# N642AE: 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: 145193
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 25, 1999
- Certificate issued: September 9, 2011
- Expires: September 30, 2027
- Mode S code: A86CAE
- 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=642AE
- Page: https://openairdocs.org/aircraft/N642AE

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/N642AE/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 N642AE.

## FAA accident and incident reports

None matched to N642AE.

## Service difficulty reports (253, 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 HNAA2026051500380](https://openairdocs.org/sdr/HNAA2026051500380), May 14, 2026: UPLOCK BOX. ABNORMAL. NOSE GEAR DID NOT RETRACT DURING TAKEOFF. MAIN GEAR WAS GREEN BUT NOSE GEAR WENT RED AND HEARD TRIPLE CHIMEWITH LANDING GEAR DISAGREE. FACT 15MAY26 18:48 ROA R+
- [SDR HNAA2026030400194](https://openairdocs.org/sdr/HNAA2026030400194), Feb 19, 2026: SHEAR TIE. CRACKED. 00738 CRACK FOUND IN SHEAR TIE AT FRAME 24 BETWEEN STR 15L AND 16L. REMOVED AND INSTALLED NEW SHEAR TIE AT FR 24 BETWEEN STR 15L AND 16L. REF EMB 145 SRM 51-40-
- [SDR HNAA2026030400193](https://openairdocs.org/sdr/HNAA2026030400193), Feb 12, 2026: FRAME. DAMAGED. 00705 AFTER REMOVAL OF SILL FROM RH SIDE BETWEEN FR 61 TO FR 64 FOUND ELONGATED HOLE AT FR 62. COMPLIED WITH REPAIR TO FRAME 62 AT STR 16R PER EMB 145 SRM 53-00
- [SDR HNAA2026030400192](https://openairdocs.org/sdr/HNAA2026030400192), Feb 10, 2026: FLOOR SUPPORT. DAMAGED. AFTER REMOVAL OF LH FLOOR SILL AT FR 23 TO FR 29 FOUND ELONGATED HOLE AT FR 24. COMPLIED WITH PERMANENT REPAIR ON FR 24 BETWEEN STR 15L - 16L PER EMB145 SRM 53-
- [SDR HNAA2026030400191](https://openairdocs.org/sdr/HNAA2026030400191), Feb 10, 2026: FLOOR SUPPORT. DAMAGED. 00691 AFTER REMOVAL OF LH SILL FROM FR23 TO FR29 FOUND ELONGATED HOLE AT FR 28. COMPLIED WITH PERMANENT REPAIR ON FR 28 BETWEEN STR 15L - 16L PER EMB 145 SRM 53
- [SDR HNAA2026030400190](https://openairdocs.org/sdr/HNAA2026030400190), Feb 9, 2026: FLOOR SUPPORT. DAMAGED. AFTER REMOVAL OF LH FLOOR SILL FR30-FR35 FOUND 1EA ELONGATED HOLE AND 1EA OVERSIZED HOLE AT FR 31. COMPLIED WITH PERMANENT REPAIR OF FR 31 BETWEEN STR 15L - 16L
- [SDR HNAA2026030400184](https://openairdocs.org/sdr/HNAA2026030400184), Feb 2, 2026: ANGLE. CORRODED. 00491 RH INBD FLAP HAS CORROSION ON LOWER INBOARD TRAILING EDGE ANGLE. REMOVED AND INSTALLED LOWER INBOARD TRAILING EDGE L-ANGLE AND CLOSE OUT PANEL ON RH INBD 
- [SDR HNAA2026030400183](https://openairdocs.org/sdr/HNAA2026030400183), Jan 31, 2026: FLOOR SUPPORT. CORRODED. 00437 MID FLOOR GUSSET FROM FR 45 TO FR 47 HAS CORROSION. REMOVED AND REPLACED CENTER OMEGA BEAM FROM FR 46 - FR 53 (GUSSET P/N 145-30634-011) PER EMB 145 SRM 5
- [SDR HNAA2026030400182](https://openairdocs.org/sdr/HNAA2026030400182), Jan 31, 2026: FLOOR SUPPORT. CORRODED. MID FLOOR GUSSET FROM FR 38 TO FR 45 HAS CORROSION,. REMOVED AND REPLACED WITH NEW FROM STOCK MID FLOOR GUSSET FROM FR 38 TO FR 45 IAW EMB145 SRM 51-40-02-PR. R
- [SDR HNAA2026030400181](https://openairdocs.org/sdr/HNAA2026030400181), Jan 31, 2026: FLOOR SUPPORT. CORRODED. FLOOR SILL FROM FR 35 TO FR 39, LH, HAS CORROSION. REMOVED AND REPLACED FLOOR SILL FROM FR 35 TO FR 39 LH. REF EMB145 SRM 51-40-02.
