# N655AE: 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: 145452
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 23, 2001
- Certificate issued: October 6, 2011
- Expires: October 31, 2027
- Mode S code: A89F52
- Registered owner: [American Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRLINES%20INC)
- Location: [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth)
- Owner type: Corporation
- Owner's area on the map: 32.8240° N, 97.0491° W: Placed by OpenAirDocs at the center of ZIP code 76155, 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=655AE
- Page: https://openairdocs.org/aircraft/N655AE

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/N655AE/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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB OPS18IA014](https://openairdocs.org/ntsb/OPS18IA014), Jun 27, 2018: Embraer EMB145 (N655AE), Springfield, MO, incident, no damage. Probable cause: The local controller failing to follow established facility directives and issuing a clearance for takeoff from a runway not under his control.

## FAA accident and incident reports

None matched to N655AE.

## Service difficulty reports (198, 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 HNAA2026092100860](https://openairdocs.org/sdr/HNAA2026092100860), Sep 20, 2026: UNKNOWN. ODOR. DURING APP NOTICED OIL/RUBBER BURNING SMELL IN FLT DECK AT ABOUT 2000 FT. PERFORMED E1 & E2 HIGH POWER RUN IAW MAINTENANCE RUNUP CHECKLIST. NO DEFECTS NOTED DUR
- [SDR HNAA2026080400646](https://openairdocs.org/sdr/HNAA2026080400646), Aug 4, 2026: BLEED AIR SYS. LEAKING. CREW NOTIFIED CLT MX OF EXHAUST FUMES IN COCKPIT. CLT MX CREW REPORTED SMELL IN COCKPIT, CABIN NORMAL, FUTHER TROUBLESHOOTING FOUND APU BLEED CAUSE OF FUMES AND
- [SDR HNAA2026072700637](https://openairdocs.org/sdr/HNAA2026072700637), Jul 26, 2026: A/C PACK. ODOR. OIL SMELL IN FLIGHTDECK FROM PACK 1. FACT 27JUL26 01:02 CLT INSPECTED PAX 1. FOUND TO BE GOOD. FOUND PAX 2 TO HAVE MELTED DUCT. REMOVED AND REPLACED DUCT AS REQ
- [SDR HNAA2026052000422](https://openairdocs.org/sdr/HNAA2026052000422), May 4, 2026: SKIN. DAMAGED. COCKPIT UNDERFLOOR HATCH 123BL HAS TOOLING MARK ON EXTERNAL SKIN CLOSE TO THE BLACK RUBBER SEAL. REPAIRED COCKPIT UNDERFLOOR HATCH 123BL TOOLING MARK ON EXTERNA
- [SDR HNAA2026052000421](https://openairdocs.org/sdr/HNAA2026052000421), Apr 22, 2026: FLOOR SUPPORT. CRACKED. LAVATORY RT HAT BEAM AT FR 59-60, CRACK ON FWD END OF NUT-PLATE. PERFORMED DOUBLER REPAIR FOR LAVATORY R/H HAT BEAM AT FR 59-60 IAW ETD2026-145-007317 AND SRM 5
- [SDR HNAA2026052000420](https://openairdocs.org/sdr/HNAA2026052000420), Apr 21, 2026: FRAME. CRACKED. CRACKED FRAME 72, BETWEEN STRINGER 17L AND 16L. R & R FRAME 72 IAW ETD-2026-145-007557 AND EO1-53-26-0206.
