# N14542: 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: 145547
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 22, 2001
- Certificate issued: August 18, 2022
- Expires: August 31, 2029
- Mode S code: A0B842
- 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=14542
- Page: https://openairdocs.org/aircraft/N14542

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/N14542/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 N14542.

## FAA accident and incident reports

None matched to N14542.

## Service difficulty reports (57, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ASOA2019042375061](https://openairdocs.org/sdr/ASOA2019042375061), Apr 17, 2019: ACM. ODOR. PILOT REPORTED A BURNING SMELL NOTICED, PACK 1 OVHT AND DESELECTED PACK SMELL DISSAPATED.MX REMOVED AND REPLACED #1 PACK SYSTEM AIR CYCLE MACHINE WITH OPERATION
- [SDR ASOA201904075050](https://openairdocs.org/sdr/ASOA201904075050), Apr 7, 2019: ENGINE. LEAKING. ODOR OF RUBBER GETTING HOT WHILE THRUST LEVERS IN THE DETENT. MX R & R THE NR 1 ENGINE, OPS AND LEAK CHECKED GOOD. OCF SUCCESSFUL. A/C WAS APPROVED FOR RETURN T
- [SDR ASOA2019041075050](https://openairdocs.org/sdr/ASOA2019041075050), Apr 7, 2019: UNKNOWN. ODOR. PILOT REPORTED "ODOR OF RUBBER GETTING HOT WHILE THRUST LEVERS WERE IN THE DETENT. NO SMOKE OR FIRE, BUT ODOR PRESENT". AIR RETURN.
- [SDR ASOA2019040329547](https://openairdocs.org/sdr/ASOA2019040329547), Mar 29, 2019: FAN. FAILED. PILOT REPORTED "SMOKE SMELL IN THE CABIN AND COCKPIT GOT BETTER ONCE PACK #1 TURNED OFF. MX INSPECTED AND FOUND #1 RECIRCULATION FAN MUFFLER BLOWN AND DAMAGED A
- [SDR ASOA201903275046](https://openairdocs.org/sdr/ASOA201903275046), Mar 27, 2019: ACM. SEIZED. CREW REPORT SMOKE IN CABIN DURING CLIMBOUT. CLEARED AFTER SHUTTING OFF PACK 1. SMELL OF SMOKE BEFORE BEFORE PACK 1 OVERLOADED AND SHUT DOWN. AIR RETURNED. FLT 4
- [SDR ASOA2018092583058](https://openairdocs.org/sdr/ASOA2018092583058), Sep 18, 2018: ENGINE. LEAKING. THE CREW REPORTED BAD/NOXIOUS ODOR FROM PACK DURING CLIMB. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD.
- [SDR ASOA2018091973057](https://openairdocs.org/sdr/ASOA2018091973057), Sep 17, 2018: DUCT. FAULTY. THE CREW REPORTED STRONG ODOR COMING FROM THE PACKS WITH BLEEDS SELECTED ON TAKE-OFF, CLIMB AND DESCEND. MAINTENANCE REPLACED NR 1 PACK DUCT. OPERATIONAL CHECKS
- [SDR ASOA2018091835202](https://openairdocs.org/sdr/ASOA2018091835202), Sep 13, 2018: UNKNOWN. ODOR. PILOT REPORTED BAD/NOXIOUS ODOR IN COCKPIT DURING CLIMBOUT AND DESCENT. MX RAN PACKS FOR EXTENDED PERIOD AND COULD NOT DUPLICATE ODOR. A/C WAS APPROVED FOR RETU
- [SDR ASOA201806263037](https://openairdocs.org/sdr/ASOA201806263037), Jun 26, 2018: ACM. SEIZED. THE CREW REPORTED SMOKE IN THE COCKPIT DURING FLIGHT. MAINTENANCE INSPECTED AND FOUND THE NR 2 ACM SEIZED. THE RIGHT PACK AIR CYCLE MACHINE WAS REPLACED. OPS CH
- [SDR ASOA2018067035151](https://openairdocs.org/sdr/ASOA2018067035151), Jun 3, 2018: CONTROL VALVE. FAILED. PILOT REPORTED THE MAIN BRAKES WERE LESS EFFECTIVE THAN NORMAL, ALMOST FEELS LIKE THEY WERE OVERHEATED AND GLAZED ON THE DISCS. MX REMOVED AND REPLACED THE OTBD
- [SDR ASOA2018422010](https://openairdocs.org/sdr/ASOA2018422010), Apr 2, 2018: FIRE DETECTOR. FAILED. NR 2 ENGINE FIRE DETECT FAILED DURING TAXING FOR TAKEOFF. MAINTENANCE REMOVED AND REPLACED ENGINE FIRE DETECTOR IAW AMM 26-11-01. REMOVED AND REPLACED THE PYLON
