# Embraer EMB-135ER

- Type: Aircraft model (FAA registry)
- Registry code: 3260307
- Manufacturer (registry): EMBRAER
- Model: EMB-135ER
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-jet
- Seats: 37
- 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: 10
- Page: https://openairdocs.org/model/embraer-emb-135er

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 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 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
- [AD 2004-25-12](https://openairdocs.org/ad/2004-25-12): Passenger service unit (PSU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 13, 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 2006-04-02](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 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

All 93: https://openairdocs.org/model/embraer-emb-135er/ads.md

## Information bulletins (advisory) (9)

- [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

## Registered aircraft (10)

- [N15509](https://openairdocs.org/aircraft/N15509): [Corporate Flight Management Inc](https://openairdocs.org/faa-owner/CORPORATE%20FLIGHT%20MANAGEMENT%20INC), [Smyrna, TN](https://openairdocs.org/faa-place/TN/Smyrna), built 2000, S/N 145238
- [N16501](https://openairdocs.org/aircraft/N16501): [Corporate Flight Management Inc](https://openairdocs.org/faa-owner/CORPORATE%20FLIGHT%20MANAGEMENT%20INC), [Smyrna, TN](https://openairdocs.org/faa-place/TN/Smyrna), built 1999, S/N 145145
- [N16502](https://openairdocs.org/aircraft/N16502): [Corporate Flight Management Inc](https://openairdocs.org/faa-owner/CORPORATE%20FLIGHT%20MANAGEMENT%20INC), [Smyrna, TN](https://openairdocs.org/faa-place/TN/Smyrna), built 1999, S/N 145166
- [N16510](https://openairdocs.org/aircraft/N16510): [Corporate Flight Management Inc](https://openairdocs.org/faa-owner/CORPORATE%20FLIGHT%20MANAGEMENT%20INC), [Smyrna, TN](https://openairdocs.org/faa-place/TN/Smyrna), built 2000, S/N 145251
- [N16511](https://openairdocs.org/aircraft/N16511): [Corporate Flight Management Inc](https://openairdocs.org/faa-owner/CORPORATE%20FLIGHT%20MANAGEMENT%20INC), [Smyrna, TN](https://openairdocs.org/faa-place/TN/Smyrna), built 2000, S/N 145267
- [N268JX](https://openairdocs.org/aircraft/N268JX): [Delux Public Charter LLC](https://openairdocs.org/faa-owner/DELUX%20PUBLIC%20CHARTER%20LLC), [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas), built 2001, S/N 145499
- [N27512](https://openairdocs.org/aircraft/N27512): [Corporate Flight Management Inc](https://openairdocs.org/faa-owner/CORPORATE%20FLIGHT%20MANAGEMENT%20INC), [Smyrna, TN](https://openairdocs.org/faa-place/TN/Smyrna), built 2000, S/N 145274
- [N538M](https://openairdocs.org/aircraft/N538M): [Menards Inc](https://openairdocs.org/faa-owner/MENARDS%20INC), [Eau Claire, WI](https://openairdocs.org/faa-place/WI/Eau%20Claire), built 2001, S/N 145467
- [N548M](https://openairdocs.org/aircraft/N548M): [Ga-Erj135 LLC](https://openairdocs.org/faa-owner/GA-ERJ135%20LLC), [Seiling, OK](https://openairdocs.org/faa-place/OK/Seiling), built 2000, S/N 145364
- [N926FM](https://openairdocs.org/aircraft/N926FM): [Rvr Air Charter LLC](https://openairdocs.org/faa-owner/RVR%20AIR%20CHARTER%20LLC), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth), built 2001, S/N 145466

## 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 IAD01LA102](https://openairdocs.org/ntsb/IAD01LA102), Aug 30, 2001: Embraer ERJ-135ER (N25504), Richmond, VA, no damage. Probable cause: Inadequate company procedures/directives, which resulted in the flight attendant leaving her seat prematurely, while the airplane was still in an area of turbulence.

