# N624AE: 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: 145111
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 27, 1999
- Certificate issued: September 28, 2011
- Expires: September 30, 2027
- Mode S code: A8251E
- 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=624AE
- Page: https://openairdocs.org/aircraft/N624AE

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/N624AE/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 N624AE.

## FAA accident and incident reports

None matched to N624AE.

## Service difficulty reports (147, 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 HNAA2022062300227](https://openairdocs.org/sdr/HNAA2022062300227), Jun 22, 2022: ANTI-ICE SYSTEM. FAILED. WING ANTI ICE FAIL IN ICING CONDITIONS. PERFORMED OPS CHECK OF WING 1 AND 2 ANTI ICE SYSTEMS IN REFERENCE WITH AMM 30-00-00. NO FAULTS NOTED. PS CHECK GOOD. OK 
- [SDR HNAA2022031400123](https://openairdocs.org/sdr/HNAA2022031400123), Mar 11, 2022: NONE. NONE. PDIS 624 21-01 2759911 11MAR22 YYZ CLOSE ABORTED T/O DUE TO STRONG FUMES SMELLED IN COCKPIT. (ABORTED SPEED WAS 90, AND FUMES DID GO AWAY PROMPTLY, THOUGH EMERG
- [SDR HNAA2021071500323](https://openairdocs.org/sdr/HNAA2021071500323), Jul 13, 2021: ENGINE. SMOKE. SMOKE AND SMELL COMING FROM #1 ENG AFTER SHUTDOWN FROM INLET AND EXHAUST. USED BORESCOPE TO INVESTIGATE POSSIBLE OIL LEAK FOUND OIL COATING ON OIL SUPPLY LINE T
- [SDR HNAA2021071500322](https://openairdocs.org/sdr/HNAA2021071500322), Jul 13, 2021: UNKNOWN. FUMES. F/A REPORTED UNKNOWN FUMES IN GALLEY. CLEARED PRIOR TO LANDING. MX REMOVED PANELS 223 UZ, 224NZ AND 234 AR INSPECTED ELECTRICAL AROUND GALLEY AREA FOR SMELL AND
- [SDR HNAA2020072800236](https://openairdocs.org/sdr/HNAA2020072800236), Jul 27, 2020: ANTI-ICE VALVE. OUT OF LIMITS. WING A-ICE FAIL TWICE DURING TEST IN FLIGHT. MAINTENANCE: FOUND WING 1 A/I LOW PSI ON CMC. PERFORMED WING THERMAL A/I FUNCTION TEST AND FOUND WING 1 A/I VALVE O
- [SDR HNAA2019121800388](https://openairdocs.org/sdr/HNAA2019121800388), Dec 17, 2019: CONTROLLER. FAILED. W/S HEAT 1 FAIL IN FLIGHT. C/W QRH. MAINTENANCE PERFORMED REMOVEL AND REPLACEMENT #100 W/S TEMP CONTROLLER IN REF TO AMM 30-42-01-400-801A, OPS CHECK GOOD.
