# N640AE: 1999 Embraer EMB-145LR

- Status: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212, 55 seats)
- Engine: [Allison AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030)
- 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: 145183
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 29, 1999
- Certificate issued: September 12, 2011
- Expires: September 30, 2027
- Mode S code: A86540
- 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=640AE
- Page: https://openairdocs.org/aircraft/N640AE

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

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

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

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-08-07](https://openairdocs.org/ad/2025-08-07): Flight Controls · Embraer EMB-145, EMB-145ER, EMB-145MR and 4 more. Effective Jun 26, 2025
- [AD 2024-26-07](https://openairdocs.org/ad/2024-26-07): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 11, 2025
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2021-07-14](https://openairdocs.org/ad/2021-07-14): Main landing gear · Yaborã Indústria Aeronáutica EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Apr 20, 2021
- [AD 2021-04-09](https://openairdocs.org/ad/2021-04-09): Engine fuel and control · Yaborã Indústria Aeronáutica EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Mar 30, 2021
- [AD 2019-03-30](https://openairdocs.org/ad/2019-03-30): Engine Exhaust · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 26, 2019
- [AD 2017-15-16](https://openairdocs.org/ad/2017-15-16): Flight controls · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Sep 5, 2017
- [AD 2017-12-09](https://openairdocs.org/ad/2017-12-09): Fuel · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Jul 20, 2017
- [AD 2017-04-12](https://openairdocs.org/ad/2017-04-12): Ice and rain protection · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Mar 29, 2017
- [AD 2015-02-13](https://openairdocs.org/ad/2015-02-13): Nacelles/pylons; Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 6, 2015
- [AD 2013-22-18](https://openairdocs.org/ad/2013-22-18): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Nov 20, 2013
- [AD 2012-19-06](https://openairdocs.org/ad/2012-19-06): Stabilizers · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 9 more. Effective Oct 29, 2012
- [AD 2011-21-15](https://openairdocs.org/ad/2011-21-15): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 7 more. Effective Nov 23, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2010-16-02](https://openairdocs.org/ad/2010-16-02): Airborne Auxiliary Power · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 9, 2010
- [AD 2010-16-01](https://openairdocs.org/ad/2010-16-01): Fuel · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Sep 9, 2010
- [AD 2010-12-07](https://openairdocs.org/ad/2010-12-07): Wings · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jul 22, 2010
- [AD 2010-11-01](https://openairdocs.org/ad/2010-11-01): Fuselage · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jul 6, 2010
- [AD 2010-10-11](https://openairdocs.org/ad/2010-10-11): Landing gear · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jun 21, 2010
- [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010
- [AD 2010-03-07](https://openairdocs.org/ad/2010-03-07): Landing gear · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 11, 2010
- [AD 2009-26-02](https://openairdocs.org/ad/2009-26-02): Ice and rain protection · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 19, 2010
- [AD 2009-01-05](https://openairdocs.org/ad/2009-01-05): Maximum takeoff weight (MTOW) · Embraer EMB-145, EMB-145EP, EMB-145ER and 4 more. Effective Mar 27, 2009
- [AD 2008-22-19](https://openairdocs.org/ad/2008-22-19): Flight deck · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 19, 2008
- [AD 2008-17-05](https://openairdocs.org/ad/2008-17-05): Fuel tanks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 23, 2008
