# N629AE: 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 AE3007C series](https://openairdocs.org/engine/allison-ae3007c-series) (registry code 03028)
- 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: 145130
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 12, 1999
- Certificate issued: October 6, 2011
- Expires: October 31, 2027
- Mode S code: A837B1
- 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=629AE
- Page: https://openairdocs.org/aircraft/N629AE

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. The registry lists only the engine series, so ADs for every Allison AE3007C model are included.

## ADs that may apply (OpenAirDocs): 102 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 AE3007C series)

- [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 2017-11-05](https://openairdocs.org/ad/2017-11-05): Turbine/ turboprop Engine, Turbine Section · Rolls-Royce AE 3007C and AE 3007C1. Effective Jul 18, 2017
- [AD 2015-02-08](https://openairdocs.org/ad/2015-02-08): Turbine wheels · Rolls-Royce AE 2100D2, AE 2100D2A, AE 2100D3 and 11 more. Effective Mar 11, 2015
- [AD 2009-24-04](https://openairdocs.org/ad/2009-24-04): Fan spinner · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 5 more. Effective Dec 28, 2009
- [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 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 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 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 113: https://openairdocs.org/aircraft/N629AE/ads.md

## Information bulletins (advisory) (9 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 NE-11-22](https://openairdocs.org/saib/NE-11-22): Engine Controls. Issued Feb 23, 2011
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N629AE.

## 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 20070727016639I](https://openairdocs.org/incident/20070727016639I), Jul 27, 2007: Emb EMB145LR (N629AE), Little Rock, AR, No damage. (-23) On takeoff the aircraft hit a flock of birds. Two struck the radome and one hit the left hand wing. The flight returned to lit for inspection and landed…

