# N606AE: 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: 145062
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 20, 1998
- Certificate issued: September 6, 2011
- Expires: September 30, 2027
- Mode S code: A7DD8E
- 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=606AE
- Page: https://openairdocs.org/aircraft/N606AE

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/N606AE/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 N606AE.

## FAA accident and incident reports

None matched to N606AE.

## Service difficulty reports (180, 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 SIMA20220726002](https://openairdocs.org/sdr/SIMA20220726002), Jul 26, 2022: EICAS. MULTIPLE FAIL. REPEATED EVENT WHILE LEVEL AT 16000' WITH POWER AT IDLE, SPEED BRAKE LEVER SELECTED OPEN, NORMAL SPEED BRAKE APPLICATION AND INDICATION. AFTER CLOSING SPEED BRA
- [SDR SIMA20220723005](https://openairdocs.org/sdr/SIMA20220723005), Jul 23, 2022: EICAS. FALSE INDICATION. DURING DESCENT RECEIVED EICAS SPOILER FAIL MSG AFTER CLOSING SPEEDBRAKE LEVER EVEN THOUGH SPEED BRAKE POSITION INDICATED OPEN ON EICAS. FLIGHT ATT VISUALLY VERI
- [SDR SIMA20220720004](https://openairdocs.org/sdr/SIMA20220720004), Jul 20, 2022: PROXIMITY SENSOR. UNSERVICEABLE. SPOILER OPENED INFLIGHT UNCOMANDED. EMERGENCY DECLARED. LANDED SAFELY - TROUBLE SHOOTING ITEM #2 LGPG 4848173 ON TAKE OFF ROLL AFTER THRUST SET, SPOILER DEPLOYE
- [SDR SIMA20220622003](https://openairdocs.org/sdr/SIMA20220622003), Jun 22, 2022: LIGHT. INOPERATIVE. PER TRIAD GROUP, PERFORM SMOKE / ABNORMAL SMELL IN THE CABIN / COCKPIT UNKNOWN SOURCE FIM TASK 21-20-00-810-801-A.-C/A-C/W FIM TASK 21-20-00-810-801-A. FOUND SE
- [SDR SIMA20220618003](https://openairdocs.org/sdr/SIMA20220618003), Jun 18, 2022: CABIN PRESSURE. FAILED. AIRCRAFT NOT PRESSURIZING AFTER TAKEOFF. DID NOT DECLARED EMRGENCY RETURN TO FIELD. -C/A-RAR DIGITAL CONTROLLER IAW AMM 21-31-01 OPC GOOD NO FURTHER DEFECTS NOT
- [SDR SIMA20220603001](https://openairdocs.org/sdr/SIMA20220603001), Jun 3, 2022: NONE. NONE. MAIN DOOR EXTREMELY DIFFICULT TO OPEN-C/A-AT THIS TIME C/W MAIN CABIN DOOR FRAME ROLER LUBRICATION PER AMM 53-21-02
- [SDR SIMA20211103004](https://openairdocs.org/sdr/SIMA20211103004), Nov 3, 2021: NONE. NONE. OVERWING EMERGENCY EXIT LOCATOR MARKER AFT FACING INOP.-C/A-T/S PER WM 33-50-50. FOUND SP9125 DISCONNECTED.RAR SP9125 IAW SWPM 20-21-00. OPC GOOD IAW AMM 33-50-
- [SDR SIMA20211027002](https://openairdocs.org/sdr/SIMA20211027002), Oct 27, 2021: NONE. NONE. ALL AFT INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP-C/A-T/S PER FIM TASK 33-50-00-810-804-A. FOUND #4 EMERGENCY LIGHT POWER SUPPLY TO BE INNOPERATIVE. RAR #4 EM
