# N838AE: 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: 145651
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 30, 2002
- Certificate issued: September 12, 2023
- Expires: September 30, 2030
- Mode S code: AB7617
- 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=838AE
- Page: https://openairdocs.org/aircraft/N838AE

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/N838AE/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 N838AE.

## 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 20030907032179I](https://openairdocs.org/incident/20030907032179I), Sep 7, 2003: Emb EMB135KL (N838AE), Syracuse, NY. (-23) On September 7, 2003, an American eagle, Emb-135, flt. 4320, diverted into Syracuse airport, Syracuse, NY due to smoke in the cockpit. The ARFF responded…

## Service difficulty reports (87, 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 SIMA202001232002](https://openairdocs.org/sdr/SIMA202001232002), Jan 22, 2020: BOOT. DISCONNECTED. WG A/ICE FAIL IN FLIGHT IN ICING CONDITIONS. QRH PROC. COMPLIED WITH, MSG REMAINS-C/A-FOUND WING 2 A/ICE LEAK ON CMC PERFORMED EMB 140 FIM TASK 30-11-00-810-807
- [SDR SIMA2020010229002](https://openairdocs.org/sdr/SIMA2020010229002), Dec 29, 2019: FLASHLIGHT. UNSECURE. MEL 25-53 AUTH# 121051-C AFT FA FLASHLIGHT INOPREF LOG PAGE 4550081 ITEM 1 .-C/A-RESEATED FLASH LIGHT IN HOLDER AND LET CHARGE ALL NIGHT. OPC GOOD. MEL 25-53 RE
- [SDR SIMA2020010228001](https://openairdocs.org/sdr/SIMA2020010228001), Dec 28, 2019: FLASHLIGHT. INOPERATIVE. AFT FA FLASHLIGHT INOP-C/A-FLIGHT CREW PLACARDED AFT FA FLASHLIGHTAUTH 121051-CREF 25-53 MOC 696266. RESEATED FLASH LIGHT IN HOLDER AND LET CHARGE ALL NIGHT. OP
- [SDR SIMA201911298003](https://openairdocs.org/sdr/SIMA201911298003), Nov 28, 2019: THERMOSTAT. FAILED. BLEED 1-2 VLV OVR TEMP IN FLIGHT WHILE IN ICING CONDITIONS DECLARED EMERGENCY AND AIR RETURN "TRANSFERRED TO NRWC 838-SGF-03378"-C/A-RAR LH AND RH FAN AIR CONTR
- [SDR SIMA201911132001](https://openairdocs.org/sdr/SIMA201911132001), Nov 12, 2019: HANDSET. ODOR. UPON LANDING FA REPORTED A BURNING SMELL IN GALLEY AREA-C/A-PERFORMED FIM TASK 21-20-00-810-801-A- FOUND FWD FA HAND MIC TO HAVE AN ELECTRICAL BURNT SMELL.CHECK
- [SDR SIMA201911121003](https://openairdocs.org/sdr/SIMA201911121003), Nov 11, 2019: FLASHLIGHT. UNKNOWN. AFT FA FLASH LIGHT INOP-C/A-FLT CREW PLACARD AFT FA FLASH LIGHT IAW MEL 2553 AUTH # 110372-C MOC # 624980. OPS CHECKED AFT FA FLASHLIGHT. OPS CHECKED GOOD. IAW 
- [SDR SIMA20190928005](https://openairdocs.org/sdr/SIMA20190928005), Sep 28, 2019: WIRE. DAMAGED. FLOOR PROXIMITY LIGHT STRIP LAST IN AISLE IS INOP-C/A-REPAIRED THE WIRING TO THE FLOOR PROXIMITY LIGHT STRIP LAST IN AISLE IAW EMB SWPM 20-20-00 OPS CHECK GOOD
