# N837AE: 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: 145647
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 23, 2002
- Certificate issued: August 30, 2023
- Expires: August 31, 2030
- Mode S code: AB7260
- 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=837AE
- Page: https://openairdocs.org/aircraft/N837AE

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/N837AE/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 N837AE.

## 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 20140730014529I](https://openairdocs.org/incident/20140730014529I), Jul 30, 2014: Embraer EMB-135KL (N837AE), Flushing, NY, No damage. Envoy air, flight 3340, N837AE, was operating a revenue flight from laguardia airport, NY (lga) to knoxville, TN (tys). According to air carrier reports,…

## Service difficulty reports (94, 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 SIMA20200917003](https://openairdocs.org/sdr/SIMA20200917003), Sep 17, 2020: A/C PACK. OVERHEATED. ABORTED TAKEOFF PACK 2 OVERHEAT MSG. C/A FLIGHT CREW PLACARDED PACK 2 MEL 21-30 AUTH 090257-C MOC ID 373623.
- [SDR SIMA201911213011](https://openairdocs.org/sdr/SIMA201911213011), Nov 13, 2019: PUMP. FAILED. LO HYD 1 LO QTY DURING FLT IT DROPPED TO BOTTOM OF LEVEL AND GND OPS REPORT LEAKING FROMUNDER # 1 ENGINE FLUID-C/A-FOUND E1 LOWER COWLING WITH HYD FLUID COMING 
- [SDR SIMA201911143008](https://openairdocs.org/sdr/SIMA201911143008), Nov 13, 2019: PUMP. FAILED. LO HYD 1 LO QTY DURING FLT IT DROPPED TO BOTTOM OF LEVEL AND GND OPS REPORT LEAKING FROMUNDER # 1 ENGINE FLUID-C/A-FOUND E1 LOWER COWLING WITH HYD FLUID COMING 
- [SDR SIMA201911087001](https://openairdocs.org/sdr/SIMA201911087001), Nov 7, 2019: FLASHLIGHT. INOPERATIVE. AFT FA FLASHLIGHT INOP-C/A-FLIGHT CREW PLACARDED AFT FA FLASHLIGHT MEL 25-53 AUTH 110212-C MOC 056048. REMOVED AND REPLACED AFT FA FLASHLIGHT IAW AMM 33-50-16 O
- [SDR SIMA201910110006](https://openairdocs.org/sdr/SIMA201910110006), Oct 10, 2019: LAMP. INOPERATIVE. SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LAMP IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END
- [SDR SIMA201908196001](https://openairdocs.org/sdr/SIMA201908196001), Aug 16, 2019: SEAL. DAMAGED. AIRCRAFT UNABLE TO MAINTAIN PRESSURIZATION. REMOVED AND REPLACED MAIN DOOR RUBBER TRIM SEAL IAW AMM 52-18-04 AND PERFORMED FUNCTIONAL TEST FOR CABIN LEAKAGE WIT
- [SDR SIMA201904110002](https://openairdocs.org/sdr/SIMA201904110002), Apr 10, 2019: LAMP. INOPERATIVE. COCKPIT EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-05-000-801-A AND 33-50-05-400-801-A. OPC GOOD NO FURTHER DE
- [SDR SIMA20190323001](https://openairdocs.org/sdr/SIMA20190323001), Mar 23, 2019: SOLENOID VALVE. FAILED. LDG GEAR LEVER DISAGEE ON RETRATION WITH 3 RED GEAR INDICATION RECYCLED GEAR IAW QRH PROCEDUR, 3 GREEN DOWN INDICATION PREFORMED OVERWEIGHT LANDING "TRANSFERRED
- [SDR SIMA20190102003](https://openairdocs.org/sdr/SIMA20190102003), Jan 2, 2019: INVERTER. INOPERATIVE. DURING COURTESY CHECK FOUND EMERGENCY EXIT MARKING SIGN ABOVE FLIGHT ATTENDANT SEAT INOP. REMOVED AND REPLACED EMERGENCY LIGHT DC/AC INVERTER IAW AMM 33-50-11 O
- [SDR SIMA201812242001](https://openairdocs.org/sdr/SIMA201812242001), Dec 22, 2018: LAMP. INOPERATIVE. RH EXTERIOR EMERGENCY LIGHT ON OVERWING INOP.-C/A-RAR EXTERNAL EMERGENCY LIGHT RH LAMP IAW EMB 140 AMM 33-50-10. OPC GOOD.
