# Embraer EMB-145

- Type: Aircraft model (FAA registry)
- Registry code: 3260210
- Manufacturer (registry): EMBRAER
- Model: EMB-145
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-jet
- Seats: 55
- Weight class: 12,500 to 19,999 lb
- Certification: Type certificated
- Data sheet: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (OpenAirDocs)
- Holder: Embraer S.A.
- Registered aircraft: 7
- Page: https://openairdocs.org/model/embraer-emb-145

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [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 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 2007-04-09](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 2006-25-07](https://openairdocs.org/ad/2006-25-07): Fuel quantity indication system (FQIS) wire harness and the direct current (DC) fuel pump wire harness · Embraer EMB-135ER, EMB-135KE, EMB-145 and 4 more. Effective Jan 16, 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
- [AD 2004-25-21](https://openairdocs.org/ad/2004-25-21): Pitch trim system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 26, 2005

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 2005-25-04](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 2005-08-02](https://openairdocs.org/ad/2005-08-02) (historical): Electric fuel pumps · Embraer - Empresa Brasileira de Aeronautica EMB-135 Series (all) and EMB-145 Series (all). Effective May 19, 2005
- [AD 2004-09-15](https://openairdocs.org/ad/2004-09-15) (historical): Nose Landing Gear Wheel Nuts and Associated Inner and Outer Seals and Reidentify Landing Gear Strut · Embraer - Empresa Brasileira de Aeronautica EMB-135 Series (all) and EMB-145 Series (all). Effective Jun 9, 2004
- [AD 2003-09-03](https://openairdocs.org/ad/2003-09-03) (historical): Cartridge flange · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 3 more. Effective May 14, 2003
- [AD 2002-16-06](https://openairdocs.org/ad/2002-16-06) (historical): Auxiliary power unit (APU) · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 2 more. Effective Aug 27, 2002
- [AD 2002-08-21](https://openairdocs.org/ad/2002-08-21) (historical): Bonding Jumpers that Connect the Horizontal Stabilizer to the Vertical Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 2 more. Effective May 16, 2002
- [AD 2002-08-18](https://openairdocs.org/ad/2002-08-18) (historical): Actuator Clutches of the Primary and Backup Pitch Trim Systems of the Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 2 more. Effective May 16, 2002
- [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 2001-17-03](https://openairdocs.org/ad/2001-17-03) (historical): Engine Thrust Reverser Stow/Transit Switches · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Sep 5, 2001
- [AD 2001-10-15](https://openairdocs.org/ad/2001-10-15) (historical): Fire Extinguisher Bottles · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Jun 8, 2001
- [AD 2001-10-01](https://openairdocs.org/ad/2001-10-01) (historical): Airplane Flight Manuals--APU Start/Stop Switch Panel · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective May 29, 2001
- [AD 2000-19-03](https://openairdocs.org/ad/2000-19-03) (historical): Fuel System Tubing · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 1 more. Effective Oct 3, 2000
- [AD 2000-19-02](https://openairdocs.org/ad/2000-19-02) (historical): Electric Fuel Pumps · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Oct 3, 2000
- [AD 2000-13-02](https://openairdocs.org/ad/2000-13-02) (historical): Precooler Differential Pressure Switches · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Jul 3, 2000
- [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 99-11-01](https://openairdocs.org/ad/99-11-01) (historical): Bleed Air Check Valve · Embraer - Empresa Brasileira de Aeronautica EMB-145 Series (all). Effective Jun 2, 1999
- [AD 99-05-04](https://openairdocs.org/ad/99-05-04) (historical): Aileron Power Control Actuator (PCA) Rod Ends · Embraer - Empresa Brasileira de Aeronautica EMB-145 Series (all). Effective Mar 29, 1999