## Service difficulty reports (150, 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 HNAA2023050100148](https://openairdocs.org/sdr/HNAA2023050100148), Apr 30, 2023: UNKNOWN. UNKNOWN. LOUD WHOOSHING NOISE ON TAKEOFF ROLL, A/C NOT ACCELERATING PROPERLY. FACT 30APR23 21:42 PHL MX FOUND FO'S DV WINDOW TRIM SEAL PARTIALLY UNSEATED. APPLY RTV 230 
- [SDR HNAA2023030600060](https://openairdocs.org/sdr/HNAA2023030600060), Mar 5, 2023: NONE. NONE. DURING FLIGHT PACK 1 VLV CLOSED APPEARED ON EICAS AND WOULDNT RESET. PACK 2 CURRENTLY ON MEL, A/C COULD NOT HOLD PRESSURIZATION FACT 05MAR23 20:27 CLT FOUND MUL
- [SDR HNAA2023010400015](https://openairdocs.org/sdr/HNAA2023010400015), Jan 2, 2023: BLEED VALVE. FAILED. REJECTED TAKEOFF AT 60 KNOTS. BLEED 2 VALVE FAIL WITH TAKEOFF POWER SELECTED. R & R #2 ENGINE BLEED VALVE IRT AMM 36-11-05. OPS CHECK / LEAK CHECK GOOD. NO DEFE
- [SDR HNAA2022100500266](https://openairdocs.org/sdr/HNAA2022100500266), Oct 4, 2022: BLEED VALVE. FAULTED. BLEED 2 VALVE FAILURE ON T/O POWER ( C/W RMM 36-11-05) T/S FIM 36-11-00-810-806-A STEPS 1 2 3 20 21 AND 22 R/R #2 HIGH STAGE PRESSURE SWITCH IAW AMM 36-11-07. O
- [SDR HNAA2022061400223](https://openairdocs.org/sdr/HNAA2022061400223), Jun 12, 2022: NONE. NONE. PDIS 629 36-21 2116541 12JUN22 RIC CLOSE BLEED 1 LEAK IN FLT 29363 00 RS FACT 13JUN22 06:07 RIC FOUND THERMAL SWITCH WIRE NOT SOLDERED IN AFT AVIONIS BAY BY THE
- [SDR HNAA2022022000082](https://openairdocs.org/sdr/HNAA2022022000082), Feb 17, 2022: NONE. NONE. PDIS 629 21-01 2706202 17FEB22 CAK CLOSE ELETRICAL BURNING SMELL DURING DESCENT LASTED FOR 30 SEC. SMELL WAS NOTICED FWD CABIN/FLT DECK AREA. 27933 00 RS FACT 1
- [SDR HNAA2022020900068](https://openairdocs.org/sdr/HNAA2022020900068), Feb 7, 2022: NOT REPORTED. NOT REPORTED. PDIS 629 36-11 2706101 07FEB22 ISP CLOSE HS 1 VLV FAIL MSG DURING TAKE OFF ROLL. REJECTED TAKE OFF AT 65 KTS FULL THROTTLE FACT 07FEB22 11:24 ISP PERFORMED OPS 
- [SDR HNAA2012081700384](https://openairdocs.org/sdr/HNAA2012081700384), Aug 14, 2021: VALVE. FAULTED. ON TAKE OFF PACK 2 VALVE CLOSED MSG WOULD NOT CLEAR UNTIL LANDING. DURING INSPECTION OF AIR CON/PNUMATIC PANEL FOUND AND REPAIRED BROKEN WIRE IAW SWPM 20-5000 (
- [SDR HNAA2021071300320](https://openairdocs.org/sdr/HNAA2021071300320), Jul 10, 2021: PIPE. LEAKING. BLEED 1 LEAK MSG DURING CLIMB. T/S IN REF W/FIM TASK 36-20-00-810-801-A. FOUND Y-PIPE AFTER #100 ENG BLD VLV TO BE DAMAGED. R&R'D Y-PIPE AFTER #100 ENG BLD VLV 
- [SDR HNAA2021062400295](https://openairdocs.org/sdr/HNAA2021062400295), Jun 22, 2021: UPLOCK. FAULTED. AFTER GEAR RETRACTION, RIGHT MAIN INDICATION ALTERNATED BETWEEN UP AND LOCKED AND IN TRANSIT. R&R'D R/H MLG UP LOCK BOX IAW AMM 32-33-10-04. OPS CHECK GOOD. NO 
- [SDR HNAA2021062400294](https://openairdocs.org/sdr/HNAA2021062400294), Jun 22, 2021: UPLOCK. MALFUNCTIONED. AFTER GEAR RETRACTION CONTINUOUS THUMPING NOISE HEARD FROM NOSE BAY AREA. AFTER R/H MLG UP LOCK BOX WAS R&R'D REF LOG PAGE 260829-2. NO NOISE HEARD IN NOSE BAY 
- [SDR HNAA2021060900235](https://openairdocs.org/sdr/HNAA2021060900235), Jun 8, 2021: ACTUATOR. FAULTED. PITCH TRIM BACK UP INOP. R&R HORIZONTAL STABILIZE ACTUATOR IAW EMB 145 AMM 27-40-02-000/A00-801A REQUIRES ZERO RIG CHECK AMM TASK 27-40-02-700-801-A/500. PERFOR
