# N602AE: 1998 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: 145048
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 8, 1998
- Certificate issued: September 6, 2011
- Expires: September 30, 2027
- Mode S code: A7CEB2
- 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=602AE
- Page: https://openairdocs.org/aircraft/N602AE

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/N602AE/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 N602AE.

## 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 20190618024559I](https://openairdocs.org/incident/20190618024559I), Jun 18, 2019: Embraer EMB-145LR (N602AE), Sea Isle, NJ, No damage. Uas/drone incident | PDT4865 | Sea Isle city, NJ 06-18-2019 1930Z Event id: 580829 Zulu date/time: 06/18/2019 1930Z Local date/time: 06/18/2019 1530 EDT Event…
- [Incident 20190615024579I](https://openairdocs.org/incident/20190615024579I), Jun 15, 2019: Embraer EMB-145LR (N602AE), Norfork, VA, No damage. Norfolk, VA: PDT4911, E145, clt-phf, reported a small white drone opposite direction 500 feet below aircraft at 7,000 feet. No evasive action taken. Unknown if…

## Service difficulty reports (179, 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 HNAA2021102500522](https://openairdocs.org/sdr/HNAA2021102500522), Oct 21, 2021: NONE. NONE. AFTER TAKEOFF DURING CLIMB OUT ENG #1 FIRE MESSAGE APPEARED ON EICAS AND FIRE EXTINGUISHING HANDLE ILLUMINATED. RAN QRH, PULLED EXTINGUISHING HANDLE, BLEW BOTTL
- [SDR HNAA2021082400389](https://openairdocs.org/sdr/HNAA2021082400389), Aug 23, 2021: WIRE HARNESS. DAMAGED. APU GEN OVERLOAD. MAX OBSERVED AMPS 660. C/W FIM 24-34-00-810-803-A. INSP APU SHUNT FOR ANY OVERHEATING/BURNING AND REPLACE/REPAIR AS NEEDED. WORK COMPLETED. DE
- [SDR HNAA2021072800347](https://openairdocs.org/sdr/HNAA2021072800347), Jul 25, 2021: RELAY. FAULTED. TAT 2 HEAT INOP ON EICAS IN FLT WITH NO ICING. TROUBLESHOT AND MEG WIRE W102-3812, W102-3814-OK,W102-3815,FOUND HIGH RESISTANCE @ WIRE W102-3817 FROM K0496 RELA
- [SDR HNAA2021070600313](https://openairdocs.org/sdr/HNAA2021070600313), Jul 3, 2021: BATTERY PACK. INOPERATIVE. ROW 1 EMERGENCY FLOOR PATH LIGHTS AND SERVICE DOOR EMERGENCY LIGHT IS INOP. R&R OLD EMERGENCY BATTERY PACK IN THE #2 POSITION WITH A NEW ONE IAW EMB 145 AMM 33-
- [SDR HNAA2021061400262](https://openairdocs.org/sdr/HNAA2021061400262), Jun 11, 2021: ACM. FUMES. ON DESCENT AT 24K FT FUMES NOTICED IN COCKPIT. FOLLOWED QRH, TURNED OFF GASPER, RECIRC, AND WINDSHIELD HEAT. SMELL SEEMED TO DISSIPATE. ON GROUND RESIDUAL SMELL
