# N643AE: 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: 145200
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 12, 1999
- Certificate issued: September 26, 2011
- Expires: September 30, 2027
- Mode S code: A87065
- 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=643AE
- Page: https://openairdocs.org/aircraft/N643AE

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/N643AE/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 N643AE.

## FAA accident and incident reports

None matched to N643AE.

## Service difficulty reports (147, 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 HNAA2024051400380](https://openairdocs.org/sdr/HNAA2024051400380), Apr 14, 2024: SHEAR TIE. CRACKED. E032512 SHEAR CLIP AT FR.67 BETWEEN STGR. 6L-7L IS CRACKED. RAR SHEAR CLIP AT FR67 BETWEEN STGR 6L-7L IAW EMB 145 SRM 51-40-02
- [SDR HNAA2023060600184](https://openairdocs.org/sdr/HNAA2023060600184), Jun 5, 2023: UNKNOWN. UNKNOWN. RANDOMLY THROUGHOUT FLIGHT LOST COMBINATIONS OF BOTH PACK AND BLEED SYSTEMS. AIR CONDITIONING PACK. R&R UPPER SLEEVE AT DUAL TEMPERATURE CONTROL VALVE ON PACK 2
- [SDR HNAA2023060100181](https://openairdocs.org/sdr/HNAA2023060100181), May 31, 2023: UNKNOWN. UNKNOWN. ABORTED TAKEOFF DUE TO NO. 2 BLEED VALVE FAIL MESSAGE. CAPTAIN REPORTS MESSAGE COMES ON AT IDLE AND GOES AWAY INTERMITTENTLY. R & R #2 DAU IAW AMM 31-41-01. OPS
- [SDR HNAA2023052300177](https://openairdocs.org/sdr/HNAA2023052300177), May 22, 2023: UNKNOWN. UNKNOWN. CABIN ALTITUDE ROSE RAPIDLY AT CRUISE (FLIGHT LEVEL 240) ECEEDED 10000 THEN DURING DECENT IT REACHED AS HIGH AS 12000 CABIN ALTITUDE HISTORY: NONE FACT 22MAY23 
- [SDR HNAA2023051800161](https://openairdocs.org/sdr/HNAA2023051800161), May 17, 2023: UNKNOWN. UNKNOWN. E1 FIRE DETECT FAIL DISPLAYED ON EICAS DURING T/O ROLL FOLLOWED BY NO T/O CONFIG EICAS. OPENED E1 LOWER COWLING PER AMM 71 12 01. INSPECTED CP P0914/P0915. FOUN
- [SDR HNAA2023013000024](https://openairdocs.org/sdr/HNAA2023013000024), Jan 28, 2023: WARNING MESSAGE. FALSE ACTIVATION. DURING T/O ROLL TAT HEAT 1 INOP DISPLAYED ON EICAS. REJECTED T/O AT 80 KTS. TROUBLESHOT WITH FIM 30-33-00-810-801-A FOUND TO BE TRANSITORY. PERFORMED TAT HEAT O
- [SDR HNAA2022122700319](https://openairdocs.org/sdr/HNAA2022122700319), Dec 22, 2022: WARNING MESSAGE. ILLUMINATED. PACK 2 OVRHT MSG DISPLAYED FOLLOWED BY SLIGHT BURNING SMELL. SMELL IMMEDIATELY DISSIPATED. CHECKED #2 A/C PACK IRT AMM 21-51-14-NO DISCREPANCIES FOUND.PACK OPS 
- [SDR HNAA2022062000225](https://openairdocs.org/sdr/HNAA2022062000225), Jun 17, 2022: HEAT EXCHANGER. CRACKED. STRONG SMOKE SMELL IN AIRCRAFT. CHECKED FOR SIGNS OF SMOKE. NO DEFECTS NOTED AT THIS TIME. FOUND CRACKED HEAT EXCHANGER. R&R'S #200 HEAT EXCHANGER IAW AMM 21-51
- [SDR HNAA2021122000602](https://openairdocs.org/sdr/HNAA2021122000602), Dec 18, 2021: NONE. NONE. NDIS 643 30-00 0030750 18DEC21 ROC ASSGN CAPT REPORTED RTO DUE TO ICE COND A/I INOP MSG BELOW 25KTS. ADVISED CREW OF NORMAL OPERATION AND TO PERFORM PNEUMATIC C
- [SDR HNAA2021063000297](https://openairdocs.org/sdr/HNAA2021063000297), Jun 28, 2021: EICAS. FAULT MESSAGE. A/C REJECTED TAKE OFF DUE TO DAU 2A FAIL. MESSAGE SELF CLEARED WITHIN 10 SECONDS. ADVISED CREW TO CYCLE REVERSIONARY SG PUSHBUTTONS AND CYCLE IC-600 CIRCUIT BRE
- [SDR HNAA2021062100265](https://openairdocs.org/sdr/HNAA2021062100265), Jun 18, 2021: ENGINE. ODOR. BURNING OIL SMELL IN COCKPIT ALSO CAUSING EYE IRRITATION. REMOVED AND REPLACE #1 ENGINE. OP CK AND LEAK CHECKS GOOD.