- [SDR HNAA2026052000419](https://openairdocs.org/sdr/HNAA2026052000419), Apr 21, 2026: STRINGER SPLICE. CHAFED. STRINGER 19R (INTERIOR STRINGER) STRINGER SPLICE BETWEEN FR 52/53 CHAFED. REMOVED AND REPLACED STGR 19R SPLICE BTW FR 52-53 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026052000406](https://openairdocs.org/sdr/HNAA2026052000406), Apr 21, 2026: STRUCTURE. CORRODED. GALLEY FLOOR, FWD DIGITAL BETWEEN FR 16-17, STGR 18L-19L AROUND NUT PLATE HOLE HAS CORROSION. PERFORMED DOUBLER ON GALLEY FLOOR FWD DIGITAL BETWEEN FR 16-17, ST
- [SDR HNAA2026052000418](https://openairdocs.org/sdr/HNAA2026052000418), Apr 20, 2026: FLOOR SUPPORT. CRACKED. FOUND CRACKS ON LH OMEGA BEAM #2 AT FR 29. PERFORMED CUT-OUT OF DAMAGE, AND DOUBLER REPAIR TO LT OMEGA BEAM #2 AT FR 29 IAW EMB ETD2026-145-007261 AND EO1-53-26
- [SDR HNAA2026052000417](https://openairdocs.org/sdr/HNAA2026052000417), Apr 18, 2026: DOOR FRAME. DAMAGED. MAIN DOOR LOWER FRAME AFT NUTPLATE HOLE DOUBLER HAS NO DTA INFORMATION. REPAIR WAS ACCOMPLISHED IAW ETN-EM-52-041. RE-ACCOMPLISHED DOUBLER FOR REPAIR OF MAIN DO
- [SDR HNAA2026052000416](https://openairdocs.org/sdr/HNAA2026052000416), Apr 17, 2026: DOUBLER. NOT REPORTED. FUSELAGE EXTERNAL SKIN REPAIR DOUBLER BETWEEN FR 35/36 AT STR 1L HAS NO REPAIR INFORMATION. RE-ACCOMPLISHED DOUBLER REPAIR ON FUSELAGE EXTERNAL SKIN BETWEEN FR 
- [SDR HNAA2026052000415](https://openairdocs.org/sdr/HNAA2026052000415), Apr 17, 2026: REPAIR. CHAFED. STRINGER 19R PREVIOUS REPAIR BETWEEN FR 52/53 CHAFED. PERFORMED NEW REPAIR OF STRINGER 19R (2 ANGLE REPAIR) BETWEEN FR 52/53 IAW SRM 53-24-02RE, ITEM 2, FIG 202
- [SDR HNAA2026052000414](https://openairdocs.org/sdr/HNAA2026052000414), Apr 16, 2026: DOUBLER. NOT OPENED. FUSELAGE EXTERNAL SKIN REPAIR DOUBLER BETWEEN FR 70/71 STR 16R/18R HAS NO REPAIR INFORMATION. FABRICATED AND INSTALLED NEW DOUBLER AND FILLER FOR FUSELAGE EXTER
- [SDR HNAA2026052000413](https://openairdocs.org/sdr/HNAA2026052000413), Apr 16, 2026: STRINGER. CRACKED. STGR 2L AT FR-75 HAS A CRACK. PERFORMED SPLICE REPAIR ON STGR 2L AT FR-75 IAW ETD2026-145-007461 AND SRM 51-40-02 AND EO1-53-26-0207.
- [SDR HNAA2026052000405](https://openairdocs.org/sdr/HNAA2026052000405), Apr 16, 2026: SEAT TRACK. CORRODED. LEFT UPPER SEAT TRACK 4 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED LT UPPER SEAT TRACK 4 IAW AMM 53-01-06.
- [SDR HNAA2026052000404](https://openairdocs.org/sdr/HNAA2026052000404), Apr 16, 2026: SEAT TRACK. CORRODED. RIGHT UPPER SEAT TRACK NR 3 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED RT UPPER SEAT TRACK NR 3 IAW AMM 53-01-06.
- [SDR HNAA2026052000403](https://openairdocs.org/sdr/HNAA2026052000403), Apr 15, 2026: GUSSET. CORRODED. LEFT FLOORBEAM GUSSET AROUND NUT-PLATE HOLE BETWEEN FRAME'S 60 AND 61 HAS CORROSION. REMOVED AND INSTALLED NEW LAV LT FLOOR BEAM GUSSET IAW SRM 51-40-02 & SRM 5
- [SDR HNAA2026052000412](https://openairdocs.org/sdr/HNAA2026052000412), Apr 13, 2026: BULKHEAD. DAMAGED. PILOT'S BULKHEAD OTBD UPPER GUIDE PIN HOLE IS ELONGATED. INSTALLED NEW FABRICATED DOUBLER AND SACRIFICIAL PLATE FOR PILOT UPPER OUTBD GUIDE PIN HOLE REPAIR IAW 
- [SDR HNAA2026052000402](https://openairdocs.org/sdr/HNAA2026052000402), Apr 13, 2026: SEAT TRACK. CORRODED. RIGHT INBD SEAT TRACK 2 HAS MULTIPLE CORRODED SPOTS. R & R RT INBD SEAT TRACK 2 IAW AMM 53-01-06.
