# N16502: 1999 Embraer EMB-135ER

- Status: Valid registration
- Airframe: [Embraer EMB-135ER](https://openairdocs.org/model/embraer-emb-135er) (registry code 3260307, 37 seats)
- Engine: [Allison AE3007C series](https://openairdocs.org/engine/allison-ae3007c-series) (registry code 03028)
- 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: 145166
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: September 3, 1999
- Certificate issued: September 19, 2019
- Expires: September 30, 2029
- Mode S code: A106B4
- 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=16502
- Page: https://openairdocs.org/aircraft/N16502

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. The registry lists only the engine series, so ADs for every Allison AE3007C model are included.

## ADs that may apply (OpenAirDocs): 87 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 AE3007C series)

- [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 2017-11-05](https://openairdocs.org/ad/2017-11-05): Turbine/ turboprop Engine, Turbine Section · Rolls-Royce AE 3007C and AE 3007C1. Effective Jul 18, 2017
- [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 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 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 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 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 107: https://openairdocs.org/aircraft/N16502/ads.md

## Information bulletins (advisory) (9 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 NE-11-22](https://openairdocs.org/saib/NE-11-22): Engine Controls. Issued Feb 23, 2011
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N16502.

## FAA accident and incident reports (1)

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

- [Incident 20040815030839I](https://openairdocs.org/incident/20040815030839I), Aug 15, 2004: Emb EMB135ER (N16502), Newark, NJ. (-23) On August 14, 2004, jet link flight 2885 a Emb-135-ER aircraft, N16502, while enroute from kcle to khpn, declared an inflight emergency and diverted to…

## Reports on N16502 not matched to an aircraft (1)

They name N16502, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19950130004719I](https://openairdocs.org/incident/19950130004719I), Jan 30, 1995: Cessna STC185 (N16502), Fairbanks, AK. Narrative: rough engine during level test flight of new stc'd eng & prop installation. Made precautionary landing on tanana river ice. Mechanic flew to landing…