- [SDR HNAA2021030800093](https://openairdocs.org/sdr/HNAA2021030800093), Mar 7, 2021: UNKNOWN. ODOR. PDIS 643 21-51 2409671 07MAR21 CLT CLOSE FOUL SMELL FROM BLEED SYSTEM FACT 07MAR21 12:35 CLT TROUBLE SHOT SMELL IN BLEEDS IN REF TO FIM 21-20-00-810-801-A FOUND
- [SDR HNAA2020111600327](https://openairdocs.org/sdr/HNAA2020111600327), Nov 13, 2020: CONTROL UNIT. FAILED. PDIS 643 27-52 2165021 13NOV20 CLT. CLOSE FLAP FAIL ON ARRIVAL. LANDED WITH FLAPS AT ZERO. FACT 13NOV20 14:35 CLT. INSPECTED NR 1 AND NR 2 FLAPS. NO DEFECTS NOT
- [SDR HNAA2020100800284](https://openairdocs.org/sdr/HNAA2020100800284), Oct 7, 2020: DOOR FRAME. CHAFED. CARGO DOOR WEB FRAME HAS 4 CHAFES, MARKED. COMPLETE: SMOOTHED CHAFES (4 EACH) ON CARGO DOOR WEB FRAME, IAW EMB 145 SRM 51-10-03. 2 EA FOUND TO BE WITHIN ALLOWAB
- [SDR HNAA2020100800283](https://openairdocs.org/sdr/HNAA2020100800283), Oct 7, 2020: SKIN. CRACKED. INVESTIGATE POSSIBLE SKIN CRACKS AT FR 79 BETWEEN STGRS 03R/08R (4EA), MARKED. PERFORMED PT INSPECTION, IAW EASI NDTM. SKIN FOUND CRACKED AT 1 FASTENER ON FR 79
- [SDR HNAA2020100800282](https://openairdocs.org/sdr/HNAA2020100800282), Oct 7, 2020: SKIN. CRACKED. INVESTIGATE POSSIBLE SKIN CRACKS AT FR 78 BETWEEN STGRS 03R/07R (2EA), MARKED. COMPLETE: REPAIRED SKIN CRACK AT FR 78 BETWEEN STGRS 06R/07R, IAW PIEDMONT EO1-53
- [SDR HNAA2020100800281](https://openairdocs.org/sdr/HNAA2020100800281), Oct 7, 2020: SKIN. CRACKED. INVESTIGATE POSSIBLE SKIN CRACKS AT FR 77 BETWEEN STGRS 04R/07R 7EA, MARKED. PERFORMED PT INSPECTION, IAW EASI NDTM SKIN FOUND CRACKED AT 3 FASTENERS ON FR 77 B
- [SDR HNAA2020100800280](https://openairdocs.org/sdr/HNAA2020100800280), Oct 7, 2020: SKIN. CRACKED. INVESTIGATE POSSIBLE SKIN CRACKS AT FR 79 BETWEEN STGRS 03L-05L 2EA, MARKED. PERFORMED PT INSPECTION, IAW EASI NDTM SKIN FOUND CRACKED AT 2 FASTENERS ON FR 79 B
- [SDR HNAA2020100800279](https://openairdocs.org/sdr/HNAA2020100800279), Oct 7, 2020: YOKE. CRACKED. LT PYLON FWD UPPER ENGINE YOKE HAS EVIDENCE OF CRACK. COMPLETE: INSTALLED SERVICEABLE LT UPPER FORWARD YOKE FITTING AND GUSSET PLATE, IAW ETD2020-145-026985 REV
- [SDR HNAA2020100800278](https://openairdocs.org/sdr/HNAA2020100800278), Oct 7, 2020: YOKE. CRACKED. LT PYLON FWD LOWER ENGINE YOKE IS CRACKED. COMPLETE: INSTALLED SERVICEABLE LT LOWER FORWARD YOKE FITTING AND GUSSET PLATE, IAW ETD2020-145-026985 REV A AND EO1-