- [AD 2008-10-08](https://openairdocs.org/ad/2008-10-08): Reduces the compliance time for doing the modification · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective May 23, 2008
- [AD 2008-05-02](https://openairdocs.org/ad/2008-05-02): Tail section or rudder pedals · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Apr 8, 2008
- [AD 2008-03-03](https://openairdocs.org/ad/2008-03-03): Elevator control system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Feb 14, 2008
- [AD 2007-24-03](https://openairdocs.org/ad/2007-24-03): Forward fuselage right hand (RH) side skin · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jan 2, 2008
- [AD 2007-10-11](https://openairdocs.org/ad/2007-10-11): Electrical bonding clamps · Embraer EMB-135BJ (Legacy 600), EMB-135LR, EMB-145LR and 2 more. Effective Jun 21, 2007
- [AD 2007-04-09](https://openairdocs.org/ad/2007-04-09): Left- and right-hand windshield temperature controllers · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 23, 2007
- [AD 2007-04-03](https://openairdocs.org/ad/2007-04-03): Pitot static heating relay K0057 · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 21, 2007
- [AD 2006-19-04](https://openairdocs.org/ad/2006-19-04): Honeywell COM unit and Mode S transponder · Bombardier BD-700-1A10, BD-700-1A11, 550 and 26 more. Effective Oct 17, 2006
- [AD 2006-16-17](https://openairdocs.org/ad/2006-16-17): Torque values of the screws that attach the seat tracks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 25, 2006
- [AD 2006-07-01](https://openairdocs.org/ad/2006-07-01): Horizontal stabilizer control unit (HSCU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective May 1, 2006
- [AD 2006-03-06](https://openairdocs.org/ad/2006-03-06): Pilot's and co-pilot's seat tracks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 13, 2006
- [AD 2005-25-17](https://openairdocs.org/ad/2005-25-17): Auxiliary power unit (APU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 18, 2006
- [AD 2005-24-11](https://openairdocs.org/ad/2005-24-11): Elevator gust lock system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 9, 2006
- [AD 2005-24-02](https://openairdocs.org/ad/2005-24-02): Airplane flight manual (AFM) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 28, 2005
- [AD 2005-23-20](https://openairdocs.org/ad/2005-23-20): Auxiliary power unit (APU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 27, 2005
- [AD 2005-23-13](https://openairdocs.org/ad/2005-23-13): Nose landing gear (NLG) wheel · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 19, 2005
- [AD 2005-22-08](https://openairdocs.org/ad/2005-22-08): Total air temperature (TAT) sensor heating system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Nov 30, 2005
- [AD 2005-20-37](https://openairdocs.org/ad/2005-20-37): Main landing gear (MLG) trailing arms and integrity of the MLG pivot axle sealant. · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Nov 16, 2005
- [AD 2005-14-02](https://openairdocs.org/ad/2005-14-02): Left and right engine fire handles · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Aug 15, 2005
- [AD 2005-14-03](https://openairdocs.org/ad/2005-14-03): Engine-driven hydraulic pump · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Aug 10, 2005
- [AD 2005-13-22](https://openairdocs.org/ad/2005-13-22): Electric fuel pumps · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jul 7, 2005
- [AD 2005-05-09](https://openairdocs.org/ad/2005-05-09): Forward upper liners · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Apr 14, 2005
- [AD 2005-04-05](https://openairdocs.org/ad/2005-04-05): Air turbine starter (ATS) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 24, 2005
- [AD 2005-01-05](https://openairdocs.org/ad/2005-01-05): Nose Landing Gear Wheel Nuts and Associated Inner and Outer Seals, and Reidentifying the Landing Gear Strut · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Feb 9, 2005

