# N15509: 2000 Embraer EMB-135ER

- Status: Valid registration
- Airframe: [Embraer EMB-135ER](https://openairdocs.org/model/embraer-emb-135er) (registry code 3260307, 37 seats)
- Engine: [Allison AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 145238
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: March 28, 2000
- Certificate issued: January 28, 2019
- Expires: January 31, 2029
- Mode S code: A0DF3C
- 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=15509
- Page: https://openairdocs.org/aircraft/N15509

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): 89 in force

### Matched by airframe (Embraer EMB-135ER)

- [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 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 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 2007-04-09](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 2006-25-07](https://openairdocs.org/ad/2006-25-07): Fuel quantity indication system (FQIS) wire harness and the direct current (DC) fuel pump wire harness · Embraer EMB-135ER, EMB-135KE, EMB-145 and 4 more. Effective Jan 16, 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
- [AD 2004-25-21](https://openairdocs.org/ad/2004-25-21): Pitch trim system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 26, 2005
- [AD 2004-25-12](https://openairdocs.org/ad/2004-25-12): Passenger service unit (PSU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 13, 2005

### Matched by engine (Allison AE-3007A)

- [AD 2020-16-13](https://openairdocs.org/ad/2020-16-13): Turbine Engine Compressor Section · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Aug 14, 2020
- [AD 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018
- [AD 2013-26-06](https://openairdocs.org/ad/2013-26-06): High-pressure turbine (HPT) stage 2 wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Feb 7, 2014
- [AD 2011-22-03](https://openairdocs.org/ad/2011-22-03): Low-cycle fatigue cracks · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 4 more. Effective Nov 17, 2011
- [AD 2007-24-05](https://openairdocs.org/ad/2007-24-05): Engine oil temperature · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 8 more. Effective Jan 2, 2008
- [AD 2004-04-05](https://openairdocs.org/ad/2004-04-05): Engine oil system · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Mar 9, 2004
- [AD 2001-25-05](https://openairdocs.org/ad/2001-25-05): Compressor Cone Shafts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jan 23, 2002
- [AD 2001-19-03](https://openairdocs.org/ad/2001-19-03): High Pressure Turbine 1st to 2nd Stage Turbine Spacer · Rolls-Royce AE 3007A and AE 3007C. Effective Oct 29, 2001
- [AD 2001-17-31](https://openairdocs.org/ad/2001-17-31): Second Stage High Pressure Turbine Wheel · Rolls-Royce AE 2100A, AE 2100C, AE 2100D3 and 2 more. Effective Oct 5, 2001
- [AD 2000-18-06](https://openairdocs.org/ad/2000-18-06): Digital Electronic Controls · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 22, 2000
- [AD 2000-13-01](https://openairdocs.org/ad/2000-13-01): Turbine Wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 1, 2000
- [AD 2000-11-22](https://openairdocs.org/ad/2000-11-22): Critical Life-Limited Parts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Aug 7, 2000
- [AD 99-03-03](https://openairdocs.org/ad/99-03-03): Full Authority Digital Engine Control (FADEC) · Rolls-Royce AE 3007A and AE 3007A1/1. Effective Feb 16, 1999
- [AD 98-11-32](https://openairdocs.org/ad/98-11-32): Sump Magnetic Chip Collector Plug · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Jun 18, 1998

