# N13978: 1999 Embraer EMB-145LR

- Status: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212, 55 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: 145180
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 6, 1999
- Certificate issued: August 18, 2022
- Expires: August 31, 2029
- Mode S code: A0A00E
- 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=13978
- Page: https://openairdocs.org/aircraft/N13978

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): 102 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 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 2006-20-08](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 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 113: https://openairdocs.org/aircraft/N13978/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 N13978.

## 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 20001007038359I](https://openairdocs.org/incident/20001007038359I), Oct 7, 2000: Emb EMB145LR (N13978), Washington, DC. (-23) BTA3899 southwest bound at FL350 reported moderate turbulence. Shortly thereafter R04 observed BTA3899'S mode c altitude at FL347 and asked the pilot to…

## Service difficulty reports (135, 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 ASOA20200205003](https://openairdocs.org/sdr/ASOA20200205003), Feb 1, 2020: BULB. FAILED. PILOT REPORTED ROW 18 EMERGENCY LIGHT INOP. MX RELAMPED EMERGENCY LIGHT IAW EMB145 AMM 33-50-08 WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERV
- [SDR ASOA2019062094032](https://openairdocs.org/sdr/ASOA2019062094032), Jun 19, 2019: ACM. FAILED. FLIGHT 4390 THE CREW REPORTED THAT A BANG WAS HEARD BY A PASSENGER NEAR ROW 8-9 AND THE CABIN FILLED WITH A FOG TYPE OF SMOKE THAT NEVER REACHED THE COCKPIT. TH
- [SDR ASOA201810187172](https://openairdocs.org/sdr/ASOA201810187172), Oct 17, 2018: STRINGER. DENTED. BETWEEN FRAME 23 AND 24 STRINGER 19R AND 20R DENTED. REMOVED AND REPLACED A SECTION OF STRINGER 19R AT FRAME 23 TO 25. AIRCRAFT STILL IN C CHECK.
- [SDR ASOA201808277156](https://openairdocs.org/sdr/ASOA201808277156), Aug 27, 2018: BATTERY PACK. INOPERATIVE. FOUND THE FLOOR LIGHTS AT ROWS 7 THRU 18, AND ALL EXIT SIGNS AT ROW 18 WERE OUT. MAINTENANCE R & R THE EMERGENCY BATTERY NR 3 IAW 33-50-04. R & R THE NR 5 INVER
- [SDR ASOA201808257155](https://openairdocs.org/sdr/ASOA201808257155), Aug 25, 2018: BATTERY. DISCHARGED. A/C WAS IN FOR AN A-CHECK WHEN INSPECTION FOUND THE EXIT ROW EMERGENCY LIGHT PROXIMITY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE #3 LIGHT BATTERY 
- [SDR ASOA2018073175169](https://openairdocs.org/sdr/ASOA2018073175169), Jul 27, 2018: BATTERY PACK. DISCHARGED. DURING MX INSPECTION THE FLOOR PROXIMITY EMERGENCY EXIT LIGHT AT SEAT 8A THROUGH 11A WAS INOP. MX REMOVED AND REPLACED THE NR 3 BATTERY PACK WITH OPERATIONAL CH
- [SDR ASOA2018062541033](https://openairdocs.org/sdr/ASOA2018062541033), Jun 15, 2018: BATTERY PACK. DISCHARGED. DURING MAINTENANCE INSPECTION, AN EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 3 EMERGENCY LIGHT BATTERY PACK, OPERA
