# N11539: 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: 145536
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 7, 2001
- Certificate issued: August 18, 2022
- Expires: August 31, 2029
- Mode S code: A041A9
- Registered owner: [Delux Public Charter LLC](https://openairdocs.org/faa-owner/DELUX%20PUBLIC%20CHARTER%20LLC)
- Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas)
- Owner type: LLC
- Owner's area on the map: 32.8483° N, 96.8255° W: Placed by OpenAirDocs at the center of ZIP code 75209, 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=11539
- Page: https://openairdocs.org/aircraft/N11539

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/N11539/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 N11539.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20040202002289I](https://openairdocs.org/incident/20040202002289I), Feb 2, 2004: Emb EMB145LR (N11539), Grand Rapids, MI. (-23) After landing on the snow covered runway the flight was cleared by ATCT to take any left turn and taxi to the ramp. After referring to the taxi diagram,…

## Service difficulty reports (67, 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 ASOA2019123045119](https://openairdocs.org/sdr/ASOA2019123045119), Dec 24, 2019: UNKNOWN. ODOR. PILOT REPORTED SMOKE ODOR IN FLIGHT DECK AFTER STARTING APU. MX PERFORMED A FEW APU STARTS NO SMOKE OR ODOR DETECTED IN FLIGHT DECK. ACFT WAS APPROVED FOR RETUR
- [SDR ASOA2019121864066](https://openairdocs.org/sdr/ASOA2019121864066), Dec 16, 2019: ENGINE. FAILED. IAH - FLIGHT 4047 THE CREW REPORTED THAT INITIATED CLIMB OUT AT 5000FT WHEN THRUST LEVER WAS ADVANCED #2 ENGINE FLAMED OUT. EICAS MESSAGE PRESENTED SHORTLY AFTE
- [SDR ASOA20191115111](https://openairdocs.org/sdr/ASOA20191115111), Nov 11, 2019: BATTERY PACK. INOPERATIVE. MX REPORTED CABIN EMERGENCY LIGHTS INOP. MX REMOVED AND REPLACED EMERGENCY BATTERIES 1&2 WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20191115110](https://openairdocs.org/sdr/ASOA20191115110), Nov 11, 2019: BULB. BURNED OUT. MX REPORTED THE LEFT AND RIGHT FWD OVER WING EMERGENCY LIGHTS INOP. MX RE-LAMPED EMERGENCY LIGHTS WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2019081314044](https://openairdocs.org/sdr/ASOA2019081314044), Aug 11, 2019: ACM. INOPERATIVE. MAINTENANCE RECORDED THAT THE FLIGHT CREW COMPLAINED ABOUT SMOKE / ELECTRICAL BURNING SMELL IN THE COCKPIT AND CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND FOU
- [SDR ASOA201908073041](https://openairdocs.org/sdr/ASOA201908073041), Aug 3, 2019: MUFFLER. DIRTY. FLIGHT 4478 THE CREW REPORTED A BURNING EXHAUST ODOR IN AC PACKS/GASPERS WITH THE SMELL OCCURRING MULTIPLE TIMES DURING DESCENT WITH THE ENGINES AT IDLE. THE AI
- [SDR ASOA201907207074](https://openairdocs.org/sdr/ASOA201907207074), Jul 19, 2019: BUSHING. DAMAGED. LT HORIZONTAL STABILIZER I/B AND O/B HINGE PIN LUGS STATIONARY HAT BUSHINGS DAMAGED. REMOVED BUSHINGS, REAMED TO 1ST OVERSIZE AND INSTALLED NEW BUSHINGS. AIRCRA
- [SDR ASOA201907207073](https://openairdocs.org/sdr/ASOA201907207073), Jul 19, 2019: BUSHING. DAMAGED. RT HORIZONTAL STAB I/B HINGE PIN LUGS STATIONARY BUSHING MIGRATED AND DAMAGED. REMOVED BUSHINGS AND REAMED TO 4TH REWORK AND INSTALLED NEW BUSHINGS.