- [SDR SIMA201908263001](https://openairdocs.org/sdr/SIMA201908263001), Aug 23, 2019: CABIN PRESSURE. MALFUNCTIONED. AIRCRAFT FAILED TO PRESSURIZE ABOVE 900 FT AT 13,000 FT. PERFORMED PRESSURIZATION CONTROL OPS TEST IN BOTH MANUAL & AUTOMATIC MODE IAW AMM 21-31-00. PERFORMED G
- [SDR SIMA20190821001](https://openairdocs.org/sdr/SIMA20190821001), Aug 21, 2019: SKIN. DENTED. DENT FOUND ON LOWER EDGE OF PASSENGER DOOR. PERFORMED PERMANENT REPAIR IAW ERS-EM-52MR-1016 PART A
- [SDR SIMA201908196004](https://openairdocs.org/sdr/SIMA201908196004), Aug 16, 2019: STRUCTURE. DENTED. PERFORM PERMANENT REPAIR OF PAX DOOR DENT IAW ERS-EM-52DF-1006 PTD. MAJOR REPAIR. REPAIRED PAX DOOR IAW ERS-EM-52DF-1006R2 PART D AND ERS-EM- 52MR-1016. SEE NRW
- [SDR SIMA201908164001](https://openairdocs.org/sdr/SIMA201908164001), Aug 14, 2019: BATTERY. OVERHEATED. BATT 2 OVTEMP ON SHORT FINAL APPROACH TURNED PER EPC OFF BAT 2, THEN RECIEVED PROPER EICAS BATT 2 OFF BUS. PRIOR TO POWERING DOWN A GATE, SAW BATT 2 TEMP OF 104
- [SDR SIMA20190519001](https://openairdocs.org/sdr/SIMA20190519001), May 19, 2019: LIGHT. INOPERATIVE. MOST AFT EMERGENCY LIGHT STRIP INOP. C/A-REMOVED AND REPLACED AFT FLOOR PROXIMITY LIGHT IAW AMM 33-50-12. OPC IS GOOD.
- [SDR SIMA201904098002](https://openairdocs.org/sdr/SIMA201904098002), Apr 8, 2019: A/C PACK. SMOKE. SMOKE IN CABIN REAR TO MIDDLE STRONG BURNING SMELL-C/A-FOLLOWED FIM TASK 21-20-00-810-801A FOUND RH ACM SEIZED RAR ACM #2 IAW AMM 21-51-03 PERFORMED GENERAL INS
- [SDR SIMA20190227001](https://openairdocs.org/sdr/SIMA20190227001), Feb 27, 2019: LIGHT. INOPERATIVE. EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT 7A AND 8A INOP. C/A-DEFERRED EMERGENCY FLOOR PROXIMITY LIGHT AS PER MEL 33-30. REMOVED AND REPLACED EMERGENCY FLOOR PRO
- [SDR SIMA20190123004](https://openairdocs.org/sdr/SIMA20190123004), Jan 23, 2019: UNKNOWN. ODOR. OILY SMELL FROM PACKS WHEN TO THRUST IS APPLIED. GOES AWAY AFTER A FEW MIN "TRANSFERRED TO NRWC 838-DFW-02889". C/A- PERFORMED ETN-EM-72-034. RUNS CHECKED GOOD.
- [SDR SIMA201811196002](https://openairdocs.org/sdr/SIMA201811196002), Nov 16, 2018: CONTROLLER. FAILED. AUTOMATIC PRESSURIZATION SYSTEM FAILED AS WE BEGAN OUR CLIMB.-C/A-RAR CABIN PRESS. CONTROL SYSTEM DIGITAL CONTROLLER IAW AMM 21-31-01. PERFORMED PRESS. CONTROL 
- [SDR SIMA201809042003](https://openairdocs.org/sdr/SIMA201809042003), Sep 2, 2018: DAU. FAILED. DAU NR 2 FAILED. PERFORMED FIM TASK 31-40-00-810-809-A. FOUND TO BE TRANSITORT CONDITION OF THE IC-60 COMPUTER. OPS CHECK OF IC-600 GOOD REF AMM 31-42-00. AIRCR
- [SDR SIMA20180322005](https://openairdocs.org/sdr/SIMA20180322005), Mar 22, 2018: SHEAR TIE. CORRODED. FWD SHEAR TIE AFT OF FRAME 65 CORRODED. THE SHEAR WAS REPAIRED IAW SRM 53-31-04 RE.
