# N48901: 2001 Embraer EMB-145LR

- Status: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212, 55 seats)
- Engine: [Rolls-Royce AE-3007A1P](https://openairdocs.org/engine/rolls-royce-ae-3007a1p) (registry code 54571)
- 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: 145501
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 21, 2001
- Certificate issued: August 18, 2022
- Expires: August 31, 2029
- Mode S code: A60C7A
- 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=48901
- Page: https://openairdocs.org/aircraft/N48901

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 (Rolls-Royce AE-3007A1P)

- [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 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 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 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 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 2003-25-08](https://openairdocs.org/ad/2003-25-08): 1st and 2nd stage turbine spacers · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 3 more. Effective Jan 21, 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 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 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 2008-19-51](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 118: https://openairdocs.org/aircraft/N48901/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 N48901.

## 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 20030107000109I](https://openairdocs.org/incident/20030107000109I), Jan 7, 2003: Emb EMB145LR (N48901), Pittsburgh, PA. (-23) C2XA flight 2678 diverted and landed on runway 28L with the number 1 engine shut down. A review of aircraft log page 782637, dated 1/7/2003 revealed the…

## Service difficulty reports (72, 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 ASOA2020040984014](https://openairdocs.org/sdr/ASOA2020040984014), Apr 8, 2020: LIGHT. INTERMITTENT. IAH - FLIGHT 4229, DURING MX INSPECTION THE MAIN PAX DOOR EMERGENCY LIGHT WAS FOUND TO BE INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSE
- [SDR ASOA201907195087](https://openairdocs.org/sdr/ASOA201907195087), Jul 19, 2019: LIGHT. INOPERATIVE. DURING MX THE EMERGENCY LIGHT FLOOR PROXIMITY STRIP ROW 22A TO 24A WAS DISCOVERED INOP. MX PLACED ON MEL. ON 7/24/19 MX REMOVED AND REPLACED THE LIGHT STRIP WIT
- [SDR ASOA2019062433035](https://openairdocs.org/sdr/ASOA2019062433035), Jun 23, 2019: ACM. SEIZED. THE CREW REPORTED FUMES AND VAPOR/MINOR SMOKE IN CABIN IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE #2 AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE GOOD.
- [SDR ASOA201904017035](https://openairdocs.org/sdr/ASOA201904017035), Mar 29, 2019: FRAME. CRACKED. CRACKED FRAME RT SIDE ABOVE RT WINDSHIELD LATERAL POST. REMOVED CRACKED SECTION OF LATERAL BRACKET, INSTALLED NEW SECTION OF LATERAL BRACKET AND DOUBLER. AIRCRA
- [SDR ASOA201903247034](https://openairdocs.org/sdr/ASOA201903247034), Mar 24, 2019: SKIN. CORRODED. TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND FUSELAGE CORRODED UNDER THE RA ANTENNA BETWEEN FRAMES 69 AND 70 AND STR 21L AND 21R. MAINTENANCE PERFORMED A DOUBLER
