# N608LM: 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 AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030)
- 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: 145068
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 25, 1998
- Certificate issued: September 30, 2011
- Expires: September 30, 2027
- Mode S code: A7E5FD
- 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=608LM
- Page: https://openairdocs.org/aircraft/N608LM

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.

## ADs that may apply (OpenAirDocs): 104 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 AE-3007A)

- [AD 2020-16-13](https://openairdocs.org/ad/2020-16-13): Turbine Engine Compressor Section · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Aug 14, 2020
- [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 2013-26-06](https://openairdocs.org/ad/2013-26-06): High-pressure turbine (HPT) stage 2 wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Feb 7, 2014
- [AD 2011-22-03](https://openairdocs.org/ad/2011-22-03): Low-cycle fatigue cracks · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 4 more. Effective Nov 17, 2011
- [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 2004-04-05](https://openairdocs.org/ad/2004-04-05): Engine oil system · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Mar 9, 2004
- [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 99-03-03](https://openairdocs.org/ad/99-03-03): Full Authority Digital Engine Control (FADEC) · Rolls-Royce AE 3007A and AE 3007A1/1. Effective Feb 16, 1999
- [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 2010-19-01](https://openairdocs.org/ad/2010-19-01) (historical): High pressure turbine · Rolls-Royce AE 3007A. Effective Oct 27, 2010
- [AD 2009-08-51](https://openairdocs.org/ad/2009-08-51) (historical): High-pressure turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 6 more. Effective May 27, 2009
- [AD 2008-26-06](https://openairdocs.org/ad/2008-26-06) (historical): High-pressure turbine (HPT) · AE 3007A. Effective Jan 8, 2009
- [AD 2008-19-51](https://openairdocs.org/ad/2008-19-51) (historical): AE 3007A, AE 3007A1, AE 3007A1E and 5 more
- [AD 2001-08-15](https://openairdocs.org/ad/2001-08-15) (historical): Oil System · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective May 14, 2001
- [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 120: https://openairdocs.org/aircraft/N608LM/ads.md

## Information bulletins (advisory) (8 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 AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N608LM.

## FAA accident and incident reports

None matched to N608LM.

