# N836AE: 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: 145635
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 13, 2002
- Certificate issued: October 6, 2025
- Expires: October 31, 2032
- Mode S code: AB6EA9
- Registered owners: [Corporate Flight Management Inc DBA](https://openairdocs.org/faa-owner/CORPORATE%20FLIGHT%20MANAGEMENT%20INC%20DBA), [Contour Aviation](https://openairdocs.org/faa-owner/CONTOUR%20AVIATION)
- Location: [Smyrna, TN](https://openairdocs.org/faa-place/TN/Smyrna)
- Owner type: Corporation
- Owner's area on the map: 35.9628° N, 86.5297° W: Placed by OpenAirDocs at the center of ZIP code 37167, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=836AE
- Page: https://openairdocs.org/aircraft/N836AE

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/N836AE/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 N836AE.

## FAA accident and incident reports

None matched to N836AE.

## Service difficulty reports (82, 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 SIMA2020031312001](https://openairdocs.org/sdr/SIMA2020031312001), Mar 12, 2020: UNKNOWN. ODOR. ON TAXI OUT ENG #1 ON, APU BLEED RUNNING PACKS. STRONG OIL SMELL OR FLIGHT DECK "DIRTY SOCK SMELL".-C/A-COMPLIED WITH EMB 140 ETN-EM-72-034 NO FAULTS/ SMELL FOU
- [SDR SIMA201912021002](https://openairdocs.org/sdr/SIMA201912021002), Dec 1, 2019: DISPLAY. FAILED. WHILE AT ALTITUDE, A FISHY SMELL FILLED THE COCKPIT AND CABIN, THE SMELL DISIPATED DURING DESCENT. REMOVED AND REPLACED THE NR 1 PFD IAW AMM 34-22-01. EFIS OPT 
- [SDR SIMA2019111109001](https://openairdocs.org/sdr/SIMA2019111109001), Nov 9, 2019: FLASHLIGHT. MISSING. MEL 2553 - AUTH# 11-252-CREF ORG LG PG 4500501/1 PAX STOLE AFT CABIN FLASHLIGHT-C/A-INSTALLED NEW FLASHLIGHT IAW EMB140 AMM 33-50-16. OPS CHECK GOOD. MEL RESTOR
- [SDR SIMA201910243005](https://openairdocs.org/sdr/SIMA201910243005), Oct 23, 2019: FLASHLIGHT. INOPERATIVE. SUPPLEMENTAL AFT CABIN FLASH LIGHT INOP. CHARGING BASE NOT WORKING.-C/A-ITEM DEFERRED PER MEL 25-53 AUTH# 100787-C. REMOVED AND REPLACED AFT CABIN FLASH LIGHT P
- [SDR SIMA201910109004](https://openairdocs.org/sdr/SIMA201910109004), Oct 9, 2019: WIRE. BROKEN. AFT EMERGENCY FLASHLIGHT INOPERATIVE. REPAIRED BROKEN GROUND WIRE ON AFT FLASHLIGHT HARNESS IAW SWPM 20-21-00. OPS CHECKED GOOD IAW AMM 33-51-01.
- [SDR SIMA20190714003](https://openairdocs.org/sdr/SIMA20190714003), Jul 14, 2019: LIGHT. INOPERATIVE. SUPPLEMENTAL EMERGENCY LIGHT BETWEEN ROW 7&8 INOP. C/A-DEFERRED EMERGENCY LIGHT STRIP IAW MEL 33-30. REMOVED AND REPLACED ROW 7 AND 8 EMERGENCY FLOOR PROXIMITY 
- [SDR SIMA20190613001](https://openairdocs.org/sdr/SIMA20190613001), Jun 13, 2019: SWITCH. DIRTY. AFTER TAKEOFF, CAPTAIN'S PITCH TRIM WOULD NOT WORK. PTRIM MAIN INOP THEN DISPLAYED ON EICAS-C/A-CLEANED CAPT'S AND 1ST OFFICERS PITCH TRIM SWITCHES. PERFORMED O
- [SDR SIMA201812030002](https://openairdocs.org/sdr/SIMA201812030002), Nov 30, 2018: CHARGER. INOPERATIVE. LAST 3 EMERGENCY LIGHT STRIPS INOP-C/A-REMOVED AND REPLACED #4 BATT AND CHARGER AND #6 INVERTER IAW EMB 140 AMM 33-50-11 AND W/C 33-700-19. OPS CHK GOOD. INVERT
- [SDR SIMA2018080130006](https://openairdocs.org/sdr/SIMA2018080130006), Jul 30, 2018: HANDLE. DEFECTIVE. PARKING BRAKE HANDLE VERY DIFFICULT TO PULL AND TWIST TO SET. SERVICED EMERG PARKING BRAKE HANDLE IAW AMM 32-44-10.
