# N833AE: 2002 Embraer EMB-135KL

- Status: Valid registration
- Airframe: [Embraer EMB-135KL](https://openairdocs.org/model/embraer-emb-135kl) (registry code 3260302, 37 seats)
- Engine: [Rolls-Royce DART RDA-10](https://openairdocs.org/engine/rolls-royce-dart-rda-10) (registry code 54524)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.) (OpenAirDocs)
- Serial number: 145629
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 29, 2002
- Certificate issued: October 14, 2023
- Expires: October 31, 2030
- Mode S code: AB6384
- 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=833AE
- Page: https://openairdocs.org/aircraft/N833AE

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): 67 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 (Rolls-Royce DART RDA-10)

None in force.

### 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

All 77: https://openairdocs.org/aircraft/N833AE/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 N833AE.

## FAA accident and incident reports

None matched to N833AE.

## Service difficulty reports (79, 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 SIMA2020010228002](https://openairdocs.org/sdr/SIMA2020010228002), Dec 28, 2019: LIGHT. INOPERATIVE. MEL # 33-30 AUTH # 130676-C LOG PG 4551574 EMERGENCY FLOOR PATH LIGHT STRIP 16A INOP-C/A-REMOVED AND REPLACED FLOOR PROXIMITY STRIP LIGHT AT ROW 16A IAW EMB 140
- [SDR SIMA201906109003](https://openairdocs.org/sdr/SIMA201906109003), Jun 9, 2019: FLASHLIGHT. INOPERATIVE. FA EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FA EMERGENCY FLASHLIGHT. IAW AMM 33-50-16. OPC GOOD.
- [SDR SIMA201904097003](https://openairdocs.org/sdr/SIMA201904097003), Apr 7, 2019: CONTROL UNIT. FAILED. LDG GEAR NOT INDICATING CORRECTLY ON TAKEOFF AND LANDING (NO TRANSITION JUST UP OR DOWN)-C/A-REMOVED AND REPLACED LGEU. PERFORMED EXTENSION AND RETRACTION CHECK
- [SDR SIMA20190303004](https://openairdocs.org/sdr/SIMA20190303004), Mar 3, 2019: BATTERY. DISCHARGED. FWD FA FLASHLIGHT INOP. C/A-REMOVED AND REPLACED FWD FA FLASHLIGHT BATTERY IN REFERENCE WITH AMM 33-50-16-000-801-A AND 33-50-16-400-801-A OPS CHECK GOOD END.
- [SDR SIMA20190105001](https://openairdocs.org/sdr/SIMA20190105001), Jan 5, 2019: COMPUTER. MALFUNCTIONED. A/P FULL NOSE DOWN AND RIGHT BANK WHEN ENGAGED AND AUTO TRIM INOP WITH NO EICAS MSG WHILE IN FLIGHT. C/A-REMOVED AND REPLACED IC 600 #1 IAW AMM 31-42-01 OPS CHE
- [SDR SIMA201812176001](https://openairdocs.org/sdr/SIMA201812176001), Dec 16, 2018: TUBE. INOPERATIVE. INFLIGHT RAN ICE DECTIONS TEST AND GOT A WING ANTI ICE FAIL CAUTION MESSAGE. RAN THE TEST TWICE AND CAUTION MESSAGE CAME ON BOTH TIMES. "TRANSFERRED TO NRWC 833
