# N13992: 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: 145284
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 8, 2000
- Certificate issued: August 18, 2022
- Expires: August 31, 2029
- Mode S code: A0A04E
- 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=13992
- Page: https://openairdocs.org/aircraft/N13992

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/N13992/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 N13992.

## FAA accident and incident reports

None matched to N13992.

## Service difficulty reports (84, 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 ASOA201908197097](https://openairdocs.org/sdr/ASOA201908197097), Aug 19, 2019: SHEAR TIE. CORRODED. CORROSION ON SHEAR CLIP AT FRAME 61 STRINGER 20R-18R. REMOVED AND REPLACED CORRODED SHEAR CLIP IAW SRM 51-40-02.
- [SDR ASOA201803205084](https://openairdocs.org/sdr/ASOA201803205084), Mar 20, 2018: BULB. INOPERATIVE. DURING MX INSPECTION, THE LT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MX R & R THE BULB, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201706273216](https://openairdocs.org/sdr/ASOA201706273216), Jun 27, 2017: SEAT TRACK. CORRODED. CABIN SEAT TRACK CORRODED RIGHT OTBD NR 3. REPLACED THE SEAT TRACK IAW 53-01-06-400
- [SDR ASOA201706273215](https://openairdocs.org/sdr/ASOA201706273215), Jun 27, 2017: SEAT TRACK. CORRODED. CABIN NR 6 SEAT TRACK CORRODED. REPLACED IAW SRM 53-01-06-400.
- [SDR ASOA201706263211](https://openairdocs.org/sdr/ASOA201706263211), Jun 26, 2017: SKIN. CRACKED. LEFT FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 2L. CRACK FOUND DURING NDT INSPECTION. LEFT FUSELAGE SKIN REPAIRED WITH DOUBLER (11" X 9") IAW SRM 53-31-01, IT
- [SDR ASOA201706263210](https://openairdocs.org/sdr/ASOA201706263210), Jun 26, 2017: TRUNNION. CRACKED. LEFT MAIN LANDING GEAR AFT UPPER TRUNNION CRACKED. THE TRUNNION WAS REPLACED IAW T1-145-14-018 REV E, AND ETD-2017-145-053707.
- [SDR ASOA201706263209](https://openairdocs.org/sdr/ASOA201706263209), Jun 26, 2017: CHANNEL. CORRODED. SERVICE DOOR CHANNEL CORRODED. SERVICE DOOR CHANNEL REPLACED IAW SRM 51-40-02
- [SDR ASOA201706223208](https://openairdocs.org/sdr/ASOA201706223208), Jun 22, 2017: BEAM. CORRODED. CENTER FUSELAGE 4 FLOOR STRUCTURE CENTER BEAM CORRODED AROUND ANCHOR NUT. CENTER BEAM REPAIRED AROUND ANCHOR NUT WITH DOUBLER IAW SRM 53-24-10 ITEM 3 FIG 202.
- [SDR ASOA201706223207](https://openairdocs.org/sdr/ASOA201706223207), Jun 22, 2017: GUSSET. CORRODED. CENTER FUSELAGE FLOOR STRUCTURE LEFT GUSSET UNDER CARBON BEAM CORRODED. LEFT GUSSET BETWEEN FRAME 59 AND 61 REPLACED IAW SRM 51-40-02.
- [SDR ASOA201706223206](https://openairdocs.org/sdr/ASOA201706223206), Jun 22, 2017: GUSSET. CORRODED. CENTER FUSELAGE 4 FLOOR STRUCTURE MID GUSSET CORRODED. MID GUSSET WAS REPLACED IAW SRM 51-40-02.
- [SDR ASOA201706223205](https://openairdocs.org/sdr/ASOA201706223205), Jun 22, 2017: WINDOW FRAME. CRACKED. FRAME CRACKED TOP FORWARD CO-PILOT SLIDING WINDOW. SLIDING WINDOW UPPER LATERAL FRAME WAS REPLACED AS PER SRM 51-40-02.
- [SDR ASOA201706223204](https://openairdocs.org/sdr/ASOA201706223204), Jun 22, 2017: TRUNNION. CRACKED. RIGHT MAIN GEAR AFT UPPER TRUNNION CRACKED. THE TRUNNION WAS REPLACED IAW T1-145-14-018R/H, AND ETD 2017-145-67014-608.