## FAA accident and incident reports (8)

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 20240724009649I](https://openairdocs.org/incident/20240724009649I), Jul 24, 2024: Embraer EMB-135ER (N16511), Phoenix, AZ, Minor damage. Aircraft departed phx with 6 souls on board. After ascent, at cruise level 290, pilots side of windshield shattered. No loss or pressurization. Aircrew…
- [Incident 20230612005639I](https://openairdocs.org/incident/20230612005639I), Jun 12, 2023: Embraer EMB-135ER (N16510), Murphysboro, IL, No damage. On June 12th, 2023, at 1340 local time, VTE510, [privacy data omitted], was conducting a local maintenance flight to check the landing gear function at kmdh.…
- [Incident 20060322011189I](https://openairdocs.org/incident/20060322011189I), Mar 22, 2006: Emb EMB135ER (N14505), Newark, NJ. (-23) On 03/22/06, at approximately 1725, aircraft tookoff from ewr enroute to alb. While in-flight crew heard and felt a loud vibration followed by a buzzing…
- [Incident 20040815030839I](https://openairdocs.org/incident/20040815030839I), Aug 15, 2004: Emb EMB135ER (N16502), Newark, NJ. (-23) On August 14, 2004, jet link flight 2885 a Emb-135-ER aircraft, N16502, while enroute from kcle to khpn, declared an inflight emergency and diverted to…
- [Incident 20040618020539I](https://openairdocs.org/incident/20040618020539I), Jun 18, 2004: Emb EMB135ER (N27506), Richmond, VA. (-23) The aircraft was parked at the gate. The passengers had already been deplaned. The pilot was dry motoring the #1 engine after a previous hung start. The…
- [Accident 20010830026339A](https://openairdocs.org/incident/20010830026339A), Aug 30, 2001: Emb EMB135ER (N25504), Richmond, VA, No damage. (-23) At 1600E, flight 3608, while in route to Richmond international airport (ric), encountered turbulence over the flat rock, Virginia VOR (pak) at 15,000…
- [Incident 20010120001799I](https://openairdocs.org/incident/20010120001799I), Jan 20, 2001: Emb EMB135ER (N14505), Pittsburgh, PA, Minor damage. (-23) On January 20, 2001, at 1400E,a FMB-135, s/n 145192, registered as N14505 and being operated as C2XA flight 3657, diverted to "pit" due to cracked…
- [Incident 20001029021399I](https://openairdocs.org/incident/20001029021399I), Oct 29, 2000: Emb EMB135ER (N14505), Erie, PA. (-23) On October 29, 2000, at 2250 hours UTC, Continental express flight #4290 diverted to Erie, PA. With a number one bleed air leak. Flight #4290 was enroute…

