# N843AE: 2003 Embraer EMB-135KL, registration cancelled 2025-11-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 19, 2025 - Exported to: Nigeria - Status when cancelled: Valid registration - Airframe: [Embraer EMB-135KL](https://openairdocs.org/model/embraer-emb-135kl) (registry code 3260302) - 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), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 145680 - Year built: 2003 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 24, 2003 - Certificate issued: March 16, 2024 - Last registry action: March 16, 2024 - Mode S code: AB8B03 - Owner when cancelled: [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE) - Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake) - Owner type: Corporation - Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N843AE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=843AE - Page: https://openairdocs.org/deregistered/N843AE-2025-11-19 From the FAA registry file of November 5, 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 (89, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SIMA20201121001](https://openairdocs.org/sdr/SIMA20201121001), Nov 21, 2020: POWER SUPPLY. INOPERATIVE. AFTMOST 3 EMERGENCY LIGHT STRIPS INOPERABLE. C/A: REMOVED AND REPLACED BATTERY POWER SUPPLY NR 4, IAW AMM 33-50-04. OPERATIONS CHECK GOOD. - [SDR SIMA202009032001](https://openairdocs.org/sdr/SIMA202009032001), Sep 2, 2020: CABIN PRESSURE. MALFUNCTIONED. AUTO PRESSURIZATION ISSUE CABIN ALT REACHED 9000FT A/C AT 33,000FT, REPRESSURIZED UPON DESCENT INITIATION. C/A-PERFORMED FUNCTIONAL TEST OF PRESSURIZATION CONTR - [SDR SIMA20200716001](https://openairdocs.org/sdr/SIMA20200716001), Jul 16, 2020: A/C PACK. SHUTDOWN. NR 2 PACK SHUT DOWN WITH NO MESSAGE. PERFORMED OPERATIONAL TEST OF COOLING PACK SYSTEM IAW AMM 21-51-00. OPC GOOD, NO DEFECTS NOTED AT THIS TIME. - [SDR SIMA202006187003](https://openairdocs.org/sdr/SIMA202006187003), Jun 17, 2020: LAMP. INOPERATIVE. MAIN DOOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECK - [SDR SIMA202006187004](https://openairdocs.org/sdr/SIMA202006187004), Jun 17, 2020: LAMP. INOPERATIVE. COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED COCKPIT CEILING EMERGENCY LAMP IAW AMM TASK 33-50-05-000-801-A AND 33-50-05-400-801-A. OPC GOOD. - [SDR SIMA202004032001](https://openairdocs.org/sdr/SIMA202004032001), Apr 2, 2020: LIGHT. INOPERATIVE. MAIN DOOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-10. OPS CHECK GOOD. - [SDR SIMA2019122019001](https://openairdocs.org/sdr/SIMA2019122019001), Dec 19, 2019: DUCT. UNSECURE. STRANGE ODOR OF DIRTY SOCKS COMING FROM PACKS WHILE RUNNING ON APU BLEED. SECURED RISER DUCT AT SEAT 9BC IAW AMM 21-20-04 . REMOVED AND REPLACED THE LT CONDENSE - [SDR SIMA201910310003](https://openairdocs.org/sdr/SIMA201910310003), Oct 30, 2019: BLEED VALVE. FAILED. PACK VALVE AND BLD VALVE CLOSED INFLIGHT ON #2. PACK 2 VALVE C/B POPPED.