- [SDR SIMA20210920002](https://openairdocs.org/sdr/SIMA20210920002), Sep 20, 2021: NONE. NONE. HYDRAULIC #2 FAIL IN FLIGHTL. EMERGENCY DECLARED-C/A-FOUND #2 HYDRAULIC SYSTEM PRESSURE TRANSMITTER TO BE LEAKING. RAR TRANSMITTER O-RING PER AMM 29-30-02. OPER
- [SDR SIMA20210723002](https://openairdocs.org/sdr/SIMA20210723002), Jul 23, 2021: ROLLER. LACK OF LUBE. MAIN DOOR HARD TO OPEN GETS STUCK WHEN TRYING TO OPEN IT.-C/A-PERFORMED LUBRICATED MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02 OPS CK GOOD
- [SDR SIMA20210619003](https://openairdocs.org/sdr/SIMA20210619003), Jun 19, 2021: APU. FAILED. APU FAIL WHEN IT FAIL DISTINCT SMELL SMOKE SMELL IN CABIN-C/A-DEFERRED APU SYSTEM M PROCEURES C/W AUTH 060253DM-CREF 49-01
- [SDR SIMA20210526003](https://openairdocs.org/sdr/SIMA20210526003), May 26, 2021: BATTERY. FAULTED. FA EMERGENCY FLASHLIGHT FLICKERING ON AND OFF-C/A-RAR FA EMERGENCY FLASHLIGHT BATTERY IAW E145 AMM 33-50-16. OPS CKED GOOD. IAW E145 AMM 33-51-01
- [SDR SIMA20210515001](https://openairdocs.org/sdr/SIMA20210515001), May 15, 2021: CRADLE. DETACHED. FA EMEREGNCY FLASHLIGHT HOLDER BROKEN REF AML PAGE 4734410/1 MEL 25-32, AUTH# 05-196M-C.-C/A-R&R FA EMERGENCY FLASHLIGHT HOLDER & PERFORMED OPS CHECK IAW AMM 33
- [SDR SIMA20210401003](https://openairdocs.org/sdr/SIMA20210401003), Apr 1, 2021: ROLLER. LACK OF LUBE. MAIN CABIN DOOR HARD TO OPEN AND CLOSE. C/A-LUBRICATED MAIN CABIN DOOR GUIDE ROLLERS, OPS CHECK GOOD AS PER AMM 52-10-00.
- [SDR SIMA20200818 7004](https://openairdocs.org/sdr/SIMA20200818%207004), Aug 17, 2020: QUICK DISCONNECT. BROKEN. EMERGENCY FLOOR STRIP LIGHTING QUICK DISCONNECT BROKEN AT FLOOR BOARD PANEL 241BF. PERFORMED QUICK DISCONNECT REPLACEMENT AT EMERGENCY FLOOR STRIP LIGHTING IAW 
- [SDR SIMA202007187003](https://openairdocs.org/sdr/SIMA202007187003), Jul 17, 2020: ECU. MALFUNCTIONED. FLAP LOW SPEED MESSAGE DURING DESCENT. PERFORMED FIM 27-51-00-810-A, FOUND FECU BIT CODE 1110 CHANNEL 1 FAILURE. R & R FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-5
- [SDR SIMA2020042119001](https://openairdocs.org/sdr/SIMA2020042119001), Apr 19, 2020: WIRE. BROKEN. ROW 3 THRU 7 FLOOR PROXIMITY EMERGENCY LIGHTS ARE INOP.-C/A-REMOVED AND REPLACED #2 EMERGENCY BATTERY AND POWER SUPPLY IAW EMB 145 AMM 33-50-04, OP CHECK BAD. F
- [SDR SIMA2020041716011](https://openairdocs.org/sdr/SIMA2020041716011), Apr 16, 2020: DOOR SILL. CORRODED. SSI 53-20-10 LOWER SERVICE DOOR SILL CORRODED AROUND MULTIPLE NUTPLATE HOLES-C/A-REMOVED AND REPLACED LOWER SERVICE DOOR SILL IAW EMB 145 SRM 51-40-02 AND SRM 5
- [SDR SIMA2020041714007](https://openairdocs.org/sdr/SIMA2020041714007), Apr 14, 2020: GUIDE. CORRODED. SSI 53-20-10 AFT SERVICE DOOR CUTOUT CORRODED UNDER AFT LOWER TEFLON GUIDE-C/A-REMOVED AND RE[LACED AFT SERVICE DOOR CUTOUT UNDER AFT TEFLON GUIDE (FR 22 BTW ST
