# N626AE: 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: 145117
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 20, 1999
- Certificate issued: September 28, 2011
- Expires: September 30, 2027
- Mode S code: A82C8C
- 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=626AE
- Page: https://openairdocs.org/aircraft/N626AE

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/N626AE/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 N626AE.

## FAA accident and incident reports

None matched to N626AE.

## Service difficulty reports (132, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR HNAA2022052500179](https://openairdocs.org/sdr/HNAA2022052500179), May 18, 2022: NONE. NONE. PDIS 626 36-11 2667913 18MAY22 RIC CLOSE DURING TAKE OFF HIGH STAGE 1 VALVE FAILURE OCCURRED FOLLOWED QRH AND FLEW BELOW FL 250, NO INDICATION ON EICAS AT THIS 
- [SDR HNAA2022052500178](https://openairdocs.org/sdr/HNAA2022052500178), May 18, 2022: NONE. NONE. PDIS 626 25-00 2667912 18MAY22 RIC CLOSE FIRST OFFICER PFD GOES BLANK SEVERAL TIMES IN FLIGHT FACT 18MAY22 01:37 RIC R/R FO PDF IAW AMM 34-22-00/400-801A. OPS C
- [SDR HNAA2022041400165](https://openairdocs.org/sdr/HNAA2022041400165), Apr 13, 2022: NONE. NONE. PDIS 626 30-42 2475971 13APR22 PHL CLOSE WINDSHIELD HEAT 2 FAIL DURING CLIMB. FACT 13APR22 11:08 PHL R/R W/S 2 TEMP CONTROLLER IAW EMB AMM 30-42-01. OPS CHECK G
- [SDR HNAA2022030700119](https://openairdocs.org/sdr/HNAA2022030700119), Mar 3, 2022: NONE. NONE. PDIS 626 36-11 2475521 03MAR22 PHL CLOSE ICING PROTECTION TEST FAIL 2 TIMES IN FLIGHT DONE THROUGH 18K FT WITH EICAS MESSAGES BLEED 2 VLV CLOSED AND BLEED 2 VLV
- [SDR HNAA2022020900070](https://openairdocs.org/sdr/HNAA2022020900070), Feb 8, 2022: NOT REPORTED. NOT REPORTED. PDIS 626 30-10 2530291 08FEB22 ALB CLOSE WING ANTI ICE FAIL MSG ON CLIMB-OUT FACT 08FEB22 13:50 ALB TROUBLESHOT WG A-ICE FAIL ON EICAS IAW EMB 145 FIM 30-11-00-
- [SDR HNAA2022011700054](https://openairdocs.org/sdr/HNAA2022011700054), Jan 16, 2022: NONE. NONE. PDIS 626 73-30 2530071 16JAN22 BTV CLOSE E2 FUEL LOW TEMP ON EICAS DURING T/O ROLL ENG TEMPS E1 50C AND E2C_ENG PRESSURE NORMAL FACT 16JAN22 03:57 BTV CREW PERF
- [SDR HNAA2021120600596](https://openairdocs.org/sdr/HNAA2021120600596), Dec 5, 2021: NONE. NONE. PDIS 626 36-11 2498141 05DEC21 CLT CLOSE ON T/O AROUND 60KTS, HS VALVE1 FAIL EICAS CAUTION MESSAGE FACT 05DEC21 18:07 CLT UPON ARRIVAL AT A/C NO FAIL MESSAGE WE
- [SDR HNAA2021052500226](https://openairdocs.org/sdr/HNAA2021052500226), May 23, 2021: BRAKE. MALFUNCTIONED. PDIS 626 32-44 2386091 23MAY21 PHL CLOSE PARKING BRAKE DOES NOT WORK WITH HANDLE ENGAGED. FACT 23MAY21 16:41 PHL INSPECTED PARKING BRAKE FOUND NO LEAKS AT ACCUM