- [SDR ASOA2019062195080](https://openairdocs.org/sdr/ASOA2019062195080), Jun 19, 2019: BULB. INOPERATIVE. DURING MX INSPECTION THE ROW 23 CEILING EMERGENCY LIGHT WAS FOUND INOP. MX R/R LIGHT BULB WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201905205070](https://openairdocs.org/sdr/ASOA201905205070), May 20, 2019: CONTROLLER. FAULTY. WINDSHIELD HEAT 2 FAIL ON T/O LOUD CLICKING FROM RELAY FOLLOWED BY STRONG BURNT SMELL. REMOVED AND REPLACED WINDSHIELD NR 2 TEMP CONTROLLER IAW AMM 30-42-01. OP
- [SDR ASOA201812051323](https://openairdocs.org/sdr/ASOA201812051323), Dec 1, 2018: BATTERY PACK. DISCHARGED. DURING MX INSPECTION THE FIRST 3 SETS OF INTERIOR EMERGENCY LIGHTS AND RH LOWER EXTERIOR EMERGENCY LIGHT TURNS ON AND FADES OFF. MX REMOVED AND REPLACED #2 EMER
- [SDR ASOA2018090414046](https://openairdocs.org/sdr/ASOA2018090414046), Aug 31, 2018: SKIN. CRACKED. IAH - DURING MAINTENANCE INSPECTION A PREVIOUS REPAIR TO THE FUSELAGE SKIN AT FR21-22 STR 10L-11L WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE DAMAGED SECTI
- [SDR ASOA201807105162](https://openairdocs.org/sdr/ASOA201807105162), Jul 10, 2018: LIGHT. MALFUNCTIONED. PILOT REPORTED THE EMERGENCY LIGHT INSIDE EXIT ROW WAS NOT ILLUMINATING. MX PREFORMED A SYSTEM RESET AND PERFORMED OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR 
- [SDR ASOA201804134021](https://openairdocs.org/sdr/ASOA201804134021), Apr 13, 2018: CONTROL MODULE. INOPERATIVE. THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT COME ON WITH THE F/A CONTROL PANEL. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANT CONTROL MODULE, 
- [SDR ASOA201804124022](https://openairdocs.org/sdr/ASOA201804124022), Apr 12, 2018: CONTROL MODULE. MALFUNCTIONED. GRK - THE CREW REPORTED A BURNING SMELL ABOVE SEAT 1A. MAINTENANCE REMOVED AND REPLACED A LIGHT CONTROL MODULE, OPERATIONALLY TESTED WITH NO DEFECTS OR SMELL NO
- [SDR ASOA201711307028](https://openairdocs.org/sdr/ASOA201711307028), Nov 30, 2017: UPLOCK. FAILED. NOSE GEAR WOULDN'T RETRACT AFTER TAKEOFF AND RETURNED TO DEPARTURE. FOUND THE NLG UPLOCK BOX AND NLG PROXIMITY SWITCHED BAD. MAINTENANCE REMOVED AND REPLACED TH
- [SDR ASOA201711147027](https://openairdocs.org/sdr/ASOA201711147027), Nov 13, 2017: BRACKET. CRACKED. A 2 INCH LONG CRACK WAS FOUND ON THE UPPER LATERAL BRACKET IN THE COCKPIT OVERHEAD. CUTOUT DAMAGED SECTION, SPLICED IN A NEW SECTION, FABRICATED AND INSTALLED D
- [SDR ASOA201709092009](https://openairdocs.org/sdr/ASOA201709092009), Sep 9, 2017: O-RING. LEAKING. NR 1 ENGINE PRODUCED SMOKE ON EXHAUST DURING WALK AROUND. REPLACE LPT SHAFT PLUG O-RING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201705154023](https://openairdocs.org/sdr/ASOA201705154023), May 15, 2017: WIRE HARNESS. DEFECTIVE. FLIGHT 4189 THE CREW REPORTED AN ENGINE ONE FIRE DET FAIL MESSAGE ON EICAS DURING CLIMB AND DESCENT. THE AIRCRAFT LANDED IN JAN WITHOUT INCIDENT WHERE MAINTENAN
