# N634AE: 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: 145150
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 23, 1999
- Certificate issued: September 19, 2011
- Expires: September 30, 2027
- Mode S code: A84C9D
- 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=634AE
- Page: https://openairdocs.org/aircraft/N634AE

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/N634AE/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 N634AE.

## FAA accident and incident reports (2)

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 20090104001799I](https://openairdocs.org/incident/20090104001799I), Jan 4, 2009: Emb EMB145LR (N634AE), Syracuse, NY, Minor damage. (-23) On Sunday January 4, 2009, at 2204 EDT, an Embraer Emb-145-LR, s/n 145150, N634AE, operated by American eagle airlines landed on runway 10 at the…
- [Incident 20070819825929I](https://openairdocs.org/incident/20070819825929I), Aug 19, 2007: Emb EMB145LR (N634AE), Rochester, MN, No damage. (-23) On 08/19/2007 American eagle flight egf 397 in bound to rst from ord when they reported a burning smell in the cockpit. Aircraft landed without incident…

## Service difficulty reports (138, 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 HNAA2023102300366](https://openairdocs.org/sdr/HNAA2023102300366), Oct 22, 2023: UNKNOWN. UNKNOWN. EMERGENCY LIGHT STRIP IS DIM FROM ROW 8 TO 12. R&R'D EMERGENCY LIGHT #3 BATTERY IAW WORKCARD 33-70-19
- [SDR HNAA2023081700310](https://openairdocs.org/sdr/HNAA2023081700310), Aug 17, 2023: UNKNOWN. UNKNOWN. SPOILER FAIL SPOILER OLPEN INDICATION ON EICAS AFTER TAKE-OFF. VISUALLY CONFIRMED SPOILERS WERE NOT OPEN. MESSAGE STAYED ENTIRE FLIGHT. CHECKED CMC AND FOUNS IN
- [SDR HNAA2023072500253](https://openairdocs.org/sdr/HNAA2023072500253), Jul 25, 2023: UNKNOWN. UNKNOWN. SPOILER FAIL MSG ON EICAS AFTER TAKEOFF, SPOILERS WERE OPENED AND STAYED OPEN. T/S PER FIM TASK 27-63-00-800-806-A, BLOCKS 1 TO 5,15, 21 GROUND SPOILER VALVE FO
- [SDR HNAA2023071800249](https://openairdocs.org/sdr/HNAA2023071800249), Jul 18, 2023: UNKNOWN. UNKNOWN. DURING TAKEOFF SPOILER FAIL DISPLAYED ON EICAS. WITH SPOILER I/B FAIL DISPLAYED ON CMC. FOUND "SPOILER IB FAIL" ON CMC. INSPECTED I/B SPOILERS PROX SENSORS WITH
- [SDR HNAA2021022500056](https://openairdocs.org/sdr/HNAA2021022500056), Feb 20, 2021: SKIN. DENTED. EXTERNAL FUSELAGE SKIN HAS 2 DENTS BETWEEN FRAMES 12-13, STRINGERS 20--21L. COMPLETED INSTALLING REPAIR DOUBLER AND FILLER ON EXTERNAL FUSELAGE SKIN NR 4 BETWEE
- [SDR HNAA2021022500059](https://openairdocs.org/sdr/HNAA2021022500059), Feb 5, 2021: FLANGE. BENT. RIGHT NR 1 WING LEADING EDGE UPPER ATTACHMENT FLANGE BENT-NRWC E838627. REPAIRED RT NR 1 WING LEADING EDGE BY INSTALLING (MS20426AD8), DRILLED AND COUNTERSUNK F
