# N605KS: 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: 145059
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 31, 1998
- Certificate issued: September 2, 2011
- Expires: September 30, 2027
- Mode S code: A7DAC4
- 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=605KS
- Page: https://openairdocs.org/aircraft/N605KS

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/N605KS/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 N605KS.

## FAA accident and incident reports

None matched to N605KS.

## Service difficulty reports (153, 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 SIMA20211223001](https://openairdocs.org/sdr/SIMA20211223001), Dec 23, 2021: NONE. NONE. MAIN DOOR EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. NO DEFECTS NOTED. E
- [SDR SIMA20211115001](https://openairdocs.org/sdr/SIMA20211115001), Nov 15, 2021: WARNING MESSAGE. FALSE ACTIVATION. TAKEOFF 1000 CLIMBING 115 VAC BUS OFF CAUTION LOSE EICAS INDICATIONS ITT, N1, T/O, N2. PPH, FLAPS, GEAR ALL YELLOW DASH RUN QRH. SPS 1/2 INOP WARNING ON CLIMBOU
- [SDR SIMA20211103007](https://openairdocs.org/sdr/SIMA20211103007), Nov 3, 2021: NONE. NONE. BLEED 2 LEAK WARNING MESSAGE DECLARED EMERGENCY FLIGHT CONT.-C/A-CHECKED ORINGS ON#2 BLEED SYSTEM #2 THROUGH #26 AND FOUND NO LEAKS PER ETN EM-36-048 AND RAN #2
- [SDR SIMA20211019001](https://openairdocs.org/sdr/SIMA20211019001), Oct 19, 2021: NONE. NONE. "TRANSFERRED FROM AML PAGE 4607688 ITEM 2" REF. ITEM 1 OF THIS LG. PG. INSPECTED F/O'S DV WINDOW AND FOUND F/O'S DV WINDOW FUSELAGE FRAME CRACKED AT FWD LOWER C
- [SDR SIMA20211007003](https://openairdocs.org/sdr/SIMA20211007003), Oct 7, 2021: NONE. NONE. MAIN DOOR EMERGENCY LIGHT INOP.-C/A-RAR MAIN DOOR EMERGENCY LIGHT IAW EMB 145 AMM 33-50-06 OCK GOOD
- [SDR SIMA20210619004](https://openairdocs.org/sdr/SIMA20210619004), Jun 19, 2021: THERMAL SWITCH. FAULTED. BLEED 2 LEAK MESSAGE DURING CLIMB MESSAGE REMAINED DESPITE COMPLETING QRH PROCEDURE-C/A-FOLLOWED FIM TASK 36-20-00-800-802-A, DETERMINED ITS A FAULTY THERMAL SW
- [SDR SIMA20210517001](https://openairdocs.org/sdr/SIMA20210517001), May 17, 2021: O-RING. LEAKING. BLEED 2 LEAK CLIMBING THROUGH APROX 8000' EXECUTED CHECKLISTS RETURNED TO DFW W/' UNDERWEIGHT LANDING DECLARED EMERGENCY-C/A-FOUND #25 BLEED SYSTEM JOINT HISSIN
- [SDR SIMA20210415004](https://openairdocs.org/sdr/SIMA20210415004), Apr 15, 2021: WARNING MESSAGE. FALSE ACTIVATION. BLD 2 LEAK ON CLIMB OUT DECLARED EMERGENCY -C/A-SUSPECT BAD DUCT LEAK DETECTOR.PERFORMED CONTINUITY TEST FORM CONNECTOR J1020 PN A-6 TO GROUND IAW SWPM 20-20-03
- [SDR SIMA20210322004](https://openairdocs.org/sdr/SIMA20210322004), Mar 22, 2021: WARNING MESSAGE. FALSE ACTIVATION. BLEED 2 LEAK CLIMBING OUT OF 10K' RAN QRH, NO REMEDY, DIVERTED TO ABI, NORMAL LNG @ 43.5K LBS. UPON PARKING WE SAW THE MESSAE CLEAR AND THEN REAPPEAR 2X. ACCOMP
- [SDR SIMA20210320001](https://openairdocs.org/sdr/SIMA20210320001), Mar 20, 2021: LAMP. INOPERATIVE. FOUND MAIN DOOR EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP IN REF WITH EMB 145 AMM 33-50-10. OPS CHECK GOOD.