- [SDR ASOA201802117010](https://openairdocs.org/sdr/ASOA201802117010), Feb 9, 2018: WIRE. MISSING. EMERGENCY FLOOR LIGHTING STRIP AT ROWS 5,6 & 7 HAS MISSING WIRES. INSTALLED NEW LIGHT STRIP. OPS CHECK GOOD.
- [SDR ASOA201802117009](https://openairdocs.org/sdr/ASOA201802117009), Feb 9, 2018: BATTERY. NOT REPORTED. EMERGENCY LIGHT BATTERY NEEDS REPLACED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY NR 4. OPS CK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA201802077007](https://openairdocs.org/sdr/ASOA201802077007), Feb 7, 2018: SKIN. DENTED. TYS A/C IS IN A C-CHECK STATUS WHEN INSPECTION FOUND FUSELAGE DENTED BETWEEN FRAME 20-21 STR-11L AND 12L. MAINTENANCE REPAIRED AREA IAW ETD 2018-002931. ALL WOR
- [SDR ASOA201802117011](https://openairdocs.org/sdr/ASOA201802117011), Jan 25, 2018: STRINGER. CRACKED. STRINGER 2L AT FRAME 75 CRACKED. REMOVED SHEAR CLIP, CUT-OUT DAMAGED STR 2L SECTION BETWEEN FRM 74-75, INSTALLED STRINGER AND REINSTALLED SHEAR CLIP COMPLETED R
- [SDR ASOA201801267003](https://openairdocs.org/sdr/ASOA201801267003), Jan 6, 2018: YOKE. CRACKED. DURING INSPECTION AT TYS, THE NR 2 ENGINE FWD PYLON UPR LINKAGE FITTING WAS FOUND CRACKED. THE CRACK MEASURED .20" IN LENGTH LOCATED ALONG THE INNER FLANGE, NEA
- [SDR ASOA201706253212](https://openairdocs.org/sdr/ASOA201706253212), Jun 25, 2017: OIL SYSTEM. LEAKING. THE CREW REPORTED STRONG OIL ODOR FROM THE ENGINES IN FLIGHT. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGI
- [SDR ASOA201705265079](https://openairdocs.org/sdr/ASOA201705265079), May 26, 2017: ACM. FAILED. PILOT REPORTED SMOKE IN CABIN AND COCKPIT AFTER TAKEOFF. RETURNED TO DEPARTURE. MX REMOVED AND REPLACED THE LT ACM . OPERATIONAL CHECKED GOOD. ACFT RETURNED TO 
- [SDR ASOA201705023131](https://openairdocs.org/sdr/ASOA201705023131), May 2, 2017: WIRE HARNESS. BURNED. ELECTRICAL ODOR IN THE BACK OF THE CABIN. FOUND BETWEEN ROW 20CD AND 23CD WALL LIGHTING HARNESS BURNED. REMOVED AND REPLACED ELECTRICAL HARNESS. OPERATIONAL CHE
- [SDR ASOA201610110575](https://openairdocs.org/sdr/ASOA201610110575), Oct 11, 2016: INVERTER. INOPERATIVE. CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT DOES NOT LIGHT UP. MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER WITH OPERATIONAL CHECK GOO
- [SDR ASOA20160927051R](https://openairdocs.org/sdr/ASOA20160927051R), Sep 27, 2016: HOLDER. SMOKE. CREW REPORTED SMOKE COMING FROM CAPTAIN`S CHART HOLDER LIGHT AREA. ACFT PERFORMED SAFE AND UNEVENTFUL AIR RETURN BACK TO DEPARTURE. MX REMOVED AND REPLACED THE 
- [SDR ASOA20150625138V](https://openairdocs.org/sdr/ASOA20150625138V), Jun 25, 2015: MOUNT. CRACKED. DURING C-CHECK, THE LT ENGINE FORWARD LOWER MOUNT YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FITTING IAW EC5450-01156. THE ACFT WAS APPROVED FO
- [SDR ASOA20141124140](https://openairdocs.org/sdr/ASOA20141124140), Nov 24, 2014: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE AISLE EMERGENCY LIGHT SEATS 18 & 19 WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R LIGHT AND OPS TESTED WITH NO DEFECTS. THE 
- [SDR ASOA20140308033](https://openairdocs.org/sdr/ASOA20140308033), Mar 8, 2014: LIGHT. ARCED. A BURNED PLASTIC ODOR REPORTED IN CABIN BY SEAT 2A. MX INSPECTED ACFT CABIN AND FOUND SEAT 6A LIGHT TO BE THE CAUSE. MX R & R SEAT 6A CEILING LIGHT ASSY WITH OP