- [SDR SIMA201808165004](https://openairdocs.org/sdr/SIMA201808165004), Aug 15, 2018: ANTENNA. INOPERATIVE. RADAR BECAME INOPERATIVE. REMOVED AND REPLACED THE RECIEVER TRANSMITTER ANTENNA ASSY IAW 34-42-01, OPS TESTED GOOD IAW 34-42-00. NO DEFECTS FOUND
- [SDR SIMA201808165003](https://openairdocs.org/sdr/SIMA201808165003), Aug 15, 2018: CONNECTOR. DIRTY. RADAR FAILED. REMOVED AND CLEANED THE CONNECTOR PLUG. RESET UNIT. OPS CHECKED GOOD IAW 34-42-00.
- [SDR SIMA2018081310001](https://openairdocs.org/sdr/SIMA2018081310001), Aug 10, 2018: DOOR. LACK OF LUBE. MAIN CABIN DOOR HARD TO OPPERATE. LUBRICATED THE DOOR IAW ETN-EM-52-061. OPS CHECKED GOOD. NO DEFECT NOTED.
- [SDR SIMA2018053026004](https://openairdocs.org/sdr/SIMA2018053026004), May 26, 2018: SWITCH. FAILED. DURING CLIMB, RECEIVED A LG AIR/GND FAIL MESSAGE. COMPLIED WITH QRH, DECLARED AN EMERGENCY AND DIVERTED. TROUBLESHOT IAW FIM 32-63-00-810-806-A SUBTASK 816-003-
- [SDR SIMA20180407003](https://openairdocs.org/sdr/SIMA20180407003), Apr 7, 2018: DOOR. LACK OF LUBE. FA ADVISED THAT THE MAIN CABIN DOOR WAS HARD TO OPEN .CYCLED AND LUBRICATED MAIN CABIN DOOR IAW AMM 52-10-01. NO DEFECTS NOTED.
- [SDR SIMA20180315001](https://openairdocs.org/sdr/SIMA20180315001), Mar 15, 2018: BATTERY PACK. INOPERATIVE. NUMEROUS FORWARD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY AND CHARGER IAW AMM 33-50-04. OPS CHECKED GOOD.
- [SDR SIMA20180130008](https://openairdocs.org/sdr/SIMA20180130008), Jan 30, 2018: SKIN. DENTED. RUDDER LOWER RTH SKIN DENTED BETWEEN RIBS ZV 920 AND ZV 1164. THE RUDDER SKIN WAS REPAIRED IAW SRM 55-40-01, ITEM 2.
- [SDR SIMA20161107003](https://openairdocs.org/sdr/SIMA20161107003), Nov 7, 2016: LIGHT. DAMAGED. PROXIMITY LIGHT FOUND DAMAGED. R & R THE LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD
- [SDR SIMA20161019002](https://openairdocs.org/sdr/SIMA20161019002), Oct 19, 2016: POWER SUPPLY. INOPERATIVE. DURING PS-2 INSPECTION FOUND LT FAIRING FWD EMERGENCY LIGHT INOP. R&R BATTERY POWER SUPPLY IAW AMM 33-50-04. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. LT LIGHT 
- [SDR SIMA20160929002](https://openairdocs.org/sdr/SIMA20160929002), Sep 29, 2016: WARNING SYSTEM. FALSE ACTIVATION. AT CRUISE ALT SPS ADVANCE AND FLAP LOW SPEED MSG. REF LOG PAGE 4000496 ITEM 3 FOR ACTION TAKEN. SPS SYSTEM RESET PER AMM 27-36-00. NO MESSAGE NOTED, OPS GOOD
- [SDR SIMA20160727001](https://openairdocs.org/sdr/SIMA20160727001), Jul 27, 2016: PRESSURE SWITCH. INOPERATIVE. RUDDER SYSTEM 1 AND 2 EICAS MESSAGE. TROUBLESHOT IAW FIM 27-22-00 AND ENVOY ETN -EM -27 -079. REMOVED AND REPLACED NR 1 & 2 RUDDER PRESSURE SWITCH IAW 27-23-04.
- [SDR SIMA20160714002](https://openairdocs.org/sdr/SIMA20160714002), Jul 14, 2016: LAMP. INOPERATIVE. RIGHT EXTERIOR EMERGENCY LIGHT FORWARD OF WING INOPERATIVE. REPLACED THE LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.