## Service difficulty reports (126, 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 HNAA2021083100437](https://openairdocs.org/sdr/HNAA2021083100437), Aug 31, 2021: WARNING MESSAGE. FALSE ACTIVATION. DURING CLIMBOUT, BLEED 1 LOW TEMP MSG IN ICING CONDITIONS. PERFORMED OPERATION CHECK OF THE AIR BLEED SYSTEM IAW AMM 36-00-00-700-806. NO DEFECTS NOTED COULD NO
- [SDR HNAA2021070600315](https://openairdocs.org/sdr/HNAA2021070600315), Jul 5, 2021: SIGN. INOPERATIVE. EMERGENCY LIGHT STRIP ON SIDEWALL PANEL AFT OF LH EMERGENCY EXIT WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY SIGN ASSEMBLY PANEL ON LH AFT UPPER SIDEWAL
- [SDR HNAA2021052000221](https://openairdocs.org/sdr/HNAA2021052000221), May 19, 2021: INVERTER. FAULTED. L/H SIDEWALL EMERGENCY EXIT SIDEWALL SIGN LIGHT INOP, JUST AFT OF EXIT OPENING. FOUND TO BE NUMBER 5 INVERTER IN CEILING TO BE FAULTY, REMOVED AND REPLACED NUMB
- [SDR HNAA2021022700063](https://openairdocs.org/sdr/HNAA2021022700063), Feb 24, 2021: SWITCH. MALFUNCTIONED. ENGINE NR 2 T/R DEPLOYED AT 85 TO 90 KNOTS ON TAKE OFF ROLL. ABORTED TAKEOFF. MAINTENANCE PERFORMED: MEL 24FEB21 09:04 ROA C05503 78-1 THRUST REVERSES C/W MAINT
- [SDR HNAA2021022500061](https://openairdocs.org/sdr/HNAA2021022500061), Feb 23, 2021: BLEED VALVE. FAILED. PDIS 608 36-11 2329701 23FEB21 ROA CLOSE ENG 1 BLEED VALVE FAIL WHEN AT FULL POWER. EICAS MESSAGE CLEARS WHEN POWER AT IDLE. FACT 23FEB21 23:11 ROA. R & R'D HIG
- [SDR HNAA2020102200288](https://openairdocs.org/sdr/HNAA2020102200288), Oct 20, 2020: INVERTER. INOPERATIVE. AISLE FLOOR SECTIONS 4-5 EMERGENCY LIGHTS INOPERABLE. MAINTENANCE: R & R NR 5 EMERGENCY LIGHT INVERTER, IAW AMM 33-50-11-000-801-A. OPERATIONS CHECK GOOD, OK FO
- [SDR HNAA2020030900091](https://openairdocs.org/sdr/HNAA2020030900091), Mar 7, 2020: FCU. MALFUNCTIONED. REJECTED TAKEOFF DUE TO FUEL 2 LO LEVEL WARNING MSG ON EICAS. WING TANK FUEL QTY INDICATIONS ON EICAS AND MFD NORMAL. MOC ISSUED MEL 28-12 WITH CREW. MAINTENANC
- [SDR HNAA2019120200373](https://openairdocs.org/sdr/HNAA2019120200373), Nov 27, 2019: WIRE. BROKEN. MDIS 608 33-50 2106261 27NOV19 LEX CLOSE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 12 INOP DUE TO BROKEN WIRE AND DAMAGED FIXTURE AT CONNECTOR. 42300 00 DEW OVERHEAD
- [SDR HNAA2019112700371](https://openairdocs.org/sdr/HNAA2019112700371), Nov 22, 2019: SPOILER SYS. MALFUNCTIONED. SPOILER FAIL MESSAGE ON DESCENT WITH STRONG LEFT ROLLING TENDENCY....FIX: INSPECTED AND CLEANED PROX SWITCH FOR SPOILER SYSTEM, NO DEFECTS NOTED.PERFORMED SPOIL
- [SDR HNAA2019110400341](https://openairdocs.org/sdr/HNAA2019110400341), Nov 3, 2019: ACTUATOR. FAULTY. PDIS 608 27-31 2128242 03NOV19 CLT CLOSE CONTROL COLUMN FEELS LIKE IT CATCHING ON SOMETHING WITH INCREASED FRICTION WHEN PULLED BACK ACCOMPANIED BY FAINT CLICKI
- [SDR HNAA2019050200133](https://openairdocs.org/sdr/HNAA2019050200133), Apr 30, 2019: LIGHT. INOPERATIVE. NDIS 608 33-51 0021800 30APR19 RIC CLOSE EMERGENCY EXIT AISLE ILLUMINATION LIGHT AT RT WING EXIT DOOR INOP. 36218 00 NGR FACT 30APR19 09:57 RIC R/R LAMP FOR PSU