- [SDR ASOA20130910105](https://openairdocs.org/sdr/ASOA20130910105), Sep 10, 2013: LIGHT. INOPERATIVE. DURING SCHEDULED MX INSPECTION, THE ROWS 10 & 11 EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE. MX R & R THE LIGHT STRIP AT ROW 10 & 11 WITH OPS CHECK SUCCESSFUL.
- [SDR ASOA20121117108R](https://openairdocs.org/sdr/ASOA20121117108R), Nov 17, 2012: CONTROL UNIT. FAULTY. ON TOUCHDOWN CREW REPORTED INBD BRAKE INOPERATIVE MESSAGE ON EICAS AND COULD FEEL BRAKE NOT WORKING. MX PERFORMED OPS CHECK OF INBD BRAKE WITH NO FAULTS FOUND. 
- [SDR ASOA20121025086C](https://openairdocs.org/sdr/ASOA20121025086C), Oct 25, 2012: LIGHT. ODOR. THE CREW REPORTED SMOKE ODOR IN THE CABIN. MX TIGHTENED LOOSE WIRE ON ROW 8A LIGHT ASSY. OPS CHECKS WERE GOOD.
- [SDR ASOA20120521039](https://openairdocs.org/sdr/ASOA20120521039), May 21, 2012: CHARGER. INOPERATIVE. DURING SCHEDULED MX INSPECTION, THE LT FWD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R THE NR 1 EMER LIGHT BATTERY CHARGER IAW AMM 33-50-04 WITH OP
- [SDR C2XA11SH118](https://openairdocs.org/sdr/C2XA11SH118), Aug 10, 2011: FRAME. CORRODED. SHV - DURING C-CHECK THE LOWER AFT CORNER OF THE SERVICE DOOR CUTOUT WAS FOUND TO BE CORRODED, FRAME 22 STRINGERS 14-15R. MAINTENANCE REMOVED THE CORROSION AND 
- [SDR C2XA10RI067](https://openairdocs.org/sdr/C2XA10RI067), May 28, 2010: BATTERY. OVERTEMP. FLIGHT 5671 - ALB - FLIGHT CREW REPORTED NR 2 MAIN BATTERY OVERTEMP ON DECENT. CREW DECLARED EMERGENCY AND PROCEED WITH THE DESCENT AND LANDED ACFT UNEVENTFULLY
- [SDR C2XA10TY035](https://openairdocs.org/sdr/C2XA10TY035), Mar 10, 2010: LIGHT. INOPERATIVE. SEAT 12A OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB IAW EMB 145 AMM 33-50-02, OPS CHECK GOOD.
- [SDR C2XA10CL017](https://openairdocs.org/sdr/C2XA10CL017), Feb 2, 2010: BLEED VALVE. FAULTY. ORD FLT 5666 THE CREW REPORTED A NR 1 ENGINE BLEED VALVE CLOSED MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPE
- [SDR C2XA09IA258](https://openairdocs.org/sdr/C2XA09IA258), Oct 14, 2009: O-RING. LEAKING. FLIGHT 2488, THE CREW REPORTED A BLEED TWO LEAK ON CLIMB AT 8000 FT. THE AIRCRAFT RETURNED TO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED
- [SDR C2XA09IA259](https://openairdocs.org/sdr/C2XA09IA259), Oct 14, 2009: BLEED VALVE. INOPERATIVE. IAH - FLIGHT 2488, THE CREW REPORTED A BLLED(?) ONE LEAK ON CLIMB-OUT AT 8000 FEET. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE R
- [SDR C2XA09TY231](https://openairdocs.org/sdr/C2XA09TY231), Aug 26, 2009: OUTFLOW VALVE. INOPERATIVE. AIRCRAFT FAILED TO PRESSURIZE NORMALLY ON TAKEOFF. REMOVED AND REPLACED OUTFLOW VALVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR C2XA09TY224](https://openairdocs.org/sdr/C2XA09TY224), Aug 18, 2009: FITTING. CRACKED. NR 2 ENG FWD LWR PYLON CRACKED AT STOP DRILLED HOLE. REMOVED AND REPLACED NR 2 ENG FWD LWR YOKE LINKAGE FITTING.
- [SDR C2XA09TY219](https://openairdocs.org/sdr/C2XA09TY219), Aug 13, 2009: SILL. CORRODED. CARGO DOOR SILL CORRODED. REMOVED AND REPLACED CARGO DOOR SILL.
- [SDR C2XA09CL034](https://openairdocs.org/sdr/C2XA09CL034), Mar 29, 2009: SWITCH. FAULTY. CLE FLIGHT 2378 - THE CREW REPORTED A WING AND STAB ANTI-ICE FAIL MESSAGE IN ICING CONDITIONS DURING CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT F
- [SDR C2XA09RI018](https://openairdocs.org/sdr/C2XA09RI018), Jan 24, 2009: PROXIMITY SWITCH. INTERMITTENT. FLIGHT 2188 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR/GROUND C/B POPPED ON LANDING. EWR MX REMOVED AND REPLACED WEIGHT ON WHEEL PROXIMITY SWITCH AND PERFORM
