# N712AE: Embraer EMB-135LR

- Status: Valid registration
- Airframe: [Embraer EMB-135LR](https://openairdocs.org/model/embraer-emb-135lr) (registry code 3260305, 37 seats)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.) (OpenAirDocs)
- Serial number: 145247
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Certificate issued: February 14, 2022
- Expires: February 28, 2029
- Mode S code: A98380
- Registered owner: [Aero Aircraft Holdings LLC](https://openairdocs.org/faa-owner/AERO%20AIRCRAFT%20HOLDINGS%20LLC)
- Location: [Van Nuys, CA](https://openairdocs.org/faa-place/CA/Van%20Nuys)
- Owner type: LLC
- Owner's area on the map: 34.1975° N, 118.4890° W: Placed by OpenAirDocs at the center of ZIP code 91406, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=712AE
- Page: https://openairdocs.org/aircraft/N712AE

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): 75 in force

### Matched by airframe (Embraer EMB-135LR)

- [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 2007-10-11](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
- [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/aircraft/N712AE/ads.md

## Information bulletins (advisory) (8 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB AIR-20-17](https://openairdocs.org/saib/AIR-20-17): Air Conditioning - Cabin Pressure Control System. Issued Nov 3, 2020
- [SAIB NM-19-17](https://openairdocs.org/saib/NM-19-17): Ice and Rain Protection: Electrical Wiring Terminations at Pitot and TAT Relays. Issued Dec 5, 2019
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008
- [SAIB NM-08-15](https://openairdocs.org/saib/NM-08-15): Instruments: Contamination of the Attitude Heading Reference System (AHRS) Computers. Issued Mar 26, 2008
- [SAIB NM-07-40](https://openairdocs.org/saib/NM-07-40): Embraer EMB-135/145 Landing Gear Incident. Issued Jul 9, 2007
- [SAIB NM-07-20](https://openairdocs.org/saib/NM-07-20): Flight Data Recorders. Issued Mar 21, 2007
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N712AE.

## FAA accident and incident reports (1)

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 20220224000959I](https://openairdocs.org/incident/20220224000959I), Feb 24, 2022: Embraer EMB-135LR (N712AE), Aspen, CO, Minor damage. The aircraft landed on runway 15 at Aspen/Pitkin county airport (ase). After landing the pilot deployed the thrust reverser. The pilot applied the aircraft…