- [SDR HNAA2026052000401](https://openairdocs.org/sdr/HNAA2026052000401), Apr 13, 2026: SEAT TRACK. CORRODED. RIGHT OTBD SEAT TRACK 1 HAS MULTIPLE CORRODED SPOTS. R & R RT OTBD SEAT TRACK 1 IAW AMM 53-01-06.
- [SDR HNAA2026052000400](https://openairdocs.org/sdr/HNAA2026052000400), Apr 13, 2026: SEAT TRACK. CORRODED. RIGHT INBD SEAT TRACK 1 HAS MULTIPLE CORROSION SPOTS. REMOVED AND REPLACED RT INBD SEAT TRACK 1 IAW AMM 53-01-06.
- [SDR HNAA2026052000399](https://openairdocs.org/sdr/HNAA2026052000399), Apr 13, 2026: FLOORBEAM. CORRODED. LEFT FLOORBEAM SUPPORT LOCATED ON FR35 HAS CORROSION. R & R LT FLOORBEAM SUPPORT LOCATED ON FR35 IAW SRM 51-40-02.
- [SDR HNAA2026052000398](https://openairdocs.org/sdr/HNAA2026052000398), Apr 13, 2026: FLOORBEAM. CORRODED. LH FLOORBEAM SUPPORT LOCATED ON FR25 HAS CORROSION. R & R LH FLOORBEAM SUPPORT AT FR 25 IAW SRM 51-40-02.
- [SDR HNAA2026052000397](https://openairdocs.org/sdr/HNAA2026052000397), Apr 13, 2026: FLOORBEAM. CORRODED. LH FLOOR CROSS SUPPORT LOCATED ON FR28 HAS CORROSION. REMOVED AND REPLACED LH FLOOR CROSS SUPPORT LOCATED ON FR28 IAW EMB 145 SRM 51-40-02
- [SDR HNAA2026052000396](https://openairdocs.org/sdr/HNAA2026052000396), Apr 13, 2026: FLOOR SUPPORT. CORRODED. RIGHT OTBD FLOOR SILL 1 HAS MULTIPLE CORROSION SPOTS. R & R RT OTBD FLOOR SILL 1 IAW SRM 51-40-02, 51-40-09.
- [SDR HNAA2026052000395](https://openairdocs.org/sdr/HNAA2026052000395), Apr 13, 2026: FLOOR SUPPORT. CORRODED. LEFT OTBD FLOOR SILL 3 HAS MULTIPLE CORROSION SPOTS. R & R LT OTBD FLOOR SILL 3 IAW SRM 51-40-02.
- [SDR HNAA2026052000394](https://openairdocs.org/sdr/HNAA2026052000394), Apr 13, 2026: DOOR SILL. CORRODED. GALLEY FLOOR SERVICE DOOR LOWER AFT SILL HAS CORROSION IN MULTIPLE AREAS. PERFORMED DOUBLER REPAIR ON GALLEY FLOOR SERVICE DOOR LOWER AFT SILL IAW EMB-145 SRM 5
- [SDR HNAA2026052000393](https://openairdocs.org/sdr/HNAA2026052000393), Apr 13, 2026: DOOR SILL. CORRODED. GALLEY FLOOR SERVICE DOOR FUSELAGE CUT-OUT LOWER CENTER SILL HAS CORROSION IN MULTIPLE AREAS. GALLEY FLOOR SERVICE DOOR FUSELAGE CUT-OUT LOWER CENTER SILL HAS C
- [SDR HNAA2026052000392](https://openairdocs.org/sdr/HNAA2026052000392), Apr 13, 2026: SEAT TRACK. CORRODED. F118708 L/H UPPER SEAT TRACK #1 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED L/H UPPER SEAT TRACK #1 IAW EMB 145 AMM 53-01-06.