- [SDR SIMA20200413004](https://openairdocs.org/sdr/SIMA20200413004), Apr 13, 2020: SKIN. CORRODED. INTERNAL FUSELAGE SKIN CORROSION AT FR 11-12 BETWEEN STGR 20R-21R ON PREVIOUS BLEND.-C/A-ACCOMPLISHED PERMANENT REPAIR ON INTERNAL FUSELAGE SKIN CORROSION BETWE
- [SDR SIMA202004098005](https://openairdocs.org/sdr/SIMA202004098005), Apr 8, 2020: SUPPORT. CORRODED. DURING MBV INSPECTION, QA FOUND THE LH UPPER SEAT TRACK SUPPORT CORRODED AT FR 46 AROUND LOWER RIVETS-C/A-REMOVED AND REPLACED LH UPPER SEAT TRACK SUPPORT AT FR
- [SDR SIMA202004098002](https://openairdocs.org/sdr/SIMA202004098002), Apr 8, 2020: SUPPORT. CORRODED. DURING MBV INSPECTION, QA FOUND THE LH UPPER SEAT TRACK SUPPORT CORRODED AT FR 50 AROUND LOWER RIVETS-C/A-REMOVED AND REPLACED LH UPPER SEAT TRACK SUPPORT AT FR
- [SDR SIMA20200408001](https://openairdocs.org/sdr/SIMA20200408001), Apr 8, 2020: DOOR SILL. CORRODED. CORROSION FOUND ON CARGO DOOR SILL BETWEEN FR 65 AND FR 68-C/A-REMOVED AND REPLACED CARGO DOOR SILL BETWEEN FR 65 AND FR 68 IAW EMB 145 SRM 51-40-02. REPAIR PN 
- [SDR SIMA2020033130002](https://openairdocs.org/sdr/SIMA2020033130002), Mar 30, 2020: DOOR SEAL. CRACKED. DURING MBV INSPECTION, QA FOUND THE CARGO DOOR FWD LOWER SEAL FLANGE CRACKED-C/A-REMOVED AND REPLACED CARGO DOOR FWD LOWER SEAL FLANGE IAW EMB 145 SRM 51-20-03 
- [SDR SIMA2020042111004](https://openairdocs.org/sdr/SIMA2020042111004), Mar 11, 2020: WIRE. BROKEN. 1EA PROX LIGHT WITH ARROWS HAS BROKEN WIRES-C/A-COMPLETE:REMOVED AND REPLACED 1EA PROX LIGHT WITH ARROWS IAW EMB 145 AMM 33-50-12 SEE NRTC BOW340840 FOR FINAL I
- [SDR SIMA2020042111005](https://openairdocs.org/sdr/SIMA2020042111005), Mar 11, 2020: CONNECTOR. DISCONNECTED. LH OVERWING EXIT DOOR SMALL "EXIT" LIGHT IS INOP-C/A-COMPLETE:CONNECTED LH OVERWING EXIT DOOR SMALL EMERGENCY LIGHT CANNON PLUG/CONNECTOR IAW EMB 145 SWPM 20-50
- [SDR SIMA2020042111007](https://openairdocs.org/sdr/SIMA2020042111007), Mar 11, 2020: FLOOR SUPPORT. CRACKED. RH FLOOR SUPPORT AT FR 68 IS CRACKED-C/A-COMPLETE:REMOVED AND REPLACED RH FLOOR SUPPORT AT FR 68 IAW EMB 145 SRM 51-40-02.
- [SDR SIMA2020042111006](https://openairdocs.org/sdr/SIMA2020042111006), Mar 11, 2020: CONNECTOR. NOT SEATED. R/H OVERWING EMERGENCY LIGHT IS INOP.-C/A-COMPLETE:RE-SEATED CANNON PLUG TO R/H OVERWING EXTERIOR EMERGENCY LIGHT IAW EMB 145 SWPM 20-50-00 AND AMM 33-50-00. OP
- [SDR SIMA20200213001](https://openairdocs.org/sdr/SIMA20200213001), Feb 13, 2020: CABLE. LACK OF LUBE. EMERGENCY PARKING BRAKE DIFFICULT TO SET.-C/A-CLEANED AND LUBED PARKING BRAKE HANDLE / CABLE REF STD MTX PRACTICES.
