# N627AE: 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: 145121
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 11, 1999
- Certificate issued: September 8, 2011
- Expires: September 30, 2027
- Mode S code: A83043
- 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=627AE
- Page: https://openairdocs.org/aircraft/N627AE

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/N627AE/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 N627AE.

## FAA accident and incident reports

None matched to N627AE.

## Service difficulty reports (148, 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 HNAA2022120600314](https://openairdocs.org/sdr/HNAA2022120600314), Dec 3, 2022: INDICATOR. FAULTED. NR 2 ENGINE FUEL IMPENDING BYPASS EICAS MESSAGE. ACCOMPLISHED MNT. PROC.APP1 73-4FUEL IMP BYP ADV MSG. AS A PRECAUTION, R & R FUEL FILTER IRT RREM 73-21-10-000/
- [SDR HNAA2022042600174](https://openairdocs.org/sdr/HNAA2022042600174), Apr 25, 2022: NONE. NONE. PDIS 657 27-36 2473951 25APR22 CLT CLOSE REJECTED TAKEOFF AT APPROX 100KTS FOR SPS 1 INOP WARNING MESSAGE. 24741 00 AD FACT 26APR22 02:00 CLT R&R'D #1 AOA IAW A
- [SDR HNAA2022013100058](https://openairdocs.org/sdr/HNAA2022013100058), Jan 29, 2022: NOT REPORTED. NOT REPORTED. PDIS 627 34-22 2753131 29JAN22 CLT CLOSE IN FLIGHT FO'S PFD LOST ATT IND WITH ALL NUMBERS SHOWING RED. SELECTED AHRS REVERSION NO CHANGE. SWITCHED REVERSION KNO
- [SDR HNAA2021120800599](https://openairdocs.org/sdr/HNAA2021120800599), Dec 7, 2021: NONE. NONE. PDIS 627 21-31 2596072 07DEC21 PHL CLOSE ON CLIMB OUT AIRCRAFT WOULD NOT PRESSURIZE. RESET DUMP SWITCH ON GROUND. FACT 07DEC21 11:02 PHL FOUND PRESSURE CONTROLL
- [SDR HNAA2021120800598](https://openairdocs.org/sdr/HNAA2021120800598), Dec 6, 2021: NONE. NONE. PDIS 627 34-41 2596061 06DEC21 ALB CLOSE AT FL310 GPWS INOP AND WINDSHEAR INOP DISPLAYED ON EICAS. FACT 07DEC21 03:19 ALB FOUND LOOSE COAXIAL CONNECTORS ON RADI
- [SDR HNAA2020121700374](https://openairdocs.org/sdr/HNAA2020121700374), Nov 30, 2020: SKIN. DENTED. DENT ON FUSELAGE SKIN BETWEEN FR 22-23 AND BETWEEN STR 12L-13L. INSTALLED AND EDGE SEALED SERVICEABLE REPAIR DOUBLER AND FILLER ON FUSELAGE SKIN BETWEEN FR 22-2
- [SDR HNAA2020121700368](https://openairdocs.org/sdr/HNAA2020121700368), Nov 23, 2020: FRAME. CRACKED. FRAME 66 IS CRACKED AT CARGO DOOR CENTER SILL. PERFORMED REPAIR AT FR 66 BETWEEN STGR 20-L 21-L, IAW EO1-53-20-0436.
- [SDR HNAA2020121700367](https://openairdocs.org/sdr/HNAA2020121700367), Nov 18, 2020: TRUNNION. CRACKED. PERFORMED HFEC INSPECTION, IAW EASI NDTM RELEVANT INDICATION NOTED ON RT MLG AFT TRUNNION. ET EASI 8958 SETTINGS: FREQ. 400KHZ, ANGLE 291.1 DEG. H-61.3DB. V-77.
- [SDR HNAA2020121700366](https://openairdocs.org/sdr/HNAA2020121700366), Nov 17, 2020: FLOOR SUPPORT. CORRODED. CABIN CENTER OMEGA BEAM NR 4 HAS AREAS OF CORROSION. REPAIRED CABIN CENTER OMEGA BEAM NR 4 CORROSION, IAW PIEDMONT EO1-53-20-0431.
