# N818AE: 2002 Embraer EMB-135KL, registration cancelled 2025-05-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 23, 2025
- Status when cancelled: Valid registration
- Airframe: [Embraer EMB-135KL](https://openairdocs.org/model/embraer-emb-135kl) (registry code 3260302)
- Engine: [Rolls-Royce AE-3007A1P](https://openairdocs.org/engine/rolls-royce-ae-3007a1p) (registry code 54571)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs)
- Serial number: 145561
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 24, 2002
- Certificate issued: March 17, 2023
- Last registry action: March 17, 2023
- Mode S code: AB2719
- Owner when cancelled: [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 was based
- The mark today: https://openairdocs.org/aircraft/N818AE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=818AE
- Page: https://openairdocs.org/deregistered/N818AE-2025-05-23

From the FAA registry file of November 4, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Embraer EMB-135KL: https://openairdocs.org/model/embraer-emb-135kl.md

## Service difficulty reports (93, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR SIMA202003198001](https://openairdocs.org/sdr/SIMA202003198001), Mar 18, 2020: AUDIO PANEL. FAILED. ELECTRICAL BURNING SMELL AS INDICATED ON PAGE 9134 MECH DISC #1-C/A-PERFORMED WORK SCOPE FROM MOC AND FIM TASK # 21-20-00-810-801. NO EVIDENCE OF ELECTRICAL BUR
- [SDR SIMA202001021001](https://openairdocs.org/sdr/SIMA202001021001), Jan 1, 2020: LAMP. INOPERATIVE. 11A OVERHEAD EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED 11A OVERHEAD EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPS CHECK GO
- [SDR SIMA20191107002](https://openairdocs.org/sdr/SIMA20191107002), Nov 7, 2019: ANTI-ICE VALVE. FAILED. WG A/ICE FAIL ON DESCENT IN ICING CONDITIONS, QRH COMPLIED WITH, MESSAGE WENT AWAY-C/A-REMOVED AND REPLACED WING A/ICE VALVE 2. IAW AMM 30-11-01. NO DEFECTS NOT
- [SDR SIMA2019083029001](https://openairdocs.org/sdr/SIMA2019083029001), Aug 29, 2019: DOOR. LACK OF LUBE. MAIN CABIN DOOR DIFFICULT TO CLOSE AND OPEN. INSPECTED ,CLEANED & LUBED MAIN DOOR ACTUATING & LOCKING MECHANISM IAW AMM 52-11-00 OPS CHECKS GOOD.
- [SDR SIMA201906243001](https://openairdocs.org/sdr/SIMA201906243001), Jun 23, 2019: MECHANISM. LACK OF LUBE. FA REPORTS MAIN DOOR DIFFICULT TO OPEN AND CLOSE. LUBRICATED MAIN DOOR ACTUATING AND LOCKING MECHANISM IAW EMB 140 AMM 52-18-00. OPC GOOD.
- [SDR SIMA201906032002](https://openairdocs.org/sdr/SIMA201906032002), Jun 2, 2019: FLASHLIGHT. MALFUNCTIONED. FWD FLASHLIGHT FLICKERS WHEN TURNED TO ON. REMOVED AND REPLACED FWD FLASHLIGHT ASSY IAW AMM 33-50-16 OPC GOOD
- [SDR SIMA20190520001](https://openairdocs.org/sdr/SIMA20190520001), May 20, 2019: DOOR. LACK OF LUBE. FA UNABLE TO OPEN PAX DOOR FROM INSIDE. DOOR IS ABLE TO OPEN FROM THE OUTSIDE. C/A-APLIED LUBED TO PAX DOOR IAW AMM 52-10-00.
- [SDR SIMA201812031004](https://openairdocs.org/sdr/SIMA201812031004), Dec 1, 2018: LIGHT. INOPERATIVE. EMERGENCY LIGHT ABOVE FA SEAT FOUND TO BE INOP DURING PS2 CHECK-C/A-REMOVED AND REPLACED PANEL SIGN ASSEMBLY OF FWD EXIT SIGN IAW EMB140 AMM 33-50-14. OPC FAIL.
