# N622AE: 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: 145108
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 13, 1999
- Certificate issued: September 28, 2011
- Expires: September 30, 2027
- Mode S code: A81DB0
- 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=622AE
- Page: https://openairdocs.org/aircraft/N622AE

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/N622AE/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 N622AE.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20220704022929I](https://openairdocs.org/incident/20220704022929I), Jul 4, 2022: Embraer EMB-145LR (N622AE), Fort Worth, TX, Minor damage. Received ATC report: dallas-Fort Worth tower reports, dallas-Fort Worth, TX (dfw): [privacy data omitted], E145, bmi-dfw, reported a cracked windshield. Acft…
- [Incident 20030302003849I](https://openairdocs.org/incident/20030302003849I), Mar 2, 2003: Emb EMB145LR (N622AE), Omaha, NE. (-23) N622AE, being operated as American eagle flight 4108, departed Omaha, NE. Enroute to chicago, IL. After takeoff the crew received a gear disagreement in…

## Service difficulty reports (183, 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 SIMA20230221001](https://openairdocs.org/sdr/SIMA20230221001), Feb 21, 2023: STRIP. INOPERATIVE. EMERGENCY FLOOR LIGHT INOP AT ROWS 8 AND 9-C/A-RAR EMERGENCY EXIT LIGHT STRIP INTO MEL AT ROW 8 AND 9.
- [SDR SIMA20230208002](https://openairdocs.org/sdr/SIMA20230208002), Feb 8, 2023: BATTERY. UNSERVICEABLE. BOTH OVERWING EMERGENCY LIGHTS INOP-C/A-RAR #4 EMERGENCY LIGHT BATTERY IAW MM 33-50-04 OPS CHECK GOOD
- [SDR SIMA20230113001](https://openairdocs.org/sdr/SIMA20230113001), Jan 13, 2023: LAMP. INOPERATIVE. RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RT OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD.
- [SDR SIMA20221002001](https://openairdocs.org/sdr/SIMA20221002001), Oct 2, 2022: LAMP. INOPERATIVE. RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPC GOOD. END.
- [SDR SIMA20220925003](https://openairdocs.org/sdr/SIMA20220925003), Sep 25, 2022: LAMP. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.
- [SDR SIMA20220831001](https://openairdocs.org/sdr/SIMA20220831001), Aug 31, 2022: LAMP. INOPERATIVE. RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPS CHECK GOOD
- [SDR SIMA20220710001](https://openairdocs.org/sdr/SIMA20220710001), Jul 10, 2022: LIGHT. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICED DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD. END.
- [SDR SIMA20220704003](https://openairdocs.org/sdr/SIMA20220704003), Jul 4, 2022: WINDSCREEN. CRACKED. SUPPLEMENTAL CA FOR FO LOWER OUTSIDE EDGE OF WINDSCREEN CRACKED DECLARED EMERGENCY."TRANSFERRED TO NRWC 622-DFW-05541".-C/A-RAR THE FO,S WINDSHIELD IAW EMB145 A
- [SDR SIMA20220609001](https://openairdocs.org/sdr/SIMA20220609001), Jun 9, 2022: LAMP. INOPERATIVE. RH OVER WING EMERGENCY LIGHT INOP-C/A-RAR THE RH OVERWING EMERGENCY LT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. END.
- [SDR SIMA20220404004](https://openairdocs.org/sdr/SIMA20220404004), Apr 4, 2022: BATTERY. INOPERATIVE. RH OVERWING AFT EMERGENCY LIGHT INOP.-C/A-RAR # 2 BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPS CHK GOOD.
- [SDR SIMA20220404005](https://openairdocs.org/sdr/SIMA20220404005), Apr 4, 2022: BATTERY. INOPERATIVE. EMERGENCY FLOOR PROXIMITY STRIP LIGHTS INOP AT SEATS 1A THRU 7A.-C/A-RAR # 2 BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPS CHK GOOD.
- [SDR SIMA20220213001](https://openairdocs.org/sdr/SIMA20220213001), Feb 13, 2022: NONE. NONE. AFT CABIN EMERGENCY FLASHLIGHT CLAMP BROKEN-C/A-RAR AFT CABIN EMERGENCY FLASHLIGHT CLAMP IAW EMB 145 CMM 25-60-14.
- [SDR SIMA20220105001](https://openairdocs.org/sdr/SIMA20220105001), Jan 5, 2022: NONE. NONE. FLIGHT ATTENDANT LED FLASHLIGHT INOP-C/A-RAR FLIGHT ATTENDANT LED FLASHLIGHT ASSY IAW EMB 145 AMM 33-50-16. OPC GOOD.