- [SDR SIMA2018091115006](https://openairdocs.org/sdr/SIMA2018091115006), Mar 15, 2018: RELIEF VALVE. FAILED. FNC OF THE EMERGENCY PARKING BRAKE SYS THERMAL RELIEF VALVE FAILED TEST. EMERGENCY PARKING BRAKE SYSTEM THERMAL RELIEF VALVE REPLACED IAW AMM 32-44-06.
- [SDR SIMA2018090615005](https://openairdocs.org/sdr/SIMA2018090615005), Mar 15, 2018: DOOR SILL. CORRODED. LT SILL NUMBER 5 CORRODED AT SEVERAL PLACES. LT SILL NUMBER 5 BLENDED IAW SRM 51-10-03 AND FOUND OUT OF LIMIT IAW SRM 5323-10 LT SILL NUMBER 5 REMOVED FOR REPLA
- [SDR SIMA2018090615003](https://openairdocs.org/sdr/SIMA2018090615003), Mar 15, 2018: DOOR SILL. CORRODED. CF2 FLOOR STRUCTURE LT SILL NR 3 BTW FR31 & FR35 CORRODED. CF2 FLOOR STRUCTURE LT SILL NR 3 OUT OF LIMITS AND REMOVED PER SRM 53-22-10 AND 51-40-20 AND INSTALLE
- [SDR SIMA2018090615004](https://openairdocs.org/sdr/SIMA2018090615004), Mar 15, 2018: FRAME. CORRODED. IN RFI AT FR 65, FRAME Z PN 145-25672-203 FOUND CORRODED AROUND ANCHOR NUT HOLES. IN RFI AT Z FR65 ON LT SIDE CORROSION BLENDED IAW SRM 51-10-03. AFTER FURTHER 
- [SDR SIMA2018090615002](https://openairdocs.org/sdr/SIMA2018090615002), Mar 15, 2018: GUSSET. CORRODED. CF2 FLOOR STRUCTURE RT GUSSET 1 BTW FR24 & FR31 CORRODED. CF2 FLOOR STRUCTURE RT GUSSET 1 BTW FR24 & FR31 CORRODED OUT OF LIMITS, REPLACED IAW SRM 51-40-02.
- [SDR SIMA20161101001](https://openairdocs.org/sdr/SIMA20161101001), Nov 1, 2016: CHARGER. FAILED. WHILE PERFORMING PS-1 INSPECTION FOUND EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY HOLDER ASSY AND CHARGER ASSY IAW AMM 33-50-04. OPS CHECKED 
- [SDR SIMA20160602004](https://openairdocs.org/sdr/SIMA20160602004), Jun 2, 2016: B-NUT. LEAKING. WITH APU BLEED OPEN, GET A SRONG ODOR OF FUEL, POST FLIGHT INSPECTION REVEALS FUEL LEAKING FROM UNDER APU AREA. FOUND LOOSE B-NUT ON APU FUEL CONTROL INLET, ADJ
- [SDR SIMA20160514003](https://openairdocs.org/sdr/SIMA20160514003), May 14, 2016: SMOKE WARNING. FALSE ACTIVATION. IN CRUISE FLIGHT AT 320 THE BAGGAGE SMOKE WARNING MSG APPEARED MOMENTARILY & THE BAGGAGE EXTINGUISHER LIGHT ILLUMINATED & STAYED ON REST OF FLIGHT. PERFORMED SE
- [SDR SIMA20160226003](https://openairdocs.org/sdr/SIMA20160226003), Feb 26, 2016: INVERTER. INOPERATIVE. SECOND & THIRD EMER FLOOR STRIP LIGHTING INOPERATIVE. R & R NR 3 EMER LIGHT INVERTER IAW 33-50-11. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150923002](https://openairdocs.org/sdr/SIMA20150923002), Sep 23, 2015: SWITCH. DIRTY. ANTI-ICE LGA ACCT MX & BAGGAGE DOOR, OPEN INDICATION RIGHT AFTER TAKEOFF FLIGHT CONTINUED. CLEAN BOTH MICRO SWITCHES IAW 52-76-01. OPERATIONS CHECKED GOOD, NO F
