# N631AE: 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: 145139
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 19, 1999
- Certificate issued: September 9, 2011
- Expires: September 30, 2027
- Mode S code: A84178
- 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=631AE
- Page: https://openairdocs.org/aircraft/N631AE

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/N631AE/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 N631AE.

## 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 20031019031799I](https://openairdocs.org/incident/20031019031799I), Oct 19, 2003: Emb EMB145LR (N631AE), Rochester, NY. (-23) On October 19, 2003, an Emb-145, N631AE, flt. 4223, departed Rochester airport, Rochester, NY. The crew reported a #1 bleed leak message on eicas during…

## Service difficulty reports (132, 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 HNAA2022053100217](https://openairdocs.org/sdr/HNAA2022053100217), Mar 25, 2022: NONE. NONE. REPORTED LIGHTING STRIKE TO AIRCRAFT REF LG PG 270905-2 C/W LIGHTING STRIKE INSPECTION W/C 05-20-00 AT THIS RON. CW W/C 05-20-00 SEE WORKCARD FOR DETAILS NOTE: 
- [SDR HNAA2021060100229](https://openairdocs.org/sdr/HNAA2021060100229), May 28, 2021: UNKNOWN. ODOR. ELECTRICAL SMELL IN CRUISE AND DESENT IN RAIN WITH W/S HEAT ON. OPS CHECKED W/S HEAT SYSTEM,WINDSHIELD WIPER SYSTEM, AND RAN APU AND PACKS PER AMM 20-42-00 AMM 
- [SDR HNAA2021050600196](https://openairdocs.org/sdr/HNAA2021050600196), May 5, 2021: UNKNOWN. ODOR. ABNORMAL SMELL AFTER TAKEOFF WITH PACK AND BLEED ON. R&R'D RECIRC FAN REF 21-24-011,OPS CHECK GOOD. R&R'D 3100 MUFFLER DUCT REF AMM21-24-02.CHANGED ALL 3 HEPA F
- [SDR HNAA2021041200134](https://openairdocs.org/sdr/HNAA2021041200134), Apr 8, 2021: ECS. ODOR. PDIS 631 21-01 2533072 08APR21 ROA CLOSE AFTER TAKE OFF UPTO 6000FT WITH BOTH BLEEDS ON BURNT BAGEL SMELL IN COCKPIT. SMELL REAPPEARED ON SHORT FINAL FACT 08APR
- [SDR HNAA2021021500053](https://openairdocs.org/sdr/HNAA2021021500053), Feb 13, 2021: LOCALIZER. ERRATIC. PDIS 631 34-32 2353451 13FEB21 MDT CLOSE LOCALIZER ERRATIC 12 MILES FROM CHO. GOT WORSE THE CLOSER TO RUNWAY 3. AUTO PILOT COUPLED TO CAPTS SIDE AND ISSUE PERSI
- [SDR HNAA2020122100375](https://openairdocs.org/sdr/HNAA2020122100375), Dec 20, 2020: UNKNOWN. ODOR. ONCE REACHING CRUISE CAPT NOTICED A BURNING SMELL FOR APPROXIMATELY 3 SECONDS, THEN DISSIPATED. ON ARRIVAL SMELL CAME BACK FOR APPROXIMATELY 10 SECONDS, THEN DI
- [SDR HNAA2020080200237](https://openairdocs.org/sdr/HNAA2020080200237), Jul 29, 2020: UNKNOWN. ODOR. HEAVY BURNING RUBBER ODOR IN FLT DECK DURING TAKE-OFF. ABORTED T/O. MAINTENANCE: PILOTS TAXIED TO RUNWAY 24 ROA AND REJECTED T/O AT 100 KTS. NO UNUSAUL SMELLS, 
- [SDR HNAA2020070900190](https://openairdocs.org/sdr/HNAA2020070900190), Jun 4, 2020: INVERTER. INOPERATIVE. DURING RON FOUND FLOOR LIGHTS AT ROW 7 TO 12 ARE INOP. RR NR 5 EMERGENCY LIGHT POWER INVERTER IAW 33-50-01. THIS SUPERSEDES PREVIOUS SDR REPORT. THE PREVIOUS SD