- [SDR ASOA201704305070](https://openairdocs.org/sdr/ASOA201704305070), Apr 30, 2017: LAMP. INOPERATIVE. DURING MX INSPECTION, THE CABIN OVERHEAD LIGHT AT ROW 7 WAS INOPERATIVE. MX REPLACED THE LAMPS AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201704055035](https://openairdocs.org/sdr/ASOA201704055035), Apr 5, 2017: CRADLE. BURNED. CREW REPORTED A BURNING ODOR, FOLLOWED BY LOSS OF CA'S AIRSPEED INDICATOR, ALTIMETER, AND SPS. ADVANCED ON EICAS DURING FLIGHT. MX FOUND BURNING ODOR TO BE F/A'
- [SDR ASOA201610234078](https://openairdocs.org/sdr/ASOA201610234078), Oct 23, 2016: ACM. FROZEN. FLIGHT 3888 THE CREW REPORTED SMOKE IN THE CABIN IN CRUISE FLIGHT AT FL250. THE SMOKE DISSIPATED AFTER APPROXIMATELY 15 SECONDS. THE AIRCRAFT RETURNED TO IAH WH
- [SDR ASOA20160406015](https://openairdocs.org/sdr/ASOA20160406015), Apr 6, 2016: FMU. FAILED. PILOT REPORTED A NR 2 ENGINE OUT MESSAGE ENGINE UNCOMMANDED SHUTDOWN, DID NOT INDICATE ON GROUND OR IN FLIGHT. MAINTENANCE INSPECTED AND FOUND DEBRIS IN FUEL FI
- [SDR ASOA20150621031R](https://openairdocs.org/sdr/ASOA20150621031R), Jun 21, 2015: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE FLOOR EMERGENCY LIGHT STRIP AT SEATS 7 & 8A WAS FOUND INOPERATIVE. MAINTENANCE R & R THE LIGHT STRIP WITH OPS CHECK GOOD. AIR
- [SDR ASOA20150413094](https://openairdocs.org/sdr/ASOA20150413094), Apr 13, 2015: RIB. CRACKED. DURING C-CHECK, RIB 21 ON RT WING INSIDE PANEL 651CB IS CRACKED. MAINTENANCE REPAIRED RT WING RIB 21 IAW EC 5720-01201. THE ACFT WAS APPROVED FOR RETURN TO SERV
- [SDR ASOA20150409092](https://openairdocs.org/sdr/ASOA20150409092), Apr 9, 2015: SKIN. CORRODED. DURING C-CHECK, FUSELAGE SKIN CORRODED BETWEEN FRAME 57-58, STR 20R-19R. REPAIRED SKIN IAW EC5330-03001. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150409091](https://openairdocs.org/sdr/ASOA20150409091), Apr 9, 2015: DOOR SILL. CORRODED. DURING C-CHECK, SERVICE DOOR AFT SILL CORRODED. REPAIRED SERVICE DOOR SILL IAW SRM 53-21-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150409090](https://openairdocs.org/sdr/ASOA20150409090), Apr 9, 2015: SKIN. CRACKED. DURING C-CHECK, SKIN CRACKS AROUND RIVETS FRAME 75 STR 2R-3R. REPAIRED SKIN CRACKS IAW EC5330-02997. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150409089](https://openairdocs.org/sdr/ASOA20150409089), Apr 9, 2015: SKIN. CRACKED. DURING C-CHECK, SKIN CRACKS AROUND RIVETS FRAME 78, STR 3L-5L. REPAIRED SKIN CRACKS AROUND RIVETS IAW EC 5330-03000. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150409088](https://openairdocs.org/sdr/ASOA20150409088), Apr 9, 2015: FRAME. CRACKED. DURING C-CHECK, FRAME 25 CRACKED AT STR 15R-16R. REPAIRED FRAME 25 IAW SRM 53-00-04. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140626086](https://openairdocs.org/sdr/ASOA20140626086), Jun 26, 2014: SMOKE WARNING. FALSE ACTIVATION. DURING DESCENT THE CREW REPORTED A LAVATORY SMOKE WARNING ON EICAS WITH NO SIGN OF SMOKE IN LAVATORY. THE CREW DEACTIVATED TWO CIRCUIT BREAKERS IAW THE QRH AND 
- [SDR ASOA20130720076](https://openairdocs.org/sdr/ASOA20130720076), Jul 20, 2013: TRANSDUCER. FAULTY. CREW REPORTED THE RT BRAKES NOT WORKING ON LANDING, ACFT PULLED TO THE LEFT AND TOWER SAW SMOKE FROM THE RT MLG DURING LANDING. MX R & R NR 3 WHEEL SPEED TRANSD
