# N840AE: 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: 145656
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 14, 2002
- Certificate issued: September 1, 2023
- Expires: September 30, 2030
- Mode S code: AB7FDE
- 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=840AE
- Page: https://openairdocs.org/aircraft/N840AE

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/N840AE/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 N840AE.

## FAA accident and incident reports

None matched to N840AE.

## 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 SIMA20201020001](https://openairdocs.org/sdr/SIMA20201020001), Oct 20, 2020: DUCT. BLOWN. BLEED 1 LEAK SHORTLY AFTER TAKEOFF. MESSAGE APPEARED AFTER WE GOT PACK 2 CLOSED MESSAGE AND PACK WAS RESET. OVERWEIGHT LANDING WITHING LIMITS EMERGENCY DECLARED
- [SDR SIMA20201002003](https://openairdocs.org/sdr/SIMA20201002003), Oct 2, 2020: DUCT. BLOWN. BLEED 2 LEAK MESSAGE IN FLIGHT. BURNING SMELL NOTICED BY CREW AND PAX. PASSENGERS SEATED IN ATF CABIN ALSO NOTED BURNING SMELL. FLIGHT DECLARED EMERGENCY. C/A: 
- [SDR SIMA202009187002](https://openairdocs.org/sdr/SIMA202009187002), Sep 17, 2020: BATTERY PACK. INOPERATIVE. LEFT FWD WING FUSELAGE EMERGENCY LIGHT INOP. C/A REMOVED AND REPLACE NR 1 EMERGENCY BATTERY AND CHARGER, IAW EMB 140 AMM 33-50-04. OPS CHECK GOOD.
- [SDR SIMA202008243001](https://openairdocs.org/sdr/SIMA202008243001), Aug 23, 2020: INVERTER. INOPERATIVE. NR 2 AND 3 EMERGENCY LIGHT FLOOR PROXIMITY STRIPS INOPERATIVE. FOUND THE NR 3 DC/AC INVENTER INOPERATIVE. R & R THE NR 3 EMERGENCY LIGHT DC/AC INVENTER IAW AMM 
- [SDR SIMA202008242001](https://openairdocs.org/sdr/SIMA202008242001), Aug 22, 2020: SEAL. DAMAGED. WHISTLING NOISE FROM UPPER MAIN CABIN DOOR IN FLIGHT. PRESSURIZATION NORMAL. R & R MAIN CABIN DOOR RUBBER TRIM SEAL IAW AMM 52-18-04. PERFORMED CABIN LEAK CHECK
- [SDR SIMA202007287001](https://openairdocs.org/sdr/SIMA202007287001), Jul 27, 2020: BULB. INOPERATIVE. RH OVERWING EMERGENCY LIGHT INOPERATIVE. R & R THE OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHECKED GOOD.
- [SDR SIMA202007076004](https://openairdocs.org/sdr/SIMA202007076004), Jul 6, 2020: LIGHT. INOPERATIVE. EMERGENCY LIGHTING SYSTEM, FLOOR PROXIMITY STRIP AT SEAT 12A WAS INOPERATIVE. R & R FLOOR PROXIMITY STRIP LIGHTS AT SEAT 12A. OPS CHECKED GOOD IAW AMM 33-50-12.
- [SDR SIMA202006154003](https://openairdocs.org/sdr/SIMA202006154003), Jun 14, 2020: LIGHT. INOPERATIVE. AFT PASSENGER OVERHEAD EMERGENCY LIGHT INOP. R&R AFT PASSENGER OVERHEAD EMERGENCY LIGHT BULB IAW AMM 33-50-08. OPS CHK GOOD.
