# N825AE: 2002 Embraer EMB-135KL

- Status: Valid registration
- Airframe: [Embraer EMB-135KL](https://openairdocs.org/model/embraer-emb-135kl) (registry code 3260302, 37 seats)
- Engine: [Allison AE-3007A1/3](https://openairdocs.org/engine/allison-ae-3007a1-3) (registry code 03036)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 145589
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 15, 2002
- Certificate issued: January 10, 2024
- Expires: January 31, 2031
- Mode S code: AB4373
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=825AE
- Page: https://openairdocs.org/aircraft/N825AE

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): 81 in force

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

- [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 2006-19-04](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
- [AD 2004-24-03](https://openairdocs.org/ad/2004-24-03): Internal o-ring seal · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 23 more. Effective Jan 3, 2005

### Matched by engine (Allison AE-3007A1/3)

- [AD 2020-16-13](https://openairdocs.org/ad/2020-16-13): Turbine Engine Compressor Section · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Aug 14, 2020
- [AD 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018
- [AD 2015-02-08](https://openairdocs.org/ad/2015-02-08): Turbine wheels · Rolls-Royce AE 2100D2, AE 2100D2A, AE 2100D3 and 11 more. Effective Mar 11, 2015
- [AD 2013-26-06](https://openairdocs.org/ad/2013-26-06): High-pressure turbine (HPT) stage 2 wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Feb 7, 2014
- [AD 2011-22-03](https://openairdocs.org/ad/2011-22-03): Low-cycle fatigue cracks · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 4 more. Effective Nov 17, 2011
- [AD 2009-24-04](https://openairdocs.org/ad/2009-24-04): Fan spinner · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 5 more. Effective Dec 28, 2009
- [AD 2007-24-05](https://openairdocs.org/ad/2007-24-05): Engine oil temperature · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 8 more. Effective Jan 2, 2008
- [AD 2004-04-05](https://openairdocs.org/ad/2004-04-05): Engine oil system · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Mar 9, 2004
- [AD 2003-25-08](https://openairdocs.org/ad/2003-25-08): 1st and 2nd stage turbine spacers · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 3 more. Effective Jan 21, 2004
- [AD 2001-25-05](https://openairdocs.org/ad/2001-25-05): Compressor Cone Shafts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jan 23, 2002
- [AD 2000-18-06](https://openairdocs.org/ad/2000-18-06): Digital Electronic Controls · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 22, 2000
- [AD 2000-13-01](https://openairdocs.org/ad/2000-13-01): Turbine Wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 1, 2000
- [AD 2000-11-22](https://openairdocs.org/ad/2000-11-22): Critical Life-Limited Parts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Aug 7, 2000
- [AD 98-11-32](https://openairdocs.org/ad/98-11-32): Sump Magnetic Chip Collector Plug · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Jun 18, 1998

### Historical (superseded or no longer in force)

- [AD 2008-13-14](https://openairdocs.org/ad/2008-13-14) (historical): Fuel system limitations (FSL) · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jul 30, 2008
- [AD 2007-12-17](https://openairdocs.org/ad/2007-12-17) (historical): Metallic tubes enclosing the vent and pilot valve wires · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Jul 19, 2007
- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 2006-04-02](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 2009-08-51](https://openairdocs.org/ad/2009-08-51) (historical): High-pressure turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 6 more. Effective May 27, 2009
- [AD 2008-19-51](https://openairdocs.org/ad/2008-19-51) (historical): AE 3007A, AE 3007A1, AE 3007A1E and 5 more
- [AD 2001-08-15](https://openairdocs.org/ad/2001-08-15) (historical): Oil System · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective May 14, 2001
- [AD 2000-09-05](https://openairdocs.org/ad/2000-09-05) (historical): Cone Shafts · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jul 5, 2000
- [AD 99-02-51](https://openairdocs.org/ad/99-02-51) (historical): Starter Shaft Seal · AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Apr 20, 1999

All 96: https://openairdocs.org/aircraft/N825AE/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 N825AE.

