# N604AE: 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: 145058
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 27, 1998
- Certificate issued: September 28, 2011
- Expires: September 30, 2027
- Mode S code: A7D620
- 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=604AE
- Page: https://openairdocs.org/aircraft/N604AE

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/N604AE/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 N604AE.

## FAA accident and incident reports

None matched to N604AE.

## Service difficulty reports (128, 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 HNAA2021080300353](https://openairdocs.org/sdr/HNAA2021080300353), Aug 2, 2021: WARNING MESSAGE. FALSE INDICATION. STEERING INOP MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF. STEERING FAIL IN LEFT AND RIGHT TURNS ON TAXI IN TO GATE. NO CMC MESSAGES. INSPECTED NLG FOR OBVIOUS DEF
- [SDR HNAA2021051000198](https://openairdocs.org/sdr/HNAA2021051000198), Apr 29, 2021: UPLOCK. FAULTED. PDIS 604 32-20 2406601 29APR21 PIT CLOSE. AMBER NLG UP IND CYCLED INTERMITTANTLY ON EICAS WITH CLUNKING NOISE FROM NLG AREA. CYCLED GEAR AND COND. CONTINUED. NO
- [SDR HNAA2021042700162](https://openairdocs.org/sdr/HNAA2021042700162), Apr 22, 2021: SWITCH. WORN. ON T/O E1 REVERSE DISAGREE DISPLAYED. MAINTENANCE PERFORMED: REACTIVATED #1 T/R. CMC DOWNLOADS DATING BACK TO FEB 27 SHOWS #1 TR UP STOW OUT SWITCH FAIL. INSPEC
- [SDR HNAA2021041200137](https://openairdocs.org/sdr/HNAA2021041200137), Apr 9, 2021: WARNING MESSAGE. FALSE ACTIVATION. ON TAKE OFF ROLL GOT EICAS MESSAGE E2 REVERSE DISAGREE. PERFORMED OPS CHECK OF #2 TR IAW EMB AMM 78-31-01 NO DEFECTS NOTED. OPS CHECK GOOD. OK FOR SERVICE AT TH
- [SDR HNAA2021030700089](https://openairdocs.org/sdr/HNAA2021030700089), Mar 4, 2021: RELAY. MALFUNCTIONED. NR 1 ENGINE THRUST REVERSER DISAGREE MESSAGE ON TAKE OFF ROLL (C/W TASK 78-31-01-980-801-A). REACTIVATED ICU AND REMOVED LOCK PINS. T/S E1 REV DISAGREE MSG IAW 
- [SDR HNAA2020032700109](https://openairdocs.org/sdr/HNAA2020032700109), Mar 26, 2020: TRIM SYSTEM. MALFUNCTIONED. PDIS 604 27-41 2220941 26MAR20 PHL CLOSE MAIN PITCH TRIM INOP ON DEPARTURE. BACK UP TRIM WORKS FINE. FACT 26MAR20 19:50 PHL TROUBLESHOT IAW FIM 27-43-00. RESET 
- [SDR HNAA2020031100093](https://openairdocs.org/sdr/HNAA2020031100093), Mar 10, 2020: WARNING SYSTEM. FALSE ACTIVATION. WING AND STAB A/I DISPLAYED IN ICING CONDITIONS. MAINTENANCE:PERFORMED OPS CHECK IN REF TO AMM 30-00-00-700-802-A OPS CHECK GOOD OK FOR SERVICE.