- [SDR HNAA2021041900157](https://openairdocs.org/sdr/HNAA2021041900157), Apr 18, 2021: WIRE HARNESS. BROKEN. ON GEAR RETRACTION, GEAR INDICATED UP AND LOCKED WITH LOUD AIR RUSHING NOISE AND NOTICEABLE DRAG ON A/C. FOUND NLG HARNESS W014 BROKEN AT AFT CONNECTOR PLUG. R 
- [SDR HNAA2021041501550](https://openairdocs.org/sdr/HNAA2021041501550), Apr 14, 2021: WARNING MESSAGE. ILLUMINATED. PDIS 626 78-30 2443681 14APR21 ERI ASSGN E1 REV DISAGREE MSG ON EICAS .... MEL ASSIGNED - DEACTIVATED AND STOWED #1 T/R IAW AMM 78-31-01-980-801-A
- [SDR HNAA2021032900105](https://openairdocs.org/sdr/HNAA2021032900105), Mar 26, 2021: WARNING MESSAGE. FALSE INDICATION. ENG 1 REV DISAGREE UPON TL ADVANCE. DEACTIVATED I/A/W AMM 78-31-01-980-801-A NO. 1 T/R. FOLLOWED FIM TASK 78-30-00-810-802A. R/R ENG1 ICU IN REF TO AMM 78-33-01
- [SDR HNAA2021030800090](https://openairdocs.org/sdr/HNAA2021030800090), Mar 5, 2021: DAU. FAULTED. ENG 1 REV DISAGREE DISPLAYED ON EICAS. T/S ENG 1 REV DISAGREE MESSAGE IAW FIM 78-34-00-810-803-A. FOUND ENG1 T/R ICU VLV FAIL MESSAGE ON CMC. T/S IAW FIM 78-30-
- [SDR HNAA2021021500052](https://openairdocs.org/sdr/HNAA2021021500052), Feb 13, 2021: WARNING MESSAGE. FALSE ACTIVATION. PDIS 626 78-34 2356563 13FEB21 BGR CLOSE E1 REV DISAGREE MESSAGE AT 67% FACT 14FEB21 03:29 RIC DE-INHIBITED #1 T/R IN REF TO AMM 78-33-01-980-801A, SUBTASK 980-
- [SDR HNAA2020101200286](https://openairdocs.org/sdr/HNAA2020101200286), Oct 11, 2020: ELECTRONIC UNIT. FAILED. PDIS 626 32-60 2421192 11OCT20 ROA CLOSE ON GEAR EXTENSION. EICAS DISPLAYED LG AIR GROUND FAIL. DID NOT EXTINGUISH ON GROUND 29061 00 AR FACT 11OCT20 03:57 ROA.
- [SDR HNAA20200420144](https://openairdocs.org/sdr/HNAA20200420144), Apr 17, 2020: PROXIMITY SWITCH. UNSECURE. NR 1 ENGINE REVERSER DISAGREE MESSAGE ON TAKEOFF ROLL. FOUND 2 PROXIMITY SWITCHES IN NLG TO BE LOOSE. SECURED THE CONNECTORS IAW SWPM 20-50-00. OPS CHECKED GOOD
- [SDR HNAA2020042000143](https://openairdocs.org/sdr/HNAA2020042000143), Apr 17, 2020: CONNECTOR. LOOSE. PDIS 626 78-34 2222221 17APR20 PHL CLOSE E-1 REV DISAGREE MESSAGE ON TAKEOFF ROLL. 28574 00 PCS FACT 17APR20 23:17 ALB FOUND 2 PROX SWITCHES IN NLG TO BE LOOSE.
- [SDR HNAA2020041400133](https://openairdocs.org/sdr/HNAA2020041400133), Apr 13, 2020: SWITCH. WORN. PDIS 626 78-34 2222182 13APR20 ROC CLOSE ENG 1 TR REV DISAGREE EICAS MSG ILLUMINATED ON TAKEO FF ROLL MAX SPEED 70 KNOTS. MEL 13APR20 18:46 ROC C10428 78-2 ENG 
- [SDR HNAA2020041300131](https://openairdocs.org/sdr/HNAA2020041300131), Apr 10, 2020: CONNECTOR. DISCONNECTED. COCKPIT AND MAIN ENTRY OVERHEAD EMERGENCY LIGHTS INOP. DROPPED MAIN DOOR REGION CEILING PANEL AND FOUND EMERGENCY COURTESY LIGHT CANNON PLUG NOT CONNECTED. RECO
- [SDR HNAA2020041300130](https://openairdocs.org/sdr/HNAA2020041300130), Apr 10, 2020: CONNECTOR. DISCONNECTED. FWD EMERGENCY EXIT LIGHT ABOVE FLIGHT ATTENDANT SEAT INOP. DROPPED MAIN DOOR REGION CEILING PANEL AND FOUND EMERGENCY COURTESY LIGHT CANNON PLUG NOT CONNECTED. 