- [SDR SIMA20150908003](https://openairdocs.org/sdr/SIMA20150908003), Sep 8, 2015: ENGINE. SMOKE. SMOKE COMING OUT OF ENG 2, AFTER SHUTDOWN WITH A STRONG SMELL OF BURNED OIL. COMPLIED WITH ETN-EM-79-015 STEPS 1 - 9. RETURNED ENG TO SERVICE. NO FURTHER DEFECT
- [SDR SIMA20150122003](https://openairdocs.org/sdr/SIMA20150122003), Jan 22, 2015: BRAKE. FAILED. FLAP LOW SPEED EICAS MESSAGE ON APPROACH. M PROCEDURES COMPLIED WITH, NO CMC MESSAGE. R & R RT FLAP TRANSMISSION BRAKE IAW AMM 27-51-01. OPS CHECKED GOOD. PERFO
- [SDR SIMA20150116002](https://openairdocs.org/sdr/SIMA20150116002), Jan 16, 2015: FLAP. MALFUNCTIONED. FLAP FAIL ON FINAL AT 2000 FT ALL SET FOR 22 FAILED AT 11 ON GLIDE SLOPE SLOWING THROUGH 120 KT 450 FPM DESCENT. RESET & PERFORMED OPERATIONS CHECK OF FLAP SYS 
- [SDR SIMA20141119006](https://openairdocs.org/sdr/SIMA20141119006), Nov 19, 2014: FLASHLIGHT. INOPERATIVE. CAPTAIN'S FLASHLIGHT INOPERATIVE. R & R CAPTAIN'S FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140902005](https://openairdocs.org/sdr/SIMA20140902005), Sep 2, 2014: HOLDER. BROKEN. FLIGHT ATTENDANT EMER FLASHLIGHT HOLDER BASE IS BROKEN. R & R FLIGHT ATTENDANT EMER FLASHLIGHT BRACKET IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIO
- [SDR SIMA20140722001](https://openairdocs.org/sdr/SIMA20140722001), Jul 22, 2014: SWITCH. INOPERATIVE. AILERON SYS 1 INOPERATIVE IN FLIGHT. R & R AIL SYS NR 1 PUSH BUTTON IAW AMM 20-13-08. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR SIMA20140701010](https://openairdocs.org/sdr/SIMA20140701010), Jul 1, 2014: PROXIMITY SWITCH. OUT OF ADJUST. DOWN LOCK RELEASE BUTTON PRESSED FOR GEAR RETRACTION ON TAKEOFF. LG AIR & GND FAIL MSG AFTER GEAR SELECTED DOWN. FOUND PROXIMITY SWITCHES ON RT & LT MLGS OUT OF
- [SDR SIMA20140629010](https://openairdocs.org/sdr/SIMA20140629010), Jun 29, 2014: SKIN. CRACKED. RIGHT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 1R & 2R. PERFORMED PERMANENT REPAIR OF RT REAR FUSELAGE I SKIN AT FRAME 75 BETWEEN STRINGERS 1R
- [SDR SIMA20140629011](https://openairdocs.org/sdr/SIMA20140629011), Jun 29, 2014: SKIN. CRACKED. LEFT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 1L & 2L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN AT FRAME 75 BETWEEN STRINGERS 1L 
- [SDR SIMA20140628003](https://openairdocs.org/sdr/SIMA20140628003), Jun 28, 2014: WIRE. BROKEN. NUMBER 2 EMER PROXIMITY LIGHT STRIP HAS BROKEN & DAMAGED WIRES. R & R FWD GALLEY EMER LIGHT STRIP IAW AMM 33-50-12.
- [SDR SIMA20140620003](https://openairdocs.org/sdr/SIMA20140620003), Jun 20, 2014: FITTING. WORN. RIGHT AILERON DAMPER FITTING WORN. REMOVED & INSTALL DAMPER FITTING IAW EO EM-27MR-112.
