# N16987: 2000 Embraer EMB-145LR

- Status: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212, 55 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: 145261
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 13, 2000
- Certificate issued: August 18, 2022
- Expires: August 31, 2029
- Mode S code: A116AD
- Registered owner: [Delux Public Charter LLC](https://openairdocs.org/faa-owner/DELUX%20PUBLIC%20CHARTER%20LLC)
- Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas)
- Owner type: LLC
- Owner's area on the map: 32.8483° N, 96.8255° W: Placed by OpenAirDocs at the center of ZIP code 75209, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16987
- Page: https://openairdocs.org/aircraft/N16987

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 (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 2006-20-08](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 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 120: https://openairdocs.org/aircraft/N16987/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 N16987.

## FAA accident and incident reports

None matched to N16987.

## Service difficulty reports (81, 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 ASOA20191115112](https://openairdocs.org/sdr/ASOA20191115112), Nov 11, 2019: FUSE. FAILED. MX REPORTED MULTIPLE EXTERNAL EMERGENCY LIGHTS INOP. MX FOUND EMERGENCY LIGHT TRAY #1 FUSE BLOWN TO LH WING FUSELAGE FRONT AND CEILING PANEL LIGHT AISLE AND AT 
- [SDR ASOA2019062065078](https://openairdocs.org/sdr/ASOA2019062065078), Jun 16, 2019: UNKNOWN. ODOR. CREW REPORTED BURNING SMELL WHEN COFFEE MAKER #2 IN OPERATION. ITEM PLACED ON MEL. MX PERFORMED OPERATIONAL CHECK GOOD WITH NO BURNING SMELL NOTED.
- [SDR ASOA201905237050](https://openairdocs.org/sdr/ASOA201905237050), May 23, 2019: FRAME. CHAFED. TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND CHAFFING FROM A SCREW AT FRAME 70 BETWEEN STRINGER 12R AND 13R. MAINTENANCE REPAIRED THE CHAFE AREA FROM STR.12R TO 
- [SDR ASOA201905237049](https://openairdocs.org/sdr/ASOA201905237049), May 23, 2019: TRUNNION. CRACKED. TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE LT MLG AFT TRUNION CRACKED. MAINTENANCE REMOVED AND REPLACED THE LT TRUNION ON THE LT MLG AFT SIDE IAW ECTC ETD 
- [SDR ASOA201905147046](https://openairdocs.org/sdr/ASOA201905147046), May 14, 2019: RIB. CRACKED. TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND RIB 21 INSIDE ACCESS PANEL 551CB CRACKED. MAINTENANCE REMOVED THE DAMAGED AREA AND FAB. A FILLER AND DOUBLER FOR RIB
- [SDR ASOA201905147045](https://openairdocs.org/sdr/ASOA201905147045), May 14, 2019: RIB. CRACKED. TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND A CRACK AT RIB 21 INSIDE ACCESS PANEL 651CB. MAINTENANCE REMOVED THE DAMAGED AREA OF RIB 21 AND REPLACED WITH FILLER
- [SDR ASOA201901023001](https://openairdocs.org/sdr/ASOA201901023001), Jan 2, 2019: COFFEEMAKER. FAULTY. THE CREW REPORTED ELECTRICAL SMELL COMING FROM GALLEY, WENT AWAY WHEN COFFEE MAKERS WERE SHUT OFF. MAINTENANCE REPLACED COFFEE BREWER IN LT POSITION. OPS CHECK 
- [SDR ASOA201705113145](https://openairdocs.org/sdr/ASOA201705113145), May 11, 2017: STRINGER. CRACKED. LEFT REAR FUSELAGE STRINGER 2L CRACKED AT FRAME 75. THE STRINGER WAS REPAIRED IAW SRM 53-00-03.