- [SDR HNAA2026052000391](https://openairdocs.org/sdr/HNAA2026052000391), Apr 12, 2026: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SILL 3 HAVE CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED RT FLOOR SILL 3 IAW SRM 51-40-02.
- [SDR HNAA2026052000390](https://openairdocs.org/sdr/HNAA2026052000390), Apr 12, 2026: FLOOR SUPPORT. CORRODED. LEFT FLOOR SILL 4 HAVE CORROSION IN MULTIPLE AREAS. R & R LT FLOOR SILL 4 IAW SRM 51-40-02.
- [SDR HNAA2026052000389](https://openairdocs.org/sdr/HNAA2026052000389), Apr 12, 2026: FLOOR SUPPORT. CORRODED. LEFT FLOOR SILL 6 HAVE CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED LT FLOOR SILL 6 IAW SRM 51-40-02.
- [SDR HNAA2026052000388](https://openairdocs.org/sdr/HNAA2026052000388), Apr 12, 2026: SEAT TRACK. CORRODED. LEFT UPPER SEAT TRACK 5 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED LT UPPER SEAT TRACK 5 IAW AMM 53-01-06.
- [SDR HNAA2026052000387](https://openairdocs.org/sdr/HNAA2026052000387), Apr 12, 2026: SEAT TRACK. CORRODED. RT UPPER SEAT TRACK 4 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED RT UPPER SEAT TRACK 4 IAW AMM 53-01-06.
- [SDR HNAA2026052000408](https://openairdocs.org/sdr/HNAA2026052000408), Apr 11, 2026: SEAT TRACK. CORRODED. LEFT UPPER SEAT TRACK 6 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED LT UPPER SEAT TRACK 6 IAW AMM 53-01-06.
- [SDR HNAA2026052000386](https://openairdocs.org/sdr/HNAA2026052000386), Apr 11, 2026: FLOOR SUPPORT. CORRODED. LEFT FLOOR SILL 7 AROUND NUT-PLATES HOLES HAVE CORROSION. REMOVED AND REPLACED LT FLOOR SILL 7 IAW SRM 51-40-02.
- [SDR HNAA2026052000411](https://openairdocs.org/sdr/HNAA2026052000411), Apr 10, 2026: SHEAR TIE. CRACKED. F118310 CARGO SHEAR CLIP AT FR-65 BETWEEN STGRS 6L/7L HAS CRACK. REMOVED AND INSTALLED NEW CARGO SHEAR CLIP AT FR-65 BETWEEN STGRS 6L/7L IAW EMB-145 SRM 51-40-0
- [SDR HNAA2026052000410](https://openairdocs.org/sdr/HNAA2026052000410), Apr 10, 2026: SHEAR TIE. CORRODED. CARGO DOOR FUSELAGE CUT-OUT FR-65 SHEAR CLIP ABOVE LWR CENTER SILL IS CORRODED. RE-ACCOMPLISHED CARGO DOOR FUSELAGE CUT-OUT FR-65 SHEAR CLIP SPLICE PATCH REPAIR
- [SDR HNAA2026052000409](https://openairdocs.org/sdr/HNAA2026052000409), Apr 10, 2026: HINGE FITTING. WORN. RUDDER I UPPER HINGE ATTACHMENT FITTING TRIANGLE FITTING ATTACHMENT TANGS WORN. REMOVED AND REPLACED WORN RUDDER I UPPER HINGE ATTACHMENT FITTING/ TRIANGLE FITT
- [SDR HNAA2026052000407](https://openairdocs.org/sdr/HNAA2026052000407), Apr 10, 2026: DOOR SILL. CORRODED. CARGO DOOR FUSELAGE CUT-OUT LWR CENTER SILL IS CORRODED. REMOVED AND REPLACED CARGO DOOR FUSELAGE CUT-OUT LWR CENTER SILL IAW SRM 51-40-02.
- [SDR HNAA2026052000429](https://openairdocs.org/sdr/HNAA2026052000429), Apr 9, 2026: YOKE. CRACKED. RIGHT ENGINE YOKE LOWER FWD FITTING HAS A POSSIBLE CRACK. REMOVED AND REPLACED CRACKED RT ENGINE YOKE LOWER FWD FITTING IAW PDT FCD1-54-21-0017 REV D.