- [SDR HNAA2021022500057](https://openairdocs.org/sdr/HNAA2021022500057), Feb 5, 2021: SKIN. CRACKED. CARGO DOOR EXTERNAL HANDLE CUTOUT HAS A POSSIBLE CRACK AT THE AFT END. CUT OUT CRACKED AREA OF CARGO DOOR SKIN AT AFT END OF HANDLE, FABRICATED EXTERNAL DOUBLER
- [SDR HNAA2021022500058](https://openairdocs.org/sdr/HNAA2021022500058), Feb 1, 2021: PROFILE. CORRODED. FR 65 L-SHAPE PROFILE IS CORRODED ON THE LOWER END JUST ABOVE THE DOOR. PERFORMED REPAIR OF FR 65 L-SHAPE PROFILE ON THE LOWER END JUST ABOVE THE DOOR SILL IAW 
- [SDR HNAA2020091800256](https://openairdocs.org/sdr/HNAA2020091800256), Sep 18, 2020: CARBON SEAL. LEAKING. THIS WAS THE FIRST OF 2 CABIN ODOR EVENTS ASSOCIATED WITH THIS AIRCRAFT/ENGINE. INITIAL TROUBLESHOOTING (INCLUDING BORESCOPE OF THE COMPRESSOR) DID NOT FIND ANY
- [SDR HNAA2020081700247](https://openairdocs.org/sdr/HNAA2020081700247), Aug 15, 2020: UNKNOWN. ODOR. FLIGHT DECK HAZY WITH PLASTIC SMELL ON CLIMB OUT BUT NO SMOKE. MAINTENANCE: DISPLACED POWER DISTRIBUTION AND RELAY PANELS IN FLIGHT DECK FOR INSPECTION, DETAILE
- [SDR HNAA2020081700245](https://openairdocs.org/sdr/HNAA2020081700245), Aug 14, 2020: UNKNOWN. ODOR. DURING TAKEOFF AND THROUGHOUT FLIGHT FUMES NOTED IN COCKPIT AND CABIN WITH BOTH PACKS IN AUTO AND APU OFF. CREW NOTICED THAT LH SIDEWALL AND CEILING PANEL AT RO
- [SDR HNAA2020081100243](https://openairdocs.org/sdr/HNAA2020081100243), Aug 10, 2020: UNKNOWN. SMOKE. ABORTED TAKEOFF DUE TO SMOKE IN FLIGHT DECK AND CABIN. CREW REPORTED OILY AND ELECTRICAL ODOR TO THE SMOKE. ABORTED AT 80 KNOTS. OPEN
- [SDR HNAA2020081000242](https://openairdocs.org/sdr/HNAA2020081000242), Aug 8, 2020: UNKNOWN. ODOR. FLIGHT DECK HAD CHEMICAL ODOR DURING CLIMB OUT AND GOT WORSE ON DECENT WITH NO VISABLE SMOKE. BLEEDS AND PACKS WERE ON. CABIN AREA HAD NO ODOR. RAN PACKS FOR 30
- [SDR HNAA2020030900090](https://openairdocs.org/sdr/HNAA2020030900090), Mar 8, 2020: VALVE. FAILED. ON TAKEOFF ATTEMP, AT 65KNOTS, GOT HIGH STAGE VLV 2 FAIL EICAS MESSAGE. REMOVED PANEL 422BT TO FOM. R/R'D #2 HIGH STAGE VALVE REF AMM 36-11-02. OPS CGHECK GOOD.
- [SDR HNAA2020020500046](https://openairdocs.org/sdr/HNAA2020020500046), Feb 4, 2020: WARNING MESSAGE. ILLUMINATED. ON CLIMB OUT E1 FIRE DETECTION FAIL MESSAGE ON EICAS. DISCREPANCY IS STILL IN WORK AT THIS TIME.
- [SDR HNAA2020011700020](https://openairdocs.org/sdr/HNAA2020011700020), Jan 15, 2020: WARNING MESSAGE. FALSE ACTIVATION. ON T/O ROLL EICAS CAUTION MESSAGE FOR HIGH STAGE VALVE 1 0R 2 FAILED. CAPTAIN SAID HE DID NOT KNOW FOR SURE WHICH IT WAS. AND MESSAGE WENT AWAY, WITH NO CMC MES
- [SDR HNAA2020011530017](https://openairdocs.org/sdr/HNAA2020011530017), Jan 14, 2020: WARNING MESSAGE. FALSE ACTIVATION. ON TAKE-OFF, E1 FIRE DET FAIL, EICAS CAUT MESS, PERFORMED QRH, MESS EXTINGUISHED. PERFORMED FIRE DETECTION SYSTEM OPERATIONAL CHECK PER AMM 26-10-00-700-802-A. 