- [SDR HNAA2026030400189](https://openairdocs.org/sdr/HNAA2026030400189), Jan 30, 2026: BRACKET. CRACKED. 00350 AIR PRESSURE TUBE BRACKET ON OMEGA BEAM IS CRACKED AT FR 30 RH. REMOVED AND REPLACED AIR PRESSURE TUBE BRACKET ON OMEGA BEAM AT FR 30 RH. REF EMB 145 SRM 
- [SDR HNAA2026030400180](https://openairdocs.org/sdr/HNAA2026030400180), Jan 30, 2026: FLOOR SUPPORT. CORRODED. FLOOR SILL FROM FR 36 TO FR 42, RH, HAS CORROSION. REMOVED AND INSTALLED NEW FLOOR SILL FROM FR 36 TO FR 42, RHS. REF EMB 145 SRM 51-40-02 SRM 51-20-01
- [SDR HNAA2026030400179](https://openairdocs.org/sdr/HNAA2026030400179), Jan 30, 2026: FLOOR SUPPORT. CORRODED. MID FLOOR GUSSET FROM FR 36 TO FR 39 HAS CORROSION. REMOVED AND INSTALLED NEW CENTER OMEGA BEAM GUSSET AT FR 36 - FR 39 PER EMB 145 SRM 51-40-02-PR.
- [SDR HNAA2026030400178](https://openairdocs.org/sdr/HNAA2026030400178), Jan 30, 2026: FLOOR SUPPORT. CORRODED. MID FLOOR GUSSET FROM FR 31 TO FR 35 HAS CORROSION. INSTALLED NEW MID FLOOR GUSSET FROM FR29.5 TO FR 35.5 REF EMB 145 SRM 51-40-02, SRM 51-20-0
- [SDR HNAA2026030400177](https://openairdocs.org/sdr/HNAA2026030400177), Jan 30, 2026: FLOOR SUPPORT. CORRODED. FLOOR SILL FROM FR 30 TO FR 35, RH, HAS CORROSION. REMOVED BAD SILL AND INSTALLED NEW FROM STOCK NEW FLOOR SILL FROM FR 30 TO FR 35, RH REF EMB 145 SRM 51-40-02
- [SDR HNAA2026030400176](https://openairdocs.org/sdr/HNAA2026030400176), Jan 30, 2026: FLOOR SUPPORT. CORRODED. 00360 FLOOR SILL AT FR 30 AND FR 35, LH, HAS CORROSION. REMOVED AND REPLACED LT FLOOR SILL AT FR 30 - FR 35 PER EMB 145 SRM 51-40-02-PR.
- [SDR HNAA2026030400175](https://openairdocs.org/sdr/HNAA2026030400175), Jan 30, 2026: FLOOR SPLICE. CORRODED. MID FLOOR GUSSET FROM FR 25 TO FR 27 HAS CORROSION. REMOVED BAD GUSSET AND INSTALLED NEW FROM STOCK MID FLOOR GUSSET FROM FR 24-29, REF EMB145 SRM 51-40-02
- [SDR HNAA2026030400174](https://openairdocs.org/sdr/HNAA2026030400174), Jan 30, 2026: FLOOR SUPPORT. CORRODED. FLOOR SILL FROM FR 25 TO FR 28, RH, HAS CORROSION. REMOVED BAD FLOOR SILL FROM FR 25 TO FR28, RH, AND INSTALLED NEW FROM STOCK FLOOR SILL IAW SRM 51-40-02
- [SDR HNAA2026030400173](https://openairdocs.org/sdr/HNAA2026030400173), Jan 30, 2026: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT FR 27 - 29, LT, CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-PR.