- [SDR ASOA2018060615147](https://openairdocs.org/sdr/ASOA2018060615147), Jun 1, 2018: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS OVER THE DOORS WOULD NOT LIGHT UP. MX REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY AND OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RET
- [SDR ASOA2018053055140](https://openairdocs.org/sdr/ASOA2018053055140), May 25, 2018: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT WAS REPORTED INOPERATIVE. MX REMOVED AND REPLACED THE BATTEYR PACK, OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201711305242](https://openairdocs.org/sdr/ASOA201711305242), Nov 30, 2017: BATTERY PACK. INOPERATIVE. PILOT REPORTED 3RD & 4TH EMERGENCY LIGHTS IN CABIN CEILING ARE INOP. MX REMOVED AND REPLACED #3 EMERGENCY LIGHT BATTERY ASSY RELAMPED #3 & #4 ZONAL LAMPS WITH O
- [SDR ASOA201707015093](https://openairdocs.org/sdr/ASOA201707015093), Jul 1, 2017: SIGN. INOPERATIVE. PILOT REPORTED EMERGENCY ROW WINDOW LIGHT 18D INOPERATIVE. MX REMOVED AND REPLACED THE ROW SIGN AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201610180605](https://openairdocs.org/sdr/ASOA201610180605), Oct 18, 2016: BALLAST. SHORTED. PILOT REPORTED THE LAVATORY CIRCUIT BREAKER TRIPPED FOLLOWED BY ELECTRICAL ODOR. REMOVED AND REPLACED THE LAVATORY LIGHT BALLAST AND OPS CHECKED GOOD. APPROVED 
- [SDR ASOA20160926070](https://openairdocs.org/sdr/ASOA20160926070), Sep 26, 2016: MOUNT. CRACKED. DURING A C-CHECK. LT FWD LOWER ENGINE MOUNT CRACKED. REMOVED AND REPLACED ENGINE MOUNT IAW EC5450-01211. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160920067](https://openairdocs.org/sdr/ASOA20160920067), Sep 20, 2016: TRUNNION. CRACKED. DURING A C-CHECK, LT MLG AFT TRUNNION CRACKED. REMOVED AND REPLACED THE TRUNNION IAW EC5750-01766. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160907061](https://openairdocs.org/sdr/ASOA20160907061), Sep 7, 2016: BEAM. CORRODED. DURING A C-CHECK, CARGO DOOR CUTOUT LOWER BEAM WAS FOUND CORRODED. REMOVED AND REPLACED THE BEAM IAW SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160907060](https://openairdocs.org/sdr/ASOA20160907060), Sep 7, 2016: SKIN. CRACKED. DURING A C-CHECK. FOUND THE FUSELAGE SKIN CRACKED AT FRAME 75 STRINGER 2R. REPAIRED THE SKIN IAW EC5330-03120. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160907059](https://openairdocs.org/sdr/ASOA20160907059), Sep 7, 2016: SKIN. CRACKED. DURING A C-CHECK. THE FUSELAGE SKIN WAS FOUND CRACKED AT FRAME 75 STRINGER 2L. REPAIRED THE SKIN IAW EC5330-03119. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160602025](https://openairdocs.org/sdr/ASOA20160602025), Jun 2, 2016: CONTROL MODULE. SHORTED. CREW REPORTED BURNING ODOR IN CABIN. MAINTENANCE PERFORMED GVI OF CABIN AND FOUND ODOR COMING FROM SEAT 1A OVERHEAD AREA. R & R LIGHT CONTROL MODULE UNIT WITH O