- [SDR SIMA20140606008](https://openairdocs.org/sdr/SIMA20140606008), Jun 6, 2014: WIRE. BROKEN. TWO EMER LIGHT STRIP WIRES ARE BROKEN AT FLOOR PANEL 261BF. INSTALLED SERVICEABLE PINS ON TWO EMER LIGHT STRIP WIRES, AT FLOOR PANEL 261BF IAW WM 91-10-02, SWPM
- [SDR SIMA20140606007](https://openairdocs.org/sdr/SIMA20140606007), Jun 6, 2014: STRUCTURE. CRACKED. BATTERY COMPARTMENT DOOR CUT OUT CRACKED, AFT EDGE MARKED. REPAIRED CRACK ON BATTERY COMPARTMENT DOOR CUT OUT AFT EDGE IAW ERS-EM-5300-527. SEE WIP & TASK ENTRI
- [SDR SIMA20140606006](https://openairdocs.org/sdr/SIMA20140606006), Jun 6, 2014: DOOR. DENTED. MAIN DOOR DENTED NEAR AFT EDGE, 9 INCHES ABOVE AFT LOWER CORNER. MAIN DOOR DENTED NEAR AFT EDGE, 9 INCHES ABOVE AFT LOWER CORNER FOUND TO BE ACCEPTED AS IS IAW 
- [SDR SIMA20140606005](https://openairdocs.org/sdr/SIMA20140606005), Jun 6, 2014: DOOR. GOUGED. MAIN DOOR GOUGED ALONG LOWER EDGE, METAL MOVED, NOT PAINT DAMAGE ONLY. MAIN DOOR GOUGED ALONG LOWER EDGE FOUND TO BE ACCEPTED AS IS IAW ERS-EM-5200-159. SEE TAS
- [SDR SIMA20140606004](https://openairdocs.org/sdr/SIMA20140606004), Jun 6, 2014: SPLICE. CORRODED. CIRCUMFERENTIAL SPLICE IS CORRODED BETWEEN FRAME 12 & 13, STRINGER 21L & 21R. COMPLIED WITH ERS-EM-5300-528 JUNCTION 02 CIRCUMFERENTIAL SPLICE CORROSION BETWEEN
- [SDR SIMA20140424002](https://openairdocs.org/sdr/SIMA20140424002), Apr 24, 2014: ROLLER. LACK OF LUBE. MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED MAIN PAX DOOR ROLLERS IAW MM 52-18-00, OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR SIMA20140312002](https://openairdocs.org/sdr/SIMA20140312002), Mar 12, 2014: ISIS. FAILED. STANDBY ATT FAIL DURING ROTATION, DIVERT BACK TO LGA. R & R ISIS IAW AMM 34-01-01. OPERATIONS CHECK & LEAK CHECKED GOOD IAW AMM 34-01-01.
- [SDR SIMA20140119007](https://openairdocs.org/sdr/SIMA20140119007), Jan 19, 2014: DOOR. LACK OF LUBE. MAIN CABIN ENTRY DOOR EXCESSIVE FORCE USED TO OPEN OR CLOSE DOOR USING INSIDE HANDLE. CLEANED & LUBED MAIN CABIN DOOR IAW MX STANDARD PRACTICES, OPERATIONS CHEC
- [SDR SIMA20131222014](https://openairdocs.org/sdr/SIMA20131222014), Dec 22, 2013: BATTERY. DISCHARGED. OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EMERGENCY BATTERY & CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD IAW WC 33-700-17.
- [SDR SIMA20131214003](https://openairdocs.org/sdr/SIMA20131214003), Dec 14, 2013: POWER SUPPLY. INOPERATIVE. RIGHT & LT AFT OVERWING EMERGENCY LIGHT IS INOPERATIVE. R & R NR 4 BATTERY POWER SUPPLY IAW EMB 140 AMM 33-50-04, OPERATIONS CHECKED GOOD.
- [SDR SIMA20131019003](https://openairdocs.org/sdr/SIMA20131019003), Oct 19, 2013: FLASHLIGHT. INOPERATIVE. AFT FLASHLIGHT IN CABIN NOT CHARGING. R & R AFT FLASHLIGHT, OPS GOOD AMM 33-50-16.

All 87: https://openairdocs.org/aircraft/N838AE/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/N838AE/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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