### Historical (superseded or no longer in force)

- [AD 2008-13-14](https://openairdocs.org/ad/2008-13-14) (historical): Fuel system limitations (FSL) · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jul 30, 2008
- [AD 2007-12-17](https://openairdocs.org/ad/2007-12-17) (historical): Metallic tubes enclosing the vent and pilot valve wires · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Jul 19, 2007
- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 2006-04-02](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 2003-09-03](https://openairdocs.org/ad/2003-09-03) (historical): Cartridge flange · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 3 more. Effective May 14, 2003
- [AD 2002-16-06](https://openairdocs.org/ad/2002-16-06) (historical): Auxiliary power unit (APU) · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 2 more. Effective Aug 27, 2002
- [AD 2002-08-21](https://openairdocs.org/ad/2002-08-21) (historical): Bonding Jumpers that Connect the Horizontal Stabilizer to the Vertical Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 2 more. Effective May 16, 2002
- [AD 2002-08-18](https://openairdocs.org/ad/2002-08-18) (historical): Actuator Clutches of the Primary and Backup Pitch Trim Systems of the Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 2 more. Effective May 16, 2002
- [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 2001-17-03](https://openairdocs.org/ad/2001-17-03) (historical): Engine Thrust Reverser Stow/Transit Switches · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Sep 5, 2001
- [AD 2001-10-15](https://openairdocs.org/ad/2001-10-15) (historical): Fire Extinguisher Bottles · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Jun 8, 2001
- [AD 2001-10-01](https://openairdocs.org/ad/2001-10-01) (historical): Airplane Flight Manuals--APU Start/Stop Switch Panel · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective May 29, 2001
- [AD 2000-19-03](https://openairdocs.org/ad/2000-19-03) (historical): Fuel System Tubing · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 1 more. Effective Oct 3, 2000
- [AD 2000-19-02](https://openairdocs.org/ad/2000-19-02) (historical): Electric Fuel Pumps · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Oct 3, 2000
- [AD 2000-13-02](https://openairdocs.org/ad/2000-13-02) (historical): Precooler Differential Pressure Switches · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Jul 3, 2000
- [AD 2000-04-09](https://openairdocs.org/ad/2000-04-09) (historical): Elevator Servo Tab and Spring Tab Hinge Fittings of the Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Mar 10, 2000
- [AD 2010-19-01](https://openairdocs.org/ad/2010-19-01) (historical): High pressure turbine · Rolls-Royce AE 3007A. Effective Oct 27, 2010
- [AD 2009-08-51](https://openairdocs.org/ad/2009-08-51) (historical): High-pressure turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 6 more. Effective May 27, 2009
- [AD 2008-26-06](https://openairdocs.org/ad/2008-26-06) (historical): High-pressure turbine (HPT) · AE 3007A. Effective Jan 8, 2009
- [AD 2008-19-51](https://openairdocs.org/ad/2008-19-51) (historical): AE 3007A, AE 3007A1, AE 3007A1E and 5 more
- [AD 2001-08-15](https://openairdocs.org/ad/2001-08-15) (historical): Oil System · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective May 14, 2001
- [AD 2000-09-05](https://openairdocs.org/ad/2000-09-05) (historical): Cone Shafts · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jul 5, 2000
- [AD 99-02-51](https://openairdocs.org/ad/99-02-51) (historical): Starter Shaft Seal · AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Apr 20, 1999

All 114: https://openairdocs.org/aircraft/N15509/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 N15509.

## NTSB investigations on N15509 not matched to an aircraft (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ANC84LA058](https://openairdocs.org/ntsb/ANC84LA058), Apr 21, 1984: Fairchild C-119 (N15509), Venetie, AK, destroyed

## FAA accident and incident reports

None matched to N15509.

## Reports on N15509 not matched to an aircraft (1)

They name N15509, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Accident 19840421045909A](https://openairdocs.org/incident/19840421045909A), Apr 21, 1984: Frchld C119 (N15509), Tobin Creek, AK, Substantial damage. Left wheel struck a snow berm on takeoff and pulled aircraft into a snowbank. Steering degraded by wind and gravel.