- [SDR ASOA2018042655110](https://openairdocs.org/sdr/ASOA2018042655110), Apr 25, 2018: CONNECTOR. UNSECURE. DURING MX INSPECTION THE RIGHT SIDE OVERWING EMERGENCY EXIT LIGHT WAS DISCOVERED INOPERATIVE. MX RE-SEATED CANON PLUG AND PERFORMED OPERATIONAL CHECK WITH GOOD 
- [SDR ASOA201706105086](https://openairdocs.org/sdr/ASOA201706105086), Jun 10, 2017: INVERTER. INOPERATIVE. DURING MX INSPECTION, THE EMERGENCY LIGHTS FROM ROWS 3 TO 7 WAS FOUND INOPERATIVE. MX REMOVED AND REPLACED THE INVERTER NR 3. OPERATIONAL CHECKED GOOD. ACFT WAS
- [SDR ASOA201706105085](https://openairdocs.org/sdr/ASOA201706105085), Jun 10, 2017: BATTERY PACK. INOPERATIVE. DURING MX INSPECTION, THE MAIN CABIN DOOR, EXIT, OVERHEAD ROW 3, AND FWD LEFT WING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REMOVED AND REPLACED THE NR 1 EME
- [SDR ASOA201612121596](https://openairdocs.org/sdr/ASOA201612121596), Dec 12, 2016: SKIN. CRACKED. DURING C-CK FR 75 FUSELAGE SKIN IS CRACKED BTW STR 1R-2R. REPAIRED FR 75 SKIN AT STR 1-2R BY CUTTING DAMAGE AND INSTALLING A FILLER AND DOUBLER IAW SRM 53-31-01
- [SDR ASOA201612121586](https://openairdocs.org/sdr/ASOA201612121586), Dec 12, 2016: STRINGER. CRACKED. DURING C-CK STRINGER 2L IS CRACKED AT FR 75. REPAIRED STRINGER 2L IAW SRM 53-00-03 TABLE 202. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160323013V](https://openairdocs.org/sdr/ASOA20160323013V), Mar 21, 2016: POWER SUPPLY. INOPERATIVE. DURING ROUTINE MAINTENANCE THE FORWARD CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 1 EMERGENCY LIGHT POWER SUPPLY AND BATTERY 
- [SDR ASOA20160317018](https://openairdocs.org/sdr/ASOA20160317018), Mar 17, 2016: BATTERY. INOPERATIVE. DURING ROUTINE MAINTENANCE THE LT WING EXTERNAL FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK. OPS C
- [SDR ASOA20150326015](https://openairdocs.org/sdr/ASOA20150326015), Mar 26, 2015: SOLENOID VALVE. FAULTY. ON APPROACH AT 5000 FT PILOTED REPORTED THE NOSE GEAR DOORS OPENED AND REMAINED OPEN WITH THE GEAR LEVER IN THE UP POSITION. MAINTENANCE R & R THE NOSE GEAR DOO
- [SDR ASOA20150104002](https://openairdocs.org/sdr/ASOA20150104002), Jan 4, 2015: INVERTER. INOPERATIVE. DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FLOOR EMERGENCY LIGHT STRIPS WERE NOT ILLUMINATING DURING A TEST. MAINTENANCE R & R THE NR 6 EMERGENCY L
- [SDR ASOA20141017085](https://openairdocs.org/sdr/ASOA20141017085), Oct 17, 2014: BLEED VALVE. FAULTY. THE CREW REPORTED AFTER STARTING APU, RECEIVED A STRONG FUEL ODOR IN COCKPIT, WHICH DISSIPATED. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPS CHEC
- [SDR ASOA20140607064](https://openairdocs.org/sdr/ASOA20140607064), Jun 7, 2014: BATTERY PACK. INOPERATIVE. DURING MX INSPECTION THE NR 3 EMERGENCY LIGHT BATTERY WOULD NOT ILLUMINATE THE EMERGENCY LIGHTS. MX R & R THE NR 3 EMERGENCY LIGHT SYS BATTERY PACK, OPS CHECKED