- [SDR HNAA2019060300158](https://openairdocs.org/sdr/HNAA2019060300158), May 30, 2019: WARNING LIGHT. FALSE ACTIVATION. WING A/I FAIL IN CONJUCTION WITH WING ICE CONDITION, NO A/I EICAS WARNING FOLLOWED BY STAB A/I FAIL AND BLEED LOW TEMP EICAS MESSAGES. EICAS MESSAGES PERSISTED 
- [SDR HNAA2019043000124](https://openairdocs.org/sdr/HNAA2019043000124), Apr 28, 2019: BUTTON. LOOSE. PDIS 634 36-10 2040022 28APR19 PHL CLOSE BLD 1 VLV CLSD ON TAKEOFF. 28569 00 VAG HISTORY: YES FACT 28APR19 18:03 PHL INSP #1 BLEED PUSH BUTTON, FOUND TO BE LOOS
- [SDR HNAA2019043000123](https://openairdocs.org/sdr/HNAA2019043000123), Apr 27, 2019: SENSOR. FAILED. PDIS 634 36-21 2040011 27APR19 PHL CLOSE BLD 1 VLV CLSD ADVISORY MESS ON T/O. C/W QRH. 28370 00 LLS RETURN TO FIELD 00 HISTORY: SWAPPED TO 672. FACT 27APR19 06:
- [SDR HNAA2019042600121](https://openairdocs.org/sdr/HNAA2019042600121), Apr 24, 2019: WARNING MESSAGE. FALSE ACTIVATION. PDIS 634 36-12 1846482 24APR19 PWM CLOSE BLEED 1 VALVE CLOSED MESSAGE ON TAKEOFF. C/W QRH. FACT 24APR19 11:36 PWM CHECKED CMC FOR MESSAGES. NO RELEVANT MESSAGES
- [SDR HNAA2019030100053](https://openairdocs.org/sdr/HNAA2019030100053), Feb 28, 2019: WARNING SYSTEM. FALSE ACTIVATION. HSV 2 VLV FAIL MSG ON TAKEOFF FLASHED AND SELF-CLEARED. GROUND RAN NO.2 WITH BLEEDS ON NO DEFECTS OR MESSAGES NOTED CND OKAY FOR SERVICE AT THIS TIME.
- [SDR HNAA2019020600035](https://openairdocs.org/sdr/HNAA2019020600035), Feb 5, 2019: WARNING SYSTEM. FALSE ACTIVATION. ABORTED T/O DUE TO HS 2 VLV MSG FLASHED AND SELF CLEARED. C/W QRH AND NO MSG NOTED.
- [SDR HNAA2019010700009](https://openairdocs.org/sdr/HNAA2019010700009), Jan 4, 2019: LIGHT. INOPERATIVE. NDIS 634 33-51 0019600 04JAN19 RIC CLOSE MAIN DOOR EMERGENCY LIGHT WILL NOT ILLUMINATE. FACT 04JAN19 10:12 RIC. R/R THE EMERGENCY LIGHT ASSEMBLY IAW AMM TASK 33
- [SDR HNAA2018122100326](https://openairdocs.org/sdr/HNAA2018122100326), Dec 20, 2018: BULB. INOPERATIVE. MAIN DOOR EMERGENCY LIGHT INOP. R&R LIGHT BULB
- [SDR HNAA2018111600284](https://openairdocs.org/sdr/HNAA2018111600284), Nov 15, 2018: WIRE. BROKEN. DISCREPANCY: WIRE OF THE EMERGENCY LIGHT AT SERVICE DOOR IS BROKEN. ACTION TAKEN: R&R WIRE CONNECTOR ON MALE SIDE OF CONNECTOR FOR EMERGENCY LIGHT AT SERVICE DO
- [SDR HNAA2018092600229](https://openairdocs.org/sdr/HNAA2018092600229), Sep 21, 2018: NONE. NONE. PDIS 634 05-51 1691272 21SEP18 ILM CLOSE BIRD STRIKE R/H SIDE OF NOSE AREA, NO EVIDENCE OF IN GESTION NOTICED 21584 00 EK FACT 21SEP18 00:22 ILM ACCOMPLISH DETA
- [SDR HNAA2018081300195](https://openairdocs.org/sdr/HNAA2018081300195), Aug 11, 2018: LIGHT. INOPERATIVE. EMERGENCY FLOOD LIGHT ON SERVICE DOOR WAS INOPERATIVE. R & R THE EMERGENCY FLOOD LIGHT ASSEMBLY. OPS CHECKED GOOD.
- [SDR HNAA2018081300194](https://openairdocs.org/sdr/HNAA2018081300194), Aug 11, 2018: GROUND WIRE. DIRTY. EMERGENCY FLOOD LIGHT ON MAIN DOOR WORKS INTERMITTENLY. CLEANED THE GROUND WIRE AND ADJUSTED THE GROUND WIRE ON THE EMERGENCY FLOOD LIGHT. OPS CHECKED GOOD.