- [SDR SIMA202004143007](https://openairdocs.org/sdr/SIMA202004143007), Apr 13, 2020: POWER SUPPLY. FAILED. 2ND AND 3RD FLOOR PROXIMITY LIGHTS ARE INOP-C/A-REMOVED AND REPLACED #2 EMERG PWR SUPPLY IAW EMB-140 AMM 33-50-04. OPC GOOD. EMERGENCY LIGHTING BATTERY P/N 2013
- [SDR SIMA202003032002](https://openairdocs.org/sdr/SIMA202003032002), Mar 2, 2020: BUTTON. DEFECTIVE. AUTOMATIC A/ICE SYSTEM DID NOT ACTIVATE IN MODERATE ICING CONDITIONS UPON MANUAL ACTIVATION NO OPEN INSCRIPTION ON WING A/ICE. SHORTLY AFTER A/ICE FAIL WARNING 
- [SDR SIMA202003028001](https://openairdocs.org/sdr/SIMA202003028001), Feb 28, 2020: COMPUTER. FAILED. SUPPLEMENTAL IC #2 CB POPPED FOLLOWED BY ELECTRICAL SMELL-C/A-REMOVED AND REPLACED #2 IC600 COMPUTER IAW EMB AMM 31-42-01 OPC GOOD. VERIFIED ELECTRICAL ODOR WAS
- [SDR SIMA20200215001](https://openairdocs.org/sdr/SIMA20200215001), Feb 15, 2020: BULB. INOPERATIVE. RH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RH OVERWING EMBERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-10. OPS CHECK GOOD.
- [SDR SIMA201912109005](https://openairdocs.org/sdr/SIMA201912109005), Dec 9, 2019: LIGHT. INOPERATIVE. RH UPPER WING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT IAW EMB AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A OPC GOOD
- [SDR SIMA2019103029002](https://openairdocs.org/sdr/SIMA2019103029002), Oct 29, 2019: CONNECTOR. BROKEN. EMERGENCY LIGHT 3RD FLOOR STRIP REMOVABLE SPLICE CONNECTION BROKEN-C/A-INSTALLED A NEW DISCONNECTABLE SPLICE AT EMERGENCY LIGHT 3RD STRIP IAW SWPM 20-21-00. OPT
- [SDR SIMA20190904001](https://openairdocs.org/sdr/SIMA20190904001), Sep 4, 2019: UNKNOWN. SMOKE. AT GATE WITH WINDSHIELD OFF LIGHT PANEL HAD NOT BEEN TOUCHED FO SMELLED AND SAW SMOKE COMING FROM FO SIDE GLARESHIELD LIGHT CONTROL PANEL. C/A-FOLLOWED FIM TASK
- [SDR SIMA20190830001](https://openairdocs.org/sdr/SIMA20190830001), Aug 30, 2019: O-RING. DAMAGED. BLD 1 LEAK EICAS WARNING MESSAGE ALONG WITH LEAK INSCRIPTION ON BLEED 1 PUSH BUTTON PRESENT WHILE RUNNING THE APU AT THE GATE. APU BLEED WAS OPEN BLEED 1 AND BL
- [SDR SIMA201908298003](https://openairdocs.org/sdr/SIMA201908298003), Aug 28, 2019: UNKNOWN. ODOR. AFTER LANDING A STRONG SMELL OF BURNT RUBBER WAS PRESENT IN COCKPIT AND CABIN. GROUND PERFORMED OPS TEST FOR COOLING PACK SYS IN REF TO AMM 21-51-00,TEST PASS &
- [SDR SIMA201906132002](https://openairdocs.org/sdr/SIMA201906132002), Jun 12, 2019: CONNECTOR. LOOSE. IN FLIGHT PTRIM BACK INOP AND PTRIM MAIN INOP WARNING MESSAGE IN FLIGHT. PERFORMED GVI BEHIND TRIM PANEL AND FOUND LOOSE CONNECTION. RECONNECTED PLUG. REINSTALL
- [SDR SIMA20190430005](https://openairdocs.org/sdr/SIMA20190430005), Apr 30, 2019: FADEC. FAULTY. SUPPLEMENTAL TO SAVE GAS WE SHUT ON NR 2 ENGINE DOWN. TO COOL THE CABIN, WE ATTEMPT TO START THE APU. IT SHUT DOWN WHEN APU SHUT DOWN IT TRIP AIRPLANE INTO ELEC