- [SDR SIMA20210227001](https://openairdocs.org/sdr/SIMA20210227001), Feb 27, 2021: BULB. INOPERATIVE. R/H EXTERIOR EMEREGNCY LIGHT FORWARD OF WING INOP-C/A-RAR BULB PER AMM 33-50-10.
- [SDR SIMA20210211001](https://openairdocs.org/sdr/SIMA20210211001), Feb 11, 2021: LAMP. INOPERATIVE. DURING PS-1 CHECK FOUND RH FOWAD LOWER FAIRING EMERGENCY LIGHT INOP.-C/A-RAR RH FOWARD LOWER FAIRING EMERGENCY LIGHT LAMP IAW 33-50-10
- [SDR SIMA20210108001](https://openairdocs.org/sdr/SIMA20210108001), Jan 8, 2021: CRADLE. BROKEN. AFT EMERGENCY CABIN FLASHLIGHT CRADLE BROKEN MEL 2553-AUTH NR 01-85-C. C/A: R & R AFT EMERGENCY CABIN FLASHLIGHT CRADLE, IAW EMB AMM 33-50-16-000-801-A AND 33-5
- [SDR SIMA20210104002](https://openairdocs.org/sdr/SIMA20210104002), Jan 4, 2021: CRADLE. BROKEN. AFT CABIN EMERGENCY FLASHLIGHT CRADLE BROKEN. C/A: DEFFERED PER MEL 25-53.
- [SDR SIMA20201231003](https://openairdocs.org/sdr/SIMA20201231003), Dec 31, 2020: SWITCH. MALFUNCTIONED. BLEED 2 LEAK. DECLARED EMERGENCY "TRANSFERRED TO NRWC 605-DFW-03237". C/A: REPLACED ENGINE START GROUND CONNECTION LEAK SWITCH S7263, PER MM 36-20-02. OPERATION
- [SDR SIMA20201104001](https://openairdocs.org/sdr/SIMA20201104001), Nov 4, 2020: CRADLE. BROKEN. FLIGHT ATTENDANT FORWARD EMERGENCY FLASH LIGHT INOPERABLE. MEL 2553-AUTH NR 110047-C. C/A: FOUND F/A'S FWD EMERGENCY FLASH LIGHT HOLDER BROKEN. R & R F/A'S FLAS
- [SDR SIMA20200922002](https://openairdocs.org/sdr/SIMA20200922002), Sep 22, 2020: LAMP. INOPERATIVE. FWD RT EXTERIOR EMERGENCY LIGHT INOP. C/A: R&R EXTERNAL EMERGENCY LIGHT LAMP, IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD, IAW EMB 145 AMM 33-50-00.
- [SDR SIMA202005042001](https://openairdocs.org/sdr/SIMA202005042001), May 2, 2020: SIGN. UNSECURE. EMERGENCY EXIT SIGN ON CEILING NEXT TO THE GALLEY IS FALLEN DOWN AND HANGING BY WIRES-C/A-SECURED EXIT SIGN IN PLACE, PERFORMED OPS CHECK. IAW AMM 33-50-00. OPS
- [SDR SIMA2020031312003](https://openairdocs.org/sdr/SIMA2020031312003), Mar 12, 2020: LIGHT. INOPERATIVE. MAIN DOOR EXTERNAL EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED MAIN DOOR EXTERNAL EMERGENCY LIGHT IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC 
- [SDR SIMA202002141002](https://openairdocs.org/sdr/SIMA202002141002), Feb 11, 2020: CHARGER. FAILED. EMERGENCY LIGHT AT LH EMERGENCY DOOR IS INOP-C/A-RAR BATTERY POWER SUPPY #3 IAW 33-50-04 AND REMOVED AND REPLACED LH EMERGENCY DOOR EXIT IDENTIFIER SIGN IAW 33-
- [SDR SIMA202001298003](https://openairdocs.org/sdr/SIMA202001298003), Jan 28, 2020: SKIN. DENTED. DURING MBV INSPEECTION, QC FOUND A DENT BETWEEN FRAMES 4-5, STRINGERS 11R-14R-C/A-REPAIRED DENT BETWEEN FRAMES 4-5 AND STRINGERS 11R-14R IAW ERS-EM-53MR- 4022.
