# N11535: 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: 145518
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 12, 2001
- Certificate issued: September 30, 2022
- Expires: September 30, 2029
- Mode S code: A041A5
- 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=11535
- Page: https://openairdocs.org/aircraft/N11535

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/N11535/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 N11535.

## FAA accident and incident reports

None matched to N11535.

## Service difficulty reports (71, 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 ASOA202004027033](https://openairdocs.org/sdr/ASOA202004027033), Apr 2, 2020: DOOR SILL. CORRODED. CARGO DOOR CUT-OUT SILL HAS CORROSION. REMOVED AND REPLACED CARGO DOOR CUT-OUT SILL. AIRCRAFT STILL IN C CHECK.
- [SDR ASOA202003307033](https://openairdocs.org/sdr/ASOA202003307033), Mar 30, 2020: FLOOR SUPPORT. CORRODED. RH OMEGA BEAM CORRODED BETWEEN FRAMES 59-60 AT NUTPLATE. REPAIRED RH OMEGA BEAM BETWEEN FRAMES 56-60 AT NUTPLATE IAW EMB 145 SRM 53-24-10.
- [SDR ASOA202003307032](https://openairdocs.org/sdr/ASOA202003307032), Mar 30, 2020: STRINGER SPLICE. CRACKED. STRINGER 6R SPLICE IS CRACKED @ FWD END @ FRAME 19 (MARKED). REMOVED AND REPLACED CRACKED STIFFENER IAW EMB 145 SRM 51-40-02.
- [SDR ASOA202003257029](https://openairdocs.org/sdr/ASOA202003257029), Mar 24, 2020: SKIN PANEL. CRACKED. CRACK IN SKIN PANEL @ FRAME 75 BETWEEN 1L & 2L. CUT OUT CRACKED SECTION, FABRICATED AND INSTALLED FILLER AND DOUBLER. AIRCRAFT STILL IN C CHECK.
- [SDR ASOA202001287015](https://openairdocs.org/sdr/ASOA202001287015), Jan 28, 2020: WIRE HARNESS. DAMAGED. TYS A/C ONCE AIRBORNE THE AIR-GROUND FAIL AND CREW RETURN TO BASE. MAINTENANCE REMOVED AND REPLACED THE NLG WOW PROXY SWITCH HARNESS IAW EMB 145AMM 20-10-01 AND
- [SDR ASOA2019041745055](https://openairdocs.org/sdr/ASOA2019041745055), Apr 14, 2019: BATTERY PACK. INOPERATIVE. MX REPORTED THE EMERGENCY FLOOR LIGHT BY WING EMERGENCY EXIT INOP. REMOVED AND REPLACED THE #3 PSU BATTERY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RET
- [SDR ASOA2019041745054](https://openairdocs.org/sdr/ASOA2019041745054), Apr 14, 2019: BATTERY PACK. INOPERATIVE. MX REPORTED THE EMERGENCY LIGHTS BY WING EMERGENCY EXIT NOT WORKING. REMOVED AND REPLACED THE #3 PSU BATTERY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR R
- [SDR ASOA201805257093](https://openairdocs.org/sdr/ASOA201805257093), May 25, 2018: CONTROL UNIT. FAILED. DURING CLIMB OUT, WHILE ACTIVATING MAIN PITCH TRIM SWITCH, ICAS WENT TO INOPERATIVE, THE MASTER WARNING WENT TO INOPERATIVE, THE MESSAGE REMAINED AFTER THE TRIM
- [SDR ASOA201703213051](https://openairdocs.org/sdr/ASOA201703213051), Mar 21, 2017: CHARGER. INOPERATIVE. LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY CHARGER IAW AMM 33-50-04. OPERATIONAL CHECKS WERE
- [SDR ASOA201702017002](https://openairdocs.org/sdr/ASOA201702017002), Jan 27, 2017: ENGINE. MALFUNCTIONED. ENGINE NR 1 OUT IN FLIGHT. REMOVED AND REPLACED NR 1 ENG. OPS AND LEAK CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA201701163002](https://openairdocs.org/sdr/ASOA201701163002), Jan 16, 2017: BATTERY PACK. DISCHARGED. DURING ROUTINE MAINTENANCE THE EXTERNAL EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE NR 4 EMERGENCY BATTERY CHARGER AND BATTERY PACK. OPERATI