- [SDR HNAA2020100800277](https://openairdocs.org/sdr/HNAA2020100800277), Oct 7, 2020: SKIN. CRACKED. BAGGAGE DOOR EXTERIOR SKIN HAS A CRACK AT THE AFT END OF THE OPEN/CLOSE HANDLE. COMPLETE: ACCOMPLISHED REPAIR OF CRACK ON BAGGAGE DOOR EXTERIOR SKIN AT AFT END 
- [SDR HNAA2020100800276](https://openairdocs.org/sdr/HNAA2020100800276), Oct 7, 2020: SKIN. CRACKED. INVESTIGATE POSSIBLE SKIN CRACKS AT FR 79 BETWEEN STGRS 03L-05L 2EA, MARKED. PERFORMED PT INSPECTION, IAW EASI NDTM SKIN FOUND CRACKED AT 2 FASTENERS ON FR 79 B
- [SDR HNAA2020100800275](https://openairdocs.org/sdr/HNAA2020100800275), Oct 7, 2020: HOUSING. CRACKED. CARGO DOOR HANDLE CUTOUT INTERIOR BUCKET IS CRACKED. REMOVED AND REPLACED THE CARGO DOOR HANDLE CUTOUT INTERIOR BUCKET, IAW EMB145 SRM 51-40-02 AND PIEDMONT EO-
- [SDR HNAA2019102800324](https://openairdocs.org/sdr/HNAA2019102800324), Oct 25, 2019: INVERTER. INOPERATIVE. NDIS 643 33-50 0015130 25OCT19 SBY CLOSE EMERGENCY EXIT SIGN ABOVE F/A SEAT DOES NOT ILLUMINA TE 33384 00 BAD FACT 25OCT19 12:08 SBY TROUBLESHOT IAW FIM TASK 33
- [SDR HNAA2018101700258](https://openairdocs.org/sdr/HNAA2018101700258), Oct 13, 2018: UNKNOWN. ODOR. PDIS 643 05-50 1612811 13OCT18 CLT CLOSE STRONG RUBBER ODOR DURING TAKEOFF AND AT GATE. 25437 00 DS HISTORY: FACT 13OCT18 09:45 CLT RAN AIRCRAFT, NO ODORS DETEC
- [SDR HNAA2018071200169](https://openairdocs.org/sdr/HNAA2018071200169), Jul 23, 2018: SHUTOFF VALVE. MALFUNCTIONED. ON CLIMBOUT BLEED 1 VLV CLOSED EICAS MESSAGE. RAN QRH MSG PERSISTED. ON DESCENT MESSAGE EXTINGUISHED. R&R PRSOV IAW AMM 36-11-05. OPS CHECK GOOD AT THIS TIME. O
- [SDR HNAA2018030800054](https://openairdocs.org/sdr/HNAA2018030800054), Mar 6, 2018: RELAY. DAMAGED. INSPECTED RELAYS K1237 AND K0058 IAW FCD1-30-16-0276, FOUND EVIDENCE OF HEAT DAMAGE. R & R THE RELAYS IAW AMM 20-13-02-0001, OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR SIMA20180222001](https://openairdocs.org/sdr/SIMA20180222001), Feb 22, 2018: STRUCTURE. CRACKED. RIGHT HAND CENTER ATTACHMENT POINT FOR COCKPIT FLOORBOARD 221GF, CRACKED AT FLOOR STRUCTURE DOUBLER. COMPLIED WITH ERS-EM-5300-3154.