## Service difficulty reports (43)

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 C2XA08CL014](https://openairdocs.org/sdr/C2XA08CL014), Jan 29, 2008: MODULE. DEFECTIVE. DAY FLIGHT 2382 - THE CREW REPORTED 10 MINUTES INFLIGHT IN CLIMB MODE THE NR 2 ENGINE POWERED BACK TO FLIGHT IDLE UNCOMMANDED. THE AIRCRAFT DIVERTED TO CLE AND 
- [SDR C2XA07RI059](https://openairdocs.org/sdr/C2XA07RI059), Jul 11, 2007: INVERTER. INOPERATIVE. DURING A ROUTINE MX INSPECTION, NR 1 EMERGENCY SIDE MARKER LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 INVERTER WITH OPERATIONAL CHECK GO
- [SDR C2XA06SD014](https://openairdocs.org/sdr/C2XA06SD014), Aug 15, 2006: LIGHT. INOPERATIVE. SDF - DISCREPANCY - 12A EMERGENCY LIGHT INOP. REMOVED AND REPLACED 12A EMERGENCY LIGHT IAW EMB 135 AMM 33-50-13. OPS CHECK GOOD.
- [SDR C2XA06CL068](https://openairdocs.org/sdr/C2XA06CL068), Aug 12, 2006: INVERTER. INOPERATIVE. DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT LIGHT WAS INOPERATIVE AT THE LEFT OVERWING EXIT DOOR. MAINTENANCE INSPECTED AND REPLACED THE NR 4 INVERTER. OPERAT
- [SDR C2XA06CL062](https://openairdocs.org/sdr/C2XA06CL062), Jun 20, 2006: SIGN. INOPERATIVE. DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT WALL LIGHTED PLACARD WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LIGHTED PLACARD. OPERATIONAL CHECKS W
- [SDR C2XA06CL022](https://openairdocs.org/sdr/C2XA06CL022), Feb 7, 2006: WINDSHIELD. FAULTY. CLE FLIGHT 2453 THE CREW REPORTED SMOKE VISIBLE FROM CAPTAIN'S LOWER WINDSHIELD. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD. OPERATIONAL CHECKS 
- [SDR C2XA05CL040](https://openairdocs.org/sdr/C2XA05CL040), May 25, 2005: BELLCRANK. WORN. CREW REPORTED MAIN CABIN DOOR HARD TO OPEN. MX INSP AND REPLACED ACTUATING CAM BELLCRANK AND BUSHING. OPS CHECK GOOD.
- [SDR C2XA05CL039](https://openairdocs.org/sdr/C2XA05CL039), May 22, 2005: BAR. BINDING. CLE FLIGHT 2944 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND ADJUSTED THE UPPER AND LOWER STABILIZER BARS OF THE MAIN 
- [SDR C2XA05CL020](https://openairdocs.org/sdr/C2XA05CL020), Apr 13, 2005: SIGN. INOPERATIVE. DURING ROUTINE MAINTENANCE, THE EXIT ROW EMERGENCY EXIT SIGN DID NOT ILLUMINATE DURING TESTING. MAINTENANCE REPLACED THE EXIT SIGN AND OPERATIONAL TESTS WERE GO
- [SDR C2XA04SH196](https://openairdocs.org/sdr/C2XA04SH196), Apr 5, 2004: LIGHT. BURNED OUT. SHV- DURING C-CHECK THE EMERGENCY LIGHT ON PANEL 234ARC FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW EMB 135 AMM 33-50-14. THE 
- [SDR C2XA04SH197](https://openairdocs.org/sdr/C2XA04SH197), Apr 5, 2004: LIGHT. BURNED OUT. SHV- DURING C-CHECK THE EMERGENCY LIGHT ON PANEL 233 BLC WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW EMB 135 AMM 33-50-15. THE
- [SDR C2XA04SH192](https://openairdocs.org/sdr/C2XA04SH192), Apr 3, 2004: SILL. CORRODED. SHV- DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPR
- [SDR C2XA04SH185](https://openairdocs.org/sdr/C2XA04SH185), Mar 27, 2004: CROSSBEAM. CORRODED. SHV- DURING C-CHECK THE CROSSBEAM AT FRAME 22 BETWEEN THE RIGHT SILL AND THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFF
- [SDR C2XA04SH184](https://openairdocs.org/sdr/C2XA04SH184), Mar 27, 2004: ANGLE. CORRODED. SHV- DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 135 SRM 51-40-02. TH