- [SDR ASOA20150510045](https://openairdocs.org/sdr/ASOA20150510045), May 10, 2015: ACM. INOPERATIVE. THE CREW REPORTED THAT PACK 2 OVERLOADED MULTIPLE TIMES IN FLIGHT, THE PACK WAS DESELECTED IAW THE QRH AND THE COCKPIT AND CABIN FILLED WITH SMOKE AFTER 2 MINUT
- [SDR ASOA20150128005](https://openairdocs.org/sdr/ASOA20150128005), Jan 28, 2015: TRANSDUCER. FAULTY. PILOT REPORTED AN INTERMITTENT LOSS OF BRAKES ON LANDING WITH BRAKES DEGRADED EICAS MESSAGE. MX R & R NR 3 WHEEL SPEED TRANSDUCER WITH OPS CHECK GOOD. AC WAS AP
- [SDR ASOA20140805247](https://openairdocs.org/sdr/ASOA20140805247), Aug 5, 2014: SEAT TRACK. CORRODED. DURING C-CHECK AFTER REMOVAL OF NR 3 RT WALL SEAT TRACK FOUND SUPPORT CORRODED BETWEEN FRAMES 42-49. MAINTENANCE REMOVED CORROSION ON RT WALL SEAT TRACK FOUND S
- [SDR ASOA20140805246](https://openairdocs.org/sdr/ASOA20140805246), Aug 5, 2014: SEAT TRACK. CORRODED. DURING C-CHECK, MULTIPLE AREAS OF CORROSION IN LT SIDEWALL SEAT TRACK FRAMES 41-46. MAINTENANCE REMOVED CORROSION ON LT SIDEWALL SEAT TRACK AND IS OUT OF LIMITS
- [SDR ASOA20140805245](https://openairdocs.org/sdr/ASOA20140805245), Aug 5, 2014: DOOR FRAME. CORRODED. DURING C-CHECK, CORROSION FOUND AROUND AFT TWO NUTPLATES ON INSIDE AND OUTSIDE OF PAX DOOR BOTTOM FRAME. MAINTENANCE R & R PAX DOOR BOTTOM AFT FRAME WITH NEW FR
- [SDR ASOA20140805244](https://openairdocs.org/sdr/ASOA20140805244), Aug 5, 2014: SHEAR TIE. CORRODED. DURING C-CHECK CARGO DOOR CUTOUT STRUCTURE FWD FRAME LOWER CORNER CORRODED. MAINTENANCE R & R CORRODED SHEAR TIE AT CARGO DOOR FWD FRAME IAW SRM 51-40-02. THE A
- [SDR ASOA20140805243](https://openairdocs.org/sdr/ASOA20140805243), Aug 5, 2014: SUPPORT BRACKET. CRACKED. DURING C-CHECK, FOUND A CRACK IN UPPER AFT CORNER OF SUPPORT BRACKET FOR INTERNAL HANDLE ON PAX DOOR. MAINTENANCE REMOVED CRACKED PAX DOOR HANDLE SUPPORT BRACKE
- [SDR ASOA20140803101](https://openairdocs.org/sdr/ASOA20140803101), Aug 3, 2014: LIGHT. OVERHEATED. THE F/A REPORTED A BURNING ODOR IN THE CABIN ASSOCIATED WITH THE F/O'S SIDE FLOOR AND WALL LIGHTING FLICKERING. MAINTENANCE INSPECTED THE ACFT AND R & R THE AFF
- [SDR ASOA20140728242](https://openairdocs.org/sdr/ASOA20140728242), Jul 28, 2014: SUPPORT. CORRODED. DURING C-CHECK, FOUND SEAT TRACK SUPPORT CORRODED BETWEEN FRAMES 36-41. REMOVED CORROSION AND FOUND WITHIN LIMITS SRM 53-00-11. RESTORED SURFACE PROTECTION IAW 
- [SDR ASOA20140728241](https://openairdocs.org/sdr/ASOA20140728241), Jul 28, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, LT FLOOR SUPPORT BETWEEN FRAMES 18 AND 23 CHAFED AND CORRODED. MAINTENANCE REMOVED CORROSION IAW SRM 53-21-10. FOUND OUT OF LIMITS IAW SRM 53-21
- [SDR ASOA20140728240](https://openairdocs.org/sdr/ASOA20140728240), Jul 28, 2014: SUPPORT. CORRODED. DURING C-CHECK, MULTIPLE AREAS OF CORROSION ON LT SIDEWALL SEAT TRACK SUPPORT FROM FRAME 41-36. MAINTENANCE REMOVED CORROSION AND WAS FOUND OUT OF LIMITS SRM 53