- [SDR HNAA2020021800068](https://openairdocs.org/sdr/HNAA2020021800068), Feb 17, 2020: UNKNOWN. UNKNOWN. PDIS 631 27-11 2232271 17FEB20 MDT CLOSE ABOVE 250KNOTS A/C HAD SIGNIFICANT RIGHT ROLLING TENDENCY ALONG WITH MINIMAL ARTIFCIAL AILERON FEEDBACK. SLIGHT BANK IN
- [SDR HNAA2019072900202](https://openairdocs.org/sdr/HNAA2019072900202), Jul 26, 2019: INDICATOR. DEFECTIVE. STAND-BY ATTITUDE INDICATOR NOT ERECT IN FLIGHT. FIX: R&RD STAND-BY ATTITUDE INDICATOR REF AMM 34-24-01. OPS CHECK GOOD IAW AMM 34-24-00. OK FOR SERVICE. NOTE: 
- [SDR HNAA2019062400180](https://openairdocs.org/sdr/HNAA2019062400180), Jun 23, 2019: BULB. BURNED OUT. CEILING EMERGENCY LIGHT AT ROW 12 DOES NOT ILLUMINATE. R & R THE CEILING EMERGENCY LIGHT BULB. OPS CHECKED GOOD.
- [SDR HNAA2019062000177](https://openairdocs.org/sdr/HNAA2019062000177), Jun 19, 2019: BULB. INOPERATIVE. RH AFT EXTERIOR EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE.... FIX: R&R D RH AFT EMERGENCY LIGHT,OPS CHCK GOOD IAW AMM TASK 33-50-10-000/400-801-A
- [SDR HNAA2019061900175](https://openairdocs.org/sdr/HNAA2019061900175), Jun 17, 2019: ACTUATOR. FAILED. NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. CYCLED PER QRH, NO CHANGE. RTF. INSPECTED CONNECTORS. NO DEFECTS NOTED. R & R THE NLG UNLOCK ACTUATOR IAW AMM 32-33-0
- [SDR HNAA2019042400118](https://openairdocs.org/sdr/HNAA2019042400118), Apr 23, 2019: LAMP. INOPERATIVE. NDIS 631 33-51 0014870 23APR19 RIC CLOSE EMERGENCY LIGHT IN 12BC PSU INOP 27751 00 NGR FACT 23APR19 09:56 RIC R/R LIGHT LAMP IN PSU OVER SEATS 12BC IAW AMM 33-5
- [SDR HNAA2019021500046](https://openairdocs.org/sdr/HNAA2019021500046), Feb 14, 2019: WARNING MESSAGE. ILLUMINATED. PDIS 631 30-10 1867981 14FEB19 PHL ASSGN DURING A/I TEST IN FLIGHT, STAB A/I FAIL MSG APPEARED ON EICAS.
- [SDR HNAA2019021500045](https://openairdocs.org/sdr/HNAA2019021500045), Feb 13, 2019: RELAY. FAILED. PDIS 631 30-10 1867972 13FEB19 PHL CLOSE STAB A/ICE FAIL MESSAGE APPEARED ON EICAS. RAN QRH B ROUGHT POWER LEVER UP INDICATION REMAINED ON. FACT 13FEB19 18:06 P
- [SDR HNAA201902112041](https://openairdocs.org/sdr/HNAA201902112041), Feb 11, 2019: ANTI-ICE VALVE. FAILED. PDIS 631 30-10 1867951 11FEB19 ALB CLOSE STAB ANTI ICE FAIL EICAS MESSAGE APPEARED DURING ANTI ICE PNEUMATIC TEST IN FLIGHT. FACT 11FEB19 02:59 ALB REMOVED AND 
- [SDR HNAA2017080200260](https://openairdocs.org/sdr/HNAA2017080200260), Aug 2, 2017: RELAY. MALFUNCTIONED. SPOILER FAIL EICAS MESSAGE DISPLAYED AFTER RETRACTION. EXTINGUISHED DURING TAXI. PERFORMED SPOILER OPS CHECK. NO DEFECTS NOTED. R & R THE RELAYS K0030 AND K0031
- [SDR SIMA20170703002](https://openairdocs.org/sdr/SIMA20170703002), Jul 3, 2017: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM IS CORRODED ON BOTTOM SIDE BELOW FRAME 59 CROSSMEMBER. ACCOMPLISHED A REPAIR IAW ERS.