- [SDR ASOA201705093143](https://openairdocs.org/sdr/ASOA201705093143), May 9, 2017: CHANNEL. CORRODED. SERVICE DOOR CHANNEL CORRODED. CHANNEL REPLACED AS PER SRM 51-40-02.
- [SDR ASOA201705093142](https://openairdocs.org/sdr/ASOA201705093142), May 9, 2017: STRUCTURE. CORRODED. PAX DOOR SILL AFT "U" SHAPE CORRODED. AFT "U" SHAPE REPLACED AS PER SRM 51-40-02.
- [SDR ASOA201705093141](https://openairdocs.org/sdr/ASOA201705093141), May 9, 2017: STRUCTURE. CORRODED. PAX DOOR SILL FORWARD U SHAPE CORRODED. FORWARD U SHAPE REPLACED AS PER SRM 51-40-02.
- [SDR ASOA201705073140](https://openairdocs.org/sdr/ASOA201705073140), May 7, 2017: SEAT TRACK. CORRODED. CABIN SEAT TRACK LT NR 4 OUTBOARD CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06-400-801.
- [SDR ASOA201705073139](https://openairdocs.org/sdr/ASOA201705073139), May 7, 2017: SEAT TRACK. CORRODED. CABIN SEAT TRACK RT NR 3 INBOARD CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06-400-801.
- [SDR ASOA201705073138](https://openairdocs.org/sdr/ASOA201705073138), May 7, 2017: SEAT TRACK. CORRODED. CABIN SEAT TRACK RT NR 4 OUTBOARD CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06-400-801.
- [SDR ASOA201705073137](https://openairdocs.org/sdr/ASOA201705073137), May 7, 2017: BEARING. CORRODED. RT MLG AFT LOWER HALF BEARING CAP CORRODED. THE BEARING CAP WAS REPLACED IAW 57-26-00-220-CO2-A00.
- [SDR ASOA201705073136](https://openairdocs.org/sdr/ASOA201705073136), May 7, 2017: BEARING. CORRODED. LT MLG AFT LOWER HALF BEARING CAP CORRODED. THE BEARING CAP WAS REPLACED IAW 57-26-00-220-C02-A00.
- [SDR ASOA201705053135](https://openairdocs.org/sdr/ASOA201705053135), May 5, 2017: DOUBLER. CORRODED. CORROSION ON DOUBLER AROUND POTABLE WATER NIPPLES. DOUBLER REPLACED IAW SRM 51-40-02.
- [SDR ASOA201705053134](https://openairdocs.org/sdr/ASOA201705053134), May 5, 2017: STRINGER. CORRODED. STRINGER 15R BETWEEN FRAMES 40 AND 41 CORRODED BEYOND LIMITS. REPLACED IAW SRM 53-10-02.
- [SDR ASOA201705043133](https://openairdocs.org/sdr/ASOA201705043133), May 4, 2017: DOOR SILL. CORRODED. SERVICE DOOR AFT SILL CORRODED. SERVICE DOOR AFT SILL REPAIRED AS PER SRM 53-21-10 ITEM 5 FIG 204 SHEET 3. HFEC PERFORMED WITH NO FAULT FOUND.
- [SDR ASOA201705023128](https://openairdocs.org/sdr/ASOA201705023128), May 2, 2017: FLOORBEAM. CORRODED. CENTER FUSELAGE MIDDLE FLOORBEAM CORRODED AROUND ANCHOR NUT HOLES. FLOORBEAM REPLACED IAW SRM 51-40-02.
- [SDR ASOA201705023127](https://openairdocs.org/sdr/ASOA201705023127), May 2, 2017: CHANNEL. CRACKED. RIGHT WEB CRACKED ON FORWARD PRESSURE BULKHEAD IN NOSE WHEELWELL. CHANNEL REPLACED IAW SRM 51-40-02.
- [SDR ASOA201704203096](https://openairdocs.org/sdr/ASOA201704203096), Apr 20, 2017: CROSSBEAM. CRACKED. NLG UPLOCK AFT CROSSBEAM CRACKED. THE UPLOCK CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.
- [SDR ASOA201704203095](https://openairdocs.org/sdr/ASOA201704203095), Apr 20, 2017: CROSSBEAM. CRACKED. NLG UPLOCK FORWARD CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.
- [SDR ASOA201612223088](https://openairdocs.org/sdr/ASOA201612223088), Dec 22, 2016: BATTERY PACK. INOPERATIVE. DURING ROUTINE MAINTENANCE THE LEFT AND RIGHT OVERWING AFT EMERENGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY POWE