- [SDR SIMA20160210007](https://openairdocs.org/sdr/SIMA20160210007), Mar 10, 2016: PUMP. FAILED. HYD LO QTY ADVISORY NR 1 HYD SYS IS IN AMBER, NO RECOVERY & CONTINUED TO DROP. NO INDICATION OF HYD LEAK ON POST FLIGHT. R & R NR 1 EDP IAW AMM CH 29-10-03. OPE
- [SDR SIMA20160125003](https://openairdocs.org/sdr/SIMA20160125003), Jan 25, 2016: LIGHT. INOPERATIVE. SERVICE DOOR CEILING EMER LIGHT INOPERATIVE. REMOVED & INSTALLED SERVICEABLE SERVICE DOOR CEILING EMER LIGHT LAMP IAW AMM 33-50-09. OPERATIONAL CHECKED GOOD.
- [SDR SIMA20160108005](https://openairdocs.org/sdr/SIMA20160108005), Jan 8, 2016: BATTERY. DISCHARGED. 1ST CEILING LIGHT IN CABIN INOPERATIVE. R & R NR 1 BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.
- [SDR SIMA20151228001](https://openairdocs.org/sdr/SIMA20151228001), Dec 28, 2015: FIRE LOOP. CHAFED. MOMENTARY APU FIRE INDICATION. PERFORMED GVI AROUND APU, NO DEFECTS FOUND. DEFERRED APU, M PROCEDURES COMPLIED WITH IAW 49-1. FOUND APU FIRELOOP CHAFFING AGAINS
- [SDR SIMA20151220001](https://openairdocs.org/sdr/SIMA20151220001), Dec 20, 2015: SPOILER SYS. MALFUNCTIONED. ON DECENT WHILE USING SPOILERS TO ASSIST THE DECENT, ONCE THE SPOILERS HANDLE WAS RETURNED TO STOWED POSITION, EICAS MSG SPOILER FAIL WITH SPOILERS INDICATION O
- [SDR SIMA20151215001](https://openairdocs.org/sdr/SIMA20151215001), Dec 15, 2015: HYDRAULIC LINE. DAMAGED. RAMP PERSONNEL INDICATE SUSPICIOUS ODOR IN THE CARGO COMPARTMENT. TRANSFERRED TO NRWC 833-DFW-02181. PERFORMED PERMANENT REPAIR TO RUDDER PRESS LINE AT LAVATORY
- [SDR SIMA20150413003](https://openairdocs.org/sdr/SIMA20150413003), Apr 13, 2015: TRANSCEIVER. FAILED. NUMBER 1 & 2 PFD'S ARE DISPLAYING AN AMBER WX IN THE RADAR INFO AREA. BOTH WX RADARS ARE DEPICTING ERRONEOUS & INVALID WEATHER RETURNS. R & R WX RADAR ASSEMBLY 
- [SDR SIMA20150311003](https://openairdocs.org/sdr/SIMA20150311003), Mar 11, 2015: HOLDER. BROKEN. CAPTAINS FLASHLIGHT HOLDER BROKEN. R & R CAPTAINS FLASHLIGHT HOLDER ASSEMBLY IAW AMM 33-60-02. OPERATIONS CHECKED GOOD.
- [SDR SIMA20141026002](https://openairdocs.org/sdr/SIMA20141026002), Oct 26, 2014: TRANSMITTER. FAILED. RIGHT FUEL QTY INDICATION ON EICAS DECREASED TO 0 IN FLIGHT, FOLLOWED BY MFD TOTAL INDICATION LOSS ASSOCIATED MASTER CAUTION FUEL IMBALANCE. ON FINAL APPROACH A
- [SDR SIMA20140906003](https://openairdocs.org/sdr/SIMA20140906003), Sep 6, 2014: FLASHLIGHT. INOPERATIVE. EMERGENCY FLASHLIGHT CHARGER ASSEMBLY INOPERATIVE. R & R EMER FLASHLIGHT & CRADLE ASSEMBLY IAW AMM 33-50-16.
- [SDR SIMA20140705007](https://openairdocs.org/sdr/SIMA20140705007), Jul 5, 2014: SKIN. CRACKED. RIGHT UPPER FUSELAGE SKIN HAS 2 AREAS WITH RELEVANT CRACK INDICATIONS JUST AFT OF FRAME 75 & ABOVE STRINGER 2R. REPAIRED RT UPPER FUSELAGE SKIN JUST AFT OF FRAM