### Matched by engine (Allison AE-3007A)

- [AD 2020-16-13](https://openairdocs.org/ad/2020-16-13): Turbine Engine Compressor Section · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Aug 14, 2020
- [AD 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018
- [AD 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 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 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 120: https://openairdocs.org/aircraft/N640AE/ads.md

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

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

## NTSB investigations

None matched to N640AE.

## 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 20031124036469I](https://openairdocs.org/incident/20031124036469I), Nov 24, 2003: Emb EMB145LR (N640AE), Covington/Cinci, KY, Minor damage. (-23) Normal taxi from gate. Upon reaching the end of concourse a, first officer alerted the PIC of an approaching baggage tug and said, "stop". The PIC…

## Service difficulty reports (282, 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 HNAA2026100200941](https://openairdocs.org/sdr/HNAA2026100200941), Oct 1, 2026: PIN. DAMAGED. WIRE DE-PINNED @ EMERGENCY FLOOR LIGHTS CONNECTOR BETWEEN ROWS 9 AND 10. REPINNED WIRE & INSTALLED NEW MALE CONNECTOR IAW WM 33-50-50. PERFORMED OPS CHECK IRW A
- [SDR HNAA2026092300899](https://openairdocs.org/sdr/HNAA2026092300899), Sep 4, 2026: SPAR. CRACKED. RELEVANT INDICATION NOTED DURING HFEC OF LT PYLON SPAR 2 UPPER FLANGE AFT FASTENER HOLE. REPAIRED LT PYLON SPAR 2 UPPER FLANGE AFT FASTENER HOLE TO 1ST OVERSIZE
- [SDR HNAA2026092300898](https://openairdocs.org/sdr/HNAA2026092300898), Sep 4, 2026: SPAR. CRACKED. RELEVANT INDICATION NOTED DURING HFEC OF RT PYLON SPAR 2 UPPER FLANGE AFT FASTENER HOLE. REPAIRED RT PYLON SPAR 2 UPPER FLANGE AFT FASTENER HOLE TO 1ST OVERSIZE
- [SDR HNAA2026092300897](https://openairdocs.org/sdr/HNAA2026092300897), Aug 30, 2026: MOUNT. CRACKED. RUDDER II PANEL 327FR LOWER MOUNTING FLANGE CRACKED ON RH SIDE. REMOVED CRACKED RUDDER II PANEL 327FR LOWER MOUNTING FLANGE (RIB), PREPPED AND INSTALLED SERVICE
- [SDR HNAA2026092300896](https://openairdocs.org/sdr/HNAA2026092300896), Aug 25, 2026: SHEAR TIE. CRACKED. CABIN SHEAR TIE CRACKED AT FR-61 BETWEEN STGRS 6L/7L. REMOVED AND REPLACED CRACKED CABIN SHEAR TIE IAW SRM 51-40-02.
- [SDR HNAA2026092300895](https://openairdocs.org/sdr/HNAA2026092300895), Aug 25, 2026: DOOR SILL. CORRODED. CARGO DOOR SILL CORRODED IN MULTIPLE AREAS. R & R CARGO DOOR SILL IAW SRM 51-40-02.