- [SDR SIMA2018091008002](https://openairdocs.org/sdr/SIMA2018091008002), Sep 8, 2018: BOLT. MISSING. EMERGENCY PARKING BRAKE IS DIFFICULT TO SET. OPENED PARKING BRAKE MECHANISM AND FOUND BOLT MISSING. REMOVED AND REPLACED IAW AMM 32-44-11. OPS CHECK GOOD. NO FU
- [SDR SIMA20180426001](https://openairdocs.org/sdr/SIMA20180426001), Apr 26, 2018: FIRE DETECTOR. FALSE ACTIVATION. CAPTAIN REPORTED A CARGO FIRE WARNING DURING SHORT FINAL, CARGO FIRE BOTTLES DISCHARGED, AN EMERGENCY WAS DECLARED. FIRE DEPT INSPECTION REVEALED NO EVIDENCE OF
- [SDR SIMA2018042019005](https://openairdocs.org/sdr/SIMA2018042019005), Apr 19, 2018: PRESSURE SWITCH. INOPERATIVE. RUDDER OVERBOOST AFTER TAKE OFF. RETURNED TO DEPARTURE. PERFORMED TROUBLESHOOTING IAW FIM 27-22-10, FOUND THE NR 1 RUDDER PRESSURE SWITCH INOPERATIVE. REMOVED A
- [SDR SIMA2018042014006](https://openairdocs.org/sdr/SIMA2018042014006), Apr 14, 2018: LIGHT. INOPERATIVE. EMERGENCY LIGHT NR 8 NOT WORKING. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12 . OPS CHECKED GOOD
- [SDR SIMA20180413012](https://openairdocs.org/sdr/SIMA20180413012), Apr 13, 2018: SKIN. CRACKED. SKIN PLATE CRACKED AT FRAME 81 BETWEEN STRINGERS 1L - 2R. REPAIRED THE SKIN IAW SRM 51-40-02
- [SDR SIMA2018042011007](https://openairdocs.org/sdr/SIMA2018042011007), Apr 11, 2018: SKIN. CRACKED. RIGHT REAR FUSELAGE SKIN CRACKED AT FRAME 75, BETWEEN STRINGERS 1R AND 2R. REPAIRED THE SKIN IAW SRM 53-31-01.
- [SDR SIMA2018042011006](https://openairdocs.org/sdr/SIMA2018042011006), Apr 11, 2018: FITTING. CRACKED. FITTING AT FRAME 19 STRINGER 3L CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-40-02.
- [SDR SIMA20180410003](https://openairdocs.org/sdr/SIMA20180410003), Apr 10, 2018: SUPPORT. GOUGED. SERVICE DOOR LOWER VERTICAL SUPPORT GOUGED. REPAIRED THE VERTICAL SUPPORT IAW ERS-EM-52MR-869.
- [SDR SIMA201804192003](https://openairdocs.org/sdr/SIMA201804192003), Apr 9, 2018: SKIN. DENTED. FUSELAGE SKIN DENTED BETWEEN FRAMES 19 - 20, STRINGERS 20R - 21R. THE SKIN WAS REPAIRED IAW SRM 53-21-01, TYPE A1.
- [SDR SIMA201804192002](https://openairdocs.org/sdr/SIMA201804192002), Apr 8, 2018: SUPPORT. CRACKED. CORRODED AND CRACKED LT EMERGENCY EXIT LOWER LOWER WEB SUPPORT. REMOVED AND REPLACED THE WEB SUPPORT IAW SRM 51-40-02.
- [SDR SIMA201804192005](https://openairdocs.org/sdr/SIMA201804192005), Apr 7, 2018: SKIN. CRACKED. RIGHT ELEVATOR EXTERNAL UPPER SKIN IS CRACKED AT THE OUTBD AFT CORNER. REPAIRED THE ELEVATOR SKIN IAW EO EM-53MR-XXXX.
- [SDR SIMA201804192006](https://openairdocs.org/sdr/SIMA201804192006), Apr 7, 2018: CONNECTOR. MISSING. EMERGENCY LIGHT, NR 1 CONNECTOR MISSING. INSTALLED THE CONNECTOR IAW SWPM 20-21-00.
- [SDR SIMA201804191004](https://openairdocs.org/sdr/SIMA201804191004), Apr 7, 2018: SKIN. CRACKED. RIGHT ELEVATOR EXTERNAL LOWER SKIN IS CRACKED AT THE OUTBD AFT CORNER. REPAIRED THE ELEVATOR SKIN IAW EO EM-55MR-660.