## Service difficulty reports (465, newest 50)

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

- [SDR FJTA2026072716502](https://openairdocs.org/sdr/FJTA2026072716502), Jul 26, 2026: WINDSHIELD. CRACKED. WHILE CLIMBING THROUGH FL220 THE OUTER PANE OF THE FIRST OFFICER'S WINDSHIELD SHATTERED. THIS WINDSHIELD WAS RECENTLY REPLACED ON 7/18/2026 WITH AN OVERHAULED U
- [SDR FJTA202407265111](https://openairdocs.org/sdr/FJTA202407265111), Jul 24, 2024: WINDSHIELD. CRACKED. 7/24/2024 - FLT VTE3348 - CREW REPORTED THAT CAPT WINDSHIELD BROKE UPON LEVELING AT FL290. RETURNED TO KPHX. MAITNENANCE REMOVED AND REPLACED THE WINDSHIELD IAW
- [SDR 4DPA2024013000001](https://openairdocs.org/sdr/4DPA2024013000001), Jan 30, 2024: PROXIMITY SWITCH. OUT OF ADJUST. CREW REPORTED; AFTER TO, CALLED POSITIVE RATE, GEAR UP, WE RECEIVED A LDG GEAR AIR/GND FAIL. GEAR INDICATED 3 WHITE, UP. AT 500, CALLED FOR AP AND AURAL WARNING
- [SDR 4DPA2023042100002](https://openairdocs.org/sdr/4DPA2023042100002), Apr 21, 2023: SWITCH PANEL. FAILED. ISSUE-CREW REPORTED LOSS OF ALL GENERATORS, ISIS, ALL SCREENS EXCEPT PFD1, PFD1 HAD NUMEROUS CAUTION FLAGS, CREW RAN QRH WITH NO HELP DECIDED TO STOP CLIMB AT A
- [SDR 4DPA2023042100001](https://openairdocs.org/sdr/4DPA2023042100001), Apr 21, 2023: COMPUTER. FAILED. ISSUE-CREW REPORTED SPS ADVANCE AND AHRS 2 FAIL MESSAGES. AP ALSO INOP IN FLIGHT. CORR ACTION- MX TROUBLESHOT THE ISSUE TO A BAD AHRS #2 COMPUTER. R&R'D AHRS CO
- [SDR 4DPA202303260002](https://openairdocs.org/sdr/4DPA202303260002), Mar 26, 2023: CONTROLLER. FAILED. ISSUE-CREW REPORTED LOSS CABIN ALTITUDE INDICATION IS IN THE CLIMB, STOPPED AT 10,000 THEN LOST ALL CABIN INDICATIONS WITH ORANGE DASHES AND CABIN RATE WAS 0.CO
- [SDR 4DPA2022111400001](https://openairdocs.org/sdr/4DPA2022111400001), Nov 14, 2022: CONTROL MODULE. FAILED. ISSUE-CREW REPORTED PACK1 FAIL AND PACK 2 OVERHEAT ON CLIMB OUT AND RTF TO LAS. CORR ACTION-MX TROUBLESHOT TO BAD TEMP CONTROL MODULE AND BAD #2 PUSHBUTTON SWIT
- [SDR 4DPA2022061600002](https://openairdocs.org/sdr/4DPA2022061600002), Jun 16, 2022: WINDSHIELD. CRACKED. LEFT SIDE WINDSHIELD OUTER PANE SHATTERED DURING DESCENT AT ABOUT FL 250 +/- CREW DECLARED AND EMERGENCY AND LANDED NO FURTHER ISSUES REPORTED. CORR ACTION- R&R
- [SDR 4DPA2022052100001](https://openairdocs.org/sdr/4DPA2022052100001), May 21, 2022: NONE. NONE. CREW REPORTED HIGH PITCH NOISE FROM COCKPIT, SOUNDS LIKE AIR ESCAPING DURING CLIMB. CREW RTF TO PHX. MX DISCOVERED HARDWARE ON MED SILL IMPROPERLY INSTALLED, RE
- [SDR ASOA201703314015](https://openairdocs.org/sdr/ASOA201703314015), Mar 31, 2017: FLOOR SUPPORT. CORRODED. DURING A MAINTENANCE INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE PERFORMED AN INSERTION REPAIR ON THE AFFECTED BEAM, AND