- [SDR SIMA20180318003](https://openairdocs.org/sdr/SIMA20180318003), Mar 18, 2018: LAMP. INOPERATIVE. LEFT EXIT ROW CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-50-07. OPS CHECKED GOOD.
- [SDR SIMA20180110002](https://openairdocs.org/sdr/SIMA20180110002), Jan 10, 2018: WARNING MESSAGE. FALSE ACTIVATION. ON DEPARTURE, RECEIVED NUMEROUS MESSAGES ON THE CAPTAIN`S FMS. IC600-L, RW FAIL, ADC INPUT INVALID, FAIL, TAS INVALID, IC-600-R BUSS FAIL, , NO HEADING IC600 L 
- [SDR SIMA20171119002](https://openairdocs.org/sdr/SIMA20171119002), Nov 19, 2017: SKIN. CRACKED. SKIN CRACKED AT FR 77 STR 3R. REPAIRED FR 77 STR 3R IAW SRM 53-32-01 ITEM 3FIGURE 204 SHEET 3.
- [SDR SIMA20171119003](https://openairdocs.org/sdr/SIMA20171119003), Nov 19, 2017: SKIN. DAMAGED. MAIN DOOR EXTERNAL DOOR SKIN HAS MULTIPLE GOUGES AND POSSIBLE CRACK. PERFORMED PERMANENT REPAIR OF PAX DOOR SKIN IAW ERS-EM-52MR-830.
- [SDR SIMA20171116004](https://openairdocs.org/sdr/SIMA20171116004), Nov 16, 2017: FRAME. CRACKED. RT FRAME 10 IS CRACKED ON UPPER AFT SIDE. REMOVED AND REPLACED RT FRAME 10 IAW SRM 53-00-04.
- [SDR SIMA20171113003](https://openairdocs.org/sdr/SIMA20171113003), Nov 13, 2017: SKIN. CRACKED. LT UPPER AFT FUSELAGE CRACKED ABOVE STRINGER 2L JUST AFT OF FR75. REPAIRED LT UPPER AFT FUSELAGE SKIN ABOVE STRINGER 2L AND JUST AFT OF FRAME 75 IAW SRM 53-31-0
- [SDR SIMA20171109008](https://openairdocs.org/sdr/SIMA20171109008), Nov 9, 2017: DOOR. CRACKED. REAR ELECTRONICS COMPARTMENT DOOR CRACKED UNDER SUPPORT BRACKET FOR PIN. REPAIRED REAR ELECTRONICS COMPARTMENT DOOR IAW SRM 52-44-02.
- [SDR SIMA20171101002](https://openairdocs.org/sdr/SIMA20171101002), Nov 1, 2017: LIGHT. INOPERATIVE. SEAT 11A EMERGENCY EXIT LIGHT ON PSU INOP. REMOVED AND INSTALLED SEAT 11A EMERGENCY EXIT LIGHT BULB ON PSU AS REQUIRED.