- [SDR HNAA2018081300193](https://openairdocs.org/sdr/HNAA2018081300193), Aug 11, 2018: LIGHT. DAMAGED. RIGHT EMERGENCY LIGHT WAS INOPERATIVE. INSPECTED AND FOUND THE BULB MOVED INSIDE THE ASSEMBLY. R & R LIGHT ASSY IAW AMM 33-50-10-000-801-A SECTION M AND 33-50-1
- [SDR HNAA2018070600140](https://openairdocs.org/sdr/HNAA2018070600140), Jun 12, 2018: CROSSBEAM. CORRODED. GALLEY CROSSBEAM AT FRAME 20 CORRODED. INSTALLED 3 NUTPLATES ON GALLEY CROSSBEAM AT FRAME 20 IAW SRM 51-40-09.
- [SDR HNAA2018070600139](https://openairdocs.org/sdr/HNAA2018070600139), Jun 12, 2018: FITTING. CORRODED. TWO LT APU FIRE WALL SHEER CLIPS INSIDE 312AR HAVE SURFACE CORROSION. REMOVED AND REPLACED TWO APU FIRE WALL SHEER CLIPS INSIDE 312AR IAW SRM 51-40-02.
- [SDR HNAA2018070600138](https://openairdocs.org/sdr/HNAA2018070600138), Jun 10, 2018: STRUCTURE. CORRODED. SERVICE DOOR LOWER FWD NUT PLATE HOLE CORROSION. PERFORMED HFEC INSPECTIONS AND UT THICKNESS IAW EASI NDTM NO CRACK NOTED. BLENDED SERVICE DOOR LOWER FWD NUT PL
- [SDR HNAA2018070600137](https://openairdocs.org/sdr/HNAA2018070600137), Jun 10, 2018: DOOR FRAME. CORRODED. CARGO DOOR FWD UPPER TWO NUTPLATE HOLES HAVE SURFACE CORROSION. PERFORMED HFEC INSPECTION AND UT THICKNESS IAW EASI NDTM, NO DEFECTS NOTED. FABRICATED REPAIR DO
- [SDR HNAA2018070600136](https://openairdocs.org/sdr/HNAA2018070600136), Jun 10, 2018: STRUCTURE. CORRODED. CARGO DOOR FWD LOWER NUT PLATE HOLES HAVE SURFACE CORROSION. PERFORMED HFEC AND UT THICKNESS IAW EASI NDTM, NO DEFECTS NOTED. CARGO DOOR FWD LOWER NUT PLATE PRO
- [SDR HNAA2018070600133](https://openairdocs.org/sdr/HNAA2018070600133), Jun 10, 2018: STRUCTURE. CORRODED. CARGO DOOR NUT PLATE HOLE HAS SURFACE CORROSION. PERFORMED HFEC AND UT THICKNESS IAW EASI NDTM NO DEFECTS NOTED. R&R CARGO DOOR UPPER SURFACE ANGLE PROFILE IAW 
- [SDR HNAA2018041800082](https://openairdocs.org/sdr/HNAA2018041800082), Apr 16, 2018: LIGHT. INOPERATIVE. RT SERVICE DOOR EMERGENCY LIGHT INTERMITTENT. R & R THE LIGHT ASSY.
- [SDR HNAA2018033000077](https://openairdocs.org/sdr/HNAA2018033000077), Mar 28, 2018: LIGHT. UNKNOWN. REAR OVERHEAD AND AISLE EMERGENCY LIGHT WILL NOT ILLUMINATE. INSPECTED THE OVERHEAD & AISLE EMERGENCY LIGHTS, NO DEFECTS NOTED. OPS CHECKED GOOD IAW AMM 33-50-0
- [SDR HNAA2017013000029](https://openairdocs.org/sdr/HNAA2017013000029), Jan 30, 2017: ANTI-ICE SYSTEM. MALFUNCTIONED. ON DESCENT, IN ICING CONDITIONS, WING ANTI-ICE FAIL EICAS CAUTION MESSAGE APPEARED ON QRH, STAB ANTI-ICE FAIL CAUTION AND ICE CONDITION ANTI-ICE INOP WARNING AP
- [SDR HNAA2017010400005](https://openairdocs.org/sdr/HNAA2017010400005), Jan 4, 2017: WARNING LIGHT. ILLUMINATED. ICE DETECTION PNEUMATIC ON GROUND CHECK, ICAS MESSAGE ENG , A/I DISAGREE. ILLUMINATES DURING TEST AND THEN EXTINGUISHES AFTER TEST IS COMPLETE. REMOVED AND REPL
- [SDR HNAA2017010400004](https://openairdocs.org/sdr/HNAA2017010400004), Jan 4, 2017: WARNING LIGHT. FALSE ACTIVATION. ABORTED TAKEOFF DUE TO ICE CONDITION ADVISORY AND ANTI ICE INOPERATIVE WARNING MESSAGE. GROUND RAN, OPS CHECKED NORMAL. IAW FIM 30-80-810-801-A AND MM 30-00-700
- [SDR HNAA2016111600350](https://openairdocs.org/sdr/HNAA2016111600350), Nov 16, 2016: LAMP. INOPERATIVE. EMERGENCY LIGHT OVER THE WING ON THE RIGHT SIDE IS INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW MM 33-50-10. OPS CHECKED GOOD.