## Service difficulty reports (51, 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 SIMA20130227004](https://openairdocs.org/sdr/SIMA20130227004), Feb 27, 2013: HOLDER. BROKEN. DURING MAINTENANCE INSPECTION FOUND THE FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTEND
- [SDR SIMA20130119004](https://openairdocs.org/sdr/SIMA20130119004), Jan 19, 2013: CONNECTOR. DEFECTIVE. DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT ON THE SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE WIRE CON
- [SDR SIMA20130114003](https://openairdocs.org/sdr/SIMA20130114003), Jan 14, 2013: LIGHT. INOPERATIVE. DURING B INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IAW 33-50-10. THE O
- [SDR SIMA20130105001](https://openairdocs.org/sdr/SIMA20130105001), Jan 5, 2013: FLASHLIGHT. UNSERVICEABLE. ON FLIGHT 3248 THE CREW REPORTED THE CAPTAIN'S FLASHLIGHT WOULD NOT STAY IN FLASHLIGHT HOLDER/CHARGER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLAC
- [SDR SIMA20121115002](https://openairdocs.org/sdr/SIMA20121115002), Nov 15, 2012: WIRE. BROKEN. DURING B INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED BROKEN WIRE AT SERVICE DOOR EMERGENCY LIG
- [SDR SIMA20121026004](https://openairdocs.org/sdr/SIMA20121026004), Oct 26, 2012: ACM. MALFUNCTIONED. FOR FLIGHT 2802 THE CREW REPORTED THAT WHILE PARKED AT THE GATE RUNNING APU FOR ABOUT 20 MINUTES CLOSED THE MAIN DOOR AND ABOUT 30 SECONDS LATER HAD SMOKE IN TH
- [SDR SIMA20121019002](https://openairdocs.org/sdr/SIMA20121019002), Oct 19, 2012: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION FOUND THE 4TH EMERGENCY LIGHTING STRIP FROM REAR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERG
- [SDR SIMA20121019001](https://openairdocs.org/sdr/SIMA20121019001), Oct 19, 2012: FAN. MALFUNCTIONED. ON FLIGHT 2802 THE CREW REPORTED THAT AFTER LANDING THE SMELL OF ELECTRICAL SMOKE WAS DETECTED AND THEN DISSIPATED SHORTLY THEREAFTER. THE AIRCRAFT WAS REMOVED 
- [SDR SIMA20120718001](https://openairdocs.org/sdr/SIMA20120718001), Jul 18, 2012: UNKNOWN. ODOR. FLIGHT 3337, RAMP CREW REPORTED THEY NOTICED A SMOKE ODOR IN CARGO BAY. AIRCRAFT REMOVED FROM SERVICE. INSPECTED CARGO BAY FOR OBVIOUS DEFECTS, NONE NOTED. GROU
- [SDR SIMA20120710005](https://openairdocs.org/sdr/SIMA20120710005), Jul 10, 2012: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION, FOUND THE OVERHEAD AISLE EMERGENCY EXIT LIGHT OUT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE OVERHEAD AISLE EMERGEN
- [SDR SIMA201136315](https://openairdocs.org/sdr/SIMA201136315), Dec 28, 2011: LIGHT. INOPERATIVE. MEL 3330. EMERGENCY FLOOR PROXIMITY LIGHT INOP ON FLOOR SEATS 5 AND 6. REMOVED AND REPLACED EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT SEATS 5 AND 6 IAW EMB 135 A
- [SDR SIMA201136309](https://openairdocs.org/sdr/SIMA201136309), Dec 23, 2011: LIGHT. INOPERATIVE. EMERGENCY LIGHT FLOOR PROXIMITY STRIP INOP SEAT 5 & 6. DEFERRED PER MEL 33-30, M PROCEDURE C/W.
- [SDR SIMA201136303](https://openairdocs.org/sdr/SIMA201136303), Dec 22, 2011: LIGHT. INOPERATIVE. FOUND 2ND LIGHT STRIP EMERGENCY AISLE INOP. REMOVED AND REPLACED AISLE LIGHT STRIP EMERGENCY IAW EMB-135 AMM 33-50-08. OPS CHECK GOOD.
- [SDR SIMA201111601](https://openairdocs.org/sdr/SIMA201111601), Apr 23, 2011: ANTENNA. DAMAGED. ON FLIGHT 2895 CREW REPORTED ACFT EXPOSED TO SEVERE AND EXTREME TURBULENCE, LIGHTNING STRIKES & STRONG VIBRATIONS THROUGH COCKPIT FLOOR & CABIN ROW 2. CREW LOST
