# N632AE: 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: 145143
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 25, 1999
- Certificate issued: September 9, 2011
- Expires: September 30, 2027
- Mode S code: A8452F
- 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=632AE
- Page: https://openairdocs.org/aircraft/N632AE

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/N632AE/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 N632AE.

## 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 20040520012309I](https://openairdocs.org/incident/20040520012309I), May 20, 2004: Emb EMB145LR (N632AE), Omaha, NE. (-23) American eagle flight 4179 was enroute from ord to oma, the crew reported on approach to Omaha that they had received an icas message regarding nose gear…

## Service difficulty reports (197, 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 HNAA2023061900201](https://openairdocs.org/sdr/HNAA2023061900201), May 28, 2023: UNKNOWN. UNKNOWN. E978500 SERVICE DOOR LOWER CENTER SILL CORRODED. DRILLED AND INSTALLED SERVICEABLE SERVICE DOOR LOWER CENTER SILL IAW EMB145 SRM 51-20-03, SRM 51-40-06 AND SRM 
- [SDR HNAA2023061900200](https://openairdocs.org/sdr/HNAA2023061900200), May 27, 2023: UNKNOWN. UNKNOWN. E978456 SERVICE DOOR FWD SILL IS CORRODED IN MULTIPLE AREAS. REMOVED AND REPLACED SERVICE DOOR FWD SILL IAW EMB145 SRM 51-40-02.
- [SDR HNAA2023061900199](https://openairdocs.org/sdr/HNAA2023061900199), May 24, 2023: UNKNOWN. UNKNOWN. E977696 CORROSION FOUND ON AFT SIDE OF FR 65 STR 16L-17L. COMPLETED INSTALLATION OF SERVICEABLE LH LOWER SECTION OF FR 65 IAW EMB 145 SRM 51-40-02, ETD# ETD2023
- [SDR HNAA2023061900198](https://openairdocs.org/sdr/HNAA2023061900198), May 19, 2023: UNKNOWN. UNKNOWN. E976668 NOSE-WHEEL SPIN-BRAKE NUT PLATE SUPPORT BEAM CRACK NEXT TO NUT PLATE HOLES. RAR NOSE-WHEEL SPIN-BRAKE NUT PLATE SUPPORT BEAM IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2023061900197](https://openairdocs.org/sdr/HNAA2023061900197), May 18, 2023: UNKNOWN. UNKNOWN. E976100 SERVICE DOOR AFT SILL IS CORRODED AROUND FWD SCREW HOLE. REMOVED OLD SERVICE DOOR AFT SILL AND INSTALLED NEW SERVICE DOOR AFT SILL IAW EMB 145 SRM 51-40
- [SDR HNAA2023061900196](https://openairdocs.org/sdr/HNAA2023061900196), May 17, 2023: UNKNOWN. UNKNOWN. E975876 SSI 53-30-48, CARGO DOOR LOWER SILL FWD "T" PROFILE HAS CORROSION. REMOVED AND REPLACED CARGO DOOR LOWER SILL FWD “T” PROFILE IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2023061900195](https://openairdocs.org/sdr/HNAA2023061900195), May 17, 2023: UNKNOWN. UNKNOWN. E975875 SSI 53-30-48, CARGO DOOR CUTOUT AFT SHEAR CLIP LOWER CORNER HAS CORROSION. ACCOMPLISHED REPAIR OF FR 68 SHEAR CLIP BTW STGR 15L AND 18L IAW EMB 145 SRM 