- [SDR ASOA20140506053](https://openairdocs.org/sdr/ASOA20140506053), May 6, 2014: FLAPPER VALVE. BROKEN. PILOT REPORTED A SUSPECTED FUEL LEAK, ENGINE NR 2, FUEL PPH AT CRUISE SET SIMILAR, YET TANK NR 2 INDICATOR SHOWED TANK NR 2 FUEL USAGE WAS MUCH GREATER. AFTER I
- [SDR ASOA20130802088](https://openairdocs.org/sdr/ASOA20130802088), Aug 2, 2013: FLAPPER VALVE. LEAKING. CREW REPORTED FUEL LEAKING FROM THE RT WING AFTER TAKEOFF ALONG WITH FUEL IMBALANCE. CREW PERFORMED UNEVENFUL AIR RETURN. MX R & R THE RT WING FLAPPER VALVE WIT
- [SDR ASOA20130607085](https://openairdocs.org/sdr/ASOA20130607085), Jun 7, 2013: UNKNOWN. SMOKE. THE CREW REPORTED SMOKE IN THE CABIN, APPROX 2 MINUTES AFTER SELECTING ENGINE BLEEDS, WITH A SMELL BEING IMMEDIATELY NOTICEABLE. THE ACFT RETURNED TO DEPARTURE,
- [SDR ASOA20130315027R](https://openairdocs.org/sdr/ASOA20130315027R), Mar 15, 2013: BULB. INOPERATIVE. DURING MX INSPECTION THE CEILING GALLEY EMERGENCY LIGHT WAS FOUND TO BE DIM DURING OPERATION. MX R & R THE CEILING GALLEY EMERGENCY LIGHT BULB, OPS CHECK SUCCES
- [SDR ASOA20121126136V](https://openairdocs.org/sdr/ASOA20121126136V), Nov 26, 2012: SILL. CORRODED. DURING C-CHECK CARGO DOOR SILL CORRODED. MX R & R CARGO DOOR SILL IAW CPM 51-21-06 AND SRM 53-31-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121126135V](https://openairdocs.org/sdr/ASOA20121126135V), Nov 26, 2012: SKIN. CORRODED. DURING C-CHECK CARGO DOOR CUTOUT FWD AND AFT LOWER CORNERS CORRODED (LOCAL LEVEL 2). MX R & R CARGO DOOR CUTOUT FWD AND AFT LOWER CORNERS IAW EC5320-01494, REV 
- [SDR ASOA20121125134](https://openairdocs.org/sdr/ASOA20121125134), Nov 25, 2012: FLOOR SUPPORT. CORRODED. DURING C-CHECK RT OMEGA BEAM HAS CORROSION, LOCAL LEVEL 2, AT NUTPLATE FRAME 19A. MX PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 18-19A IAW EC5320-01718 (ORIG). 
- [SDR ASOA20121125133V](https://openairdocs.org/sdr/ASOA20121125133V), Nov 25, 2012: SILL. CORRODED. DURING C-CHECK, SERVICE DOOR CENTER SILL CORRODED, LOCAL LEVEL 2. MX R & R SERVICE DOOR CENTER SILL IAW SRM 51-40-02 AND CPM 51-21-00. THE ACFT WAS APPROVED FOR
- [SDR C2XA11RI123](https://openairdocs.org/sdr/C2XA11RI123), Jul 6, 2011: ANTI-ICE VALVE. DEFECTIVE. FLIGHT 2829 - EWR - FLIGHT CREW REPORTED ENG NR 2 ANTI ICE FAIL IN FLIGHT. EWR MX REMOVED AND REPLACED NR 2 ENG ANTI-ICE VALVE AND PERFORMED OPERATIONAL CHECK S
- [SDR C2XA11CL151](https://openairdocs.org/sdr/C2XA11CL151), Jun 20, 2011: PROXIMITY SWITCH. DIRTY. ORD FLT 6131 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND CLEANED AND RE-SECURED LANDING GEAR PROXIMITY SWITCHE
- [SDR C2XA11RI001](https://openairdocs.org/sdr/C2XA11RI001), Jan 6, 2011: WARNING SYSTEM. FALSE ACTIVATION. FLIGHT 2228 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. EWR MX RESET THE SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AC
- [SDR C2XA10CL139](https://openairdocs.org/sdr/C2XA10CL139), Aug 28, 2010: MANIFOLD. FAULTY. THE CREW REPORTED AN AILERON SYSTEM 2 INOPERATIVE MESSAGE ON THE ECIAS DURING CRUISE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 AILERON HYDRAULIC MANIFOLD. OP