- [SDR SIMA20160709004](https://openairdocs.org/sdr/SIMA20160709004), Jul 9, 2016: CONTROL MODULE. INOPERATIVE. EMERGENCY LIGHT NOT ARMED ILLUMINATES OCCASIONALLY WITH SWITCH IN ARMED POSITION. REMOVED AND REPLACED CABIN LIGHT CONTROL MODULE ASSY IAW AMM 33-21-01. OPS CHE
- [SDR SIMA20160709003](https://openairdocs.org/sdr/SIMA20160709003), Jul 9, 2016: CONTROL MODULE. FAILED. AFTER GPU HOOKUP, POWER DROPPED OFFLINE WITH CHATTERING RELAYS AND STRONG ELECTRICAL BURNING ODOR IN CABIN. REMOVED AND REPLACED CEILING BALAST IAW AMM 33-21-05
- [SDR SIMA20160709002](https://openairdocs.org/sdr/SIMA20160709002), Jul 9, 2016: UNKNOWN. ODOR. FA SAYS EKECTRCAL BURN ODOR FROM FOWARD CABIN. REMOVED AND REPLACED CEILING BALLAST IAW AMM 33-21-05 REMOVED AND REPL.ACED 1A PSU ASSY IAW 25-22-05. OPS CHECKED
- [SDR SIMA20160221002](https://openairdocs.org/sdr/SIMA20160221002), Feb 21, 2016: CONTROLLER. FAILED. AUTO PRESSURIZATION CONTROLLER FAILED, HAD TO MANUALLY CONTROL THE PRESSURIZATION. R & R AUTO PRESSURIZATION DIGITAL CONTROLLER IAW AMM 21-31-01. OPERATIONS CHE
- [SDR SIMA20160204003](https://openairdocs.org/sdr/SIMA20160204003), Feb 4, 2016: LIGHT. INOPERATIVE. OVERHEAD EMER LIGHT IN COCKPIT INOPERATIVE. R & R BULB IN OVERHEAD EMER LIGHT IN COCKPIT IAW AMM 33-50-05. OPERATIONS CHECKED GOOD.
- [SDR SIMA20151230001](https://openairdocs.org/sdr/SIMA20151230001), Dec 30, 2015: HOLDER. BROKEN. CAPTAINS FLASHLIGHT HOLDER BROKEN. R & R CAPTAINS FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.
- [SDR SIMA20150827003](https://openairdocs.org/sdr/SIMA20150827003), Aug 27, 2015: LIGHT. INOPERATIVE. AFT AISLE EMER LIGHT ASSEMBLY INOPERATIVE. R & R AFT AISLE EMER LIGHT ASSEMBLY BULB IAW AMM 33-50-08. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150706002](https://openairdocs.org/sdr/SIMA20150706002), Jul 6, 2015: DOOR. LACK OF LUBE. FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR HARD TO OPEN. LUBRICATED ALL MAIN CABIN DOOR POINTS & PERFORMED MULTIPLE DOOR CLOSURE CHECKS. OPERATIONS CHECKED NORMAL
- [SDR SIMA20150421005](https://openairdocs.org/sdr/SIMA20150421005), Apr 21, 2015: FRAME. CRACKED. FRAME 17 IS CRACKED BETWEEN STRINGER 12R & 13R. THIS IS A MAJOR REPAIR. REPAIRED FRAME 17 IAW ERS-EM-53MR-1259.
- [SDR SIMA20150421006](https://openairdocs.org/sdr/SIMA20150421006), Apr 21, 2015: STRINGER. BENT. STRINGER 12R IS BENT BETWEEN FRAME 16 & 19. THIS IS A MAJOR REPAIR. REPAIRED STRINGER 12R IAW ERS-EM-53MR-1259.
- [SDR SIMA20150421007](https://openairdocs.org/sdr/SIMA20150421007), Apr 21, 2015: STRINGER. BENT. STRINGER 13R IS BENT BETWEEN FRAME 16 & 19. THIS IS A MAJOR REPAIR. REPAIRED STRINGER 13R IAW ERS-EM-53MR-1259.
