# N268SK: 2000 Embraer EMB-145LR, registration cancelled 2018-09-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 8, 2018 - Status when cancelled: Valid registration - Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212) - Engine: [Allison AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030) - Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 145270 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 29, 2000 - Certificate issued: July 13, 2000 - Last registry action: May 7, 2018 - Mode S code: A29E4F - Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%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/N268SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=268SK - Page: https://openairdocs.org/deregistered/N268SK-2018-09-08 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-145LR: https://openairdocs.org/model/embraer-emb-145lr.md ## Service difficulty reports (27) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CHQA20140711210](https://openairdocs.org/sdr/CHQA20140711210), Jul 11, 2014: LIGHT. INOPERATIVE. DURING INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX RELAMPED THE EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTH - [SDR CHQA20140621190](https://openairdocs.org/sdr/CHQA20140621190), Jun 21, 2014: SOLENOID VALVE. FAILED. CREW REPORTED THAT THERE WAS A LOUD NOISE IN COCKPIT DURING FLIGHT. THE CREW SUSPECTED THAT THE NLG DOORS WERE OPEN. THE ACFT WAS RETURNED TO FIELD & LANDED WIT - [SDR CHQA20131013369](https://openairdocs.org/sdr/CHQA20131013369), Oct 13, 2013: A/C PACK. FAILED. CREW REPORTED THAT DURING CRUISE, SMOKE WAS NOTICED IN THE COCKPIT. THE CREW DIVERTED AND DECLARED AN EMERGENCY. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MAINT - [SDR CHQA20130725190](https://openairdocs.org/sdr/CHQA20130725190), Jul 25, 2013: INVERTER. INOPERATIVE. DURING INSPECTION, THE AISLE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE NR 2 INVERTER. OPS CHECKED GOOD WITH NO FURTHER DEFECTS - [SDR CHQA20130725189](https://openairdocs.org/sdr/CHQA20130725189), Jul 25, 2013: INVERTER. INOPERATIVE. DURING INSPECTION, THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE NR 3 INVERTER. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS - [SDR CHQA20130610209](https://openairdocs.org/sdr/CHQA20130610209), Jun 10, 2013: FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON FRAME 65 AT THE LOWER DOOR PLATE. THE FRAME WAS REPAIRED IAW SRM 53-31-04 AND SRM 51-40-02. - [SDR CHQA20120628209](https://openairdocs.org/sdr/CHQA20120628209), Jun 28, 2012: SUPPORT. CORRODED. DURING INSPECTION, THE AFT RIGHT FUSELAGE INSIDE ACCESS DOOR 272AR TOILET DRAIN VALVE SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE DISCHARGE CUP I - [SDR CHQA20120628208](https://openairdocs.org/sdr/CHQA20120628208), Jun 28, 2012: FRAME. DAMAGED. DURING INSPECTION, A HOLE WAS FOUND IN FRAME 65 ON THE RIGHT SIDE NEAR STRINGER 12R. MAINTENANCE INSTALLED A NEW REPAIR DOUBLER IN ACCORDANCE WITH ETD2012-145-0 - [SDR CHQA20120605180](https://openairdocs.org/sdr/CHQA20120605180), Jun 5, 2012: TRANSDUCER. DISCONNECTED. CREW REPORTED LOSS OF BRAKING EFFECTIVENESS ON LANDING ROLL. A BRAKE DEGRADED MESSAGE APPEARED AS WELL. AFTER PUSHING THE BRAKES TO THE FLOOR BRAKES BEGAN WORKI - [SDR CHQA20120203040](https://openairdocs.org/sdr/CHQA20120203040), Feb 3, 2012: WARNING SYSTEM. FALSE ACTIVATION. CREW REPORTED THAT THEY RECEIVED AN EMERGENCY LIGHT NO ARMED EICAS MESSAGE WITH THE EMERGENCY LIGHTS IN THE ARMED POSITION DURING PRE-FLIGHT INSPECTION. MAINTEN - [SDR CHQA201200037](https://openairdocs.org/sdr/CHQA201200037), Jan 30, 2012: INVERTER. INOPERATIVE. DURING INSPECTION, MULTIPLE INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHEC - [SDR CHQA201100415](https://openairdocs.org/sdr/CHQA201100415), Oct 24, 2011: BATTERY. DISCHARGED. DURING INSPECTION, THE EMERGENCY FLOOR LIGHTS BETWEEN ROW 8 AND 12 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 3 EMERGENCY LIGHT BATTERY. OPER - [SDR CHQA201100253](https://openairdocs.org/sdr/CHQA201100253), Jun 12, 2011: FRAME. CRACKED. DURING INSPECTION, THE FORWARD FUSELAGE II LEFT AND RIGHT FRAME 10 WAS FOUND TO BE CRACKED AT THE INTERSECTION OF THE DIRECT VISION WINDOW LOWER BEAM. MAINTENAN - [SDR CHQA201100255](https://openairdocs.org/sdr/CHQA201100255), Jun 11, 2011: FRAME. CORRODED. DURING INSPECTION, SURFACE CORROSION WAS FOUND ON THE LEFT WINDSHIELD AIRCRAFT FRAME ON THE LOWER OUTBOARD SIDE AROUND THE DOME NUT. MAINTENANCE REPAIRED THE LE - [SDR CHQA201100254](https://openairdocs.org/sdr/CHQA201100254), Jun 11, 2011: FLOOR SUPPORT. