLASHLIGHT PROVIDED TO FLIGHT ATTENDANT. FLASHLIGHT DEFERRED PER EMB145 MEL 25-32. M PROCEDURES C/W
- [SDR SIMA20220826002](https://openairdocs.org/sdr/SIMA20220826002), Aug 26, 2022: NONE. BROKEN. REAR FA EMERGENCY FLASHLIGHT CLIP BROKEN-C/A-REMOVED AND REPLACED BROKEN CLIP ON REAM FA FLASHLIGHT IAW ASTRONICS DME CMM 25-60-14.
- [SDR SIMA20220426004](https://openairdocs.org/sdr/SIMA20220426004), Apr 26, 2022: NONE. NONE. BLEED 1 LEAK ON CLIMBOUT DECLARED EMERGENCY. REF ITEM #1 WHILE PERFORMING BLEED LEAK INSPECTION FOUND WARNING ELEMENT IN ENG 1 DISCONNECTED AND CHAFFING ON FITT
- [SDR SIMA20220131001](https://openairdocs.org/sdr/SIMA20220131001), Jan 31, 2022: NONE. NONE. FA EMERGENCY FLASHLIGHT HOLDER BRACKET CRACKED-C/A-RAR FA FLASHLIGHT HOLDER BRACKET IAW EMB 145 CMM 25-60-14.
- [SDR SIMA20211001001](https://openairdocs.org/sdr/SIMA20211001001), Oct 1, 2021: NONE. NONE. FA REPORTS REAR CABIN FLASHLIGHT HOLDER BROKEN.-C/A-RAR AFT CABIN FLASHLIGHT HOLDER ASSY IAW ETN-EM-33-059.
- [SDR SIMA20210609004](https://openairdocs.org/sdr/SIMA20210609004), Jun 9, 2021: COMPRESSOR. DAMAGED. ENG 1 FAILURE ON CLIMBOUT, AFTER T/O CHECK COMPLETE, PASSING 5,500 FT LOUD BANG ENG 1 FAIL MESSAGE ON EICAS E1 FAILURE / DECLARED EMERGENCY / EQP SWAP FLT CONT.
- [SDR SIMA20210528001](https://openairdocs.org/sdr/SIMA20210528001), May 28, 2021: POWER SUPPLY. FAILED. EMERGENCY LIGHT NOT ARMED CAUTION MESSAGE AFTER TAKEOFF. RAN QRH AND DIDN?T FIX PROBLEM. C19 CRCT BRKR POPPED AND EMER LGTS LASTED 20 MIN-C/A-RAR EMERGENCY LIGH
- [SDR SIMA20210310001](https://openairdocs.org/sdr/SIMA20210310001), Mar 10, 2021: CRADLE. BROKEN. FA EMETRGENCY FLASHLIGHT HOLDER BROKEN-C/A- RAR FWD FA EMERGENCY FLASHLIGHT ASSY IAW ETN-EM-33-059
- [SDR SIMA20210109004](https://openairdocs.org/sdr/SIMA20210109004), Jan 9, 2021: LIGHT. INOPERATIVE. MAIN DOOR HINGE COVER EMERGENCY LIGHT INOPERABLE. C/A: R & R MAIN DOOR HINGE COVER EMERGENCY LIGHT, IAW EMB 145 AMM 33-50-10 2J(3) AND 3I(3). OPERATIONS CHECK G
- [SDR SIMA20201208001](https://openairdocs.org/sdr/SIMA20201208001), Dec 8, 2020: FLASHLIGHT. MISSING. COCKPIT EMERGENCY FLASH LIGHT MISSING ABOVE PBE. C/A: FLIGHT CREW PLACARDED, PER MEL2553 AUTH120078-C MOC 135181.
- [SDR SIMA20201020002](https://openairdocs.org/sdr/SIMA20201020002), Oct 20, 2020: LIGHT. INOPERATIVE. MAIN DOOR EMERGENCY LIGHT INOPERABLE. C/A: R & R MAIN DOOR EXTERNAL EMERGENCY LIGHT, IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPERATIONS CHECK GO
- [SDR SIMA2020031306004](https://openairdocs.org/sdr/SIMA2020031306004), Mar 6, 2020: HINGE FITTING. DAMAGED. RUDDER 1 UPPER HINGE POINT FOR RUDDER 2 BALL BEARING REQUIRES REPLACEMENT DUE TO BOLT FAILING DIMENSIONAL CHECK.-C/A-REMOVED AND REPLACED RUDDER 1 UPPER HINGE F
- [SDR SIMA2020031205006](https://openairdocs.org/sdr/SIMA2020031205006), Mar 5, 2020: BUSHING. MIGRATED. LH AILERON DAMPER FITTING HAS MIGRATING HAT BUSHINGS-C/A-LH AILERON DAMPER FITTING REPLACEMENT IAW EO-EM-27MR-112.