- [SDR HNAA2020032700107](https://openairdocs.org/sdr/HNAA2020032700107), Mar 25, 2020: SOLENOID VALVE. FAULTY. PDIS 626 32-20 2287501 25MAR20 MDT CLOSE NOSE GEAR DOOR OPENED AFTER GEAR RETRACTION. 30784 00 SMK FACT 25MAR20 17:32 MDT RNR NLG SOLENOID VALVE IAW 32-33-02. O
- [SDR HNAA2020021700067](https://openairdocs.org/sdr/HNAA2020021700067), Feb 16, 2020: WARNING MESSAGE. ILLUMINATED. PDIS 626 78-33 2287121 16FEB20 PHL ASSGN E1 REVERSE DISAGREE EICAS MESSAGE SYSTEM IS CURRENTLY ON THE MEL
- [SDR HNAA2020021100053](https://openairdocs.org/sdr/HNAA2020021100053), Feb 8, 2020: WARNING MESSAGE. FALSE INDICATION. E1 REV DISAGREE ON TAKEOFF ROLL AND FOLLOWED BY NO TAKE OFF CONFIG. PERFORMED TAKE OFF CONFIG TEST OPS NORMAL. PERFORMED HIGH POWER RUN NO DEFECTS OR MESSAGES O
- [SDR HNAA2020021100052](https://openairdocs.org/sdr/HNAA2020021100052), Feb 8, 2020: DAU. MALFUNCTIONED. E1 REV DISAGREE MSG DURING TAKEOFF (ABORTED TAKEOFF) PER FIM 78-30-810-814-A TASK 3, REMOVED AND REPLACED DAU1 PER EMB 145 AMM 31-41-00. OPS CHECK GOOD. AIRCRAF
- [SDR HNAA2020020700047](https://openairdocs.org/sdr/HNAA2020020700047), Feb 5, 2020: CONNECTOR. DIRTY. E1 T/R DISAGREE MESS DISPLAYED DURING T/O(ABORTED T/O)....FIX:MELD ENG1(2) REV DISAGREE MESS FOLLOW UP, PHL, 06FEB20, CLEANED CONNECTOR PLUGS ASSOCIATED WITH IC
- [SDR HNAA2020010600011](https://openairdocs.org/sdr/HNAA2020010600011), Jan 3, 2020: BLEED VALVE. FAILED. PDIS 626 36-11 2132151 03JAN20 ORF CLOSE BLEED 2 VLV FAIL EICAS MSG, WING A/ICE FAIL, AND ICE COND A/ICE INOP. ALL MSGS CLEARED OUT OF ICING. BLE ED 2 CLOSED RE
- [SDR HNAA2020010300001](https://openairdocs.org/sdr/HNAA2020010300001), Jan 2, 2020: WARNING MESSAGE. FALSE ACTIVATION. E1 REV DISAGREE MSG ON TAKE OFF....FIX: PERFORMED OPS CHECK OF T/R IN REF TO AMM 78-31-01-700-801A. CND FAILURE.OK FOR SERVICE, NO HISTORY 90 DAYS
- [SDR HNAA2019120460345](https://openairdocs.org/sdr/HNAA2019120460345), Oct 29, 2019: SKIN. DAMAGED. COULD NOT LOCATE ORIGINAL - FUSELAGE SKIN HAS A BURN MARK AT FR63 BETWEEN STR 20R-21R.....INSTALLED FILLER AND REPAIR DOUBLER IAW EMB 145 SRM 53-31-01, ITEM 4, 
- [SDR HNAA2019110600347](https://openairdocs.org/sdr/HNAA2019110600347), Oct 28, 2019: YOKE. CRACKED. RH PYLON FWD LWR YOKE FIXTURE HAS POSSIBLE CRACK....FIX: REMOVED AND REPLACED RH PYLON FWD LWR YOKE IAW PIEDMONT EO1-54-19-0495. NOTE: A/C IN ABI HVY CHECK
- [SDR HNAA2019110600346](https://openairdocs.org/sdr/HNAA2019110600346), Oct 28, 2019: STRUCTURE. CRACKED. CARGO DOOR HANDLE CUT-OUT CRACKED AT AFT END, MARKED....FIX: ACCOMPLISHED REPAIR OF CARGO DOOR HANDLE CUT-OUT CRACK IAW PIEDMONT EO1-52-19-0488. NOT: A/C IN ABI
- [SDR HNAA2019110600344](https://openairdocs.org/sdr/HNAA2019110600344), Oct 28, 2019: DOOR FRAME. CORRODED. CARGO DOOR INTERIOR WEB FRAME LWR CORNER N/P HOLE HAS CORROSION....FIX:N/P HOLE CORROSION REPAIRED IAW PIEDMONT EO1-52-19-0498. A/C IN ABI HVY CHECK