- [AD 99-01-12](https://openairdocs.org/ad/99-01-12) (historical): Pitch Trim System · Embraer - Empresa Brasileira de Aeronautica EMB-145 Series (all). Effective Feb 2, 1999
- [AD 98-13-34](https://openairdocs.org/ad/98-13-34) (historical): Test NLG For Extension (Free-Fall) Function · Embraer - Empresa Brasileira de Aeronautica EMB-145 Series (all). Effective Jul 9, 1998

All 118: https://openairdocs.org/model/embraer-emb-145/ads.md

## Information bulletins (advisory) (10)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 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 NM-04-55](https://openairdocs.org/saib/NM-04-55): . Issued Mar 8, 2004

## Registered aircraft (7)

- [N47VA](https://openairdocs.org/aircraft/N47VA): [Advanced Air LLC](https://openairdocs.org/faa-owner/ADVANCED%20AIR%20LLC), [Statesville, NC](https://openairdocs.org/faa-place/NC/Statesville), built 1999, S/N 145110
- [N607AE](https://openairdocs.org/aircraft/N607AE): [American Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRLINES%20INC), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth), built 1998, S/N 145064
- [N610AE](https://openairdocs.org/aircraft/N610AE): [American Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRLINES%20INC), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth), built 1998, S/N 145073
- [N611AE](https://openairdocs.org/aircraft/N611AE): [American Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRLINES%20INC), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth), built 1998, S/N 145074
- [N612AE](https://openairdocs.org/aircraft/N612AE): [American Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRLINES%20INC), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth), built 1998, S/N 145079
- [N613AE](https://openairdocs.org/aircraft/N613AE): [American Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRLINES%20INC), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth), built 1998, S/N 145081
- [N697EE](https://openairdocs.org/aircraft/N697EE): [Embraer Executive Aircraft Inc](https://openairdocs.org/faa-owner/EMBRAER%20EXECUTIVE%20AIRCRAFT%20INC), [Melbourne, FL](https://openairdocs.org/faa-place/FL/Melbourne), S/N 145-1197

## 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 CEN11IA369](https://openairdocs.org/ntsb/CEN11IA369), Jun 3, 2011: Embraer EMB-145 (N607AE), Chicago, IL, incident, no damage. Probable cause: The overheat and failure the brake during landing due to oxidation of the brake rotors, which went undetected by maintenance personnel. Contributing to the accident was maintenance personnel’s lack…

## FAA accident and incident reports (11)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20230112002849I](https://openairdocs.org/incident/20230112002849I), Jan 12, 2023: Embraer EMB-145 (N613AE), Little Rock, AR, Minor damage. Little Rock tower reports, Little Rock, AR (lit):[privacy data omitted], E145, lit-ord, blew a tire during departure RWY4R. Arpt ops recovered tire FOD from…
- [Incident 20201020020109I](https://openairdocs.org/incident/20201020020109I), Oct 20, 2020: Embraer EMB-145 (N607AE), Mosinee, WI, No damage. On 10/20/2020, eny 3541 completed a stable approach (RNAV rwy 35) to kcwa, WI. Weather was 400 feet overcast, 1 mile visibility, light snow. The runway…
- [Incident 20151228021119I](https://openairdocs.org/incident/20151228021119I), Dec 28, 2015: Embraer EMB-145 (N612AE), Montreal, PO, Minor damage. On climb from yul encountered bird strike at 3000FT on left side of aircraft nose. Inflight evaluation of aircraft handling and performance revealed no adverse…
- [Incident 20110603009499I](https://openairdocs.org/incident/20110603009499I), Jun 3, 2011: Embraer EMB-145 (N607AE), Chicago, IL, No damage. On 06/03/11, anerican eagle airlines, inc., aircraft N607AE, operating as flight 4176 from cmh to ord, landed ord on runway 22 right at approximately 0610. The…
- [Incident 20050813018169I](https://openairdocs.org/incident/20050813018169I), Aug 13, 2005: Emb EMB145LR (N260SK), Coraopolis, PA. (-23) Aircraft diverted and landed on runway 28R after reporting a problem with the number 2 engine. No evacuation reported, no injuries reported.