- [SDR SIMA201107604](https://openairdocs.org/sdr/SIMA201107604), Mar 17, 2011: SUPPORT BRACKET. CRACKED. DURING MAINTENANCE VISIT FOUND THE PASSENGER DOOR INTERNAL HANDLE SUPPORT BOX BRACKET CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED PASSENGER DOOR IN
- [SDR SIMA201106905](https://openairdocs.org/sdr/SIMA201106905), Mar 6, 2011: LIGHT. INOPERATIVE. FOR FLIGHT 2712 DURING PREFLIGHT INSPECTION FOUND THE FIRST CEILING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACE
- [SDR SIMA201034304](https://openairdocs.org/sdr/SIMA201034304), Dec 5, 2010: WARNING SYSTEM. MALFUNCTIONED. ON FLIGHT 4470 THE CREW REPORTED A FLAP FAIL MESSAGE ON EICAS WHEN SELECTED TO 9 DEGREES FLAPS STAYED AT 0 DEGREES. THE CAPTAIN DECLARED AN EMERGENCY AND THE AI
- [SDR SIMA201030503](https://openairdocs.org/sdr/SIMA201030503), Oct 29, 2010: CRADLE. BROKEN. FOR FLIGHT 4547 DURING TAXI THE REAR CABIN FLASHLIGHT WAS LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT AND CRADLE
- [SDR SIMA201023801](https://openairdocs.org/sdr/SIMA201023801), Aug 25, 2010: BALLAST. DEFECTIVE. ON FLIGHT 4524 THE CREW REPORTED A STRONG SMOKE ODOR COMING FROM A PASSENGER SERVICE UNIT AT SEAT 8A IN THE CABIN. THE CAPTAIN DECLARED AN EMERGENCY AND THE AIR
- [SDR SIMA200934303](https://openairdocs.org/sdr/SIMA200934303), Dec 5, 2009: FLAP SYSTEM. MALFUNCTIONED. DURING FLIGHT 4546 WHILE ON APPROACH THE CREW RECEIVED A FLAP FAIL MESSAGE. THE MESSAGE INDICATED THAT THE FLAPS WERE ON 0 DEGREES. THE CREW DECLARED AN EMERGEN
- [SDR SIMA200933803](https://openairdocs.org/sdr/SIMA200933803), Dec 3, 2009: BRAKE. FAILED. DURING FLIGHT 4485 ON APPROACH THE CREW REPORTED A FLAP FAIL. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE.
- [SDR SIMA200931301](https://openairdocs.org/sdr/SIMA200931301), Nov 5, 2009: FLAP. MALFUNCTIONED. ON FLIGHT 4552 DURING DESCENT WHILE SELECTING FLAPS 9 FROM ZERO THE CREW RECEIVED AN EICAS FLAP FAIL MESSAGE. THE MESSAGE INDICATED ZERO DEGREES. THE CREW DECLA
- [SDR SIMA200929906](https://openairdocs.org/sdr/SIMA200929906), Oct 25, 2009: VELOCITY SENSOR. DEFECTIVE. ON FLIGHT 4472 DURING THE DESCENT THE CREW REPORTED A FLAP FAILURE MESSAGE ON EICAS. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WA
- [SDR SIMA200912001](https://openairdocs.org/sdr/SIMA200912001), Apr 29, 2009: UNKNOWN. ODOR. ON FLIGHT 3226 CREW REPORTED, RETURNED TO GATE DUE TO AN ELECTRICAL BURNING ODOR IN THE COCKPIT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTION, NO 
- [SDR SIMA200910406](https://openairdocs.org/sdr/SIMA200910406), Apr 9, 2009: FLOOR SUPPORT. CORRODED. DURING A MBV INSPECTION, THE CENTER OMEGA BEAM AT FRAME 38 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE OMEGA BEAM TO REMOVE THE DAMAGE. PREPARED A DOUBLER, F
- [SDR SIMA200909805](https://openairdocs.org/sdr/SIMA200909805), Apr 7, 2009: FLOOR SUPPORT. CORRODED. DURING A MBV INSPECTION, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. PERFORMED A CUTOUT TO REMOVE THE CORROSION. TRIMMED EPNEM5354701 AND 54703 FOR 
- [SDR SIMA200909806](https://openairdocs.org/sdr/SIMA200909806), Apr 6, 2009: FLOOR SUPPORT. CORRODED. DURING MBV, THE CENTER OMEGA BEAM WAS FOUND CORRODED. REMOVED CORROSION AND PERFORMED NDR INSPECTION. CLEANED, ALODINED, PRIMED AND FILLED BLEND AREA. FABRICATE