- [SDR SIMA202003022007](https://openairdocs.org/sdr/SIMA202003022007), Feb 22, 2020: CROSSBEAM. CRACKED. CROSSBEAM JUST BEHIND NOSE UPLOCK BOX IS CRACKED.-C/A-INSTALLED NEW CROSSBEAM BEHIND NOSEE UPLOCK BOX IAW SRM 51-40-02.
- [SDR SIMA2020031321010](https://openairdocs.org/sdr/SIMA2020031321010), Feb 21, 2020: SKIN. CRACKED. CARGO DOOR SKIN HAS APPROXIMATELY A 1" CRACK ON UPPER AFT SIDE OF HANDLE CUT OUT.-C/A-COMPLIED WITH REPAIR IAW ERS-EM-52MR-1064.
- [SDR SIMA2020030621009](https://openairdocs.org/sdr/SIMA2020030621009), Feb 21, 2020: RIB. CRACKED. RIGHT SIDE OF THE UPPER FUSELAGE WINDSHIELD CUTOUT IS CRACKED BY THE NUT PLATE.-C/A-REPAIRED RH SIDE WHINSHIELD CUT-OUT GRAB HANDLE IAW ERS-EM-5300-4064.
- [SDR SIMA2020030621008](https://openairdocs.org/sdr/SIMA2020030621008), Feb 21, 2020: FRAME. DAMAGED. FRAME 60 HAS A TOOLING MARK BETWEEN STRINGERS 4L-5L.-C/A-REPAIRED FRAME 60, BETWEEN STRS 4L-5L IAW SRM 53-00-04 ENTERED INTO DET-EM-53-972.
- [SDR SIMA2020030521005](https://openairdocs.org/sdr/SIMA2020030521005), Feb 21, 2020: ANGLE. CRACKED. LEFT WING UPPER SURFACE "L" ANGLE AT WING ROOT IS CRACKED, ANGLE SUPPORT FOR 193EL.-C/A-REMOVED AND REPLACED LT WING UPPER SURFACE L ANGLE AT WING ROOT IAW SRM 
- [SDR SIMA2020030521004](https://openairdocs.org/sdr/SIMA2020030521004), Feb 21, 2020: ANGLE. CRACKED. RIGHT WING FORWARD UPPER "L" ANGLE AT WING ROOT IS CRACKED, ANGLE SUPPORT FOR PANEL 194ER.-C/A-REMOVED AND REPLACED RT WING UPPER SURFACE WING L ANGLE AT WING R
- [SDR SIMA2020030521006](https://openairdocs.org/sdr/SIMA2020030521006), Feb 21, 2020: SKIN PANEL. CRACKED. RIGHT AFT UPPER FUSELAGE SKIN PANEL HAS NUMEROUS CRACKS AROUND RIVETS.-C/A-INSTALLED REPAIR BUSHING ON RH AFT FUSELAGE FRAME 77 AND RESTORED PAINT FINISH IAW SR
- [SDR SIMA2020030521007](https://openairdocs.org/sdr/SIMA2020030521007), Feb 21, 2020: SKIN PANEL. CRACKED. LEFT AFT UPPER FUSELAGE SKIN PANEL HAS NUMEROUS CRACKS AROUND RIVETS.-C/A-INSTALLED REPAIR BUSHINGS 4EA ON L/H AFT FUSELAGE SKIN ON FRAME 77 AND RESTORED PAINT 
- [SDR SIMA2020030519011](https://openairdocs.org/sdr/SIMA2020030519011), Feb 19, 2020: DOOR SILL. CORRODED. CENTER SERVICE DOOR SILL IS CORRODED-C/A-COMPLETED INSTALLATION OF SERVICE DOOR SILL IAW SRM 51-40-02, RESTORED SURFACE PROTECTION IAW CPM 51-21-06.
- [SDR SIMA2020030519012](https://openairdocs.org/sdr/SIMA2020030519012), Feb 19, 2020: SUPPORT BRACKET. CRACKED. BAGGAGE DOOR LIFTING/LOWERING MECH AFT LOWER SUPPORT BRACKET IS CRACKED.( APPROX 1" LONG) -C/A-REPLACED BAGGAGE DOOR LIFTING/LOWERING MECH AFT LOWER SUPPORT BRA
- [SDR SIMA202003029006](https://openairdocs.org/sdr/SIMA202003029006), Feb 19, 2020: DOOR SILL. CORRODED. CARGO DOOR CUTOUT SILL IS CORRODED.-C/A-REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02. RESTORED SURFACE PROTECTION IAW CPM 51-21-06.
- [SDR SIMA2020040612007](https://openairdocs.org/sdr/SIMA2020040612007), Feb 12, 2020: WIRE. BROKEN. EMERGENCY LIGHT STRIPS #2 AND #3 HAVE BROKEN WIRES.-C/A-REMOVED AND REPLACED THE EMERGENCY LIGHT STRIPS #2 AND #3. IAW AMM 33-50-12.

All 179: https://openairdocs.org/aircraft/N693AE/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/N693AE/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

---
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