# N12540: 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: 145537
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 7, 2001
- Certificate issued: August 18, 2022
- Expires: August 31, 2029
- Mode S code: A06942
- Registered owner: [Dulux Public Charter LLC](https://openairdocs.org/faa-owner/DULUX%20PUBLIC%20CHARTER%20LLC)
- Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas)
- Owner type: LLC
- Owner's area on the map: 32.8153° N, 96.8763° W: Placed by OpenAirDocs at the center of ZIP code 75247, 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=12540
- Page: https://openairdocs.org/aircraft/N12540

From the FAA registry file of October 22, 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/N12540/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 N12540.

## FAA accident and incident reports

None matched to N12540.

## Service difficulty reports (86, 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 ASOA201902274011](https://openairdocs.org/sdr/ASOA201902274011), Feb 27, 2019: WIRE. BROKEN. LCH - FLIGHT 4264 THE VERY LAST EMERGENCY PROX LIGHT STRIP WAS FOUND TO BE INOPERATIVE DUE TO A BROKEN WIRE ON THE LIGHT ASSEMBLY. MAINTENANCE PLACED THE ITEM O
- [SDR ASOA201710134054](https://openairdocs.org/sdr/ASOA201710134054), Oct 13, 2017: ACM. FROZEN. THE CREW REPORTED SMOKE IN THE CABIN AND FLIGHT DECK. THE AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACE
- [SDR ASOA201710047018](https://openairdocs.org/sdr/ASOA201710047018), Oct 4, 2017: RIB. CRACKED. LEFT WING RIB 21 CRACKED. CUT OUT THE SECTION AND INSTALLED FILLER AND DOUBLER.
- [SDR ASOA201710047016](https://openairdocs.org/sdr/ASOA201710047016), Oct 4, 2017: FLOOR SUPPORT. CORRODED. RIGHT OMEGA BEAM, FRAME 23 CORRODED BEYOND LIMITS AT SCREW HOLES. REMOVED AND REPLACED THE OMEGA BEAM.
- [SDR ASOA201805264030](https://openairdocs.org/sdr/ASOA201805264030), May 26, 2017: BATTERY PACK. DISCHARGED. IAH - DURING MAINTENANCE INSPECTION THE UPPER EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY LIGH
- [SDR ASOA201702134006](https://openairdocs.org/sdr/ASOA201702134006), Feb 13, 2017: LIGHT. DISCONNECTED. FLIGHT 4045, THE CREW REPORTED AN OVERHEAD EMERGENCY LIGHT TO BE OUT IN THE AISLE NEAR THE GALLEY. MAINTENANCE INSPECTED THE AIRCRAFT AND RECONNECTED THE AFFECT
- [SDR ASOA201701163003](https://openairdocs.org/sdr/ASOA201701163003), Jan 16, 2017: AXLE. BROKEN. DURING ROUTINE MAINTENANCE, THE RIGHT MAIN LANDING GEAR SHOCK ABSORBER LOWER AXLE WAS FOUND BROKEN. MAINTENANCE REPLACED THE RIGHT SHOCK ABSORBER LOWER AXLE SPE
- [SDR ASOA20150727039C](https://openairdocs.org/sdr/ASOA20150727039C), Jul 27, 2015: INVERTER. INOPERATIVE. DURING ROUTINE MAINTENANCE THE GALLEY EMERGENCY LIGHT WOULD NOT TURN ON. MAINTENANCE REPLACED THE NR 2 AND NR 3 EMERGENCY LIGHT INVERTERS. OPS CHECKS WERE GOOD.
- [SDR ASOA20150506109V](https://openairdocs.org/sdr/ASOA20150506109V), May 5, 2015: BEAM. CORRODED. DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVI
- [SDR ASOA20150506108V](https://openairdocs.org/sdr/ASOA20150506108V), May 5, 2015: FLOOR SUPPORT. CORRODED. DURING C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59-61. MAINTENANCE REMOVED THE CORROSION AND PERFORMED DOUBLER REPAIRS IAW EC5320-