- [SDR SIMA20140701012](https://openairdocs.org/sdr/SIMA20140701012), Jul 1, 2014: WIRE. BROKEN. EMERGENCY LIGHT STRIP 3 HAS BROKEN WIRES. R & R FLOOR EMER LIGHT STRIP 3 IAW AMM 33-50-12. SEE NRWC BOW 158177 FOR FLOOR EMER LIGHTS OPERATIONAL CHECK. FOUND DU
- [SDR SIMA20140701013](https://openairdocs.org/sdr/SIMA20140701013), Jul 1, 2014: WIRE. BROKEN. EMERGENCY LIGHT LENS NR 2 HAS BROKEN WIRES. R & R FLOOR EMER LIGHT STRIP NR 2 IAW AMM 33-50-12. SEE NRTC BOW 158177 FOR OPERATIONAL CHECK OF EMER FLOOR LIGHTS F
- [SDR SIMA20140627003](https://openairdocs.org/sdr/SIMA20140627003), Jun 27, 2014: FRAME. CRACKED. FRAME 23 CRACKED BETWEEN STRINGER 15R & 16R. REPAIRED FRAME 23 BETWEEN STRINGER 15R & 16R IAW EM-53MR-1808.
- [SDR SIMA20140607008](https://openairdocs.org/sdr/SIMA20140607008), Jun 7, 2014: SUPPORT. CRACKED. LEFT BEAM CRACKED AT OTBD SUPPORT AT FRAME 47. R & R LT BEAM OTBD SUPPORT IAW SRM 53-23-02.
- [SDR SIMA20140607009](https://openairdocs.org/sdr/SIMA20140607009), Jun 7, 2014: RELIEF VALVE. FAILED. EMERGENCY PARKING BRAKE SYS THERMAL RELIEF VLV FAILED FUNCTIONAL CHECK. REMOVED & RELOCATED EMER PARKING BRAKE SYS THERMAL RELIEF VLV WITH A SERVICEABLE UNIT IA
- [SDR SIMA20140607007](https://openairdocs.org/sdr/SIMA20140607007), Jun 7, 2014: SUPPORT. CRACKED. RIGHT BEAM CRACKED AT INBD & OTBD SUPPORTS AT FRAME 47. R & R INBD OTBD SUPPORTS FOR RT OMEGA BEAM BETWEEN FRAME 46 - 50 IAW SRM 53-23-02.
- [SDR SIMA20131231003](https://openairdocs.org/sdr/SIMA20131231003), Dec 31, 2013: FADEC. MALFUNCTIONED. ON FLIGHT 3350 CREW REPORTED E2 SHORT DISPATCH ADVISORY CAME ON WHILE ENG NR 1 SHUT DOWN. THE ACFT WAS REMOVED FROM SERVICE. RESET E 2 FADEC SYS, OPERATIONS CHE
- [SDR SIMA20131129005](https://openairdocs.org/sdr/SIMA20131129005), Nov 29, 2013: LIGHT. INOPERATIVE. CEILING EMERGENCY LAMP AT ROW 11 INOPERATIVE. REMOVE AND REPLACED AISLE EMERGENCY LIGHT AT ROW 11 IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPS CHE
- [SDR SIMA20131121003](https://openairdocs.org/sdr/SIMA20131121003), Nov 21, 2013: FLASHLIGHT. MISSING. ENTRANCE EMERGENCY FLASHLIGHT MISSING. INSTALLED FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16.
- [SDR SIMA20131103003](https://openairdocs.org/sdr/SIMA20131103003), Nov 3, 2013: CRADLE. BROKEN. AFT CABIN FLASHLIGHT MOUNT IS BROKEN. REPLACED AFT CABIN FLASHLIGHT IAW AMM 33-50-16.
- [SDR SIMA20120727007](https://openairdocs.org/sdr/SIMA20120727007), Jul 26, 2012: FRAME. CRACKED. DURING MAINTENANCE INSPECTION, FOUND FRAME 23 HAS 3/4 INCH CRACK AT LOWER ATTACHMENT RIVET BETWEEN STRINGERS 15R AND 16R. AIRCRAFT REMOVED FROM SERVICE. COMPLET