- [SDR HNAA2026092300893](https://openairdocs.org/sdr/HNAA2026092300893), Aug 25, 2026: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT NR 4 HAD CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR HNAA2026092300892](https://openairdocs.org/sdr/HNAA2026092300892), Aug 25, 2026: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT HAD CORROSION IN MULTIPLE AREAS. R & R THE FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR HNAA2026092300891](https://openairdocs.org/sdr/HNAA2026092300891), Aug 25, 2026: FLOOR SUPPORT. CORRODED. RIGHT CABIN FLOOR SUPPORT NR 2 CORRODED IN NUMEROUS AREAS. R & R RT CABIN FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR HNAA2026092300890](https://openairdocs.org/sdr/HNAA2026092300890), Aug 25, 2026: FLOOR SUPPORT. CORRODED. LEFT CABIN FLOOR SUPPORT NR 2 CORRODED IN NUMEROUS AREAS. REMOVED AND REPLACED LH CABIN FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR HNAA2026092300889](https://openairdocs.org/sdr/HNAA2026092300889), Aug 25, 2026: SEAT TRACK. CORRODED. LEFT UPPER SEAT TRACK NR 3 CORRODED IN NUMEROUS AREAS. R & R LT UPPER SEAT TRACK IAW AMM 53-01-06
- [SDR HNAA2026092300901](https://openairdocs.org/sdr/HNAA2026092300901), Aug 22, 2026: SKIN. CRACKED. FUSELAGE SKIN HAD A POSSIBLE CRACK AT A RIVET AT FRAME 78, JUST BELOW STRINGER 4L. REPAIRED CRACKED FUSELAGE SKIN IAW EO1-53-26-0433 AND SRM 53-32-01
- [SDR HNAA2026092300900](https://openairdocs.org/sdr/HNAA2026092300900), Aug 22, 2026: SKIN. DENTED. LEFT ELEVATOR LOWER EXTERNAL SKIN HAS A DENT, AFT AND OTBD OF 335BB. PERFORMED DRILL OUT AND RECONTOURED DENTED AREA, INSTALLED BLIND RIVET IAW ETD2026-145-0147
- [SDR HNAA2026092300894](https://openairdocs.org/sdr/HNAA2026092300894), Aug 22, 2026: HINGE FITTING. EXCESS PLAY. RUDDER UPPER HINGE FITTING, AT VERTICAL STAB, HAS PLAY. REMOVED AND REPLACED RUDDER UPPER HINGE FITTING IAW SRM 51-40-02 AND AMM 20-10-01.
- [SDR HNAA2026051800383](https://openairdocs.org/sdr/HNAA2026051800383), May 15, 2026: LIGHT. INOPERATIVE. EMERGENCY LIGHT STRIP FOR SEAT 8A TO 9A INOP. R & R LIGHT STRIP IRT AMM 33-50-12 P/N ON 6636-8 P/N OFF 6636-8
- [SDR HNAA2026042400356](https://openairdocs.org/sdr/HNAA2026042400356), Apr 23, 2026: SWITCH. OUT OF ADJUST. AFTER TAKE OFF AIR/GND FAIL MSG. SELECTED GEAR UP WITH NO GEAR RETRACTION. UPON INSPECTION FOUND NLG WOW SWITCH NO MAKING GAP WITH TARGET. ADJUSTED GAP ON NLG W
- [SDR HNAA2026020400110](https://openairdocs.org/sdr/HNAA2026020400110), Feb 3, 2026: GEARBOX. FAILED. ON APPROACH FLAP LOW SPEED FOLLOWED BY FLAP FAIL. STUCK AT 45*. MESSAGES APPEARED FROM 22* TO 45* R/R L/H O/B FLAP ANGLE GEARBOX IRT AMM 27-51-02-000/400-801-A.
- [SDR HNAA202601230072](https://openairdocs.org/sdr/HNAA202601230072), Jan 22, 2026: CONTROL UNIT. ABNORMAL. FLAP FAIL DISPLAYED ON EICAS ON APPROACH. RMU SHOWS RT FLAP AT 41 DEGREES & LEFT FLAP BLANKED OUT. EICAS & ACTUAL FLAP SHOWS 45 DEGREES BOTH SIDES. FACT 24JAN26