- [SDR SIMA201806186004](https://openairdocs.org/sdr/SIMA201806186004), Jun 16, 2018: HANDLE. LACK OF LUBE. MAIN PAX DOOR HANDLE BINDING, UNABLE TO OPEN THE DOOR. CLEANED, LUBRICATED, AND TESTED THE MAIN PAX DOOR IAW AMM 52-18-00. OPS CHECKED GOOD. ACFT OK FOR SERVICE
- [SDR SIMA201805140006](https://openairdocs.org/sdr/SIMA201805140006), May 10, 2018: ENGINE. ODOR. WITH THE RT ENGINE RUNNING AT MAX POWER, THE NR 2 BLEED OPEN AND NR 1 PACK SELECTED, A STRONG ODOR WAS PRESENT IN THE COCKPIT. WITH THE RT ENGINE AT MAX POWER A
- [SDR SIMA2018042700001](https://openairdocs.org/sdr/SIMA2018042700001), Apr 27, 2018: ROLLER. LACK OF LUBE. MAIN CABIN DOOR WILL STICH & NOT CLOSE OR OPEN. LUBRICATED MAIN DOOR ROLLERS AND OPS CHECKED GOOD IAW AMM 52-18-00.
- [SDR SIMA20180403003](https://openairdocs.org/sdr/SIMA20180403003), Apr 3, 2018: SUPPORT. LOOSE. CARGO DOOR OPENED AFTER TAKEOFF, NO PRESSURIZATION ISSUES. FOUND THE AFT CARGO DOOR SWITCH SUPPORT LEVER WITH A LOT OF PLAY. REMOVED AND REPLACED THE AFT CARGO 
- [SDR SIMA20180323003](https://openairdocs.org/sdr/SIMA20180323003), Mar 23, 2018: SIGN. INOPERATIVE. AFT EMERGENCY EXIT ROW 11 A, B, & C CENTER AISLE INOPERATIVE. CONNECTED THE AFT OVERHEAD EMERGENCY EXIT SIGN. OPS CHECKED GOOD.
- [SDR SIMA20180203003](https://openairdocs.org/sdr/SIMA20180203003), Feb 3, 2018: CONNECTOR. BROKEN. NR 1 EMERGENCY LIGHT CONNECTOR FOUND BROKEN. REMOVED AND REPLACED THE CONNECTOR IAW SWPM 20-21-00.
- [SDR SIMA20180203004](https://openairdocs.org/sdr/SIMA20180203004), Feb 3, 2018: FRAME. CHAFED. FRAME 81 HAS MULTIPLE CHAFES AT THE 6 O'CLOCK POSITION. ACCOMPLISHED A REPAIR IAW ERS-EM-53MR-3111.
- [SDR SIMA20180126008](https://openairdocs.org/sdr/SIMA20180126008), Jan 26, 2018: DOOR SILL. CORRODED. SERVICE DOOR LOWER SILL IS CORRODED AROUND 2 SCREW HOLES. REMOVED CORROSION, SERVICE DOOR LOWER SILL AROUND 2 SCREW HOLES. IAW CPM 51-14-02. BLENDED AREA ON SER
- [SDR SIMA20180126009](https://openairdocs.org/sdr/SIMA20180126009), Jan 26, 2018: DOOR SILL. CORRODED. CARGO DOOR CUT-OUT LOWER SILL CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02, AND 51-20-03.
- [SDR SIMA20180126010](https://openairdocs.org/sdr/SIMA20180126010), Jan 26, 2018: ANGLE. CORRODED. CARGO DOOR CUT-OUT FWD ANGLE CORRODED ON LOWER END. REMOVED AND THE ANGLE IAW SRM 53-31-04, FIGURE 212.
- [SDR SIMA20180125005](https://openairdocs.org/sdr/SIMA20180125005), Jan 25, 2018: FRAME. CHAFED. FRAME 69 CHAFED AT THE V-BAND CLAMP, STRINGER 19L. REPAIRED THE FRAME IAW SRM 53-00-04.