- [SDR HNAA2020121700365](https://openairdocs.org/sdr/HNAA2020121700365), Nov 17, 2020: FLOOR SUPPORT. CORRODED. CABIN LT OMEGA BEAM NR 6 HAS AREAS OF CORROSION. REPAIRED CABIN LT OMEGA BEAM NR 6 CORROSION, IAW EO1-53-20-0430.
- [SDR HNAA2020121700364](https://openairdocs.org/sdr/HNAA2020121700364), Nov 15, 2020: FITTING. WORN. RT AILERON TO PCA FITTING OUTBOARD LUGS WORN. REMOVED AND REPLACED RT AILERON TO PCA FITTING, IAW EMB 145 SRM 51-40-02, AMM 20-10-01.
- [SDR HNAA2020121700363](https://openairdocs.org/sdr/HNAA2020121700363), Nov 12, 2020: SKIN. CHAFED. BLENDED CHAFE ON CARGO DOOR INNER SKIN AT HB4 AND VB3 FOUND TO BE OUT OF LIMITS, REQUIRES REPAIR REFERENCE EMB 145 SRM 52-30-01 ITEM 12. REPAIRED BLENDED CHAFE 
- [SDR HNAA2020121700373](https://openairdocs.org/sdr/HNAA2020121700373), Nov 11, 2020: DOOR SILL. CORRODED. CARGO DOOR FUSELAGE SILL HAS NUMEROUS CORROSION SPOTS. R & R CARGO DOOR LOWER CENTER SILL, IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2020121700372](https://openairdocs.org/sdr/HNAA2020121700372), Nov 11, 2020: FRAME. CHAFED. FR 70 BETWEEN STR 12R-13R IS CHAFED. REPAIRED FR 70 BETWEEN STR 12R-13R, IAW EO1-53-20-0428.
- [SDR HNAA2020121700371](https://openairdocs.org/sdr/HNAA2020121700371), Nov 11, 2020: STOP FITTING. CORRODED. LT CABIN EMERGENCY EXIT LOWER EDGE ROUND STOP HAS CORROSION AROUND THE BASE. REMOVED CORRODED NR 4 BEAM, POSITIONED, DRILLED AND INSTALLED SERVICEABLE NR 4 BEAM
- [SDR HNAA2020121700362](https://openairdocs.org/sdr/HNAA2020121700362), Nov 11, 2020: BRACKET. CORRODED. SSI 53-30-48 CARGO DOOR CUTOUT FWD LOWER CORNER L-SHAPE BRACKET HAS SURFACE CORROSION. REPAIRED CARGO DOOR CUTOUT FWD LOWER CORNER L-SHAPE BRACKET CORROSION, IA
- [SDR HNAA2020121700370](https://openairdocs.org/sdr/HNAA2020121700370), Nov 10, 2020: RIB. CRACKED. RT WING RIB 21 IS CRACKED INSIDE PANEL 651CB. REPAIRED RT WING RIB 21 CRACK INSIDE PANEL 651CB, IAW PIEDMONT EO1-57-20-0433.
- [SDR HNAA2020121700369](https://openairdocs.org/sdr/HNAA2020121700369), Nov 10, 2020: RIB. CRACKED. LT WING RIB 21 IS CRACKED IN 2 AREAS INSIDE 551CB. REPAIRED LT WING RIB 21 CRACKED IN 2 AREAS INSIDE 551CB, IAW PIEDMONT EO1-57-20-0434.
- [SDR HNAA2020062200171](https://openairdocs.org/sdr/HNAA2020062200171), Jun 21, 2020: WARNING MESSAGE. FALSE ACTIVATION. MASTER WARNING LDG DISAGREE ON TAKE OFF. MAINTENANCE: FOLLOWED FIM TASK 32-32-00-810-803-A UP TO BLOCK DIAGRAM STEP 22 AND FOUND TO BE TRANSITORY CONDITION OF T
- [SDR HNAA2020020500045](https://openairdocs.org/sdr/HNAA2020020500045), Feb 4, 2020: CONTROLLER. FAILED. W/S HEAT 1 FAILED INTERMITTENTLY OUTSIDE OF ICING CONDITIONS. REMOVED AND REPLACED WINDSHEILD #1 TEMP CONTROLLER. OPS CHECK GOOD AT THIS TIME, REF AMM 30-42-01.