- [SDR C2XA04SH183](https://openairdocs.org/sdr/C2XA04SH183), Mar 27, 2004: SILL. CORRODED. SHV- DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED AT FRAME 19 TO FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 1
- [SDR C2XA04SH182](https://openairdocs.org/sdr/C2XA04SH182), Mar 27, 2004: STIFFENER. GOUGED. SHV- DURING C-CHECK THE NR 1 LOWER COWLING AFT EDGE STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 135 SRM 51
- [SDR C2XA04SH181](https://openairdocs.org/sdr/C2XA04SH181), Mar 24, 2004: RIB. GOUGED. SHV- DURING C-CHECK THE NR 1 ENGINE UPPER COWLING, AFT OUTBOARD RIB WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR 
- [SDR C2XA04SH180](https://openairdocs.org/sdr/C2XA04SH180), Mar 24, 2004: STRAP. CORRODED. SHV- DURING C-CHECK THE AFT FLOORBEAM AT FRAME 17 TO 19 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 135 SRM 51-40-
- [SDR C2XA04SH179](https://openairdocs.org/sdr/C2XA04SH179), Mar 24, 2004: STRAP. CORRODED. SHV- DURING C-CHECK THE FORWARD FLOORBEAM AT FRAME 16 TO FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DIGITAL IAW EMB 135 SR
- [SDR C2XA04SH178](https://openairdocs.org/sdr/C2XA04SH178), Mar 21, 2004: ANGLE. CORRODED. SHV- DURING C-CHECK THE LEFT RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE AFFECTED ANGLE, FABRICATED AND INSTALLED A NEW RAMP ANGLE 
- [SDR C2XA04SH177](https://openairdocs.org/sdr/C2XA04SH177), Mar 21, 2004: SILL. CORRODED. SHV- DURING C-CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAF
- [SDR C2XA04SH176](https://openairdocs.org/sdr/C2XA04SH176), Mar 21, 2004: BUTTSTRAP. CORRODED. SHV- DURING C-CHECK THE AFT FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE 
- [SDR C2XA04SH175](https://openairdocs.org/sdr/C2XA04SH175), Mar 21, 2004: FIREWALL. CRACKED. SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT HAND UPPER APU MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW 
- [SDR C2XA04CL012](https://openairdocs.org/sdr/C2XA04CL012), Feb 23, 2004: CONNECTOR. LOOSE. CLE FLIGHT 2152 THE CREW REPORTED THE FORWARD AISLE PATH EMERGENCY LIGHT WAS INTERMITTENT WHEN TESTED. MAINTENANCE INSPECTED AND RESECURED THE CONNECTION ON THE
- [SDR C2XA03CL104](https://openairdocs.org/sdr/C2XA03CL104), Jun 5, 2003: LIGHT. INOPERATIVE. CLE FLIGHT 2083, THE CREW REPORTED AISLE PATH EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOO
- [SDR C2XA03CL068](https://openairdocs.org/sdr/C2XA03CL068), Mar 13, 2003: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE THE FIRST ALL WHITE EMERGENCY AISLE PATH LIGHTING STRIP WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE AISLE PATH LIGHT STRIP. OPERA
- [SDR C2XA03CL035](https://openairdocs.org/sdr/C2XA03CL035), Feb 8, 2003: FIRE DETECTOR. CHAFED. CLE FLIGHT 2116 THE CREW REPORTED A ENGINE NR 2 FIRE DETECT FAIL MESSAGE INTERMITTENTLY IN FLIGHT. MAINTENANCE REPLACED THE NR 2 ENGINE PYLON FIRE DETECTOR ASSE
- [SDR C2XA03CL028](https://openairdocs.org/sdr/C2XA03CL028), Feb 2, 2003: DETECTOR. FAILED. CLE FLIGHT#2083 THE CREW REPORTED A ENGINE #2 FIRE DETECTOR FAIL MESSAGE INTERMITTENTLY ON THE DESCENT.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE 
- [SDR C2XA01TY178](https://openairdocs.org/sdr/C2XA01TY178), Nov 11, 2001: FLOORBEAM. CORRODED. TYS DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE FORWARD DIGITAL BETWEEN FRAMES 15 AND 16 AT CENTER AND LEFT SIDE. MAINTENANCE REMOVED THE DAMAGED 