- [SDR HNAA2023061900194](https://openairdocs.org/sdr/HNAA2023061900194), May 17, 2023: UNKNOWN. UNKNOWN. 975874 SSI 53-30-48, CARGO DOOR CUTOUT FWD SHEAR CLIP LOWER CORNER HAS CORROSION. BLENDED CORROSION ON CARGO DOOR CUTOUT FWD SHEAR CLIP LOWER CORNER IAW EMB 145
- [SDR HNAA2021062100268](https://openairdocs.org/sdr/HNAA2021062100268), Jun 20, 2021: LINE. CRACKED. DURING FLIGHT. E2 A/I FAIL MESSAGE APPEARED. FOLLOWED QRH AND MESSAGE REMAINED. T/S IN REF TO FIM 30-11-00-810-801-A. INSPECTED ENG BLEED DUCTS ON #2 ENGINE. FO
- [SDR HNAA2021062100267](https://openairdocs.org/sdr/HNAA2021062100267), Jun 18, 2021: LINE. CRACKED. DURING FLIGHT WING A/I FAIL MESSAGE APPEARED. FOLLOWED QRH AND MESSAGE REMAINED. HA300 FACTED OUT AS - T/S IN REF TO FIM 30-11-00-810-801-A. INSPECTED ENG BLEED
- [SDR HNAA2021060200232](https://openairdocs.org/sdr/HNAA2021060200232), Jun 1, 2021: WARNING MESSAGE. FALSE ACTIVATION. PDIS 632 27-36 2379001 01JUN21 EVV CLOSE SPS 1-2 INOP, SPS ADANCE, NO TAKEOFF CONFIG DURING TAKEOFF MESSAGES CLEARED WHEN A/C STOPPING. FACT 01JUN21 10:52 EVV P
- [SDR HNAA2021052100222](https://openairdocs.org/sdr/HNAA2021052100222), May 19, 2021: ANTI-ICE SYSTEM. MALFUNCTIONED. DURING CLIMB AT 14000 FEET EICAS E2 A/ICE FAIL PRESENTED. RAN QRH MSG WAS INTERMITTENT WITH OVERRIDE KNOB SELECTED TO ALL. ENG AIR INLET 2 OPEN INSCRIPTION WAS 
- [SDR HNAA2021032500102](https://openairdocs.org/sdr/HNAA2021032500102), Mar 24, 2021: WARNING MESSAGE. FALSE ACTIVATION. NDIS 632 27-00 0029100 24MAR21 PHF CLOSE FOR MIR PURPOSE: PILOT DID ABORTED TAKE OFF WHEN HE NOTED A POSSIBLE SPOILER DEPLOYMENT WITH FAIL MESSAGE.DIRECTED CA T
- [SDR HNAA2021012500029](https://openairdocs.org/sdr/HNAA2021012500029), Jan 24, 2021: SOLENOID VALVE. MALFUNCTIONED. AROUND 8000 FT NLG DOOR OPENED UNCOMMANDED. FOUND NLG DOOR NOT CLOSING WITH GEAR UP. T/S IN REF TO EMB145 FIM 32-32-00. R & R NLG DOOR SOLENOID VALVE, REF EMB14
- [SDR HNAA2021011800027](https://openairdocs.org/sdr/HNAA2021011800027), Jan 16, 2021: ANTI-ICE VALVE. FAILED. E2 ANTI ICE FAIL AT 60 KNOTS ON TAKEOFF ROLL *NOTE* PASSED GROUND PNEUMATIC TEST, MESSAGE EXTINGUISHED WHEN THRUST LEVER RETURNED TO IDLE. REINSTALLED ORIGINAL 
- [SDR HNAA2020060800168](https://openairdocs.org/sdr/HNAA2020060800168), Jun 7, 2020: ACM. MALFUNCTIONED. SMOKE IN CABIN OBSERVED. CLEARED UP WITH PACK 1 ON. SMOKE PERSISTED WITH PACK 2 ON. CREW NOTICED PACK 2 MAKING NOISE. R&R'D RT ACM IAW AMM 21-51-03-04. RAN PACK