- [SDR HNAA2025111700740](https://openairdocs.org/sdr/HNAA2025111700740), Nov 16, 2025: PRESSURE SWITCH. FAULTED. RUDDER SYSTEM 2 INOP DISPLAYED DURING TAKE-OFF AT ABOUT 50 KNOTS. R&R RUDDER PRESSURE SWITCH IN REF WITH 27-23-04-000-A/400-801-A. R&R RELAY K0387 IN REF WITH A
- [SDR HNAA2025102700724](https://openairdocs.org/sdr/HNAA2025102700724), Oct 26, 2025: CONTROLLER. FAULTED. AUTO PRESS FAIL MEL C29930 21-12-3 PRESS CONTROL AUTO AND MANUAL
- [SDR HNAA2025090400586](https://openairdocs.org/sdr/HNAA2025090400586), Sep 4, 2025: CONTROL UNIT. FAILED. WHILE ON RUNWAY AN EICAS MESSAGE OF BRAKE DEGRADED APPEARED. REMOVED AND REPLACED BCU IRT EMB 145 AMM 32-41-02 OP. S CHECK GOOD.
- [SDR HNAA2025072300472](https://openairdocs.org/sdr/HNAA2025072300472), Jul 22, 2025: START VALVE. FAULTED. DURING CLIMB AT ABOUT 3K BLEED 2 LEAK MESAGE ON EICAS, C/W QRH, MESSAGE CLEARED FACT 22JUL25 10:51 CLT RRD GROUND AIR START CONNNECTION ASSY IAW AMM 36-10-02. L
- [SDR HNAA2025050100295](https://openairdocs.org/sdr/HNAA2025050100295), Apr 30, 2025: CHECK VALVE. MISINSTALLED. AFTER T/O LG LEVER DISAGREE. HANDLE SELECTED UP GEAR REMAINED DOWN FACT 01MAY25 15:59 SBY UPON INSPECTION OF #100 HYDRULIC ACCUMILATOR, FOUND T-FITTING CHECK VA
- [SDR HNAA2024032700233](https://openairdocs.org/sdr/HNAA2024032700233), Mar 8, 2024: NONE. NONE. E026820 NO REPAIR INFO FOUND FOR SKIN BUSHING REPAIR FR 77 STGR 8L-9L. REMOVED EXISTING SKIN BUSHING REPAIR AT FR 77 BTW STR 8L-9L, RE-ACCOMPLISHED SKIN BUSHING
- [SDR HNAA2024032700232](https://openairdocs.org/sdr/HNAA2024032700232), Mar 8, 2024: NONE. NONE. E026819 NO REPAIR INFO FOUND FOR STGR 19L REPAIR BTW FR 52-53. RE-ACCOMPLISHED REPAIR FOR DTI FCD ON STR 19L BTW FR 52-53 IAW PIEDMONT EO1-53-24-0204 AND EMB 14
- [SDR HNAA2024032700231](https://openairdocs.org/sdr/HNAA2024032700231), Mar 8, 2024: NONE. NONE. E026818 NO REPAIR INFO FOUND FOR STGR 19R REPAIR BTW FR 52-53. REACCOMPLISHED SINGLE DOUBLER REPAIR ON STGR 19R BETWEEN FR 52-53 IAW EMB 145 SRM 53-24-02, ITEM 
- [SDR HNAA2024032700230](https://openairdocs.org/sdr/HNAA2024032700230), Mar 8, 2024: FRAME. CRACKED. E026728 FR 66 CRACKED STGR 17L-18L BELOW CARGO DOOR SILL. RAR LOWER FR 66 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024032700220](https://openairdocs.org/sdr/HNAA2024032700220), Mar 8, 2024: NONE. NONE. E026833 NO REPAIR INFO FOUND FOR EXTERNAL LAV BUCKET DOUBLER. RE-ACCOMPLISHED EXTERNAL LAV BUCKET DOUBLER IAW EMB 145 SRM 53-31-02/RE AND ITEM 2 FIG 201, ETD202
- [SDR HNAA2024032700219](https://openairdocs.org/sdr/HNAA2024032700219), Mar 8, 2024: NONE. NONE. E026827 : NO REPAIR INFO FOUND FOR SKIN BUSHING REPAIR FR 77 STGR 8R-9R. REMOVED EXISTING SKIN BUSHING REPAIR AT FR 77 BTW STR 8R-9R, RE-ACCOMPLISHED SKIN BUSHI
- [SDR HNAA2024032700218](https://openairdocs.org/sdr/HNAA2024032700218), Mar 8, 2024: NONE. NONE. E026826 NO REPAIR INFO FOUND FOR SKIN BUSHING REPAIR FR 79 STGR 5R-6R. REMOVED EXISTING SKIN BUSHING REPAIR AT FR 79 BTW STR 5R-6R, RE-ACCOMPLISHED SKIN BUSHING