- [Incident 20030604011999I](https://openairdocs.org/incident/20030604011999I), Jun 4, 2003: Emb EMB145 (N260SK), Boston, MA. (-23) Date: June 4, 2003 Logan international airport Boston ma (bos) 10:30 EDT ASI: donald e. small N260SK dornier Emb-145-145 s/n 3145128 FSDO-01 Wednesday…
- [Incident 20020131001039I](https://openairdocs.org/incident/20020131001039I), Jan 31, 2002: Emb EMB145 (N265SK), Boston, MA. (-23) On climb out, aircraft N265SK, Emb-145-145, s/n 145226, went into an uncontrollable vertical climb. Aircraft pitched up to 6300 ft. with run-away trim.…
- [Incident 20010703015319I](https://openairdocs.org/incident/20010703015319I), Jul 3, 2001: Emb EMB145 (N607AE), Pittsburgh, PA. (-23) July 03, 2001, at 2045 EST, American eagle flight #4039, an Emb 145, landed on runway 28R after the number 2 engine was shut down for unknown reasons.…
- [Incident 20010104002909I](https://openairdocs.org/incident/20010104002909I), Jan 4, 2001: Emb EMB145 (N260SK), Newburgh, NY. (-23) Flight 4857 was inbound to lga and a flap fail message illuminated the flight diverted to ewr and landed without incident. Maintenance from lga replaced…
- [Incident 20000713035089I](https://openairdocs.org/incident/20000713035089I), Jul 13, 2000: Emb EMB145 (N265SK), Pittsburgh, PA. (-23)On July 13, 2000, at 1035E, chqa flight 4870, an Emb-145, registered as N265SK, S/N145-226, diverted to "pit" after the "in flight" shutdown of the #1…
- [Accident 19980211006759A](https://openairdocs.org/incident/19980211006759A), Feb 11, 1998: Emb EMB145 (N14931), Beaumont Port A, TX, Substantial damage. Retarted throttle at V1 for student test. Airborne. Wing hit runway Emb cartwheeled. Rescue crew put out fuel fire. (-23) this flight was a…

## Service difficulty reports (3,003, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR OEJA2025082900001](https://openairdocs.org/sdr/OEJA2025082900001), Aug 27, 2025: WARNING MESSAGE. ILLUMINATED. ON CLIMB OUT HEADING TOWARDS 25,000 FT A PACK 2 VAILVE FAIL CAS MESSAGE APPEARED , WHE THE AIRCRAFT REACHED 25,000 THE CABIN BEGAN TO RAPIDLY RISE. CREW PERFORM
- [SDR KY72024F00006](https://openairdocs.org/sdr/KY72024F00006), Jun 9, 2024: SENSOR. DEFECTIVE. BLEED1 OVERTEMP IN FLIGHT ATB. REMOVED & REPLACED #1 HIGH TEMP THERMOSTAT 36-11-06, OPS CHECK GOOD.
- [SDR OEJA2023100900915](https://openairdocs.org/sdr/OEJA2023100900915), Oct 5, 2023: UNKNOWN. UNKNOWN. DEPARTING OMAHA, NEBRASKA KOMA FOR MCALLEN TEXAS KMFE THURSDAY AFTERNOON AT 2200Z, IMMEDIATELY AFTER TAKEOFF DURING CLIMB-OUT A SERVICE DOOR OPN FUEL DOOR INDIC
- [SDR OEJA202301100026](https://openairdocs.org/sdr/OEJA202301100026), Jan 8, 2023: CONTROL BOX. FAILED. UPON APPROACH IN TO KDRO WE STARTED TO CONFIGURE THE AIRCRAFT FOR LANDING. WHEN WE PUT THE FLAPS TO 9 WE RECEIVED A FLAPS FAIL CAUTION. WE THEN VECTORED AROUN A
- [SDR SIMA20221031004](https://openairdocs.org/sdr/SIMA20221031004), Oct 31, 2022: LIGHT. UNSERVICEABLE. DURING PS-1 CHECK FOUND EXTERNAL EMERGENCY LIGHT RH OVERWING INOP-C/A-RAR EXTERNAL EMERGENCY LIGHT ASSEMBLY RH OVERWING IAW EMB 145 AMM 33-50-10, OPS CHECK GOOD