- [SDR SIMA20150329003](https://openairdocs.org/sdr/SIMA20150329003), Mar 29, 2015: ENGINE. LEAKING. DURING NORMAL CRUISE FLIGHT AT 36,000 FT. OBSERVE NR 1 ENGINE OIL TEMP WENT UP GRADUALLY TO THE RED ARC INDICATION 156. REDUCE THE THRUST LEVEL IAW AOM AND NOTH
- [SDR SIMA20150126008](https://openairdocs.org/sdr/SIMA20150126008), Jan 26, 2015: ACM. SEIZED. DURING CLIMB CREW HEARD A LOW INTERMITTENT NOISE FOLLOWED BY A LIGHT SMOKE ENTERING THE COCKPIT THROUGH THE CEILING VENTS. CREW TURNED OFF PACKS & SMOKE DISSIPA
- [SDR SIMA20150121003](https://openairdocs.org/sdr/SIMA20150121003), Jan 21, 2015: VALVE. FAILED. ABORTED TAKEOFF, AT LOW SPEED NR 2 ENGINE ATTCS NO MARGIN EICAS MESSAGE. NR 2 ENGINE EXCEEDENCE EICAS CAUTION. NR 2 ENGINE HAS VALVE FAIL EICAS MESSAGE. TROUBLE
- [SDR SIMA20141221005](https://openairdocs.org/sdr/SIMA20141221005), Dec 21, 2014: DOOR. DAMAGED. PREFLIGHT FOUND DAMAGE TO CARGO DOOR, VENT HANDLE WILL NOT STAY FLUSHED, APPEARS TO LEAK AIR.
- [SDR SIMA20141211002](https://openairdocs.org/sdr/SIMA20141211002), Dec 11, 2014: ROLLER. LACK OF LUBE. FLIGHT ATTENDANT ADVICE MAIN CABIN DOOR HARD TO OPEN. CLEANED & LUBRICATED MAIN DOOR FRAME ROLLERS IAW MM 53-21-02. DOOR LOAD OPEN TEST GOOD IAW MM 52-18-00.
- [SDR SIMA20140720005](https://openairdocs.org/sdr/SIMA20140720005), Jul 20, 2014: LIGHT. INOPERATIVE. PAX COMPARTMENT ROW 11 RT EMER LIGHT INOPERATIVE. R & R PAX COMPARTMENT EMER LAMP AT ROW 11 RT IAW AMM 33-50-08. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140501001](https://openairdocs.org/sdr/SIMA20140501001), May 1, 2014: PROXIMITY SENSOR. FAILED. LG AIR & GND FAIL CAUTION ON EICAS SHORTLY AFTER ROTATION. R & R INTERCHANGEABLE NLG PROX SWITCH IAW AMM 32-62-02, OPERATIONS CHECKED GOOD.
- [SDR SIMA20140419001](https://openairdocs.org/sdr/SIMA20140419001), Apr 19, 2014: FLASHLIGHT. DEFECTIVE. SIGNIFICANT ELEC BURNING SMELL IN MIDDLE OF CABIN & COCKPIT DURING CRUISE FLIGHT. FOUND ODOR COMING FROM PILOTS EMERGENCY FLASHLIGHT. R & R FLASHLIGHT IAW AMM 3
- [SDR SIMA20140318004](https://openairdocs.org/sdr/SIMA20140318004), Mar 18, 2014: HINGE. OUT OF ADJUST. CABIN ENTRY DOOR HARD TO OPEN. ADJUSTED MAIN DOOR SIDE HINGE BY INSERTING WASHER IN TO DOOR FRAME LOWER SUPPORT IAW ETN EM-52-013R1.
- [SDR SIMA20140314006](https://openairdocs.org/sdr/SIMA20140314006), Mar 14, 2014: ROLLER. LACK OF LUBE. MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN ON TWO OCCASIONS. LUBE ALL DOOR ROLLERS, DOOR OPERATION CHECK IS GOOD IAW 140 52-10-00 AMM.
- [SDR SIMA20140303006](https://openairdocs.org/sdr/SIMA20140303006), Mar 3, 2014: FITTING. CORRODED. FRAME 68 SHEAR CLIP CORRODED AT CARGO DOOR LOWER SILL. REPAIRED FRAME 68 SHEAR CLIP IAW AEA ERS EM-53MR-1129.
- [SDR SIMA20140303007](https://openairdocs.org/sdr/SIMA20140303007), Mar 3, 2014: FITTING. CORRODED. FRAME 65 SHEAR CLIP CORRODED AT CARGO DOOR LOWER SILL. PERFORMED REPAIR OF FRAME 65 SHEAR CLIP IAW AEA ERS EM-53MR-1129.