-C/A-REMOVED AND REPLACED #2 PACK VALVE IAW AMM 21-51-01. OPERATIONAL CHECK GOOD. #2 BLD - [SDR SIMA20190915003](https://openairdocs.org/sdr/SIMA20190915003), Sep 15, 2019: INVERTER. INOPERATIVE. COCKPIT EMERGENCY SIGN EXIT LIGHT INOP. C/A-REMOVED AND REPLACED EMERGENCY EXIT SIGN INVERTER 1 IAW AMM 33-50-11. OPS CHECK GOOD. - [SDR SIMA2019083029002](https://openairdocs.org/sdr/SIMA2019083029002), Aug 29, 2019: LAMP. INOPERATIVE. DURING INSPECTION, FOUND AISLE EMERGENCY LIGHT LAMP INOPERATIVE AT SEAT 11A. REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP. OPS CHECKED GOOD IAW AMM 33-50-08. - [SDR SIMA20190708002](https://openairdocs.org/sdr/SIMA20190708002), Jul 8, 2019: HOLDER. BROKEN. FOUND AFT FLASHLIGHT HOLDER BROKEN. C/A-REMOVED AND REPLACED FLASHLIGHT, AFT HOLDER ASSEMBLY IAW AMM 33-50-16. OPC GOOD. - [SDR SIMA20190313001](https://openairdocs.org/sdr/SIMA20190313001), Mar 13, 2019: SPLICE. INOPERATIVE. SUPPLEMENTAL FOUND EMERG. FLOOR STRIP LIGHT AT PAX SEAT 11 AND 12 DOES NOT ILLUMINATE. C/A-REMOVED AND REPLACED BATTERY AND CHARGER ASSY. IAW W/C # 33-700-19. D - [SDR SIMA2018062100002](https://openairdocs.org/sdr/SIMA2018062100002), Jun 20, 2018: LIGHT. INOPERATIVE. FLOOR EMERGENCY LIGHT IN THE CABIN, ALONG SEATS 12A AND 13A DID NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. NO - [SDR SIMA2018053126006](https://openairdocs.org/sdr/SIMA2018053126006), May 26, 2018: SWITCH. DIRTY. LEFT WING LEADING EDGE DAMAGED, ACCESS DOOR OPEN MESSAGE. REAR AVIONICS DOOR INDICATION RED. CLEARED AFTER 5 MINUTES. CLEANED WARNING MICROSWITCH FOR REAR ELEC - [SDR SIMA2018052512007](https://openairdocs.org/sdr/SIMA2018052512007), May 12, 2018: WIRE. BROKEN. WIRE FOR EMERGENCY LIGHT WAS BROKEN. REPAIRED EMERGENCY LIGHT WIRE IAW SWPM 20-21-00. - [SDR SIMA2018052512006](https://openairdocs.org/sdr/SIMA2018052512006), May 12, 2018: WIRE. BROKEN. EMERGENCY LIGHT WIRE WAS BROKEN. REPAIRED WIRE IAW SWPM 20-21-00. - [SDR SIMA2018052510007](https://openairdocs.org/sdr/SIMA2018052510007), May 10, 2018: SHEAR TIE. CORRODED. FRAME 65 SHEAR TIE WAS CORRODED. REPAIRED THE SHEAR IAW IAW SRM 53-31-04. - [SDR SIMA2018052510008](https://openairdocs.org/sdr/SIMA2018052510008), May 10, 2018: SKIN. CRACKED. FUSELAGE SKIN UPPER SPLICE PLATE BETWEEN FRAMES 80 AND 81 WAS CRACKED. PERFORMED A PERMANENT REPAIR IAW SRM 51-40-02 - [SDR SIMA2018052510010](https://openairdocs.org/sdr/SIMA2018052510010), May 10, 2018: SKIN. CRACKED. RIGHT UPPER FUSELAGE SKIN WAS CRACKED AFT OF FRAME 75 AND ABOVE STRINGER 2R, THE CRACK WAS APPROXIMATELY 1 INCH LONG . PERFORMED A PERMANENT REPAIR IAW SRM 53-3 - [SDR SIMA2018052510009](https://openairdocs.org/sdr/SIMA2018052510009), May 10, 2018: SHEAR TIE. CORRODED. FRAME 68, FWD SHEAR TIE, AT THE CARGO DOOR CUTOUT HAD AN AREA OF CORROSION BETWEEN STRINGERS 15 - 16L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-31-04 - [SDR SIMA2018052509007](https://openairdocs.org/sdr/SIMA2018052509007), May 9, 2018: PROFILE. GOUGED. LEFT OVERWING EXIT LOWER PROFILE GOUGED IN THE RADIUS. REMOVED AND REPALCED LOWER FRAME PROFILE IAW SRM 51-40-02. - [SDR SIMA20180508004](https://openairdocs.org/sdr/SIMA20180508004), May 8, 2018: PROFILE. CORRODED. CARGO DOOR LOWER FRAME PROFILE CORRODED AT NUTPLATE HOLES. REMOVED AND REPLACED CARGO DOOR LOWER FRAME PROFILE IAW SRM 51-40-02. - [SDR SIMA20180508005](https://openairdocs.org/sdr/SIMA20180508005), May 8, 2018: SKIN. GOUGED. FUSELAGE EXTERNAL SKIN INSIDE PYLON PANEL 414DB GOUGED. FUSELAGE EXTERNAL SKIN INSIDE PYLON PANEL 414DB GOUGE REPAIRED IAW SRM 53-31-01 FIG 220. - [SDR SIMA20180504006](https://openairdocs.org/sdr/SIMA20180504006), May 4, 2018: FITTING. DAMAGED. LT AILERON DAMPER FITTING GOUGED INSIDE FITTING. REMOVED AND INSTALLED LT AILERON DAMPER FITTING IAW EO EM-27MR-112 REPAIR. - [SDR SIMA20180504008](https://openairdocs.org/sdr/SIMA20180504008), May 4, 2018: DOOR SILL. CORRODED. SSI 53-20-10 SERVICE DOOR CENTER SILL CORRODED AT FWD SCREW HOLE. REPAIRED SERVICE DOOR CUTOUT LOWER CENTER SILL IAW SRM 53-21-02, FIGURE 201. - [SDR SIMA20180504007](https://openairdocs.org/sdr/SIMA20180504007), May 4, 2018: SKIN. DENTED. PERFORM PERMANENT REPAIR OF DENT(.5 X .5 X .028) WITH PAINT MISSING ON LT SIDE OF FUSELAGE BELOW CABIN WINDOW 1A IN RED STRIPE IAW SRM 53-21-01. PERFORMED PERMA - [SDR SIMA2018060400010](https://openairdocs.org/sdr/SIMA2018060400010), Apr 4, 2018: STRINGER. CRACKED. STRINGER 2R CRACKED AT FRAME 75. ACCOMPLISHED A REPAIR OF THE STRINGER IAW ERS-EM-53MR-3276. - [SDR SIMA2018060400007](https://openairdocs.org/sdr/SIMA2018060400007), Apr 4, 2018: LAMP. INOPERATIVE. EMERGENCY LIGHT INOPERATIVE AT THE FA CEILING PANEL. REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT IAW AMM 33-50-08. OPS CHECKED GOOD. - [SDR SIMA2018060400008](https://openairdocs.org/sdr/SIMA2018060400008), Apr 4, 2018: BULB. INOPERATIVE. EMERGENCY EXIT ROW CEILING PANEL EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE BULB IN THE EMERGENCY LIGHT IAW AMM 33-50-08. OPS CHECKED GOOD. - [SDR SIMA2018060400009](https://openairdocs.org/sdr/SIMA2018060400009), Apr 4, 2018: FRAME. CRACKED. FRAME 66 CRACKED, LOCATED BETWEEN STRINGERS 17L AND 18L. REPAIRED THE FRAME IAW ERS-EM-53MR-3279. - [SDR SIMA2018060400006](https://openairdocs.org/sdr/SIMA2018060400006), Apr 4, 2018: LIGHT. DAMAGED. LEFT EMERGENCY LIGHT STRIP EXTRUSIONS NR 1 THRU 8 WERE