- [SDR 9JLA2022031430862](https://openairdocs.org/sdr/9JLA2022031430862), Feb 21, 2022: PCB. DEFECTIVE. THE FLIGHT CREW REPORTED THAT PRIOR TO TAXI THE 3 LEFT DISPLAY SCREENS ALL DISPLAYED RED X. THE MAINTENANCE TEAM DETERMINE THE IC-600 CARD WAS DEFECTIVE. THE CA
- [SDR 9JLA2021110324848](https://openairdocs.org/sdr/9JLA2021110324848), Oct 23, 2021: POWER UNIT. DEFECTIVE. THE FLIGHT CREW REPORTED OF A "GEN 1 BEARING FAIL" ADVISORY MESSAGE DISPLAYED ON THE EICAS SYSTEM. OPERATIONS WERE CONTINUED PER MEL. THE MAINTENANCE VENDOR DET
- [SDR SIMA20210701001](https://openairdocs.org/sdr/SIMA20210701001), Jul 1, 2021: BATTERY PACK. INOPERATIVE. ROWS 8-12 EMERGENCY LIGHTS INOP-C/A-T/S IAW EMB FIM 33-50-00-810-804-A. FOUND #3 BATTERY BAD. RAR #3 BATTERY AND CHARGER IAW ENVOY W/C 33-700-19. OPS CHECK GOOD
- [SDR SIMA20210517004](https://openairdocs.org/sdr/SIMA20210517004), May 17, 2021: CONTROL MODULE. FAULTED. EMERGENCY LIGHT NOT ARMED CAUTION ON EICAS W/ EMERG LT SWITCH ARMED TRIED CYCLING MULTIPLE TIMES"TRANSFERRED TO NRWC 610-ORD-03512" GR 417418-C/A-RAR CONTROL MO
- [SDR KY7A20210503002](https://openairdocs.org/sdr/KY7A20210503002), May 3, 2021: A/C PACK. MALFUNCTIONED. CREW REPORTED ON CLIMB OUT OF MSP THEY RECEIVED A PACK 1 FAIL CAS MESSAGE. WHEN TRYING TO RESET PACK 1, PACK 2 FAILED. WHILE TRYING TO RESET BOTH PACKS THEY NOT
- [SDR SIMA20210417003](https://openairdocs.org/sdr/SIMA20210417003), Apr 17, 2021: BULB. INOPERATIVE. LEFT HAND OVER WING EMERGANCY LIGHT INOP-C/A-REMOVED AND REPLACED LEFT HAND OVER WING EMERGANCY LIGHT BULB IAW AMM 33-50-10. OPERATIONAL CHECK GOOD.
- [SDR SIMA20210330001](https://openairdocs.org/sdr/SIMA20210330001), Mar 30, 2021: LAMP. INOPERATIVE. AFT EMERGENCY LIGHT CEILING LIGHT INOP-C/A-RAR AFT EMERGENCY LIGHT CEILING LIGHT LAMP IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.
- [SDR 9JLA2021022524810](https://openairdocs.org/sdr/9JLA2021022524810), Feb 14, 2021: GENERATOR. DEFECTIVE. THE FLIGHT CREW REPORTED THAT DURING FLIGHT THE GEN 2 BEARING FAIL EICAS MESSAGE ILLUMINATED. THE MAINTENANCE VENDOR DETERMINED THAT NO2 DC GEN WAS DEFECTIVE. T
- [SDR 9JLA2021022529157](https://openairdocs.org/sdr/9JLA2021022529157), Feb 14, 2021: PRESSURE SWITCH. DEFECTIVE. THE FLIGHT CREW REPORTED THAT DURING FLIGHT WITH HYDRAULIC SYSTEM ON NO1 RUDDER SYSTEM CAUTION ILLUMINATED ON EICAS. THE MAINTENANCE VENDOR TROUBLESHOT AND DETE
- [SDR SIMA20210125002](https://openairdocs.org/sdr/SIMA20210125002), Jan 25, 2021: STRUCTURE. CRACKED. THE COCKPIT RT DIAGONAL CEILING MEMBER IS CRACKED JUST FORWARD OF THE SPEAKER, AS MARKED. C/A: R & R COCKPIT RT DIAGONAL CEILING MEMBER, IAW EMB 145 SRM 51-40-0
- [SDR SIMA20210125003](https://openairdocs.org/sdr/SIMA20210125003), Jan 25, 2021: FAN. ODOR. BRIEFLEY ON TAKEOFF AND INTERMITTENTLY IN FLIGHT AN ODD SMELL WOULD COME UP IN THE COCKPIT/CABIN SMELL WAS SIMILAR TO ELECTRICAL BURNING. TRANSFERRED TO NRWC 61
- [SDR SIMA20210111001](https://openairdocs.org/sdr/SIMA20210111001), Jan 11, 2021: BULB. INOPERATIVE. RT OVERWING EXIT AFT EMERGENCY LIGHT INOPERABLE. C/A: REMOVED AND INSTALLED LIGHT BULB, IAW EMB AMM 33-50-10. OPERATIONS CHECK GOOD.
