# N16541: 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: 145542
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 14, 2001
- Certificate issued: January 27, 2023
- Expires: January 31, 2030
- Mode S code: A1073F
- 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=16541
- Page: https://openairdocs.org/aircraft/N16541

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/N16541/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 N16541.

## FAA accident and incident reports

None matched to N16541.

## Service difficulty reports (79, 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 JJBA20220306007](https://openairdocs.org/sdr/JJBA20220306007), Mar 6, 2022: PROXIMITY SWITCH. LOOSE. LG AIR GROUND FAIL MESSAGE ON LANDING AT 50FT. PERFORMED TROUBLESHOOTING. FOUND PROXIMITY SWITCH BRACKET ON RH MAIN LANDING GEAR LEG LOOSE. BRACKET BOLT WAS BRO
- [SDR JJBA2022022006021](https://openairdocs.org/sdr/JJBA2022022006021), Feb 26, 2022: LAMP. INOPERATIVE. EMERGENCY CEILING LIGHT ON CEILING PANEL 253CLC INOPERATIVE. REMOVED AND REPLACED EMERGENCY CEILING LIGHT ON CEILING PANEL 253CLC.
- [SDR JJBA202201184023](https://openairdocs.org/sdr/JJBA202201184023), Jan 14, 2022: LIGHT. INOPERATIVE. COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT. OPS CHECK SAT
- [SDR JJBA20210929054](https://openairdocs.org/sdr/JJBA20210929054), Sep 29, 2021: BATTERY PACK. INOPERATIVE. LH FWD WING/FUSELAGE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH FWD EMERGENCY LIGHT LAMP. OPS CHECK FAIL. SUSPECTED EMERGENCY BATTERY #1 NEEDS TO BE R
- [SDR JJBA20210923036](https://openairdocs.org/sdr/JJBA20210923036), Sep 23, 2021: BATTERY PACK. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS AFT OF EXIT ROW ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK SAT.
- [SDR JJBA20210808027](https://openairdocs.org/sdr/JJBA20210808027), Aug 8, 2021: BRAKE ASSY. LEAKING. HYD 1 LOW QUANTITY ADVISORY CAME ON IN CRUISE. TRANSFERRED HYDRAULIC FLUID FROM #2 SYSTEM TO #1 SYSTEM. DUE TO HYD 1 LOW ADVISORY MESSAGE, R&R OUTBOARD BRAKES. 
- [SDR JJBA20210414050](https://openairdocs.org/sdr/JJBA20210414050), Apr 14, 2021: SEALANT. MISSING. SEALANT MISSING FROM RIGHT LANDING GEAR NUT WHERE MAIN BRACE STRUT AND LOWER SIDE ARM CONNECT. APPLIED SEALANT TO RLG NUT.
- [SDR JJBA2021370003](https://openairdocs.org/sdr/JJBA2021370003), Mar 7, 2021: ARMREST. CRACKED. ARMREST STRUCTURE CRACKED ON PAX SEAT 10A. REMOVED AND REPLACED SEAT 10A INBOARD ARMREST STRUCTURE (SPREADER).
- [SDR JJBA20210212040](https://openairdocs.org/sdr/JJBA20210212040), Feb 12, 2021: NONE. NONE. FUSELAGE SKIN DAMAGED AT FR29 TO FR31 BETWEEN S12R TO S13R. REMOVED DAMAGED FUSELAGE SKIN STR 13R FR 29R TO 31R. LOCATED AND DRILLED REPAIR DOUBLER AND FILLER. 
- [SDR JJBA20210206020](https://openairdocs.org/sdr/JJBA20210206020), Feb 6, 2021: SHEAR TIE. DAMAGED. SHEAR CLIP AT FRAME 30 BETWEEN STRINGER 12R AND 13R. REPAIRED SHEAR CLIP AT FRAME 30 BETWEEN STRINGER 12 AND 13R BY STEPPING FASTENER SIZE HOLD UP 1/32 ORG HOLE
- [SDR JJBA20210205019](https://openairdocs.org/sdr/JJBA20210205019), Feb 5, 2021: SKIN. DAMAGED. FUSELAGE SKIN DAMAGE AT FR29 TO FR31 BETWEEN S12R TO S13R. REPAIRED CENTER FUSELAGE II SKIN DAMAGE AT FR29 TO FR31 BETWEEN S12R TO S13R.
- [SDR ASOA201907143038](https://openairdocs.org/sdr/ASOA201907143038), Jul 14, 2019: LIGHT. INOPERATIVE. THE CREW REPORTED AISLE PATH EMERGENCY LIGHT AFT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE AFT AILSE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD
