# N11536: 2001 Embraer EMB-145LR

- Status: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212, 55 seats)
- Engine: [Rolls-Royce AE-3007A1P](https://openairdocs.org/engine/rolls-royce-ae-3007a1p) (registry code 54571)
- 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: 145520
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 19, 2001
- Certificate issued: October 14, 2023
- Expires: October 31, 2030
- Mode S code: A041A6
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, 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=11536
- Page: https://openairdocs.org/aircraft/N11536

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 (Rolls-Royce AE-3007A1P)

- [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 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 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 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 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 2003-25-08](https://openairdocs.org/ad/2003-25-08): 1st and 2nd stage turbine spacers · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 3 more. Effective Jan 21, 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 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 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 2008-19-51](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 118: https://openairdocs.org/aircraft/N11536/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 N11536.

## FAA accident and incident reports

None matched to N11536.

## Service difficulty reports (72, 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 ASOA2020040104011](https://openairdocs.org/sdr/ASOA2020040104011), Mar 31, 2020: BATTERY PACK. DISCHARGED. IAH DURING MAINTENACE INSPECTION THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY
- [SDR ASOA2020040104010](https://openairdocs.org/sdr/ASOA2020040104010), Mar 30, 2020: BATTERY PACK. DISCHARGED. IAH DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTS AFT OF THE EMERGENCY ROW WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT
- [SDR ASOA2020040104009](https://openairdocs.org/sdr/ASOA2020040104009), Mar 30, 2020: BATTERY PACK. DISCHARGED. IAH DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTS AFT OF THE EMERGENCY ROW WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT
- [SDR ASOA2020031614005](https://openairdocs.org/sdr/ASOA2020031614005), Mar 11, 2020: BAR. LOOSE. SDF - FLIGHT 4448 THE REW REPORTED THAT WHEN APU STARTED WITH THE ENGINES RUNNING HEARD A LOUD CRACKLING AND SMELL OF BURNT ELECTRICAL, ALSO HAPPENED DURING ENG
- [SDR ASOA2020031315010](https://openairdocs.org/sdr/ASOA2020031315010), Mar 11, 2020: TERMINAL. LOOSE. CREW REPORTED"WHEN APU IS STARTED WHILE THE ENGINES WAS RUNNING LOUD CRACKLING AND SMELL OF SMOKE AND BURNT AND ELECTRICAL ALSO HAPPENED DURING ENGINE SHUT DOWN
- [SDR ASOA2020013104001](https://openairdocs.org/sdr/ASOA2020013104001), Jan 30, 2020: BATTERY PACK. DISCHARGED. IAH FLIGHT 4385, THE CREW RPORTED THAT THE FLOOR EMERGENCY LIGHTS BETWEEN SEATS 8 AND 18 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EME
- [SDR ASOA201805252137](https://openairdocs.org/sdr/ASOA201805252137), May 22, 2018: TERMINAL. BURNED. CREW REPORTED SMOKE IN THE COCKPIT, VISIBLE SMOKE FROM THE LOWER LEFT CORNER OF FIRST OFFICERS WINDSHIELD. ACFT DIVERTED FROM DESTINATION AND LANDED SAFELY. MX 