- [SDR HNAA2019121100381](https://openairdocs.org/sdr/HNAA2019121100381), Dec 9, 2019: LIGHT. INOPERATIVE. LEFT SIDE OVERWING EMERGENCY LIGHT INOP...FIX: R&RD OVERWING EMERGENCY LIGHT IAW AMM 33-50-10
- [SDR HNAA2019091600273](https://openairdocs.org/sdr/HNAA2019091600273), Sep 15, 2019: SLEEVE. NOT REPORTED. PDIS 624 36-11 1881631 15SEP19 BGR CLOSE AFTER TAKE OFF BLD 1 LEAK MESSAGE DISPLAYED. FOLLOWED QRH ITEM CLEARED. HISTORY: RETURN TO FIELD / AIR TURNBACK. FACT 1
- [SDR HNAA2019091300268](https://openairdocs.org/sdr/HNAA2019091300268), Sep 12, 2019: WARNING SYSTEM. FALSE ACTIVATION. PDIS 624 49-10 1881591 12SEP19 PHL CLOSE APU FAIL MESSAGE ON EICAS. 28876 00 MDC FACT 12SEP19 19:23 PHL PERFORMED ELECTRICAL RESET, OPERATED APU FOR 30 MINS WIT
- [SDR HNAA2019082600239](https://openairdocs.org/sdr/HNAA2019082600239), Aug 23, 2019: DAU. FAILED. DAU 1A FAILED ON ROLL OUT, REJECTED TAKE-OFF. REMOVED AND REPLACED IC600 IAW AMM 31-42-00 OPS CHECK GOOD. OK FOR SERVICE
- [SDR HNAA2019082100233](https://openairdocs.org/sdr/HNAA2019082100233), Aug 19, 2019: DAU. FAILED. DAU NR 1 FAIL MESSAGE DISPLAYED DURING ROTATION. AOA FAIL AT V1. REMOVED AND REPLACED NR 1 IC600,OPS CHECK GOOD, OK FOR SERVICE
- [SDR HNAA2019082100232](https://openairdocs.org/sdr/HNAA2019082100232), Aug 19, 2019: WARNING MESSAGE. FALSE ACTIVATION. DAU #1 FAIL MESSAGE DISPLAYED ON EICAS AT TAKE-OFF....FIX: MAINTENANCE ACTION COMPLETE. SUBJECT TO SATISFACTORY EVAL FLIGHT. EVAL FLT SAT
- [SDR HNAA2019082100231](https://openairdocs.org/sdr/HNAA2019082100231), Aug 19, 2019: WARNING MESSAGE. FALSE ACTIVATION. DAU NR 1 FAIL MESSAGE DISPLAYED ON EICAS AT TAKE-OFF. MESSAGE CLEARED PRIOR TO MX ARRIVING AT AIRCRAFT.SUSPECT TRANSITORY CONDITION REF SEQ 2 FOR EVALUATION FLT
- [SDR HNAA2019081400228](https://openairdocs.org/sdr/HNAA2019081400228), Aug 13, 2019: DAU. FAILED. NR 1 DAU FAILED IN FLT, WITH ASSOCIATED DAU 1 MISCOMPARE. R & R THE NR 1 DAU IAW AMM 31-41-01. OPS CHECK GOOD, OK FOR SERVICE.
- [SDR HNAA2019052700149](https://openairdocs.org/sdr/HNAA2019052700149), May 23, 2019: UNKNOWN. ODOR. 624 21-01 2045341 23MAY19 PHL CLOSE ELECTRIC BURNING SMELL IN COCKPIT AT 23K FT. ICING SYSTEM BRIEFLY CAME ON. ODOR DISSIPATED AT 20K FT DESCENDING. 27371 00 JJ
- [SDR HNAA2018112600291](https://openairdocs.org/sdr/HNAA2018112600291), Nov 24, 2018: BULB. INOPERATIVE. NDIS 624 33-51 0013850 24NOV18 SBY CLOSE PAX DOOR EMERGENCY LIGHT INOP 70100 00 SPE FACT 24NOV18 08:21 SBY R & R'ED LIGHT BULB FOR PAX DOOR EMERGENCY LIGHT AND 
- [SDR HNAA2018111300280](https://openairdocs.org/sdr/HNAA2018111300280), Nov 9, 2018: LIGHT. INOPERATIVE. 624 33-51 0013420 09NOV18 RIC CLOSE LEFT OVERWING EMERGENCY LIGHT INOP 29490 00 PAL FACT 09NOV18 13:37 RIC REMOVED AND REPLACED LEFT OVERWING EMERGENCY LIGHT AS