- [SDR HNAA2021041400154](https://openairdocs.org/sdr/HNAA2021041400154), Apr 14, 2021: SWITCH. ODOR. PDIS 602 05-00 14APR21 MDT, CLOSE STRONG ODOR IN BAGGAGE COMPARTMENT. FACT 14APR21 10:01 MDT, AFTER AIR OF COMPARTMENT NO ODOR NOTICED. SUSPECT LUBING OF BAG DO
- [SDR HNAA2021031500096](https://openairdocs.org/sdr/HNAA2021031500096), Mar 15, 2021: UNKNOWN. ODOR. PDIS 602 21-01 2179641 13MAR21 ORD CLOSE FUMES SMELLED IN FLIGHT DECK DURING TAXI TO GATE FACT 13MAR21 20:49 ORD INSPECTED BOTH PACK SYSTEMS FOR ANY OBVIOUS DEF
- [SDR HNAA2021031600099](https://openairdocs.org/sdr/HNAA2021031600099), Mar 14, 2021: BUTTON. FAULTED. MAIN PITCH TRIM INOPERATIVE EICAS MESSAGE DURING CRUISE FLIGHT WITH OUT SELECTING A CHANGE OF TRIM AND A/P ON FO'S SIDE. T/S IN REF TO FIM TASK 27 43 00 STEPS 1
- [SDR HNAA2021031600098](https://openairdocs.org/sdr/HNAA2021031600098), Mar 14, 2021: CONTROL UNIT. FAILED. MAIN PITCH TRIM INOP EICAS MESSAGE IN CRUISE FLIGHT WITHOUT SELECTING A CHANGE OF TRIM AND A/P ON FO'S. T/S FOUND HOR STAB CTL UNIT FAILURE TWICE ON MFD, R&R ST
- [SDR HNAA2021021500054](https://openairdocs.org/sdr/HNAA2021021500054), Feb 13, 2021: WARNING MESSAGE. ILLUMINATED. 602 HAD AN ABORTED TAKE OFF FOR AN ADVISORY ICE CONDITION MSG AND TAKEOFF CONFIG MSG. NO CMC MESSAGES AND NO HISTORY... DID AN ELECTRICAL ICE PROTECTION TEST.
- [SDR HNAA2020102600291](https://openairdocs.org/sdr/HNAA2020102600291), Oct 24, 2020: INVERTER. INOPERATIVE. DISCREPANCY: INTERIOR REAR EXIT LOCATOR LIGHT INOPERABLE (EMERGENCY LIGHT). ACTION TAKEN: REMOVED HEADLINER PANEL IN REF TO AMM TASK 25-22-04-000-802-A. IN ORDE
- [SDR HNAA2020022800083](https://openairdocs.org/sdr/HNAA2020022800083), Feb 26, 2020: CONTROL UNIT. MALFUNCTIONED. SPOILER FAILED MSG IN FLT WITH SPOILERS DOWN MSG CLEARED W/GEAR DOWN. MSG RETURNED WITH LANDING AND SPOILERS DEPLOYED. CMC MSG,S GND SPOILER ENG FAULT AND GROUN
- [SDR HNAA2019112700369](https://openairdocs.org/sdr/HNAA2019112700369), Nov 18, 2019: WARNING MESSAGE. FALSE ACTIVATION. PACK 1 OVRHEAT MESSAGE URING T/O ROLL.#2 PACK ON MEL....FIX: GROUND RAN A/C WITH BOTH ENGINES,OPS CK #1 PACK IAW EMB 145 21-51-00 OPS CK GOOD NO OBVIOUS DEFECTS
- [SDR HNAA2019110800351](https://openairdocs.org/sdr/HNAA2019110800351), Nov 7, 2019: INVERTER. INOPERATIVE. ROW 12 CEILING EMERGENCY EXI LIGHT INOP....FIX: R&RD #4 INVERTER IAW 33-50-11-000-801-A AND 33-50-11-400-801-A. OPS CHECK GOOD
- [SDR HNAA2019102500321](https://openairdocs.org/sdr/HNAA2019102500321), Oct 24, 2019: LIGHT. INOPERATIVE. EMERGENCY CEILING LIGHT BY SEAT 12 WILL NOT TURN ON....FIX: REMOVED CEILING PNL AT ROW 12INSTALLED NEW LIGHT, REINSTALLED CEILING PNL IAW AMM33-50-15. OPS CHECK