DAMAGED. REMOVED AND REPLACED THE LT EMERGENCY LIGHT IAW AMM 33-50-12. - [SDR SIMA20170107006](https://openairdocs.org/sdr/SIMA20170107006), Jan 7, 2017: FLASHLIGHT. INOPERATIVE. AFT CABIN FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT. - [SDR SIMA20160828002](https://openairdocs.org/sdr/SIMA20160828002), Aug 28, 2016: SWITCH. FAILED. F/A FWD FLASHLIGHT SWITCH CAME APART. REMOVED AND REPLACED THE FLASHLIGHT IAW STANDARD MAINTENANCE PRACTICES - [SDR SIMA20160523004](https://openairdocs.org/sdr/SIMA20160523004), May 23, 2016: DISPLAY. FAILED. FIRST OFFICERS MFD FAILED, ACCOMPANIED BY STRONG ELEC ODOR. NO EVIDENCE OF BURNED PINS OR WIRES. R & R FIRST OFFICERS MFD IAW AMM 34-22-01. OPERATIONS CHECKED G - [SDR SIMA20160203003](https://openairdocs.org/sdr/SIMA20160203003), Feb 3, 2016: HOLDER. BROKEN. FIRST OFFICERS FLASHLIGHT HOLDER BROKEN. DEFERRED IAW MEL 25-53. R & R FIRST OFFICERS FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONAL CHECK GOOD & MEL RESTORE - [SDR SIMA20150921004](https://openairdocs.org/sdr/SIMA20150921004), Sep 21, 2015: SWITCH. FAILED. ABORTED TAKEOFF AT 80 KNOTS, WARNING TAKEOFF CONFIG BRAKES & SPOILER OPEN. R & R EMER PARKING BRAKE SWITCH IAW AMM 32-44-07. ALL CHECKED GOOD, OK FOR SERVICE. S - [SDR SIMA20150709004](https://openairdocs.org/sdr/SIMA20150709004), Jul 9, 2015: INVERTER. INOPERATIVE. LEFT EMER EXIT DOOR, EXIT SIGN INOPERATIVE. R & R NR 5 EMER LIGHT INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD. - [SDR SIMA20150709003](https://openairdocs.org/sdr/SIMA20150709003), Jul 9, 2015: LIGHT. INOPERATIVE. OVERHEAD EMER LIGHT AT ROW 15 - 16 INOPERATIVE. RELAMPED CEILING EMER LIGHT AT ROW 15 - - 16 IAW AMM 33-50-08. OPERATIONS CHECKED GOOD. - [SDR SIMA20150512006](https://openairdocs.org/sdr/SIMA20150512006), May 12, 2015: INVERTER. MALFUNCTIONED. LEFT CABIN EMER LIGHT AT LT OVERWING EMER EXIT MARKER SIGN INOPERATIVE. RESET EMER LIGHT INVERTER AT LT OVERWING EXIT IAW AMM 33-50-11. OPERATIONS CHECKED GOOD. - [SDR SIMA20150301004](https://openairdocs.org/sdr/SIMA20150301004), Mar 1, 2015: CRADLE. BROKEN. CAPTAINS FLASHLIGHT CRADLE BROKEN. R & R CAPTAINS EMER FLASHLIGHT ASSEMBLY IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD. - [SDR SIMA20150209006](https://openairdocs.org/sdr/SIMA20150209006), Feb 9, 2015: BRAKE. DEFECTIVE. AFTER LANDING WHEN TAXING ON TAXIWAY, THE LT BRAKE WAS MAKING UNUSUAL NOISE & FELT LIKE IT WAS CATCHING ALMOST LOCKING, COULD FEEL IT ON THE PEDAL. STOPPED ACFT - [SDR SIMA20150113010](https://openairdocs.org/sdr/SIMA20150113010), Jan 13, 2015: SKIN. CHAFED. RUDDER NR 1 LE IS CHAFED. REPAIRED IAW ERS EM-55MR-217. - [SDR SIMA20150112008](https://openairdocs.org/sdr/SIMA20150112008), Jan 12, 2015: FITTING. LOOSE. RIGHT AILERON PCA FITTING INBD LUG & OTBD