- [SDR HNAA2018091400224](https://openairdocs.org/sdr/HNAA2018091400224), Sep 13, 2018: WARNING SYSTEM. FALSE ACTIVATION. ENG REF A/I DISAGREE EICAS MESSAGE DISPLAYED DURING TAKE OFF. PER FIM 73-25-00-810-836 RESET T/O AND GROUND RAN A/C AT T/O POWER. NO DEFECT NOTED AT THIS TIME O
- [SDR HNAA2018071900159](https://openairdocs.org/sdr/HNAA2018071900159), Jul 18, 2018: MIXING UNIT. LEAKING. SWEETODOR NOTICED IN COCKPIT ON T/O AND DECEND IN SBY WITH PACK 1 AND 2 ON. WITH ENG BLEEDS DURING CRUISE. OPERATED NR 1 PACK, FOUND NO LEAKS AT HEAT EXCHANGER 
- [SDR HNAA2017112100377](https://openairdocs.org/sdr/HNAA2017112100377), Nov 17, 2017: LINE. CONTAMINATED. RIGHT MLG, AFTER GEAR RETRACTION, WOULD CONTINUE TO UNLOCK AND LOCK. SELECTED GEAR DOWN, ALL NORMAL WITH THE GEAR DOWN. R & R NOSE GEAR DOOR SOLINOID VALVE IAW 
- [SDR HNAA2017101000348](https://openairdocs.org/sdr/HNAA2017101000348), Oct 10, 2017: UNKNOWN. ODOR. UNKNOWN ODOR IN CABIN. CREW REPORTED NO SMOKE OR NO ELECTRICAL ODOR IN CABIN. F/A BECAME NAUSEOUS DUE TO ODOR. GROUND RAN BOTH ENGINES AND APU WITH THE NR 1 & 2
- [SDR HNAA2017092900333](https://openairdocs.org/sdr/HNAA2017092900333), Sep 28, 2017: INVERTER. INOPERATIVE. RIGHT EMERGENCY LIGHT AT THE RT EMERGENCY EXIT WILL NOT ILLUMINATE. REPLACED THE NR 5 INVERTER, OPS CHECKED GOOD IAW AMM 33-50-11-000/400-801A.
- [SDR HNAA2017091400307](https://openairdocs.org/sdr/HNAA2017091400307), Sep 8, 2017: LIGHT. INOPERATIVE. EMERGENCY LIGHT NOT ILLUMINATING. CLEANED AND RESEATED EMERGENCY LIGHT, OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR HNAA2017080700264](https://openairdocs.org/sdr/HNAA2017080700264), Aug 6, 2017: LIGHT. INOPERATIVE. ROW 12 RT SIDEWALL EMERGENCY LIGHT INOPERATIVE. R & R ROW 12 EMERGENCY LIGHT IAW AMM 33-50-14-400-801-A, OPS CHECKED GOOD.
- [SDR HNAA2017071000232](https://openairdocs.org/sdr/HNAA2017071000232), Jul 8, 2017: WARNING MESSAGE. FALSE ACTIVATION. NR 1 ENGINE ANTI ICE DISAGREE MESSAGE DISPLAYED ON EICAS. INSPECTED CMC, NO RELATED MESSAGES DISPLAYED. OPS CHECKED IAW AMM 30-21-00-700-804-A, OPS CHECKED GOOD
- [SDR HNAA2017071000231](https://openairdocs.org/sdr/HNAA2017071000231), Jul 8, 2017: WARNING MESSAGE. FALSE ACTIVATION. DURING TAKE OFF ROLL, TAKE OFF WARNING SPOILER SOUNDED. SPOILERS DID DEPLOY. INSPECTED CMC WITH NO RELATED MESSAGES DISPLAYED, OPS CHECKED IAW AMM 27-63-01-700-
- [SDR SIMA20170531007](https://openairdocs.org/sdr/SIMA20170531007), May 31, 2017: FRAME. CRACKED. FRAME 73 CRACKED BETWEEN STRINGERS 16 - 17R. REMOVED AND REPLACEDTHE FRAME SECTION IAW SRM 51-40-02.