- [SDR 7GMB2013082300001](https://openairdocs.org/sdr/7GMB2013082300001), Aug 22, 2013: UNKNOWN. ODOR. 30 MINUTES BEFORE LANDING, DETECTED AN ELECTRICAL BURNING ODOR THROUGHT ENTIRE CABIN. TURNED OFF PC POWER SYS IMMEDIATELY AND ODOR SLOWLY WENT AWAY. F/A COULD N
- [SDR ASOA20130814209V](https://openairdocs.org/sdr/ASOA20130814209V), Aug 14, 2013: BEAM. CORRODED. DURING SCHEDULED MX, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MX R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 7GMB0201306244991](https://openairdocs.org/sdr/7GMB0201306244991), Jun 20, 2013: FLEX HOSE. CHAFED. ON DESCENT AT 14,000FT, HYD 2 QTY LOW MESSAGE APPEARED, THEN FOLLOWED SHORTLY BY ENG 2 HYD PUMP FAIL MESSAGE. THE CREW DIVERTED DUE TO RUNWAY REQUIREMENT AND LA
- [SDR 7GMB2013006186181](https://openairdocs.org/sdr/7GMB2013006186181), Jun 15, 2013: TUBE. BROKEN. NR 1 ENGINE ANTI-ICE PRESSURE TRANSDUCER TUBE FOUND BROKEN AT TRANSDUCER AND ENGINE AIR INTAKE ANTI-ICE DUCT. R & R WITH NEW. OPS CHECKED GOOD.
- [SDR 7GMB201306070466](https://openairdocs.org/sdr/7GMB201306070466), Jun 7, 2013: CONTROLLER. FAILED. WINDSHIELD HEAT NR 2 FAIL MESSAGE APPEARED WHEN SELECTED ON DURING DESENT. ELECTRIC BURNING SMELL SHORTLY AFTER. FOLLOWED QRH PROCEDURES AND PERFORMED A NORMAL 
- [SDR ASOA20130518157](https://openairdocs.org/sdr/ASOA20130518157), May 17, 2013: LIGHT. INOPERATIVE. DURING ROUTINE CHECK THE NR 4 EMERGENCY PROXIMITY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MX R & R THE DEFECTIVE LIGHT STRIP IAW AMM 33-50-12. THE ACFT WAS APP
- [SDR ASOA20130423154](https://openairdocs.org/sdr/ASOA20130423154), May 10, 2013: DRAG ANGLE. CRACKED. DURING A-CHECK, THE RT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED AT FRAME 76, STRINGER 1R. MX R & R THE ANGLE IAW SRM 51-40-02. THE ACF
- [SDR SIMA20121228005](https://openairdocs.org/sdr/SIMA20121228005), Dec 28, 2012: BATTERY. DISCHARGED. EMERGENCY PANEL LIGHT IN FRONT OF ROW 3BC IS INOP. REMOVED AND REPLACED BATTERY NR 2 AND EMERGENCY BATTERY NR 2 CHARGER IAW AEWC 33-700-19. PERFORMED EMERGENCY 
- [SDR I06B2012113641](https://openairdocs.org/sdr/I06B2012113641), Nov 9, 2012: PANEL. DEFECTIVE. AFTER NR 1 ENGINE START, NR 1 ENGINE FAILED (SHUTDOWN) WHEN NR 1 FADEC SWITCH WAS CYCLED FROM RESET/ALTN. PERFORMED EMB135 FIM 72-00-00-810-805-A FOR ENGINE SHU
- [SDR I06B2012114991](https://openairdocs.org/sdr/I06B2012114991), Nov 6, 2012: GCU. MALFUNCTIONED. GEN 3 OFF BUS ON TAXI IN AFTER SHUTDOWN OF NR 2 ENGINE. SMELL OF SMOKE IN THE COCKPIT. PERFORMED FIM 21-20-00-810-801-A FOR SMELL OF SMOKE IN THE CABIN COCKPIT.
- [SDR I06B201210233641](https://openairdocs.org/sdr/I06B201210233641), Oct 23, 2012: UNKNOWN. MALFUNCTIONED. ON DESCENT AT FL 250 NR 2 ENGINE THRUST WAS FLUCTUATING. THROTTLES WERE STEADY AND SET APPROX 1/3 OF TRAVEL FROM IDLE POSITION. YAWING WAS EXPERIENCED AND ITT W
- [SDR I06B201209274992](https://openairdocs.org/sdr/I06B201209274992), Sep 26, 2012: WIRE. BROKEN. 3RD EMERGENCY FLOOR PROXIMITY STRIP LIGHT INOP, CONNECTOR WIRES BROKEN AT BASE. REMOVED DEFECTIVE UNIT AND INSTALLED SERVICEABLE (NEW) 3RD EMERGENCY FLOOR PROXI