- [SDR HNAA2019050200132](https://openairdocs.org/sdr/HNAA2019050200132), Apr 30, 2019: CONNECTOR. NOT SEATED. NDIS 608 33-51 0021790 30APR19 RIC CLOSE AISLE 12 EMERGENCY EXIT SIGN AFT PORTION NOT ILLUMINATED 36218 00 NGR FACT 30APR19 09:55 RIC RESEATED CONNECTORS FOR AF
- [SDR HNAA2019043000130](https://openairdocs.org/sdr/HNAA2019043000130), Apr 29, 2019: WARNING LIGHT. ILLUMINATED. PDIS 608 52-30 1869733 29APR19 PHL ASSGN ON CLIMBOUT, RECEIVED BAG DOOR OPEN INDICATION. RETURN TO FIELD. LARRYS HISTORY: NONE MEL 29APR19 22:27 PHL C11918 52-3
- [SDR HNAA2019041300099](https://openairdocs.org/sdr/HNAA2019041300099), Apr 5, 2019: SKIN. CORRODED. DURING HVY CHK MAINTENANCE FOUND CORROSION ON FUSELAGE INTERNAL SKIN UNDER FR 61 TEAR STRAP BETWEEN STGR 17L-18L. REPAIRED IAW SRM 53-31-01
- [SDR HNAA2019041100098](https://openairdocs.org/sdr/HNAA2019041100098), Apr 2, 2019: ROD END. DAMAGED. R/H AILERON ACTUATOR ROD END FITTING O/B HAT BUSHING HOLE OVERSIZED FOUND IN HVY CHK. INSTALLED BUSHING PER SRM 51-20-09
- [SDR HNAA2019040700091](https://openairdocs.org/sdr/HNAA2019040700091), Apr 1, 2019: DOOR SILL. CORRODED. DURING HVY CHK MAINTENANCE FOUND CORROSION AROUND SERVICE DOOR FWD SILL NUT PLATE HOLES. R&R.
- [SDR HNAA2019041300100](https://openairdocs.org/sdr/HNAA2019041300100), Mar 29, 2019: SKIN. DENTED. DISCREPANCY: DURING HVY CHK MAINTENANCE FOUND CARGO DOOR EXTERNAL SKIN HAS A DENT WITH A GOUGE ON THE FWD LOWER CORNER. CORRECTIVE ACTION: REPAIRED IAW ETD2019-
- [SDR HNAA2019041100097](https://openairdocs.org/sdr/HNAA2019041100097), Mar 29, 2019: HOUSING. CRACKED. DURING HVY CHECK CARGO DOOR EXTERNAL HANDLE CUTOUT IS CRACKED AT THE END. REPAIRED IAW SRM 52-30-01RE.
- [SDR HNAA2018082400205](https://openairdocs.org/sdr/HNAA2018082400205), Aug 23, 2018: UPLOCK. FAILED. PDIS 608 32-30 1576422 23AUG18 PHL CLOSE ON GEAR UP SELECTION LANDING GEAR DISAGREE MESSAGE D ISPLAYED ON EICAS AND LEFT GEAR DID NOT RETRACT CREW PERFORMED QRH
- [SDR HNAA2017081600275](https://openairdocs.org/sdr/HNAA2017081600275), Aug 14, 2017: ANTI-ICE VALVE. FAILED. IN ICING CONDITIONS, WING ANTI-ICE FAILED MESSAGE. CMC SHOWS WING 2 ANTI-ICE LEAK. PUSHED BUTTON OPEN INSCRIPTION SHOWED VALVE CLOSED DURING ICING IN AUTO MODE.
- [SDR HNAA2017062100210](https://openairdocs.org/sdr/HNAA2017062100210), Jun 16, 2017: ENGINE. FAILED. NR 1 ENGINE FAILURE DURING LANDING ROLLOUT. EICAS MESSAGES FOR NR 1 ENGINE EXCEEDANCE, HS VALVE NR 1 FAILED. CREW STATED A STRONG ELECTRICAL ODOR IN COCKPIT AND
- [SDR HNAA2017050700154](https://openairdocs.org/sdr/HNAA2017050700154), May 7, 2017: SWITCH. DIRTY. DURING TAKE OFF, RECEIVED A MASTER CAUTION EICAS MESSAGE FOR THE CARGO DOOR OPEN. ABORTED TAKE OFF AND RETURNED TO GATE. CLEANED AND LUBED FWD AND AFT CARGO DOO
- [SDR HNAA2017032000089](https://openairdocs.org/sdr/HNAA2017032000089), Mar 18, 2017: WARNING MESSAGE. FALSE ACTIVATION. ANTI ICE FAIL MESSAGE ILLUMINATED ON EICAS AT 65 KTS DURING TAKEOFF. THE TAKEOFF WAS ABORTED. GROUND RAN AIRCRAFT AND PERFORMED OPS CHECK IAW AMM 30-00-00. NO D
- [SDR HNAA2017021500051](https://openairdocs.org/sdr/HNAA2017021500051), Feb 10, 2017: PRESSURE SWITCH. FAILED. DURING CLIMBOUT, WING ANTI ICE FAIL EICAS CAUTION FOLLOWED BY ANTI ICE WARNING EICAS , COMPLIED WITH QRH AND MESSAGE DISAPPEARED SHORTLY BEFORE REAPPEARING. R &