- [SDR HNAA2019111400357](https://openairdocs.org/sdr/HNAA2019111400357), Oct 11, 2019: FIREWALL. CRACKED. APU FIREWALL IS CRACKED AT THE LEFT LWR MOUNT....FIX: PERFORMED REPAIR TO APU FIREWALL LEFT LWR MOUNT AREA IAW EMB SRM 53-32-13 FIG 202 AND EO1-53-19-0499. NOTE
- [SDR HNAA2019110600348](https://openairdocs.org/sdr/HNAA2019110600348), Oct 11, 2019: DOOR SILL. CORRODED. SERVICE DOOR CENTER SILL HAS AREAS OF CORROSION....FIX:REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB 145 SRM 51-40-02. NOTE: A/C IN ABI HVY CHCK
- [SDR HNAA2019111400358](https://openairdocs.org/sdr/HNAA2019111400358), Oct 10, 2019: NUT PLATE. MISSING. RUDDER 2 PROTACTOR ATTACH POINT NUT PLATE IS MISSING....FIX: PERFORMED INTERNAL DOUBLER REPAIR IAW EO1-55-19-0494. NOTE:A/C IN HVY CHK (ABI)
- [SDR HNAA2019111400356](https://openairdocs.org/sdr/HNAA2019111400356), Oct 10, 2019: FRAME. CRACKED. FRAME 81 LWR HALF HAS A CRACK....FIX: R&RD FRAME 81 LWR HALF IAW EMB 145 SRM 51-40-02. NOTE: A/C IN HVY CHK (ABI)
- [SDR HNAA2019111400355](https://openairdocs.org/sdr/HNAA2019111400355), Oct 10, 2019: FIREWALL. CRACKED. APU FIREWALL CRACKED AT RH SUPPORT ROD....FIX: REPAIRED APU FIREWALL AT THE RH SUPPORT IAW EMG SRM 53-32-13 AND EO1-53-19-0499. NOTE: A/C IN ABI UNDER HVY CHK
- [SDR HNAA2019091300269](https://openairdocs.org/sdr/HNAA2019091300269), Sep 12, 2019: WARNING SYSTEM. FALSE ACTIVATION. PDIS 626 78-32 1830691 12SEP19 CLT CLOSE E1 T/R DISAGREE MSG DISPLAYED ON TAKEOFF ROLL. C/W MX PROCEDURE. NOTE CMC SHOWS E1 T/R VALVE FAIL. FACT 13SEP19 01:07 M
- [SDR HNAA2019060700162](https://openairdocs.org/sdr/HNAA2019060700162), Jun 5, 2019: SLEEVE. TORN. BLEED 2 LEAK EICAS MSG WITH SWITCH ANNUNCIATOR ILLUMINATED.RAN QRH LIGHT EXTINGUISHED.FIX: INSPECTED AND FOUND ORANGE SLEEVE RIPPED AT #2 AC PACK, REPLACED SLEE
- [SDR HNAA2018100200238](https://openairdocs.org/sdr/HNAA2018100200238), Sep 29, 2018: SLEEVE. LEAKING. PDIS 626 36-21 1299531 29SEP18 PHL CLOSE NR 1 BLEED LEAK ON CLIMB OUT THROUGH 5000 FT . RAN QRH INDICATION WENT OUT AFTER 1.5 MINUTES. BOTH PACKS RUNNING AT TIM
- [SDR HNAA2018082400207](https://openairdocs.org/sdr/HNAA2018082400207), Aug 22, 2018: BATTERY PACK. INOPERATIVE. NDIS 626 33-51 0009560 22AUG18 RIC CLOSE AFT CEILING EMERGENCY LIGHT DOES NOT ILLUMINATE 28916 00 NGR FACT 22AUG18 09:19 RIC R/R #4 BATTT IAW EMB-145 AMM 33-50-
- [SDR HNAA2018070600142](https://openairdocs.org/sdr/HNAA2018070600142), Jul 5, 2018: BATTERY. MALFUNCTIONED. SMOKE ODOR IN PLANE, WHEN RECIRC FAN TURNED OFF, SMELL WENT AWAY. OPS CHECK RECIRC FAN WITH NO DEFECTS NOTED. INSP CABIN & FOUND AFT CABIN FLASHLIGHT BATTERIES 
- [SDR HNAA2018011700010](https://openairdocs.org/sdr/HNAA2018011700010), Jan 16, 2018: EXTINGUISHER. FAILED. DURING A FAILED APU START, THE CARGO BAY SMOKE BUTTON ILLUMINATED, FOLLOWED BY A CARGO EXTINGUISHER BOTTLE INOPERATIVE. THEN LIGHTS WENT OUT EXCEPT THE CARGO EX
- [SDR HNAA2017082800293](https://openairdocs.org/sdr/HNAA2017082800293), Aug 27, 2017: WARNING MESSAGE. ILLUMINATED. STEERING INOPERATIVE MASSAGE ILLUMINATED ON TAKEOFF ROLL BETWEEN 40 - 50 KTS.