- [SDR SIMA200721801](https://openairdocs.org/sdr/SIMA200721801), Aug 2, 2007: RELAY. FAILED. EMERGENCY LIGHTS NOT ARM AND ELECTRICAL EMERGENCY ABNORMAL MESSAGE, ABORTED TAKEOFF. REMOVED AND REPLACED BATTERY RELAY BOX IAW EMB AMM 24-33-02. OPERATIONAL CH
- [SDR SIMA200716202](https://openairdocs.org/sdr/SIMA200716202), Jun 7, 2007: UNKNOWN. ODOR. SMOKE APPEARED AFTER SELECTING CRUISE THRUST, EMERGENCY DECLARED. DIVERTED TO JFK. PERFORMED TROUBLESHOOTING IAW ROLLS ROYCE FAULT ISOLATION MANUAL 72-00-00 AND
- [SDR SIMA200708202](https://openairdocs.org/sdr/SIMA200708202), Mar 21, 2007: UNKNOWN. SMOKE. SMOKE REPORTED IN CABIN AFTER NR 1 ENGINE START. PERFORMED VISUAL INSPECTION OF NR 1 ENGINE, APU AND BOTH PACKS WITH NO DEFECTS NOTED. PERFORMED ENGINE START OF
- [SDR SIMA200705707](https://openairdocs.org/sdr/SIMA200705707), Feb 16, 2007: FLOORBEAM. CORRODED. PREVIOUS REPAIR ON LEFT OMEGA BEAM AT FRAME 20 CORRODED. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS. CLEANED, TREATED AND RESTORED PROTECTIVE FINISH I
- [SDR SIMA200705706](https://openairdocs.org/sdr/SIMA200705706), Feb 13, 2007: SKIN. DENTED. FOUND RIGHT NOSE SKIN DENTED BETWEEN STRINGER 13 RIGHT AND 16 RIGHT AND FRAMES 7 AND 8. PERFORMED RECONTOUR OF DENT, PERFORMED NDT. FABRICATED AND INSTALLED REP
- [SDR SIMA200705101](https://openairdocs.org/sdr/SIMA200705101), Feb 13, 2007: SILL. CORRODED. BAGGAGE DOOR FRAME LOWER SILL FOUND CORRODED. REMOVED EXISTING SILL, CLEANED AND TREATED AREA. INSTALLED NEW SILL IAW EMB SRM 51-40-02. RESTORED PROTECTIVE FINI
- [SDR SIMA200704501](https://openairdocs.org/sdr/SIMA200704501), Feb 13, 2007: SILL. CORRODED. FOUND CARGO DOOR FRAME LOWER SILL CORRODED. REMOVED EXISTING SILL, CLEANED AND TREATED REPAIR AREA. INSTALLED NEW SILL IAW EMB SRM 51-40-02. RESTORED PROTECTIVE
- [SDR SIMA200630204](https://openairdocs.org/sdr/SIMA200630204), Oct 24, 2006: FLAP SYSTEM. MALFUNCTIONED. ON APPROACH SELECTED FLAPS 9, FLAPS STAYED AT 0 WITH ASSOCIATED EICAS MESSAGE "FLAP FAIL". NO CIRCUIT BREAKERS POPPED. COMPLIED WITH AIRCRAFT OPERATING MANUAL V
- [SDR SIMA200519315](https://openairdocs.org/sdr/SIMA200519315), Jul 7, 2005: FLOORBEAM. CORRODED. THE GALLEY AREA FORWARD DIGITAL PREVIOUS REPAIR WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR, BLENDED THE DAMAGE AREA OF THE FORWARD DIGITAL TO REMOVE THE CO
- [SDR SIMA200519314](https://openairdocs.org/sdr/SIMA200519314), Jul 7, 2005: FLOOR SUPPORT. CORRODED. THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE CENTER OMEGA BEAM TO REMOVE CORROSION FABRICATED A FILLER DOUBLER AND 2 SHIMS. 
- [SDR SIMA200317608](https://openairdocs.org/sdr/SIMA200317608), Jun 23, 2003: FLOORBEAM. CORRODED. ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM LOEW FLANGE AND WEB WERE FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 20 AND 22. BLENDED THE DAMGE
- [SDR SIMA200317604](https://openairdocs.org/sdr/SIMA200317604), Jun 21, 2003: FLOORBEAM. CORRODED. ABI - DURING AN IMBV INSPECTION, FOUND CORROSOIN ON THE EXISTING REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED EXISTING REPAIR. FABRICATED AN EXTERNAL ANGL
- [SDR SIMA200317401](https://openairdocs.org/sdr/SIMA200317401), Jun 18, 2003: SILL. CORRODED. ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER SILL, INSTALLED NEW CENTER SILL
- [SDR SIMA200307001](https://openairdocs.org/sdr/SIMA200307001), Mar 10, 2003: ODOR. DETECTED. CMH - FLT 4576 - AFTER TAKEOFF, THE FLIGHT ATTENDANT REPORTED STRONG BURNING RUBBER ODOR. PERFORMED PNEUMATIC BLEED CHECK WITH BOTH ENGINES AND APU OPERATING AN