- [SDR HNAA2019091600274](https://openairdocs.org/sdr/HNAA2019091600274), Sep 14, 2019: LIGHT. INOPERATIVE. NDIS 602 33-50 0024580 14SEP19 SBY CLOSE EMERGENCY FLOOR LIGHT STRIP BETWEEN ROWS 6 & 7 IS INOP. FACT 14SEP19 14:42 SBY. R&R EMERGENCY FLOOR LIGHT STRIP BETWEEN
- [SDR HNAA2019062000176](https://openairdocs.org/sdr/HNAA2019062000176), Jun 19, 2019: WIRE. BROKEN. AFT PORTION OF OVER-WING EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE....FIX:FOUND BROKEN WIRE W200-8508-20,CRIMPED NEW CONTACT AND CONNECTOR IAW 20-21-00. INSTALLE
- [SDR HNAA2019021300044](https://openairdocs.org/sdr/HNAA2019021300044), Feb 11, 2019: FAN. FAILED. PDIS 602 05-50 1874192 11FEB19 PGV CLOSE ELECTRICAL SMELL/ODOR COMING FROM FLIGHT DECK CAPTAINS SIDE. FACT 11FEB19 00:30 PGV INSP SMELL IN FLT DECK FOUND NO OBV
- [SDR HNAA2019020800038](https://openairdocs.org/sdr/HNAA2019020800038), Feb 6, 2019: WARNING MESSAGE. FALSE ACTIVATION. PDIS 602 30-10 1874141 06FEB19 SYR CLOSE ICE COND-A/ICE MESSAGE APPEARED DURING TAKEOFF ROLL. MSG EXTINGUISHED FACT 06FEB19 16:56 SYR PERFORMED ELECTRICAL RESET
- [SDR HNAA2019012100021](https://openairdocs.org/sdr/HNAA2019012100021), Jan 20, 2019: TERMINAL. NOT SEATED. DISCREPANCY: EMERGENCY FLOOR LIGHTS ROW 2 AND 3 INOP. CORRECTIVE ACTION: RESEATED TERMINAL ENDS ON EMERG. FLOOR LIGHT ROW 2, RESECURED LIGHT STRIP WITH RETAINED
- [SDR HNAA2018123100334](https://openairdocs.org/sdr/HNAA2018123100334), Dec 31, 2018: BATTERY. DISCHARGED. DIS 602 33-51 0018450 31DEC18 SBY CLOSE LT AND RT OVERWING EMERGENCY EXIT LIGHTS INOP. FACT 31DEC18 10:52 SBY R&R BOTH LT AND RT OVER WING EMERGENCY EXIT LIGHT 
- [SDR HNAA2018121800317](https://openairdocs.org/sdr/HNAA2018121800317), Dec 16, 2018: WIRE. BROKEN. MDIS 602 33-51 1978093 16DEC18 CLT ASSGN EMERGENCY LIGHT AT AFT GALLEY WALL HAS BROKEN WIRE A T SPLICE. 26390 00 DS HISTORY: . DFRL 16DEC18 13:40 CLT INSTALLED 
- [SDR HNAA2018121800319](https://openairdocs.org/sdr/HNAA2018121800319), Dec 15, 2018: BATTERY PACK. INOPERATIVE. MDIS 602 33-51 1978082 15DEC18 CLT CLOSE L/H AND R/H EXTERIOR OVERWING EMERGENCY LIGHTS INOP FACT 16DEC18 11:56 CLT R\R EMERGENCY BATTERY PACK AT ROW 15A OPS CH
- [SDR HNAA2018101100253](https://openairdocs.org/sdr/HNAA2018101100253), Oct 10, 2018: PRESSURE SWITCH. MALFUNCTIONED. AT 400 FEET AGL AT TAKEOFF YD FAILED AND RUD SYS 1/2 INOP CAUTION MSG PRESENTED. RAN QRH WHEN RUD SYS 2 DESELECTED RUD SYS 1 CAME BACK ON LINE. YD RE-ENGAGE AND
- [SDR HNAA2018091100218](https://openairdocs.org/sdr/HNAA2018091100218), Sep 10, 2018: PROCESSOR. MALFUNCTIONED. ATC REPORTS BOTH TRANSPONDERS FAIL INFLIGHT -WILL NOT IDENT-. R&R TCAS PROCESSOR IAW AMM 34-43-01. OPS CHECK IAW AMM 34-43-00 REQUIRES FUNCTIONAL CHECK.