- [SDR HNAA2019110200336](https://openairdocs.org/sdr/HNAA2019110200336), Oct 30, 2019: WARNING SYSTEM. FALSE ACTIVATION. BLD 1 VLV FAIL,PACK 1 FAIL, WG A/ICE FAIL, STAB ICE FAIL, ICE COND A/ICE FAIL ON TAXI.....FIX: OPS CHECK OF ENG BLEED AND A/ICE SYSTEM C/W. NO DEFECTS.CND. REF 
- [SDR HNAA2019102800329](https://openairdocs.org/sdr/HNAA2019102800329), Oct 27, 2019: UNKNOWN. ODOR. MDIS 627 21-01 1898121 27OCT19 PHL CLOSE STRONG BURNING ODOR IN FLT COMPARTMENT DURING FLIGHT , NO ABNORMAL INDICATIONS OR EICAS MSGS FACT 27OCT19 16:50 PHL RAN
- [SDR HNAA2019071700196](https://openairdocs.org/sdr/HNAA2019071700196), Jul 15, 2019: CLAMP. LOOSE. BLEED 2 LEAK WARNING IN FLIGHT. FIX: RETIGHTENED FWD V-BAND CLAMP ON #2 ENG BLEED VALVE IN PYLON. RAN ENG 2 PLUS BLEED 2 FOR 30 MIN LEAK CHECK GOOD. OK FOR SERV
- [SDR HNAA2019041500101](https://openairdocs.org/sdr/HNAA2019041500101), Apr 12, 2019: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS BATTERY INOPERATIVE. REMOVED AND REPLACED THE BATTERY IAW WORKCARD 33-70-19, OK FOR SERVICE.
- [SDR HNAA2018080200179](https://openairdocs.org/sdr/HNAA2018080200179), Jul 30, 2018: VANE. OUT OF ALIGNMENT. SPS ADVANCED DISPLAYED ON EICAS AFTER TAKEOFF, AND WENT AWAY AT TOUCHDOWN. ALIGNED AOA VANES AND PERFORMED OPS CK IAW 27-36-00. OPS CHECK GOOD.
- [SDR HNAA2018041800084](https://openairdocs.org/sdr/HNAA2018041800084), Apr 17, 2018: DOOR SILL. CORRODED. CARGO DOOR SILL HAS SEVERAL SPOTS OF CORROSION BETWEEN FRAMES 65 AND 68. REMOVE AND REPLACED THE CARGO DOOR SILL IAW SRM 51-40-02, AND EO1-53-18-0113.
- [SDR RAIA201803100001](https://openairdocs.org/sdr/RAIA201803100001), Mar 10, 2018: DOOR SILL. CORRODED. SERVICE DOOR CENTER SILL HAS MULTIPLE AREAS OF CORROSION. R & R SERVICE DOOR SILL.