- [SDR ASOA2018121073071](https://openairdocs.org/sdr/ASOA2018121073071), Dec 7, 2018: ENGINE. LEAKING. THE CREW REPORTED ON CLIMBOUT AT 6000 FEET LAV SMOKE WARNING ON EICAS. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE #1 ENG
- [SDR ASOA2018120763069](https://openairdocs.org/sdr/ASOA2018120763069), Dec 6, 2018: CONTROL PANEL. FAULTY. THE CREW REPORTED @1000' LAV SMOKE MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LAV SMOKE DETECTOR P
- [SDR ASOA2018112874067](https://openairdocs.org/sdr/ASOA2018112874067), Nov 27, 2018: ACM. FROZEN. IAH - THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPEVCTED THE AIRCRAFT, REMOVED AND REPLACED THE
- [SDR ASOA2018090495181](https://openairdocs.org/sdr/ASOA2018090495181), Aug 29, 2018: CONNECTOR. DISCONNECTED. DURING MX INSPECTION THE ROW 18 CEILING AFT EXIT SIGN WAS FOUND INOP. MX INSTALLED CONNECTORS ON ROW 18 AFT EXIT SIGN WITH OPS CHECK GOOD. A/C WAS APPROVED FOR 
- [SDR ASOA201706024041](https://openairdocs.org/sdr/ASOA201706024041), Jun 2, 2017: SKIN. DENTED. DURING C-CHECK INSPECTION, THE CENTER FUSELAGE RT SKIN WAS FOUND WAS FOUND TO BE DENTED 3.5 INCH FWD OF FRAME 24 AND 1 INCH BELOW STRINGER 15R. MAINTENANCE REMO
- [SDR ASOA201706024040](https://openairdocs.org/sdr/ASOA201706024040), Jun 2, 2017: FRAME. CRACKED. DURING C-CHECK INSPECTION, THE UPPER FRAME 10 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED AT A RIVET LOCATION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME
- [SDR ASOA201706024039](https://openairdocs.org/sdr/ASOA201706024039), Jun 2, 2017: CROSSBEAM. CRACKED. DURING A C-CHECK INSPECTION, THE NLG UPLOCK BOX CROSSBEAM WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM AND THE AIRCRAFT WAS 
- [SDR ASOA201706024033S](https://openairdocs.org/sdr/ASOA201706024033S), Jun 2, 2017: GUSSET. CORRODED. DURING A C-CHECK INSPECTION, THE LEFT INBD FLOOR SUPPORT GUSSET WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND RPELACED THE AFFECTED GUSSET AND
- [SDR ASOA201706024035](https://openairdocs.org/sdr/ASOA201706024035), Jun 2, 2017: CROSSBEAM. CORRODED. DURING A C-CHECK INSPECTION, THE CENTER AISLE CROSSBEAM SUPPORT AT FRAME 20 WAS FOUND TO HAVE BARE METAL AND CORROSION BEYOND LIMITS. MAINTENANCE REMOVED AND RE
- [SDR ASOA201706024034](https://openairdocs.org/sdr/ASOA201706024034), Jun 2, 2017: GUSSET. CORRODED. DURING A C-CHECK INSPECTION, THE CENTER FLOOR SUPPORT GUSSET AT FRAMES 60 - 61 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFE
- [SDR ASOA201706024033](https://openairdocs.org/sdr/ASOA201706024033), Jun 2, 2017: GUSSET. CORRODED. DURING A C-CHECK INSPECTION, THE LT INBD FLOOR SUPPORT GUSSET WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSET AND T
- [SDR ASOA201705304037](https://openairdocs.org/sdr/ASOA201705304037), May 30, 2017: FRAME. DAMAGED. DURING A C-CHECK INSPECTION, FRAME 72 WAS FOUND TO BE DAMAGED BETWEEN STRINGERS 15 & 16R. MAINTENANCE REMOVED THE DAMAGED.
- [SDR ASOA201705294036](https://openairdocs.org/sdr/ASOA201705294036), May 29, 2017: SKIN. DAMAGED. DURING A C-CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO HAVE A SMALL NICK AT FRAME 68 BETWEEN STRINGERS 10 & 11L. MAINTENANCE BLENDED THE AFFECTED AREA 
- [SDR ASOA201704077006](https://openairdocs.org/sdr/ASOA201704077006), Apr 7, 2017: WIRE. BROKEN. A/C WAS IN FOR A ROUTINE CHECK WHEN INSPECTION FOUND THE AFT EMERGENCY EXIT LIGHT INOP. MAINTENANCE FOUND A BROKEN WIRE AND SPLICE THE WIRE BACK IAW SWPM 20-21-