## 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 20050313009459I](https://openairdocs.org/incident/20050313009459I), Mar 13, 2005: Emb EMB135KL (N825AE), Buffalo, NY. (-23) On 03/13/2004 at 0959 edst an Emb-135-KL, operated by sima, while on approach to buf entered icing conditions. When the ice protection systems cycled on,…

## Service difficulty reports (80, 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 SIMA202006298003](https://openairdocs.org/sdr/SIMA202006298003), Jun 28, 2020: PRESSURE SWITCH. FAILED. SUPPLEMENTAL EMERG BRK LO PRES-C/A-ACCUMULATOR LOW PRESSURE SWITCH DEFERRED PER MEL 32-5,''M'' PROCUDERS IN SECTION 4 C/W. PERFORMED FIM TASK 32-44-00-810-801-A
- [SDR SIMA201912043001](https://openairdocs.org/sdr/SIMA201912043001), Dec 3, 2019: CONTROL VALVE. FAILED. AFTER TAKEOFF, THE NR 2 PACK VALVE CLOSED ON EICAS. RESET IAW QRH. CREW SMELLED SLIGHT BURNING SMELL. NO ODOR NOTED IAW ETN-EM-72-034. REMOVED AND REINSTALLED T
- [SDR SIMA2019111109004](https://openairdocs.org/sdr/SIMA2019111109004), Nov 9, 2019: WARNING MESSAGE. FALSE ACTIVATION. AFTER TAKE OFF "BAGGAGE DOOR" LIGHT ILLUMINATED RETURNED TO DFW "BAGGAGE DOOR LIGHT" TURNED OFF AFTER LANDING-C/A-DEFFERED BAGGAGE DOOR INDICATION PER MEL 52-5.
- [SDR SIMA201911087003](https://openairdocs.org/sdr/SIMA201911087003), Nov 7, 2019: CONNECTOR. DAMAGED. DURING PS-1 CHECK INSPECTION FOUND EMERGENCY FLOOR PROXIMITY STRIP LIGHT INOP-C/A-REPAIRED ELECTRICAL CONNECTOR AT AFT EMERGENCY FLOOR LIGHT STRIP PER SWPM 20-5
- [SDR SIMA20191031005](https://openairdocs.org/sdr/SIMA20191031005), Oct 31, 2019: WARNING SYSTEM. FALSE ACTIVATION. PACK 1 OVERHEAT IN CRUISE BURNING SMELL RIGHT BEFORE CATION MESSAGE-C/A-FOUND PACK 1 SWITCH IN MANUAL MODE AND IN FULL HOT POSITION. PERFORMED PACK DUCT INSP. I
- [SDR SIMA201908013001](https://openairdocs.org/sdr/SIMA201908013001), Jul 31, 2019: COUPLING. LEAKING. BLEED 2 LEAK IMMEDIATELY AFTER TAKEOFF ASSOCIATED EICAS MESSAGE AND RED LEAK ON BLEED 2 BUTTON-C/A-INSPECTED AND FOUND ENGINE START GROUND CONNECTION COUPLING T
- [SDR SIMA201812276001](https://openairdocs.org/sdr/SIMA201812276001), Dec 26, 2018: PITOT TUBE. CONTAMINATED. EMERGENCY DIVERT DUE TO UNRELIABLE AIRSPEED ON ALL 3 AIRSPEED INDICATORS AT FL 300. THE ISSUE DID NOT CLEAR UP UNTIL DESCENDING THROUGH FL 190 APPROXIMATLY. DEC
- [SDR SIMA20181031001](https://openairdocs.org/sdr/SIMA20181031001), Oct 31, 2018: FLASHLIGHT. BROKEN. FA FLASHLIGHT BROKEN. REMOVED AND REPLACED FA FWD FLASHLIGHT IAW AMM 33-50-16 AND PERFORMED OPS CHECK IAW AMM 33-51-01. OPS CHK GOOD. NO FURTHER DEFECTS NOTED A
- [SDR SIMA201808064001](https://openairdocs.org/sdr/SIMA201808064001), Aug 4, 2018: LIGHT. INOPERATIVE. FLOOR EMERGENCY LIGHT STRIPS NEAR THE LAVATORY WAS INOPERATIVE. REMOVED AND REPLACED FLOOR THE EMERGENCY LIGHTS IAW AMM 33-50-12. OPS CHECKED GOOD.
- [SDR SIMA201808064002](https://openairdocs.org/sdr/SIMA201808064002), Aug 4, 2018: LIGHT. INOPERATIVE. FLOOR EMERGENCY LIGHT STRIPS BY THE SERVICE DOOR WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT BY SERVICE DOOR IAW AMM 33-50-12. OPS CHECKED G
- [SDR SIMA201807050001](https://openairdocs.org/sdr/SIMA201807050001), Jul 4, 2018: RELAY. FAILED. SMELL OF BURNING ELECTRICAL STRONGEST ON CA SIDE DURING CRUSE. REMOVED AND REPLACED RELAY K0550 IAW AMM 20-13-02. OP CHECKING GOOD IAW AMM 27-25-00 SUBTASK 710-