- [SDR HNAA2017020800045](https://openairdocs.org/sdr/HNAA2017020800045), Feb 5, 2017: ANTI-ICE SYSTEM. MALFUNCTIONED. DURING DESCENT AT 66% POWER, WING ANTI ICE FAIL CAUTION LIGHT ILLUMINATED WITH NO ICE CONDITION. MESSAGE CHANGED TO ANTI ICE FAIL ICE CONDITION ON ENTERING ICE 
- [SDR HNAA2017020300038](https://openairdocs.org/sdr/HNAA2017020300038), Feb 3, 2017: PRESSURE SWITCH. MALFUNCTIONED. DURING CLIMB, NR 2 BLEED LEAK EICAS MESSAGE ILLUMINATED ALONG WITH PB LEAK ILLUMINATED. CLEARED MESSAGE. REMOVED AND REPLACED NR 2 LOW PRESSURE, OPS CHECKED OK 
- [SDR HNAA2017020300034](https://openairdocs.org/sdr/HNAA2017020300034), Feb 3, 2017: WARNING MESSAGE. FALSE ACTIVATION. AURAL TAKEOFF TRIM DURING TAKEOFF. TRIM WAS IN GREEN. COMPLIED WITH TASK 27-40-00-700-805-A. OPS CHECKED GOOD. OKAY FOR SERVICE.
- [SDR HNAA2016121200383](https://openairdocs.org/sdr/HNAA2016121200383), Dec 11, 2016: ANTI-ICE SYSTEM. NO TEST. DURING AN ANTI-ICE TEST IN FLIGHT, EICAS MESSAGE STAB ANTI ICE FAILED DISPLAYED. ATTEMPTED TEST 3 TIMES.
- [SDR SIMA20161119003](https://openairdocs.org/sdr/SIMA20161119003), Nov 19, 2016: FRAME. BENT. FRAME 72 IS BENT AT STRINGER 16R INSIDE CARGO. REMOVED AND REPLACED THE FRAME LOWER SECTION IAW SRM 51-40-02.
- [SDR SIMA20161114005](https://openairdocs.org/sdr/SIMA20161114005), Nov 14, 2016: RIB. CHAFED. LEFT WING RIB LOCATED BETWEEN 551CB AND 551DB, CHAFED UNDER THE PCA HOSES. REPAIRED THE RIB IAW ERS-EM-57MR-723.
- [SDR SIMA20161114004](https://openairdocs.org/sdr/SIMA20161114004), Nov 14, 2016: FRAME. CRACKED. OUTBOARD RIVET HOLE CRACKED ON LOWER END OF FRAME 66. REPAIRED THE FRAME IAW ERS-EM-53MR-2405.
- [SDR SIMA20161114003](https://openairdocs.org/sdr/SIMA20161114003), Nov 14, 2016: SHEAR TIE. CORRODED. FRAME 68 SHEAR TIE IS CORRODED AT CARGO DOOR CUT LOWER CORNER. REPAIRED THE SHEAR TIE IAW SRM 53-31-04.
- [SDR SIMA20161114002](https://openairdocs.org/sdr/SIMA20161114002), Nov 14, 2016: SHEAR TIE. CORRODED. FRAME 65 SHEAR TIE CORRODED BELOW CARGO LOWER GUIDE AND AT CARGO DOOR SILL . REPAIRED THE SHEAR TIE IAW SRM 53-31-04.
- [SDR SIMA20161112004](https://openairdocs.org/sdr/SIMA20161112004), Nov 12, 2016: SKIN. CRACKED. LEFT REAR FUSELAGE SKIN CRACKED AT FRAME 75, BETWEEN STRINGERS 1 AND 2L. REPAIRED THE SKIN IAW SRM 53-31-01.
- [SDR SIMA20161111004](https://openairdocs.org/sdr/SIMA20161111004), Nov 11, 2016: DOOR SILL. CORRODED. CARGO DOOR LOWER SILL CORRODED REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 53-40-02.
- [SDR SIMA20161111003](https://openairdocs.org/sdr/SIMA20161111003), Nov 11, 2016: STRINGER. CRACKED. STRINGER 6R CRACKED AT FRAME 13. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-02.
- [SDR SIMA20161111002](https://openairdocs.org/sdr/SIMA20161111002), Nov 11, 2016: FRAME. CRACKED. AFT CARGO DOOR CUTOUT FRAME 68 FRAME CRACKED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.
- [SDR SIMA20161111001](https://openairdocs.org/sdr/SIMA20161111001), Nov 11, 2016: DOOR FRAME. CORRODED. LEFT OVERWING EMERGENCY EXIT LOWER FRAME CORRODED AT AFT GUIDE BLOCK AND FWD GROUNDING CLIP. REMOVED AND REPLACED THE DOOR FRAME IAW SRM 51-40-02
