# N11565: 2002 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: 145621
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 27, 2002
- Certificate issued: March 27, 2020
- Expires: March 31, 2030
- Mode S code: A0420E
- Registered owner: [Corporate Flight Management Inc](https://openairdocs.org/faa-owner/CORPORATE%20FLIGHT%20MANAGEMENT%20INC)
- Location: [Smyrna, TN](https://openairdocs.org/faa-place/TN/Smyrna)
- Owner type: Corporation
- Owner's area on the map: 35.9628° N, 86.5297° W: Placed by OpenAirDocs at the center of ZIP code 37167, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=11565
- Page: https://openairdocs.org/aircraft/N11565

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/N11565/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 N11565.

## FAA accident and incident reports

None matched to N11565.

## Service difficulty reports (76, 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 ASOA2018060871051](https://openairdocs.org/sdr/ASOA2018060871051), Jun 8, 2018: HOUSING. DAMAGED. RT AND LT SPHERICAL BEARING HOUSINGS HAVE DISPLACED METAL. REPAIRED LT AND RT SPHERICAL BEARING HOUSING IN ACCORDANCE WITH SRM 55-30-02.
- [SDR ASOA201806087105](https://openairdocs.org/sdr/ASOA201806087105), Jun 8, 2018: SKIN. CRACKED. RT REAR FUSELAGE SKIN AT FRAME 75, STRINGER 2R-3R CRACKED. REPAIRED FUSELAGE SKIN IN ACCORDANCE WITH SRM 53-31-01.
- [SDR ASOA201806067098](https://openairdocs.org/sdr/ASOA201806067098), Jun 4, 2018: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 2L. CUTOUT THE DAMAGE SECTION, FABRICATED A FILLER, AND DOUBLER. INSTALLED THE REPAIR.
- [SDR ASOA201805277094](https://openairdocs.org/sdr/ASOA201805277094), May 27, 2018: SKIN. CRACKED. TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND A CRACK IN THE REAR FUSELAGE SKIN AT FRAME 75 AND STRINGER 2R. MAINTENANCE CUTOUT A 2" BY 2" SECTION OF SKIN A
- [SDR ASOA20151215060](https://openairdocs.org/sdr/ASOA20151215060), Dec 15, 2015: DISPLAY. FAILED. CREW REPORTED AN ELECTRICAL ODOR AFTER CAPTAINS MFD WENT BLANK. MAINTENANCE R & R CAPTAIN`S MFD WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20151215091](https://openairdocs.org/sdr/ASOA20151215091), Dec 15, 2015: DISPLAY. SHORTED. THE CREW REPORTED MFD 1 IS OUT WITH BURNING ODOR IN FLIGHT DECK. THE ACFT LANDED IN ECP WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE AFFECTED MFD ON MEL 34-22-
- [SDR ASOA20151009058](https://openairdocs.org/sdr/ASOA20151009058), Oct 9, 2015: FUEL CONTROL. LEAKING. THE CREW REPORTED A FUEL ODOR COMING FROM APU BLEED. AFTER ROTATION WHEN APU WAS PROVIDING AIR TO THE PACKS. MAINTENANCE INSPECTED AND REPLACED THE APU FUEL CON
- [SDR ASOA20150210009](https://openairdocs.org/sdr/ASOA20150210009), Feb 10, 2015: UNKNOWN. ODOR. CREW REPORTED A BURNING ODOR BEFORE LANDING. MAINTENANCE PERFORMED TROUBLESHOOTING AND NO UNUSUAL ODORS COULD BE DETECTED OR REPRODUCED. ACFT WAS APPROVED FOR R
- [SDR ASOA20141117092](https://openairdocs.org/sdr/ASOA20141117092), Nov 17, 2014: LIGHT. UNKNOWN. THE CREW REPORTED EMERGENCY LIGHT WAS INTERMITTENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE EMERGENCY LIGHTS. NO DEFECTS WERE FOUND. THE A
- [SDR ASOA20141014109](https://openairdocs.org/sdr/ASOA20141014109), Oct 14, 2014: STRUCTURE. DAMAGED. ACFT WAS ON TAKEOFF WHEN A BIRD HIT THE NOSE. ACFT LANDED WITHOUT INCIDENT AND MAINTENANCE REMOVED THE BAD RIVETS AND INSTALL 5 OF A OVERSIZE RIVETS. ALODINED, 