- [SDR SIMA20210105003](https://openairdocs.org/sdr/SIMA20210105003), Jan 5, 2021: YOKE. CRACKED. DURING IMBV INSPECTION, QC FOUND RT PYLON FWD LOWER YOKE FITTING CRACKED. C/A: REMOVED AND REPLACED RT FWD LOWER YOKE FITTING, IAW ERS-EM-54MR-698.
- [SDR SIMA20210101002](https://openairdocs.org/sdr/SIMA20210101002), Jan 1, 2021: LAMP. INOPERATIVE. CABIN AFT AISLE EMERGENCY LIGHT INOPERABLE. C/A: REMOVED AND REPLACED AFT AISLE EMERGENCY LIGHT LAMP, IAW EMB 145 AMM 33-50-08. OPERATIONAL CHECK GOOD.
- [SDR SIMA20201223003](https://openairdocs.org/sdr/SIMA20201223003), Dec 23, 2020: FLOOR SUPPORT. CORRODED. LT OMEGA BEAM AT FRAME 20 PREVIOUS REPAIR IS CORRODED. C/A: REACCOMPLISHED REPAIR ON LT OMEGA BEAM AT FRAME 20, IAW EMB 145 SRM 53-00-10RE.
- [SDR SIMA20201221002](https://openairdocs.org/sdr/SIMA20201221002), Dec 21, 2020: SUPPORT. CORRODED. TOILET WASTE VALVE SUPPORT EXTERIOR HAS CORROSION. C/A: REMOVED AND REPLACED THE TOILET WASTE VALVE SUPPORT, IAW EMB 145 SRM 51-40-02.
- [SDR SIMA20201220007](https://openairdocs.org/sdr/SIMA20201220007), Dec 20, 2020: SPAR. CRACKED. LT WING SPAR I CRACKED AT RIB 9. CRACK LENGHT 0.3 NUMBER OF CRACKS 1. C/A: ACCOMPLISHED PERMANENT REPAIR ON LT WING SPAR I AT RIB 9, IAW EMB 145 SRM 57-20-05 IT
- [SDR SIMA20201220001](https://openairdocs.org/sdr/SIMA20201220001), Dec 20, 2020: SKIN. CHAFED. CARGO DOOR INTERNAL LOWER SKIN CHAFED AT VB5 BETWEEN HB4 AND HB3. C/A: REMOVED PREVIOUS REPAIR DOUBLER AND FABRICATED AND INSTALLED A NEW DOUBLER, IAW EMB 145 S
- [SDR SIMA20201220003](https://openairdocs.org/sdr/SIMA20201220003), Dec 20, 2020: SKIN. CHAFED. CARGO DOOR INTERNAL LOWER SKIN CHAFFED AT HB4 APPROXIMATELY 2' FROM FWD EDGE. C/A: REMOVED PREVIOUS REPAIR DOUBLER AND FABRICATED AND INSTALLED A NEW DOUBLER ON
- [SDR SIMA20201220002](https://openairdocs.org/sdr/SIMA20201220002), Dec 20, 2020: SKIN. CHAFED. CARGO DOOR INTERNAL LOWER SKIN CHAFED BETWEEN HB3 AND HB2. C/A: REMOVED PREVIOUS REPAIR DOUBLER AND FABRICATED AND INSTALLED A NEW DOUBLER ON CARGO DOOR LOWER I
- [SDR HNAA2020121200360](https://openairdocs.org/sdr/HNAA2020121200360), Dec 10, 2020: STARTER GEN. MALFUNCTIONED. APU GEN OFF BUS MESSAGE APPEARED ON EICAS WITH CLICKING NOISE AND ELECTRICAL BURNING SMELL IN COCKPIT. RESTARTED APU WITH GEN OFF NO SMELL NOTED OR CB S POPPED.