## Service difficulty reports (57, 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 FJTA2026072716502](https://openairdocs.org/sdr/FJTA2026072716502), Jul 26, 2026: WINDSHIELD. CRACKED. WHILE CLIMBING THROUGH FL220 THE OUTER PANE OF THE FIRST OFFICER'S WINDSHIELD SHATTERED. THIS WINDSHIELD WAS RECENTLY REPLACED ON 7/18/2026 WITH AN OVERHAULED U
- [SDR ASOA201703314015](https://openairdocs.org/sdr/ASOA201703314015), Mar 31, 2017: FLOOR SUPPORT. CORRODED. DURING A MAINTENANCE INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE PERFORMED AN INSERTION REPAIR ON THE AFFECTED BEAM, AND
- [SDR C2XA08RI070](https://openairdocs.org/sdr/C2XA08RI070), May 12, 2008: MODULE. INACCURATE. FLIGHT 1202 - EWR - FLIGHT CREW REPORTED STEERING PULLED TO LEFT AND SHAKING LEFT & RIGHT. CREW RETURNED AIRCRAFT TO GATE. EWR MX REMOVED AND REPLACED HYDRAULIC
- [SDR C2XA08RI067](https://openairdocs.org/sdr/C2XA08RI067), May 11, 2008: SMOKE DETECTOR. FALSE ACTIVATION. FLIGHT 3096 - EWR - FLIGHT CREW REPORTED BAGGAGE EXTINGUISH WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALSO, INTERMITTENT BAGGAGE SMOKE WARNING ON EICA
- [SDR C2XA08RI061](https://openairdocs.org/sdr/C2XA08RI061), May 2, 2008: SMOKE DETECTOR. LOOSE. FLIGHT 2424 - BAG SMOKE WARNING IN FLIGHT, BOTH LIGHTS AND EICAS MESSAGES STAYED FOR FEW SECONDS THEN WENT OFF. MX RESECURED LOOSE CONNECTOR PLUG AT AFT SMOKE D
- [SDR C2XA08CL053](https://openairdocs.org/sdr/C2XA08CL053), May 1, 2008: WIRE. CHAFED. CLE FLIGHT 2419 - THE CREW REPORTED A APU FIRE DETECT FAIL MESSAGE INTERMITTENTLY DURING FLIGHT. MAINTENANCE INSPECTED AND REPAIRED A CHAFED WIRE ON THE APU HAR
- [SDR C2XA08RI068](https://openairdocs.org/sdr/C2XA08RI068), Jan 11, 2008: SMOKE DETECTOR. INTERMITTENT. FLIGHT 3096 - EWR - FLIGHT CREW REPORTED BAGGAGE EXTINGUISH WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALSO, INTERMITTENT BAGGAGE SMOKE WARNING ON EICA
- [SDR C2XA07CL077](https://openairdocs.org/sdr/C2XA07CL077), Sep 13, 2007: SHOCK ABSORBER. BINDING. CLE FLIGHT 2514 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND
- [SDR C2XA07CL069](https://openairdocs.org/sdr/C2XA07CL069), Aug 16, 2007: WIRE HARNESS. FAULTY. CLE FLIGHT 2457 - THE CREW REPORTED A INTERMITTANT ENGINE NR 1 FIRE DETECT FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 1ENGINE HARNESS. OP
- [SDR C2XA07RI002](https://openairdocs.org/sdr/C2XA07RI002), Jan 13, 2007: SEAL. LEAKING. FLT 3031 - RIC - DURING FLIGHT, RIGHT OVERWING EMERGENCY EXIT DOOR AIR LEAK. RIC MX REMOVED THE DOOR, LUBRICATED DOOR SEAL, AND REINSTALLED IT. OPERATIONAL CHEC
- [SDR C2XA06CL085](https://openairdocs.org/sdr/C2XA06CL085), Oct 13, 2006: BATTERY. DISCHARGED. DURING ROUTINE MAINTENANCE THE FLIGHT ATTENDANT'S EMERGENCY FLASHLIGHT WAS DIM. MAINTENANCE INSPECTED AND REPLACED THE FLASHLIGHT BATTERY. OPERATIONAL CHECKS WE
- [SDR C2XA06CL072](https://openairdocs.org/sdr/C2XA06CL072), Sep 5, 2006: SPLICE. DAMAGED. CLE - FLIGHT 2828, THE CREW REPORTED THE RIGHT SIDE EXIT ROW EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED DAMAGED WIRE SPLICE BEHIND
- [SDR C2XA06SD015](https://openairdocs.org/sdr/C2XA06SD015), Aug 22, 2006: SMOKE DETECTOR. INOPERATIVE. SDF - BAGGAGE FIRE DETECTOR INOP. REMOVED AND REPLACED FWD BAGGAGE SMOKE DETECTOR IAW EMB 135 AMM 26-15-01. OPS CHECK GOOD.