- [SDR SIMA20210325001](https://openairdocs.org/sdr/SIMA20210325001), Mar 25, 2021: CRADLE. BROKEN. AFT EMERGENCY FLASHLIGHT HOLDER BRACKET BROKEN-C/A-DEFERRED PER MEL 25-32 AUTH# 030362M-C
- [SDR SIMA20210221002](https://openairdocs.org/sdr/SIMA20210221002), Feb 21, 2021: WIRE. BROKEN. SERVICE DOOR EMERGENCY LIGHT HAS BROKEN WIRE. C/A-INSTALLED SPLICE TO SERVICE DOOR EMERGENCY LIGHT IAW SWPM 20-21-00. OPC GOOD. END.
- [SDR SIMA20210213002](https://openairdocs.org/sdr/SIMA20210213002), Feb 13, 2021: FLASHLIGHT. MISSING. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT MISSING-C/A-RAR MISSING FA EMERGENCY FLASH LIGHT AS REQ NO MTX REQ. OP'S CHECK GOOD
- [SDR SIMA20210207001](https://openairdocs.org/sdr/SIMA20210207001), Feb 7, 2021: LAMP. INOPERATIVE. OVERWING EMERGENCY LIGHT ON ROW 12CB INOP-C/A-RAR LAMP ON OVERWING EMERGENCY LIGHT IN ROW 12CB ABOVE PASSENGER SEATS IN REF WITH EMB 145 AMM 33-50-07. OPS CHECK
- [SDR SIMA20201202002](https://openairdocs.org/sdr/SIMA20201202002), Dec 2, 2020: FLASHLIGHT. MISSING. F/A AFT FLASHLIGHT MISSING. C/A: R & R AFT CABIN EMERGENCY FLASHLIGHT, REF AMM 33-50-16.
- [SDR SIMA20201004001](https://openairdocs.org/sdr/SIMA20201004001), Oct 4, 2020: A/C PACK. INOPERATIVE. HAD PACK 1 VALVE CLOSED ADVISORY MESSAGE ON EICAS AND LATER IN CRUISE. FA REPORTED SMOKE IN THE CABIN DECLARED EMERGENCY. C/A: PERFORMED E145 FIM 21-20-00-810-8
- [SDR SIMA20200919003](https://openairdocs.org/sdr/SIMA20200919003), Sep 19, 2020: DOOR SILL. CORRODED. SERVICE DOOR SILL HAS CORROSION. C/A REMOVED AND REPLACED SERVICE DOOR CENTER DOOR SILL, IAW EMB 145 SRM 51-40-02 AND ERS-EM-5300-4190. CENTER SILL PN: 145-2217
- [SDR SIMA20200917005](https://openairdocs.org/sdr/SIMA20200917005), Sep 17, 2020: WEB. DAMAGED. CARGO DOOR INNER WEBBING LOWER NUTPLATE HOLE BLENDED BEYOND LIMITS. C/A: FABRICATED AND INSTALLED REPAIR DOUBLER ON CARGO DOOR INNER WEBBING LOWER NUTPLATE HOLE
- [SDR SIMA20200917006](https://openairdocs.org/sdr/SIMA20200917006), Sep 17, 2020: WEB. DAMAGED. CARGO DOOR INNER WEBBING AFT NUTPLATE HOLE BLENDED BEYOND LIMITS. C/A: FABRICATED AND INSTALLED REPAIR DOUBLER ON CARGO DOOR INNER WEBBING AFT NUT PLATE HOLE, I
- [SDR SIMA202009187001](https://openairdocs.org/sdr/SIMA202009187001), Sep 17, 2020: SHEAR TIE. CORRODED. CARGO FR 65 PREVIOUS SHEAR CLIP REPAIR HAS CORROSION NEAR STR 17L. C/A REMOVED AND REPLACED REPAIR SECTION OF CARGO FR 65 SHEAR CLIP, IAW EMB 145 SRM 53-31-04 F
- [SDR SIMA202009186002](https://openairdocs.org/sdr/SIMA202009186002), Sep 16, 2020: FLOOR SUPPORT. CORRODED. RT LAV OMEGA BEAM CORRODED AT FWD NUTPLATE HOLE. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER ON RT LAV OMEGA BEAM AT FWD NUTPLATE HOLE, IAW ERS-EM-53
- [SDR SIMA202009176001](https://openairdocs.org/sdr/SIMA202009176001), Sep 16, 2020: DOOR SILL. CORRODED. CARGO DOOR ENTRANCE SILL IS CORRODED. C/A REMOVED AND REPLACED CARGO DOOR ENTRANCE SILL, IAW EMB 145 SRM 51-40-02 SILL PN: 145-25480-003.