- [SDR ASOA20150506107](https://openairdocs.org/sdr/ASOA20150506107), May 5, 2015: FRAME. CORRODED. DURING C-CHECK, FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15-17L. MAINTENANCE PERFORMED A FRAME SEGMENT SPLICE REPAIR IAW SRM 53-31-04, FIGURE 212. TH
- [SDR ASOA20150428102](https://openairdocs.org/sdr/ASOA20150428102), Apr 28, 2015: SHEAR TIE. CORRODED. DURING C-CHECK SHEAR TIE AT FRAME 68 CARGO DOOR LOWER BEAM HAS CORROSION. REPAIRED SHEAR TIE AT FRAME 68 IAW SRM 53-31-04. ACFT WAS APPROVED FOR RETURN TO SERVI
- [SDR ASOA20130514315T](https://openairdocs.org/sdr/ASOA20130514315T), May 14, 2013: FLOOR SUPPORT. CORRODED. CORROSION AT RT OMEGA BEAM AT NUTPLATE HOLES CORRODED BEYOND LIMITS. R & R HAT SECTION ASSY.
- [SDR ASOA20130514314](https://openairdocs.org/sdr/ASOA20130514314), May 14, 2013: PROFILE. CORRODED. CORROSION AT "T" PROFILE BEYOND LIMITS. R & R T PROFILE LT SIDE AT OMEGA BEAM.
- [SDR ASOA20130514313](https://openairdocs.org/sdr/ASOA20130514313), May 14, 2013: GUSSET. CORRODED. CORROSION AT GUSSET Y=0.00 CORRODED AROUND SCREW HOLES BEYOND LIMITS. R & R GUSSET
- [SDR ASOA20130514312](https://openairdocs.org/sdr/ASOA20130514312), May 14, 2013: GUSSET. CORRODED. CENTER OMEGA BEAM GUSSET HAS CORROSION BEYOND LIMITS. R & R GUSSET.
- [SDR ASOA20130513311](https://openairdocs.org/sdr/ASOA20130513311), May 13, 2013: GUSSET. CORRODED. CORROSION BEYOND LIMITS ON GUSSET. R & R GUSSET.
- [SDR ASOA20130513310](https://openairdocs.org/sdr/ASOA20130513310), May 13, 2013: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.
- [SDR ASOA20130513309](https://openairdocs.org/sdr/ASOA20130513309), May 13, 2013: FLOOR SUPPORT. CORRODED. RT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.
- [SDR ASOA20130513308](https://openairdocs.org/sdr/ASOA20130513308), May 13, 2013: FLOOR SUPPORT. CORRODED. CORROSION BEYOND LIMITS AT FLOOR SUPPORT. R & R FLOOR SUPPORT.
- [SDR ASOA20130513307](https://openairdocs.org/sdr/ASOA20130513307), May 13, 2013: FLOOR SUPPORT. CORRODED. RT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.
- [SDR ASOA20130513306](https://openairdocs.org/sdr/ASOA20130513306), May 13, 2013: SILL. CORRODED. RT SILL CORRODED BEYOND LIMITS. R & R SILL.
- [SDR ASOA20130513305](https://openairdocs.org/sdr/ASOA20130513305), May 13, 2013: SILL. CORRODED. LT SILL CORRODED BEYOND LIMITS. R & R SILL.
- [SDR ASOA20130513304](https://openairdocs.org/sdr/ASOA20130513304), May 13, 2013: SILL. CORRODED. LT SILL CORRODED BEYOND LIMITS. R & R SILL.
- [SDR ASOA20130123005C](https://openairdocs.org/sdr/ASOA20130123005C), Jan 23, 2013: LIGHT. INOPERATIVE. DURING ROUTINE MX, THE LT EXTERNAL AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX REPLACED THE LIGHT ASSY AND OPS CHECKED GOOD.
- [SDR ASOA20121126155](https://openairdocs.org/sdr/ASOA20121126155), Nov 23, 2012: BATTERY. INOPERATIVE. NR 4 BATTERY FOR EMERGENCY LIGHT IN CEILING IS INOPERATIVE. R & R NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20121127158](https://openairdocs.org/sdr/ASOA20121127158), Nov 22, 2012: SKIN. DAMAGED. THE REAR FUSELAGE RT SKIN WAS DAMAGED DURING GROUND OPERATIONS. THE DAMAGE IS LOCATED BETWEEN FRAMES 62 & 63, STR 15R & 17R. REPAIRED DENT WITH FILLER AND DOUBL