- [SDR SIMA200232907](https://openairdocs.org/sdr/SIMA200232907), Nov 23, 2002: ENGINE. MALFUNCTIONED. LGA - FLT 4401 - AFTER TAKEOFF, CREW REPORTED LAVATORY SMOKE MESSAGE ON EICAS AND SMOKE IN CABIN. APU ALREADY ON MEL. MAINTENANCE REMOVED AND REPLACED THE LEFT 
- [SDR SIMA200232906](https://openairdocs.org/sdr/SIMA200232906), Nov 22, 2002: SOLENOID. MALFUNCTIONED. CMH - FLT 4564 - AFTER TAKEOFF, CREW REPORTED SMELLING FUMES IN COCKPIT AND FLIGHT ATTENDANT REPORTED A HAZE IN THE CABIN LIKE A BURNING PLASTIC SMELL. MAINTENA
- [SDR SIMA200131805](https://openairdocs.org/sdr/SIMA200131805), Nov 13, 2001: SUPPORT. CORRODED. THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY RAMP SUPPORT CORRODED. REMOVED RAMP SUPPORT AND INSTALLED NEW RAMP IAW EMB 135/145 SRM 51-40-02. (M
- [SDR SIMA200131806](https://openairdocs.org/sdr/SIMA200131806), Nov 13, 2001: FLOOR SUPPORT. CORRODED. ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY CENTER BEAM GUSSET CORRODED. RAI SERVICEABLE GALLEY CENTER BEAM IAW EMB 135 SRM 51-40-02. (M)
- [SDR SIMA200130304](https://openairdocs.org/sdr/SIMA200130304), Oct 25, 2001: FLOORBEAM. CORRODED. DURING MBV INSPECTION, FOUND CORROSION ON THE GALLEY LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUTOUT. FABRICATED FILLER AND DOUBLER. REPAIR DONE IAW EM
- [SDR SIMA200130303](https://openairdocs.org/sdr/SIMA200130303), Oct 25, 2001: FLOORBEAM. CORRODED. ABI - DURING MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE FORWARD DIGITAL IN GALLEY AREA. REMOVED CORROSION BY BLENDING IT OUT. PERFORMED AN NDT INSPECTIO
- [SDR SIMA07817](https://openairdocs.org/sdr/SIMA07817), Mar 19, 2001: ROD. OUT OF ADJ. ORD - FLT 4230 - DURING TAKEOFF ROLL, CREW NOTED T/REV DISAGREE MSG ON EICAS. CREW ABORTED TAKEOFF AND RETURNED TO GATE SAFELY. NO FURTHER INCIDENTS WERE REPORT
- [SDR SIMA0737](https://openairdocs.org/sdr/SIMA0737), Mar 14, 2001: RELAY. FAILED. ORD - FLT 4123 - DURING TAKEOFF ROLL, AFTER 80 KNOTS BUT PRIOR TO Y1 CREW RECEIVED THE NR 2 REVERSER DISAGREE MESSAGE. TAKEOFF WAS ABORTED. MESSAGE CLEARED DURI
- [SDR SIMA2093](https://openairdocs.org/sdr/SIMA2093), Jul 27, 2000: SWITCH. MALFUNCTIONED. BOS - FLT 5172 - DURING TAKEOFF ROLL, CREW NOTED NR 2 THRUST REVERSER DISAGREE MESSAGE. ABORTED TAKEOFF AND RETURNED TO GATE. NO FURTHER INCIDENTS REPORTED. THR

All 51: https://openairdocs.org/aircraft/N712AE/reports.md

## STCs that may be installed (OpenAirDocs) (72, 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-135LR)

- [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 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 ST04525AT](https://openairdocs.org/stc/ST04525AT): Installation of the Universal Avionics Flight Management System (FMS) Model No. UNS-1LW. SKH Aerospace 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 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 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 ST00010IB](https://openairdocs.org/stc/ST00010IB): Installation of convection oven model 1546-1 series, P/N 400-2095-01-R, on left-hand galley, P/N 135-85121-401. 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

All 72: https://openairdocs.org/aircraft/N712AE/stcs.md

## Related

- Other Embraer EMB-135LR aircraft: https://openairdocs.org/model/embraer-emb-135lr/aircraft.md

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