- [SDR SIMA20200729007](https://openairdocs.org/sdr/SIMA20200729007), Jul 29, 2020: PIN. CORRODED. RT EMERGENCY EXIT LOWER FWD ALIGNMENT PIN CORRODED. C/A COMPLETE: REMOVED AND REPLACED RT EMERGENCY EXIT LOWER FWD ALIGNMENT PIN, IAW EMB 145 AMM 52-21-00, SEE 
- [SDR SIMA20200729008](https://openairdocs.org/sdr/SIMA20200729008), Jul 29, 2020: SEAL. WORN. LT EMERGENCY EXIT LOWER SEAL WORN. C/A COMPLETE: REMOVED AND REPLACED LT EMERGENCY EXIT LOWER SEAL, IAW EMB 145 AMM 52-21-01.
- [SDR SIMA20200729009](https://openairdocs.org/sdr/SIMA20200729009), Jul 29, 2020: CONNECTOR. BROKEN. EMERGENCY LIGHT STRIP NR 5 HAS BROKEN OFF CONNECTOR. C/A COMPLETE: INSTALLED SERVICEABLE CONNECTOR ON EMERGENCY LIGHT STRIP NR 5 AIRCRAFT SIDE, IAW EMB-145 SWPM
- [SDR SIMA20200729006](https://openairdocs.org/sdr/SIMA20200729006), Jul 29, 2020: BATTERY PACK. NOT REPORTED. STD-REQ A3265 OPS A-REMOVE AND REPLACE EMERGENCY LIGHTING BATTERY ASSY/ BATTERY CHARGER EMB WC 33-700-19 CRJ WC 33-002 ETN-EM-25-385. P/N: 2013-1ASMI SN: 80045 
- [SDR SIMA20200729005](https://openairdocs.org/sdr/SIMA20200729005), Jul 29, 2020: WIRE. BROKEN. COCKPIT STEP PANEL EMERGENCY EXIT LIGHT WIRE IS BROKEN. C/A COMPLETE: R & R COCKPIT STEP PANEL EMERGENCY EXIT LIGHT, IAW EMB 145 AMM 33-50-13. SEE NRTC BOW34668
- [SDR SIMA2020062218004](https://openairdocs.org/sdr/SIMA2020062218004), Jun 18, 2020: CONNECTOR. BROKEN. FOUND EMERGENCY LIGHT STRIP CONNECTION BROKEN UNDER FLOOR BOARD PANEL 261BF. INSTALLED NEW CONNECTOR FOR EMERG LIGHT STRIP FLOOR PANEL 261BF IAW SWPM 20-50-01 O
- [SDR SIMA2020062218005](https://openairdocs.org/sdr/SIMA2020062218005), Jun 18, 2020: CONNECTOR. BROKEN. FLOORBOARD PANEL 261 BF PROXIMITY LIGHT STRIP BROKEN. INSTALLED NEW CONNECTOR FOR EMERG LIGHT STRIP FLOOR PANEL 261BF IAW SWPM 20-50-01 OPC OF EMERG LIGHTS GOOD
- [SDR SIMA202003054003](https://openairdocs.org/sdr/SIMA202003054003), Mar 4, 2020: FASTENER. NOT REPORTED. SUPPLEMENTAL WITH NUMBER 2 ENGINE RUNNING, DURING APU START MULTIPLE DISPLAY FAILURES WITH EICAS MESSAGES ACCOMPANIED BY A STRONG ELECTRICAL BURNING FUME PRESEN
- [SDR SIMA202002184001](https://openairdocs.org/sdr/SIMA202002184001), Feb 14, 2020: WINDOW FRAME. CRACKED. SUPPLEMENTAL FOUND CRACK ON AFT UPPER SIDE OF RH DV WINDOW FRAME. THIS HAS BEEN UPGRADED TO A MAJOR REPAIR.-C/A-REPAIRED CRACK ON AFT UPPER SIDE OF RH DV WINDOW
- [SDR SIMA202002065007](https://openairdocs.org/sdr/SIMA202002065007), Feb 5, 2020: INVERTER. INOPERATIVE. UPPER EXIT MARKER ON RH CABIN EMERGENCY DOOR SHROUD FAILS TO ILLUMINATE.-C/A-T/S IAW WM 33-50-50. REMOVED AND REPLACED #5 INVERTER IAW AMM 33-50-11. OPC GOOD.
- [SDR SIMA202001064002](https://openairdocs.org/sdr/SIMA202001064002), Jan 4, 2020: ACTUATOR. MALFUNCTIONED. PTRIM MAIN INOP EICAS MESSAGE AFTER TAKEOFF "TRANSFERRED TO NRWC 622-MIA-03884"-C/A-ACCOMPLISHED REMOVED AND REPLACED HORIZONTAL STAB ACTUATOR IAW EMB145 AMM 27
- [SDR SIMA201910286001](https://openairdocs.org/sdr/SIMA201910286001), Oct 26, 2019: SIGN. INOPERATIVE. DURING PS-2 FOUND RH EXIT MARKING SIGN INOP-C/A-INSTALLED RH EXIT MARKING SIGN ASSEMBLY IAW EMMB 145 AMM 33-50-14 OPS CHECK GOOD.