- [SDR HNAA2020021400062](https://openairdocs.org/sdr/HNAA2020021400062), Feb 13, 2020: CLAMP. LOOSE. MDIS 604 36-21 2292503 13FEB20 ALB CLOSE WHILE RUNNING ENGINES FOR BLEED OVERTEMP DISCREPANCY BLEED 1 LEAK MSG ON EICAS FACT 13FEB20 18:33 ALB TIGHTEN CLAMPS ON
- [SDR HNAA2020021400061](https://openairdocs.org/sdr/HNAA2020021400061), Feb 13, 2020: THERMOSTAT. FAILED. PDIS 604 36-21 2292501 13FEB20 ALB CLOSE BLD 1 OVTEMP AT ALTITUDE, IN ICING. FACT 13FEB20 18:32 ALB R&R FAN AIR VALVE THERMOSTAT IAW EMB 145 AMM 36-11-0 6 OPS C
- [SDR HNAA2020021200058](https://openairdocs.org/sdr/HNAA2020021200058), Feb 11, 2020: BLEED AIR SYS. LEAKING. PDIS 604 36-11 2292482 11FEB20 PHL CLOSE BLEED 1 LEAK EICAS MESSAGE DISPLAYED IN FLIGHT 27371 00 EAV FACT 11FEB20 02:43 PHL T\S IAW FIM 36-20-00-810-801-A. FOUN
- [SDR HNAA2020012000025](https://openairdocs.org/sdr/HNAA2020012000025), Jan 18, 2020: THERMOSTAT. MALFUNCTIONED. DURING CLIMBOUT BLD 1 OVTEMP MSG ON EICAS, CREW C/W QRH MSG EXTINGUISHED. REMOVED AND REPLACED FAN AIR VALVE FILTER AND FAN AIR CONTROL THERMOSTAT IAW 36-11-03 
- [SDR HNAA2019122400391](https://openairdocs.org/sdr/HNAA2019122400391), Dec 20, 2019: WARNING MESSAGE. FALSE ACTIVATION. PITCH TRIM MAIN INOPERTIVE EICAS MESSAGE DISPLAYED AFTER TAKE OFF. MAINTENANCE PERFORMED A PITCH TRIM OPS TEST IAW 27-40-00, OPS CHECKED GOOD. AIRCRAFT GOOD FOR
- [SDR HNAA2019110800349](https://openairdocs.org/sdr/HNAA2019110800349), Nov 7, 2019: WARNING MESSAGE. FALSE ACTIVATION. DURING ICING CONDITIONS BLD 1 OVTEMP, CREW C/W QRH MESSAGE EXTINGUISHED UPON LEAVING ICING CONDITIONS. R & R BLEED 1 OUTLET SENSOR IAW AMM 36-20-01. GROUND RAN 
- [SDR HNAA2019082600238](https://openairdocs.org/sdr/HNAA2019082600238), Aug 25, 2019: LIGHT. INOPERATIVE. RIGHT OVERWING EMERGENCY LIGHT INOP. REPLACED RH EMERGENCY LIGHT IAW AMM 33-50-10-000/400-801-A. OPS CHECK GOOD
- [SDR HNAA2019072200197](https://openairdocs.org/sdr/HNAA2019072200197), Jul 21, 2019: LIGHT. INOPERATIVE. RT WING ROOT AFT EMERGENCY LIGHT INOP. FIX: R&RD BULB IAW AMM 33-50-10.
- [SDR HNAA2019042500119](https://openairdocs.org/sdr/HNAA2019042500119), Apr 24, 2019: SLEEVE. LEAKING. PDIS 604 36-20 2030541 24APR19 PHL CLOSE BLD 1 OVER TEMP ON C/O, RET TO FIELD, DECLARED EMERGENCY 28507 00 MS HISTORY: . FACT 24APR19 21:22 PHL INSPECTED AND FO
- [SDR HNAA2019042200105](https://openairdocs.org/sdr/HNAA2019042200105), Apr 17, 2019: WARNING LIGHT. FALSE ACTIVATION. PDIS 604 33-51 2049463 17APR19 CLT CLOSE DURING APPROACH EMERGENCY LIGHT NOT ARMED MSG ON EIC AS, MSG PERSISTED FOR 5 MIN, EMER. LT CAME ON BY THE MSELVES. FACT
- [SDR HNAA2019042200104](https://openairdocs.org/sdr/HNAA2019042200104), Apr 17, 2019: BULB. BURNED OUT. NDIS 604 33-51 0024260 17APR19 SBY CLOSE EMERGENCY LIGHT ON RH LATERAL PANEL 194ER INOP 30155 00 BAD FACT 17APR19 10:21 SBY R&R BULB FOR EMERGENCY LIGHT ON RH L