- [SDR ASOA201706203203](https://openairdocs.org/sdr/ASOA201706203203), Jun 20, 2017: SKIN. CRACKED. RIGHT FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 2R. DAMAGE FOUND BY NDT INSPECTION. FUSELAGE SKIN REPAIRED WITH DOUBLER INSTSALLATION (9" X 10") IAW SRM 53-31
- [SDR ASOA201706193202](https://openairdocs.org/sdr/ASOA201706193202), Jun 19, 2017: BEAM. CORRODED. CARGO ENTRANCE LOWER BEAM CORRODED BEYOND LIMITS. CARGO ENTRANCE LOWER BEAM REPLACED IAW SRM 51-40-02.
- [SDR ASOA201706193201](https://openairdocs.org/sdr/ASOA201706193201), Jun 19, 2017: FITTING. CORRODED. CARGO AFT LATERAL L SHAPE CORRODED ON LOWER SECTION AT FRAME 68. THE L SHAPE WAS REPLACED IAW SRM 53-31-04.
- [SDR ASOA201706193200](https://openairdocs.org/sdr/ASOA201706193200), Jun 19, 2017: SUPPORT. CORRODED. PAX DOOR SILL SUPPORT CORRODED. THE SUPPORT WAS REPLACED.
- [SDR ASOA201706193199](https://openairdocs.org/sdr/ASOA201706193199), Jun 19, 2017: DOOR SILL. CORRODED. SERVICE DOOR LOWER SILL CORRODED. SERVICE DOOR SILL WAS REPLACED IAW SRM 51-40-02.
- [SDR ASOA201706193198](https://openairdocs.org/sdr/ASOA201706193198), Jun 19, 2017: BEARING CAP. CORRODED. NOSE LANDING GEAR LEG LOWER BEARING CAP CORRODED. THE BEARING CAP WAS REPLACED IAW 32-20-01.
- [SDR ASOA201706163197](https://openairdocs.org/sdr/ASOA201706163197), Jun 16, 2017: DOUBLER. CORRODED. CORROSION ON DOUBLER AROUND POTABLE WATER SERVICING NIPPLES. THE DOUBLER WAS REPLACED IAW SRM.
- [SDR ASOA201706163196](https://openairdocs.org/sdr/ASOA201706163196), Jun 16, 2017: SUPPORT BRACKET. CRACKED. SUPPORT BRACKET CRACKED ON THE CARGO DOOR BALANCE SPRING ASSEMBLY FORWARD OF FRAME 68. THE SUPPORT BRACKET WAS REPLACED IAW SRM 51-40-02.
- [SDR ASOA201706163195](https://openairdocs.org/sdr/ASOA201706163195), Jun 16, 2017: SEAT TRACK. CORRODED. LEFT OTBD SEAT TRACK NR 5 BETWEEN FRAMES 47 - 52 CORRODED. REPLACED THE SEAT TRACK IAW SRM 53-01-06.
- [SDR ASOA201706163194](https://openairdocs.org/sdr/ASOA201706163194), Jun 16, 2017: SEAT TRACK. CORRODED. LEFT OUTBOARD SEAT TRACK NR 4 BETWEEN FRAMES 36 - 47 CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06.
- [SDR ASOA201706163193](https://openairdocs.org/sdr/ASOA201706163193), Jun 16, 2017: FLOORBEAM. CRACKED. FLOORBEAM ANGLE AT FRAME 18 FOUND CRACKED. THE FLOORBEAM ANGLE WAS REPLACED IAW SRM 51-40-02.
- [SDR ASOA201706153192](https://openairdocs.org/sdr/ASOA201706153192), Jun 15, 2017: FLOORBEAM. CRACKED. FLOORBEAM ANGLE CRACKED AT FRAME 18. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-02.
- [SDR ASOA20150805027](https://openairdocs.org/sdr/ASOA20150805027), Aug 5, 2015: ACM. FAILED. DURING CRUISE, SMOKE APPEARED IN THE CABIN AND ODOR WAS ALSO OBSERVED. ACFT LANDED OK AND THEN WAS FERRIED, MAINTENANCE R & R THE NR 2 ACM IAW AMM 21-51-03, ALS
- [SDR ASOA20150802042R](https://openairdocs.org/sdr/ASOA20150802042R), Aug 2, 2015: ACM. SEIZED. AFTER TAKEOFF, AT 4000FT F/A CALLED AND STATED SMOKE IN THE CABIN. PILOT AND F/O COULD SEE SMOKE AND DECLARED EMERGENCY, RETURNED TO AIRPORT. MAINTENANCE INSPEC
- [SDR ASOA20150620030](https://openairdocs.org/sdr/ASOA20150620030), Jun 20, 2015: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHT FLOOR STRIP NR 3 WAS DISCOVERED INOPERATIVE. MAINTENANCE R & R NR 3 FLOOR LIGHT STRIP WITH OPS CHECK GOOD. AI
- [SDR ASOA20130508149V](https://openairdocs.org/sdr/ASOA20130508149V), May 8, 2013: BEAM. CORRODED. DURING C-CHECK CARGO DOOR CUTOUT LOWER BEAM 65-68 IS CORRODED (LOCAL LEVEL 2). MX PERFORMED REPAIR ON CARGO DOOR CUTOUT LOWER BEAM AT FRAMES 65-68 IAW SRM 51-40