- [SDR ASOA20140804085](https://openairdocs.org/sdr/ASOA20140804085), Aug 4, 2014: SOCKET. DIRTY. DURING MX INSPECTION, THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED BULB, CLEANED DEBRIS FROM SOCKET AND REINSTALLED BULB, OPS CHEC
- [SDR ASOA20140706089](https://openairdocs.org/sdr/ASOA20140706089), Jul 6, 2014: CONTROLLER. MELTED. THE CREW REPORTED A STRONG SMOKE ODOR, CIGARETTE & PAPER ODOR EMITTING FROM MCD, F/A JUMPSEAT, AROUND EQUIPMENT CLOSET. THE ACFT RETURNED, WHERE IT LANDED WITHO
- [SDR ASOA20140417046](https://openairdocs.org/sdr/ASOA20140417046), Apr 17, 2014: COFFEEMAKER. DIRTY. F/A REPORTED AN ODOR COMING FROM THE GALLEY COFFEEMAKERS. MAINTENANCE CLEANED THE WARMERS ON BOTH COFFEE BREWERS AND PERFORMED AN OPS CHECK, CHECKED GOOD, WITH 
- [SDR ASOA20140112005](https://openairdocs.org/sdr/ASOA20140112005), Jan 12, 2014: BRAKE ASSY. FAULTY. A "BRAKE DEGRADE" MESSAGE APPEARED ON EICAS DURING LANDING AND REPORTED MORE THAN NORMAL BRAKE PEDAL PRESSURE NEEDED. ACFT PULLED TO THE LEFT. R & R NR 4 BRAKE 
- [SDR ASOA20140109011](https://openairdocs.org/sdr/ASOA20140109011), Jan 9, 2014: WEB. CRACKED. DURING C-CHECK, LT OTBD FLAP INBD ROOT RIB INTERNAL WEBBING CRACKED. MAINTENANCE REPAIRED IAW EC 5750-01562.
- [SDR ASOA20140107010](https://openairdocs.org/sdr/ASOA20140107010), Jan 7, 2014: FITTING. CORRODED. DURING C-CHECK, INSPECTION FOUND VERTICAL STAB SPAR TO FRAME 75 FRETTING AT THE FUSELAGE. MAINTENANCE COMPLIED WITH THE EC 5310-01317 TO REMOVED FITTING, REMOVE
- [SDR ASOA20130724078](https://openairdocs.org/sdr/ASOA20130724078), Jul 24, 2013: UNKNOWN. ODOR. PILOT REPORTED A STRONG ODOR OF PLASTIC/ELECTRICAL SMOKE INFLIGHT DURING DESCENT WITH THE TOP OF GLARESHIELD/AVIONICS PANEL EXTREMELY HOT TO THE TOUCH. MX INSPE
- [SDR ASOA20130609328](https://openairdocs.org/sdr/ASOA20130609328), Jun 9, 2013: SWITCH. FAILED. MAIN PITCH TRIM INOPERATIVE MESSAGE ON CLIMBOUT, AUTO TRIM FAIL, ELEVATOR MISTRIM. R & R PITCH TRIM SWITCH AND ACTUATOR. OPS CHECK GOOD ACFT RELEASED AND RETURN
- [SDR ASOA20120806068](https://openairdocs.org/sdr/ASOA20120806068), Aug 6, 2012: BALLAST. FAILED. THE CREW REPORTED SMOKE FROM 4C SIDEWALL LIGHT. MX REPLACED 4 B & C LIGHT ASSY AND 4 B&C LIGHT BALLAST. OPS CHECKS WERE GOOD.
- [SDR ASOA20120201004](https://openairdocs.org/sdr/ASOA20120201004), Feb 1, 2012: WIRE. BROKEN. EMERGENCY LIGHT FLOOR STRIP INOP. R & R LIGHT STRIP. OPS CHECK GOOD.
- [SDR C2XA11IA248](https://openairdocs.org/sdr/C2XA11IA248), Nov 3, 2011: CONTACTOR. INOPERATIVE. IAH - FLIGHT 4457 THE CREW REPORTED A BACKUP BATTERY OFF BUSS INDICATION IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE R
- [SDR C2XA11CL179](https://openairdocs.org/sdr/C2XA11CL179), Aug 1, 2011: INVERTER. INOPERATIVE. DURING ROUTINE MAINTENANCE THE RIGHT AFT EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE NR 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WE
- [SDR C2XA11IA249](https://openairdocs.org/sdr/C2XA11IA249), Jul 3, 2011: SWITCH. INOPERATIVE. IAH - FLIGHT 4457 THE CREW REPORTED A BACKUP BATTERY OFF BUSS INDICATION IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE R
- [SDR C2XA11CL144](https://openairdocs.org/sdr/C2XA11CL144), Jun 15, 2011: CONTROL UNIT. FAULTY. CLE FLT 2521 CREW REPORTED THAT THE SPOILERS OPENED ON TAKEOFF ROLL AT APPROXIMATELY 100 KIAS. THE SPOILERS INDICATED OPEN ON THE EICAS SYSTEM. THE CREW THEN AB