- [SDR ASOA20130607318](https://openairdocs.org/sdr/ASOA20130607318), Jun 7, 2013: FLAP SYSTEM. OUT OF RIG. FLAP FAIL MESSAGE INFLIGHT. PERFORMED FLAP RIGGING. OPS CHECK GOOD, ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20130421134](https://openairdocs.org/sdr/ASOA20130421134), Apr 19, 2013: SHEAR TIE. CORRODED. DURING C-CHECK THE FRAME 65 SHEAR TIE AT THE CARGO DOOR CUTOUT WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW EC5320-01494
- [SDR ASOA20130421133](https://openairdocs.org/sdr/ASOA20130421133), Apr 19, 2013: FRAME. CORRODED. DURING C-CHECK, FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15L-16L. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01505. THE ACFT 
- [SDR ASOA20130421132V](https://openairdocs.org/sdr/ASOA20130421132V), Apr 19, 2013: BEAM. CORRODED. DURING C-CHECK, THE CARGO DOOR LOWER BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 65-68 AND STRINGERS 15L-16L. MX R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS 
- [SDR ASOA20130315016C](https://openairdocs.org/sdr/ASOA20130315016C), Mar 15, 2013: FAN. FAULTY. THE CREW REPORTED A ELECTRICAL BURNING ODOR IN THE CABIN. MX INSPECTED AND REPLACED THE NR 1 PACK RECIRCULATION FAN. OPS CHECKS WERE GOOD.
- [SDR ASOA20120813111](https://openairdocs.org/sdr/ASOA20120813111), Aug 13, 2012: INVERTER. INOPERATIVE. DURING MX INSPECTION, THE AISLE PATH LIGHTING FROM ROW 3 TO 7 WERE FOUND TO BE INOPERATIVE. MX R & R THE NR 3 EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFEC
- [SDR C2XA11CL133](https://openairdocs.org/sdr/C2XA11CL133), May 22, 2011: SMOKE DETECTOR. FAULTY. ORD FLT 5904 THE CREW REPORTED A LAV SMOKE INOPERATIVE MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11TY054](https://openairdocs.org/sdr/C2XA11TY054), May 1, 2011: DOOR FRAME. DAMAGED. SERVICE DOOR STRUCTURE FOR DOOR STOPS 3.9 AND 3.10 REQUIRE MOUNT HOLES TO BE REWORKED FOR SB145-53-0031. SERVICE DOOR FRAME STOP BACKUP STRUCTURE POSITION 3.9 A
- [SDR C2XA11TY032](https://openairdocs.org/sdr/C2XA11TY032), Mar 19, 2011: SMOKE DETECTOR. DEFECTIVE. THE FORWARD SMOKE DETECTOR IN CARGO HAS A STEADY LIGHT ON. REMOVED AND REPLACED DETECTOR IAW EMB 145 AMM 26-15-01. OPS CHECK GOOD.
- [SDR C2XA11TY026](https://openairdocs.org/sdr/C2XA11TY026), Mar 2, 2011: A/C PACK. OVERHEATED. DURING TAXI PACK 1 OVERHEAT RESULTED IN SMOKE IN THE CABIN. PLACED PACK 1 ON MEL.
- [SDR C2XA11CL066](https://openairdocs.org/sdr/C2XA11CL066), Mar 2, 2011: ACM. FAILED. BNA FLT 6097 THE CREW REPORTED PACK NR 1 OVERHEAT AND SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND PLACED NR 1 PACK ON MEL. 
- [SDR C2XA10CL166](https://openairdocs.org/sdr/C2XA10CL166), Nov 1, 2010: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE THE EMERGENCY AISLE PATH LIGHT STRIP AT SEAT 12A WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP AT SEAT 12A.OPERAT
- [SDR C2XA10IA218](https://openairdocs.org/sdr/C2XA10IA218), Aug 3, 2010: LIGHT. INOPERATIVE. IAH - FLIGHT 2044, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY LIGHT STRIP AT ROW 12A WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFE
- [SDR C2XA10CL065](https://openairdocs.org/sdr/C2XA10CL065), May 1, 2010: ENGINE. FAULTY. MHT-CLE FLT 2582 THE CREW REPORTED A PUNGENT ODOR FROM THE PACKS THROUGHOUT THE ENTIRE FLIGHT. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE 