- [SDR C2XA06SH069](https://openairdocs.org/sdr/C2XA06SH069), Jun 21, 2006: STRINGER. CORRODED. SHV - DURING C-CHECK CORROSION DAMAGE WAS DISCOVERED ON STR 20L BETWEEN FRAME 59 AND 60. MAINTENANCE REMOVED CORROSION AND REPAIRED STR 20L BETWEEN FRAME 59 AND
- [SDR C2XA06SH064](https://openairdocs.org/sdr/C2XA06SH064), Jun 17, 2006: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 32 TO 35. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER RE
- [SDR C2XA06SH063](https://openairdocs.org/sdr/C2XA06SH063), Jun 17, 2006: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LEFT OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IA
- [SDR C2XA06SH062](https://openairdocs.org/sdr/C2XA06SH062), Jun 17, 2006: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LEFT OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED BETWEEN FRAMES 23 TO 32. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A FILLER RE
- [SDR C2XA06SH061](https://openairdocs.org/sdr/C2XA06SH061), Jun 17, 2006: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LEFT OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IA
- [SDR C2XA06SH065](https://openairdocs.org/sdr/C2XA06SH065), Jun 17, 2006: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 135 
- [SDR C2XA04BT089](https://openairdocs.org/sdr/C2XA04BT089), Aug 15, 2004: TUBE. LEAKING. ENROUTE, DIVERTED, CREW REPORTED, ENGINE NR 1 LOST OIL INFLIGHT. PERFORMED SHUTDOWN IAW QRH. AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED PRES
- [SDR C2XA03TY161](https://openairdocs.org/sdr/C2XA03TY161), Sep 11, 2003: FLOORBEAM. CORRODED. DURING A SCHEDULED INSPECTION THE RT HAND FORWARD DIGITAL UNDER THE GALLEY WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21
- [SDR C2XA03TY160](https://openairdocs.org/sdr/C2XA03TY160), Sep 11, 2003: ANGLE. CORRODED. TYS DUEING A SCHEDULED INSPECTION THE LEFT HAND FORWARD RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB SRM 51-40-0
- [SDR C2XA03TY159](https://openairdocs.org/sdr/C2XA03TY159), Sep 11, 2003: FLOORBEAM. CORRODED. DURING A SCHEDULED INSPECTION THE FORWARD FLOORBEAM TOP CAP WAS FOUND TO BE CORRODED UNDER SEAT TRACK LF1. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB 
- [SDR C2XA03TY158](https://openairdocs.org/sdr/C2XA03TY158), Sep 11, 2003: SILL. DAMAGED. DURING A SCHEDULED INSPECTION, DAMAGE WAS FOUND TO THE SERVICE DOOR FORWARD SILL AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR SILL IAW EMB SRM
- [SDR C2XA03TY157](https://openairdocs.org/sdr/C2XA03TY157), Sep 10, 2003: AXLE. DAMAGED. DURING A SCHEDULED INSPECTION THE RIGHT MLG RETRACTION AXLE CHROME PLATED AREA DAMAGED. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG RETRACTION AXLE I/A/W-EMB
- [SDR C2XA03TY156](https://openairdocs.org/sdr/C2XA03TY156), Sep 10, 2003: SILL. DAMAGED. DURING A SCHEDULED INSPECTION, DAMAGE WAS FOUND TO THE MAIN DOOR SILL SKIN, MAINTENANCE REMOVED AND REPLACED THE SILL I/A/W-EMB-135-AMM-53-21-00.
- [SDR C2XA03TY155](https://openairdocs.org/sdr/C2XA03TY155), Sep 10, 2003: SKIN. DENTED. DURING A SCHEDULED INSPECTION 2 DENTS WHERE FOUND AFT OF THE PAX DOOR BETWEEN FRAMES 19 AND 20, ABOVE STR 12L. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED 