- [SDR C2XA11TY022](https://openairdocs.org/sdr/C2XA11TY022), Mar 4, 2011: INVERTER. INOPERATIVE. SECOND FLOOR PROXIMITY EMERGENCY LIGHT STRIP INOP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11.
- [SDR C2XACL006](https://openairdocs.org/sdr/C2XACL006), Jan 6, 2011: THERMOSTAT. FAULTY. IAD FLT 3153 THE CREW REPORTED A BLEED NR 1 OVERTEMP INDICATION IN FLIGHT DURING ICING CONDITIONS. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. M
- [SDR C2XA10RI0148](https://openairdocs.org/sdr/C2XA10RI0148), Nov 26, 2010: CONTROL PANEL. INOPERATIVE. FLIGHT 2030 - YYZ - FLIGHT CREW REPORTED LAV SMOKE DETECTOR IN GALLEY TEST INOPERATIVE. EWR MX REMOVED AND REPLACED SMOKE DETECTOR PANEL AND PERFORMED OPERATION
- [SDR C2XA10RI0144](https://openairdocs.org/sdr/C2XA10RI0144), Nov 26, 2010: CONTROL PANEL. INOPERATIVE. FLIGHT 2030 - EWR - FLIGHT CREW REPORTED SMOKE DETECTOR SWITCH IN GALLEY NOT WORKING. EWR MX REMOVED AND REPLACED GALLEY SMOKE DETECTOR PANEL AND PERFORMED OPER
- [SDR C2XA10SH076](https://openairdocs.org/sdr/C2XA10SH076), Feb 22, 2010: SKIN. CORRODED. SHV - DURING C-CHECK FUSELAGE SKIN HAS CORROSION AT FR 58 POTABLE WATER SUPPORT DOUBLER MATING SURFACE. REPAIRED SKIN IAW EC5330-02079. AIRCRAFT WAS APPROVED FO
- [SDR C2XA10SH075](https://openairdocs.org/sdr/C2XA10SH075), Feb 22, 2010: STRINGER. CORRODED. SHV - DURING C-CHECK STR 21R HAS CORROSION AT FR 13. REPAIRED STR 21R IAW EC5310-01507. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH073](https://openairdocs.org/sdr/C2XA10SH073), Feb 21, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LEFT OMEGA BEAM CORROSION FRM 29-34. REPAIRED LEFT OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH072](https://openairdocs.org/sdr/C2XA10SH072), Feb 21, 2010: SILL. CORRODED. SHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT HAS CORROSION. REPAIRED CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVI
- [SDR C2XA10SH071](https://openairdocs.org/sdr/C2XA10SH071), Feb 21, 2010: SILL. CORRODED. SHV - DURING C-CHECK SERVICE DOOR CENTER SILL HAS CORROSION. REPAIRED SERVICE DOOR SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH070](https://openairdocs.org/sdr/C2XA10SH070), Feb 21, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 35-38. REPAIRED OMEGA BEAM IAW EMB 145 SRM 51-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH069](https://openairdocs.org/sdr/C2XA10SH069), Feb 21, 2010: SUPPORT. CORRODED. SHV - DURING C-CHECK WASTE DRAIN VALVE SUPPORT HAS CORROSION. REMOVED AND REPLACED SUPPORT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE
- [SDR C2XA10SH068](https://openairdocs.org/sdr/C2XA10SH068), Feb 21, 2010: ATTACH FITTING. DAMAGED. SHV - DURING C-CHECK LEFT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT FITTING IAW EC5750-01177. AIRCRAFT WAS APPROV
- [SDR C2XA10SH067](https://openairdocs.org/sdr/C2XA10SH067), Feb 21, 2010: ATTACH FITTING. DAMAGED. SHV - DURING C-CHECK LEFT O/B GROUND SPOILER ATTACHMENT HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT FITTING IAW EMB 145 AMM 57-51-02. AIRCRAFT WAS
- [SDR C2XA10SH061](https://openairdocs.org/sdr/C2XA10SH061), Feb 21, 2010: FLOOR SUPPORT. CORRODED. LT OMEGA BEAM PREVIOUS REPAIR AT FR 20 HAS CORROSION (LEVEL 3). MAINTENANCE REMOVED AND REPLACED PREVIOUS REPAIR WITH NEW REPAIR IAW EC5320-01229. THE AIRCRAFT 
- [SDR C2XA10SH058](https://openairdocs.org/sdr/C2XA10SH058), Feb 10, 2010: LIGHT. INOPERATIVE. SHV - DURING C-CHECK RT LOWER EXT EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. AIRCRAFT WAS APPROVED FOR RETURN TO 