- [SDR SIMA202001276004](https://openairdocs.org/sdr/SIMA202001276004), Jan 26, 2020: PROFILE. CORRODED. DURING MBV INSPECTION, QC FOUND CORROSION ON THE PAX DOOR LOWER NUT PLATE HOLE.-C/A-REPAIRED CORROSION ON PAX DOOR LOWER NUT PLATE HOLE IAW EMB 145 SRM 52-10-02
- [SDR SIMA202001275004](https://openairdocs.org/sdr/SIMA202001275004), Jan 25, 2020: FLOOR SUPPORT. CORRODED. DURING MBV INSPECTION, QC FOUND THE GALLEY LH FLOOR BEAM CORRODED AT CARBON CROSS MEMBER AT FR 20.-C/A-REPAIRED GALLEY LH FLOOR BEAM AT CARBON CROSS MEMBER AT F
- [SDR SIMA202001273003](https://openairdocs.org/sdr/SIMA202001273003), Jan 23, 2020: CHANNEL. CORRODED. DURING MBV INSPECTION, QC FOUND THE SERVICE DOOR CENTER SILL CORRODED AT PREVIOUS BLENDED AREAS.-C/A-REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW EMB 145 S
- [SDR SIMA202001272006](https://openairdocs.org/sdr/SIMA202001272006), Jan 22, 2020: WEB. GOUGED. DURING MBV INSPECTION, QC FOUND 2 PREVIOUS REPAIR DOUBLERS ON CARGO DOOR INNER SKIN WEB WITH GOUGES-C/A-REMOVED AND REPLACED 2 PREVIOUS REPAIR DOUBLERS ON CARGO
- [SDR SIMA202001272005](https://openairdocs.org/sdr/SIMA202001272005), Jan 22, 2020: SKIN. CRACKED. DURING MBV INSPECTION, QC FOUND THE CARGO DOOR HANDLE CUTOUT CRACKED AT AFT UPPER END.-C/A-CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLER TO CARGO DOOR HANDLE 
- [SDR SIMA202001272004](https://openairdocs.org/sdr/SIMA202001272004), Jan 22, 2020: PROFILE. CORRODED. DURING MBV INSPECTION, QC FOUND THE CARGO DOOR LOWER PROFILE NUT PLATE HOLES CORRODED.-C/A-REMOVED AND REPLACED CARGO DOOR LOWER PROFILE IAW EMB 145 SRM 51-40-0
- [SDR SIMA202001272007](https://openairdocs.org/sdr/SIMA202001272007), Jan 22, 2020: BEAM. CRACKED. DURING MBV INSPECTION, QC FOUND THE CARGO DOOR INNER BEAM ON VB4 BETWEEN HB3 AND HB4 CRACKED.-C/A-REMOVED AND REPLACED CARGO DOOR INNER BEAM ON VB4 BETWEEN HB3 
- [SDR SIMA2020021131010](https://openairdocs.org/sdr/SIMA2020021131010), Dec 31, 2019: LIGHT. DAMAGED. 8EA FLOOR PROXIMITY LIGHT PANELS DAMAGED-C/A-COMPLETE:REMOVED AND REPLACED ALL FLOOR PROXIMITY LIGHT PANELS IAW EMB 145 AMM 33-50-12.