- [SDR HNAA2026030400172](https://openairdocs.org/sdr/HNAA2026030400172), Jan 30, 2026: FLOOR SUPPORT. CORRODED. 00334 1EA FLOOR SUPPORTFROM FR 25 - 29 LT, CORRODED. REMOVED AND REPLACED WITH NEW IAW SRM 51-40-02-PR.
- [SDR HNAA2026030400188](https://openairdocs.org/sdr/HNAA2026030400188), Jan 29, 2026: BRACKET. CRACKED. AFT CARGO FRAME MOUNTING BRACKET AT FR 61 RH, STR 5R, IS CRACKED. REMOVED AND REPLACED AFT CARGO FRAME MOUNTING BRACKET P/N 145-40575-603 AT FR 61 RH STR 5R PER
- [SDR HNAA2026030400171](https://openairdocs.org/sdr/HNAA2026030400171), Jan 29, 2026: GUSSET. CORRODED. SIGNS OF CORROSION ON THE LT GUSSET AT MULTIPLE PLACES FROM FR 52 - 60. REMOVED AND REPLACED WITH NEW IAW SRM 51-40-02-PR.
- [SDR HNAA2026030400170](https://openairdocs.org/sdr/HNAA2026030400170), Jan 29, 2026: FLOORBEAM. CORRODED. FWD WET AREA FLOORBEAM FR 20, HAD CORROSION. REMOVED THE FLOORBEAM AND INSTALLED NEW IAW SRM 51-40-02-PR
- [SDR HNAA2026030400187](https://openairdocs.org/sdr/HNAA2026030400187), Jan 23, 2026: FLOOR SUPPORT. CRACKED. AFT WET AREA OB FLOOR SILL AT FR 60 RH, HAS A CRACK. REMOVED AND REPLACED THE AFT WET AREA 1 EA OUTBD FLOOR SILL AT FR 60 PER EMB 145 SRM 51-40-02-PR.
- [SDR HNAA2026030400169](https://openairdocs.org/sdr/HNAA2026030400169), Jan 23, 2026: FLOOR SUPPORT. CORRODED. FWD WET AREA RT OMEGA BEAM AT FR 23 CORRODED. REMOVED AND REPLACED THE RT OMEGA BEAM, FR 18 - 23 IAW SRM 51-40-02-PR.
- [SDR HNAA2026030400168](https://openairdocs.org/sdr/HNAA2026030400168), Jan 23, 2026: FLOOR SUPPORT. CORRODED. FWD WET AREA FLOOR SUPPORT AFT OF SERVICE DOOR CORRODED. REMOVED AND REPLACED THE AFT FLOOR SUPPORT FROM FR 22 - 23 IAW SRM 51-40-02-PR.
- [SDR HNAA2026030400167](https://openairdocs.org/sdr/HNAA2026030400167), Jan 23, 2026: FLOORBEAM. CORRODED. AFT WET AREA FLOORBEAM, FR 58 CORRODED. INSTALLED A NEW FLOORBEAM IAW SRM 51-40-02, SECTION 3.
- [SDR HNAA2026030400166](https://openairdocs.org/sdr/HNAA2026030400166), Jan 23, 2026: DOOR SILL. CORRODED. CORROSION ON THE MAIN DOOR SILL BTW FR 20 - 22. R & R THE DOOR SILL IAW SRM 51-40-02.