- [SDR SIMA20161110003](https://openairdocs.org/sdr/SIMA20161110003), Nov 10, 2016: DOOR SILL. CORRODED. SERVICE DOOR CUTOUT LOWER CENTER SILL CORRODED. REPAIRED SERVICE DOOR CUTOUT LOWER CENTER SILL IAW EMB145 53-21-02, AND 51-20-03
- [SDR SIMA20161110004](https://openairdocs.org/sdr/SIMA20161110004), Nov 10, 2016: SKIN. CORRODED. FUSELAGE SKIN HAS CORROSION JUST AFT OF 123BL ACCESS PANEL BENEATH TCAS II ANTENNA, BETWEEN FRAMES 10 AND 11. REPAIRED THE SKIN IAW SRM 53-00-23.
- [SDR SIMA20161110002](https://openairdocs.org/sdr/SIMA20161110002), Nov 10, 2016: SKIN. CORRODED. FUSELAGE SKIN HAS CORROSION BENEATH TDR MODE-S ANTENNA, BETWEEN FRAMES 20 AND 21. REPAIRED THE SKIN IAW SRM 53-00-23.
- [SDR SIMA20161109003](https://openairdocs.org/sdr/SIMA20161109003), Nov 9, 2016: CONTACT. MISSING. LEFT NR 1 EMERGENCY LIGHT CONTACT MISSING. INSTALLED CONTACT IAW SWPM 20-00-03.
- [SDR SIMA20161025001](https://openairdocs.org/sdr/SIMA20161025001), Oct 25, 2016: YOKE. CRACKED. RT FWD LOWER YOKE CRACKED FWD UPPER EDGE. REMOVED AND INSTALLED SERVICEABLE YOKE IAW EO EM-54MR-386
- [SDR SIMA20161019013](https://openairdocs.org/sdr/SIMA20161019013), Oct 19, 2016: SKIN. CRACKED. UPPER LEFT FUSELAGE SKIN HAS TWO CRACKS, ONE CRACK IS JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L, AND 3/8 INCH LONG, AND THE OTHER CRACK IS AT FRAME 75 TOP FAST
- [SDR SIMA20161018004](https://openairdocs.org/sdr/SIMA20161018004), Oct 18, 2016: CHARGER. FAILED. LT AND RT EXTERIOR OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EPSU NR 4 IAW W/C 33-700-19 AND OPS CHECK GOOD IAW W/C 33-700-17. EMERGENCY LIGHTING BAT
- [SDR SIMA20161014001](https://openairdocs.org/sdr/SIMA20161014001), Oct 14, 2016: LIGHT. INOPERATIVE. LEFT WING EMEGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT AW AMM 33-50-10. OPS CHECKED GOOD.
- [SDR SIMA20160708006](https://openairdocs.org/sdr/SIMA20160708006), Jul 8, 2016: PUMP. FAILED. HYD2 LO QTY FOLLOWED BY HYD SYS 2 FAILED. REMOVED AND REPLACED ENGINE NR 2 HYDRAULIC EDP IAW EMB 145 AMM 29-10-03 PERFORMED LEAK AND OPS CHECK IAW AMM 72-00-00 
- [SDR SIMA20160627001](https://openairdocs.org/sdr/SIMA20160627001), Jun 27, 2016: BRAKE. FAILED. LEFT MAIN BRAKES ON FIRE, REPORTED BY TOWER, PERFORMED GROUND EVACUATION. REF ITEMS NR 1 AND NR 2 LOG PAGE 4036786, ITEMS NR 1,2 AND 3. NR 2 BRAKE FAILURE. R & 
- [SDR SIMA20160520003](https://openairdocs.org/sdr/SIMA20160520003), May 20, 2016: POWER SUPPLY. INOPERATIVE. LEFT & RIGHT OVERWING EMER LIGHTING INOPERATIVE. TROUBLE SHOT LT & RT OVERWING EMER LIGHTING & ISOLATED PROBLEM TO EMER BATTERY POWER SUPPLY. R & R EMER BATTERY
- [SDR SIMA20160130001](https://openairdocs.org/sdr/SIMA20160130001), Jan 30, 2016: GCU. FAILED. ON FINAL WE TURNED THE APU ON IAW MEL 24-4, ONCE APU ON LINE, RECVD GEN 1 - 4 OFF BUS, SHORTLY AFTER WE LOST EICAS FOR 5 - 10 SECONDS, GEN 1 WAS SHOWING 7.4 VOL

All 126: https://openairdocs.org/aircraft/N608LM/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/N608LM/stcs.md

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/aircraft.md
- The Allison AE-3007A engine: https://openairdocs.org/engine/allison-ae-3007a.md

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