- [SDR ASOA201612214114](https://openairdocs.org/sdr/ASOA201612214114), Dec 21, 2016: LIGHT. INOPERATIVE. CREW REPORTED ONE FLOOR EMERGENCY LIGHT STRIP OUT BETWEEN ROWS 8 & 9. REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS. THE A
- [SDR ASOA20160815044R](https://openairdocs.org/sdr/ASOA20160815044R), Aug 15, 2016: CONNECTOR. UNSECURE. PILOT REPORTED UNABLE TO OPERATE EMERGENCY LIGHTS FROM THE FA PANEL. MX FOUND CONNECTOR ON F/A'S LIGHT CONTROL PANEL LOOSE. SECURED THE CONNECTER AND OPS CHECKE
- [SDR ASOA20150427012](https://openairdocs.org/sdr/ASOA20150427012), Apr 23, 2015: FITTING. CRACKED. THE RT OTBD FLAP HAS A CRACK ON THE INBD ROOT FITTING. REPAIRED USING PRINCIPALES OF TECH INSTRUCTIONS TI-145-13-200, REV U. GENERATED A DMI TO PERFORM AN INTER
- [SDR ASOA20140526044](https://openairdocs.org/sdr/ASOA20140526044), May 26, 2014: FLAPPER VALVE. LEAKING. THE CREW REPORTED FUEL VENTING FROM RT WING ON TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE RT WING FLAPPER VALVE. OPS CHECKS WERE GOOD.
- [SDR ASOA20131203212](https://openairdocs.org/sdr/ASOA20131203212), Dec 6, 2013: SKIN. CRACKED. DURING A-CHECK INSPECTION, LEFT FUSELAGE SKIN WAS FOUND TO HAVE A FREE FLOATING HORIZONTAL CRACK MEASURING 9.07 MM, 0.35", WITH A 3.47 MM, 0.13", CRACK TRAVELIN
- [SDR ASOA20131203211](https://openairdocs.org/sdr/ASOA20131203211), Dec 6, 2013: PROFILE. CRACKED. DURING A-CHECK INSPECTION, LEFT L-PROFILE, DRAG ANGLE WAS FOUIND TO BE CRACKED AT FRAME 76. MAINTENANCE R & R PROFILE, AND ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131203210](https://openairdocs.org/sdr/ASOA20131203210), Dec 6, 2013: SKIN. CRACKED. DURING A-CHECK INSPECTION, RT SIDE FUSELAGE SKIN WAS FOUND TO BE CRACKED FRAME 75 BELOW STRINGER 2R. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A DOUBLER REPA
- [SDR ASOA20131017119](https://openairdocs.org/sdr/ASOA20131017119), Oct 17, 2013: UNKNOWN. ODOR. CREW REPORTED A STRONG ELECTRICAL ODOR COMING FROM COFFEEMAKER WHEN TURNED ON, ODOR WENT AWAY WHEN TURNED OFF. MX PERFORMED OPS CHECK OF THE COFFEEMAKER WITH NO
- [SDR ASOA20130628335](https://openairdocs.org/sdr/ASOA20130628335), Jun 28, 2013: PRESSURE SWITCH. DEFECTIVE. ACFT WAS ON THE GROUND WHEN CREW SAW VISABLE SMOKE ON THE F/O SIDE OF ACFT. MX R & R THE NR 2 ENGINE FUEL LOW PRESSURE SWITCH IAW AMM 28-45-01, OPS CHECK GOOD I
- [SDR ASOA20130626065R](https://openairdocs.org/sdr/ASOA20130626065R), Jun 26, 2013: PRESSURE SWITCH. INOPERATIVE. PILOT REPORTED VISIBLE SMOKE IN COCKPIT ON THE F/O'S SIDE WITH THE FUEL PUMPS ON. MX PERFORMED A DETAILED VISUAL INSPECTION IN THE COCKPIT AND NO SMOKE NOTED. R