- [SDR SIMA20170703001](https://openairdocs.org/sdr/SIMA20170703001), Jul 3, 2017: SKIN. DENTED. SKIN DENTED AFT OF FRAME 23 BETWEEN STRINGERS 9 - 10R. ACCOMPLISHED A REPAIR IAW ERS-EM-53MR-2796.
- [SDR SIMA20170623004](https://openairdocs.org/sdr/SIMA20170623004), Jun 23, 2017: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM IS CORRODED ON BOTTOM SIDE BELOW FRAME 59 CROSSMEMBER. ACCOMPLISHED A REPAIR IAW ERS-EM-53MR-2786.
- [SDR SIMA20170622001](https://openairdocs.org/sdr/SIMA20170622001), Jun 22, 2017: FLOOR SUPPORT. CORRODED. CENTER OMEGA BEAM IS CHAFED AND CORRODED BETWEEN FRAMES 26-59 ON SIDE WEB. ACCOMPLISHED A REPAIR IAW ERS-EM-53MR-2788.
- [SDR SIMA20170617005](https://openairdocs.org/sdr/SIMA20170617005), Jun 17, 2017: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM IS CORRODED AT FRAME 38. ACCOMPLISHED A REPAIR IAW SRM 53-00-10.
- [SDR SIMA20170617003](https://openairdocs.org/sdr/SIMA20170617003), Jun 17, 2017: FLOOR SUPPORT. CORRODED. CENTER OMEGA BEAM IS CORRODED BETWEEN FRAMES 58-59. ACCOMPLISHED A REPAIR IAW ERS-EM-53MR-2784.
- [SDR SIMA20170617004](https://openairdocs.org/sdr/SIMA20170617004), Jun 17, 2017: FLOOR SUPPORT. CORRODED. CENTER OMEGA BEAM IS CORRODED AT FRAME 38. ACCOMPLISHED A REPAIR IAW SRM 53-00-10.
- [SDR SIMA20170616011](https://openairdocs.org/sdr/SIMA20170616011), Jun 16, 2017: SHEAR TIE. CORRODED. CARGO DOOR CUTOUT LATERAL L-SHAPE IS CORRODED AT PREVIOUSLY BLENDED AREA AT LWR CORNER OF CUTOUT. REPAIRED IAW SRM 53-31-04 , AND 51-40-02
- [SDR SIMA20170616010](https://openairdocs.org/sdr/SIMA20170616010), Jun 16, 2017: YOKE. CRACKED. RIGHT ENGINE FWD LOWER YOKE IS CRACKED ON FWD SIDE. REPLACED THE FWD LOWER YOKE IAW EO EM-54MR-386.
- [SDR SIMA20170616008](https://openairdocs.org/sdr/SIMA20170616008), Jun 16, 2017: DOOR SILL. CORRODED. SERVICE DOOR CENTER SILL IS CORRODED AT LOWER AFT CORNER. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02, SRM 51-20-03, AND SRM 51-40-09.