- [SDR SIMA20140223008](https://openairdocs.org/sdr/SIMA20140223008), Feb 23, 2014: FRAME. CRACKED. FRAME 23 CRACKED BETWEEN STRINGER 15R & 16R. REPAIRED CRACK AT FRAME 23 IAW EO EM-53MR-1808.
- [SDR SIMA20140216009](https://openairdocs.org/sdr/SIMA20140216009), Feb 16, 2014: SUPPORT BRACKET. CRACKED. RT ENG ATS VLV SUPPORT TRIANGLE BRACKET IS CRACKED. R & R THE RT ENG TAS VLV SUPPORT TRIANGLE BRACKET IAW CMM 80-11-93 & AMM 20-10-01.
- [SDR SIMA20140216010](https://openairdocs.org/sdr/SIMA20140216010), Feb 16, 2014: SUPPORT BRACKET. CRACKED. LT BLEED AIR TUBE SUPPORT BRACKET, BELOW FLOOR, BETWEEN FRAME 68 & 69 CRACKED. R & R LT BLEED AIR TUBE SUPPORT BRACKET, BELOW FLOOR, BETWEEN FRAME 68 & FRAME 69
- [SDR SIMA20140216011](https://openairdocs.org/sdr/SIMA20140216011), Feb 16, 2014: WIRE. BROKEN. LT NR 1 PROXIMITY LIGHT STRIP HAS WIRES BROKEN OFF. R & R LT NR 1 PROXIMITY LIGHT STRIP IAW AMM 33-50-12. SEE NRTC BOW150062 TASK NR 1 FOR OPERATIONS CHECK.
- [SDR SIMA20140216008](https://openairdocs.org/sdr/SIMA20140216008), Feb 16, 2014: SUPPORT BRACKET. CRACKED. LT ENG ATS VLV SUPPORT TRIANGLE BRACKET IS CRACKED. R & R LT ENG ATS SUPPORT TRIANGLE BRACKET IAW CMM 80-11-93 & AMM 20-10-01.
- [SDR SIMA20140216012](https://openairdocs.org/sdr/SIMA20140216012), Feb 16, 2014: ANGLE. CRACKED. CARGO DOOR LOWER SILL AFT FLOOR SUPPORT LOWER L ANGLE CRACKED. REMOVED CRACKED CARGO DOOR LOWER SILL AFT FLOOR SUPPORT LOWER L ANGLE, PREPPED & INSTALLED SERVIC
- [SDR SIMA20140216007](https://openairdocs.org/sdr/SIMA20140216007), Feb 16, 2014: SUPPORT. CORRODED. AILERON FWD TORQUE TUBE RT SUPPORT CORRODED. R & R AILERON FWD TORQUE TUBE RT SUPPORT IAW SRM 51-40-02.
- [SDR SIMA20140216005](https://openairdocs.org/sdr/SIMA20140216005), Feb 16, 2014: SUPPORT. CRACKED. LT OMEGA BEAM OTBD SUPPORT CRACKED AT FRAME 47. REMOVED LT OMEGA BEAM OTBD SUPPORT CRACKED AT FRAME 47 & INSTALLED SERVICEABLE SUPPORT IAW SRM 53-23-02 SEE TURN
- [SDR SIMA20140216004](https://openairdocs.org/sdr/SIMA20140216004), Feb 16, 2014: SUPPORT. CRACKED. RT OMEGA BEAM INBD SUPPORT CRACKED AT FRAME 47. REMOVED RT OMEGA BEAM TO WING BOX INBD SUPPORT ANGLE & INSTALLED NEW TWO PIECE SUPPORT ANGLE IAW SRM 53-23-02.
- [SDR SIMA20140216003](https://openairdocs.org/sdr/SIMA20140216003), Feb 16, 2014: SUPPORT. CRACKED. RT OMEGA BEAM OTBD SUPPORT CRACKED AT FRAME 47. R & R RT OMEGA BEAM OTBD SUPPORT BETWEEN FRAME 46 & FRAME 50 IAW SRM 53-23-02.

All 82: https://openairdocs.org/aircraft/N836AE/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/N836AE/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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