- [SDR HNAA2021052500225](https://openairdocs.org/sdr/HNAA2021052500225), May 21, 2021: CONTROL UNIT. FAILED. PDIS 629 27-41 2580431 21MAY21 CLT CLOSE PITCH TRIM MAIN INOP MESSAGE AT 6000 FT AFTER TAKE OFF FACT 21MAY21 15:06 CLT R/R HORIZONTAL STAB CONTROL UNIT IAW AMM 
- [SDR HNAA2019082300235](https://openairdocs.org/sdr/HNAA2019082300235), Aug 22, 2019: CONTROL MODULE. MALFUNCTIONED. EMERGENCY LIGHT NOT ARMED, EICAS MESSAGE DISPLAYED. REMOVED AND REPLACED CONTROL MODULE ASSY IAW AMM 33-21-01 SUBTASK 33-25-00-700-801-A AND 33-50-00-700-801-A.
- [SDR HNAA2019042200111](https://openairdocs.org/sdr/HNAA2019042200111), Apr 20, 2019: BLEED VALVE. FAILED. PDIS 629 36-10 2048721 20APR19 PHL CLOSE BLD 2 VLV FAIL WHEN ENTERING ICING CONDITIONSFACT 20APR19 15:10 PHL R&R'D ENG BLEED VALVE 2 IAW EMB 145 AMM 36-11-05 OP
- [SDR HNAA2019041700102](https://openairdocs.org/sdr/HNAA2019041700102), Apr 16, 2019: INVERTER. FAILED. 629 33-51 0014160 16APR19 RIC CLOSE EMERGENCY LIGHT OVER SERVICE DOOR DOORWAY WILL NOT ILLUMINATE 27751 00 NGR FACT 16APR19 09:57 RIC DISCONNECTED EMERGENCY LIG
- [SDR HNAA2018120500304](https://openairdocs.org/sdr/HNAA2018120500304), Dec 2, 2018: DISPLAY. MALFUNCTIONED. DURING TAXI IN TO GATE. FO'S PFD WENT BLANK ALONG WITH ELECTRICAL ODOR. SELECTED AVIONICS BUSS 2 OFF. SWAPED FO'S PFD AND MFD PER AMM 34-22-01 AND DEACTIVATED M
- [SDR HNAA2018092800236](https://openairdocs.org/sdr/HNAA2018092800236), Sep 27, 2018: WIRE. CHAFED. DISCREPANCY: THE EMERGENCY LIGHTS CONNECTED TO THE #2 POWER SUPPLY DID NOT COME ON DURING OPS CHECK. CORRECTIVE ACTION: REMOVED CIELING PANEL IN FRONT OF GALLEY
- [SDR HNAA2018072500168](https://openairdocs.org/sdr/HNAA2018072500168), Jul 23, 2018: MODULE. MALFUNCTIONED. ABSENCE OF PRESSURIZATION INDICATIONS ON EICAS PANEL. DASH LINES IN BOXES. R&R CPAM, C/W OP AND ALT CK'S REF 21-32-01, C/W NR 3 STATIC SYSTEM LK CK. OK IAW TASK
- [SDR HNAA2018042000085](https://openairdocs.org/sdr/HNAA2018042000085), Apr 19, 2018: PITCH CONTROL. MALFUNCTIONED. MAIN PITCH TRIM IS INOPERATIVE. INSPECTED & OPERATED THE MAIN & B/U PITCH TRIM SWITCHES WITH NO FAULTS, COMPLIED WITH FIM 27-43-00-810-801-A, AND 27-43-810-802-
- [SDR HNAA2018011600009](https://openairdocs.org/sdr/HNAA2018011600009), Jan 15, 2018: WARNING MESSAGE. FALSE INDICATION. ICE CONDITION ADV MESSAGE DISPLAYED. ACFT WAS NOT IN ICING CONDITIONS. MESSAGE WENT OUT AT 13000 FEET AND CREW SMELLED SOMETHING BURNING. PERFORMED ICE DETECTIO
- [SDR HNAA2018011200005](https://openairdocs.org/sdr/HNAA2018011200005), Jan 11, 2018: DUCT. UNSECURE. RAPID DEPRESSURIZATION WHILE HOLDING SHORT IN AUTOMATIC MODE. MANUAL MODE OVER PRESSURIZED. INSPECTED THE NR 1 PACK AREA AND FOUND A DUCT LOOSE. SECURED THE DUC
- [SDR SIMA20171128003](https://openairdocs.org/sdr/SIMA20171128003), Nov 28, 2017: SKIN. DAMAGED. DURING POST INSPECTION WALK AROUND, FOUND A DENT AND SCRAPE UNDER CARGO DOOR. REPAIRED IAW ERS-EM-53MR-3025.
- [SDR SIMA20171117002](https://openairdocs.org/sdr/SIMA20171117002), Nov 17, 2017: CONTROL ROD. CORRODED. LEFT AND RIGHT, FORWARD AND AFT, FOUR MAIN LANDING GEAR DOOR CONTROL RODS ARE CORRODED. REMOVED AND REPLACED THE CONTROL RODS IAW AMM 32-10-06, STEPS 1, 5, & 9,