- [SDR ASOA20140728239](https://openairdocs.org/sdr/ASOA20140728239), Jul 28, 2014: SUPPORT. CORRODED. DURING C-CHECK, FOUND CORROSION ON LT WALL SEAT TRACK SUPPORT BETWEEN FRAMES 48 AND 52. MAINTENANCE REMOVED CORROSION AND FOUND WITHIN LIMITS SRM 53-00-11. REST
- [SDR ASOA20140728238](https://openairdocs.org/sdr/ASOA20140728238), Jul 28, 2014: SUPPORT. CORRODED. DURING C-CHECK, FOUND CORROSION ON LT WALL SEAT TRACK SUPPORT BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED CORROSION ON LT WALL SEAT TRACK SUPPORT BETWEEN FRAM
- [SDR ASOA20140728237](https://openairdocs.org/sdr/ASOA20140728237), Jul 28, 2014: ANGLE. CRACKED. DURING C-CHECK AFT FUSELAGE INSIDE ACCESS 312AR AT FRAME 81, STRINGER 10, RT END CLIP IS CRACKED AT APU FIREWALL. MAINTENANCE R & R FRAME 81, STRINGER 10, RT EN
- [SDR ASOA20140728236](https://openairdocs.org/sdr/ASOA20140728236), Jul 28, 2014: ANGLE. CRACKED. DURING C-CHECK, AFT FUSELAGE INSIDE ACCESS 312AR AT FRAME 81, STRINGER 11, RT END ANGLE IS CRACKED AT APU FIREWALL. MAINTENANCE R & R END ANGLE IAW SRM 51-40-02
- [SDR ASOA20140725235](https://openairdocs.org/sdr/ASOA20140725235), Jul 25, 2014: FRAME. GOUGED. DURING C-CHECK THE FRAME CHANNEL AT FRAME 61 BETWEEN STRINGERS 16L-17L WAS FOUND TO BE GOUGED. MAINTENANCE BLENDED OUT THE DAMAGE AND PERFORMED A DOUBLER REPAIR
- [SDR ASOA20140724228](https://openairdocs.org/sdr/ASOA20140724228), Jul 24, 2014: DOOR FRAME. CORRODED. DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVI
- [SDR ASOA20140724227](https://openairdocs.org/sdr/ASOA20140724227), Jul 24, 2014: DOOR FRAME. CORRODED. DURING C-CHECK, THE CARGO DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE FRAME IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140724226V](https://openairdocs.org/sdr/ASOA20140724226V), Jul 24, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAMES 59-61. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01959. T
- [SDR ASOA20140503050](https://openairdocs.org/sdr/ASOA20140503050), May 3, 2014: TRANSDUCER. FAULTY. PILOT REPORTED A BRAKE DEGRADED MESSAGE ON EICAS WHEN GEAR WAS LOWERED AND BRAKES FELT LESS EFFECTIVE AND UNEVEN ON LANDING. MAINTENANCE R & R THE NR 4 BRAKE PR
- [SDR ASOA20131028122](https://openairdocs.org/sdr/ASOA20131028122), Oct 28, 2013: UNKNOWN. ODOR. PILOT REPORTED A STRONG FUEL ODOR DURING TAKEOFF, WHILE APU POWERED THE PACKS. MAINTENANCE PERFORMED OPS CHECK, CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SE
- [SDR ASOA20120821063](https://openairdocs.org/sdr/ASOA20120821063), Aug 21, 2012: ENGINE. FAILED. REJECTED TAKEOFF DUE TO ENGINE NR 1 AUTO SHUTDOWN ON TAKEOFF ROLL. MX DETERMINED LOW N1 AND E1 EXCEEDANCE AND R & R NR 1 ENGINE IAW TASK CARD 6271001 WITH OPS A
- [SDR ASOA20111220023](https://openairdocs.org/sdr/ASOA20111220023), Dec 20, 2011: PROXIMITY SWITCH. FAULTY. THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON ROTATION. MX INSPECTED AND PERFORMED FUNCTIONAL CHECKS OF THE PROXIMITY SWITCHES. REPLACED THE NOSE 