- [SDR HNAA2019040700090](https://openairdocs.org/sdr/HNAA2019040700090), Apr 4, 2019: SLEEVE. TORN. 604 36-21 2049321 04APR19 CLT CLOSE AT 8000 FT BLD 1 LEAK WARNING MSG ON EICAS, FOLLOWED QRH, SHUT OFF CROSSFEED AND PUSH OUT AFFECTED BLD SWITCH, MSG EXTINGUIS
- [SDR HNAA2019040400089](https://openairdocs.org/sdr/HNAA2019040400089), Apr 3, 2019: BULB. INOPERATIVE. DIS 604 33-51 0024070 03APR19 SBY CLOSE R/H OVER WING EMERGENCY EXIT LIGHT IS INOP. 27617 00 SPE FACT 03APR19 10:09 SBY R & R R/H OVERWING EMERGENCY EXIT LIGHT 
- [SDR HNAA2019030600062](https://openairdocs.org/sdr/HNAA2019030600062), Mar 4, 2019: WARNING SYSTEM. ACTIVATED. PDIS 604 52-30 1913481 04MAR19 CLT ASSGN BAG DOOR OPEN WARNING, ABORTED T/O HISTORY: YES MEL 04MAR19 18:19 CLT C06317 52-3-2 BAGGAGE DOOR WARNING / POSITION WAR
- [SDR HNAA2018123100331](https://openairdocs.org/sdr/HNAA2018123100331), Dec 28, 2018: WARNING MESSAGE. FALSE ACTIVATION. PDIS 604 36-21 1913091 28DEC18 PHL CLOSE BLEED ONE LEAK MESSAGE AND INSCRIPTION DISPLAYED CAP T RAN QRH MESSAGE EXTINGUISHED. (ADDED: EICAS MESSAG E AND LEAK IN
- [SDR HNAA2018122100325](https://openairdocs.org/sdr/HNAA2018122100325), Dec 20, 2018: WARNING MESSAGE. ILLUMINATED. EICAS MESSAGE ON CLIMB OUT...AIRCRAFT CURRENTLY DOWN IN PHL FOR REPAIRS
- [SDR HNAA2018072600171](https://openairdocs.org/sdr/HNAA2018072600171), Jul 24, 2018: UNKNOWN. MALFUNCTIONED. ON CLIMBOUT, A/P FAILED ALONG WITH NR 1 AHRS. PERFORMED AMM TASK 22-11-00-700-803-A. OPS CHECK OF AUTOPILOT AND AHRS SYSTEMS SEVERAL TIMES WITH NO DEFECTS NOTED
- [SDR HNAA2018021900033](https://openairdocs.org/sdr/HNAA2018021900033), Feb 14, 2018: CLAMP. LOOSE. DURING TAKEOFF, A BLEED 1 LEAK MESSAGE DISPLAYED ON EICAS FOR 10 SECONDS AND SELF EXTINGUISHED. TIGHTENED THE NR 1 ENGINE BLEED VALVE V-BAND CLAMP IAW AMM 36-00
- [SDR HNAA2018020100016](https://openairdocs.org/sdr/HNAA2018020100016), Jan 31, 2018: SWITCH. OUT OF RIG. NR 2 ENGINE THRUST REVERSER DISAGREE MESSAGE DISPLAYED DURING TAKE OFF ROLL, ABORTED TAKEOFF. ENGAGED THE NR 2 THRUST REVERSER SYSTEM & OPS CHECKED. DISCREPANCY
- [SDR HNAA2017122000396](https://openairdocs.org/sdr/HNAA2017122000396), Dec 19, 2017: CLAMP. LOOSE. BLEED 1 LEAK EICAS MESSAGE AT 8500 FEET. TIGHTENED CLAMP ON ACM NR 1 BLEED LINE IN REF TO AMM 21-51-03. OPS CK GOOD. GOOD FOR SERVICE.
- [SDR HNAA2017092100324](https://openairdocs.org/sdr/HNAA2017092100324), Sep 19, 2017: ENGINE. SMOKE. AFTER PREVIOUS FLIGHT, SMOKE WAS REPORTED COMING FROM THE INLET OF THE NR 1 ENGINE. GROUND RAN THE AIRCRAFT, ALL ENGINE INDICATIONS NORMAL. ON SHUTDOWN, NO SMOK
- [SDR HNAA2017082100281](https://openairdocs.org/sdr/HNAA2017082100281), Aug 18, 2017: LAMP. INOPERATIVE. LEFT ABOVE WING EMERGENCY LIGHT NOT ILLUMINATING . R & R THE LAMP.