- [SDR ASOA20150305007](https://openairdocs.org/sdr/ASOA20150305007), Mar 5, 2015: RIB. CRACKED. ACFT IS IN C-CHECK WHEN INSPECTION FOUND A CRACK ON THE LT WING AT RIB NR 5 IN AREA FWD OF PREVIOUS SB MOD. CRACK RUNS FROM LOWER FLANGE OTBD THRU THE HYLOCK HO
- [SDR ASOA20150305006](https://openairdocs.org/sdr/ASOA20150305006), Mar 5, 2015: SKIN. GOUGED. ACFT IS IN A C-CHECK STATUS WHEN INSPECTION FOUND TOOLING MARKS ON THE LT WING ZONE 532 UPPER SKIN, THAT SHOWED A GROOVE CUT INTO THE SKIN. MAINTENANCE INSTALLE
- [SDR ASOA20140124022](https://openairdocs.org/sdr/ASOA20140124022), Jan 24, 2014: ENGINE. SMOKE. STRONG SMELL AND A SMOKE HAZE WAS PRESENT IN CABIN WHEN PACK 1 WAS SELECTED. MAINTENANCE R & R THE NR 1 ENGINE IAW MM.
- [SDR ASOA20130812062](https://openairdocs.org/sdr/ASOA20130812062), Aug 12, 2013: VALVE. LEAKING. THE CREW REPORTED A SUSPECTED FUEL LEAK IN OTBD LT WING DURING FLIGHT. MX INSPECTED AND REPLACED A LT WING FUEL FLAP VALVE. OPS CHECKS WERE GOOD .
- [SDR ASOA20130525052](https://openairdocs.org/sdr/ASOA20130525052), May 25, 2013: CONTROL UNIT. FAULTY. CREW REPORTED OTBD BRAKE INOPERATIVE. MX R & R THE BRAKE CONTROL UNIT WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130423152](https://openairdocs.org/sdr/ASOA20130423152), May 11, 2013: DOOR FRAME. CORRODED. DURING A-CHECK, PAX DOOR CUTOUT WAS FOUND CORRODED AT FRAME 18 BETWEEN STRINGERS 15-16L. MX REMOVED THE CORRODED SECTION AND PERFORMED A SPLICE REPAIR IAW EC531
- [SDR V0XR201303100178](https://openairdocs.org/sdr/V0XR201303100178), Mar 7, 2013: FLOORBEAM. DAMAGED. FLOORBEAM AT BS 5125 IS DAMAGED. R & R FLOORBEAM IAW SRM 51-40-02, CPM 51-04-00, 51-21-04, 51-21-05, AND 51-21-06.
- [SDR V0XR201303100177](https://openairdocs.org/sdr/V0XR201303100177), Mar 7, 2013: FLOORBEAM. DAMAGED. FLOORBEAM AT BS 5125 IS DAMAGED. R & R FLOORBEAM IAW SRM 51-40-02, CPM 51-04-00, 51-21-04,51-21-05, AND 51-21-06.
- [SDR V0XR201303100176](https://openairdocs.org/sdr/V0XR201303100176), Mar 7, 2013: FLOORBEAM. DAMAGED. FLOORBEAM AT BS 5125 IS DAMAGED. R & R FLOORBEAM IAW SRM 51-40-02,CPM 51-04-00, 51-21-04,51-21-05, AND 51-21-06.
- [SDR V0XR20130310J0175](https://openairdocs.org/sdr/V0XR20130310J0175), Mar 7, 2013: FAIRING. LOOSE. LOOSE FASTENERS AT FRAME BETWEEN 59/60 BETWEEN STR 21L AND 21R. INSTALLED DOUBLERS IAW EC5320-01761 AND INSTALLED RT AND LT FAIRINGS IAW SRM 51-40-02.
- [SDR V0XR201303100174](https://openairdocs.org/sdr/V0XR201303100174), Mar 7, 2013: DOOR FRAME. CORRODED. SURFACE UNDER LOWER AFT MAIN DOOR GUIDE AT FRAME 18 BS 5417 CORRODED. BLENDED CORRODED AREA , FOUND WITHIN LIMITS AT FRAME 18 STA. 5417 IAW EC5310-01684 (TEMPOR
- [SDR V0XR201303100173](https://openairdocs.org/sdr/V0XR201303100173), Mar 7, 2013: FLOORBEAM. CORRODED. PAX FLOORBEAM CORRODED AT FS 693.80 R & R PAX FLOORBEAM IAW SRM 51-40-02 AND CPM 51-20-04.
- [SDR V0XR201303100172](https://openairdocs.org/sdr/V0XR201303100172), Mar 7, 2013: FLOORBEAM. CORRODED. PAX FLOORBEAM CORRODED AT FS 693.80. R & R PAX FLOORBEAM IAW SRM 51-40-02 AND CPM 51-20-04.
- [SDR V0XR201303100171](https://openairdocs.org/sdr/V0XR201303100171), Mar 7, 2013: FLOORBEAM. CORRODED. PAX FLOORBEAM CORRODED AT FS 693.80. R & R PAX FLOORBEAM IAW SRM 51-40-02 AND CPM 51-20-04.