- [SDR C2XA03TY153](https://openairdocs.org/sdr/C2XA03TY153), Sep 10, 2003: BEARING CAP. CRACKED. DURING A SCHEDULED INSPECTION THE RIGHT HAND AFT MAIN LANDING GEAR BEARING CAP FAILED NDI FOR CRACKS AT THE MOUNTING HOLES. MAINTENANCE REMOVED AND REPLACED THE
- [SDR C2XA03TY152](https://openairdocs.org/sdr/C2XA03TY152), Sep 10, 2003: CAP. CRACKED. DURING A SCHEDULED INSPECTION THE LT MLG BEARING CAP FAILED NDI FOR CRACKS AT THE MOUNTING HOLES. MAINTENANCE REMOVED AND REPLACED THE BEARING CAP IAW EMB M.M. 
- [SDR C2XA03TY151](https://openairdocs.org/sdr/C2XA03TY151), Sep 10, 2003: FLOORBEAM. CORRODED. DURING A SCHEDULED INSPECTION THE FLOORBEAM AT FRAME 22 RT, WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FRAME 2
- [SDR C2XA03TY150](https://openairdocs.org/sdr/C2XA03TY150), Sep 10, 2003: GUSSET. CORRODED. DURING A SCHEDULED INSPECTION THE GALLEY FLOOR AFT GUSSET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT GUSSET IAW EMB SRM 51-40-02, THE RE
- [SDR C2XA03TY149](https://openairdocs.org/sdr/C2XA03TY149), Sep 10, 2003: PLATE. CORRODED. DURING A SCHEDULED INSPECTION THE GALLEY RIGHT HAND AFT CROSS BEAM PLATE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CROSS BEAM PLATE IAW EMB
- [SDR C2XA03TY148](https://openairdocs.org/sdr/C2XA03TY148), Sep 10, 2003: CAM. CORRODED. DURING A SCHEDULED INSPECTION THE NOSE LANDING GEAR STRUT MAIN HOUSING AND LOWER CAM WERE FOUND TO HAVE AREAS OF CORROSION AND PITTING. MAINTENANCE REMOVED AND 
- [SDR C2XA03TY147](https://openairdocs.org/sdr/C2XA03TY147), Sep 10, 2003: BRACKET. CORRODED. DURING A SCHEDULE INSPECTION THE MAIN PASSENGER DOOR THRESHOLD BRACKETS WERE FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE THRESHO
- [SDR C2XA03TY145](https://openairdocs.org/sdr/C2XA03TY145), Sep 4, 2003: SILL. CORRODED. TYS DURING A SCHEDULED INSPECTION THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR SILL IAW EMB SRM 51-
- [SDR C2XA03TY144](https://openairdocs.org/sdr/C2XA03TY144), Aug 30, 2003: BUTTSTRAP. CORRODED. TYS DURING A SCHEDULED 2C INSPECTION THE FWD DIGITAL BUTTSTRAP WAS CORRODED. MAINT REMOVED THE FWD DIGITAL, FAB A DOUBLER AND INSTALL A NEW FWD DOUBLER, ALLODIN
- [SDR C2XA03TY142](https://openairdocs.org/sdr/C2XA03TY142), Aug 28, 2003: FLOORBEAM. CORRODED. TYS DURING A SCHEDULED 2C INSPECTION THE FLOORBEAM AT FR 22 RT SIDE WAS FOUND CORRODED IN SEVERAL AREAS. MAINT R&R THE FLOOR BEAM AT FR 22 IAW EMB 135/145 SRM 5
- [SDR C2XA03TY141](https://openairdocs.org/sdr/C2XA03TY141), Aug 28, 2003: PLATE. CORRODED. TYS DURING A SCHEDULED 2C INSPECTION THE RT AFT CROSS BEAM PLATE WAS CORRODED. MAINT R&R THE AFT CROSS BEAM PLATE IAW EMB 135/145 SRM 51-10-02 ALLODINED, PRIMED
- [SDR C2XA03TY140](https://openairdocs.org/sdr/C2XA03TY140), Aug 28, 2003: GUSSET. CORRODED. TYS DURING A SCHEDULED 2C INSPECTION THE AFT GUSSET WAS FOUND WITH SEVERAL AREAS THAT WAS CORRODED. MAINT R&R THE AFT GUSSET IAW 135/145 SRM 51-40-02. ALL WORK 
- [SDR C2XA03BT038](https://openairdocs.org/sdr/C2XA03BT038), Mar 14, 2003: BEARING. SEIZED. EWR ACFT PULLS RIGHT ON T/O. ABORTED T/O AND TAXI BACK TO GATE. ACFT CONTINUED TO PULL RIGHT DURING TAXI. REMOVED AND REPLACED NOSE TIRE/WHEEL ASSYS. FOUND SEIZ