- [SDR SIMA20170531006](https://openairdocs.org/sdr/SIMA20170531006), May 31, 2017: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT CORRODED AROUND AND UNDER CARBON CROSSBEAM, BETWEEN FR 33-34. COMPLETED INSTALLATION OF REPAIR DOUBLER, FILLER AND SHIMS IAW SRM 53-00-10, AN
- [SDR SIMA20170531005](https://openairdocs.org/sdr/SIMA20170531005), May 31, 2017: SKIN. CORRODED. INTERNAL FUSELAGE SKIN CORRODED BETWEEN FRAMES 9-10, STRINGRS 20 - 21L. PERFORMED DRILL OUT OF CORRODED AREA AND INSTALLED A RIVET IAW SRM 53-12-01 AND RESTORED
- [SDR SIMA20170531004](https://openairdocs.org/sdr/SIMA20170531004), May 31, 2017: DOOR SILL. CORRODED. CARGO DOOR CUTOUT LOWER SILL CORRODED. REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA20170531003](https://openairdocs.org/sdr/SIMA20170531003), May 31, 2017: FRAME. CRACKED. LEFT FRAME 10 CRACKED BELOW DV WINDOW CUTOUT. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-40-02, AND SRM 51-20-03.
- [SDR SIMA20170531002](https://openairdocs.org/sdr/SIMA20170531002), May 31, 2017: FRAME. CRACKED. RIGHT FRAME 10 CRACKED BELOW DV WINDOW CUTOUT. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-40-02, AND SRM 51-20-03.
- [SDR SIMA20170531001](https://openairdocs.org/sdr/SIMA20170531001), May 31, 2017: FRAME. CRACKED. FRAME 72 CRACKED BETWEEN STRINGER 16 - 17L. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-40-02.
- [SDR SIMA20170521007](https://openairdocs.org/sdr/SIMA20170521007), May 21, 2017: CONNECTOR. BROKEN. NR 4 EMERGENCY LIGHT WIRE CONNECTOR BROKEN AT THE FUSELAGE END. REPLACED THE MISSING WIRE SPLICE IAW SWPM 20-00-03.
- [SDR SIMA20170521006](https://openairdocs.org/sdr/SIMA20170521006), May 21, 2017: STRINGER. CHAFED. EXTERNAL STRINGER 19R CHAFED BETWEEN FRAMES 52 - 53. REMOVED AND INSTALLED REPAIR ANGLES AND FILLER IAW SRM 53-24-02
- [SDR SIMA20170521004](https://openairdocs.org/sdr/SIMA20170521004), May 21, 2017: STRINGER. CHAFED. EXTERNAL STRINGER 19L CHAFED BETWEEN FRAMES 52 - 53. REMOVED AND INSTALLED REPAIR ANGLES AND FILLER IAW SRM 53-24-02
- [SDR SIMA20170521005](https://openairdocs.org/sdr/SIMA20170521005), May 21, 2017: DRAG ANGLE. CRACKED. LEFT VERTICAL TO FUSELAGE DRAG ANGLE CRACKED AT APPROXIMATELY FRAME 76. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-40-02.
- [SDR SIMA20170519006](https://openairdocs.org/sdr/SIMA20170519006), May 19, 2017: FRAME. CRACKED. FRAME 72 CRACKED, BETWEEN STRINGERS 16 - 17L. REMOVED AND REPLACED THE LOWER FRAME SECTION IAW SRM 51-40-02.
- [SDR SIMA20170519005](https://openairdocs.org/sdr/SIMA20170519005), May 19, 2017: FRAME. CORRODED. FRAME 65 NEAR STRINGER 16L IS CORRODED AT THE NUTPLATE HOLE NEAR THE CARGO DOOR FORWARD TRACK. REWORKED THE AREA, AND FOUND TO BE A PREVIOUSLY INSTALLED REPAIR 
- [SDR SIMA20170517002](https://openairdocs.org/sdr/SIMA20170517002), May 17, 2017: FRAME. CRACKED. FRAME 66 CRACKED AT STRINGER 16R. REPLACED THE FRAME SECTION IAW ERS-EM-53MR-2733.