- [SDR SIMA20181221001](https://openairdocs.org/sdr/SIMA20181221001), Dec 21, 2018: LIGHT. INOPERATIVE. EMERGENCY LIGHT BY ROW 4-6 ON THE FLOOR INOP-C/A-EMERGENCY LIGHT STRIP BY ROWS 4-6 DEFERRED
- [SDR SIMA20181217004](https://openairdocs.org/sdr/SIMA20181217004), Dec 17, 2018: CONNECTOR. INOPERATIVE. EMERGENCY LIGHT INOP FWD LAV FLOOR PROXIMITY STRIP. INSTALLED NEW CONNECTOR FOR FWD LAV FLOOR PROXIMITY EMERGENCY LIGHT STRIP IAW SWPM 20-50-00 OPS CHECKED GOOD
- [SDR SIMA20181216002](https://openairdocs.org/sdr/SIMA20181216002), Dec 16, 2018: UNKNOWN. ODOR. ODOR OF DECOMPOSING VARMIT IN COCKPIT. FOUND MUFFLER DUCT DISCONNECTED FROM LT RECIRC FAN. SECURED MUFFLER DUCT IAW AMM 21-24-01. RAN BOTH ENGS AT IDLE, MAX POW
- [SDR SIMA2018100124007](https://openairdocs.org/sdr/SIMA2018100124007), Sep 24, 2018: PROXIMITY SWITCH. FAILED. SPOILER FAIL ON DESCENT.-C/A-REMOVED AND REPLACED LT INBD PROX SWITCH AND RT OUTBOARD PROX SWITCH IAW AMM 27-63-04 OPS CHECK GOOD PER AMM 27-63-01. PROXIMITY SE
- [SDR SIMA2018092524004](https://openairdocs.org/sdr/SIMA2018092524004), Sep 24, 2018: WARNING SYSTEM. ACTIVATED. AT 90KTS RECIEVED MX. SPOILER FAIL INBOUND LGA DUE MX. LGA AOA COPARATOR ON CAPTAINS PFD AS WELL AS SPS 1 INOP WARNING EICAS FAULT CODE 273M0100. SPS 1 INOP WAR
- [SDR SIMA20180921002](https://openairdocs.org/sdr/SIMA20180921002), Sep 21, 2018: SENSOR. DIRTY. SPOILER FAIL MSG INDICATING CLOSED EMERGENCY DECLARED. AFTER INSPECTION FOUND LT INBD SPOILER SENSOR DIRTY CLEANED SENSOR AND RT INBD SPOILER SENSOR DIRTY. CLEA
- [SDR SIMA201808021001](https://openairdocs.org/sdr/SIMA201808021001), Aug 1, 2018: LIGHT. INOPERATIVE. RT OVER WING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RT OVER WING EMERGENCY LIGHT LAMP PER AMM 33-50-07. OP CHECKED GOOD PER AMM 33-50-00.
- [SDR SIMA2018071615001](https://openairdocs.org/sdr/SIMA2018071615001), Jul 15, 2018: ROLLER. LACK OF LUBE. MAIN CABIN DOOR HARD TO OPEN. CLEANED & LUBRICATED THE DOOR ROLLERS IAW AMM 52-21-02. OPC GOOD. NO DEFECTS NOTED AT THIS TIME.
- [SDR SIMA201806076008](https://openairdocs.org/sdr/SIMA201806076008), Jun 6, 2018: ENGINE. VIBRATION. AT 6000 FT, THE NR 2 ENGINE STARTED TO VIBRATE AND MADE A LOUD SOUND, EICASE INDICATED E2 CTL FAIL, FOLLOWED QRH PROCEDURES, STARTED THE APU AND RECOVERED THE E
- [SDR SIMA2018043028007](https://openairdocs.org/sdr/SIMA2018043028007), Apr 28, 2018: SHEAR TIE. CRACKED. CRACKED SHEAR TIE AT FRAME 67, STRINGERS 6L AND 7L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 53-31-04, 51-30-01, DRAWING 140-04109, SRM 51-20-03
- [SDR SIMA2018043028006](https://openairdocs.org/sdr/SIMA2018043028006), Apr 28, 2018: SHEAR TIE. CRACKED. CRACKED SHEAR TIE AT FRAME 73, STRINGERS 8R AND 9R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 53-31-04, AND DRAWING 140-04111.