- [SDR C2XA01TY177](https://openairdocs.org/sdr/C2XA01TY177), Nov 11, 2001: FLOORBEAM. CORRODED. TYS DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED SECTION, FABRICATED NEW ANGLE, SHIM, 
- [SDR C2XA01TY176](https://openairdocs.org/sdr/C2XA01TY176), Nov 11, 2001: ANTENNA. CORRODED. TYS During a scheduled inspection the lower TCAS antenna was found corroded. Maintenance removed and replaced the TCAS antenna I.A.W.-EMB-135-AMM-34-43-03, oper
- [SDR C2XA01TY175](https://openairdocs.org/sdr/C2XA01TY175), Nov 11, 2001: ROD END. CORRODED. TYS DURING A SCHEDULED 1-C INSPECTION THE LEFT FUSELAGE TO SPAR 3 ROD END ASSEMBLY HAD CORRODED ON THE LOWER ROD END. MAINTENANCE REMOVED AND REPLACED THE LEFT 
- [SDR C2XA01TY174](https://openairdocs.org/sdr/C2XA01TY174), Nov 11, 2001: ROD END. CORRODED. TYS DURING A 1-C INSPECTION THE RIGHT FUSELAGE TO SPAR 3 ROD ASSEMBLY HAD CORROSION ON THE LOWER ROD ENDS. MAINTENANCE REMOVED AND REPLACED RIGHT ROD ASSEMBLIES
- [SDR C2XA01TY173](https://openairdocs.org/sdr/C2XA01TY173), Nov 9, 2001: FLOOR SUPPORT. CORRODED. TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE AFT GUSSET AT FRAME 18. MAINTENANCE REMOVED AND REPLACED AFT GUSSET AT FRAME 18 IAW EMB-135 SRM 51-
- [SDR C2XAS01TY172](https://openairdocs.org/sdr/C2XAS01TY172), Nov 8, 2001: ANGLE. CORRODED. TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM RAMP ANGLE AT FRAME 17. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-1
- [SDR C2XA01CL211](https://openairdocs.org/sdr/C2XA01CL211), Oct 3, 2001: TRANSPONDER. FAILED. CLE FLIGHT NR 3899 CREW REPORTED THAT THE NUMBER 1 TRANSPONDER NO MODE "C". NUMBER 2 TRANSPONDER ALREADY ON MEL. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MA
- [SDR C2XA01CL034](https://openairdocs.org/sdr/C2XA01CL034), Feb 25, 2001: SENSOR. FAILED. YYZ FLIGHT 3991 THE CREW REPORTED A AIR/GROUND MESSAGE WHILE POWERING UP THE AIRCRAFT AT THE GATE. REPORTED THE SENSORS APPEAR TO INDICATE THE AIRCRAFT WAS IN F
- [SDR C2XA01CL005](https://openairdocs.org/sdr/C2XA01CL005), Jan 14, 2001: SENSOR. BURNED. EWR - FLT 3619 - THE CREW REPORTED SMOKE IN THE COCKPIT WHILE TAXI. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED
- [SDR C2XA01IA085](https://openairdocs.org/sdr/C2XA01IA085), Dec 20, 2000: LIGHT. INOPERATIVE. TYS - FLIGHT 3809, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH EMERGENCY EXIT LIGHTS DID NOT STAY ILLUMINATED. MAINTENANCE CLEANED AND 
- [SDR C2XA01IA084](https://openairdocs.org/sdr/C2XA01IA084), Dec 19, 2000: LIGHT. INOPERATIVE. CLE - FLIGHT 3667, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH LIGHTING STRIP AT ROWS 8 AND 9 WERE INOPERATIVE. MAINTENANCE REMOVED AND
- [SDR 20010112SG058](https://openairdocs.org/sdr/20010112SG058), Dec 13, 2000: SMOKE DETECTOR. MALFUNCTIONED. CLE - FLT 4194 - THE CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A LAVATORY SMOKE WARNING. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINT
- [SDR C2XA00CL084](https://openairdocs.org/sdr/C2XA00CL084), Oct 16, 2000: NOZZLE. MALFUNCTIONED. CLE - FLT 4046 - THE CREW REPORTED WHEN THE ANTI-ICE WAS TURNED ON IN FLIGHT THERE WERE EXHAUST FUMES EVIDENT IN THE CABIN. MAINTENANCE REMOVED AND REPLACED THE
- [SDR C2XA00CL045](https://openairdocs.org/sdr/C2XA00CL045), Jun 7, 2000: WARNING SYSTEM. ACTIVATED. CLE - FLT 3815 - THE CREW REPORTED AFTER TAKEOFF, RECEIVED A LAVATORY SMOKE WARNING. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE IN