- [SDR SIMA20180125004](https://openairdocs.org/sdr/SIMA20180125004), Jan 25, 2018: SKIN. CHAFED. RUDDER 1 HAS CHAFE ABOVE PANEL 326AL. REPAIRED THE SKIN IAW ERS-EM-55MR-633.
- [SDR SIMA20170414003](https://openairdocs.org/sdr/SIMA20170414003), Apr 14, 2017: LIGHT. UNKNOWN. MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. PERFORMED AN OPS CHECK, CHECKED GOOD IAW AMM TASK 33-50-00-700-801-A
- [SDR SIMA20161216001](https://openairdocs.org/sdr/SIMA20161216001), Dec 16, 2016: TANK UNIT. FAILED. IMMEDIATELY AFTER TAKE OFF, RECEIVED A FUEL IMBALANCE. TANK 1 INDICATION DROPPED APROX. 900 LBS. BOTH QUANTITY INDICATIONS WERE ERRATIC AND BECAME UNRELIABLE. D
- [SDR SIMA20160323002](https://openairdocs.org/sdr/SIMA20160323002), Mar 23, 2016: CONNECTOR. BROKEN. FLOOR PROXIMITY STRIP LIGHT AT FLOORBOARD 251JF HAS A BROKEN CONNECTOR. REPAIRED FLOOR PROXIMITY STRIP LIGHT IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD.
- [SDR SIMA20151229002](https://openairdocs.org/sdr/SIMA20151229002), Dec 29, 2015: FILTER. DIRTY. BLEED 1 OVERTEMP INFLIGHT. VISUALLY INSPECTED FAN AIR VLV LINES, NO DAMAGE FOUND. FOUND CLEAN FAN AIR VLV FILTER IAW AMM 36-11-03. PERFORMED OPERATIONS CHECK IA
- [SDR SIMA20151127001](https://openairdocs.org/sdr/SIMA20151127001), Nov 27, 2015: DETECTOR. FAILED. AFTER TAKING RUNWAY FOR POSITION & HOLD RECEIVED ICE CONDITION ADVISORY MSG FOLLOWED BY A ICE CONDITION. ANTI-ICE WARNING MSG PRIOR TO TAKEOFF ROLL. AFTER A FEW
- [SDR SIMA20151125002](https://openairdocs.org/sdr/SIMA20151125002), Nov 25, 2015: WIRE. BROKEN. LIGHT ELEMENT OF PROXIMITY LIGHT STRIP, NR 6 HAS A BROKEN WIRE. R & R NR 6 FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12. SEE NRTC BOW 205943 FOR OPERATIONAL CHE
- [SDR SIMA20151125003](https://openairdocs.org/sdr/SIMA20151125003), Nov 25, 2015: FRAME. CRACKED. FRAME 23 IS CRACKED, BETWEEN STRINGER 15R - 16R. REPAIRED FRAME 23 AT STRINGER 16R IAW SRM 51-40-02 & EO EM-53MR-1808.
- [SDR SIMA20151125004](https://openairdocs.org/sdr/SIMA20151125004), Nov 25, 2015: CONNECTOR. MISSING. EMERGENCY LIGHT STRIP WIRE AT SEAT LOCATION 13 A IS MISSING SPLICE CONNECTOR. REPAIRED & INSTALLED SERVICEABLE SPLICE CONNECTOR ON EMER LIGHT STRIP WIRE AT SEAT
- [SDR SIMA20151125001](https://openairdocs.org/sdr/SIMA20151125001), Nov 25, 2015: WIRE. CHAFED. PROXIMITY LIGHT STRIP NR 1 WIRE AT THE FLOORBOARD IS MISSING AN ELEC CONNECTOR & THE SAME WIRE IS CHAFED WITH BARE WIRE SHOWING. R & R ELEC CONNECTOR, MALE & AC
- [SDR SIMA20151123003](https://openairdocs.org/sdr/SIMA20151123003), Nov 23, 2015: SKIN. CRACKED. POSSIBLE CRACKS ON LT REAR FUSELAGE RIVETS FRAMES 77 - 79. REPAIRED LT UPPER FUSELAGE SKIN CRACK AT FRAME 77 & STRINGER 06L IAW ERS-EM-53MR-1795.