- [SDR SIMA201807020003](https://openairdocs.org/sdr/SIMA201807020003), Jul 1, 2018: BATTERY. FAILED. WEAK SMELL OF "WARM/OVERHEATED" ELECTRONICS MOSTLY AT CRUISE FL220 AND AQT CA SIDE. REMOVED AND REPLACED BOTH COCKPIT EMER FLASHLIGHT BATTERIES IAW CMM 25-60-11
- [SDR SIMA201806065004](https://openairdocs.org/sdr/SIMA201806065004), Jun 5, 2018: SMOKE DETECTOR. NO TEST. CARGO SMOKE DETECTOR DID NOT TEST PROPERLY. LIGHT WILL NOT ILLUMINATE DURING THE TEST BUT AFTER TEST IT WILL. REMOVED AND REPLACED THE SMOKE DETECTOR IAW AMM 26
- [SDR SIMA2018083027010](https://openairdocs.org/sdr/SIMA2018083027010), May 27, 2018: SHEAR TIE. CRACKED. CRACK IN SHEAR CLIP AT FRAME 66 BETWEEN STRINGERS 6L AND 7L-C/A-INSTALLED EWIS PROTECTION IAW EMB SWPM 20-21-00. REMOVED LH PRECOOLER FLEXIBLE DUCT TO FOM IAW E
- [SDR SIMA20180527004](https://openairdocs.org/sdr/SIMA20180527004), May 27, 2018: FITTING. DAMAGED. LEFT AILERON PCA FITTING WAS NICKED AND GOUGED. REMOVED DAMAGE, AND FOUND TO BE OUT OF LIMITS IAW SRM 57-60-02. REMOVED AND REPLACED THE PCA FITTING IAW SRM 51-
- [SDR SIMA201805297003](https://openairdocs.org/sdr/SIMA201805297003), May 27, 2018: FITTING. DAMAGED. RIGHT AILERON PCA FITTING WAS NICKED AND GOUGED. REMOVED DAMAGE, AND DETERMINED TO BE OUT OF LIMITS IAW SRM 57-60-02. REMOVED THE PCA FITTING IAW SRM 51-40-02. 
- [SDR SIMA201805296001](https://openairdocs.org/sdr/SIMA201805296001), May 26, 2018: SIGN. INOPERATIVE. LEFT OVERWING EXIT UPPER EMERGENCY EXIT SIGN WAS INOPERATIVE. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-14. OPS CHECKED GOOD IAW 33-50-00.
- [SDR SIMA201805296003](https://openairdocs.org/sdr/SIMA201805296003), May 26, 2018: WIRE. BROKEN. LEFT EMERGENCY LIGHT, NR 6 LIGHT ASSY HAD A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12, OPS CHECKED GOOD
- [SDR SIMA201805296002](https://openairdocs.org/sdr/SIMA201805296002), May 26, 2018: POWER SUPPLY. INOPERATIVE. NUMBER 1 AISLE EMERGENCY LIGHT AND COCKPIT ENTRANCE LIGHT DID NOT OPERATE. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND BATTERY CHARGER IAW AMM 33-
- [SDR SIMA2018052120004](https://openairdocs.org/sdr/SIMA2018052120004), May 20, 2018: SHEAR TIE. CORRODED. CORROSION IN THE LATERAL L SHAPE AT FRAME 65, AT THE LOWER DOOR STOP. REMOVED THE DAMAGED SEGMENT OF LATERAL L SHEAR TIE AT FRAME 65 BETWEEN STRINGERS 15L AND 1
- [SDR SIMA2018052120003](https://openairdocs.org/sdr/SIMA2018052120003), May 20, 2018: SUPPORT. CRACKED. CRACKED LT OMEGA BEAM OTBD SUPPORT BETWEEN FRAMES 47 AND 48. CUT THE LT OMEGA OTBD SUPPORT IAW SRM 53-23-02. PERFORMED HFEC INSPECTION ALONG THE CUT LINE IAW ND
- [SDR SIMA2018052120002](https://openairdocs.org/sdr/SIMA2018052120002), May 20, 2018: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON THE LT OMEGA BEAM, FRAMES 23 TO 32. BLENDED CORROSION ON THE OMEGA BEAM IAW SRM 53-22-10 AND 51-10-03, FOUND TO BE OUT OF LIMITS. LOCATED, DR
- [SDR SIMA2018052120001](https://openairdocs.org/sdr/SIMA2018052120001), May 20, 2018: BEAM. CORRODED. COROSSION IN CARGO DOOR CUTOUT LOWER THRESHOLD BEAM BETWEEN FRAMES 65 AND 68. REMOVED THE THRESHOLD BEAM IAW SRM 51-40-02, SRM 51-20-03, AND CPM 51-21-04.
- [SDR SIMA2018052119005](https://openairdocs.org/sdr/SIMA2018052119005), May 19, 2018: SHEAR TIE. CRACKED. CRACKED SHEAR AT FRAME 65, BETWEEN STRINGER 7L AND 9L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, 53-31-04, FIGURE 202, CPM 51-21-04, CP