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE RIGHT OMEGA BEAM FLANGE ANGLE AT FR 47. MAINTENANCE REPAIRED THE RIGHT OMEGA BEAM FLANGE ANGLE AT FR47 IN ACCORDANCE - [SDR CHQA201100252](https://openairdocs.org/sdr/CHQA201100252), Jun 11, 2011: FLOOR SUPPORT. CRACKED. DURING INSPECTION A CRACK WAS FOUND ON THE LEFT OMEGA BEAM FLANGE ANGLE AT FR47. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM FLANGE ANGLE AT FR47 IN ACCORDANCE WIT - [SDR CHQA201100251](https://openairdocs.org/sdr/CHQA201100251), Jun 11, 2011: FLOOR SUPPORT. CRACKED. DURING INSPECTION A CRACK WAS FOUND ON THE MID OMEGA BEAM FLANGE ANGLE AT FR47. MAINTENANCE REPAIRED THE MID OMEGA BEAM FLANGE ANGLE AT FR47 IN ACCORDANCE WITH - [SDR CHQA201100050](https://openairdocs.org/sdr/CHQA201100050), Mar 7, 2011: CHECK VALVE. DAMAGED. FLT CREW REPORTED WHILE CLIMBING THROUGH FL270, RECEIVED A "CABIN" AURAL WARNING. NO RELATED EICAS MESSAGES DISPLAYED. CABIN PRESSURE INDICATED OVER 10,000FT & - [SDR CHQA201000174](https://openairdocs.org/sdr/CHQA201000174), Sep 1, 2010: LIGHT. INOPERATIVE. DURING INSPECTION, TWO FLOOR PROXIMITY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. THE FLOOR PROXIMITY LIGHTS WERE REPLACED WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA200900220](https://openairdocs.org/sdr/CHQA200900220), Oct 12, 2009: CONNECTOR. BROKEN. DURING INSPECTION THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOP. MAINTENANCE FOUND A BROKEN WIRE AT THE OVERWING LAMP RECEPTACLE. THE CONNECTOR WAS RE - [SDR CHQA200800194](https://openairdocs.org/sdr/CHQA200800194), Oct 5, 2008: CONNECTOR. LOOSE. MAINTENANCE FOUND THE BACK SIDE OF THE CENTER AISLE EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE DURING TEST. MAINTENANCE RESET THE CONNECTOR ON THE LIGHT AND THE S - [SDR CHQA200500204](https://openairdocs.org/sdr/CHQA200500204), Dec 2, 2005: SMOKE. DETECTED. TOOK OFF FROM DCA WITH NO PROBLEMS. AT 1500 FT, BROUGHT FLAPS UP AND WENT TO CLIMB THRUST, NOTICED COCKPIT SEEMED A LITTLE HAZY. F/O OFFICER NOTICED HAZE. HAZE - [SDR CHQA200500205](https://openairdocs.org/sdr/CHQA200500205), Dec 2, 2005: LIGHT. BURNED OUT. EMERGENCY FLOOR LIGHT STRIP THIRD BACK INOPERATIVE. REMOVED AND REPLACED FLOOR LIGHT STRIP IAW MM 33-60-00. NO FURTHER DEFECTS NOTED. - [SDR CHQA200500067](https://openairdocs.org/sdr/CHQA200500067), Mar 30, 2005: WIRE. BROKEN. EMERGENCY EXIT LIGHT IDENTIFIER IS INOPERATIVE. TROUBLESHOT PROBLEM TO A BROKEN WIRE AT W192-8588-22 PRIOR TO SPLICE SP9048 REF EMB AWM 33-50-50. REQUIRED REWIR - [SDR CHQA200500024](https://openairdocs.org/sdr/CHQA200500024), Jan 31, 2005: CARBON SEAL. LEAKING. FLIGHT 3217 - LGA-PHL - WHILE EN ROUTE A LAV SMOKE MASTER WARNING APPEARED ON EICAS. THE APPROPRIATE QRH CHECKLIST WAS COMPLETED. THE FLIGHT ATTENDANT CHECKED T - [SDR CHQA200500021](https://openairdocs.org/sdr/CHQA200500021), Jan 28, 2005: SMOKE DETECTOR. MALFUNCTIONED. FLIGHT 3083 - ROC-DCA - AFTER BOARDING THE AIRCRAFT TAXIED TO THE DEICE PAD FOR DEICING. AFTER THREE MINUTES THE BLEEDS AND PACKS WERE TURNED ON AND THE AIRCRAF - [SDR CHQA200500018](https://openairdocs.org/sdr/CHQA200500018), Jan 25, 2004: CARBON SEAL. LEAKING. FLIGHT 3063 - LGA-SYR - EN ROUTE TO SYR A SMELL OF BURNING PLASTIC OR AN ELECTRICAL FIRE WAS NOTED IN THE COCKPIT AND CABIN. THE ODOR MADE EYES WATER AND THROAT ## 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 20010306002919I](https://openairdocs.org/incident/20010306002919I), Mar 6, 2001: Emb EMB145LR (N268SK), Washington, DC, Minor damage. (-23)At 0436Z, 03/07/2001, chautauqua flight (us air) 4873 from lga to iad, an Embraer 145 N268SK, declared a smoke in the cockpit emergency and landed at iad… --- 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.