- [SDR SIMA20151121009](https://openairdocs.org/sdr/SIMA20151121009), Nov 21, 2015: FLOORBEAM. CORRODED. CENTER FLOORBEAM HAS CORROSION AFT OF THE CROSS MEMBER AT FRAME 27. REPAIRED CTR FLOORBEAM CORROSION AFT OF THE CROSS MEMBER AT FRAME 27 BY INSTALLED EXTERNAL A
- [SDR SIMA20151121008](https://openairdocs.org/sdr/SIMA20151121008), Nov 21, 2015: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM HAS CORROSION, FWD OF THE CROSS MEMBER AT FRAME 27. REPAIRED LT OMEGA BEAM CORROSION BY INSTALLING REPAIR DOUBLER IAW SRM 53-00-10 FIG 202 SHEET
- [SDR SIMA20151121007](https://openairdocs.org/sdr/SIMA20151121007), Nov 21, 2015: SKIN. CRACKED. RIGHT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 & ABOVE STRINGER 2R, CRACK IS APPROX 3/8" LONG. REPAIRED IAW ERS-EM-53MR-1793.
- [SDR SIMA20151120008](https://openairdocs.org/sdr/SIMA20151120008), Nov 20, 2015: DOOR SILL. CORRODED. FORWARD SERVICE DOOR SILL IS CORRODED. REPAIRED FWD SERVICE DOOR SILL IAW ERS-EM-53MR-1792.
- [SDR SIMA20151106012](https://openairdocs.org/sdr/SIMA20151106012), Nov 6, 2015: CONNECTOR. MISSING. EMERGENCY LIGHT STRIP WIRE AT SEAT LOCATION 13A IS MISSING SPLICE CONNECTOR. REPAIRED & INSTALLED SERVICEABLE SPLICE CONNECTOR ON EMER LIGHT STRIP WIRE AT SEAT 
- [SDR SIMA20151027001](https://openairdocs.org/sdr/SIMA20151027001), Oct 27, 2015: BOLT. LEAKING. STRONG FUEL SMELL IN COCKPIT. REMOVED, REINSTALLED & RESEALED BOLT AT STRINGER 18R & FRAME 40 IAW AMM 20-10-01 & SRM 51-21-01. SEE NRWC 818-ABI-02100 FOR DETAIL
- [SDR SIMA20150811001](https://openairdocs.org/sdr/SIMA20150811001), Aug 11, 2015: LIGHT. INOPERATIVE. EMERGENCY LIGHT IN PSU PANEL AT SEAT 11A INOPERATIVE. REMOVED & INSTALLED SERVICEABLE LAMP IN PSU PANEL AT SEAT 11A IAW AMM 33-50-07. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150621005](https://openairdocs.org/sdr/SIMA20150621005), Jun 21, 2015: CONTROLLER. FAILED. AFTER CLIMB OUT ACFT WAS NOT PRESSURIZING. WE CLIMBED UP TO 10000 FT & RETURNED. R & R AUTO DIGITAL CONTROL IAW AMM 21-21-01. OPERATIONS CHECKED GOOD. PERFORMED
- [SDR SIMA20150414001](https://openairdocs.org/sdr/SIMA20150414001), Apr 14, 2015: BRAKE. CONTAMINATED. HYDRAULIC FLUID UNDER NR 1 BRAKE ASSEMBLY. VISUAL CHECK & OPERATIONAL OF NR 1 BRAKE ASSEMBLY NO LEAKS NOTED IAW AMM 32-41-00.