- [SDR ASOA20130601169V](https://openairdocs.org/sdr/ASOA20130601169V), Jun 1, 2013: SILL. CORRODED. DURING C-CHECK THE CARGO DOOR CUTOUT CENTER SILL WAS FOUND TO BE CORRODED. BETWEEN FRAMES 65-68 AND STRINGERS 15-16L. MX R & R THE SILL IAW SRM 51-40-02. THE AC
- [SDR ASOA20130601168](https://openairdocs.org/sdr/ASOA20130601168), Jun 1, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01443. THE ACFT WAS AP
- [SDR ASOA20130601167](https://openairdocs.org/sdr/ASOA20130601167), Jun 1, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10, FIG 202. TH
- [SDR ASOA20130601166](https://openairdocs.org/sdr/ASOA20130601166), Jun 1, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK, OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 34. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-01, FIG 202. THE ACFT WAS
- [SDR ASOA20130601165](https://openairdocs.org/sdr/ASOA20130601165), Jun 1, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK, OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 55. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10, FIG 202. THE ACFT WAS
- [SDR C2XA11CL232](https://openairdocs.org/sdr/C2XA11CL232), Oct 13, 2011: ACTUATOR. FAULTY. ORD FLT 5946 THE CREW REPORTED A FLAP FAIL MESSAGE AT 500 FT ON FINAL APPROACH WITH FLAPS SHOWING 45 DEGREES. MAINTENANCE INSPECTED AND REPLACED THE LEFT OUTBOA
- [SDR C2XA20111002152](https://openairdocs.org/sdr/C2XA20111002152), Oct 2, 2011: SWITCH. FAULTY. ACFT WAS IN FOR A SERVICE ROUTINE AND ON THE MORNING DEPARTURE CLIMBOUT THE CREW GOT A AURA WARNING OF A FIRE. ACFT RETURNED TO DEPARTURE WHERE MX FOUND THE NR1
- [SDR C2XA11CL184](https://openairdocs.org/sdr/C2XA11CL184), Aug 6, 2011: POTENTIOMETER. FAULTY. ORD FLT 5912 THE CREW REPORTED THE STEERING WAS UNRESPONSIVE WHILE TAXIING. THE AIRCRAFT STARTED PULLING RIGHT AND GRINDING NOISE CAME FROM THE NOSE WHEEL AREA.
- [SDR C2XA11IA097](https://openairdocs.org/sdr/C2XA11IA097), May 19, 2011: ENGINE. LEAKING. IAH - FLIGHT 3051, THE CREW REPORTED THAT AT FULL POWER SETTING DURING CLIMB PACK TWO EMITTED A BURNING SMELL. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WIT
- [SDR C2XA10IA091](https://openairdocs.org/sdr/C2XA10IA091), Mar 8, 2010: ISIS. INOPERATIVE. IAH - FLIGHT 2237, THE CREW REPORTED THAT ON LANDING THE ISIS FAILED WITH AN OUT OF ORDER MESSAGE FOLLOWED BY AN ELECTRICAL BURNING SMELL ON THE FLIGHT DECK. TH
- [SDR C2XA09RI206](https://openairdocs.org/sdr/C2XA09RI206), Dec 8, 2009: STARTER GEN. INOPERATIVE. FLIGHT 2082 - IND - FLIGHT CREW REPORTED ELECTRIC BURN SMELL IN COCKPIT AND GALLEY FOLLOWED BY APU AUTO SHUTDOWN. MX REMOVED AND REPLACED APU STARTER GENERATOR 
- [SDR C2XA09IA280](https://openairdocs.org/sdr/C2XA09IA280), Nov 2, 2009: UNKNOWN. ODOR. ABQ - FLIGHT 2728, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE COCKPIT AND CABIN. CONTRACT MAINTENANCE INSPECTED THE AIRCRA