- [SDR I06B201209274991](https://openairdocs.org/sdr/I06B201209274991), Sep 26, 2012: WIRE. BROKEN. 2ND EMERGENCY FLOOR PROXIMITY STRIP LIGHT INOP, CONNECTOR WIRES BROKEN AT BASE. REMOVED DEFECTIVE UNIT AND INSTALLED SERVICEABLE (NEW) 2ND EMERGENCY FLOOR POXIM
- [SDR I06B201208153641](https://openairdocs.org/sdr/I06B201208153641), Aug 15, 2012: ACTUATOR. LEAKING. DURING CLIMB THROUGH 17,000 FEET HYD1 LOW QTY MESSAGE WAS DISPLAYED ON EICAS. UPON LANDING AT PDX AND SERVICING OF THE NR 1 HYDRAULIC SYSTEM A LEAK WAS IDENTIFI
- [SDR I06B201207094671](https://openairdocs.org/sdr/I06B201207094671), Jul 9, 2012: UNKNOWN. NOISY. CREW HEARD AN UNUSUAL NOISE ON GEAR RETRACTION FOLLOWING TAKEOFF, AND ELECTED TO MAKE A PRECAUTIONARY LANDING TO INVESTIGATE AT THE DEPARTURE AIRPORT. PASSENGER
- [SDR I06B201206274672](https://openairdocs.org/sdr/I06B201206274672), Jun 27, 2012: FILTER. UNKNOWN. ON TAKEOFF ROLL "E1 FUEL IMPENDING BYPASS" MESSAGE WAS DISPLAYED ON EICAS. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE PERFORMED THE PROC
- [SDR I06B20120416001](https://openairdocs.org/sdr/I06B20120416001), Apr 16, 2012: UPLOCK. FAILED. ON GEAR UP, RECEIVED MLG LEVER DISAGREE MESSAGE AND RT MLG NOT LOCKED INDICATION. CYCLED MLG AND RECEIVED SAME INDICATIONS. EXTENDED MLG AND RETURNED TO BASE NO
- [SDR 2012FA0000066](https://openairdocs.org/sdr/2012FA0000066), Jan 23, 2012: STATIC INVERTER. INOPERATIVE. STATIC INVERTER FAILED TO OPERATE. SYS POWERS THE EGPWS AND TCAS SYS, AND IS SOLE SOURCE OF POWER FOR THESE SYS.
- [SDR 2012FA0000060](https://openairdocs.org/sdr/2012FA0000060), Jan 18, 2012: WARNING MESSAGE. ILLUMINATED. CAPTAINS DISPLAY UNIT DU FAN FAIL MESSAGE APPEARED ON EICAS.
- [SDR I06B2010 01 18 JF](https://openairdocs.org/sdr/I06B2010%2001%2018%20JF), Jan 18, 2010: ENGINE. CONTAMINATED. AFTER TAKEOFF AT APPROX 400 FT, PILOTS RECEIVED "LAV SMOKE" EICAS INDICATION. DECLARED EMERGENCY & RETURNED FOR LANDING AT DEPARTURE. ACFT GROUNDED UNTIL MX DET
- [SDR 2009FA0000918](https://openairdocs.org/sdr/2009FA0000918), Sep 2, 2009: RING. CORRODED. (16) OF THE ATTACHMENT RINGS THAT SECURE THE ENGINE INLET TO THE ENGINE, HAVE CORROSION IN ALL ATTACH HOLES. THESE RINGS WERE LOCATED IN A REPAIR STATION. (K)
- [SDR I06B20090501FM](https://openairdocs.org/sdr/I06B20090501FM), Apr 30, 2009: PANEL. INACTIVE. ON CLIMB OUT, THROUGH APPROX 17,000, FLT ATTENDANT REPORTED THAT WHEN THE PC-POWER SYSTEM WAS TURNED ON, 1 PASSENGER MOMENTARILY SMELLED A FAINT ODOR, WHICH CAM
- [SDR I06B2009 02 06 TM](https://openairdocs.org/sdr/I06B2009%2002%2006%20TM), Feb 6, 2009: THRUST REVERSER. DEFECTIVE. CONDUCTED ABORTED TAKEOFF AT APPROX 80 " 90 KIAS DUE TO EICAS MESSAGE " ENG 1 REV DISAGREE". COMPLIED WITH ABORT PROCEDURE. MESSAGE DISAPPEARED DURING DECELERAT