- [SDR SIMA20201105002](https://openairdocs.org/sdr/SIMA20201105002), Nov 5, 2020: LAMP. INOPERATIVE. DURING PS-2 CHECK FOUND RIGHT HAND CENTER FAIRING EMERGENCY LIGHT OUT. C/A: R & R RT CENTER FAIRING EMERGENCY LIGHT LAMP, IAW EMB AMM 33-50-10. OPERATIONS CHECK
- [SDR SIMA20200921001](https://openairdocs.org/sdr/SIMA20200921001), Sep 21, 2020: LAMP. INOPERATIVE. RT AFT OVERWING EMERGENCY LIGHT INOP. C/A: R & R RT AFT OVERWING EMERGENCY LAMP, IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD, IAW EMB 145 AMM 33-50-00.
- [SDR SIMA2020060130002](https://openairdocs.org/sdr/SIMA2020060130002), May 30, 2020: SUPPORT. CORRODED. DURING MBV INSPECTION, QC FOUND THE TOILET WASTE VALVE SUPPORT CORRODED. REMOVED AND REPLACED THE TOILET WASTE VALVE SUPPORT IAW SRM 51-40-02.
- [SDR SIMA2020060130001](https://openairdocs.org/sdr/SIMA2020060130001), May 30, 2020: SPAR. CRACKED. DURING MBV INSPECTION, QC FOUND THE RT WING SPAR 1 CRACKED AT A PREVIOUS REPAIR AT RIB 9. REPAIRED RT WING SPAR 1 AT RIB 9 IAW SRM 57-20-05-RE ITEM 3.
- [SDR SIMA2020060219002](https://openairdocs.org/sdr/SIMA2020060219002), May 19, 2020: BRACKET. CRACKED. FORWARD CARGO DOOR TORSION BAR BRACKET AT FRAME 61 HAS A 1/8" CRACK. INSTALLED NEW BRACKET IAW SRM 51-40-02.
- [SDR SIMA2020042018001](https://openairdocs.org/sdr/SIMA2020042018001), Apr 18, 2020: STRUCTURE. CRACKED. SMALL CRACK IN SHEET METAL WHERE LH NLG FORWARD HINGE ASSEMBLY PASSES THROUGH TO ATTACHMENT POINT.-C/A-REPAIRED LH NLG DOOR FORWARD HINGE ASSY PASS THROUGH POIN
- [SDR SIMA20200416002](https://openairdocs.org/sdr/SIMA20200416002), Apr 16, 2020: FRAME. CHAFED. FR 59 LH IS CHAFFED AT THE OVER HEAD BIN ATTACHMENT ARM NEAR STR. 5 LH.-C/A-REPAIRED SRM 53-00-04. CHAFE DAMAGE ASSIGNED DT-EM-53-1299.
- [SDR ASOA202004147036](https://openairdocs.org/sdr/ASOA202004147036), Apr 13, 2020: FLAP. DELAMINATED. L/H I/B FLAP HAS AREAS OF DELAMINATION ON TRAILING EDGE. REPAIRED DELAMINATION IAW EA12-2020-055. FLAP WAS RETURNED TO STOCK.
- [SDR ASOA202004027033](https://openairdocs.org/sdr/ASOA202004027033), Apr 2, 2020: DOOR SILL. CORRODED. CARGO DOOR CUT-OUT SILL HAS CORROSION. REMOVED AND REPLACED CARGO DOOR CUT-OUT SILL. AIRCRAFT STILL IN C CHECK.