- [SDR HNAA2019090900260](https://openairdocs.org/sdr/HNAA2019090900260), Sep 6, 2019: PRESSURE SWITCH. MALFUNCTIONED. PDIS 632 29-10 1948251 06SEP19 CLT CLOSE RUDDER SYS 1/2 INOP MSG IN FLIGHT WEITH HYD SYSTEM 1 FAIL MSG INTERMITTENT. 27717 00 RNR HISTORY: NONE FACT 06SEP19 17:
- [SDR HNAA2019012300026](https://openairdocs.org/sdr/HNAA2019012300026), Jan 22, 2019: VALVE. MALFUNCTIONED. PDIS 632 36-10 1856433 22JAN19 PHL CLOSE HS VLV 2 FAIL EICAS MSG DURING TAKE OFF ROLL HISTORY: FACT 22JAN19 20:17 PHL TROUBLESHOT WITH FIM 36-11-00-810-810-A UP
- [SDR HNAA201809040012](https://openairdocs.org/sdr/HNAA201809040012), Sep 2, 2018: CONNECTOR. DIRTY. PILOT'S EMERGENCY FLASHLIGHT WILL NOT ILLUMINATE. TRIED BATTERY, NO FIX. BATTERY BACK TO ORIGINAL. CLEANED AND RESEATED CONNECTORS IN REF TO SWPM 20-50-00, GOOD
- [SDR HNAA2018081300197](https://openairdocs.org/sdr/HNAA2018081300197), Aug 12, 2018: UNKNOWN. ODOR. EXAUST FUMES WERE DETECTED IN THE COCKPIT AFTER ENGINE START USING THE APU. APU EGT GOES TO AMBER DURING ENGINE START. EGT FLUCTUATES IN HIGH 600S WITH NO EICAS
- [SDR HNAA2018071800155](https://openairdocs.org/sdr/HNAA2018071800155), Jul 14, 2018: WIRE. BROKEN. NR 2 ENGINE FAILED TO START. NO ROTATION. ON APU BLEED. FOUND BROKEN WIRES ON PINS 10 AND 39 ON PNEUMATIC CONTROL PANEL CONNECTOR P7128. REPAIRED WIRES IAW SWPM
- [SDR HNAA2017081400271](https://openairdocs.org/sdr/HNAA2017081400271), Aug 11, 2017: CONTROLLER. FAILED. NR 1 WINDSHIELD HEAT FAIL EICAS MESSAGE DURING ICING CONDITIONS. CREW COMPLIED WITH QRH. DID NOT ATTEMPT TO REACTIVATE THE SYSTEM. R & R THE NR 1 WINDSHIELD TEM
- [SDR HNAA2017073100258](https://openairdocs.org/sdr/HNAA2017073100258), Jul 31, 2017: RELAY. FAILED. DURING INSPECTION OF RELAY E FAIL STEP-11 IAW FCD1-30-16-0276. FOUND DAMAGE/BURNT PINS ON PITOT STATIC NR 3. RELAY K0058 PIN C2, RELAY SOCKET/BASE XK0058 PIN C2
- [SDR SIMA20170724003](https://openairdocs.org/sdr/SIMA20170724003), Jul 24, 2017: LIGHT. INOPERATIVE. AREA EMERGENCY LIGHT ON GALLEY DOOR HINGE INTERMITTENT. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT ASSY IAW AMM 33-50-10. OPS CHECK GOOD.
- [SDR SIMA20170609001](https://openairdocs.org/sdr/SIMA20170609001), Jun 9, 2017: ROLLER. LACK OF LUBE. FA REPORTED MAIN CABIN DOOR HARD TO OPERATE. LUBRICATED THE MAIN DOOR FRAME ROLLERS IAW ETN-EN-52-061.
- [SDR SIMA20170408003](https://openairdocs.org/sdr/SIMA20170408003), Apr 8, 2017: LAMP. NOT SEATED. SERVICE DOOR GROUND ILLUMINATION EMERGENCY LIGHT INOPERATIVE. RESEATED THE LAMP IAW AMM 33-50-09. OPS CHECKED GOOD.
- [SDR SIMA20170317001](https://openairdocs.org/sdr/SIMA20170317001), Mar 17, 2017: ROLLER. LACK OF LUBE. PASSENGER DOOR WOULD NOT OPEN INSIDE OR OUTSIDE. CLEAN AND LUBED MAIN DOOR ROLLERS IAW AMM 52-21-01. OPS CHECKED GOOD.