- [SDR SIMA20120722010](https://openairdocs.org/sdr/SIMA20120722010), Jul 22, 2012: FRAME. CRACKED. RT CABIN FRAME 23 HAS .7500" CRACK AT LOWER ATTACHMENT RIVET BETWEEN STRINGER 15R AND 16R. REPAIRED IAW EO EM-53MR-1808, PART A.
- [SDR SIMA20120722009](https://openairdocs.org/sdr/SIMA20120722009), Jul 22, 2012: WIRE. BROKEN. DURING B INSPECTION, FOUND THE EMERGENCY LIGHT WIRING BROKEN . AIRCRAFT REMOVED FROM SERVICE. REPLACED CONNECTOR AT SPLICE SP9115 IAW SWPM 20-21-00. OPS CHECKED
- [SDR SIMA201023102](https://openairdocs.org/sdr/SIMA201023102), Aug 18, 2010: UNKNOWN. ODOR. ON FLIGHT 4220 THE CREW REPORTED A DISTINCT BURNING SMELL ON APPROACH THAT SEEMED TO EMANATE FROM THE PACKS AND WHEN THROTTLE LEVER WAS AT HIGHER THRUST SETTING
- [SDR SIMA201021802](https://openairdocs.org/sdr/SIMA201021802), Aug 4, 2010: SCAVENGE PUMP. INOPERATIVE. ON FLIGHT 4238 DURING CRUISE THE CREW REPORTED THE ENGINE OIL QUANTITY FOR THE NR 2 ENGINE WENT TO 4 QUARTS. THE CAPTAIN ELECTED TO MAKE A PRECAUTIONARY LANDING
- [SDR SIMA201019604](https://openairdocs.org/sdr/SIMA201019604), Jul 15, 2010: SKIN. CRACKED. DURING MAINTENANCE BASE INSPECTION FOUND THE SKIN CRACKED AT FRAME 75 BETWEEN STRINGERS 1L AND 2L. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CRACKED SKIN 
- [SDR SIMA200836401](https://openairdocs.org/sdr/SIMA200836401), Dec 20, 2008: WARNING LIGHT. FALSE INDICATION. ON FLIGHT 4740 CREW REPORTED AFTER DEPARTURE NOSE LANDING GEAR DOOR NOT CLOSING. THE LANDING GEAR INDICATION WAS NORMAL WITH 3 GREEN AND NO WARNING MESSAGES. CR
- [SDR SIMA200808402](https://openairdocs.org/sdr/SIMA200808402), Mar 22, 2008: CARBON SEAL. WORN. ON FLIGHT 3900 - CREW REPORTED NUMBER 1 ENGINE OIL QUANTITY WENT FROM 11 TO 4 QTS IN LESS THAN 15 MINUTES. PERFORMED PRECAUTIONARY SHUTDOWN. OVERWEIGHT LANDING 
- [SDR SIMA200900901](https://openairdocs.org/sdr/SIMA200900901), Jan 26, 2008: ECU. MALFUNCTIONED. ON FLIGHT 4533 CREW REPORTED NLG DOORS DID NOT RETRACT/CLOSE UPON GEAR RETRACTION. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTR
- [SDR SIMA200729901](https://openairdocs.org/sdr/SIMA200729901), Oct 22, 2007: LIGHT. INOPERATIVE. LEFT EXTERNAL OVERWING EMERGENCY LIGHT INOP. ISSUED MEL 33-29 AUTH 100824D-C.
- [SDR SIMA200700310](https://openairdocs.org/sdr/SIMA200700310), Dec 30, 2006: PROXIMITY SENSOR. SHORTED. LANDING GEAR HANDLE WOULD NOT ALLOW LANDING GEAR TO RETRACT. RECEIVED LG AIR/GND FAIL MESSAGE AND RETURNED TO DFW. REMOVED AND REPLACED PROXIMITY SWITCH IAW EMB

All 79: https://openairdocs.org/aircraft/N833AE/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/N833AE/stcs.md

## Related

- Other Embraer EMB-135KL aircraft: https://openairdocs.org/model/embraer-emb-135kl/aircraft.md
- The Rolls-Royce DART RDA-10 engine: https://openairdocs.org/engine/rolls-royce-dart-rda-10.md

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