- [SDR SIMA202001087003](https://openairdocs.org/sdr/SIMA202001087003), Jan 7, 2020: GCU. FAILED. ELECTRICAL SMOKE SMELL NOTICED IN COCKPIT-C/A-C/W FIM TASK 21-20-00-810-801-A. FOUND SMELL TO BE APU GCU CAUSE. REMOVED AND REPLACED APU GCU IAW EMB 145 MM 24-3
- [SDR SIMA20191227002](https://openairdocs.org/sdr/SIMA20191227002), Dec 27, 2019: CONTROLLER. MALFUNCTIONED. CLIMBING THROUGH FL280 CABIN PRESSURE JUMPED RAPIDLY INTO THE AMBER ON THE EICAS BY THE TIME WE ESTABLISHED A DESCENT IT WAS IN THE RED AND RISING. FOUND KNOB O
- [SDR SIMA201911130004](https://openairdocs.org/sdr/SIMA201911130004), Nov 10, 2019: CONTROLLER. FAILED. RTF CREW REPORTS AUTO PRESSURIZATION INOP, DECLRED EMERGENCY FLIGHT CONTINUED-C/A-ITEM DEFERRED PER MEL 21-17 AUTH# 110350DM-C "M" PROCUDERS C/W. REMOVED AND RE
- [SDR SIMA2019103029004](https://openairdocs.org/sdr/SIMA2019103029004), Oct 29, 2019: MAGNETIC SEAL. LEAKING. PARKED AT THE GATE, SHUTTING DOWN ENGINE #2 PRODUCED WHITE SMOKE AND A VERY STRONG ODER IN THE COCKPIT DURING TAXI. T/S PER ETN-EM-79-015. FOUND LTP SHAFT SEAL 
- [SDR SIMA201910074001](https://openairdocs.org/sdr/SIMA201910074001), Oct 4, 2019: SMOKE DETECTOR. FALSE ACTIVATION. CARGO SMOKE INDICATION IN FLIGHT, NO SIGNS OF ACTUAL SMOKE, CARGO FIRE BOTTLE DISCHARGED. REPLACED BAGGAGE FIRE BOTTLES IAW AMM26-23-01. PERFORMED OPS CHECK OF 
- [SDR SIMA20190916003](https://openairdocs.org/sdr/SIMA20190916003), Sep 16, 2019: SMOKE DETECTOR. MALFUNCTIONED. BAG SMOKE INDICATION ON EICAS. C/A-FLIGHT CREW PACARDED BAG SMOKE IND. REOPENED MEL 26-3 MEL AUTH# 090489D-C REF# 26-3 MOC# 628765. C/W WORK SCOPE PER REAPEATS.
- [SDR SIMA20190914001](https://openairdocs.org/sdr/SIMA20190914001), Sep 14, 2019: CONTROL PANEL. FAILED. BAGG SMOKE WARNING MSG PRESENTED SHORT FINAL APPROACH. CREW REPORTS FIRE BOTTLES USED IN BAGGAGE COMPARTMENT. C/A-DEFERRED BAG SMOKE DETECTION SYSTEM MEL AUTH# 
- [SDR SIMA20190913001](https://openairdocs.org/sdr/SIMA20190913001), Sep 13, 2019: SMOKE DETECTOR. MALFUNCTIONED. WHEN RELEASING THE PARKING BRAKE BAGG SMOKE MASTER CAUTION ILL. "TRANSFERRED TO NRWC # 606-MIA-02757" . -C/A-FOUND BAGGAGE FIRE BOTTLES DISCHARGED. REMOVED AND 
- [SDR SIMA2019082019002](https://openairdocs.org/sdr/SIMA2019082019002), Aug 19, 2019: PUMP. FAILED. HYD SYS 2 FAIL INFLIGHT. R & R HYD PUMP ASSY ON THE # 2 ENGINE IAW EMB145 AMM 29-10-03 OPS CHECK AND LEAK CHECK GOOD
- [SDR SIMA20190716002](https://openairdocs.org/sdr/SIMA20190716002), Jul 16, 2019: LIGHT. INOPERATIVE. RT OVERWING EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-07 OPS CHECK GOOD.