- [SDR HNAA2024032700217](https://openairdocs.org/sdr/HNAA2024032700217), Mar 8, 2024: NONE. NONE. E026825 NO REPAIR INFO FOUND FOR SKIN BUSHING REPAIR FR 79 STGR 3R-4R. REMOVED EXISTING SKIN BUSHING REPAIR AT FR 79 BTW STR 3R-4R, RE-ACCOMPLISHED SKIN BUSHING
- [SDR HNAA2024032700216](https://openairdocs.org/sdr/HNAA2024032700216), Mar 8, 2024: NONE. NONE. E026824 NO REPAIR INFO FOUND FOR SKIN BUSHING REPAIR FR 79 STGR 3L-4L. REMOVED EXISTING SKIN BUSHING REPAIR AT FR 79 BTW STR 3L-4L, RE-ACCOMPLISHED SKIN BUSHING
- [SDR HNAA2024032700215](https://openairdocs.org/sdr/HNAA2024032700215), Mar 8, 2024: NONE. NONE. E026823 NO REPAIR INFO FOUND FOR SKIN BUSHING REPAIR FR 79 STGR 4L-5L. REMOVED EXISTING SKIN BUSHING REPAIR AT FR 79 BTW STR 4L-5L, RE-ACCOMPLISHED SKIN BUSHING
- [SDR HNAA2024032700214](https://openairdocs.org/sdr/HNAA2024032700214), Mar 8, 2024: NONE. NONE. E026821 NO REPAIR INFO FOUND FOR SKIN BUSHING REPAIR FR 79 STGR 6L-7L. REMOVED EXISTING SKIN BUSHING REPAIR AT FR 79 BTW STR 6L-7L, RE-ACCOMPLISHED SKIN BUSHING
- [SDR HNAA2024032700201](https://openairdocs.org/sdr/HNAA2024032700201), Mar 6, 2024: SUPPORT. CORRODED. E026360 GALLEY CENTER BEAM RAMP SUPPORT AT FR20 CORRODED. REMOVED CORRODED GALLEY CENTER BEAM RAMP SUPPORT, INSTALLED SERVICEABLE RAMP SUPPORT IAW EMB 145 SRM 5
- [SDR HNAA2024032700200](https://openairdocs.org/sdr/HNAA2024032700200), Mar 6, 2024: CAP. CORRODED. E026358 CORROSION ON RH MLG FWD BEARING CAP. REMOVED AND REPLACED RH MLG FWD BEARING CAP IAW EMB 145 AMM 32-10-01.
- [SDR HNAA2024032700229](https://openairdocs.org/sdr/HNAA2024032700229), Mar 4, 2024: SHEAR TIE. CRACKED. E026057 FR 10 SHEAR CLIP CRACKED JUST BELOW THE LH DV WINDOW CUT-OUT. REMOVED AND REPLACED LH FR10 SHEAR CLIP JUST BELOW DV WINDOW CUTOUT IAW EMB 145 SRM 51-40-
- [SDR HNAA2024032700228](https://openairdocs.org/sdr/HNAA2024032700228), Mar 4, 2024: BULKHEAD. CRACKED. E025977 NLG WHEEL WELL RH BULKHEAD CRACKED INSIDE NOSE HYDRAULIC COMPARTMENT, AT AFT UPPER END OF BULKHEAD. REPAIRED NLG WHEEL WELL RH BULKHEAD CRACK INSIDE NOS
- [SDR HNAA2024032700199](https://openairdocs.org/sdr/HNAA2024032700199), Mar 4, 2024: UNKNOWN. CORRODED. E025899 FWD DIGITAL IS CORRODED AT LH BEAM. ACCOMPLISHED REPAIR OF FWD DIGITAL AT LH BEAM IAW ETD# ETD2024-145-006688
- [SDR HNAA2024032700227](https://openairdocs.org/sdr/HNAA2024032700227), Mar 3, 2024: SHEAR TIE. CRACKED. E025727 RH SIDE SHEAR CLIP AT STRINGER 15R FRAME 25 IS CRACKED. RAR RH SIDE SHEAR CLIP AT STRINGER 15R FRAME 25 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024032700226](https://openairdocs.org/sdr/HNAA2024032700226), Mar 3, 2024: SHEAR TIE. CRACKED. E025726 RH SIDE SHEAR CLIP AT STRINGER 15R FRAME 26 IS CRACKED. RAR RH SIDE SHEAR CLIP AT STRINGER 15R FRAME 26 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024032700213](https://openairdocs.org/sdr/HNAA2024032700213), Mar 3, 2024: SUPPORT. CORRODED. E025820 GALLEY LH OMEGA BEAM HAS CORROSION ON SIDE WALL AT FRAME 20. REPAIRED GALLEY LH OMEGA BEAM CORROSION ON SIDE WALL AT FR 20 IAW PIEDMONT EO1-53-24-0209 A