- [SDR SIMA20170616007](https://openairdocs.org/sdr/SIMA20170616007), Jun 16, 2017: FLOOR SUPPORT. CORRODED. CENTER OMEGA BEAM IS CORRODED BETWEEN FRAMES 33-34. REPAIRED CENTER OMEGA BEAM WITH A FABRICATED DOUBLER & FILLER IAW SRM 53-00-10, 51-00-10, AND 51-20-01.
- [SDR SIMA20170616006](https://openairdocs.org/sdr/SIMA20170616006), Jun 16, 2017: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM IS CORRODED AT FRAME 29. INSTALLED A DOUBLER, FILLER, AND SHIMS ON THE OMEGA BEAM IAW SRM 53-00-10, AND 51-40-02.
- [SDR SIMA20170616005](https://openairdocs.org/sdr/SIMA20170616005), Jun 16, 2017: FLOOR SUPPORT. CORRODED. CENTER OMEGA BEAM IS CORRODED AT FRAME 29. REMOVED CORROSION IAW SRM 51-10-03.
- [SDR SIMA20170616009](https://openairdocs.org/sdr/SIMA20170616009), Jun 16, 2017: DOOR SILL. CORRODED. CARGO DOOR SILL FOUND CORRODED. REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02, AND 51-20-03.
- [SDR SIMA20161228002](https://openairdocs.org/sdr/SIMA20161228002), Dec 28, 2016: POWER SUPPLY. INOPERATIVE. BOTH LT AND RT EMERGENCY LIGHTS UNDER OVERWING EXIT DOORS ARE INOPERATIVE. R & R THE NR 4 POWER SUPPLY AND BATTERY HOLDER ASSY IAW AMM 33-50-04. OPS CHECKED GOO
- [SDR SIMA20161128001](https://openairdocs.org/sdr/SIMA20161128001), Nov 28, 2016: BRAKE. OVERHEATED. RIGHT BRAKE OVERHEAT INBD. REMOVED AND REPLACED THE NR 3 BRAKE ASSY IAW W/C 32-600-14.
- [SDR SIMA20160930001](https://openairdocs.org/sdr/SIMA20160930001), Sep 30, 2016: LIGHT. INOPERATIVE. RT OVERWING EMERGENCY LIGHT INOP. R&R RT OVERWING EMERGENCY LIGHT BULB, OPS GOOD IAW AMM 33-50-07.
- [SDR SIMA20160623003](https://openairdocs.org/sdr/SIMA20160623003), Jun 23, 2016: DOOR. LACK OF LUBE. MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. PERFORMED MAIN CABIN DOOR LUBE IAW AMM 52-10-01. OPS CHECK GOOD.
- [SDR SIMA20160405001](https://openairdocs.org/sdr/SIMA20160405001), Apr 5, 2016: UNKNOWN. ODOR. STRONG ELEC BURNING SMELL WITH NO SIGN OF SMOKE AFTER STARTING BOTH ENGS BEFORE TAXI. DEFERRED PACK ONE. PERFORMED OPERATIONS CHECK OF COOLING PACK SYS IAW AMM 
- [SDR SIMA20150917009](https://openairdocs.org/sdr/SIMA20150917009), Sep 17, 2015: INVERTER. INOPERATIVE. NUMBER 4 EMER LIGHT INVERTER INOPERATIVE. R & R NR 4 EMER LIGHT INVERTER IAW AMM 33-50-11. FOR OPERATIONS CHECK SEE BOW 202439.
- [SDR SIMA20150912004](https://openairdocs.org/sdr/SIMA20150912004), Sep 12, 2015: SKIN. CRACKED. LEFT UPPER FUSELAGE SKIN HAS 2 CRACKS AT FRAME 75 & ABOVE STRINGER 2L. REPAIRED LT UPPER FUSELAGE SKIN IAW ERS-EM-53MR-1676.
- [SDR SIMA20150912006](https://openairdocs.org/sdr/SIMA20150912006), Sep 12, 2015: SKIN. CRACKED. RIGHT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 & ABOVE STRINGER 2R. REPAIRED RT UPPER FUSELAGE SKIN IAW ERS-EM-53MR-1675.