- [SDR ASOA20121010091](https://openairdocs.org/sdr/ASOA20121010091), Oct 10, 2012: FMU. FAULTY. CREW REPORTED ENGINE NR 2 STARTED SURGING (ERRATIC ACCEL & DECEL) ON DESCENT BETWEEN FL 260& FL250 N1 SPIKE 45-65 ITT SPIKE BETWEEN 400-600. MX R & R ENGINE NR 
- [SDR ASOA20120827114](https://openairdocs.org/sdr/ASOA20120827114), Aug 27, 2012: LIGHT. MALFUNCTIONED. DURING POSTFLIGHT INSP THE CREW REPORTED THE EMERGENCY LIGHT AT 3BC TO BE INOPERATIVE. THE EMERGENCY LIGHT SYS WAS OPERATIONALLY TESTED WITH NO DEFECTS, AND THE
- [SDR ASOA20120827113](https://openairdocs.org/sdr/ASOA20120827113), Aug 27, 2012: LIGHT. MALFUNCTIONED. DURING PREFLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY LIGHT AT 3BC TO BE INOPERATIVE. MX RESET THE EMERGENCY LIGHT SYS, OPS TESTED WITH NO DEFECTS, AND TH
- [SDR ASOA20120519040R](https://openairdocs.org/sdr/ASOA20120519040R), May 19, 2012: CONTROLLER. FAULTY. CREW REPORTED LOSS OF CABIN PRESSURIZATION AT FL330. CREW MANUALLY DEPLOYED PAX O2 MASK AT 12,100 FT WITH CABIN ALT SHOWING 20,000 FT IAW ENGINEERING INSTRUCTIO
- [SDR ASOA20120121008](https://openairdocs.org/sdr/ASOA20120121008), Jan 21, 2012: UNKNOWN. ODOR. THE CREW REPORTED SEVERE TURBULANCE AT FL360. LOST ABOUT 1000FT, AP DISENGAGED AND THEY ALSO REPORTED A BURNING ODOR FOR ABOUT A MINUTE. MX COMPLIED WITH TURBUL
- [SDR C2XA11RI178](https://openairdocs.org/sdr/C2XA11RI178), Nov 9, 2011: FLASHLIGHT. MELTED. FLT 4154 EWR - CREW REPORTED A ELECTRICAL SMELL NEAR MAIN CABIN DOOR WITH OBSERVATION OF F/A FLASHLIGHT MELTED. EWR MX REMOVED AND REPLACED THE FWD F/A FLASHLIG
- [SDR C2XA11RI176](https://openairdocs.org/sdr/C2XA11RI176), Nov 6, 2011: LIGHT. MALFUNCTIONED. DURING SCHEDULED MAINTENANCE INSPECTION, ROW 12 CEILING EMERGENCY LIGHT WOULD NOT ILLUMINATE. MX RESET SYSTEM AND OPERATIONALLY CHECKED THE LIGHT SUCCESSFULLY I
- [SDR C2XA11CL227](https://openairdocs.org/sdr/C2XA11CL227), Oct 10, 2011: STRUT. WORN. CLE FLT 5850 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL, AND A ENGINE 1/2 REV DISAGREE MESSAGE DURING CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LANDED WI
- [SDR C2XA11CL154](https://openairdocs.org/sdr/C2XA11CL154), Jun 24, 2011: PROXIMITY SWITCH. FAULTY. AVP - FLT 6089 THE CREW REPORTED A LOUD BANGING NOISE FROM UNDER FIRST OFFICER'S FLOOR. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK PROXIMITY SWITCH
- [SDR C2XA11TY080](https://openairdocs.org/sdr/C2XA11TY080), Jun 8, 2011: STRUCTURE. CORRODED. MINOR CORROSION FWD AND AFT OF THE CARGO DOOR SILL. REMOVED CORROSION AND FOUND TO BE SERVICABLE IAW EC5330-01458 ALODINE, PRIMED AND PAINTED IAW EMB 135/145 CP
- [SDR C2XA10RI066](https://openairdocs.org/sdr/C2XA10RI066), May 18, 2010: SWITCH. DEFECTIVE. FLIGHT 2183 - EWR - FLIGHT CREW REPORTED BLEED NR 2 LOW TEMP ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED BLEED
- [SDR C2XA10TY027](https://openairdocs.org/sdr/C2XA10TY027), Feb 12, 2010: LINE. LEAKING. TYS - A/C WAS EN ROUTE TO ATL FROM EWR WHEN A STAB ANTI ICE FAIL MESSAGE SHOWED. CREW DIVERTED TO TYS AND CHANGE PLANES AND CONTINUED. MAINTENANCE FOUND A LINE 