- [SDR HNAA2024032700212](https://openairdocs.org/sdr/HNAA2024032700212), Mar 3, 2024: SUPPORT. CRACKED. E025819 GALLEY LH OMEGA BEAM IS CRACKED ON SIDE WALL AFT OF FRAME 23. REPAIRED CRACKED GALLEY LH OMEGA BEAM ON SIDE WALL AFT OF FRAME 23 IAW PIEDMONT EO1-53-24-
- [SDR HNAA2024032700211](https://openairdocs.org/sdr/HNAA2024032700211), Mar 3, 2024: SUPPORT. CRACKED. E025818 GALLEY LH OMEGA BEAM IS CRACKED ON SIDE WALL AFT OF FRAME 21. ACCOMPLISHED REPAIR ON CRACKED L/H GALLEY OMEGA BEAM SIDE WALL AFT OF FR21 IAW PIEDMONT EO
- [SDR HNAA2024032700210](https://openairdocs.org/sdr/HNAA2024032700210), Mar 3, 2024: DOOR SILL. CORRODED. E025813 CENTER GALLEY SERVICE DOOR SILL IS CORRODED AROUND NUTPLATE HOLES. REPAIRED CENTER GALLEY SERVICE DOOR CUTOUT LOWER SILL AT FWD AND AFT NUTPLATE HOLES I
- [SDR HNAA2024032700209](https://openairdocs.org/sdr/HNAA2024032700209), Mar 3, 2024: SHEAR TIE. CRACKED. E025729 LH SIDE SHEAR CLIP AT STRINGER 15L FRAME 24 IS CRACKED. REMOVED CRACKED SHEAR CLIP AT STRINGER 15L FRAME 24 AND INSTALLED SERVICEABLE LH SIDE SHEAR CLIP
- [SDR HNAA2024032700208](https://openairdocs.org/sdr/HNAA2024032700208), Mar 3, 2024: FLOOR SUPPORT. CORRODED. E025734 RH #2 FLOOR SUPPORT HAS CORROSION. REMOVED CORRODED RH #2 FLOOR SUPPORT AND REPLACED WITH SERVICEABLE RH #2 FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024032700207](https://openairdocs.org/sdr/HNAA2024032700207), Mar 3, 2024: FLOOR SUPPORT. CORRODED. E025732 LH #4 FLOOR SUPPORT HAS CORROSION. REMOVED CORRODED LH #4 FLOOR SUPPORT AND INSTALLED SERVICEABLE FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024032700206](https://openairdocs.org/sdr/HNAA2024032700206), Mar 3, 2024: FLOOR SUPPORT. CORRODED. E025730 LH #2 FLOOR SUPPORT HAS CORROSION. BLENDED CORROSION ON LH #2 FLOOR SUPPORT IAW EMB 145 SRM 51-10-03 REMOVED AND REPLACED WITH SERVICEABLE LH #2 FLOOR S
- [SDR HNAA2024032700198](https://openairdocs.org/sdr/HNAA2024032700198), Mar 3, 2024: CROSSBEAM. CORRODED. E025826 GALLEY LH SIDE CROSSBEAM AT FRAME 18 IS CORRODED. REMOVED CORRODED GALLEY LH SIDE CROSSBEAM AT FR 18 AND REPLACED GALLEY LH SIDE CROSSBEAM AT FR18 IAW E

All 282: https://openairdocs.org/aircraft/N640AE/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/N640AE/stcs.md

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/aircraft.md
- The Allison AE-3007A engine: https://openairdocs.org/engine/allison-ae-3007a.md

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