- [SDR ASOA20160317013](https://openairdocs.org/sdr/ASOA20160317013), Mar 17, 2016: LAMP. ARCED. A BURNING PLASTIC ODOR REPORTED FROM THE GALLEY NEAR THE OVERHEAD LIGHT. MX R & R THE LIGHT BLUBS AT SEAT 1 A WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN 
- [SDR ASOA20150912052R](https://openairdocs.org/sdr/ASOA20150912052R), Sep 12, 2015: CONTROL PANEL. FAULTY. PILOT REPORTED THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE R & R THE F/A CONTROL PANEL ASSY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVIC
- [SDR ASOA20150831048R](https://openairdocs.org/sdr/ASOA20150831048R), Aug 31, 2015: BATTERY PACK. SHORTED. AN ELECTRICAL BURNING ODOR WAS REPORTED IN THE COCKPIT. MAINTENANCE PERFORMED INSPECTION OF COCKPIT AREA AND FOUND CAPTAIN`S FLASHLIGHT TO BE CAUSE AND PLACED O
- [SDR ASOA20150807044R](https://openairdocs.org/sdr/ASOA20150807044R), Aug 7, 2015: VALVE. ODOR. PILOT REPORTED BLEED 1 & 2 OVERTEMP IN ICING THEN ODOR OF SOMETHING BURNING. MAINTENANCE R & R NR 1 ENGINE FAN AIR VALVE, FAN AIR THERMOSTATS 1 & 2, A HIGH STAG
- [SDR ASOA20141212099](https://openairdocs.org/sdr/ASOA20141212099), Dec 12, 2014: SIGN. NO TEST. DURING ROUTINE MAINTENANCE, THE CEILING EMERGENCY EXIT LIGHT DID NOT ILLUMINATE DURING TEST. MAINTENANCE REPLACED THE EXIT LOCATOR SIGN . OPS CHECKED GOOD.
- [SDR ASOA20140414062](https://openairdocs.org/sdr/ASOA20140414062), Apr 14, 2014: PITOT SYSTEM. CONTAMINATED. CREW REPORTED AT FL 370 A NOTICEABLE ICE BUILD UP ON THE UNPROTECTED SURFACES AS WELL AS THE TAT. SHORTLY AFTER IAS AND ALT INSTRUMENTS BEGAN TO FAIL FOLLOWED B
- [SDR ASOA20131211137R](https://openairdocs.org/sdr/ASOA20131211137R), Dec 11, 2013: LIGHT. INOPERATIVE. DURING SCHEDULED MAINTENANCE INSPECTION, THE CENTER AISLE EMERGENCY LIGHTS FROM SEAT 1A-3A WERE FOUND INOPERATIVE. MAINTENCE R & R THE CENTER AISLE LIGHT STRIP 
- [SDR ASOA20130506035](https://openairdocs.org/sdr/ASOA20130506035), May 6, 2013: NONE. NONE. THE CREW REPORTED EMERGENCY LIGHT NOT ARMED MESSAGE APPEARED WITH NO REASON. REPORTED 2 EMERGENCY LIGHTS WOULD NOT TURN ON. MX INSPECTED AND RESET ACFT SYS AND 
- [SDR ASOA20130402123V](https://openairdocs.org/sdr/ASOA20130402123V), Apr 3, 2013: BEAM. CORRODED. DURING C-CHECK, BAGGAGE DOOR LOWER CUTOUT MAIN BEAM CORRODED. FRAMES 65-68. BEAM R & R IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130123243T](https://openairdocs.org/sdr/ASOA20130123243T), Jan 21, 2013: ATTACH FITTING. DAMAGED. VERTICAL STAB RT AND LT MOUNT LUGS WORN BEYOND LIMITS. OVERSIZED RT AND LT VERTICAL STAB BEARING HOUSINGS TO 1ST REWORK DIMENSIONS AND INSTALLED BUSHINGS.
- [SDR C2XA11CL204](https://openairdocs.org/sdr/C2XA11CL204), Sep 11, 2011: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE THE 4TH AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP AND OPERATIONAL CHECKS WERE GOOD
- [SDR C2XA11CL120](https://openairdocs.org/sdr/C2XA11CL120), May 8, 2011: PROXIMITY SWITCH. FAULTY. EWR FLT 2038 THE CREW REPORTED DURING GEAR RETRACTION RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS. MESSAGE DID NOT CLEAR. ALSO STATED ON INITAL
- [SDR C2XA11CL118](https://openairdocs.org/sdr/C2XA11CL118), May 6, 2011: CONNECTOR. CORRODED. DAY FLT 5857 THE CREW REPORTED THE SPOILERS DEPLOYED IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT SPEED BRAKE PROXIMITY SWITCH AND CONNECTOR P1166. O