- [SDR SIMA2018043028005](https://openairdocs.org/sdr/SIMA2018043028005), Apr 28, 2018: SHEAR TIE. CRACKED. CRACKED SHEAR TIE AT FRAME 24, STRINGERS 15R - 16R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, AND CPM 51-21-04.
- [SDR SIMA2018043028004](https://openairdocs.org/sdr/SIMA2018043028004), Apr 28, 2018: SHEAR TIE. CRACKED. CRACKED SHEAR TIE AT FRAME 24, STRINGERS 16R - 17R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, AND CPM 51-21-04.
- [SDR SIMA2018043028009](https://openairdocs.org/sdr/SIMA2018043028009), Apr 28, 2018: SHEAR TIE. CRACKED. CRACKED SHEAR TIE AT FRAME 25, STRINGERS 15R - 16R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, AND CPM 51-21-04.
- [SDR SIMA2018043028002](https://openairdocs.org/sdr/SIMA2018043028002), Apr 28, 2018: FLOOR SUPPORT. CORRODED. CORROSION ON THE LEFT OMEGA BEAM FROM FRAMES 46 TO 53. BLENDED THE CORROSION AND DETERMINED TO BE OUT OF LIMITS IAW SRM 53-23-10. REMOVED AND REPLACED THE OMEGA
- [SDR SIMA2018043028008](https://openairdocs.org/sdr/SIMA2018043028008), Apr 28, 2018: STRINGER. CRACKED. CRACKED STRINGER 3L AT FRAME 20. REMOVED AND REPLACED THE STRINGER BETWEEN FRAMES 18 AND 20 IAW SRM 51-40-02, 51-20-03, AND CPM 51-21-04.
- [SDR SIMA2018043028003](https://openairdocs.org/sdr/SIMA2018043028003), Apr 28, 2018: SHEAR TIE. CORRODED. CORROSION ON THE SHEAR TIE AT FRAME 49, STRINGER 4R. APPLIED EWIS PROTECTION IAW SWPM 20-21-00. BLENDED CORROSION IAW SRM 51-10-03. REMOVED AND REPLACED THE SHE
- [SDR SIMA20141125009](https://openairdocs.org/sdr/SIMA20141125009), Nov 25, 2014: SOLENOID VALVE. FAULTY. CLIMBING THROUGH 33,000 FEET WE HEARD A LOUD NOISE & THE ACFT BEGAN TO VIBRATE. SUSPECTED GEAR DOOR OPEN. RETURNED FOR LANDING, GEAR EXTENSION WAS FASTER THAN N
- [SDR SIMA20141015007](https://openairdocs.org/sdr/SIMA20141015007), Oct 15, 2014: INVERTER. INOPERATIVE. LAST 3 FLOOR EMER LIGHTS INOPERATIVE. R & R EMER LIGHT DC & AC INVERTER 6 IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.