- [SDR HNAA2018071300148](https://openairdocs.org/sdr/HNAA2018071300148), Jul 12, 2018: DOOR. MISSING. RIGHT AFT FUSELAGE IS MISSING APU ACCESS DOOR AFTER FLIGHT.
- [SDR HNAA2018052500109](https://openairdocs.org/sdr/HNAA2018052500109), May 7, 2018: ACTUATOR. LEAKING. DURING FLIGHT, NOTICED A RAPID DEPETION OF THE NR 1 HYD SYSTEM QUANTITY WITH AN EICAS MESSAGE. R & R GROUND SPOILER ACTUATOR IAW AMM 27-62-01-400-801-A. REPLENI
- [SDR HNAA2018050200095](https://openairdocs.org/sdr/HNAA2018050200095), Apr 30, 2018: VALVE. FAILED. NR 2 HIGH STAGE VALVE FAILURE DURING TAKE OFF AT ABOUT 20 KNOTS. R&R NR 2 HIGH STAGE VALVE IAW AMM 36-11-02. OPS GOOD AT THIS TIME. OK FOR SERVICE.
- [SDR HNAA2018042500087](https://openairdocs.org/sdr/HNAA2018042500087), Apr 23, 2018: CONNECTOR. DIRTY. SEAT 12A EXIT SIGN INOPERATIVE. CLEANED CONNECTORS AND SECURED IAW AMM 33-50-14-0001/400-801-A. OPS CHECKED GOOD.
- [SDR HNAA2018041100081](https://openairdocs.org/sdr/HNAA2018041100081), Apr 10, 2018: WIRE. DAMAGED. LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. SECURED THE LIGHT WIRES IAW 20-21-00.
- [SDR HNAA2018033000078](https://openairdocs.org/sdr/HNAA2018033000078), Mar 28, 2018: LIGHT. UNKNOWN. FLOOR EMERGENCY LIGHT STRIP, SEAT 1A INOPERATIVE. PERFORMED AN OPS CHECK OF THE EMERGENCY LIGHT. OPS CHECKED NORMAL. OK FOR SERVICE. E.
- [SDR HNAA2017101600349](https://openairdocs.org/sdr/HNAA2017101600349), Oct 15, 2017: INVERTER. INOPERATIVE. LEFT AFT INTERIOR OVERWING EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. R & R THE INVERTER IAW AMM 33-50-11-000/400-801A. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR HNAA2017092900334](https://openairdocs.org/sdr/HNAA2017092900334), Sep 28, 2017: CONTACT. DIRTY. EMERGENCY LIGHT AT ROW 12A, AFT WINDOW DOES NOT ILLUMINATE. REMOVED THE EMERGENCY LIGHT. CLEANED THE CONTACTORS, AND INSTALLED THE LIGHT. OK FOR SERVICE. OPS CH
- [SDR HNAA2017052900194](https://openairdocs.org/sdr/HNAA2017052900194), May 29, 2017: RELAY. INOPERATIVE. PITOT NR 3 INOPERATIVE CAUTION EICAS MESSAGE. R & R THE RELAYS K0058 & K0060 IAW TASK 30-31-00-810-803-A. OPS GOOD.
- [SDR SIMA20161216007](https://openairdocs.org/sdr/SIMA20161216007), Dec 16, 2016: DOOR SILL. CORRODED. CARGO DOOR SILL IS CORRODED. R & R THE DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA20161216003](https://openairdocs.org/sdr/SIMA20161216003), Dec 16, 2016: SHEAR TIE. CORRODED. FRAME 65 SHEAR TIE CORRODED. INSTALLED A REPAIR IAW SRM 53-31-04.
- [SDR SIMA20161216004](https://openairdocs.org/sdr/SIMA20161216004), Dec 16, 2016: SUPPORT. CORRODED. TOILET WASTE VALVE SUPPORT IS CORRODED. PERFORMED PERMANENT REPAIR INSTALLED DOUBLER IAW ERS-EM-53MR-2471.
- [SDR SIMA20161216005](https://openairdocs.org/sdr/SIMA20161216005), Dec 16, 2016: DOOR SILL. CORRODED. CARGO DOOR SILL IS CORRODED. R & R THE DOOR SILL IAW SRM 51-40-02.