- [SDR ASOA20130508148V](https://openairdocs.org/sdr/ASOA20130508148V), May 8, 2013: SEAT TRACK. CORRODED. DURING C-CHECK LT UPPER SEAT TRACK SUPPORT CORRODED. (LOCAL LEVEL 2) AT FRAME 50. MX PERFORMED REPAIR TO LT UPPER SEAT TRACK SUPPORT FRAME 50 IAW EC5320-01522, 
- [SDR ASOA20120507071](https://openairdocs.org/sdr/ASOA20120507071), May 8, 2012: SKIN. PUNCTURED. A SMALL PUNCTURE IN THE SKIN AT FRAME 10 NEAR STRINGER 14 NEXT TO THE TAT PROBE. MX PERFORMED A DOUBLER REPAIR ON THE AFFECTED SKIN, AND THE ACFT WAS APPROVED F
- [SDR C2XA11CL191](https://openairdocs.org/sdr/C2XA11CL191), Aug 17, 2011: FLAPPER VALVE. TORN. CLE FLT 3095 THE CREW REPORTED ON DEPARTURE FROM CLE THE TOWER INFORMED THEM OF A FLUID LOSS COMING FROM THE RIGHT WING. THE AIRCRAFT RETUNED TO CLE AND LANDED 
- [SDR C2XA11CL183](https://openairdocs.org/sdr/C2XA11CL183), Aug 6, 2011: CHECK VALVE. FAULTY. CLE FLT 2510 THE CREW REPORTED A ENGINE NR 2 BLEED LEAK MESSAGE ON CLIMB. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTE
- [SDR C2XA11TY075](https://openairdocs.org/sdr/C2XA11TY075), Jun 4, 2011: BRACKET. WORN. TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RT PCA BRACKET WORN OUT OF LIMITS. MAINTENACE R/R THE BRACKET IAE EC5750-01177. A/C WILL BE RELEASED AT
- [SDR C2XA11TY074](https://openairdocs.org/sdr/C2XA11TY074), Jun 4, 2011: BRACKET. WORN. TYS - A/C CURRENTLY IN C-CHECK WHERE INSPECTION FOUND THE LT AILERON BUSHIONS MISSING WHERE THE O/B PCA ROD ATTACHES. MAINTENANCE R/R THE PCA BRACKET IAW EC5750
- [SDR C2XA11CL072](https://openairdocs.org/sdr/C2XA11CL072), Mar 17, 2011: UNKNOWN. ODOR. ORD FLT 6144 THE CREW REPORTED A BURNING SMELL IN THE COCKPIT AND FORWARD CABIN ON TAXI IN. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE ANY BURNING SMELL. OPE
- [SDR C2XA10IA201](https://openairdocs.org/sdr/C2XA10IA201), Jul 7, 2010: RELAY. INOPERATIVE. ** REFERENCE SDR C2XA10IA192 **GPT - FLIGHT 2643, THE CREW REPORTED THAT PACK ONE WAS BLOWING HOT AIR. THE AIRCRAFT DIVERTED TO GPT WHERE IT LANDED WITHOUT INCI
- [SDR C2XA10IA192](https://openairdocs.org/sdr/C2XA10IA192), Jul 7, 2010: RELAY. INOPERATIVE. FLIGHT 2643, THE CREW REPORTED THAT NR 1 A/C PACK WAS BLOWING HOT AIR. THE AIRCRAFT DIVERTED TO GPT WHERE IT LANDED WITHOUT INCIDENT. THE COOLING SYSTEM WAS RES
- [SDR C2XA10RI076](https://openairdocs.org/sdr/C2XA10RI076), May 30, 2010: FAN. INOPERATIVE. FLIGHT 2381 - EWR - FLIGHT CREW REPORTED EXHAUST ELECTRONIC BAY FAN C/B POPPED IN FLIGHT. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED
- [SDR C2XA09CL054](https://openairdocs.org/sdr/C2XA09CL054), Apr 27, 2009: TURBINE WHEEL. CRACKED. DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASO
- [SDR C2XA08TY053](https://openairdocs.org/sdr/C2XA08TY053), May 23, 2008: BATTERY. DISCHARGED. NR 4 EMERGENCY BATTERY INOP. REMOVED AND REPLACED BATTERY IAW EMB 145 MM 33-50-04, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA08RI054](https://openairdocs.org/sdr/C2XA08RI054), Apr 21, 2008: INVERTER. INOPERATIVE. FLIGHT 2197 - EWR - FLIGHT CREW REPORTED FLOOR EMERGENCY LIGHTS SEAT ROW 17A INOPERATIVE. EWR MX REMOVED AND REPLACED NR 6 INVERTER AND PERFORMED OPERATIONAL CH
- [SDR C2XA08RI069](https://openairdocs.org/sdr/C2XA08RI069), Apr 11, 2008: SWITCH. FAULTY. FLIGHT 2988 - EWR - FLIGHT CREW REPORTED STRONG ELECTRICAL BURN SMELL WITH WINDSHIELD WIPER ACTIVATED. EWR MX REMOVED AND REPLACED LT WINDSHIELD WIPER SWITCH AN
- [SDR C2XA08CL020](https://openairdocs.org/sdr/C2XA08CL020), Feb 10, 2008: PROXIMITY SWITCH. FAULTY. CLE FLIGHT 2592 - THE CREW REPORTED A UNUSUAL LOAD SOUND FROM UNDER THE COCKPIT FLOOR ONLY IN CLIMB AND CRUISE. ALSO REPORTED A SLIGHT VIBRATION OF YOLK AND RUD