- [SDR SIMA2020042030004](https://openairdocs.org/sdr/SIMA2020042030004), Mar 30, 2020: SKIN. CRACKED. BAGGAGE DOOR SKIN HAS A CRACK JUST UNDER THE OPEN/CLOSE HANDLE. (CRACK APPROX 1 " LONG)-C/A-C/W ERS-EM-52MR-1073 BAGGAGE DOOR CARGO DOOR HANGLE CUTOUT CRACK PER
- [SDR SIMA2020041625008](https://openairdocs.org/sdr/SIMA2020041625008), Mar 25, 2020: SUPPORT ANGLE. CRACKED. RH WING-TO-FUSELAGE LOWER SUPPORT ANGLE #2 IS CRACKED ON THE FWD END. UP TO THE 1ST RIVET, AND IS APPROX 3/8" LONG. -C/A-C/W REPLACEMENT OF #2 RH WING TO FUSELA
- [SDR SIMA2020041625007](https://openairdocs.org/sdr/SIMA2020041625007), Mar 25, 2020: FRAME. CRACKED. CARGO BAY UNDER FLOOR FRAME IS CRACKED AT FR 72 LH AND STR.16 LH. -C/A-REPAIRED FRAME 72 IAW ERS-EM-53MR-4094.
- [SDR SIMA2020041618005](https://openairdocs.org/sdr/SIMA2020041618005), Mar 18, 2020: STRUCTURE. CORRODED. TDMI 607T5323 ORIGNAL LG PG 4475656/3 TRANSFERRED FROM NRTC E710113, COCKPIT UNDERFLOOR BETWEEN FRAMES 13 AND 14 AND STRINGERS 20R AND 18L HAS SURFACE CORROSION
- [SDR ASOA202001287014](https://openairdocs.org/sdr/ASOA202001287014), Jan 27, 2020: NUT PLATE. CORRODED. MAIN DOOR BOTTOM NUTPLATE CUTOUT HOLES HAVE CORROSION. BLENDED AND TREATED NUTPLATE HOLES ON BOTTOM OF MAIN DOOR, REPAIRED AFT MOST NUTPLATE HOLE BY CUTTING OUT
- [SDR SIMA201911298002](https://openairdocs.org/sdr/SIMA201911298002), Nov 28, 2019: LAMP. INOPERATIVE. ROW 12 B/C OVERHEAD EMERGENCY LIGHT INOP-C/A-RAR ROW 12 B/C OVERHEAD EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECK GOOD.
- [SDR RAIA201909100001](https://openairdocs.org/sdr/RAIA201909100001), Sep 10, 2019: SKIN. CRACKED. FUSLAGE SKIN UNDER AFT DRAIN MAST CRACKED AND HAS HOLE. REPAIR INFORMATION ATTACHED TO SUPPLIMENTAL E-MAIL SENT TO 9-AMC-AFS-SDR@FAA.GOV.
- [SDR ASOA20190415052](https://openairdocs.org/sdr/ASOA20190415052), Apr 10, 2019: BULB. INOPERATIVE. DURING MX INSPECTION THE EMERGENCY LIGHT OVER SEAT 18A WAS INOP. MX REMOVED AND REPLACED THE BULB WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201902197029](https://openairdocs.org/sdr/ASOA201902197029), Feb 16, 2019: HINGE FITTING. WORN. R/H AND L/H VERTICAL STAB HINGE FITTING BORES WORN TO LIMITS. REAMED R/H AND L/H BORES AND INSTALLED BEARINGS. AIRCRAFT STILL IN C CHECK.
- [SDR ASOA201901307023](https://openairdocs.org/sdr/ASOA201901307023), Jan 30, 2019: YOKE. CRACKED. NR 1 ENGINE FORWARD YOKE, LOWER FORWARD FITTING CRACKED ON RADIUS EDGE. REMOVED AND REPLACED YOKE FITTING. AIRCRAFT STILL IN C CHECK.
- [SDR HNAA2019012300026](https://openairdocs.org/sdr/HNAA2019012300026), Jan 22, 2019: VALVE. MALFUNCTIONED. PDIS 632 36-10 1856433 22JAN19 PHL CLOSE HS VLV 2 FAIL EICAS MSG DURING TAKE OFF ROLL HISTORY: FACT 22JAN19 20:17 PHL TROUBLESHOT WITH FIM 36-11-00-810-810-A UP
- [SDR ASOA2018111217184](https://openairdocs.org/sdr/ASOA2018111217184), Nov 21, 2018: SKIN. GOUGED. GOUGES ON MAIN DOOR EXTERNAL SKIN AT PREVIOUS REPAIR. CUT-OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER & DOUBLER. AIRCRAFT STILL IN C CHECK.