- [SDR C2XA10IA026](https://openairdocs.org/sdr/C2XA10IA026), Jan 18, 2010: CONNECTOR. DEFECTIVE. IAH - DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE OUTSIDE OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH
- [SDR C2XA10RI001](https://openairdocs.org/sdr/C2XA10RI001), Jan 5, 2010: UNKNOWN. ODOR. FLIGHT 2603 - EWR - FLIGHT CREW REPORTED FUEL SMELL IN COCKPIT AFTER APU START. EWR MX PROCEEDED WITH APU OPERATIONAL CHECK BUT COULD NOT DUPLICATE ANY TYPE OF 
- [SDR C2XA09IA204](https://openairdocs.org/sdr/C2XA09IA204), Aug 12, 2009: LIGHT. INOPERATIVE. GSP - FLIGHT 2675 - THE FLIGHT ATTENDANT REPORTED THE PASSENGER READING LIGHT AT 18C STARTED SMOKING MIDWAY THROUGH THE FLIGHT AND WOULD NOT TURN OFF. THE FLIGH
- [SDR C2XA09SH241](https://openairdocs.org/sdr/C2XA09SH241), Aug 1, 2009: SILL. CORRODED. SHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER SILL HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW EMB-145 SRM 5
- [SDR C2XA09SH238](https://openairdocs.org/sdr/C2XA09SH238), Aug 1, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM FRAME 20 CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED AND COMPLETED REPAIR AT CENTER OMEGA BEAM FRAME 20 IAW EMB-145 S
- [SDR C2XA09SH237](https://openairdocs.org/sdr/C2XA09SH237), Aug 1, 2009: FLOOR SUPPORT. CRACKED. SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON LT OMEGA BEAM FACE AND FLANGE BETWEEN FRAMES 20-23 AND CRACKED AT FRAME 22. MAINTENANCE REMOVED AND REPLACED A
- [SDR C2XA09SH183](https://openairdocs.org/sdr/C2XA09SH183), Jun 29, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CK, CENTER OMEGA BEAM HAS CORROSION AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-21-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH182](https://openairdocs.org/sdr/C2XA09SH182), Jun 29, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CK, LT OMEGA BEAM HAS CORROSION BETWEEN FR 20 AND 23. REPAIRED OMEGA BEAM IAW EC 5320-01229. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH181](https://openairdocs.org/sdr/C2XA09SH181), Jun 29, 2009: BEAM. CORRODED. SHV - DURING C-CK, CARGO DOOR LOWER CUTOUT HAS CORROSION. REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETUR
- [SDR C2XA09SH180](https://openairdocs.org/sdr/C2XA09SH180), Jun 29, 2009: BRACKET. DAMAGED. SHV - DURING C-CK, LT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHINGS. REMOVED AND REPLACED LT AILERON PCA ATTACHMENT BRACKET IAW EC 5750-01177. AIRCRA
- [SDR C2XA09SH179](https://openairdocs.org/sdr/C2XA09SH179), Jun 29, 2009: BRACKET. DAMAGED. SHV - DURING C-CK, RT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHINGS. REMOVED AND REPLACED RT AILERON PCA ATTACHMENT BRACKET IAW EC 5750-01177. AIRCRA

All 86: https://openairdocs.org/aircraft/N12540/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/N12540/stcs.md

## Earlier aircraft with N12540

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N12540 before.

- [Cancelled 1980-07-10](https://openairdocs.org/deregistered/N12540-1980-07-10): Cessna 172M, S/N 17262055, built 1973. Owner: [Arizona Sly Blazers Inc](https://openairdocs.org/faa-owner/ARIZONA%20SLY%20BLAZERS%20INC), [Scottsdale, AZ](https://openairdocs.org/faa-place/AZ/Scottsdale)

## 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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