- [SDR SIMA20171109007](https://openairdocs.org/sdr/SIMA20171109007), Nov 9, 2017: ATTACH FITTING. WORN. INBOARD SPOILER FITTING ON REAR SPAR 3 HAS A WORN HAT BUSH BORE. REMOVED AND REPLACED INBD SPOILER ATTACH BRACKET (INCLUDED NEW HAT BUSHINGS) IAW AMM 57-51-02.
- [SDR SIMA20171108008](https://openairdocs.org/sdr/SIMA20171108008), Nov 8, 2017: ATTACH ANGLE. CRACKED. LEFT WING EIGHTH AFT LOWER ATTACH ANGLE FOR LATERAL PANEL IS CRACKED. INSTALLED A NEW ATTACH ANGLE IAW ETN-EM-53-142.
- [SDR SIMA20171108009](https://openairdocs.org/sdr/SIMA20171108009), Nov 8, 2017: ATTACH ANGLE. CRACKED. LEFT WING FIFTH AFT LOWER ATTACH ANGLE FOR LATERAL PANEL IS CRACKED. INSTALLED A NEW ATTACH ANGLE IAW ETN-EM-53-142 IAW NRTC E605570.
- [SDR SIMA20171108007](https://openairdocs.org/sdr/SIMA20171108007), Nov 8, 2017: ATTACH ANGLE. CRACKED. RIGHT WING THIRD AFT LOWER ATTACH ANGLE FOR LATERAL PANEL IS CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW ETN ER ETN-EM-53-142.
- [SDR SIMA20171107009](https://openairdocs.org/sdr/SIMA20171107009), Nov 7, 2017: SKIN PANEL. GOUGED. CENTER FUSELAGE UPPER SKIN PANEL BETWEEN FR 35-36 STRG 1R-3R GOUGES, PERMANENT REPAIR. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-2836.
- [SDR SIMA20171107008](https://openairdocs.org/sdr/SIMA20171107008), Nov 7, 2017: FRAME. CRACKED. COCKPIT LT FRAME 10 IS CRACKED, BELOW DV WINDOW. REMOVED AND REPLACED COCKPIT LT FRAME 10 SECTION BELOW DV WINDOW IAW SRM 51-40-02.
- [SDR SIMA20171107002](https://openairdocs.org/sdr/SIMA20171107002), Nov 7, 2017: ATTACH ANGLE. CRACKED. COCKPIT FRAME 10 ATTACH ANGLE AT TOP OF FRAME IS CRACKED. REMOVED AND REPLCED THE ATTACH ANGLE IAW SRM 51-40-02.
- [SDR SIMA20171107003](https://openairdocs.org/sdr/SIMA20171107003), Nov 7, 2017: FRAME. CRACKED. COCKPIT FRAME 10 IS CRACKED, BELOW WINDOW. REMOVED AND REPLACED THE FRAME IAW 51-40-02.
- [SDR SIMA20171107004](https://openairdocs.org/sdr/SIMA20171107004), Nov 7, 2017: CLEAT. CRACKED. COCKPIT LT FRAME 10 CLEAT IS CRACKED. -INSTALLED A NEW CLEAT IAW SRM 51-40-02.
- [SDR SIMA20171107005](https://openairdocs.org/sdr/SIMA20171107005), Nov 7, 2017: ATTACH ANGLE. CRACKED. COCKPIT LT FRAME 10 ATTACH ANGLE AT TOP OF FRAME IS CRACKED. INSTALLED A NEW ATTACH ANGLE IAW SRM 51-40-02.
- [SDR SIMA20171107006](https://openairdocs.org/sdr/SIMA20171107006), Nov 7, 2017: SUPPORT BRACKET. CRACKED. AFT CARGO DOOR FORWARD TORSION BAR SUPPORT BRACKET AT FRAME 61 CRACKED. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02.
- [SDR SIMA20171107007](https://openairdocs.org/sdr/SIMA20171107007), Nov 7, 2017: ATTACH ANGLE. CRACKED. LEFT WING SECOND AFT LOWER ATTACH ANGLE IS CRACKED IN SEVERAL PLACES. -INSTALLED A NEW ATTACH ANGLE IAW ETN-EM-53-142.
- [SDR SIMA20170927002](https://openairdocs.org/sdr/SIMA20170927002), Sep 27, 2017: A/C PACK. MALFUNCTIONED. NR 2 PACK OVERLOAD IN FLIGHT AT FL 250 WITH THE NR 1 PACK. REMOVED AND REPLACED THE RT PACK VALVE IAW AMM 21-51-01. OPS CHECK FAILED. OPEN
- [SDR SIMA20170824001](https://openairdocs.org/sdr/SIMA20170824001), Aug 24, 2017: LAMP. CRACKED. NR 1 LANDING LIGHT CRACKED. R & R THE LANDING LIGHT LAMP IAW AMM 33-41-02. OPS CHECKED OK.