- [SDR C2XA10TY005](https://openairdocs.org/sdr/C2XA10TY005), Dec 30, 2009: SIGN. INOPERATIVE. A 12BC UPPER SIDEWALL EMERGENCY LIGHT INOP. REMOVED AND REPLACED EXIT MARKING SIGN ASSY IAW EMB 145 AMM 33-50-14. OPS CHECK GOOD.
- [SDR C2XA09IA254](https://openairdocs.org/sdr/C2XA09IA254), Oct 12, 2009: DISPLAY. BURNED. CLL - FLIGHT 2593 - DURING FLIGHT THE CREW REPORTED THAT THE PFD1 CIRCUIT BREAKER POPPED WITH A CHECK PFD1 MESSAGE ON EICAS AND SMOKE COMING FROM UNDER THE PFD1
- [SDR C2XA08RI140](https://openairdocs.org/sdr/C2XA08RI140), Sep 16, 2008: RELAY. BURNED. FLIGHT 2654 EWR FLIGHT CREW REPORTED STRONG ELECTRICAL BURNING ODOR IN COCKPIT NOTICED AFTER LANDING. EWR MX R&R RELAY KO437 AND PERFORMED OPS CHECK SUCCESSFULL
- [SDR C2XA08IA070](https://openairdocs.org/sdr/C2XA08IA070), Feb 26, 2008: UNKNOWN. ODOR. IAH - FLIGHT 2656, DURING PREFLIGHT INSPECTION THE CREW REPORTED A FUEL SMELL IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFECTS NOTED, AND THE 
- [SDR C2XA08SH025](https://openairdocs.org/sdr/C2XA08SH025), Feb 16, 2008: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION BETWEEN FR 18-23. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR18-23 IAW EMB 145 SRM 51-40-02. THE AIRCRA
- [SDR C2XA07TY010](https://openairdocs.org/sdr/C2XA07TY010), Mar 2, 2007: POWER SUPPLY. DISCHARGED. 602 NR 482585- RT FWD EXTERIOR EMERGENCY LIGHT AND NR 2 AISLE CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 2 BATTERY POWER SUPPLY UNIT IAW EMB 145AMM 3
- [SDR C2XA07IA029](https://openairdocs.org/sdr/C2XA07IA029), Feb 6, 2007: FUSE. BLOWN. DURING MAINTENANCE INSPECTION THE RT FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A FUSE IN THE AFFECTED EMERGENCY
- [SDR C2XA06IA198](https://openairdocs.org/sdr/C2XA06IA198), Dec 24, 2006: WINDSHIELD. MALFUNCTIONED. BRO FLIGHT 3229 - THE CREW REPORTED SMOKE IN THE COCKPIT WHILE ARRIVING AT THE GATE. THE WINDSHIELD LEADS WERE RESECURED. LATER THAT DAY AT IAH, FLIGHT 3295, TH
- [SDR C2XA06BT018](https://openairdocs.org/sdr/C2XA06BT018), Apr 6, 2006: POWER SUPPLY. DISCHARGED. EWR - DURING ROUTINE MAINTENANCE FOUND THE AISLE EMERGENCY LIGHT AT ROW 1 - 3 NOT WORKING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY OVER SERVIC
- [SDR C2XA06SH040](https://openairdocs.org/sdr/C2XA06SH040), Mar 28, 2006: BEAM. CORRODED. SHV - DURING C CHECK, THE LOWER BAGGAGE DOOR CUT OUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02.
- [SDR C2XA06SH042](https://openairdocs.org/sdr/C2XA06SH042), Mar 28, 2006: FLOOR SUPPORT. CORRODED. SHV - DURING C CHECK, THE LEFT OMEGA BEAM LOWER FLANGE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND COMPLETED THE REPAIR IAW EMB 145 SRM 5

All 76: https://openairdocs.org/aircraft/N11565/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/N11565/stcs.md

## Earlier aircraft with N11565

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N11565 before.

- [Cancelled 1975-02-12](https://openairdocs.org/deregistered/N11565-1975-02-12): Douglas DC-6A, S/N 45499, built 1952. Exported to Colombia. Owner: [Kendall Aircraft Leasing Corp](https://openairdocs.org/faa-owner/KENDALL%20AIRCRAFT%20LEASING%20CORP), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)

## 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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