- [SDR SIMA20170107004](https://openairdocs.org/sdr/SIMA20170107004), Jan 7, 2017: CONTROL PANEL. INOPERATIVE. MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT PANEL ASSEMBLY IAW AMM 25-23-04. OPS CHECKED GOOD IAW AMM 33-50-00.
- [SDR SIMA20170107005](https://openairdocs.org/sdr/SIMA20170107005), Jan 7, 2017: LAMP. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-09. OP CHECKED GOOD IAW AMM 33-50-00.
- [SDR SIMA20170102001](https://openairdocs.org/sdr/SIMA20170102001), Jan 2, 2017: LIGHT. INOPERATIVE. MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN EXTERNAL EMERGENCY LIGHT IAW AMM 33-50-10-000-801, AND 33-50-10-400-801. OPS CHECKED GOOD.
- [SDR SIMA20161230002](https://openairdocs.org/sdr/SIMA20161230002), Dec 30, 2016: CRADLE. BROKEN. FWD CABIN EMERGENCY FLASHLIGHT CRADLE BROKEN. REMOVED AND REPLACED FWD FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801-A, AND 33-50-16-400-801-A OPS CHECKED GOOD.
- [SDR SIMA20161230001](https://openairdocs.org/sdr/SIMA20161230001), Dec 30, 2016: LAMP. INOPERATIVE. MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. OPS CHECKED GOOD.
- [SDR SIMA20161120001](https://openairdocs.org/sdr/SIMA20161120001), Nov 20, 2016: DOOR. OUT OF ADJUST. AIRCREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN FROM THE OUTSIDE HANDLE. ADJUSTED THE DOOR IAW ETN EM-52-013R1.
- [SDR SIMA20161117001](https://openairdocs.org/sdr/SIMA20161117001), Nov 17, 2016: DOOR. LACK OF LUBE. MAIN CABIN DOOR VERY HARD TO GET OPEN WHEN HANDLE FULL UP. COMPLIED WITH PAX DOOR INSPECTION IAW AMM 52-11-00 LUBE AS REQUIRED CHECK GOOD OK FOR SERVICE
- [SDR SIMA20161106001](https://openairdocs.org/sdr/SIMA20161106001), Nov 6, 2016: ROLLER. LACK OF LUBE. FA REPORTS MAIN DOOR DIFFICULT TO OPEN. LUBRICATED MAIN DOOR FRAME ROLLER IAW AMM 53-21-02. OPS CHECKED GOOD.
- [SDR SIMA20161103001](https://openairdocs.org/sdr/SIMA20161103001), Nov 3, 2016: CLAMP. UNSECURE. DURING CLIMB, CREW RECEIVED NR 1ENGINE BLEED LEAK MESSAGE. CREW COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT INCI
- [SDR SIMA20161102002](https://openairdocs.org/sdr/SIMA20161102002), Nov 2, 2016: SLEEVE. BLOWN. NR 1 BLEED LEAK AFTER TAKE OFF, RAN CHECKLISTS AND BLEED LEAK INDICATION WENT OUT AFTER ABOUT 5 MINUTES. INSPECTED AND FOUND THE NR 1 PACK DUCTING SLEEVE TO BE 
- [SDR SIMA20161023004](https://openairdocs.org/sdr/SIMA20161023004), Oct 23, 2016: CRADLE. BROKEN. FWD FLASHLIGHT CRADLE BROKEN. REMOVED AND REPLACED THE FLASHLIGHT CRADLE ASSEMBLY. OPS CHECKED GOOD IAW AMM 33-50-16.
- [SDR SIMA20160913002](https://openairdocs.org/sdr/SIMA20160913002), Sep 13, 2016: ROLLER. LACK OF LUBE. MAIN CABIN DOOR VERY DIFFICULT TO OPEN. LUBRICATED THE MAIN DOOR ROLLERS, OPS CHECKED GOOD IAW AMM 52-18-00-820-801-A.