- [SDR SIMA20150405001](https://openairdocs.org/sdr/SIMA20150405001), Apr 5, 2015: UNKNOWN. ODOR. AT FL 310 IN & OUT OF WEATHER INCLUDING THUNDERS STORM CELLS IN VICINITY, STRONG ODOR OF SMOKE POSSIBLY ELEC IN COCKPIT & CABIN LASTING 2 - 3 MINUTES & DISSIPAT
- [SDR SIMA20150302002](https://openairdocs.org/sdr/SIMA20150302002), Mar 2, 2015: CRADLE. BROKEN. CAPTAINS EMER FLASHLIGHT CRADLE BROKEN. R & R CAPTAINS EMER FLASHLIGHT CRADLE IAW TASK 33-50-16-000-801-A & TASK 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150110001](https://openairdocs.org/sdr/SIMA20150110001), Jan 10, 2015: CRADLE. BROKEN. TRANSFERRED FROM NRWC 818-CMI-01732 ITEM 1. FWD CABIN FLASHLIGHT CRADLE BROKEN. FLIGHT ATTENDANT FWD FLASHLIGHT ASSEMBLY DEFERRED IAW MEL 25-53. FLIGHT ATTENDAN
- [SDR SIMA20141222006](https://openairdocs.org/sdr/SIMA20141222006), Dec 22, 2014: FLASHLIGHT. INTERMITTENT. FLASHLIGHT IN FWD CABIN IS INTERMITTENT. R & R FWD CABIN FLASHLIGHT IAW AMM 33-50-16.
- [SDR SIMA20141222007](https://openairdocs.org/sdr/SIMA20141222007), Dec 22, 2014: FLASHLIGHT. INOPERATIVE. FLASHLIGHT IN THE AFT CABIN IS INOPERATIVE. R & R AFT CABIN FLASHLIGHT IAW AMM 33-50-16.
- [SDR SIMA20141114001](https://openairdocs.org/sdr/SIMA20141114001), Nov 14, 2014: WARNING SYSTEM. FALSE ACTIVATION. ACCESS DOOR OPEN ON EICAS & DOORS ON MFD SHOWS FWD AVIONICS DOOR OPEN AS GEAR CAME UP ON TAKEOFF. OPENED & CLOSED FWD ELEC COMPARTMENT DOOR. OPERATIONS CHECKED 
- [SDR SIMA20141108002](https://openairdocs.org/sdr/SIMA20141108002), Nov 8, 2014: LIGHT. INOPERATIVE. DURING PS 1 INSPECTION FOUND RT AFT EXTERNAL EMER LIGHT INOPERATIVE. R & R RT AFT EXTERNAL EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140525002](https://openairdocs.org/sdr/SIMA20140525002), May 25, 2014: CRADLE. BROKEN. FIRST OFFICER`S EMERGENCY FLASHLIGHT CRADLE BROKEN. R & R FIRST OFFICER`S EMERGENCY FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATION
- [SDR SIMA20140521003](https://openairdocs.org/sdr/SIMA20140521003), May 21, 2014: CONTROL VALVE. MALFUNCTIONED. DURING TAXI AFTER LANDING, RECEIVED SEVERAL BRAKE DEGRADED, WARNING MESSAGES ON EICAS. REPLACED RT INBD SHUTTLE VALVE. AMM ETN-EM-32-236 DID NOT FIX THE PROBLEM
- [SDR SIMA20140510002](https://openairdocs.org/sdr/SIMA20140510002), May 10, 2014: WINDSHIELD. CRACKED. WINDSHIELD ON FIRST OFFICER`S SIDE CRACKED TAXING IN. R & R FIRST OFFICER`S WINDSHIELD IAW AMM 56-10-01. OPERATIONS CHECK LEAK TESTED GOOD IAW ITEM NR 3 & NR 4 
- [SDR SIMA20140417003](https://openairdocs.org/sdr/SIMA20140417003), Apr 17, 2014: HOLDER. BROKEN. FLIGHT ATTENDANT`S FWD FLASHLIGHT HOLDER BROKEN. R & R FLIGHT ATTENDANT`S FWD FLASHLIGHT HOLDER IAW AMM 35-50-00, OPERATIONS CHECKED GOOD.

All 93: https://openairdocs.org/deregistered/N818AE-2025-05-23/reports.md

## 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 20160830014799I](https://openairdocs.org/incident/20160830014799I), Aug 30, 2016: Embraer EMB-135KL (N818AE), Dallas, TX, No damage. On August 30, 2016, at Dallas-fort Worth international airport (dfw), envoy maintenance ENY818, E145, entered the runway safety area on runway 36L without a…

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