- [SDR HNAA2017081400272](https://openairdocs.org/sdr/HNAA2017081400272), Aug 13, 2017: FADEC. MALFUNCTIONED. NR 1 ENGINE SHORT DISPATCH ON FADEC A. DOWNLOADED CMC IAW W/C 45-90-00. FOUND MESSAGE ST-ENG1 MMV/CVG SYS. FIM 73-21-00-810-821 OPERATED ENGINES AT MAX THRUST A
- [SDR HNAA2017071200236](https://openairdocs.org/sdr/HNAA2017071200236), Jul 11, 2017: PROXIMITY SENSOR. MALFUNCTIONED. AFTER GEAR RETRACTION, THE LANDING AIR-GND FAIL EICAS CAUTION MESSAGE APPEARED. DURING GEAR EXTENSION MESSAGE EXTINGUISHED. COMPLIED WITH LANDING GEAR AIR - GND
- [SDR HNAA2017070500226](https://openairdocs.org/sdr/HNAA2017070500226), Jul 1, 2017: PRECOOLER. LEAKING. BLEED 1 VALVE CLOSED AND PACK VALVE 1 CLOSED EICAS MESSAGES ILLUMINATED IN FLIGHT. PERFORMED A LT AIR LEAK TEST IAW 36-00-00-700-801-A. FOUND THE PRE COOLER TO 
- [SDR HNAA2017070500224](https://openairdocs.org/sdr/HNAA2017070500224), Jul 1, 2017: COUPLING. DISCONNECTED. COCKPIT AIRFLOW VERY LOW, VERY HOT IN COCKPIT. FOUND TWO LEAKING COUPLINGS IN AFT UNPRESSURIZED BAY AND DISCONNECTED COUPLING AT THE NR 1 PACK. FIXED AND SECURE
- [SDR HNAA2017061400204](https://openairdocs.org/sdr/HNAA2017061400204), Jun 10, 2017: CIRCUIT BREAKER. MALFUNCTIONED. MAIN PITCH TRIM INOPERATIVE BACK UP TRIM PITCH OPS NORMAL. CYCLED PITCH TRIM 1 AND 2 CIRCUIT BREAKERS SYSTEM, OPS CHECKED GOOD IAW 27-43-00-810-801-A OK FOR SER
- [SDR HNAA2017052300185](https://openairdocs.org/sdr/HNAA2017052300185), May 23, 2017: TIRE. FAILED. NR 3 RT MAIN TIRE FAILED. ACFT DECLARED AN EMERGENCY LANDING. LANDED WITH NO ISSUES. CREWS LOOKED AT GEAR BEFORE TAXI. NR 2 ENGINE DAMAGED DUE TO THE NR 3 MAIN 
- [SDR HNAA2017010400006](https://openairdocs.org/sdr/HNAA2017010400006), Jan 4, 2017: FIRE WARNING. FALSE ACTIVATION. DURING CRUISE, CARGO BAY FIRE ANNUNCIATOR ILLUMINATED, FIRED BOTTLES AND RETURNED TO FIELD. NO FIRE HAD ACCURED. REMOVED AND REPLACED BOTH CARGO BAY FIRE BOTTLE
- [SDR HNAA2016100300306](https://openairdocs.org/sdr/HNAA2016100300306), Oct 3, 2016: WARNING LIGHT. FALSE ACTIVATION. MESSAGE DISPLAYED, NO CONTROL IN AUTO OR MANUAL. OPS CHECKED NR 1 PACK IAW 21-51-00. OPS CHECKED GOOD.
- [SDR HNAA2016091400280](https://openairdocs.org/sdr/HNAA2016091400280), Sep 12, 2016: SWITCH. LACK OF LUBE. CARGO DOOR CAUTION LIGHT ILLUMINATED ON ROTATION FOLLOWED BY RED BAG DOOR LIGHT AT APROX 500 FT. BOTH LIGHTS EXTINGUISHED PRIOR TO LANDING. INSPECTED THE CARGO 
- [SDR SIMA20160822002](https://openairdocs.org/sdr/SIMA20160822002), Aug 22, 2016: FRAME. CORRODED. CORROSION BELOW FWD CARGO DOOR GUIDE PLATE ON FRAME 65. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-31-04 4E-1 FIG 212 SHEET 2.