- [SDR C2XA09RI007](https://openairdocs.org/sdr/C2XA09RI007), Jan 8, 2009: SIGN. INOPERATIVE. DURING ROUTINE MX, MX FOUND LOWER EMERGENCY LIGHT IDENTIFIER SIGN AT SEAT 12A INOPERATIVE. MX R&R SIGN AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED T
- [SDR C2XA09IA012](https://openairdocs.org/sdr/C2XA09IA012), Jan 6, 2009: ENGINE. MALFUNCTIONED. THE CREW REPORTED A LAV FIRE DETECTION INDICATION IN FLIGHT. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND PLACED THE L
- [SDR C2XA09IA010A](https://openairdocs.org/sdr/C2XA09IA010A), Jan 6, 2009: ENGINE. MALFUNCTIONED. SAT - FLIGHT 2630, THE CREW REPORTED A LAV FIRE DETECTION INDICATION IN FLIGHT. THE ACFT RETURNED TO SAT WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT
- [SDR C2XA08IA273](https://openairdocs.org/sdr/C2XA08IA273), Dec 23, 2008: SMOKE DETECTOR. MALFUNCTIONED. IAH - FLIGHT 2406, THE CREW REPORTED A LAV SMOKE INDICATION ON T/O FROM DAL. THE SYSTEM WAS RESET SUCCESSFULLY PER THE QRH, AND THE AIRCRAFT LANDED AT IAH WITHO
- [SDR C2XA08IA260](https://openairdocs.org/sdr/C2XA08IA260), Dec 20, 2008: SMOKE WARNING. MALFUNCTIONED. FLIGHT 2220 SHV-IAH - THE CREW REPORTED A MOMENTARY LAVATORY SMOKE WARNING DURING CRUISE. NO SMOKE CONDITIONS WERE NOTED AT THAT POINT AND THE AIRCRAFT LANDED A
- [SDR C2XA08SH164](https://openairdocs.org/sdr/C2XA08SH164), Dec 19, 2008: INLET. CORRODED. VARIOUS BOLTHOLES ON THE LT ENG AIR INLET CORRODED. REPAIRED BOLT HOLE ON LT ENG AIR INLET IAW EC 5420-01179. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08SH163](https://openairdocs.org/sdr/C2XA08SH163), Dec 19, 2008: FLOOR SUPPORT. CORRODED. CENTER OMEGA BEAM HAS CORROSION IN RADIUS AT FR 20. CENTER OMEGA BEAM WAS REPAIRED IAW SRM 53-21-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA08SH162](https://openairdocs.org/sdr/C2XA08SH162), Dec 18, 2008: SHROUD. CORRODED. SHV DURING C-CHECK LT AILERON LOWER SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED LT LOWER AILERON SHROUD IAW EC 5750-01315 (E). THE ACFT WAS APPROVED TO RETUR
- [SDR C2XA08SH161](https://openairdocs.org/sdr/C2XA08SH161), Dec 18, 2008: NUT PLATE. CORRODED. SHV DURING C-CHECK SERVICE DOOR LOWER NUTPLATE HOLES HAD CORROSION. MX REPAIRED SERVICE DOOR LOWER NUTPLATE HOLES BY REMOVING CORROSION AND FINDING SERVICE DOOR
- [SDR C2XA08SH160](https://openairdocs.org/sdr/C2XA08SH160), Dec 18, 2008: SHROUD. CORRODED. SHV DURING C-CHECK RT AILERON LOWER SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED RT AILERON LWR SHROUD IAW EC 5750-01315 (E). THE ACFT WAS APPROVED TO RETURN 
- [SDR C2XA08SH159](https://openairdocs.org/sdr/C2XA08SH159), Dec 18, 2008: PLATE. CORRODED. SHV DURING C-CHECK RT AILERON UPPER SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED RT UPPER AILERON SHROUD IAW EC 5750-01315 (E). THE ACFT WAS APPROVED TO RETUR
- [SDR C2XA08SH158](https://openairdocs.org/sdr/C2XA08SH158), Dec 18, 2008: PANEL. CORRODED. SHV DURING C-CHECK PANEL 191EL WAS FOUND TO HAVE CORRODED BONDING PLATES. MX R&R BONDING PLATES ON PANEL 191EL IAW EC 5750-01315 REV "E". THE ACFT WAS APPROVED 