- [SDR SIMA20161216009](https://openairdocs.org/sdr/SIMA20161216009), Dec 16, 2016: STRINGER. CHAFED. STRINGER 19R BETWEEN FRAMES 52-53 CHAFED. REPAIRED THE STRINGER IAW SRM 53-24-02.
- [SDR SIMA20161216008](https://openairdocs.org/sdr/SIMA20161216008), Dec 16, 2016: FRAME. BROKEN. FRAME 10 UNDER COPILOTS WINDOW IS BROKEN. REMOVE AND REPLACED THE FRAME IAW SRM 51-40-02.
- [SDR SIMA20161216006](https://openairdocs.org/sdr/SIMA20161216006), Dec 16, 2016: SUPPORT. CORRODED. TOILET WASTE VALVE SUPPORT IS CORRODED. REPAIRED THE SUPPORT AND INSTALLED A DOUBLER IAW ERS-EM-53MR-2471.
- [SDR SIMA20161215005](https://openairdocs.org/sdr/SIMA20161215005), Dec 15, 2016: FRAME. CORRODED. FRAME 25 UPPER FLANGE CRACKED BETWEEN STRINGERS 15 - 16R. REPAIRED THE FRAME IAW SRM 53-00-04 AND ERS-EM-53MR-2472.
- [SDR SIMA20161214002](https://openairdocs.org/sdr/SIMA20161214002), Dec 14, 2016: FRAME. CORRODED. FRAME 65 CORRODED UNDER FWD LOWER CARGO DOOR STRIKER PLATE. REPAIRED THE FRAME IAW ERS-EM-53MR-2466
- [SDR SIMA20161203002](https://openairdocs.org/sdr/SIMA20161203002), Dec 3, 2016: YOKE. CRACKED. RIGHT ENGINE PYLON FWD LOWER YOKE CRACKED. REMOVED AND REPLACED THE YOKE IAW EO EM-54MR-386
- [SDR SIMA20161121007](https://openairdocs.org/sdr/SIMA20161121007), Nov 21, 2016: WIRE. BROKEN. LEFT NR 7 AND 9 EMERGENCY LIGHT STRIPS HAD BROKEN WIRES. REPLACED THE LIGHT STRIPS IAW AMM 33-50-12
- [SDR SIMA20161121010](https://openairdocs.org/sdr/SIMA20161121010), Nov 21, 2016: BATTERY PACK. INOPERATIVE. NR 4 EMERGENCY LIGHT BATTERY IS DEAD. R & R THE BATTERY IAW AMM 33-50-04.
- [SDR SIMA20161121005](https://openairdocs.org/sdr/SIMA20161121005), Nov 21, 2016: FRAME. CRACKED. FRAME 25 UPPER FLANGE CRACKED BETWEEN 15R AND 16R. REPAIRED THE FRAME IAW ERS-EM-53MR-2472.
- [SDR SIMA20161121008](https://openairdocs.org/sdr/SIMA20161121008), Nov 21, 2016: YOKE. CRACKED. RIGHT ENGINE FWD LOWER YOKE CRACKED. REMOVED AND REPLACED THE YOKE IAW EO EM-54MR-386
- [SDR SIMA20161121009](https://openairdocs.org/sdr/SIMA20161121009), Nov 21, 2016: FRAME. CORRODED. FRAME 65 CORRODED UNDER FWD LOWER CARGO DOOR STRIKER PLATE. FABRICATED AND INSTALLED A REPAIR ANGLE IAW SRM 53-31-04 ITEM 4E AND ERS-EM-53MR-2466
- [SDR SIMA20161121006](https://openairdocs.org/sdr/SIMA20161121006), Nov 21, 2016: DOOR FRAME. CORRODED. SERVICE DOOR CUTOUT AFT FRAME IS CORRODED BEHIND LOWER PLASTIC GUIDE. REPAIRED IAW ERS-EM-53MR-2479

All 179: https://openairdocs.org/aircraft/N602AE/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/N602AE/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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