- [SDR I06B20090206TM](https://openairdocs.org/sdr/I06B20090206TM), Feb 6, 2009: WARNING SYSTEM. ACTIVATED. CONDUCTED ABORTED TAKEOFF AT APPROXIMATELY 80-90 KIAS DUE TO EICAS MESSAGE "ENG 1 REV DISAGREE". COMPLIED WITH ABORT PROCEDURE. MESSAGE DISAPPEARED DURING DECEL
- [SDR I06B20081030001](https://openairdocs.org/sdr/I06B20081030001), Oct 30, 2008: DOOR. DAMAGED. 14K FT NOTICED A FLASH OF LIGHT THAT APPEARED TO BE BELOW THE AIRCRAFT. THE CREW REPORTED NO AIRCRAFT ANOMALIES AS A RESULT OF THE SUSPECTED NEAR LIGHTNING STRI
- [SDR C2XA08CL092](https://openairdocs.org/sdr/C2XA08CL092), Aug 5, 2008: APU. FAULTY. CLE FLIGHT 2630 - THE CREW REPORTED A LAV SMOKE WARNING MESSAGE ON THE EICAS AFTER SELECTING COOLING PACKS DURING TAXI. THE ACFT RETURNED TO THE GATE WITHOUT FU
- [SDR C2XA08RI103](https://openairdocs.org/sdr/C2XA08RI103), Jul 16, 2008: LIGHT. DEFECTIVE. FLIGHT 2513 -EWR- FLIGHT CREW REPORTED ELECTRICAL BURNING ODOR IN FORWARD CABIN. EWR MX REMOVED AND REPLACED PASSENGER CABIN LIGHT AT ROW 1A AND PERFORMED OPERA
- [SDR C2XA08CL072](https://openairdocs.org/sdr/C2XA08CL072), Jun 17, 2008: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE THE NR 2 EMERGENCY AISLE PATH LIGHT STRIP WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT STRIP. OPERATIONAL CHE
- [SDR C2XA08CL071](https://openairdocs.org/sdr/C2XA08CL071), Jun 15, 2008: CARBON SEAL. LEAKING. CLE FLIGHT 2290. THE CREW REPORTED ON SHORT FINAL RECEIVED AN ENG 2 LOW OIL PRESSURE WARNING MESSAGE. THE ENG WAS SHUT DOWN BY THE CREW IMMEDIATELY AFTER LANDIN
- [SDR C2XA08RI070](https://openairdocs.org/sdr/C2XA08RI070), May 12, 2008: MODULE. INACCURATE. FLIGHT 1202 - EWR - FLIGHT CREW REPORTED STEERING PULLED TO LEFT AND SHAKING LEFT & RIGHT. CREW RETURNED AIRCRAFT TO GATE. EWR MX REMOVED AND REPLACED HYDRAULIC
- [SDR C2XA08RI067](https://openairdocs.org/sdr/C2XA08RI067), May 11, 2008: SMOKE DETECTOR. FALSE ACTIVATION. FLIGHT 3096 - EWR - FLIGHT CREW REPORTED BAGGAGE EXTINGUISH WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALSO, INTERMITTENT BAGGAGE SMOKE WARNING ON EICA
- [SDR C2XA08RI061](https://openairdocs.org/sdr/C2XA08RI061), May 2, 2008: SMOKE DETECTOR. LOOSE. FLIGHT 2424 - BAG SMOKE WARNING IN FLIGHT, BOTH LIGHTS AND EICAS MESSAGES STAYED FOR FEW SECONDS THEN WENT OFF. MX RESECURED LOOSE CONNECTOR PLUG AT AFT SMOKE D
- [SDR C2XA08CL053](https://openairdocs.org/sdr/C2XA08CL053), May 1, 2008: WIRE. CHAFED. CLE FLIGHT 2419 - THE CREW REPORTED A APU FIRE DETECT FAIL MESSAGE INTERMITTENTLY DURING FLIGHT. MAINTENANCE INSPECTED AND REPAIRED A CHAFED WIRE ON THE APU HAR
- [SDR C2XA08CL044](https://openairdocs.org/sdr/C2XA08CL044), Apr 5, 2008: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT STRIP AT ROW 3 & 4 FAILED OPERATIONAL CHECK. MAINTENANCE INSPECTED AND REPLACED THE FLOOR PROXIMITY LIGHT STRIP A