- [SDR V0XR201303100170](https://openairdocs.org/sdr/V0XR201303100170), Mar 7, 2013: SKIN. SCRATCHED. MULTIPLE SCRATCHES (3) FRAME 59 STR.17R AND FRAME 78 STR. 18R. PERFORMED REPAIR ON SCRATCH AT FRAME 59 STR 17R IAW EC 5330-02788.TWO OTHER SCRATCHES AT FRAME 22
- [SDR ASOA20121017093R](https://openairdocs.org/sdr/ASOA20121017093R), Oct 17, 2012: BOLT. UNSECURE. CREW REPORTED MAIN CABIN DOOR LEVER PRODUCES LOUD METAL POP SOUND WHEN OPENING AND FEELS UNUSUALLY HARD TO OPEN. MX INSPECTED AND FOUND HARDWARE LOOSE, RESECURE
- [SDR C2XA11CL228](https://openairdocs.org/sdr/C2XA11CL228), Oct 11, 2011: CONNECTOR. LOOSE. ORD FLT 5983 THE CREW REPORTED A AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERF
- [SDR C2XA11CL212](https://openairdocs.org/sdr/C2XA11CL212), Sep 20, 2011: WIRE HARNESS. CHAFED. THE CREW REPORTED AN ENGINE NR 2 FIRE DETECT FAIL MESSAGE ONLY DURING DESCENT, LOW PITCH ATTITUDE AND THRUST LEVER AT IDLE. MAINTENANCE INSPECTED AND REPLACED N
- [SDR C2XA11IA169](https://openairdocs.org/sdr/C2XA11IA169), Aug 2, 2011: UNKNOWN. ODOR. IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND GROUND RAN THE ENGINES ALL WITH NO 
- [SDR C2XA11RI048](https://openairdocs.org/sdr/C2XA11RI048), Mar 24, 2011: UNKNOWN. SMOKE. FLIGHT 2540 - EWR - FLIGHT CREW REPORTED SMOKE IN CABIN AND PERFORMED AIR RETURN UNEVENTFULLY. EWR MX PERFORMED ENGINE RUNUP (1 & 2) AT HIGH POWER WITH BLEED SY
- [SDR C2XA11SHO54](https://openairdocs.org/sdr/C2XA11SHO54), Mar 5, 2011: SKIN. CRACKED. SHV - DURING C-CHECK CRACK AROUND RIVET FRAME 75 STRINGER 2L-3L (VERIFIED WITH EDDY CURRENT). MAINTENANCE PERFORMED REPAIR OF FUSELAGE SKIN AT FRAME 75 STRINGER
- [SDR C2XA11RI008](https://openairdocs.org/sdr/C2XA11RI008), Jan 21, 2011: UNKNOWN. SMOKE. FLIGHT 2513 - MHT - FLIGHT CREW REPORTED LAV FIRE WARNING ON CLIMB - SMOKE IN THE LAV - CREW PERFORMED AIR RETURN AND LANDED SAFELY - NO EMERGENCY DECLARED. CON
- [SDR C2XA10IA347](https://openairdocs.org/sdr/C2XA10IA347), Dec 27, 2010: SKIN. CRACKED. DURING MAINTENANCE INSPECTION THE LEFT WING SKIN WAS FOUND TO BE CRACKED AT THE INBOARD SPOILER CENTER HINGE POINT CUTOUT. MAINTENANCE STOP DRILLED THE CRACK, A
- [SDR C2XA09CL157](https://openairdocs.org/sdr/C2XA09CL157), Dec 11, 2009: CARBON SEAL. MALFUNCTIONED. CLE FLT 2542 THE CREW REPORTED SMOKE IN THE CABIN AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REP
- [SDR C2XA09IA144](https://openairdocs.org/sdr/C2XA09IA144), May 28, 2009: DRAIN. DAMAGED. IAH - FLIGHT 2627 DURING CLIMB THE CREW REPORTED, LOST IAS INDICATIONS ON BOTH SIDES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE
- [SDR C2XA09IA143](https://openairdocs.org/sdr/C2XA09IA143), May 28, 2009: AHRS. MALFUNCTIONED. IAH - FLIGHT 2627 - DURING CLIMB THE CREW REPORTED THAT BOTH THE PILOT AND COPILOT ATT AND HDG FAILED. THE AIRCRAFT RETURNED TO IAH WHERE THE AIRCRAFT LANDED WI

All 81: https://openairdocs.org/aircraft/N16987/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/N16987/stcs.md

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/aircraft.md
- The Allison AE-3007A engine: https://openairdocs.org/engine/allison-ae-3007a.md

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