- [SDR HNAA2016091400281](https://openairdocs.org/sdr/HNAA2016091400281), Sep 12, 2016: INDICATION SYS. READS HIGH. DURING CLIMB AT 7000 FEET, AN EICAS MESSAGE ILLUMINATED FOR FUEL INBALANCE. DURING RETURN TO FIELD, THE RT TANK SHOWED LOWER QUANTITY BY VARIOUS AMOUNTS STARTIN
- [SDR HNAA201662000189](https://openairdocs.org/sdr/HNAA201662000189), Jun 19, 2016: ACTUATOR. MALFUNCTIONED. TRIM MAIN INOPERATIVE WARNING MESSAGE ILLUMINATED ON EICAS DURING CLIMB OUT 41500. R & R THE HSCU, NO FIX. CAN RESET P TRIM INDICATION WITH TRIM FULL DOWN. FAIL
- [SDR HNAA2016062000189](https://openairdocs.org/sdr/HNAA2016062000189), Jun 19, 2016: NOT REPORTED. MALFUNCTIONED. PTRM MAIN INOPERATIVE WARNING MESSAGE ILLUMINATED ON EICAS DURING CLIMBOUT. T/S PTRIM MAIN INOPERATIVE R & R HSCU. NO FIX. CAN RESET PTRIM INDICATION WITH TRIM 
- [SDR HNAA2016062000188](https://openairdocs.org/sdr/HNAA2016062000188), Jun 18, 2016: SWITCH. FAILED. PTRIM MAIN INOPERATIVE, WARNING MESSAGE APPEARED ON EICAS IN FLIGHT WITH AUTOPILOT ON. QRH PROCEDURE WAS FOLLOWED AND BACKUP SYS OPERATED NORMALLY. T/S PTRIM MA
- [SDR HNAA2016060600163](https://openairdocs.org/sdr/HNAA2016060600163), Jun 5, 2016: ACM. FAILED. IN ICING CONDITIONS AT CRUISE CREW NOTICED A BURNING ODOR IN THE COCKPIT AND FWD GALLEY AREA AND AFTER LANDING PACK 2 OVERHEAT AND PACK 2 OVLD EICAS MESSAGES AP
- [SDR HNAA2016052400148](https://openairdocs.org/sdr/HNAA2016052400148), May 21, 2016: UNKNOWN. ODOR. UPON LEVELING OUT FROM DESCENT WHEN THRUST LEVER ADVANCED, SMOKE ODOR COMING FROM VENTS. POSSIBLE ELECTRICAL SMOKE ODOR FOR 1-2 MINUTES. INSPECTED ACFT. GROUND 
- [SDR HNAA2016031600085](https://openairdocs.org/sdr/HNAA2016031600085), Mar 18, 2016: LINE. LEAKING. NR 1 HYDRAULIC LOST EICAS MESSAGE, HYDRAULIC LOW QTY. FOUND GEAR ACTUATOR DOWN LINE LEAKING. FERRIED ACFT.
- [SDR SIMA20160126005](https://openairdocs.org/sdr/SIMA20160126005), Jan 26, 2016: SKIN. CRACKED. RIGHT UPPER FUSELAGE SKIN CRACKED 2 PLACES, CRACK 1 IS JUST AFT OF FRAME 75, JUST ABOVE STRINGER 2R, CRACK IS APPROX 3/8" IN LENGTH. CRACK 2 IS ON FRAME 75, AT 

All 138: https://openairdocs.org/aircraft/N634AE/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/N634AE/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.