- [SDR ASOA20111209011](https://openairdocs.org/sdr/ASOA20111209011), Dec 9, 2011: CONTROL LEVER. FAULTY. FLT 4394, THE CREW REPORTED AFTER TAKEOFF THEY RECEIVED AN AIR/ROUND FAIL MESSAGE AND WAS UNABLE TO RETRACT THE LANDING GEAR. THE ACFT RETURNED TO DEPARTURE AND
- [SDR C2XA11CL243](https://openairdocs.org/sdr/C2XA11CL243), Nov 8, 2011: PROXIMITY SWITCH. FAULTY. CLE FLT 5815 THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE AND WAS UNABLE TO RAISE GEAR ON DEPARTURE. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT
- [SDR C2XA11TY155](https://openairdocs.org/sdr/C2XA11TY155), Oct 8, 2011: ELECTRONIC UNIT. MALFUNCTIONED. LG/AIR GROUND FAIL, HANDLE UNMOVABLE. REMOVED AND REPLACED LGEU IAW EMB 145 AMM 32-32-01. IPC REF 32-32-01 ITEM 1D. OPS CHECK GOOD AIRCRAFT RELEASE AND RETURNED
- [SDR C2XA11CL222](https://openairdocs.org/sdr/C2XA11CL222), Oct 2, 2011: PROXIMITY SWITCH. FAULTY. ORD FLT 6062 ON TAKEOFF CREW GOT AN AIR GROUND WARNING, AND THE GEAR WOULD NOT COME UP. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND R
- [SDR C2XA11IA207](https://openairdocs.org/sdr/C2XA11IA207), Sep 11, 2011: PROXIMITY SENSOR. FAULTY. MCI - FLIGHT 2437, THE CREW REPORTED A LANDING GEAR AIR GROUND FAILURE MESSAGE ON EICAS WITH THE GEAR IN THE DOWN POSITION. THE AIRCRAFT RETURNED TO MCI WHERE I
- [SDR C2XA11CL187](https://openairdocs.org/sdr/C2XA11CL187), Aug 15, 2011: CONNECTOR. LOOSE. ORD FLT 5872 THE CREW REPORTED JUST AFTER TAKEOFF RECEIVED A AIR/GROUND FAIL MESSAGE AND THE GEAR LEVER WOULD NOT GO UP. MAINTENANCE INSPECTED AND FOUND A LOOSE
- [SDR C2XA11IA155](https://openairdocs.org/sdr/C2XA11IA155), Jul 16, 2011: PROXIMITY SENSOR. OUT OF ADJUST. IAH - FLIGHT 2873, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL EICAS MESSAGE AFTER TAKEOFF, AND THE GEAR HANDLE WOULD NOT MOVE. THE AIRCRAFT RETURNED TO IAH 
- [SDR C2XA11IA120](https://openairdocs.org/sdr/C2XA11IA120), Jun 15, 2011: ADC. INOPERATIVE. MEM - FLIGHT 2725, THE CREW REPORTED AN ADC MISCOMPARE/LT-ENG, ADC/DATA SYS MESSAGES. THE AIRCRAFT DIVERTED TO MEM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE
- [SDR C2XA11RI073](https://openairdocs.org/sdr/C2XA11RI073), May 11, 2011: MONITOR. DEFECTIVE. FLIGHT 6135 - RIC - FLIGHT CREW REPORTED E1 ABNORMAL VIBRATION, LP NR 1 LP INDICATION MAXED - NO VIBRATION FELT. CREW SHUT DOWN THE ENGINE AND PROCEED WITH EMER

All 135: https://openairdocs.org/aircraft/N13978/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/N13978/stcs.md

## Earlier aircraft with N13978

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N13978 before.

- [Cancelled 1974-01-30](https://openairdocs.org/deregistered/N13978-1974-01-30): Piper PA-23-250, S/N 27-4596. Owner: [Jim Hankins Air Service Inc](https://openairdocs.org/faa-owner/JIM%20HANKINS%20AIR%20SERVICE%20INC), [Jackson, MS](https://openairdocs.org/faa-place/MS/Jackson)

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/aircraft.md
- The Allison AE3007C series engine: https://openairdocs.org/engine/allison-ae3007c-series.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.