- [SDR SIMA201804191005](https://openairdocs.org/sdr/SIMA201804191005), Apr 6, 2018: FLOOR SUPPORT. CORRODED. RIGHT OMEGA BEAM IN THE LAVATORY CORRODED AT FRAME 60. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-3214
- [SDR SIMA2018041900004](https://openairdocs.org/sdr/SIMA2018041900004), Apr 2, 2018: DOOR FRAME. CRACKED. RIGHT OVERWING EXIT FWD FRAME CRACKED AT UPPER END. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02
- [SDR SIMA2018041900005](https://openairdocs.org/sdr/SIMA2018041900005), Apr 2, 2018: PROFILE. CORRODED. FRAME 65 L-SHAPE PROFILE LWR END AT CARGO DOOR CUTOUT HAS AN AREA OF CORROSION. REMOVED AND REPLACED WITH SERVICEABLE SECTION OF THE PROFILE IAW SRM 53-31-04 IT
- [SDR SIMA2018041900006](https://openairdocs.org/sdr/SIMA2018041900006), Apr 2, 2018: FRAME. CRACKED. FRAME 10 UNDER COPILOTS WINDOW IS CRACKED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.
- [SDR SIMA2018041900003](https://openairdocs.org/sdr/SIMA2018041900003), Apr 2, 2018: DOOR SILL. CORRODED. CARGO DOOR CENTER SILL CORRODED. REMOVED AND REPLACED CARGO CUTOUT CENTER SILL IAW EMB 140 SRM 51-40-02.
- [SDR SIMA2018041906003](https://openairdocs.org/sdr/SIMA2018041906003), Mar 26, 2018: FITTING. DAMAGED. LEFT AILERON DAMPER FITTING DAMAGED. REMOVED AND REPLACED THE DAMPER FITTING IAW EO EM-27MR-112.
- [SDR SIMA20180326004](https://openairdocs.org/sdr/SIMA20180326004), Mar 26, 2018: FITTING. DAMAGED. RIGHT AILERON DAMPER FITTING DAMAGED. REMOVED AND REPLACED THE RT DAMPER FITTING IAW EO EM-27MR-112.
- [SDR SIMA201804256005](https://openairdocs.org/sdr/SIMA201804256005), Feb 26, 2018: LIGHT. DAMAGED. FOUR LT EMERGENCY LIGHT STRIP EXTRUSIONS ARE DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHTS IAW AMM 33-50-12.
- [SDR SIMA20140817004](https://openairdocs.org/sdr/SIMA20140817004), Aug 17, 2014: LIGHT. INOPERATIVE. SERVICE DOOR EMER LIGHT INOPERATIVE. R & R LAMP WITH NEW OPERATIONS CHECK GOOD ALL WORK IAW MM CH 33-50-10.
- [SDR SIMA20140730010](https://openairdocs.org/sdr/SIMA20140730010), Jul 30, 2014: ENGINE. FAILED. IAW ITEM NR 1 ON LOG PAGE 3529025 OIL FOUND NR 2 ENG DURING BORESCOPE INSPECTION. R & R NR 2 ENG IAW WC 71-000-00. OPERATIONS CHECKED GOOD & LEAK CHECKED GOOD.
- [SDR SIMA20140730004](https://openairdocs.org/sdr/SIMA20140730004), Jul 30, 2014: WARNING SYSTEM. ACTIVATED. LAVATORY SMOKE ON EICAS. COMPLIED WITH ETN-EM-72-034. BORESCOPE ON BOTH ENGS REQUESTED.
- [SDR SIMA20140730003](https://openairdocs.org/sdr/SIMA20140730003), Jul 30, 2014: UNKNOWN. SMOKE. FLIGHT ATTENDANT REPORTED SMOKE COMING FROM LAVATORY, PAX COUGHING ALONG WITH FLIGHT ATTENDANT. COMPLIED WITH ETN-EM-72-034. BORESCOPE ON BOTH ENGS REQUESTED.
- [SDR SIMA20140729001](https://openairdocs.org/sdr/SIMA20140729001), Jul 29, 2014: BALLAST. BURNED. SMOKE IN CABIN FROM MULTIPLE PSU'S. DURING TROUBLESHOOTING FOUND PSU BALLAST BETWEEN SEATS 14A - 15A BURNED. R & R BALLAST IAW AMM 33-21-05. OPERATIONS CHECKED 
- [SDR SIMA20140624006](https://openairdocs.org/sdr/SIMA20140624006), Jun 24, 2014: SHROUD. INOPERATIVE. AFTER LANDING DURING FLAP RETRACTION, FLAP FAILED MSG & FLAPS STUCK AT 12 DEGREES. R & R LT INBD FLAP DRIVER SHROUD TIP IAW SPM. FLAPS SYS OPERATIONS CHECKED GO
- [SDR SIMA20140521001](https://openairdocs.org/sdr/SIMA20140521001), May 21, 2014: HOLDER. BROKEN. DURING FLIGHT 3352 FOUND CAPTAIN`S FLASHLIGHT HOLDER BROKEN. THE ACFT WAS REMOVED FROM SERVICE. CORRECTIVE ACTION R & R CAPTAIN'S FLASHLIGHT HOLDER ASSEMBLY IAW
- [SDR SIMA20140404010](https://openairdocs.org/sdr/SIMA20140404010), Apr 4, 2014: CRADLE. BROKEN. FLIGHT ATTENDANT FWD FLASHLIGHT CRADLE IS BROKEN. REMOVED AND REPLACED FWD FLASHLIGHT CRADLE IAW AMM 33-50-16. OPS CHECKED GOOD.