- [SDR C2XA10RI043](https://openairdocs.org/sdr/C2XA10RI043), Mar 17, 2010: FADEC. DEFECTIVE. FLIGHT 2882 - FLIGHT CREW REPORTED PARTIAL LOSS OF POWER ON ENGINE 1, 2 TIMES IN FLIGHT. DURING CRUISE, N1 WENT DOWN TO 67 PERCENT, IGN A AND B CAME ON AND REST
- [SDR C2XA10RI042](https://openairdocs.org/sdr/C2XA10RI042), Mar 17, 2010: FADEC. DEFECTIVE. FLIGHT 2882 - FLIGHT CREW REPORTED PARTIAL LOSS OF POWER ON ENGINE 1, 2 TIMES IN FLIGHT. DURING CRUISE, N1 WENT DOWN TO 67 PERCENT, IGN A AND B CAME ON AND REST
- [SDR C2XA10IA098](https://openairdocs.org/sdr/C2XA10IA098), Mar 14, 2010: FADEC. MALFUNCTIONED. IAW - FLIGHT 2758, THE CREW REPORTED THAT ENGINE 1 SURGES IN FLIGHT. CRUISE THRUST N1 FLUCTUATES =/-15 PERCENT WITH AN ITT RISE AND FALL; N1 REQUEST CARAT ALSO 
- [SDR C2XA09CL162](https://openairdocs.org/sdr/C2XA09CL162), Dec 13, 2009: WIRE HARNESS. BURNED. SDF FLT 2343 THE CREW REPORTED UPON LANDING NOTICED ELECTRICAL/SMOKE SMELL COMING FROM OVERHEAD PANEL AT SEAT 1A. MAINTENANCE INSPECTED AND REPLACED THE SIDEWAL
- [SDR C2XA09CL125](https://openairdocs.org/sdr/C2XA09CL125), Sep 28, 2009: APU. MALFUNCTIONED. CLE FLT 2698 - THE CREW REPORTED A PLASTIC BURNING SMELL IN THE CABIN DURING CLIMB. MAINTENANCE INSPECTED AND REPLACED THE APU. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA09RI165](https://openairdocs.org/sdr/C2XA09RI165), Sep 19, 2009: UNKNOWN. ODOR. FLIGHT 2393 - EWR - FLIGHT CREW REPORTED STRONG ODOR WHEN PACKS ARE ON IN COCKPIT. EWR MX PERFORMED OPERATIONAL CHECK FOR PACK SYSTEM IAW EMB-145 AMM 21-51-00 A
- [SDR C2XA09SH173](https://openairdocs.org/sdr/C2XA09SH173), Jun 12, 2009: BEAM. CORRODED. SHV. DURING C-CK. CARGO DOOR LOWER CUTOUT BEAM HAS CORROSION. REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT BEAM IAW EMB 145 SRM 51-40-02. ACFT WAS APPROVED FOR 
- [SDR C2XA09SH172](https://openairdocs.org/sdr/C2XA09SH172), Jun 12, 2009: FLOOR SUPPORT. CORRODED. SHV. DURING C-CHECK. RT OMEGA BEAM HAS CORROSION AT FR 22. REPAIRED RT OMEGA BEAM AT FR 22 IAW IC2009-145/04543. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09CL043](https://openairdocs.org/sdr/C2XA09CL043), Apr 11, 2009: TURBINE WHEEL. CRACKED. DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASO
- [SDR C2XA09CL021](https://openairdocs.org/sdr/C2XA09CL021), Feb 23, 2009: INDICATOR. FAULTY. CLE FLIGHT 2341 - THE CREW REPORTED A ENGINE NR 1 FUEL IMPENDING BYPASS INDICATION ON CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTE
- [SDR C2XA09RI001](https://openairdocs.org/sdr/C2XA09RI001), Jan 2, 2009: BLEED VALVE. INOPERATIVE. BNA - FLIGHT 2573 - FLIGHT CREW REPORTED ENGINE NR 1 BLEED VALVE CLOSED IN FLIGHT AND THEY WERE UNABLE TO REOPEN. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEV

All 84: https://openairdocs.org/aircraft/N13992/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/N13992/stcs.md

## Earlier aircraft with N13992

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N13992 before.

- [Cancelled 1937-01-18](https://openairdocs.org/deregistered/N13992-1937-01-18): Spartan 7W, S/N 7W-1, built 1936. Owner: [Spartan Aircraft Co](https://openairdocs.org/faa-owner/SPARTAN%20AIRCRAFT%20CO), [Tulsa, OK](https://openairdocs.org/faa-place/OK/Tulsa)

## 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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