- [SDR ASOA20160502020](https://openairdocs.org/sdr/ASOA20160502020), May 2, 2016: BATTERY PACK. DISCHARGED. DURING SCHEDULED MAINTENANCE INSPECTION THE AFT EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE R & R NR 4 EMERGENCY LIGHT BATTERY WITH OPS CHECK GOOD. ACFT 
- [SDR ASOA20160429028](https://openairdocs.org/sdr/ASOA20160429028), Apr 29, 2016: WIRE. BURNED. THE CREW REPORTED CLIMBING OUT THROUGH 6000 FT, THEY SMELLED A FOUL ODOR AND RECEIVED A PITCH TRIM MAIN FAIL MESSAGE. NONE OF THE TRIM SWITCHES WOULD WORK. PITC
- [SDR ASOA20160418022](https://openairdocs.org/sdr/ASOA20160418022), Apr 18, 2016: POWER SUPPLY. INOPERATIVE. DURING ROUTINE MAINTENANCE THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY BATTERY POWER SUPPLY. OPS CHECKS WE
- [SDR ASOA20160325026](https://openairdocs.org/sdr/ASOA20160325026), Mar 25, 2016: CHARGER. INOPERATIVE. DURING MAINTENANCE INSPECTION, MAINTENANCE DISCOVERED AN OVERWING EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT CHARGER ASSY
- [SDR ASOA20160224014](https://openairdocs.org/sdr/ASOA20160224014), Feb 24, 2016: POWER SUPPLY. INOPERATIVE. DURING ROUTINE MAINTENANCE THE CABIN FLOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE FROM ROW 18 TO ROW 24. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY 
- [SDR ASOA20160214009H](https://openairdocs.org/sdr/ASOA20160214009H), Feb 14, 2016: BATTERY PACK. DISCHARGED. DURING MAINTENANCE INSPECTION THE ALL OF THE EMERGENCY LIGHTS THAT OPERATE OFF OF BATTERY NR 4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 BATTERY 
- [SDR ASOA20160207010](https://openairdocs.org/sdr/ASOA20160207010), Feb 7, 2016: BATTERY. INOPERATIVE. DURING ROUTINE MAINTENANCE, THE AFT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.
- [SDR ASOA201601070003](https://openairdocs.org/sdr/ASOA201601070003), Jan 7, 2016: BATTERY PACK. INOPERATIVE. DURING ROUTINE MAINTENANCE, THE LT AND RT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKS WE
- [SDR ASOA20150323079](https://openairdocs.org/sdr/ASOA20150323079), Mar 23, 2015: FLOOR SUPPORT. CORRODED. DURING C-CK. CENTER OMEGA BEAM CORRODED AT FR 59. REPAIRED CENTER OMEGA BEAM IAW EC5320-02020. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150323078](https://openairdocs.org/sdr/ASOA20150323078), Mar 23, 2015: SKIN. CRACKED. DURING C-CK. RT FUSELAGE SKIN CRACKED AROUND RIVET FR 79. REPAIRED FUSELAGE SKIN IAW EC5330-02992. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150323077](https://openairdocs.org/sdr/ASOA20150323077), Mar 23, 2015: SKIN. CRACKED. DURING C-CHECK, RT FUSELAGE SKIN CRACKED AROUND RIVET FRAME 75. REPAIRED FUSELAGE SKIN IAW EC5330-02992. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150323076V](https://openairdocs.org/sdr/ASOA20150323076V), Mar 23, 2015: SKIN. CRACKED. DURING C-CHECK, LEFT FUSELAGE SKIN CRACKED AROUND RIVET FRAME 77-78. REPAIRED FUSELAGE SKIN IAW EC5330-02992. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131118081](https://openairdocs.org/sdr/ASOA20131118081), Nov 18, 2013: CHARGER. INOPERATIVE. CREW REPORTED EMERGENCY LIGHT ON MAIN CABIN DOOR CEILING PANEL WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER ASSY
- [SDR ASOA20130825101](https://openairdocs.org/sdr/ASOA20130825101), Aug 25, 2013: UNKNOWN. ODOR. ON DESCENT, CREW REPORTED A VERY STRONG ODOR OF BURNING IN FLIGHT DECK. F/A REPORTED BURNING ODOR ALSO AROUND ROW 11. SMOKE WAS NOT VISIBLE ONLY STRONG ODOR. MX
- [SDR ASOA20130717075R](https://openairdocs.org/sdr/ASOA20130717075R), Jul 17, 2013: FLAPPER VALVE. LEAKING. LIQUID VAPOR WAS REPORTED TO BE TRAILING OFF THROUGH RT WING AFTER TAKEOFF BY FLIGHT ATTENDANT. MX R & R THE RT WING OTBD FLAPPER VALVE WITH LEAK CHECK GOOD. AC