## STCs that may be installed (OpenAirDocs) (68, 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-135ER)

- [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 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 ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [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 ST02815LA](https://openairdocs.org/stc/ST02815LA): Installation of Airworthy R/H and L/H Stowage Units. Airworthy Incorporated
- [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 ST04327CH](https://openairdocs.org/stc/ST04327CH): Installation of High Speed Internet System and Wireless Activation. Nextant Aerospace 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 ST09858SC](https://openairdocs.org/stc/ST09858SC): Installation of cabin automatic coffee brewing system. Safran Cabin Germany Gmbh
- [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 ST04049NY](https://openairdocs.org/stc/ST04049NY): Installation of a Hoffman Engineering LLC LED Landing Light to replace the OEM Q4559 Series Incandescent Lamp, used as a Landing/Takeoff Light. Hoffman Engineering LLC
- [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 ST03889AT](https://openairdocs.org/stc/ST03889AT): Installation of Aircell Axxess Cabin Telecommunication Router (CTR) 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
- [STC ST04282AT](https://openairdocs.org/stc/ST04282AT): Installation of the Honeywell DU-875 LCD Flight Display. Chippewa Aerospace Inc

All 68: https://openairdocs.org/aircraft/N15509/stcs.md

## Earlier aircraft with N15509

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N15509 before.

- [Cancelled 1994-05-20](https://openairdocs.org/deregistered/N15509-1994-05-20): Beech Acft B200T, S/N BT35. Exported to Malaysia. Owner: [Hawker Pacific Inc](https://openairdocs.org/faa-owner/HAWKER%20PACIFIC%20INC), [Sun Valley, CA](https://openairdocs.org/faa-place/CA/Sun%20Valley)
- [Cancelled 1937-01-15](https://openairdocs.org/deregistered/N15509-1937-01-15): National Airplane & Motor BLUEBIRD LP-1, S/N 6, built 1936. Owner: [National Airplane & Motor Co](https://openairdocs.org/faa-owner/NATIONAL%20AIRPLANE%20%26%20MOTOR%20CO), [Billings, MT](https://openairdocs.org/faa-place/MT/Billings)
- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N15509-undated): Fairchild C-119G, S/N 10775. Triennial form not returned

## Related

- Other Embraer EMB-135ER aircraft: https://openairdocs.org/model/embraer-emb-135er/aircraft.md
- The Allison AE-3007A engine: https://openairdocs.org/engine/allison-ae-3007a.md

---
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