- [SDR HNAA2017022000057](https://openairdocs.org/sdr/HNAA2017022000057), Feb 17, 2017: SWITCH. SHORTED. RAN QRH FOR A LEAK EICAS MESSAGE INFLIGHT AT 10000 FT. MESSAGE DID NOT EXTINGUISH. ALSO HAD A NR 2 BLEED VALVE CLOSED MESSAGE. INSPECTED AND FOUND GROUND AIR TE
- [SDR HNAA2016121200384](https://openairdocs.org/sdr/HNAA2016121200384), Dec 11, 2016: ANTI-ICE VALVE. MALFUNCTIONED. DURING ANTI-ICE SYSTEM TEST, THE WING ANTI-ICE FAILED EICAS MESSAGE ACTIVATED. REMOVED AND REPLACED RT WING ANTI-ICE VALVE IAW AMM 30-11-01 AND TIGHTENED DAMPER
- [SDR HNAA2016112300360](https://openairdocs.org/sdr/HNAA2016112300360), Nov 23, 2016: WARNING MESSAGE. FALSE ACTIVATION. NR 1 ENGINE FIRE DETECTOR FAILED CAUTION MESSAGE ILLUMINATED IN FLIGHT. EXTINGUISHED PRIOR TO LANDING. CREW SHUT DOWN ENGINE DURING TAXI IN. CREW REPORTED NO FI
- [SDR HNAA2016061500178](https://openairdocs.org/sdr/HNAA2016061500178), Jun 14, 2016: WARNING MESSAGE. FALSE ACTIVATION. FWA CLOSE SPOILER FAIL EICAS MESSAGE ON TAXI MESSAGE EXTINGUISHED AFTER 30 SECONDS. FLAPS WERE AT 9 DEGREES. INSPECTED AND FOUND TO BE TRANSITORY CONDITION OF T
- [SDR HNAA2016060700167](https://openairdocs.org/sdr/HNAA2016060700167), Jun 6, 2016: WIRE. BURNED. WIRE W102-0268-16 IS BURNED BETWEEN PINS C2 RELAY K0058 AND C1 RELAY K1237 ON NR 3 PITOT. STATIC HEATING SYS. REPLACED WIRE W102-0268-16 BETWEEN PINS C2 RELAY K
- [SDR HNAA2016041500105](https://openairdocs.org/sdr/HNAA2016041500105), Apr 13, 2016: UNKNOWN. ODOR. CREW REPORTS ODOR FROM LT ELECTRICAL DISTRIBUTION PANEL AREA. INSPECTED ELECTRICAL DISTRIBUTION PANEL AREA AND ASSOCIATED WIRING C/N/D AFTER POWERING UP SEVERAL
- [SDR HNAA2016041200100](https://openairdocs.org/sdr/HNAA2016041200100), Apr 8, 2016: UNKNOWN. ODOR. APU RUNNING, WITH NR 2 ENGINE BLEEDS ON 30 SEC LATER STRONG ODOR IN FLIGHT DECK AND FWD CABIN SHUTOFF BLEEDS AND RECIRCULATING FAN ODOR DISSAPATED. GROUND RAN A
- [SDR HNAA2016022900066](https://openairdocs.org/sdr/HNAA2016022900066), Feb 27, 2016: WARNING MESSAGE. FALSE ACTIVATION. CLOSE EICAS MESSAGE DISPLAYED E2 NO DISPLAY. INSPECTED ACFT FOR CODES ON IAW AMM 45-45-00. NO CODES FOUND. POWERED ACFT DOWN & UP. EICAS MESSAGE CLEARED. ACFT O
- [SDR SIMA20150922005](https://openairdocs.org/sdr/SIMA20150922005), Sep 22, 2015: DOUBLER. DAMAGED. DURING MBV INSPECTION, QA FOUND A PREVIOUS BLENDED AREA AT FWD EDGE OF THE CARGO DOOR OPENING. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURN
- [SDR SIMA20150922004](https://openairdocs.org/sdr/SIMA20150922004), Sep 22, 2015: SKIN. CRACKED. DURING MBV INSPECTION, QA FOUND 1 CRACK ON LT REAR FUSELAGE I SKIN JUST AFT OF FRAME 75 ABOVE STRINGER 2L. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WI
- [SDR SIMA20150918003](https://openairdocs.org/sdr/SIMA20150918003), Sep 18, 2015: SKIN. CHAFED. DURING MBV INSPECTION, QA FOUND THE FUSELAGE SKIN CHAFED INSIDE LT PYLON PANEL 414DB. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SER
- [SDR SIMA20150918002](https://openairdocs.org/sdr/SIMA20150918002), Sep 18, 2015: SKIN. CRACKED. DURING MBV INSPECTION, QA FOUND 1 CRACK ON RT REAR FUSELAGE I SKIN, JUST AFT OF FRAME 75 ABOVE STRINGER 2R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND
- [SDR SIMA20150915003](https://openairdocs.org/sdr/SIMA20150915003), Sep 15, 2015: FITTING. CRACKED. DURING MBV INSPECTION, QA FOUND PAX DOOR REINFORCEMENT FITTING CRACKED AT FRAME 20 & STRINGER 3L. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RET
- [SDR SIMA20150908005](https://openairdocs.org/sdr/SIMA20150908005), Sep 8, 2015: HINGE FITTING. WORN. DURING MBV INSPECTION, QA FOUND RUDDER I LOWER HINGE FITTING WORN. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSP
- [SDR SIMA20150831011](https://openairdocs.org/sdr/SIMA20150831011), Aug 31, 2015: BATTERY. DISCHARGED. EMERGENCY FLOOR LIGHTS 1 - 3 INOPERATIVE. R & R NR 2 EMER BATTERY ASSEMBLY IAW AMM 33-50-04. CHECKED GOOD.