- [SDR SIMA20140326007](https://openairdocs.org/sdr/SIMA20140326007), Mar 26, 2014: LIGHT. INOPERATIVE. EMERGENCY LIGHT ON FLIGHT DECK INOPERATIVE. R & R FLT DECK EMERGENCY LAMP IAW AMM 33-50-05. LIGHT OPERATIONS CHECKED GOOD.
- [SDR SIMA20140326005](https://openairdocs.org/sdr/SIMA20140326005), Mar 26, 2014: HOLDER. BROKEN. FLASHLIGHT BRACKET OVER FLIGHT ATTENDANT`S JUMP SEAT IS BROKEN. R & R WITH SERVICEABLE FWD FLIGHT ATTENDANT’S HOLDER IAW AMM 33-50-16. OPERATIONS CHECKED OK.
- [SDR SIMA20140326003](https://openairdocs.org/sdr/SIMA20140326003), Mar 26, 2014: HOLDER. BROKEN. FLASHLIGHT BRACKET OVER FLIGHT ATTENDANT`S JUMP SEAT IS BROKEN. R & R WITH SERVICEABLE FWD FLIGHT ATTENDANT’S FLASHLIGHT HOLDER IAW AMM 33-50-16. OPERATIONS CHE
- [SDR SIMA20140204003](https://openairdocs.org/sdr/SIMA20140204003), Feb 4, 2014: LIGHT. INOPERATIVE. LEFT EXTERIOR FWD EMERGENCY LIGHT INOPERATIVE. R & R LT FWD EXTERIOR EMERGENCY LAMP IAW TASK 33-50-10-000-801-A & TASK 33-50-10-400-801-A END.
- [SDR SIMA20131025004](https://openairdocs.org/sdr/SIMA20131025004), Oct 25, 2013: LIGHT. INOPERATIVE. EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-50-12, OPS CHECKED GOOD.
- [SDR SIMA20130816002](https://openairdocs.org/sdr/SIMA20130816002), Aug 16, 2013: UNKNOWN. ODOR. F/A REPORTS BURNING ODOR AT ROW 15. PERFORMED OPS CHECK IAW 33-21-00 OF PASSENGER CABIN LIGHTS. NO ODOR NOTED NO FURTHER DEFECT AT THIS TIME, OPS GOOD.
- [SDR SIMA20130704002](https://openairdocs.org/sdr/SIMA20130704002), Jul 4, 2013: MECHANISM. LACK OF LUBE. THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE ACFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN PAX DOOR LOCKING AND UNLOCKING MECHANI
- [SDR SIMA20130325002](https://openairdocs.org/sdr/SIMA20130325002), Mar 25, 2013: PUMP. MALFUNCTIONED. ON FLIGHT 4057 THE CREW REPORTED THEY RECEIVED INITIALLY HYD 1 LOW QTY MESSAGE THEN ROUGHLY FORTY MINUTES LATER HYD SYS 1 FAIL THEN AIL SYS 1 INOPERABLE. THE CR
- [SDR SIMA20130215004](https://openairdocs.org/sdr/SIMA20130215004), Feb 15, 2013: FLASHLIGHT. DEFECTIVE. ON FLIGHT 4233 THE CREW REPORTED THE RETENSION LATCH ON THE FIRST OFFICER'S FLASHLIGHT HOLDER WOULD NOT HOLD THE FLASHLIGHT IN POSITION TO CHARGE. THE AIRCRAFT 
- [SDR SIMA20130128006](https://openairdocs.org/sdr/SIMA20130128006), Jan 28, 2013: BRACKET. BROKEN. DURING B INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT HOLDER BRACKET BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT HOLDER BRAC
- [SDR SIMA20121226002](https://openairdocs.org/sdr/SIMA20121226002), Dec 26, 2012: FLASHLIGHT. INOPERATIVE. FLASHLIGHT BEHIND CAPTAINS SEAT INOP. REPLACED FLASHLIGHT.

All 94: https://openairdocs.org/aircraft/N837AE/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/N837AE/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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