- [SDR C2XA08CL111](https://openairdocs.org/sdr/C2XA08CL111), Oct 9, 2008: CONTROL UNIT. FAULTY. CLE FLIGHT NR 2626 THE CREW REPORTED A NR 1 T/R DISAGREE AND A SPOILER FAIL MSG IN FLIGHT. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX INSPECTED AN
- [SDR C2X2008F00012](https://openairdocs.org/sdr/C2X2008F00012), Jul 18, 2008: BRACKET. BROKEN. ACFT WAS IN FOR A SERVICE CHECK AND THE RT FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY HOLDER ASSEMBLY IAW
- [SDR C2XA08RI047](https://openairdocs.org/sdr/C2XA08RI047), Mar 13, 2008: PROXIMITY SWITCH. DEFECTIVE. FLIGHT 3156 - EWR - CREW REPORTED BANGING NOISE COMING FROM NOSE LANDING GEAR AREA DURING TAXIING. CREW RETURNED TO GATE. EWR MX REMOVED AND REPLACED UPLOCK BOX
- [SDR C2XA07CL107](https://openairdocs.org/sdr/C2XA07CL107), Dec 25, 2007: INVERTER. INOPERATIVE. DURING ROUTINE MAINTENANCE, THE OVERWING EXIT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONA
- [SDR C2XA07IA213](https://openairdocs.org/sdr/C2XA07IA213), Sep 23, 2007: INVERTER. INOPERATIVE. LCH - FLIGHT 3015, THE CREW REPORTED THE LEFT HAND WALL EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY EXIT LIGHT INV
- [SDR C2XA07RI073](https://openairdocs.org/sdr/C2XA07RI073), Aug 31, 2007: CONNECTOR. LOOSE. RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT ON SEAT 12A INOP. MX REMOVED THE EMERGENCY LIGHT ASSEMBLY AND FOUND CONNECTOR LOOSE. MX RESECURE
- [SDR C2XA07IA155](https://openairdocs.org/sdr/C2XA07IA155), Jun 27, 2007: SENSOR. SHORTED. IAH - FLIGHT 2852, THE CREW REPORTED A W/S 1 FAIL MESSAGE ON EICAS FOLLOWED BY LOUD CLICKING OF RELAYS AND A STRONG BURNED ELECTRICAL ODOR. THE AIRCRAFT LANDED 
- [SDR C2XA07BT022](https://openairdocs.org/sdr/C2XA07BT022), Feb 28, 2007: CHARGER. INOPERATIVE. EWR MX LOG SQUAWK FLT NR 3005 FOUND EMERGENCY LIGHTS (RT WING FUSELAGE FRONT FAIRING AND ISLE LIGHT NR 2) INOP. REMOVED AND REPLACED CHARGER ASSEMBLY IAW EMB 14
- [SDR C2XA06IA046](https://openairdocs.org/sdr/C2XA06IA046), Mar 22, 2006: INVERTER. INOPERATIVE. STL - DURING MAINTENANCE INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY 
- [SDR C2XA05SH034](https://openairdocs.org/sdr/C2XA05SH034), May 13, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRM 29-36. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRM 29 IAW EC5320-01237 AND EC532

All 72: https://openairdocs.org/aircraft/N48901/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/N48901/stcs.md

## Earlier aircraft with N48901

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N48901 before.

- [Cancelled 1990-07-27](https://openairdocs.org/deregistered/N48901-1990-07-27): Cessna 152, S/N 15281039. Triennial form not returned
- [Cancelled 1950-02-21](https://openairdocs.org/deregistered/N48901-1950-02-21): Fairchild M-62A, S/N T43-7064. Owner: [Hennings C H](https://openairdocs.org/faa-owner/HENNINGS%20C%20H), [Sandy, OR](https://openairdocs.org/faa-place/OR/Sandy)

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/aircraft.md
- The Rolls-Royce AE-3007A1P engine: https://openairdocs.org/engine/rolls-royce-ae-3007a1p.md

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