- [SDR SIMA20150912005](https://openairdocs.org/sdr/SIMA20150912005), Sep 12, 2015: FRAME. GOUGED. FRAME 70 GOUGED, BETWEEN STRINGERS 11R - 12R. REPAIRED FRAME 70 IAW ERS-EM-53MR-1665.
- [SDR SIMA20150906005](https://openairdocs.org/sdr/SIMA20150906005), Sep 6, 2015: MARKER. DETERIORATED. SERVICE DOOR FRAME LOCKING RED MARKS DETERIORATED. RESTORED SERVICE DOOR LOCKING RED MARKS TO THE TOP TWO FRAME STOPS IAW CPM 51-21-06, ETNS EM-51-109, GN-51-01
- [SDR SIMA20150906006](https://openairdocs.org/sdr/SIMA20150906006), Sep 6, 2015: CROSSBEAM. CORRODED. CROSSBEAM AT FRAME 25 - 26 CORRODED. R & R CROSSBEAM, BETWEEN FRAME 25 - 26 IAW SRM 51-40-02 & ETN-EM-53-139 R4, SEE WIPS & TASK FOR DETAILS.
- [SDR SIMA20150509001](https://openairdocs.org/sdr/SIMA20150509001), May 9, 2015: DISPLAY. FAILED. IN FLIGHT, CAPTAIN SIDE ALTIMETER RED X DISPLAYED. SELECTED REVERSIONARY ADC AS DIRECTED BY AOM VOL 1 PROCEDURE. REMOVED SMALL AMOUNT OF WATER FROM PITOT STATIC
- [SDR SIMA20150115004](https://openairdocs.org/sdr/SIMA20150115004), Jan 15, 2015: UPLOCK. FAILED. ON CLIMB OUT NOSE GEAR & GEAR DOOR WOULD NOT CLOSE UP. R & R NLG UPLOCK BOX IAW AMM 32-33-07. OPERATIONS & LEAK CHECKED GOOD.
- [SDR SIMA20141128001](https://openairdocs.org/sdr/SIMA20141128001), Nov 28, 2014: FLASHLIGHT. INOPERATIVE. FIRST OFFICER`S FLASHLIGHT INOPERATIVE. R & R FIRST OFFICER`S FLASHLIGHT AS REQUESTED.
- [SDR SIMA20141113003](https://openairdocs.org/sdr/SIMA20141113003), Nov 13, 2014: TRUNNION. LACK OF LUBE. DURING TAKEOFF A LOUD RHYTHMIC THUMPING NOISE WAS HEARD DURING GEAR RETRACTION. A STRONG SMELL LIKE BURNING RUBBER OCCURRED AT THE SAME TIME. NO OTHER UNUSUAL I
- [SDR SIMA20141018005](https://openairdocs.org/sdr/SIMA20141018005), Oct 18, 2014: SHUTOFF VALVE. FAILED. DURING LANDING ROLLOUT FELT LIKE PARTIAL LOSS OF BRAKING. AFTER EXITING THE RUNWAY RT OF BRAKE TEMP SPIKED INTO UPPER AMBER RANGE, LT OTBD LOWER AMBER, INBDS BO
- [SDR SIMA20140620009](https://openairdocs.org/sdr/SIMA20140620009), Jun 20, 2014: LIGHT. INOPERATIVE. LEFT AFT OVERWING EMER LIGHT FOUND INOPERATIVE IAW PS 2 INSPECTION. R & R LT AFT OVERWING EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140514011](https://openairdocs.org/sdr/SIMA20140514011), May 14, 2014: WIRE. BROKEN. SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R OF EMERGENCY LIGHT ASSEMBLY IAW TASK 33-50-09-000-802-A, A BROKEN WIRE WAS DISCOVERED, REPLACED FEMALE CONNECTOR

All 132: https://openairdocs.org/aircraft/N631AE/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/N631AE/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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