- [SDR SIMA20170626003](https://openairdocs.org/sdr/SIMA20170626003), Jun 26, 2017: LIGHT. INOPERATIVE. LEFT OVERWING PANEL EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT OVERWING PANEL EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECK GOOD.
- [SDR ASOA20160609054](https://openairdocs.org/sdr/ASOA20160609054), Jun 9, 2016: CONNECTOR. DISCONNECTED. THE CREW REPORTED THAT THE FRONT DOOR EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE WHEN IN EMERGENCY LIGHT MODE. MAINTENANCE INSPECTED THE ACFT AND FOUND THAT THE S
- [SDR SIMA20150515006](https://openairdocs.org/sdr/SIMA20150515006), May 15, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED ON FRAME 75 AT THIRD FASTENER BELOW STRINGER 2R, EASI 8071 USED. FREQ=400KHZ, LPF=100, V-GAIN=76.0, H-GAIN=65.0, 50-500KHZ PROBE. PERFORME
- [SDR SIMA20150515005](https://openairdocs.org/sdr/SIMA20150515005), May 15, 2015: ACCESS DOOR. CRACKED. REAR ELECTRONICS ACCESS HATCH 272DR IS CRACKED UNDER EYELET BRACKET. REPAIRED IAW ERS-EM-52MR-334.
- [SDR SIMA20150514004](https://openairdocs.org/sdr/SIMA20150514004), May 14, 2015: SKIN. CHAFED. AIRLINE CAP RETENTION CABLE CHAFING INNER SKIN INSIDE 414DB. PERFORMED PERMANENT REPAIR OF AIR LINE CAP RETENTION CABLE CHAFING INNER SKIN INSIDE 414DB IAW ERS-
- [SDR SIMA20150514005](https://openairdocs.org/sdr/SIMA20150514005), May 14, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 3/8" IN LENGTH, EASI 8071 USED. FREQ=400KHZ, LPF=100, V-GAIN=76.0, H-GAIN=65.0, 
- [SDR SIMA20150511007](https://openairdocs.org/sdr/SIMA20150511007), May 11, 2015: WIRE. BROKEN. EMERGENCY LIGHT STRIP NR 3 HAS BROKEN WIRE ON LIGHT STRIP SIDE. R & R EMER LIGHT STRIP NR 3 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150511006](https://openairdocs.org/sdr/SIMA20150511006), May 11, 2015: CONNECTOR. DAMAGED. POWER SUPPLY HARNESS, ACFT SIDE, TO EMER LIGHT STRIP NR 6 HAS A DAMAGED CONNECTOR. INSTALLED CONNECTOR & PIN ON POWER SUPPLY HARNESS, ACFT SIDE, TO EMER LIGHT S
- [SDR SIMA20150511005](https://openairdocs.org/sdr/SIMA20150511005), May 11, 2015: CONNECTOR. MISSING. POWER SUPPLY HARNESS, ACFT SIDE, TO EMER LIGHT STRIP NR 4 IS MISSING A CONNECTOR. INSTALLED CONNECTOR & PIN ON POWER SUPPLY HARNESS, ACFT SIDE, TO EMER LIGHT ST
- [SDR SIMA20150511003](https://openairdocs.org/sdr/SIMA20150511003), May 11, 2015: WIRE. BROKEN. EMERGENCY LIGHT STRIP NR 2 HAS BROKEN WIRE ON LIGHT STRIP SIDE. EMER LIGHT STRIP NR 2 IS INOPERATIVE. R & R EMER LIGHT STRIP NR 2 IAW AMM 33-50-12. OPERATIONS C
- [SDR SIMA20150510010](https://openairdocs.org/sdr/SIMA20150510010), May 10, 2015: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHT STRIP NR 1 IS INOPERATIVE. R & R NR 2 BATTERY POWER SUPPLY & BATTERY PACK IAW AMM 33-50-04 & AMM 20-10-01. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150421015](https://openairdocs.org/sdr/SIMA20150421015), Apr 21, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 3/8" IN LENGTH. REPAIRED SKIN CRACK AT FRAME 75 & STRINGER 2L IAW ERS-EM-53MR-13

All 150: https://openairdocs.org/aircraft/N629AE/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/N629AE/stcs.md

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/aircraft.md
- The Allison AE3007C series engine: https://openairdocs.org/engine/allison-ae3007c-series.md

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