# N376SK: 2002 Embraer EMB-135KL, registration cancelled 2017-12-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 8, 2017 - Exported to: South Africa - 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: 145578 - Year built: 2002 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 29, 2002 - Certificate issued: October 6, 2016 - Last registry action: October 6, 2016 - Mode S code: A44BAF - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%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/N376SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=376SK - Page: https://openairdocs.org/deregistered/N376SK-2017-12-08 From the FAA registry file of October 31, 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 (35) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CHQA20121201448](https://openairdocs.org/sdr/CHQA20121201448), Dec 1, 2012: LIGHT. INOPERATIVE. CREW REPORTED THAT THE FLIGHT DECK EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FLIGHT DECK EMERGENCY LIGHT BULB. OPERATIONAL CHECKS WERE GOOD WITH - [SDR CHQA20121002366](https://openairdocs.org/sdr/CHQA20121002366), Oct 2, 2012: SWITCH. MALFUNCTIONED. CREW REPORTED THAT DURING FLIGHT, AND ELECTRICAL ODOR WAS PRESENT IN THE COCKPIT. THE CREW DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE ISOLATED THE - [SDR CHQA20120927363](https://openairdocs.org/sdr/CHQA20120927363), Sep 27, 2012: WIRE HARNESS. DEFECTIVE. CREW REPORTED THAT COCKPIT READING LIGHT WENT OUT AND AN ELECTRICAL BURNING SMELL SOON APPEARED IN THE COCKPIT. MAINTENANCE ISOLATED THE BURNING SMELL TO THE FI - [SDR CHQA20120915359](https://openairdocs.org/sdr/CHQA20120915359), Sep 15, 2012: STRUCTURE. BENT. DURING INSPECTION, THE RIGHT OUTBOARD LEADING EDGE WAS BENT AT THE OUTBOARD FRAME. THE RIGHT OUTBOARD LEADING EDGE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145- - [SDR CHQA20120912358](https://openairdocs.org/sdr/CHQA20120912358), Sep 12, 2012: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT CARBON CROSSMEMBER LEFT OMEGA AT FRAME 27. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10. - [SDR CHQA20120912357](https://openairdocs.org/sdr/CHQA20120912357), Sep 12, 2012: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT CARBON CROSSMEMBER CENTER OMEGA LEFT FLOORBOARD FLANGE BETWEEN FRAME 24 AND 25. THE OMEGA BEAM WAS REPAIRED IN ACCORDA - [SDR CHQA20120912356](https://openairdocs.org/sdr/CHQA20120912356), Sep 12, 2012: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT THE CARBON CROSSMEMBER LEFT OMEGA INBOARD FLOORBOARD FLANGE BETWEEN FRAMES 24 AND 25. THE OMEGA BEAN WAS REPAIRED IN A - [SDR CHQA20120912355](https://openairdocs.org/sdr/CHQA20120912355), Sep 12, 2012: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT THE CARBON CROSSMEMBER CENTER OMEGA FRAME 27. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10. - [SDR CHQA20120508145](https://openairdocs.org/sdr/CHQA20120508145), May 8, 2012: LIGHT. INOPERATIVE. MAINTENANCE REPORTED THAT THE ROW 12 EMERGENCY LIGHT FLOOR STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE DEFERRED THE FLOOR STRIP. THE DEFERRAL WAS CLEARED BY - [SDR CHQA201100479](https://openairdocs.org/sdr/CHQA201100479), Dec 1, 2011: SKIN. DENTED. DURING INSPECTION, A DENT WAS FOUND ON THE FUSELAGE SKIN RF II BETWEEN FRAME 76 AND 77 AND STRINGERS 16R AND 18R. MAINTENANCE REPAIRED THE DENT ON THE FUSELAGE - [SDR CHQA201100482](https://openairdocs.org/sdr/CHQA201100482), Nov 30, 2011: BEAM. CORRODED. DURING INSPECTION, THE LEFT BEAM UNDER THE OUTBOARD SEAT TRACK NUMBER 5, BETWEEN FRAME 47 TO FRAME 53 WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE LEFT BE - [SDR CHQA201100480](https://openairdocs.org/sdr/CHQA201100480), Nov 30, 2011: BEAM. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT LOWER BEAM. MAINTENANCE REPLACED THE CARGO DOOR CUTOUT LOWER BEAM AND INSTALLED WITH A SOLID RIV - [SDR CHQA201100463](https://openairdocs.org/sdr/CHQA201100463), Nov 29, 2011: FRAME. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON FRAME 23 UNDER SILL NUMBER 1. MAINTENANCE REPAIRED THE RIGHT-HAND FRAME 23 UNDER SILL NUMBER 1 IN ACCORDANCE WITH ETD 20 - [SDR CHQA201100462](https://openairdocs.org/sdr/CHQA201100462), Nov 29, 2011: SHEAR PLATE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON CARGO DOOR SURROUND STRUCTURE FORWARD AND AFT L SHAPE. MAINTENANCE REPLACED THE CARGO DOOR SURROUND STRUCTURE FORWARD - [SDR CHQA201100484](https://openairdocs.org/sdr/CHQA201100484), Nov 29, 2011: ANGLE. CRACKED. DURING INSPECTION, MID WING BOX OMEGA BEAN ANGLES WERE FOUND TO BE CRACKED AT FRAME 50 (PN: 140-04214-607 AND 140-04214-609). MAINTENANCE REPLACED THE MID WING - [SDR CHQA201100483](https://openairdocs.org/sdr/CHQA201100483), Nov 29, 2011: BEAM. CORRODED. DURING INSPECTION, AN EXISTING REPAIR ON THE LEFT INBOARD BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE LEFT INBOARD BEAM AT FRAME 20 IN A - [SDR CHQA201100481](https://openairdocs.org/sdr/CHQA201100481), Nov 29, 2011: FRAME. CRACKED. DURING INSPECTION, THE LEFT FRAME 10 WAS FOUND CRACKED INSIDE THE COCKPIT BELOW THE SIDE WINDOW. MAINTENANCE REPLACED THE LEFT FRAME 10 INSIDE THE COCKPIT BELOW - [SDR CHQA201100271](https://openairdocs.org/sdr/CHQA201100271), Jul 9, 2011: SIGN. INOPERATIVE. DURING INSPECTION, THE SERVICE DOOR EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE SERVICE DOOR EMERGENCY EXIT SIGN WITH NO FURTHER D - [SDR CHQA201100176](https://openairdocs.org/sdr/CHQA201100176), May 14, 2011: ACM. DAMAGED. AFTER TAKEOFF, THE CREW REPORTED LIGHT SMOKE IN THE COCKPIT AT ABOUT 7,000FT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO KORD, LANDING WITHOUT INCIDENT. EME - [SDR CHQA201100016](https://openairdocs.org/sdr/CHQA201100016), Jan 19, 2011: SCREW. MISINSTALLED. DURING INSPECTION, THE LEFT OVERWING EMERGENCY EXIT ON THE LEFT PASSENGER ESCAPE HATCH WAS FOUND TO BE BLOCKED. MAINTENANCE FOUND A SCREW THAT WAS NOT INSTALLED - [SDR CHQA201000187](https://openairdocs.org/sdr/CHQA201000187), Sep 30, 2010: RMU. MALFUNCTIONED. ON APPROACH INTO MKE THE FLIGHT CREW REPORTED A RMU 2 FAILURE WITH RMU, ALSO NOT WORKING PROPERLY. MKE APPROACH WAS THE ONLY FREQUENCY THAT RMU WOULD TUNE. THE - [SDR CHQA201000154](https://openairdocs.org/sdr/CHQA201000154), Aug 11, 2010: LIGHT. INOPERATIVE. DURING INSPECTION, THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE AFT EXTERIOR EMERGENCY LIGHT BULB AND THE E - [SDR CHQA201000101](https://openairdocs.org/sdr/CHQA201000101), May 23, 2010: LIGHT. DISCONNECTED. DURING INSPECTION, THE FLOOR PROXIMITY EMERGENCY LIGHT NEXT TO SEAT 1A WAS INOP. MAINTENANCE FOUND DISCONNECTED WIRES ON THE LIGHT STRIP AND RE-ATTACHED IN ACCO - [SDR CHQA201000080](https://openairdocs.org/sdr/CHQA201000080), Apr 16, 2010: BRAKE. FAULTY. THE CREW REPORTED THE FLAP POSITION