HAT BUSHING IS LOOSE IN THE FITTING. R & R RT AILERON PCA FITTING IAW EO EM-27MR-112. - [SDR SIMA20150111005](https://openairdocs.org/sdr/SIMA20150111005), Jan 11, 2015: FLOOR SUPPORT. CORRODED. RIGHT OMEGA BEAM, SHOULD READ CTR, IS CORRODED BETWEEN FRAMES 57 - 59. REPAIRED RT OMEGA BEAM IAW ERS-EM-53MR-1011. - [SDR SIMA20150108035](https://openairdocs.org/sdr/SIMA20150108035), Jan 8, 2015: HINGE FITTING. DAMAGED. RUDDER II UPPER HINGE FITTING, UPPER FLANGE BUSHING HOLE BEYOND LIMITS. INSTALLED NEW RUDDER II UPPER HINGE FITTING IAW SRM 55-40-02 & ETN EM-55-070. - [SDR SIMA20150106009](https://openairdocs.org/sdr/SIMA20150106009), Jan 6, 2015: SKIN. DAMAGED. HFEC INSPECTION INDICATES FLAW 3/4 INCHES LONG IN FUSELAGE SKIN, 3.5 INCHES FROM THE VERTICAL STAB BASE AT FRAME 75 BETWEEN STRINGERS 1 - 2 LT SIDE. COMPLETED R - [SDR SIMA20150105003](https://openairdocs.org/sdr/SIMA20150105003), Jan 5, 2015: BRACKET. CRACKED. BLEED DUCT BRACKET IS COMPLETELY CRACKED THROUGH 2 INCHES AT FRAME 74 STRINGER 11R. R & R BLEED DUCT BRACKET AT RT SIDE FRAME 74 & INSTALLED AIR DUCT IAW SRM 51 - [SDR SIMA20150104030](https://openairdocs.org/sdr/SIMA20150104030), Jan 4, 2015: ATTACH ANGLE. CRACKED. RIGHT OVERWING PANEL UPPER ATTACHMENT ANGLE HAS A 1 1/4 INCH CRACK AT THE RIVET ON FRAME 49. COMPLIED WITH REPAIR OF RT OVERWING PANEL UPPER ATTACHMENT ANGLE ON - [SDR SIMA20150104031](https://openairdocs.org/sdr/SIMA20150104031), Jan 4, 2015: ATTACH ANGLE. CRACKED. RIGHT OMEGA BEAM ATTACH ANGLES ARE CRACKED BETWEEN FRAMES 47 - 48. COMPLIED WITH REPAIR OF RT OMEGA BEAM ATTACH ANGLES BETWEEN FRAMES 47 - 48 IAW SRM 52-32-02. - [SDR SIMA20150104015](https://openairdocs.org/sdr/SIMA20150104015), Jan 4, 2015: FITTING. CRACKED. FRAME SHEAR CLIP IS CRACKED APPROX 1 INCH AT FRAME 79 BETWEEN STRINGERS 2R - 3R. R & R FRAME SHEAR CLIP AT FRAME 79 BETWEEN STRINGER 2R - 3R IAW SRM 51-40-02. All 89: https://openairdocs.org/deregistered/N843AE-2025-11-19/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB WPR09LA255](https://openairdocs.org/ntsb/WPR09LA255), May 21, 2009: Embraer EMB-135 (N843AE), Los Angeles, CA, substantial damage. Probable cause: The flight crew's failure to adequately monitor and maintain clearance from a parked aircraft while taxiing. Contributing to the accident was an improperly parked airplane that encroached upon the… ## 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. - [Accident 20090521007209A](https://openairdocs.org/incident/20090521007209A), May 21, 2009: Emb EMB135KL (N843AE), Los Angeles, CA, Minor damage. (-23) American eagle #3085 (lax-san) N843AE active aircraft was pushed back from terminal by ground crew and disconnected from tow bar. Reporting inspector… --- 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.