- [SDR SIMA20180221002](https://openairdocs.org/sdr/SIMA20180221002), Feb 21, 2018: FRAME. GOUGED. CARGO FRAME 70 IS GOUGED AT STRINGER 12R. COMPLIED WITH ERS-EM-53MR-3149.
- [SDR SIMA20180217004](https://openairdocs.org/sdr/SIMA20180217004), Feb 17, 2018: BUSHING. MIGRATED. RIGHT AILERON OUTBOARD HINGE FITTING, INBOARD BUSHING MIGRATED. REMOVED AND REPLACED THE RT AILERON OTBD FITTING IAW EO EM-27MR-112.
- [SDR SIMA20180213001](https://openairdocs.org/sdr/SIMA20180213001), Feb 13, 2018: DOOR SILL. CORRODED. CARGO DOOR SILL HAS SPOTS OF CORROSION. INSTALLED A NEW CARGO DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA20180207006](https://openairdocs.org/sdr/SIMA20180207006), Feb 7, 2018: FRAME. CRACKED. FRAME 66 IS CRACKED ON THE TOP FLANGE BETWEEN STRINGERS 18 AND 19L. REPAIRED THE FRAME IAW SRM 53-00-04.
- [SDR SIMA20180207003](https://openairdocs.org/sdr/SIMA20180207003), Feb 7, 2018: SHEAR TIE. CRACKED. SHEAR TIE AT FRAME 65 BETWEEN STRINGERS 18L AND 19L WAS CRACKED. REMOVED AND REPLACED THE SHEAR TIE AW SRM 51-40-02.
- [SDR SIMA20180206008](https://openairdocs.org/sdr/SIMA20180206008), Feb 6, 2018: TRUNNION. CRACKED. RIGHT MLG AFT UPPER TRUNNION IS CRACKED. REPLACED THE TRUNNNION IAW ERS-EM-57MR-916.
- [SDR SIMA20180206009](https://openairdocs.org/sdr/SIMA20180206009), Feb 6, 2018: TRUNNION. CRACKED. LEFT MLG AFT TRUNNION HAS AN APPROXIMATELY 1.5 INCH CRACK ON THE OTBD RADIUS. REPLACED THE LT MLG AFT TRUNNION IAW WER-EM-57MR-917.
- [SDR SIMA20180206007](https://openairdocs.org/sdr/SIMA20180206007), Feb 6, 2018: FRAME. CRACKED. FRAME 67 IS CRACKED ON TOP FLANGE BETWEEN STRINGERS 18 AND 19L. INSTALLED A NEW FRAME SECTION AND SPLICE IAW SRM 53-00-04, AND 51-40-02.
- [SDR SIMA20180205008](https://openairdocs.org/sdr/SIMA20180205008), Feb 5, 2018: BRACKET. DAMAGED. CARGO FLOOR SUPPORT BRACKETS AT FRAMES 66 AND 67 BENT AND CRACKED. INSTALLED A NEW FLOOR SUPPORT BRACKET IAW SRM 51-40-02.
- [SDR SIMA20180205006](https://openairdocs.org/sdr/SIMA20180205006), Feb 5, 2018: FRAME. CRACKED. PILOTS SIDE FRAME 10LT. IS CRACKED APPROX. 1/2" BELOW DV WINDOW SILL. INSTALLED NEW FRAME SEGMENT BELOW THE DV WINDOW IAW SRM 51-40-02.
- [SDR SIMA20180205007](https://openairdocs.org/sdr/SIMA20180205007), Feb 5, 2018: FRAME. CRACKED. FIRST OFFICER`S SIDE FRAME 10 LT. IS CRACKED APPROXIMATELY 1 INCH BELOW THE DV WINDOW SILL. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.
- [SDR SIMA20180205005](https://openairdocs.org/sdr/SIMA20180205005), Feb 5, 2018: SUPPORT. CRACKED. CARGO DOOR TORSION BAR SUPPORT AT FRAME 61 RT. IS CRACKED APPROXIMATELY .250. REMOVED AND REPLACED CARGO DOOR TORSION BAR SUPPORT IAW SRM 51-40-02.