INDICATION WAS INOP ON APPROACH. MAINTENANCE REPLACED THE LEFT FLAP WING BRAKE DUE TO FAIL MESSAGES FOUND ON THE CMC WITH NO - [SDR CHQA201000075](https://openairdocs.org/sdr/CHQA201000075), Apr 10, 2010: BATTERY PACK. DISCHARGED. DURING INSPECTION, ALL FOUR EMERGENCY LIGHT BATTERY PACKS WERE FOUND TO BE DISCHARGED. ALL FOUR EMERGENCY LIGHT BATTERIES WERE REPLACED WITH NO FURTHER DEFECTS - [SDR CHQA200900213](https://openairdocs.org/sdr/CHQA200900213), Sep 30, 2009: PRESSURE SWITCH. DEFECTIVE. FLIGHT 5344 STL TO RDU. IN FLIGHT AT FL330 THE FLIGHT CREW RECEIVED AN AUTO PILOT FAIL AND YAW DAMPER FAIL MESSAGE FOLLOWED SHORTLY AFTER WITH A RUDDER 1-2 INOP - [SDR CHQA200900149](https://openairdocs.org/sdr/CHQA200900149), Jun 29, 2009: INVERTER. INOPERATIVE. DURING INSP, THE EXIT IDENTIFIER SIGN ON THE RT SIDE OF THE ACFT ABOVE SEATS 11BC WAS FOUND TO BE INOP. MX REPLACED THE NR 5 INVERTER IAW AMM 33-50-11 AND THE E - [SDR CHQA200800191](https://openairdocs.org/sdr/CHQA200800191), Oct 2, 2008: HOSE. LOOSE. ON INITIAL CLIMBOUT, THE FLIGHT CREW RECEIVED A HYD SYS 1 LO QTY EICAS MESSAGE. THE HYDRAULIC PAGE WAS BROUGHT UP ON THE MFD AND THE HYDRAULIC SYS 1 INDICATED I - [SDR CHQ2008F00011](https://openairdocs.org/sdr/CHQ2008F00011), Sep 13, 2008: SOCKET. BURNED. DURING CRUISE, THE FLIGHT CREW RECEIVED A PITOT 1 INOP EICAS MESSAGE AND SMELLED SMOKE. IMMEDIATELY AFTER THEY RECEIVED AN AOA 1 HEAT INOP MESSAGE AND THE FLIGH - [SDR CHQA200800158](https://openairdocs.org/sdr/CHQA200800158), Aug 4, 2008: PROXIMITY SENSOR. FAULTY. FLIGHT 5360, STL TO ATL. DURING CLIMB, AFTER RETRACTING THE LANDING GEAR, THE FLIGHT CREW RECEIVED A LG AIR/GND FAIL MESSAGE ON EICAS ALONG WITH AURAL WARNINGS - [SDR CHQ2008F00000](https://openairdocs.org/sdr/CHQ2008F00000), Jul 25, 2008: WINDSHIELD. CRACKED. FLIGHT 5349, MSY TO STL. DURING CRUISE THE FLIGHT CREW REPORTED HEARING A LOUD BANG AND NOTICED THAT THE FIRST OFFICER’S WINDSHIELD HAD CRACKED. THE FLIGHT THEN - [SDR CHQA200800028](https://openairdocs.org/sdr/CHQA200800028), Feb 12, 2008: PROXIMITY SENSOR. MALFUNCTIONED. STL TO MSP, ON INITIAL CLIMB, THE CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS WHEN THEY ATTEMPTED TO MOVE THE LANDING GEAR LEVER TO THE UP POS - [SDR CHQA20070053](https://openairdocs.org/sdr/CHQA20070053), Sep 17, 2007: CONTROL VALVE. FAULTED. STL TO MSP - UPON LOWERING LANDING GEAR ON FINAL APPROACH, CREW RECEIVED "INBOARD BRAKE INOP" EICAS MESSAGE. THE CREW DID A GO-AROUND TO CONSULT THE QRH AND EVA - [SDR CHQA200500069](https://openairdocs.org/sdr/CHQA200500069), Mar 31, 2005: BULB. BURNED OUT. LEFT HAND FORWARD EMERGENCY EXIT LIGHT IS INOPERATIVE. RELAMPED LEFT HAND FORWARD EMERGENCY EXIT LIGHT IAW EMB 140 AMM 33-50-07. OPS CHECK GOOD. - [SDR CHQA000543](https://openairdocs.org/sdr/CHQA000543), Aug 24, 2004: POWER SUPPLY. INOPERATIVE. OVERWING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED NR 3 AND NR 4 EMERGENCY POWER SUPPLIES AND OVERWING EMERGENCY LIGHT. OPS CHECK GOOD PER MAINTENANCE MANUA ## 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 20080913846989I](https://openairdocs.org/incident/20080913846989I), Sep 13, 2008: Emb EMB135KL (N376SK), Moline, IL, No damage. Chautauqua flight 5340 operating on September 13, 2008 from stl to msp, diverted to mli based on report of smoke in the cabin. Crewmembers initiated an… --- 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.