- [SDR C2XA11TY053](https://openairdocs.org/sdr/C2XA11TY053), May 1, 2011: DAU. MALFUNCTIONED. L/G AIR/GROUND FAIL MESSAGE ON EICAS. RECEIVED MESH PROX TRAILING ARM IAW EMB 145AMM 32-63-05 AND REMOVED AND REPLACED DAU NR 1 IAW EMB 145AMM 31-41-01 OPS CHEC
- [SDR C2XA11CL093](https://openairdocs.org/sdr/C2XA11CL093), Apr 9, 2011: ELECTRONIC UNIT. FAULTY. ORD FLT 6112 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER GEAR EXTENSION. MAINTENANCE INSPECTED AND REPLACED THE RIGHT GEAR DOWNLOCK A PROXIMI
- [SDR C2XA11CL040](https://openairdocs.org/sdr/C2XA11CL040), Feb 6, 2011: SMOKE DETECTOR. FAILED. DURING ROUTINE MAINTENANCE THE FORWARD CARGO SMOKE DETECTOR FAILED THE TASK CARD CHECK. LED STAYS ON ALL THE TIME. MAINTENANCE REPLACED THE SMOKE DETECTOR. OPER
- [SDR C2XA10CL124](https://openairdocs.org/sdr/C2XA10CL124), Aug 3, 2010: PROXIMITY SWITCH. OUT OF ADJUST. CLE FLT 5658 THE CREW REPORTED A AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. MAINTENANCE INSPECTED AND ADJUSTED THE LEFT GEAR WOW PROXIMITY SWITCH. OPERATIONAL CHECK
- [SDR C2XA10CL086](https://openairdocs.org/sdr/C2XA10CL086), Jun 5, 2010: WARNING SYSTEM. ACTIVATED. IAD FLT 5687 THE CREW REPORTED A ENGINE 2 LOW FUEL PRESSURE WARNING ON TAKEOFF ROLL WHILE ON PUMP A. MAINTENANCE INSPECTED AND RELEASED AIRCRAFT IAW MEL PROCEDU
- [SDR C2XA09CL100](https://openairdocs.org/sdr/C2XA09CL100), Jul 21, 2009: CONNECTOR. LOOSE. DURING ROUTINE MAINTENANCE, THE LEFT OVERWING EMERGENCY LIGHT EXIT SIGN WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED THE EXIT SIGN CONNECTOR. OPERATIONA
- [SDR C2XA09SH171](https://openairdocs.org/sdr/C2XA09SH171), Jun 7, 2009: ATTACH BRACKET. DAMAGED. DURING C-CK. RT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHINGS. REMOVED AND REPLACED ATTACHMENT BRACKET IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN
- [SDR C2XA09RIO90](https://openairdocs.org/sdr/C2XA09RIO90), May 4, 2009: CONTROL PANEL. INOPERATIVE. FLIGHT 3064 - RIC - FLIGHT CREW REPORTED THAT NAV NR 1 AND NAV NR 2 DASHED OUT - NO NAV INFLIGHT. CREW DIVERTED FLIGHT TO RIC AND LANDED ACFT UNEVENTFUL. RIC MX
- [SDR C2XA09CL024](https://openairdocs.org/sdr/C2XA09CL024), Mar 5, 2009: THRUST REVERSER. FAULTY. CLE FLIGHT 2767 - THE CREW REPORTED AN ENGINE 2 THRUST REVERSER DISAGREE ON TAKEOFF ROLL. THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REL
- [SDR C2XA09IA004](https://openairdocs.org/sdr/C2XA09IA004), Jan 3, 2009: CONTROLLER. MALFUNCTIONED. THE CREW REPORTED, LEVEL AT FL360 RAPID DECOMPRESSION CABIN ALT REACHED 12,000. THE ACFT LANDED WITHOUT INCIDENT WHERE MX REMOVED AND REPLACED THE DIGITAL CONTR
- [SDR C2XA08IA271](https://openairdocs.org/sdr/C2XA08IA271), Dec 29, 2008: FIRE LOOP. CHAFED. IAH - FLIGHT 2386, THE CREW REPORTED A NUMBER ONE ENGINE FIRE DETECTOR FAIL IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND

All 79: https://openairdocs.org/aircraft/N16541/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/N16541/stcs.md

## Earlier aircraft with N16541

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N16541 before.

- [Cancelled 1983-03-26](https://openairdocs.org/deregistered/N16541-1983-03-26): Piper PA-28-235, S/N 28-7310104. Administratively canceled. Owner: [Flying Chargers Inc](https://openairdocs.org/faa-owner/FLYING%20CHARGERS%20INC), [Thornton, CO](https://openairdocs.org/faa-place/CO/Thornton)

## 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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