- [SDR ASOA2018101515246](https://openairdocs.org/sdr/ASOA2018101515246), Oct 11, 2018: LIGHT. ARCED. FLT 4096 MKE-EWR PILOT REPORTED "STRONG ELECTRICAL SMELL DURING CRUISE FLIGHT. SMELL INIDENTIFIED 1 MIN DURATION THEN DISSIPATED". MX RELAMPED 4 EACH CEILING AN
- [SDR HNAA2018100300241](https://openairdocs.org/sdr/HNAA2018100300241), Oct 2, 2018: UNKNOWN. ODOR. PDIS 665 05-52 1743622 02OCT18 PHL CLOSE POSSIBLE LIGHTNING STRIKE IN CRUISE FLIGHT. CREW RETURNED TO PHL AIRPORT. STRONG ELECTRICAL SMELL IN COCKPIT. 22107 00 
- [SDR ASOA201809027159](https://openairdocs.org/sdr/ASOA201809027159), Aug 29, 2018: STRINGER. CHAFED. CHAFE DAMAGE ON PREVIOUS REPAIR AT STRINGER 19L AT FRAME 52. REMOVED AND REPLACED DAMAGED SECTION OF PREVIOUS REPAIR ON STRINGER. AIRCRAFT STILL IN C CHECK.

All 3,003: https://openairdocs.org/model/embraer-emb-145/reports.md

## STCs that may be installed (OpenAirDocs) (68, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [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 ST02310AT](https://openairdocs.org/stc/ST02310AT): Installation of SAF-T-GLO photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [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 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 ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [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 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 ST04551AT](https://openairdocs.org/stc/ST04551AT): Installation of the Universal UNS-ILW FMS/GPS. Chippewa Aerospace Inc
- [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 ST00818DE](https://openairdocs.org/stc/ST00818DE): Installation of Honeywell Control Display Unit (CDU) model CD-830. Premier Air Center LLC d/b/a West Star Aviation
- [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 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 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 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
- [STC ST04282AT](https://openairdocs.org/stc/ST04282AT): Installation of the Honeywell DU-875 LCD Flight Display. Chippewa Aerospace Inc
- [STC ST04015AT](https://openairdocs.org/stc/ST04015AT): Installation of the Honeywell NZ-2000 FMS/GPS System with or without WAAS/LPV. Chippewa Aerospace Inc
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC ST09859AC](https://openairdocs.org/stc/ST09859AC): Installation of a SkyTender Beverage Trolley. ASIG LLC
- [STC ST04263AT](https://openairdocs.org/stc/ST04263AT): Modification of Interior Arrangement Configuration from 50 to 30 Passenger Seats (All Tourist Class). VIA Airlines Inc
- [STC ST03390AT](https://openairdocs.org/stc/ST03390AT): Installation of a LIVE TV XM Satellite Radio System. Thales Avionics Inc
- [STC ST04191AT](https://openairdocs.org/stc/ST04191AT): Installation of the Honeywell Sky Connect Tracker Iridium Satcom System. Chippewa Aerospace Inc
- [STC ST02524LA](https://openairdocs.org/stc/ST02524LA): Installation of TCAS version 7.0. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST01754WI](https://openairdocs.org/stc/ST01754WI): Replacement of lighted No Smoking Signs with No Smoking Placards. Georgian Aerospace Group Inc
- [STC ST03483AT](https://openairdocs.org/stc/ST03483AT): Installation of a Portable Beverage Dispensing System, P/N B43-FA-001. Dynamo Beverage Company, USA, L.L.C
- [STC ST04149AT](https://openairdocs.org/stc/ST04149AT): Installation of a Constant Friction Mount, Cradle and Integrated Power Supply on Embraer 145 series aircraft and associated hardware. Avionics Support Group Inc

All 68: https://openairdocs.org/model/embraer-emb-145/stcs.md

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