- [SDR SIMA20141006001](https://openairdocs.org/sdr/SIMA20141006001), Oct 6, 2014: ADC. FAILED. DURING AIRSPEED PROBLEM SPS SPEEDS ON EICAS. R & R ADC IAW AMM 34-15-01. OPERATIONS CHECKED GOOD. LEAK CHECKED GOOD IAW AMM 34-13-00. NO LEAKS, ACFT IS COMPLIAN
- [SDR SIMA20140930001](https://openairdocs.org/sdr/SIMA20140930001), Sep 30, 2014: ADC. FAILED. ABORTED TAKEOFF ABOVE 80 KNOTS HIGH SPEED ABORT FOR IAS FLAG DIFFERENCE OF 10 KNOTS. R & R NR 1 ADC IAW AMM 34-15-01, 34-13-00 & 34-15-00. LEAK & OPERATIONAL CH
- [SDR SIMA20140604003](https://openairdocs.org/sdr/SIMA20140604003), Jun 4, 2014: LIGHT. INOPERATIVE. MAIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EMER LIGHT LAME IAW TASK 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140405002](https://openairdocs.org/sdr/SIMA20140405002), Apr 5, 2014: BATTERY. DISCHARGED. LEFT FWD FUSELAGE EXTERNAL EMERGENCY LAMP INOPERATIVE. TROUBLE SHOT IAW FIM 33-50-00-810-804-A. R & R NR 1 EMERGENCY LIGHT BATTERY & CHARGER IAW AE WORK CARD 33
- [SDR SIMA20140330003](https://openairdocs.org/sdr/SIMA20140330003), Mar 30, 2014: LIGHT. INOPERATIVE. RIGHT WING FWD EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R RT WING FWD EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-50-10, OPERATIONS TESTED GOOD.
- [SDR SIMA20140115007](https://openairdocs.org/sdr/SIMA20140115007), Jan 15, 2014: WIRE. BROKEN. EMERGENCY LIGHT ON SERVICE DOOR INOPERATIVE. IAW NRWC 840-DFW-01186 FOR REPAIR OF BROKEN WIRE. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.
- [SDR SIMA20131231004](https://openairdocs.org/sdr/SIMA20131231004), Dec 31, 2013: FLASHLIGHT. INOPERATIVE. ON FLIGHT 3345 CREW REPORTED AFT FLASHLIGHT INOPERABLE. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED F/A REAR FLASHLIGHT IAW EMB 140 AMM 33-50-16 OPC
- [SDR SIMA20131112012](https://openairdocs.org/sdr/SIMA20131112012), Nov 12, 2013: WIRE. DAMAGED. PAX DOOR LINER EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRE ON PAX DOOR LINER EMERGENCY LIGHT IAW SWPM 20-21-00. OPS CHECKED GOOD IAW AMM 33-50-00.
- [SDR SIMA20130910002](https://openairdocs.org/sdr/SIMA20130910002), Sep 10, 2013: LIGHT. MISINSTALLED. RIGHT OVERWING EMERGENCY LIGHT INSTALLED UPSIDE DOWN. REMOVED AND REINSTALLLED EXTERNAL EMERGENCY LIGHT'S PANEL ON RT SIDE CENTER FAIRING IN REF TO AMM 33-50-10
- [SDR SIMA20130629001](https://openairdocs.org/sdr/SIMA20130629001), Jun 29, 2013: LAMP. INOPERATIVE. DURING B INSPECTION, FOUND THE OVERHEAD EMERGENCY LIGHT INOPERATIVE AT ROW 11BC. ACFT REMOVED FROM SERVICE. R & R THE OVERHEAD EMERGENCY LIGHT AT ROW 11B,C IAW 
- [SDR SIMA20130621001](https://openairdocs.org/sdr/SIMA20130621001), Jun 21, 2013: VALVE. INOPERATIVE. DURING TAKEOFF, RECEIVED AN EICAS MLG AIR/GROUND FAIL CAUTION MESSAGE AFTER GEAR RETRACTION. SEVERAL SECONDS LATER RECEIVED EICAS ENG 1-2 REVERSER DISAGREE CAUT
- [SDR SIMA20130620006](https://openairdocs.org/sdr/SIMA20130620006), Jun 20, 2013: ELECTRONIC UNIT. INOPERATIVE. THE CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A LGL AIR/GND FAIL CAUTION MESSAGE ON EICAS FOLLOWED BY REV 1 (2) DISAGREE. THE CREW FOLLOWED AOM, VOL1 CHECK

All 94: https://openairdocs.org/aircraft/N840AE/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/N840AE/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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.