- [SDR SIMA20160905001](https://openairdocs.org/sdr/SIMA20160905001), Sep 5, 2016: ROLLER. LACK OF LUBE. MAIN CABIN DOOR VERY DIFFICULT TO OPEN. LUBRICATE MAIN CABIN DOOR'S FRAME ROLLERS AND OPC, GOOD. REFER TO AMM 53-21-02.
- [SDR SIMA20160826001](https://openairdocs.org/sdr/SIMA20160826001), Aug 26, 2016: WARNING SYSTEM. FALSE ACTIVATION. TAKEOFF CONFIGURATION TRIM WARNING AT 100KTS. ABORTED TAKEOFF. PERFORMED OPS CHECK IAW AMM 27-40-00 OPS CHECKED GOOD. PERFORMED HIGHSPEED TAXI WITH CREW TAXI CH
- [SDR SIMA20160729003](https://openairdocs.org/sdr/SIMA20160729003), Jul 29, 2016: LIGHT. INOPERATIVE. MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R MAIN CABIN DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPC GOOD AT THIS TIME.
- [SDR SIMA20160708003](https://openairdocs.org/sdr/SIMA20160708003), Jul 8, 2016: BULB. INOPERATIVE. RH INTERIOR CEILING MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED RT INTERIOR CEILING MOUNTED EMERGENCY EXIT LIGHT BULB IAW AMM 33-50-08 OPS CH
- [SDR SIMA20160706003](https://openairdocs.org/sdr/SIMA20160706003), Jul 6, 2016: ROLLER. LACK OF LUBE. FA REPORTED MAIN CABIN DOOR DIFFICULT TO OPEN & CLOSE. LUBRICATED THE ROLLERS ON FUSELAGE FRAME FOR MAIN CABIN DOOR IAW AMM 52-00-00. OPS CHECKED GOOD.
- [SDR SIMA20160629001](https://openairdocs.org/sdr/SIMA20160629001), Jun 29, 2016: DOOR SEAL. DIRTY. F/A REPORTS MAIN ENTRANCE DOOR IS VERY HARD TO OPEN. CLEANED SEAL AND PERFORMED OPS CHECK OF MAIN CABIN DOOR IAW AMM 52-10-01, OPS CHECK GOOD.
- [SDR SIMA20160430001](https://openairdocs.org/sdr/SIMA20160430001), Apr 30, 2016: DOOR FRAME. DIRTY. MAIN DOOR DIFFICULT TO OPEN. CLEANED DEBRIS OUT OF DOOR FRAME IAW AMM 53-21-02. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR SIMA20160323001](https://openairdocs.org/sdr/SIMA20160323001), Mar 23, 2016: BATTERY PACK. DISCHARGED. NUMBER 3 EMER LIGHT BATTERY PACK NEEDS REPLACEMENT INOPERATIVE. R & R NR 3 EMER LIGHTING BATTERY PACK IAW AMM 33-50-04. TESTED SATISFACTORY.
- [SDR SIMA20160315002](https://openairdocs.org/sdr/SIMA20160315002), Mar 15, 2016: LIGHT. INOPERATIVE. MAIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EMER LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR SIMA20160306002](https://openairdocs.org/sdr/SIMA20160306002), Mar 6, 2016: BULB. INOPERATIVE. CAPTAINS FLASHLIGHT INOPERATIVE. R & R CAPTAIN`S FLASHLIGHT BULB. OPS CHECKED GOOD IAW AMM 33-51-01.
- [SDR SIMA20160301002](https://openairdocs.org/sdr/SIMA20160301002), Mar 1, 2016: CONTACTOR. DEFECTIVE. AT GATE PRIOR TO DEPARTURE, PUNGENT ACRID ODOR, SUGGESTIVE OF ELEC FIRE FILLED FLIGHT DECK. APU RUNNING, NO GND POWER, INSPECTED ACFT THERMALLY, NO SIGNIFICANT 

All 197: https://openairdocs.org/aircraft/N632AE/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/N632AE/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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