- [SDR C2XA02CL105](https://openairdocs.org/sdr/C2XA02CL105), Apr 24, 2002: RECEPTACLE. BURNED. CLE FLIGHT 3180 THE CREW REPORTED ELECTRICAL SMELL COMING FROM THE COFFEE WARMERS. MAINTENANCE INSPECTED AND REPLACED BOTH LEFT AND RIGHT COFFEE WARMER RECEPTAC
- [SDR C2XA02CL102](https://openairdocs.org/sdr/C2XA02CL102), Apr 20, 2002: LIGHT. INOPERATIVE. CLE MAINTENANCE FOUND THE CABIN EMERGENCY AISLE LIGHT INOPERATIVE DURING ROUTINE MAINTENANCE. MAINTENANCE REPLACED THE EMERGENCY AISLE LIGHT STRIP. OPERATIONAL 
- [SDR C2XA01CL228](https://openairdocs.org/sdr/C2XA01CL228), Nov 12, 2001: ACTUATOR. FAILED. MSN FLIGHT#3110 THE CREW REPORTED THE HORIZONTAL STABILIZER PITCH TRIM FAILED AFTER TAKEOFF.THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT.M
- [SDR C2XA01TY090](https://openairdocs.org/sdr/C2XA01TY090), Apr 25, 2001: BRACKET. CHAFED. TYS DURING A SCHEDULED INSPECTION THE MAIN CABIN DOOR, HANDLE BRACKET WAS FOUND TO BE CHAFED. MAINTENANCE REPAIRED THE DAMAGED AREA IAW EMB-GST-1405/01, THE REP
- [SDR C2XA01TY089](https://openairdocs.org/sdr/C2XA01TY089), Apr 25, 2001: PLATE. CORRODED. TYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE JUST AFT OF FLIGHT DECK WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A SLICE REPAIR IAW EMB-GS
- [SDR C2XA01TY088](https://openairdocs.org/sdr/C2XA01TY088), Apr 24, 2001: FLOORBEAM. CORRODED. TYS DURING A SCHEDULED INSPECTION THE LEFT HAND OMEGA BEAM AFT OF FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A SPLICE REPAIR IAW EMB-135 SRM-53
- [SDR C2XA01TY087](https://openairdocs.org/sdr/C2XA01TY087), Apr 23, 2001: ANGLE. CORRODED. TYS DURING A SCHEDULED INSPECTION THE LEFT OMEGA BEAM AFT RAMP ANGLE FORWARD OF FRAME 20 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW
- [SDR C2XA01TY086](https://openairdocs.org/sdr/C2XA01TY086), Apr 23, 2001: MOUNT. CHAFED. TYS DURING A SCHEDULED INSPECTION THE LEFT ENGINE PYLON FORWARD YOKE MOUNT WAS FOUND CHAFED. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB GST-1365/01, THE RE
- [SDR C2XA01TY085](https://openairdocs.org/sdr/C2XA01TY085), Apr 22, 2001: FLOORBEAM. CORRODED. TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND OMEGA BEAM WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION AT FRAME 20. MAINTENANCE REPAIRED THE OMEGA BEAM IAW EM
- [SDR C2XA01TY084](https://openairdocs.org/sdr/C2XA01TY084), Apr 22, 2001: FITTING. GOUGED. TYS DURING A SCHEDULED INSPECTION THE RIGHT HORIZONTAL ACTUATOR SUPPORT FITTING WAS FOUND GOUGED. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB GST-1340/01, T

All 57: https://openairdocs.org/aircraft/N16502/reports.md

## 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/N16502/stcs.md

## Earlier aircraft with N16502

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N16502 before.

- [Cancelled 1991-10-16](https://openairdocs.org/deregistered/N16502-1991-10-16): Piper PA-34-200, S/N 347350153. Triennial form not returned. Owner: [Hauser Herb L](https://openairdocs.org/faa-owner/HAUSER%20HERB%20L), [Londonderry, NH](https://openairdocs.org/faa-place/NH/Londonderry)

## Related

- Other Embraer EMB-135ER aircraft: https://openairdocs.org/model/embraer-emb-135er/aircraft.md
- The Allison AE3007C series engine: https://openairdocs.org/engine/allison-ae3007c-series.md

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