- [SDR SIMA20171121002](https://openairdocs.org/sdr/SIMA20171121002), Nov 21, 2017: BULB. INOPERATIVE. FWD LT OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-10. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.
- [SDR SIMA20170713001](https://openairdocs.org/sdr/SIMA20170713001), Jul 13, 2017: CONNECTOR. LOOSE. LEFT INBOARD BRAKE INDICATOR IS HOT, BRAKE OVERHEAT ON EICAS. PERFORMED GVI OF MLG OF OVERHEAT CONDITION. NO DEFECTS NOTED. FOUND NR 2 BRAKE TEMP SENSOR CONNECT
- [SDR SIMA20170711001](https://openairdocs.org/sdr/SIMA20170711001), Jul 11, 2017: BRAKE. DAMAGED. NR 2 BRAKE FAILED. NR 1 TIRE DAMAGED AND BRAKE NR 1 DAMAGE DUE TO HYD CONTAMINATION AND FOD FROM TIRE AND BRAKE NR 2. REMOVED AND REPLACED NR 1 TIRE IAW W/C 32-
- [SDR SIMA20161222001](https://openairdocs.org/sdr/SIMA20161222001), Dec 22, 2016: FLASHLIGHT. INOPERATIVE. F/A FWD EMERG FLASHLIGHT INOP. R&R F/A FWD EMERGENCY FLASHLIGHT IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS GOOD.
- [SDR SIMA20161020001](https://openairdocs.org/sdr/SIMA20161020001), Oct 20, 2016: ACM. DAMAGED. ON CLIMBOUT PASSING 5000' SMELLED BRIEF BURNING ODOR FOR A FEW MINUTES. ALSO FA REPORTED PASSENGER IN 18A SMELLED BRIEF BURNING ODOR. APU OFF, ENG BLEEDS ON PAC
- [SDR SIMA20160820001](https://openairdocs.org/sdr/SIMA20160820001), Aug 20, 2016: LIGHT. INOPERATIVE. LEFT OVERWING FORWARD EMERGENCY LIGHT INOPERATIVE. R & R LT FORWARD EMERGENCY LIGHT ASSY. OPS CHECK GOOD IAW AMM 33-50-10.
- [SDR SIMA20160710005](https://openairdocs.org/sdr/SIMA20160710005), Jul 10, 2016: CONTROL MODULE. INOPERATIVE. CABIN OVERHEAD LIGHTS OUT AGAIN WITH STRONG ELECTRICAL ODOR IN CABIN. REMOVED AND REPLACED CONTROL MODULE ASSY FOR PAX CABIN LIGHTS IAW 145 33-21-01 OPS CHECKED
- [SDR SIMA20160629002](https://openairdocs.org/sdr/SIMA20160629002), Jun 29, 2016: DOOR SEAL. DAMAGED. THE F/A REPORTS A HUMMING NOISE COMING FROM THE MAIN CABIN DOOR DURING CLIMB. SOUND WENT AWAY WHEN LEVEL AT FL200. TRANSFERRED TO NRWC 643-ORD-02682. REPAIRED M
- [SDR SIMA20160618006](https://openairdocs.org/sdr/SIMA20160618006), Jun 18, 2016: SKIN. DENTED. TRANSFERRED FROM AML PAGE 3974409 ITEM 3, REF LOG PAGE 3974408, ITEM NR 1 FOUND DENT ON THE RT SIDE FUSELAGE FRAME 21-22, STR 18R-19R APPROXIMATELY 2.5" X 2.5",
- [SDR SIMA20160618004](https://openairdocs.org/sdr/SIMA20160618004), Jun 18, 2016: SKIN. DAMAGED. TRANSFERRED FROM AML PAGE 3974409, ITEM 2, REF LOG PAGE 3974408, ITEM NR 1 FOUND DAMAGE TO THE RT FUSELAGE AT STR 20R APPROXIMATELY 3.5" X 3" FRAME 20-21. DAMAG

All 147: https://openairdocs.org/aircraft/N643AE/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/N643AE/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

---
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.