- [SDR SIMA20170516003](https://openairdocs.org/sdr/SIMA20170516003), May 16, 2017: STRUCTURE. CHAFED. CARGO DOOR TOP EDGE HAS A 9 INCH LONG CHAFE UNDER UPPER DOOR SEAL. REMOVED AND REPLACED THE DOOR TOP EDGE, AND APPLIED EDGE SEALANT AROUND TOP EDGE SECTION IAW 
- [SDR SIMA20170516002](https://openairdocs.org/sdr/SIMA20170516002), May 16, 2017: DOOR FRAME. CORRODED. RIGHT OVER WING EXIT LOWER EXTERNAL FRAME CORRODED AT ROUND BUMPE. REMOVED AND REPLACED EXIT LOWER EXTERNAL FRAME IAW SRM 51-40-02.
- [SDR SIMA20170427006](https://openairdocs.org/sdr/SIMA20170427006), Apr 27, 2017: CHARGER. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 2 BATTERY AND CHARGER IAW AMM 33-50-04 AND AMM 33-26-00. OPERATIONAL CHECKED GOOD.
- [SDR SIMA20170427005](https://openairdocs.org/sdr/SIMA20170427005), Apr 27, 2017: BATTERY. INOPERATIVE. MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY 1 AND BATTERY CHARGER 1 IAW AMM 33-50-04 AND AMM 33-26-00. MAIN DOOR LIGHT AND EMERGENCY
- [SDR SIMA20170329001](https://openairdocs.org/sdr/SIMA20170329001), Mar 29, 2017: PRESSURE SWITCH. FAILED. RUDDER SYSTEM 1 -2 INOP MSG ON EICAS AUTOPILOT AND YAW DAMPER KICKED OFF ABOUT THE SAME TIME. PERFORMED FIM TASK, 27-22-00-810-804-A AND REMOVED AND REPLACED TH
- [SDR SIMA20170307004](https://openairdocs.org/sdr/SIMA20170307004), Mar 7, 2017: CONNECTOR. DIRTY. EMERGENCY LIGHT ON PAX DOOR INOPERATIVE. CLEANED THE CONECTER IAW SWPM 20-50-00. OPS CHECKED GOOD.
- [SDR SIMA20170307003](https://openairdocs.org/sdr/SIMA20170307003), Mar 7, 2017: CHARGER. INOPERATIVE. EMERGENCY LIGHT BATTERY PACK AND CHARGER IN THE NR 3 POSITION PAPER WORK HAS ERRORS. REMOVED AND THE BATTERY CHARGER IAW W/C 33-700-19. OPS CHECKED GOOD.
- [SDR SIMA20150617001](https://openairdocs.org/sdr/SIMA20150617001), Jun 17, 2015: YOKE. CRACKED. LEFT ENG FWD LOWER YOKE CRACKED. REMOVED & INSTALLED SERVICEABLE LT ENG FWD LOWER YOKE IAW EO EM-54MR-386R1.
- [SDR SIMA20150612002](https://openairdocs.org/sdr/SIMA20150612002), Jun 12, 2015: CONNECTOR. DAMAGED. CEILING EMER LIGHT AT GALLEY INOPERATIVE. REPAIRED WIRE SPLICE CONNECTOR ON GALLEY CEILING EMER LIGHT IAW SWPM 25-22-04. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150604007](https://openairdocs.org/sdr/SIMA20150604007), Jun 4, 2015: TRUNNION. CRACKED. DURING MBV INSPECTION, QA FOUND LT MLG UPPER AFT TRUNNION CRACKED OTBD OF BEARING TRACKS. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO

All 147: https://openairdocs.org/aircraft/N624AE/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/N624AE/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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