- [SDR HNAA2026030400186](https://openairdocs.org/sdr/HNAA2026030400186), Jan 22, 2026: FRAME. DAMAGED. 00097 AFT CARGO FRAME 64 RH, STR 8R, HAS DAMAGE, COMPLIED WITH PERMANENT REPAIR TO AFT CARGO 1EA FR 64 R/H STR 8R PER ETD 2025-145-002400 REV.:/ AND EO1-53-26-0
- [SDR HNAA2026030400185](https://openairdocs.org/sdr/HNAA2026030400185), Jan 22, 2026: ACCESS PANEL. CRACKED. TAIL CONE / OIL SERVICE ACCESS PANEL / CRACKED ACCESS PANEL AREA / AT HINGE. COMPLIED WITH PERMENANT REPAIR OF THE APU COWLING OIL SERVICE DOOR CUTOUT MOLDING P
- [SDR HNAA2025051900355](https://openairdocs.org/sdr/HNAA2025051900355), May 17, 2025: LIGHT. INOPERATIVE. EMERGENCY LIGHT STRIP AT ROW 15 IS INOP. RAR STRIP IAW AMM33-50-08
- [SDR HNAA2025022400093](https://openairdocs.org/sdr/HNAA2025022400093), Feb 22, 2025: CONTROLLER. DEFECTIVE. ON CLIMB UP UNTIL 8000 FT IN AUTO MODE. A/C DID NOT PRESSURIZE. FACT 22FEB25 03:36 ROA R&R'D DIGITAL CONTROLLER IRW AMM 21-31-01 DUE TO CODE A016 ON DIGITAL CON
- [SDR HNAA2025021000080](https://openairdocs.org/sdr/HNAA2025021000080), Feb 9, 2025: LIGHT. FAULTED. ON CLIMB AROUND 10,000 FT FA EMERGENCY LIGHTS CAME ON AND STAYED ON. OPERATIONALLY CHECKED THE EMERGENCY LIGHTING SYSTEM IAW WC 33-70-17. NO DEFECT FOUND. EMS L
- [SDR HNAA2024122601260](https://openairdocs.org/sdr/HNAA2024122601260), Dec 25, 2024: SENSOR. FAULTED. TANK 2 & TOTAL FUEL INDICATION NOT SHOWING. MEL 24DEC24 10:05 CLT B35905 28-9 WING TANK FUEL QTY INDC EICAS MFE FACT 28DEC24 06:31 SBY T/S FUEL INDICATION ISSUE
- [SDR HNAA2024052300472](https://openairdocs.org/sdr/HNAA2024052300472), May 22, 2024: CONTROL PANEL. MALFUNCTIONED. AT 18K ALTITUDE, CABIN ALTITUDE CLIMBED TO 10K FEET. MEL APPLIED. PRESS CONTROL AUTO AND MANUAL FACT 23MAY24 04:15 ALB T/S IRW EMB-145 FIM 21-31-00-810-805-A, B
- [SDR HNAA2023112200453](https://openairdocs.org/sdr/HNAA2023112200453), Nov 21, 2023: UNKNOWN. UNKNOWN. PRESSURIZATION AUTOMATIC MODE FAILURE AT 13,000 FT CABIN ALT PRESENTED RED HISTORY: YES MEL 21NOV23 10:06 MDT C32507 21-12-3 PRESS CONTROL AUTO AND MANUAL. TROU
- [SDR HNAA2023091800325](https://openairdocs.org/sdr/HNAA2023091800325), Aug 28, 2023: UNKNOWN. UNKNOWN. E993888 SHEAR CLIP CRACKED AT FR 8 BTW STGR 9L AND WINDSHIELD LOWER FRAME. ACCOMPLISHED REPAIR OF FR 8 STGR 9L TO LOWER WINDSHIELD FRAME SHEAR CLIP IAW ETD# ETD
- [SDR HNAA2023091800324](https://openairdocs.org/sdr/HNAA2023091800324), Aug 23, 2023: UNKNOWN. UNKNOWN. E992717 RH WING UPPER WING TIP ATTACHMENT FLANGE HAS AN ELONGATED NUTPLATE HOLE. : RAR R/H WING UPPER WING TIP RIB IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2023091800341](https://openairdocs.org/sdr/HNAA2023091800341), Aug 22, 2023: UNKNOWN. UNKNOWN. E992227 CABIN L/H #4 FLOORBOARD SUPPORT HAS CORROSION. : REMOVED AND REPLACED CABIN L/H #4 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2023091800344](https://openairdocs.org/sdr/HNAA2023091800344), Aug 21, 2023: UNKNOWN. UNKNOWN. E992242 L/H FLOOR BEAM HAS CORROSION BETWEEN FRAMES 36 AND 39. RAR L/H FLOOR BEAM GUSSET BETWEEN FRAMES 36 AND 39 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2023091800343](https://openairdocs.org/sdr/HNAA2023091800343), Aug 21, 2023: UNKNOWN. UNKNOWN. E992234 CABIN L/H FLOOR BEAM BETWEEN FRAME 29 AND 31 HAS CORROSION. REMOVED AND REPLACED GUSSET ON CABIN L/H FLOOR BEAM BETWEEN FRAME 29 AND 31 IAW EMB 145 SRM 
- [SDR HNAA2023091800342](https://openairdocs.org/sdr/HNAA2023091800342), Aug 21, 2023: UNKNOWN. UNKNOWN. E992228 CABIN R/H #3 FLOORBOARD SUPPORT HAS CORROSION. RAR R/H #3 CABIN FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02
- [SDR HNAA2023091800340](https://openairdocs.org/sdr/HNAA2023091800340), Aug 21, 2023: UNKNOWN. UNKNOWN. E992226 CABIN L/H #3 FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED CABIN L/H #3 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02
- [SDR HNAA2023091800339](https://openairdocs.org/sdr/HNAA2023091800339), Aug 21, 2023: UNKNOWN. UNKNOWN. E992224 CABIN R/H #2 FLOORBOARD SUPPORT HAS CORROSION. : RAR R/H #2 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2023091800338](https://openairdocs.org/sdr/HNAA2023091800338), Aug 20, 2023: UNKNOWN. UNKNOWN. E992217 CABIN L/H #2 FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED CABIN L/H #2 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2023091800337](https://openairdocs.org/sdr/HNAA2023091800337), Aug 20, 2023: UNKNOWN. UNKNOWN. E992197 R/H #5 FLOORBOARD SUPPORT HAS CORROSION. : REMOVED AND INSTALLED NEW R/H #5 FLOORBOARD SUPPORT IAW EMB 145 SRM51-40-02
- [SDR HNAA2023091800336](https://openairdocs.org/sdr/HNAA2023091800336), Aug 20, 2023: UNKNOWN. UNKNOWN. E991959 AFT FLOOR BOARD SUPPORT AT PAX DOOR ENTRENCE HAS CORROSION. RAR AFT FLOOR BOARD SUPPORT AT PAX DOOR ENTRENCE IAW EMB 145 SRM 51-40-02
- [SDR HNAA2023091800335](https://openairdocs.org/sdr/HNAA2023091800335), Aug 20, 2023: UNKNOWN. UNKNOWN. E991951 GALLEY TRIANGLE GUSSET AT WARDROBE AREA HAS CORROSION. : REMOVED AND REPLACED GALLEY TRIANGLE GUSSET AT WARDROBE AREA IAW EMB145 SRM 51-40-02.
- [SDR HNAA2023091800334](https://openairdocs.org/sdr/HNAA2023091800334), Aug 20, 2023: UNKNOWN. UNKNOWN. E992002 RUDDER 2 LIGHTNING HOLE AT UPPER CONTROL ROD ATTACH POINT CRACKED. REMOVED AND REPLACED RIB ON RUDDER 2 AT LIGHTNING HOLE AT UPPER CONTROL ROD ATTACH PO
- [SDR HNAA2023091800333](https://openairdocs.org/sdr/HNAA2023091800333), Aug 20, 2023: UNKNOWN. UNKNOWN. E992000 RUDDER 2 UPPER HINGE FITTING ELONGATED AT HAT BUSHING. REMOVED AND INSTALLED SERVICEABLE RUDDER 2 UPPER HINGE FITTING IAW EMB145 SRM 55-40-02

All 253: https://openairdocs.org/aircraft/N642AE/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/N642AE/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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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.