- [SDR SIMA2018052119001](https://openairdocs.org/sdr/SIMA2018052119001), May 19, 2018: SHEAR TIE. CRACKED. CRACKED SHEAR TIE, FRAME 68, BETWEEN STRINGERS 6L AND 7L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, AND SRM 53-31-04, FIG 205.
- [SDR SIMA2018052119002](https://openairdocs.org/sdr/SIMA2018052119002), May 19, 2018: SHEAR TIE. CRACKED. CRACKED SHEAR TIE AT FRAME 61, BETWEEN STRINGER 6L AND 7L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04, CPM 51-21-06 AND ETN
- [SDR SIMA2018052219003](https://openairdocs.org/sdr/SIMA2018052219003), May 19, 2018: SHEAR TIE. CRACKED. CRACK IN THE SHEAR TIE AT FRAME 67, BETWEEN STRINGER 6L AND 7L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, 53-31-04, FIGURE 204, CPM 51-
- [SDR SIMA2018052119004](https://openairdocs.org/sdr/SIMA2018052119004), May 19, 2018: SHEAR TIE. CRACKED. CRACKED SHEAR TIE AT FRAME 46, STRINGER 16L. REMOVED THE SHEAR TIE IAW SRM 51-40-02. LOCATED, DRILLED, ALODINED, AND INSTALLED A NEW SHEAR TIE IAW SRM 51-20-03,
- [SDR SIMA2018052119006](https://openairdocs.org/sdr/SIMA2018052119006), May 19, 2018: STRINGER. CRACKED. STRINGER 3L CRACKED AT FRAME 20, REMOVED THE STRINGER IAW SRM 51-40-02. LOCATED, DRILLED, ALODINED AND INSTALLED THE NEW STRINGER IAW SRM 51-20-03, CPM 51-21-04
- [SDR SIMA2018052119007](https://openairdocs.org/sdr/SIMA2018052119007), May 19, 2018: SHEAR TIE. CRACKED. CRACKED SHEAR TIE AT FRAME 24, BETWEEN STRINGERS 15R AND 16R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04, CPM 51-21-06 AND 
- [SDR SIMA20150702003](https://openairdocs.org/sdr/SIMA20150702003), Jul 2, 2015: FLASHLIGHT. DAMAGED. FORWARD CABIN EMER FLASHLIGHT HAS DAMAGED CONNECTOR. R & R FWD CABIN EMER FLASHLIGHT IAW WC 33-700-20. OPERATIONAL CHECKED GOOD.
- [SDR SIMA20150414005](https://openairdocs.org/sdr/SIMA20150414005), Apr 14, 2015: LIGHT. INOPERATIVE. 4TH FROM FWD EMER PROXIMITY LIGHTED STRIP IS INOPERATIVE. R & R 4TH FWD EMER PROXIMITY LIGHTED STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.
- [SDR SIMA20141014003](https://openairdocs.org/sdr/SIMA20141014003), Oct 14, 2014: INDICATOR. MALFUNCTIONED. STAND BY ATT CAGED BETWEEN 80 & 90 KTS ON TAKEOFF ROLL. PERFORMED FIM TASK 34-01-00-816-001-A. ATT FUNCTION SET TO TRUE VALUE IN STABILIZED CONDITION. CONSIDERE
- [SDR SIMA20141002005](https://openairdocs.org/sdr/SIMA20141002005), Oct 2, 2014: SWITCH. BROKEN. FLIGHT ATTENDANT FLASHLIGHT BUTTON ON & OFF BROKEN OFF. LOOSE FAS SEAT. REPAIRED WITH SERVICED FLASHLIGHT SWITCH. OPERATIONS CHECKED GOOD SMP.
- [SDR SIMA20140829004](https://openairdocs.org/sdr/SIMA20140829004), Aug 29, 2014: BRAKE ASSY. LEAKING. EMER BRAKE LOW PRESS ON EICAS. PARKING BRAKE NOT HOLDING PRESS. FOUND NR 3 BRAKE LEAKING & NR 4 BRAKE SHUTTLE VLV SEE NRWC 825-MIA-01756 FOR COMPLIANCE OF WORK 
- [SDR SIMA20140117002](https://openairdocs.org/sdr/SIMA20140117002), Jan 17, 2014: LIGHT. INOPERATIVE. EMERGENCY CEILING LIGHT AT LT EMERGENCY EXIT INOPERATIVE. R & R LAMP IAW AMM 33-50-09. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.
- [SDR SIMA20130807008](https://openairdocs.org/sdr/SIMA20130807008), Aug 7, 2013: HYDRAULIC SYSTEM. WARNING MESSAGE. DURING DESCENT AFTER GEAR RETRACTION, HYD SYS 1 QTY LOWERED TO THE BOTTOM OF THE GREEN RANGE, BUT WAS STILL IN THE GREEN RANGE. RECEIVED AN EICAS HYD 1 QTY LOW 