- [SDR V0XR20130401J0186](https://openairdocs.org/sdr/V0XR20130401J0186), Mar 29, 2013: STRINGER. CHAFED. STRINGER 2L IS CHAFED AT FRAME 20. BLENDED OUT DAMAGE IAW SRM 51-10-03, NDT PERFORMED, NO DEFECTS NOTED, ALODINED DAMAGED AREA, FABRICATED REPAIR, ALODINED AND 
- [SDR V0XR201303270185](https://openairdocs.org/sdr/V0XR201303270185), Mar 25, 2013: CHANNEL. CORRODED. RT HAT BEAM AT FRAME 60 IS CORRODED. R & R RT HAT BEAM AT FRAME 60 IAW SRM 51-40-02, 53-24-10,51-20-03, 51-20-01, AND CPM 51-21-06,51-21-05,51-21-04, AND AMM 25
- [SDR V0XR201303270184](https://openairdocs.org/sdr/V0XR201303270184), Mar 25, 2013: SILL. CORRODED. RT SILL AT FRAME 61 CABIN BOTTOM IS CORRODED. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 51-10-03 & 53-31-10. R & R SILL IAW SRM 51-10-03,51-40-02, 51-40-06
- [SDR V0XR201303270183](https://openairdocs.org/sdr/V0XR201303270183), Mar 25, 2013: SILL. CORRODED. LT SILL AT FRAME 61 CABIN BOTTOM IS CORRODED. REMOVED THE CORROSION,THE REMAINING MATERIAL WAS OUT OF LIMITS IAW SRM 51-10-03 & 53-31-10. R & R LT SILL AT FRAME
- [SDR V0XR201303270182](https://openairdocs.org/sdr/V0XR201303270182), Mar 25, 2013: SILL. CORRODED. LT SILL AT FRAME 58 CABIN BOTTOM IS CORRODED. REMOVED THE CORROSION,THE REMAINING MATERIAL WAS OUT OF LIMITS IAW SRM 51-10-03 & 53-31-10. R & R LT SILL AT FRAME
- [SDR V0XR20130325J0181](https://openairdocs.org/sdr/V0XR20130325J0181), Mar 22, 2013: GUSSET. CORRODED. GUSSET ON CENTER HAT LT BEAM AT FRAME 60 CORRODED. R & R CENTER HAT GUSSET AT FRAME 60 IAW SRM 51-40-02, 53-24-10, 51-20-03,51-20-01, AND CPM 51-21-04,51-21-05.
- [SDR V0XR20130325J0180](https://openairdocs.org/sdr/V0XR20130325J0180), Mar 22, 2013: ANGLE. CORRODED. CARGO DOOR TOP FRAME HAS CORROSION AROUND FORWARD FASTENER HOLE. INSTALLED NEW TOP CARGO DOOR ANGLE TO CARGO DOOR. PN 145-31544-001 IAW SRM 51-40-02, 51-20-03, 
- [SDR V0XR20130325J0179](https://openairdocs.org/sdr/V0XR20130325J0179), Mar 22, 2013: SILL. CORRODED. CORROSION ON AFT CARGO DOOR SILL AROUND 2 FASTENER HOLES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. R & R AFT CARGO LOWER DOOR SILL IAW SRM 51-10-03, 53-31-
- [SDR ASOA20130117003C](https://openairdocs.org/sdr/ASOA20130117003C), Jan 17, 2013: LIGHT. INOPERATIVE. THE CREW REPORTED LT EXTERNAL FORWARD EMERGENCY LIGHT INOPERATIVE. MX INSPECTED AND REPLACED THE LT WING FORWARD EMERGENCY LIGHT ASSY. OPS CHECKED GOOD.
- [SDR ASOA20121217120](https://openairdocs.org/sdr/ASOA20121217120), Dec 17, 2012: UNKNOWN. ODOR. CREW REPORTED A FUEL ODOR IN COCKPIT DURING POWER CHANGES. MX PERFORMED ENGINE RUNS AT HIGH POWER AND VARIABLE SETTINGS WITH BOTH PACKS ON AND COULD NOT DUPLICA
- [SDR C2XA11RI139](https://openairdocs.org/sdr/C2XA11RI139), Aug 22, 2011: LIGHT. INOPERATIVE. RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND CEILING EXIT LIGHT NOT WORING DURING TEST. MX REMOVED AND REPLACED LIGHT BULB AND PERFORMED OPERATIONAL CHECK SUC
- [SDR C2XA11RI135](https://openairdocs.org/sdr/C2XA11RI135), Aug 15, 2011: LIGHT. INOPERATIVE. RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND ROW 7 FLOOR PROXIMITY STRIP INOPERATIVE. MX REMOVED AND REPLACED STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFUL
- [SDR C2XA11IA076](https://openairdocs.org/sdr/C2XA11IA076), Apr 25, 2011: TRANSPONDER. INOPERATIVE. DURING CLIMB THE CREW REPORTED THE NR 2 TRANSPONDER. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE INTEGRATED COMM /TRANSPONDER 