- [SDR C2XA09SH203](https://openairdocs.org/sdr/C2XA09SH203), Jul 21, 2009: SKIN. DAMAGED. DURING C-CHECK LIGHTNING STRIKE BETWEEN FRAME 23 AND 24 STRINGER 14L (EXTERNAL). MX PERFORMED AND COMPLETED REPAIR IAW SRM 53-21-01 AND IC 2009-145/05374. THE A
- [SDR C2XA09SH211](https://openairdocs.org/sdr/C2XA09SH211), Jul 20, 2009: FITTING. CORRODED. SHV - DURING C-CHECK (FR 65/STR 16L) SHEER CLIP AT CARGO DOOR CUTOUT BASE FWD CORNER HAS CORROSION. MAINTENANCE REMOVED CORROSION AND COMPLETED REPAIR AT FRAME 
- [SDR C2XA09SH210](https://openairdocs.org/sdr/C2XA09SH210), Jul 20, 2009: SKIN. CORRODED. SHV - DURING C-CHECK LT HORIZONTAL L/E UPPER AND LOWER SURFACE HAS CORROSION AROUND ALL RIVET HEADS AND SCREW HEADS. MAINTENANCE REMOVED CORROSION BY POLISHING 
- [SDR C2XA09SH209](https://openairdocs.org/sdr/C2XA09SH209), Jul 20, 2009: DOOR FRAME. CORRODED. SHV - DURING C-CHECK SERVICE DOOR CUTOUT AFT STRUCTURE AT FRAME 22 BETWEEN STRINGER 15R AND 16R HAS CORROSION AT BOLT HOLE. MAINTENANCE REPAIRED SERVICE DOOR CU
- [SDR C2XA09SH208](https://openairdocs.org/sdr/C2XA09SH208), Jul 20, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM I/B SIDE HAS CORROSION FRAME 58-59. MAINTENANCE PERFORMED AND COMPLETED REPAIR OF LT OMEGA BEAM FRM 59 AT CROSSBEAM ATTACHMEN
- [SDR C2XA09SH207](https://openairdocs.org/sdr/C2XA09SH207), Jul 20, 2009: FITTING. CORRODED. SHV - DURING C-CHECK CORROSION FOUND AT FRAME 65 CLIP. MAINTENANCE PERFORMED AND COMPLETED REPAIR TO FRAME CLIP AT FR 65 IAW EC5330-01458 ORIG. THE AIRCRAFT WAS
- [SDR C2XA09SH206](https://openairdocs.org/sdr/C2XA09SH206), Jul 20, 2009: BUSHING. MIGRATED. SHV - DURING C-CHECK HAT BUSHING MIGRATED ON LT SPEED BRAKE ACTUATOR ATTACHMENT BRACKET. MAINTENANCE REMOVED, MEASURED AND REINSTALLED HAT BUSHING ON LT SPEED B
- [SDR C2XA09SH205](https://openairdocs.org/sdr/C2XA09SH205), Jul 20, 2009: RIVET. LOOSE. SHV - DURING C-CHECK 3 WORKING RIVETS FOUND AT FRAME 79 STRINGER 3R-6R. MAINTENANCE REMOVED AND REPLACED RIVETS AT FRAME 79 STRINGER 3R-6R IAW EC5330-01941 ORIG
- [SDR C2XA09SH204](https://openairdocs.org/sdr/C2XA09SH204), Jul 20, 2009: SKIN. DENTED. SHV - DURING C-CHECK DENT IN LT STATIC PORT AREA AT FRAME 14 STRINGER 15L. MAINTENANCE REPAIRED DENT IN LT STATIC PORT AREA AT FRAME 14 STRINGER 15L IAW IC2009-

All 67: https://openairdocs.org/aircraft/N11539/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/N11539/stcs.md

## Earlier aircraft with N11539

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N11539 before.

- [Cancelled 1984-08-06](https://openairdocs.org/deregistered/N11539-1984-08-06): Cessna 150L, S/N 15075501. Administratively canceled. Owner: [Carter Joy B](https://openairdocs.org/faa-owner/CARTER%20JOY%20B), [Tavernier, FL](https://openairdocs.org/faa-place/FL/Tavernier)

## 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

---
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.