- [SDR SIMA20130623001](https://openairdocs.org/sdr/SIMA20130623001), Jun 23, 2013: ROLLER. DAMAGED. DURING B-INSPECTION, FOUND THE MAIN CABIN DOOR UPPER AFT FRAME ROLLER OUT OF ROUND AND DIFFICULT TO ROTATE. THE DOOR WAS DIFFICULT TO OPERATE. ACFT REMOVED FROM
- [SDR SIMA20130411017](https://openairdocs.org/sdr/SIMA20130411017), Apr 11, 2013: TERMINAL. MISSING. DURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 5 WIRE TERMINALS MISSING ACFT SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERG
- [SDR SIMA20130411016](https://openairdocs.org/sdr/SIMA20130411016), Apr 11, 2013: WIRE. DAMAGED. DURING MAINTENANCE INSPECTION FOUND THE NR 2 EMERGENCY LIGHT STRIP HAS DAMAGED WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT NR 2 
- [SDR SIMA20130411015](https://openairdocs.org/sdr/SIMA20130411015), Apr 11, 2013: GUSSET. CORRODED. DURING B INSPECTION FOUND THE LAVATORY CENTER BEAM GUSSET CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CORRODED LAVATORY CENTER BEAM GUSSET, DRILLED
- [SDR SIMA20130411014](https://openairdocs.org/sdr/SIMA20130411014), Apr 11, 2013: LIGHT. DAMAGED. DURING MAINTENANCE INSPECTION FOUND THE LEFT EMERGENCY LIGHT EXTRUSIONS (1, 2, 3, 4, 6) DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE
- [SDR SIMA20130401002](https://openairdocs.org/sdr/SIMA20130401002), Apr 1, 2013: FLASHLIGHT. INTERMITTENT. DURING MAINTENANCE INSPECTION FOUND THE FLASHLIGHT ABOVE FLIGHT ATTENDANT’S SEAT WORKING INTERMITTANT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLAC
- [SDR SIMA20130225003](https://openairdocs.org/sdr/SIMA20130225003), Feb 25, 2013: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION FOUND THE RIGHT WING FUSELAGE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FU
- [SDR SIMA20130114002](https://openairdocs.org/sdr/SIMA20130114002), Jan 14, 2013: LIGHT. INOPERATIVE. DURING B INSPECTION FOUND THE EMERGENCY LIGHT IN THE COCKPIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT EMERGENCY LIGHT
- [SDR SIMA20121216005](https://openairdocs.org/sdr/SIMA20121216005), Dec 16, 2012: FLASHLIGHT. INOPERATIVE. ON FLIGHT 4463 THE CREW REPORTED THE COCKPIT FLASHLIGHT WAS INOPERATIVE AND SWAPPED WITH AFT CABIN FLASHLIGHT. THE FLIGHT CREW PLACARD PER MEL 25-53 AUTH # 1208
- [SDR SIMA20121208001](https://openairdocs.org/sdr/SIMA20121208001), Dec 8, 2012: FLASHLIGHT. INOPERATIVE. ON FLIGHT 4243 THE CREW REPORTED THE AFT FLASHLIGHT WAS INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT IAW EMB-140 
- [SDR SIMA20120627002](https://openairdocs.org/sdr/SIMA20120627002), Jun 27, 2012: CRADLE. DAMAGED. DURING MAINTENANCE INSPECTION FOUND THE COCKPIT FLASHLIGHT CRADLE RETAINING TAB BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT 
- [SDR SIMA20120611008](https://openairdocs.org/sdr/SIMA20120611008), Jun 11, 2012: DISPLAY. FAILED. FLIGHT 4450 - FIRST OFFICER’S PRIMARY FLIGHT DISPLAY UNIT FAILED, TOTAL DARK AT 65 KTS, RETURNED TO GATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED TH
- [SDR SIMA20120425010](https://openairdocs.org/sdr/SIMA20120425010), Apr 25, 2012: LIGHT. INOPERATIVE. DURING B-INSPECTION FOUND THE LEFT FORWARD WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT WING FORWARD EM