- [SDR SIMA2020021131006](https://openairdocs.org/sdr/SIMA2020021131006), Dec 31, 2019: LIGHT. DAMAGED. #2, #4, #6, #7, AND #8 FLOOR PROXIMITY LIGHT STRIPS DAMAGED-C/A-COMPLETE:REMOVED AND REPLACED #2, #4 , #6, #7, AND #8 FLOOR PROX LIGHT STRIPS IAW EMB-145 AMM 33
- [SDR SIMA2020021123107](https://openairdocs.org/sdr/SIMA2020021123107), Dec 31, 2019: LIGHT. BROKEN. RH CABIN FLOOR EMERGENCY LIGHT STRIPS BROKEN (5 EA)-C/A-COMPLETE:REMOVED AND REPLACED 5 RH FLOOR EMERGNCY LIGHT STRIPS AS REQUIRED.
- [SDR SIMA2020021131008](https://openairdocs.org/sdr/SIMA2020021131008), Dec 31, 2019: LIGHT. INOPERATIVE. EMERGENCY LIGHT UNDER PANEL 233BLC AND COCKPIT STEP UP PANEL INOP-C/A-COMPLETE:REMOVED AND REPLACED WARDROBE EMERGENCY LIGHTS DC/AC INVERTER IAW EMB 145 AMM 33-
- [SDR SIMA2020021123009](https://openairdocs.org/sdr/SIMA2020021123009), Dec 31, 2019: LIGHT. BROKEN. LH ANGLE EMERGENCY LIGHT STRIP FOR PANEL 231FF IS BROKEN-C/A-COMPLETE:REMOVED AND REPLACED LH ANGLE EMERGECNY LIGHT STRIP FOR PANEL 231FF IAW EMB 145 AMM 33-50-
- [SDR SIMA20191102001](https://openairdocs.org/sdr/SIMA20191102001), Nov 2, 2019: ACM. FAILED. AT CRUISE FL 240 FA REPORTED PASSENGERS AT SEAT 11 B/C WERE REPORTING NOISES COMINF FROM LOWER RIGHT SIDE FOLLOWED BY CABIN SMOKE MERGENCY WAS DECLARED AND EMER
- [SDR SIMA20191101002](https://openairdocs.org/sdr/SIMA20191101002), Nov 1, 2019: VALVE. FAILED. #1 PACK OVLD AND #1 PACK VALVE FAIL IN FLIGHT CLIMBING THROUGH FL340. QRH PROCEDURE FOLLOWED.-C/A-FLIGHT CREW PLACARDED #1 PACK. MEL# 21-28 AUTH# 110034D-C MOC#
- [SDR SIMA20191031003](https://openairdocs.org/sdr/SIMA20191031003), Oct 31, 2019: LIGHT. INOPERATIVE. FWD MOST CENTER CEILING EMERGENCY LIGHT IN CABIN INOP-C/A-REMOVED AND REPLACED FWD MOST CENTER CEILING EMERGENCY LIGHT IN CABIN IAW AMM TASK 33-50-08-000-801-A 
- [SDR SIMA201910287001](https://openairdocs.org/sdr/SIMA201910287001), Oct 27, 2019: DUCT. INOPERATIVE. PACK 1 OVRLD MESSAGE IN FLIGHT COMPLETED QRH, PAX NOTED NOISE & SMELL IN CABIN-C/A-REMOVED AND REPLACED DUCT IAW AMM TASK 21-51-01.
- [SDR SIMA20190908002](https://openairdocs.org/sdr/SIMA20190908002), Sep 8, 2019: LIGHT. INOPERATIVE. MAIN DOOR EXTERIOR EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED MAIN DOOR EXTERIOR EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS
- [SDR SIMA20190828001](https://openairdocs.org/sdr/SIMA20190828001), Aug 28, 2019: FAN. FAILED. STRONG FOUL ODOR COMING FROM RUNNING THE PACKS-C/A-FOUND STRONG ODOR COMING FROM GASPERFAN (PAX VENTS AND COCKPIT VENTS) DEFERED GASPER FAN AS PER MEL 21-4 (M) 
- [SDR SIMA20190725001](https://openairdocs.org/sdr/SIMA20190725001), Jul 25, 2019: SPAR. CRACKED. CRACK IN AFT SPAR 6.1 INCHES LONG LT IB FLAP. C/A-REPAIRED IAW ERS-EM-57MR-1140 PART A.