- [SDR SIMA201906065003](https://openairdocs.org/sdr/SIMA201906065003), Jun 5, 2019: CONNECTOR. LOOSE. DURING PS-1 CHECK FOUND EXIT ROW RH EMERGENCY LT INOP.-C/A-CANON PLUG CONNECTOR LOOSE. REATTACHED IAW STANDARD MAINTENANCE PRACTICES. FUNCTION CHECK GOOD.
- [SDR SIMA20190322004](https://openairdocs.org/sdr/SIMA20190322004), Mar 22, 2019: WIRE. BROKEN. NR 4 EMERGENCY FLOOR STRIP LIGHT CONNECTION WIRES BROKEN. C/A-REMOVED AND REPLACED NR 4 EMERGENCY FLOOR STRIP LIGHT ASSEMBLY IAW AMM 33-50-12. OPERATIONAL CHECK
- [SDR SIMA20180605008](https://openairdocs.org/sdr/SIMA20180605008), Jun 5, 2018: FLASHLIGHT. OUT OF ADJUST. FA FLASHLIGHT INOP. C/A-COMPLETE:PERFORMED ADJUSTMENT OF THE FA FLASHLIGHT IAW AMM 33-51-01. FUNCTION CHECK GOOD.
- [SDR RAIA201802060001](https://openairdocs.org/sdr/RAIA201802060001), Feb 6, 2018: SKIN. CRACKED. FUSELAGE SKIN HAS CRACKS AT FRAME 78 BETWEEN STRINGERS 6L - 8L. CUTOUT THE DAMAGE AND INSTALLED A DOUBLER.
- [SDR RAIA201802080002](https://openairdocs.org/sdr/RAIA201802080002), Feb 1, 2018: SUPPORT. DAMAGED. LT OMEGA BEAM SUPPORT AT FR 29 HAS DAMAGED/ELONGATED FASTENER HOLES. R & R LT OMEGA BEAM SUPPORT AT FR 29. SUPPORTING DOCUMENTS EMAILED TO PROGMGR UNDER THE SUB
- [SDR RAIA201801260007](https://openairdocs.org/sdr/RAIA201801260007), Jan 26, 2018: SKIN. CORRODED. CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN FRAMES 60 - 61, STRINGER 20 - 21L. REPAIRED THE SKIN.
- [SDR RAIA201801260006](https://openairdocs.org/sdr/RAIA201801260006), Jan 26, 2018: SHEAR TIE. CORRODED. FRAME 65 SHEAR TIE CORRODED AT THE BOTTOM. REPAIRED THE SHEAR TIE.
- [SDR RAIA201801260005](https://openairdocs.org/sdr/RAIA201801260005), Jan 26, 2018: BRACKET. CRACKED. BRACKET CRACKED UNDER THE LT OMEGA BEAM BETWEEN FRAMES 28 - 29. REPAIRED THE BRACKET, FOUND TO BE PART OF PREVIOUS REPAIR.
- [SDR RAIA201801260004](https://openairdocs.org/sdr/RAIA201801260004), Jan 26, 2018: DOOR SILL. CORRODED. CARGO DOOR SILL CORRODED. R & R THE CARGO DOOR SILL..
- [SDR RAIA201801250002](https://openairdocs.org/sdr/RAIA201801250002), Jan 25, 2018: FRAME. CRACKED. FRAME 73 IS CRACKED, UNDER THE FLOOR BOARD. R & R THE FRAME.
- [SDR RAIA201801240002](https://openairdocs.org/sdr/RAIA201801240002), Jan 24, 2018: YOKE. CRACKED. LEFT PYLON, FWD LOWER ENGINE YOKE, FWD BRACKET IS CRACKED. R & R THE YOKE FITTING.
- [SDR RAIA201801230006](https://openairdocs.org/sdr/RAIA201801230006), Jan 23, 2018: SKIN. DENTED. CENTER SKIN HAS A DENT AT FRAME 30 BETWEEN STRINGERS 6L - 7L. CUT OUT THE DAMAGE AND INSTALLED A FILLER & DOUBLER.
- [SDR RAIA201801230005](https://openairdocs.org/sdr/RAIA201801230005), Jan 23, 2018: SKIN. DENTED. CENTER FUSELAGE SKIN HAS A DENT ON THE FRAME 32 BETWEEN STRINGERS 1L - 2L. REPAIRED THE SKIN.

All 183: https://openairdocs.org/aircraft/N622AE/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/N622AE/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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.