- [SDR C2XA08RI162](https://openairdocs.org/sdr/C2XA08RI162), Oct 27, 2008: BATTERY PACK. DISCHARGED. FLIGHT 2747 - EWR - FLIGHT CREW REPORTED 2 EMERGENCY LIGHTS WOULD NOT STAY ILLUMINATED. EWR MX REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY AND PERFORMED O
- [SDR C2XA04IA106](https://openairdocs.org/sdr/C2XA04IA106), Aug 19, 2004: THERMAL SWITCH. INOPERATIVE. THE CREW REPORTED APU FAIL ON GROUND AND AUTO SHUTDOWN IN FLIGHT WITH A FUEL ODOR PRESENT. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE APU
- [SDR C2XA04BT018](https://openairdocs.org/sdr/C2XA04BT018), Feb 5, 2004: BULB. FAULTY. DURING ROUTINE INSPECTION, MAINTENANCE FOUND LEFTHAND WING EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED LEFTHAND WING EMERGENCY LIGHT IAW EMB145 MM 3
- [SDR C2XA03CL213](https://openairdocs.org/sdr/C2XA03CL213), Dec 26, 2003: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE THE LEFT AFT OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LEFT AFT LIGHT BULB. OPERATIONAL CHECK
- [SDR C2XA03BT104](https://openairdocs.org/sdr/C2XA03BT104), Nov 4, 2003: LIGHT. INOPERATIVE. BTV---CO2943, DURING SERVICE/ROUTINE INSPECTION MAINTENANCE FOUND THE AFT OVERHEAD EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED AFT OVERHEAD EMERGENC
- [SDR C2XA03SH423](https://openairdocs.org/sdr/C2XA03SH423), Oct 31, 2003: BATTERY. DISCHARGED. SHV- DURING C-CHECK THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND NOT TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY
- [SDR C2XA03SH422](https://openairdocs.org/sdr/C2XA03SH422), Oct 29, 2003: SKIN. DENTED. SHV- DURING C-CHECK THE LEFT SIDE FUSELAGE SKIN WAS FOUND TO BE DENTED. MAINTENANCE RESTORED DENTED AREA TO ORIGINAL SHAPE AND PERFORMED A DOUBLER REPAIR IAW EC
- [SDR C2XA03SH415](https://openairdocs.org/sdr/C2XA03SH415), Oct 25, 2003: FLOORBEAM. CORRODED. DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10
- [SDR C2XA03SH411](https://openairdocs.org/sdr/C2XA03SH411), Oct 24, 2003: LONGERON. CHAFED. SHV- DURING C-CHECK THE RT LOWER COWLING OUTBOARD LONGERON WAS FOUND TO BE CHAFED APPROXIMATELY 7 INCHES FORWARD OF AFT END. MAINTENANCE REMOVED DAMAGED AREA AN
- [SDR C2XA03SH410](https://openairdocs.org/sdr/C2XA03SH410), Oct 24, 2003: BUTTSTRAP. CORRODED. SHV-DURING C-CHECK THE CENTER BUTTSTRAP AT FR 20-23 WAS FOUND TO CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE
- [SDR C2XA03SH407](https://openairdocs.org/sdr/C2XA03SH407), Oct 22, 2003: CROSSBEAM. CORRODED. SHV- DURING C-CHECK THE RT CROSSBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02. THE

All 57: https://openairdocs.org/aircraft/N14542/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/N14542/stcs.md

## Earlier aircraft with N14542

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N14542 before.

- [Cancelled 1975-05-06](https://openairdocs.org/deregistered/N14542-1975-05-06): Semco Balloon TC-4A, S/N SEM133. Owner: [Flying Z Inc](https://openairdocs.org/faa-owner/FLYING%20Z%20INC), [Spokane, WA](https://openairdocs.org/faa-place/WA/Spokane)
- [Cancelled 1948-07-27](https://openairdocs.org/deregistered/N14542-1948-07-27): Aeronca C-3, S/N A-319. Owner: [Cothron James M](https://openairdocs.org/faa-owner/COTHRON%20JAMES%20M), [South Miami, FL](https://openairdocs.org/faa-place/FL/South%20Miami)

## 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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