- [SDR SIMA20190508002](https://openairdocs.org/sdr/SIMA20190508002), May 8, 2019: WARNING SYSTEM. FALSE ACTIVATION. BLEED 2 LEAK IN CLIMBOUT. C/A-PERFORMED LEAK CHECK OF NR 2 BLEED SYSTEM IAW MM 36-00-00 AND ETNEM-36-063. OPS CK AND LEAK CHECK GOOD,
- [SDR SIMA20190401101](https://openairdocs.org/sdr/SIMA20190401101), Mar 29, 2019: WARNING LIGHT. FALSE INDICATION. PACK 1 OVERLOAD DURING T/O ROLL. T/S PACK 1 OVERLOAD PER FIM TASK EMB145 FIM 21-51-00-810-801A STEPS 1-3 FOUND TO BE A TRANSITORY CONDITION OF THE A/C SYSTEM. P
- [SDR SIMA20190310004](https://openairdocs.org/sdr/SIMA20190310004), Mar 10, 2019: SKIN. CRACKED. RT FUSELAGE SKIN CRACKED AT FR 12A STR 6R. C/A-PERFORMED PERMANENT REPAIR RT FUSELAGE SKIN CRACKED AT FR 12A STR 6R IAW ERS-EM-53MR-3701.
- [SDR SIMA20190310003](https://openairdocs.org/sdr/SIMA20190310003), Mar 10, 2019: SKIN. CRACKED. RT WINDSHIELD LATERAL POST UPPER SKIN CRACKED BETWEEN WINDSHIELD AND DV WINDOW OPENING. C/A-PERFORMED PERMANENT REPAIR ON RT WINDSHIELD LATERAL POST UPPER SKIN 
- [SDR SIMA20190309002](https://openairdocs.org/sdr/SIMA20190309002), Mar 9, 2019: CONNECTOR. BROKEN. EMERGENCY FLOOR LIGHT STRIP AT PANEL 241BF HAS BROKEN CONNECTORS. C/A-REPLACED BROKEN CONNECTORS ON EMERGENCY FLOOR LIGHT STRIP AT 241BF IAW SWPM 20-21-00 AND 2
- [SDR SIMA20190307005](https://openairdocs.org/sdr/SIMA20190307005), Mar 7, 2019: SKIN. DENTED. FWD FUSELAGE 1 RT SKIN HAS DENT AT FR 4 BETWEEN STR 4R-6R. C/A-PERFORMED PERMANENT REPAIR ON FWD FUSELAGE 1 RT SKIN AT FR 4 AND STR 4R-6R IAW ERS-EM-53MR-3690.
- [SDR SIMA20190307003](https://openairdocs.org/sdr/SIMA20190307003), Mar 7, 2019: FRAME. DENTED. FRAME 4 BENT BETWEEN STR 4R AND 6R. C/A-PERFORMED PERMANENT REPAIR ON FR 4 AND STR 4R-6R IAW ERS-EM-53MR-3690.
- [SDR SIMA20190303006](https://openairdocs.org/sdr/SIMA20190303006), Mar 3, 2019: SKIN. DENTED. DENT FWD OF CARGO DOOR BUMPER. C/A-PERFORMED PERMANENT REPAIR OF THE DENT FWD OF CARGO DOOR BUMBER IAW SRM 53-31-01.
- [SDR SIMA20190303005](https://openairdocs.org/sdr/SIMA20190303005), Mar 3, 2019: SUPPORT. CRACKED. RT OMEGA BEAM INBD SUPPORT CRACKED AT FWD END OF REPLACEMENT PIECE BETWEEN FR47 AND FR48. C/A-REMOVED AND REPLACED RT OMEGA BEAM IAW SRM 53-23-02.
- [SDR SIMA20190226004](https://openairdocs.org/sdr/SIMA20190226004), Feb 26, 2019: SHUNT. CORRODED. CORROSION ON APU CONNECTING BAR MOUNTING SUFACE SHUNT. C/A-PERFORMED PERMANENT REPAIR ON APU CONNECTING BAR SHUNT AND FR 80 IAW ERS-EM-53MR-3675.

All 153: https://openairdocs.org/aircraft/N605KS/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/N605KS/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

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