- [SDR SIMA20190709004](https://openairdocs.org/sdr/SIMA20190709004), Jul 9, 2019: CONNECTOR. BROKEN. NUMBER # 1 EMERGENCY LIGHT STRIP HAS BROKEN TERMINAL ON AIRCRAFT SIDE. C/A-REPAIRED #1 EMERGENCY LIGHT STRIP CONNECTOR IAW SWPM 20-21-00. OPERATIONAL TEST GOOD.
- [SDR SIMA20190315001](https://openairdocs.org/sdr/SIMA20190315001), Mar 15, 2019: TUBE. DEFECTIVE. BLD 1 LEAK INFLIGHT. "TRANSFERRED TO NRWC 606-ORD-02422" MM 841029. C/A- REMOVE AND REPLACED LT TUBE ASSY FWD OF PACK NR 1 VALVE PER AMM 36-11-09. PERFORMED OPC
- [SDR SIMA2019103121006](https://openairdocs.org/sdr/SIMA2019103121006), Jan 21, 2019: WIRE. DAMAGED. LH #5 EMERGENCY LITE STRIP ACFT SIDE HAS DAMAGED WIRE-C/A-COMPLETE:REPLACED LH #5 EMERGENCY LITE STRIP ACFT SIDE DAMAGED WIRE IAW EMB145 SWPM 20-21-00. SEE NRTC
- [SDR SIMA2019103121007](https://openairdocs.org/sdr/SIMA2019103121007), Jan 21, 2019: LIGHT. INOPERATIVE. TRANSFERRED FROM TSA LOG PAGE 363038 ITEM #1 FWD FLOOR EMERGENCY LITES INOP-C/A-COMPLETE:REMOVED AND INSTALLED #1 FWD FLOOR EMERGENCY LITE /WITH EXTRUSION IAW E
- [SDR SIMA2019103121005](https://openairdocs.org/sdr/SIMA2019103121005), Jan 21, 2019: LIGHT. DAMAGED. LH #6 EMERGENCY LIGHT STRIP SIDEWALL IS DAMAGED.-C/A-COMPLETE:RAR LH #6 EMERGENCY LIGHT STRIP EXTRUSION IAW EMB 145 AMM 33-50-12.
- [SDR RAIA2018052970002](https://openairdocs.org/sdr/RAIA2018052970002), May 27, 2018: EXTINGUISHER. LEAKING. AFT PORTABLE FIRE EXTINGUISHER LEAKING. R & R THE PORTABLE FIRE EXTINGUISHER.
- [SDR RAIA2018052970001](https://openairdocs.org/sdr/RAIA2018052970001), May 27, 2018: SEAL. LEAKING. NR 2 BLEED LEAK DURING FLIGHT. R & R THE BLEED SEALS AT 4, 16, 20, AND 22. NO OTHER LEAKS FOUND THIS TIME. OPS CHECKED GOOD.
- [SDR RAIA201706090001](https://openairdocs.org/sdr/RAIA201706090001), Jun 9, 2017: RIB. CRACKED. RIGHT SPAR 1 WING RIB NR 9 HAS CRACK AT SCREW HOLE. REPAIRED THE RIB.
- [SDR RAIA201706070001](https://openairdocs.org/sdr/RAIA201706070001), Jun 7, 2017: YOKE. CRACKED. LEFT ENGINE FORWARD LOWER YOKE CRACKED. ACOMPLISHED REPAIR OF LT LOWER ENGINE YOKE.
- [SDR RAIA201606100001](https://openairdocs.org/sdr/RAIA201606100001), Jun 5, 2016: MUFFLER. DISCONNECTED. LOUD BANG HEARD DURING APPROACH TO RDU. SMOKE SEEN FROM BELOW 10A. TURNING OFF BLEED AND PAC STOPPED SMOKE. FOUND LT PACK MUFFLER DISCONNECTED. SECURED MUFFLER.
- [SDR RAIA201605200002](https://openairdocs.org/sdr/RAIA201605200002), May 20, 2016: BULB. INOPERATIVE. CEILING EMERGENCY EXIT LIGHT AT ROW 7, LIGHT NR 16B, IS INOPERATIVE. R & R BULB IN CEILING EMERGENCY EXIT LIGHT AT ROW 7, LIGHT NR 16B. OPS CHECKED GOOD.

All 180: https://openairdocs.org/aircraft/N606AE/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/N606AE/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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