- [SDR SIMA20160818005](https://openairdocs.org/sdr/SIMA20160818005), Aug 18, 2016: FRAME. CRACKED. RIGHT EXTERNAL FUSELAGE SKIN HAS CRACKS AROUND THREE FASTENERS AT FRAME 79 BELOW VERTICAL STAB. REPAIRED THE SKIN IAW ERS-EM-53MR-2219
- [SDR SIMA20160818004](https://openairdocs.org/sdr/SIMA20160818004), Aug 18, 2016: SKIN. CRACKED. RIGHT FUSELAGE SKIN HAS TWO CRACKS AT FRAME 75 AND STRINGER 2R. PERFORMED A PERMANENT REPAIR IAW SRM 53-31-01 FIG 219.
- [SDR SIMA20160817003](https://openairdocs.org/sdr/SIMA20160817003), Aug 17, 2016: TRUNNION. CRACKED. RIGHT MLG AFT UPPER TRUNNION CRACKED. REMOVED AND REPLACED THE TRUNNION IAW ERS-EM-57MR-672
- [SDR SIMA20160810002](https://openairdocs.org/sdr/SIMA20160810002), Aug 10, 2016: RIB. CHAFED. RIB 21 ON LEFT WING CHAFED BELOW OUTBOARD HYDRAULIC HOSES FOR AILERON PCA. REPAIRED THE WING RIB IAW ERS-EM-57MR-671.
- [SDR SIMA20160714003](https://openairdocs.org/sdr/SIMA20160714003), Jul 14, 2016: BATTERY PACK. INOPERATIVE. OVERWING AND EXIT DOOR SIGN INOPERATIVE. CHARGED THE BATTERIES IAW CMM 25-60-03 AND OPS CHECKED GOOD IAW AMM 33-50-00. NO DEFECTS NOTED.
- [SDR SIMA20160414004](https://openairdocs.org/sdr/SIMA20160414004), Apr 14, 2016: LIGHT. INOPERATIVE. LEFT OVERWING PANEL EMER LIGHT INOPERATIVE. R & R IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
- [SDR SIMA20160313001](https://openairdocs.org/sdr/SIMA20160313001), Mar 13, 2016: CONTROL PANEL. FAULTY. BLEED NR 2 LEAK WARNING AFTER TAKEOFF. TRANSFERRED TO NRWC 604-CMH-02715. ACCOMPLISHED OPERATIONS CHECK OF THERMAL SWITCHES 22, 24, 26 & 28. THE WARNING COMES U
- [SDR SIMA20160310004](https://openairdocs.org/sdr/SIMA20160310004), Mar 10, 2016: DUCT. LEAKING. BLEED 1 LEAK. REFER TO ITEM 2 OF LOG PAGE 3954291. NO DEFECTS NOTED. FOUND CRACKED BLEED LINE IN FWD LT SIDE OF AVIONICS COMPARTMENT. R & R DUCT IAW AMM 36-11-0
- [SDR SIMA20151223003](https://openairdocs.org/sdr/SIMA20151223003), Dec 23, 2015: SKIN. GOUGED. SCRATCH ON RT SIDE OF FUSELAGE, FWD OF SERVICE DOOR, FOUND TO BE GOUGED, BETWEEN FRAMES 14 RT & 15 RT, STRINGERS 14 RT - 15 RT. REPAIRED RT SIDE FUSELAGE OF CAT
- [SDR SIMA20151112007](https://openairdocs.org/sdr/SIMA20151112007), Nov 12, 2015: SPOILER. CRACKED. FOUND CRACK ON RT WING MIDDLE HINGE ATTACH POINT SURFACE OF INBD SPOILER. TRANSFERRED TO NRWC 604-MQT-02515. COMPLIED WITH REPAIR OF CRACK IAW ERS-EM-57MR-550. 
- [SDR SIMA20150917003](https://openairdocs.org/sdr/SIMA20150917003), Sep 17, 2015: O-RING. DAMAGED. CREW SAID AFTER BLEED 1 LEAK MSG POSTED, THEY FOLLOWED THEIR PROCEDURES & MSG DIDN'T CLEAR WITHIN 3 MIN, MSG REMAINED FOR APPROX 15 MIN. AFTER MSG CLEARED, IT R

All 128: https://openairdocs.org/aircraft/N604AE/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/N604AE/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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