- [SDR SIMA20150723007](https://openairdocs.org/sdr/SIMA20150723007), Jul 23, 2015: FLASHLIGHT. INOPERATIVE. FIRST OFFICER`S FLASHLIGHT INOPERATIVE. R & R FIRST OFFICER`S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.
- [SDR SIMA20150708005](https://openairdocs.org/sdr/SIMA20150708005), Jul 8, 2015: LIGHT. INOPERATIVE. AFT EMERGENCY LIGHT STRIP FOUND INOPERATIVE. LIGHT R & R IAW AMM 33-50-12. OPS CHECKED GOOD.
- [SDR SIMA20150626002](https://openairdocs.org/sdr/SIMA20150626002), Jun 26, 2015: BRAKE. LEAKING. LEFT SIDE INBD BRAKE LEAKING HYD FLUID. TIGHTENED UPPER FWD CAP ON NR 2 BRAKE ASSEMBLY IAW AMM 32-49-03. LEAK CHECKED GOOD.
- [SDR SIMA20150617002](https://openairdocs.org/sdr/SIMA20150617002), Jun 17, 2015: HOLDER. BROKEN. CAPTAINS FLASHLIGHT HOLDER BROKEN. DEFERRED IAW MEL 25-53. COMPLIED WITH MX PROCEDURES. R & R CAPTAINS FLASHLIGHT HOLDER IAW AMM 33-50-16. OPERATIONS CHECKED GO
- [SDR SIMA20150522001](https://openairdocs.org/sdr/SIMA20150522001), May 22, 2015: FAN. FAILED. JUST AFTER PUSHBACK, FLIGHT ATTENDANT CALLED WITH SMOKE IN CABIN, FINE MIST OF SMOKE, HOT AIR AT FLOW VENT OF ROW 5A. FLIGHT ATTENDANT REPORTED GRINDING NOISE A
- [SDR SIMA20141209004](https://openairdocs.org/sdr/SIMA20141209004), Dec 9, 2014: WIRE. DAMAGED. STAB ANTI-ICE FAIL DURING CLIMB. CHECKLIST PERFORMED, MSG REMAINED. TRANSFERRED TO NRWC 627-ABI-02170. REPAIRED WIRE W311-0031-22N & W311-0030-22 IAW SWPM 20-21
- [SDR SIMA20141206001](https://openairdocs.org/sdr/SIMA20141206001), Dec 6, 2014: SWITCH. MALFUNCTIONED. ON ILS APPROACH AP ON AT LOC CAPTURE AUTO PILOT COMMANDED & UNCOMMANDED TO & GA. FD STILL COMMANDED TO & GA WITH AP DISCONNECTED. ON CLIMB OUT WHEN SPEED MODE S
- [SDR SIMA20141114003](https://openairdocs.org/sdr/SIMA20141114003), Nov 14, 2014: BATTERY. DISCHARGED. OVERWING EXTERNAL EMER LIGHTS WILL NOT ILLUMINATE. R & R NR 4 EMER LIGHT BATTERY & CHARGER ASSEMBLY IAW WORK CARD 33-700-19. OPERATIONS CHECKED GOOD IAW WORK CA

All 148: https://openairdocs.org/aircraft/N627AE/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/N627AE/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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