- [SDR HNAA2026052000428](https://openairdocs.org/sdr/HNAA2026052000428), Apr 8, 2026: SKIN. SCRATCHED. RUDDER 2 RH EXTERNAL SKIN HAS A DEEP SCRATCH. PERFORMED DOUBLER REPAIR ON RUDDER 2 RH EXTERNAL SKIN IAW ETD2026-145-006765 AND EO1-55-26-0208.
- [SDR HNAA2026052000427](https://openairdocs.org/sdr/HNAA2026052000427), Apr 7, 2026: SKIN. DAMAGED. POSSIBLE LIGHTNING STRIKE ON FUSELAGE EXTERNAL SKIN AT FR 37-38, STRG 6R-7R. PERFORMED DRILL OUT OF LIGHTNING STRIKE AREA AND REPAIRED WITH SOLID BUTTON HEAD RI
- [SDR HNAA2026052000426](https://openairdocs.org/sdr/HNAA2026052000426), Apr 7, 2026: SKIN. DAMAGED. POSSIBLE LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN FR33-34, STRG 5R-6R. PREPPED PRIMED AND PAINTED FUSELAGE SKIN FR 33-34, STRG 5R-6R IAW EMB 145 CPM 51-21-05 
- [SDR HNAA2026052000425](https://openairdocs.org/sdr/HNAA2026052000425), Apr 7, 2026: SKIN. DAMAGED. POSSIBLE LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN FR-25-26, STRG 6R-7R. PERFORMED RIVET AND WASHER IN AFFECTED HOLE ON EXTERNAL FUSELAGE SKIN BTW FR 25-26 AND
- [SDR HNAA2025052000424](https://openairdocs.org/sdr/HNAA2025052000424), Apr 7, 2026: DRAG ANGLE. CRACKED. RIGHT VERTICAL STABILIZER DRAG ANGLE HAS POSSIBLE CRACK AT FRAME 78. REMOVED AND REPLACED RT VERTICAL TO FUSELAGE DRAG ANGLE IAW SRM 51-40-02.
- [SDR HNAA2026052000423](https://openairdocs.org/sdr/HNAA2026052000423), Apr 6, 2026: SKIN. DENTED. FUSELAGE SKIN BETWEEN FR-06/07 AND STGRS-14L/15L HAS A DENT. INSTALLED REPAIR DOUBLER & FILLER ON FUSELAGE SKIN BETWEEN FR-06/07 AND STGRS-14L/15L IAW SRM 53-12
- [SDR HNAA2025092300637](https://openairdocs.org/sdr/HNAA2025092300637), Sep 22, 2025: HYDRAULIC LINE. LEAKING. ENGINE HYD 1 PUMP FAIL & HYD 1 LOW QTY. PERFORMED GVI INSPECTION ENG #1 DUE TO SUSPECTED ENG #1 HYD LEAD. FOUND ABUNDACE OF HYD FLUID IN COWLING. SUSPECTED HYD 
- [SDR HNAA2025050700306](https://openairdocs.org/sdr/HNAA2025050700306), May 6, 2025: FUEL NOZZLE. FAULTED. HUNG START ON NO.2 FOLLOWED BY FUEL SMELL IN A/C. PERFORMED GVI OF ENG 2 NO OBVIOUS DEFECTS NOTED OTHER THAN POOLED FUEL. DRY MOTORED ENG TO CLEAR OUT FUEL. DUR
- [SDR HNAA2025041400202](https://openairdocs.org/sdr/HNAA2025041400202), Apr 13, 2025: FUSE. LEAKING. HYD 2 QTY IS EMPTY. HYD 2 WAS FULL AT PUSH BACK EMPTY BY GATE RETURN. FOUND #400 HYDRAULIC FUSE LEAKING. R&R #400 HYDRAULIC FUSE IAW AMM 32-41-07. LEAK CHECK AN

All 198: https://openairdocs.org/aircraft/N655AE/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/N655AE/stcs.md

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