- [SDR HNAA2017081100269](https://openairdocs.org/sdr/HNAA2017081100269), Aug 10, 2017: HYDRAULIC SYSTEM. LOW. HYDRAULIC SYSTEM NR 1, LOW QUANTITY EICAS MESSAGE APPEARED IN FLIGHT, HYDRAULIC QUANTITY WAS IN THE AMBER RANGE. SERVICED THE NR 1 HYD SYS IAW MM 12-13-01. OK F
- [SDR HNAA2017072500249](https://openairdocs.org/sdr/HNAA2017072500249), Jul 24, 2017: WARNING LIGHT. FALSE ACTIVATION. ABORTED TAKEOFF AT 60 KNOTS DUE TO A LOUD WHINING NOISE FOLLOWED BY A NO TAKEOFF CONFIGURATION WARNING LIGHT ILLUMINATING. AIRCRAFT HAS EXCESSIVE PULL TO THE LE
- [SDR SIMA20170417006](https://openairdocs.org/sdr/SIMA20170417006), Apr 17, 2017: SKIN. CRACKED. EXTERNAL FUSELAGE SKIN POSSIBLE CRACK AROUND FASTENER FR 78 STR 3L-4L. PREPPED, FABRICATED, DRILLED FILLERS (3 TOTAL) AND INSTALLED EXTERNAL FUSELAGE SKIN REPAI
- [SDR SIMA20170417007](https://openairdocs.org/sdr/SIMA20170417007), Apr 17, 2017: FRAME. CRACKED. FR 66 AT STR 16R HAS POSSIBLE CRACK ABOVE UPPER END OF SHEAR CLIP. REPAIRED FR 66 AT STR 16R ABOVE UPPER END OF SHEAR CLIP IAW ERS-EM-53MR-2706.
- [SDR SIMA20170417008](https://openairdocs.org/sdr/SIMA20170417008), Apr 17, 2017: SKIN. CRACKED. RT AFT FUSELAGE SKIN HAS CRACK AT CUT OUT FR 77 BELOW STR 7. PERFORMED PERMANENT REPAIR OF SKIN CRACK AT FR77 BELOW STR 7R IAW ERS-EM-53MR-2724.
- [SDR SIMA20170417005](https://openairdocs.org/sdr/SIMA20170417005), Apr 17, 2017: SPAR. CRACKED. RT WING SPAR 1 LOWER FLANGE IS CRACKED AT FIRST SCREW HOLE OUTBOARD OF RIB 9, FROM AFT SIDE OF HOLE REARWARD ALMOST TO RADIUS OF SPAR WEB. REPAIRED CRACK ON RT 
- [SDR SIMA20170417004](https://openairdocs.org/sdr/SIMA20170417004), Apr 17, 2017: WIRE. DAMAGED. EMERGENCY LIGHT EXIT SIGN ON THE CEILING PANEL 233BLC INOP. REPAIRED WIRE ON EMERGENCY LIGHT EXIT SIGN ON THE CEILING PANEL 233BLC IAW SWPM 20-21-00. OPS CHECK 
- [SDR SIMA20170401003](https://openairdocs.org/sdr/SIMA20170401003), Apr 1, 2017: ANTI-ICE VALVE. FAILED. HIGH SPEED ABORT PERFORMED AT APPROX 80 KTS DURING TO ROLL. RECEIVED AN ENGINE A/I DISAGREE CAUTION AND AN NR 2 ENGINE OPEN INSCRIPTION WITH ANTI-ICE OVERRIDE I

All 132: https://openairdocs.org/aircraft/N626AE/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/N626AE/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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