- [SDR CA080314007](https://openairdocs.org/sdr/CA080314007), Mar 12, 2008: ENGINE. LEAKING. OIL IMPENDING BYPASS INDICATION ILLUMINATED ALONG WITH OIL TEMPERATURE RISING TO 141 DEGREES. THE PILOT COMMANDED THE SHUT DOWN OF THE ENGINE DUE TO OIL TEMPERA
- [SDR C2XA08CL014](https://openairdocs.org/sdr/C2XA08CL014), Jan 29, 2008: MODULE. DEFECTIVE. DAY FLIGHT 2382 - THE CREW REPORTED 10 MINUTES INFLIGHT IN CLIMB MODE THE NR 2 ENGINE POWERED BACK TO FLIGHT IDLE UNCOMMANDED. THE AIRCRAFT DIVERTED TO CLE AND 
- [SDR C2XA08RI068](https://openairdocs.org/sdr/C2XA08RI068), Jan 11, 2008: SMOKE DETECTOR. INTERMITTENT. FLIGHT 3096 - EWR - FLIGHT CREW REPORTED BAGGAGE EXTINGUISH WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALSO, INTERMITTENT BAGGAGE SMOKE WARNING ON EICA
- [SDR C2XA08CL007](https://openairdocs.org/sdr/C2XA08CL007), Jan 10, 2008: FIRE DETECTOR. FAILED. YOW FLIGHT 2762 - THE CREW REPORTED AN APU FIRE DETECT FAIL MESSAGE INFLIGHT WITH APU OFF. MAINTENANCE INSPECTED AND REPLACED THE APU FIRE DETECTOR. OPERATIONAL
- [SDR C2XA08TY004](https://openairdocs.org/sdr/C2XA08TY004), Jan 9, 2008: CHARGER. INOPERATIVE. OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGING BASE IAW EMB135 AMM 33-50-04. OPS CHECK GOOD, AIRCRAFT RELEASED AND R
- [SDR C2XA08TY005](https://openairdocs.org/sdr/C2XA08TY005), Jan 8, 2008: FAIRING. DAMAGED. LEFT WING TO FUSELAGE FAIRING 193 GROUND DAMAGE REPAIR. PERFORMED PLY RESTORATION TO EACH SKIN, ONE AT A TIME INCLUDING CORE REPLACEMENT. EXPOXY PRIME AND FINIS

All 465: https://openairdocs.org/model/embraer-emb-135er/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 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 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 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 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 ST02815LA](https://openairdocs.org/stc/ST02815LA): Installation of Airworthy R/H and L/H Stowage Units. Airworthy Incorporated
- [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 ST04327CH](https://openairdocs.org/stc/ST04327CH): Installation of High Speed Internet System and Wireless Activation. Nextant Aerospace 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 ST09858SC](https://openairdocs.org/stc/ST09858SC): Installation of cabin automatic coffee brewing system. Safran Cabin Germany Gmbh
- [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 ST04049NY](https://openairdocs.org/stc/ST04049NY): Installation of a Hoffman Engineering LLC LED Landing Light to replace the OEM Q4559 Series Incandescent Lamp, used as a Landing/Takeoff Light. Hoffman Engineering LLC
- [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 ST03889AT](https://openairdocs.org/stc/ST03889AT): Installation of Aircell Axxess Cabin Telecommunication Router (CTR) 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

All 68: https://openairdocs.org/model/embraer-emb-135er/stcs.md

---
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