- [SDR C2XA11SH082](https://openairdocs.org/sdr/C2XA11SH082), Apr 3, 2011: SKIN. CRACKED. SHV - DURING C-CHECK EXTERNAL SKIN CRACKED AT FRAME 50 STRINGER 15R. MAINTENANCE PERFORMED REPAIR ON EXTERNAL SKIN AT FRAME 50 STRINGER 15R IAW EMB-145 EC5330-0
- [SDR C2XA10RI052](https://openairdocs.org/sdr/C2XA10RI052), Apr 26, 2010: COMPUTER. FAULTY. FLIGHT 2985 - EWR - FLIGHT CREW REPORTED BURNING SMELL IN COCKPIT, GPWS/WINDSHEAR/TCAS INOP, THEN MESSAGE CLEAR. CREW RETURNED TO GATE UNEVENTFULLY. EWR MX REMO
- [SDR C2XA09RI153](https://openairdocs.org/sdr/C2XA09RI153), Aug 27, 2009: STRUT. LOW. FLIGHT 2767 - EWR - FLIGHT CREW DIVERTED TO EWR DUE TO LANDING GEAR NOT RETRACTING (ORIGINAL FLIGHT WAS ALB TO CLE). EWR MX VERIFIED GAP IN ALL WOW SWITCHES, SE
- [SDR C2XA09RI146](https://openairdocs.org/sdr/C2XA09RI146), Aug 17, 2009: PROXIMITY SWITCH. CORRODED. FLIGHT 2007 - RIC - AFTER TAKING OFF OF DCA TO CLE, FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. CREW DIVERTED FLIGHT TO RIC AND LANDED A
- [SDR C2XA09CL079](https://openairdocs.org/sdr/C2XA09CL079), Jun 8, 2009: COUPLING. BLOWN. CLE FLIGHT 2351 - CREW REPORTED BOTH ENGINE BLEEDS CLOSED ADVISORY MESSAGE AND BOTH PACKS CLOSED, ADVISORY MESSAGE ON EICAS AFTER TAKEOFF. THE AIRCRAFT RETURNED
- [SDR C2XA09IA148](https://openairdocs.org/sdr/C2XA09IA148), Jun 5, 2009: PROXIMITY SWITCH. INOPERATIVE. THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT ON CLIMB. THE ACFT RETURNED TO DEPARTURE, WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED TH
- [SDR C2XA09SH148](https://openairdocs.org/sdr/C2XA09SH148), May 3, 2009: PANEL. CORRODED. SHV - DURING C-CHECK PAX DOOR BOTTOM FOUR NUT PLATE HOLES FOR MAIN LINER PANEL CORRODED. MAINTENANCE REPAIRED PAX DOOR LOWER FOUR NUT PLATE ATTACHMENT HOLES FOR
- [SDR C2XA09SH146](https://openairdocs.org/sdr/C2XA09SH146), May 3, 2009: SKIN. CORRODED. SHV - DURING C-CHECK HORIZONTAL STAB LT LEADING EDGE HAS CORROSION AROUND RIVET HEADS AT UPPER AND LOWER SURFACES. MAINTENANCE REPAIRED LT HORIZONTAL STABILIZER
- [SDR C2XA09SH147](https://openairdocs.org/sdr/C2XA09SH147), May 3, 2009: SKIN. CORRODED. SHV - DURING C-CHECK HORIZONTAL STAB RT LEADING EDGE HAS CORROSION AROUND RIVET HEADS AT UPPER AND LOWER SURFACES. MAINTENANCE REPAIRED RT HORIZONTAL STAB LEADI
- [SDR C2XA09SH145](https://openairdocs.org/sdr/C2XA09SH145), May 3, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FRAME 38. MAINTENANCE REMOVED CORROSION AT FR 38 IAW EMB-145 SRM 53-23-10 AND REPAIRED LT OMEGA BEAM AT FR 3
- [SDR C2XA09SH144](https://openairdocs.org/sdr/C2XA09SH144), May 3, 2009: FLOOR SUPPORT. CORRODED. SHV-DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FRAME 29. MAINTENANCE REMOVED CORROSION IAW EMB-145 SRM 53-22-10 AND INSTALLED FABRICATED REPAIR AT FRAME 29 I

All 71: https://openairdocs.org/aircraft/N11535/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/N11535/stcs.md

## Earlier aircraft with N11535

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N11535 before.

- [Cancelled 1976-05-26](https://openairdocs.org/deregistered/N11535-1976-05-26): Cessna 150L, S/N 15075497. Owner: [Gold Dust Flying Service Inc](https://openairdocs.org/faa-owner/GOLD%20DUST%20FLYING%20SERVICE%20INC), [Weaver, AL](https://openairdocs.org/faa-place/AL/Weaver)

## 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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