- [SDR C2XA08CL016](https://openairdocs.org/sdr/C2XA08CL016), Jan 31, 2008: PROXIMITY SWITCH. FAULTY. CLE FLIGHT 2409 THE CREW REPORTED A AIR/GROUND FAIL MESSAGE IN FLIGHT. THE LANDING GEAR WOULD NOT RETRACT, ALSO RECEIVED A ENG REV 1&2 DISAGREE MESSAGE ON THE E
- [SDR C2XA08CL017](https://openairdocs.org/sdr/C2XA08CL017), Jan 27, 2008: PROXIMITY SWITCH. OBSTRUCTED. MKE FLIGHT 2560 - THE CREW REPORTED A AIR/GROUND FAIL MESSAGE ON TAKEOFF. THE AIRCRAFT RETURNED TO MKE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CL
- [SDR C2XA07RI065](https://openairdocs.org/sdr/C2XA07RI065), Jul 19, 2007: SIGN. INOPERATIVE. FLT 2686 - EWR - CREW REPORTED GALLEY EMERGENCY LIGHT (SEAT 1A) INOP. EWR MX REMOVED AND REPLACED EMERGENCY SIGN AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. AC
- [SDR C2XA07SH037](https://openairdocs.org/sdr/C2XA07SH037), Jul 2, 2007: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM WITH CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FROM FRAMES 18 TO 24 IAW
- [SDR C2XA07CL023](https://openairdocs.org/sdr/C2XA07CL023), Feb 18, 2007: BATTERY. DISCHARGED. DURING ROUTINE MAINTENANCE THE OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE 
- [SDR C2XA07BT013](https://openairdocs.org/sdr/C2XA07BT013), Jan 31, 2007: BRAKE. MALFUNCTIONED. IND LOG SQUAWK FLT NR 2951 WITH PARKING BRAKE SET AIRCRAFT ROLLS. CYCLED NORMAL BRAKES SEVERAL TIMES AND PERFORMED OPS CHECK OF PARKING BRAKE SYSTEM IAW AMM 32-
- [SDR C2XA05SD030](https://openairdocs.org/sdr/C2XA05SD030), Dec 4, 2005: BATTERY. INOPERATIVE. SDF - EMERGENCY LIGHT OVER GALLEY DOOR INOP. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY AND BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD
- [SDR C2XA05SH093](https://openairdocs.org/sdr/C2XA05SH093), Aug 5, 2005: SKIN. DENTED. SHV - DURING C-CHECK MAINTENANCE FOUND RT EXTERNAL FUSELAGE HAS DENT AT FRAME 4, NEAR TOP FWD CORNER OF PANEL 114 CR. MAINTENANCE REPAIRED DENT IAW EC 5330-0148
- [SDR C2XA05SH092](https://openairdocs.org/sdr/C2XA05SH092), Aug 3, 2005: SKIN. LIGHTNING STRIKE. SHV - DURING C-CHECK LIGHTNING STRIKE INDICATION AT FR 16 STR 19R. MAINTENANCE REPAIR DAMAGE LIGHTNING STRIKE AT FR 16 STR 19R IAW EC 5330-01486. THE AIRCRAFT W
- [SDR C2XA05BT019](https://openairdocs.org/sdr/C2XA05BT019), Apr 6, 2005: WIRE HARNESS. DISCONNECTED. CREW REPORTED, EXIT ROW EMERGENCY LIGHT BURNED OUT OVER GALLEY DOOR. MAINTENANCE RECONNECTED THE CONNECTOR , OPS CHECKED GOOD IAW EMB145 AMM 33-50-00.
- [SDR C2XA05RI004](https://openairdocs.org/sdr/C2XA05RI004), Mar 9, 2005: LOGIC CARD. CORRUPTED. AFTER TAKEOFF, LG AIR/GROUND DISAGREE MESSAGE APPEARED ON EICAS. LANDING GEAR WOULD NOT RETRACT NORMALLY UNTIL OVERRIDE, THEN ENG 1-2 T/R DISAGREE MESSAGE APPEA
- [SDR C2XA05TY009](https://openairdocs.org/sdr/C2XA05TY009), Jan 27, 2005: CONNECTOR. DAMAGED. TYS, CONTINUATION OF CONTROL NR C2XA05TY008, AIR RETURN FOR LANDING GEAR AIR GROUND FAIL ON TAKEOFF. MAINTENANCE FOUND THE LEFT MLG FORWARD AND AFT WOW PROX SWI

All 72: https://openairdocs.org/aircraft/N11536/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/N11536/stcs.md

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/aircraft.md
- The Rolls-Royce AE-3007A1P engine: https://openairdocs.org/engine/rolls-royce-ae-3007a1p.md

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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.