All 80: https://openairdocs.org/aircraft/N825AE/reports.md

## STCs that may be installed (OpenAirDocs) (55, 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-135KL)

- [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 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 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 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 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 ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04537NY](https://openairdocs.org/stc/ST04537NY): Installation of Air Filtration. Kilroy Aviation LLC
- [STC ST09858SC](https://openairdocs.org/stc/ST09858SC): Installation of cabin automatic coffee brewing system. Safran Cabin Germany Gmbh
- [STC ST04255CH](https://openairdocs.org/stc/ST04255CH): Installation of an Automatic Dependent Surveillance-Broadcast (ADS-B Out) System. ENVOY AIR
- [STC ST03420NY](https://openairdocs.org/stc/ST03420NY): Installation of a Cabin Interior. Delta Engineering Corporation
- [STC ST02327LA](https://openairdocs.org/stc/ST02327LA): Installation of replacement proximity sensor harness assembly part numbers used on the nose and main landing gears. Safran Electrical Components USA Inc
- [STC 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 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 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 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 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 ST03999AT](https://openairdocs.org/stc/ST03999AT): Installation of a Single Honeywell HF-1050 HF Communication System. Chippewa Aerospace Inc
- [STC ST01619CH](https://openairdocs.org/stc/ST01619CH): Installation of a Lavatory Service Shutoff Valve. AeroControlex Group TransDigm Inc
- [STC ST03994AT](https://openairdocs.org/stc/ST03994AT): Installation of Bleed Air Coupling Sleeve Kit. Seal Dynamics
- [STC ST02638AT](https://openairdocs.org/stc/ST02638AT): Installation of an improved aircraft toilet rinse/fill shutoff valve and asociated hardware. Parker Hannifin Corporation, Parker Aerospace
- [STC ST03890AT](https://openairdocs.org/stc/ST03890AT): Installation of an L-3 Communications Micro Quick Access Recorder (MQAR). Chippewa Aerospace, Inc
- [STC ST02882CH-D](https://openairdocs.org/stc/ST02882CH-D): Installation of a Honeywell Flight Management System (FMS #2). Standard Aero
- [STC ST02803CH-D](https://openairdocs.org/stc/ST02803CH-D): Installation of a Honeywell KHF-1050 system. Standard Aero
- [STC ST01008LA-D](https://openairdocs.org/stc/ST01008LA-D): Installation of Hollingsead International Sentry One Cabin Mounted Video Camera System. Audio International

All 55: https://openairdocs.org/aircraft/N825AE/stcs.md

## Related

- Other Embraer EMB-135KL aircraft: https://openairdocs.org/model/embraer-emb-135kl/aircraft.md
- The Allison AE-3007A1/3 engine: https://openairdocs.org/engine/allison-ae-3007a1-3.md

---
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