# N265SK: 2000 Embraer EMB-145, registration cancelled 2018-09-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 8, 2018 - Status when cancelled: Valid registration - Airframe: [Embraer EMB-145](https://openairdocs.org/model/embraer-emb-145) (registry code 3260210) - 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: 145226 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 25, 2000 - Certificate issued: June 27, 2000 - Last registry action: May 7, 2018 - Mode S code: A2932A - 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/N265SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=265SK - Page: https://openairdocs.org/deregistered/N265SK-2018-09-08 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-145: https://openairdocs.org/model/embraer-emb-145.md ## Service difficulty reports (77, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UHLA2015040200327](https://openairdocs.org/sdr/UHLA2015040200327), Apr 2, 2015: ATTACH FITTING. DAMAGED. DURING INSPECTION, ON THE LT WING, THE OTBD FLAP ROLLER ATTACHMENT ON THE RIB INBD SIDE WAS FOUND TO BE DAMAGED. THE FLAP ROLLER ATTACHMENT WAS REPAIRED IAW ETD - [SDR UHLA2015032700316](https://openairdocs.org/sdr/UHLA2015032700316), Mar 27, 2015: TRACK. CORRODED. DURING INSPECTION, THE LT UPPER HALF BEARING TRACK ON THE NLG LEG WAS FOUND TO BE CORRODED. THE BEARING TRACK WAS REPAIRED IAW ETD2015-145-030179. - [SDR UHLA2015032200326](https://openairdocs.org/sdr/UHLA2015032200326), Mar 26, 2015: SKIN. DAMAGED. DURING INSPECTION, DAMAGE ON THE RUDDER 2, LT LOWER SKIN WAS REPAIRED IAWETD 2015-145-030496-B. - [SDR UHLA2015032600325](https://openairdocs.org/sdr/UHLA2015032600325), Mar 26, 2015: FRAME. CRACKED. DURING INSPECTION, A CRACK WAS FOUND AT FRAME 75 AND STRINGERS 2R AND 2L. THE CRACK WAS REPAIRED IAW ETD 2015-145-029344. - [SDR UHLA2015032500315](https://openairdocs.org/sdr/UHLA2015032500315), Mar 25, 2015: TRACK. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RT UPPER HALF BEARING TRACK OF THE NLG LEG. THE BEARING TRACK WAS REPAIRED IAW ETD2015-145-030179. - [SDR UHLA2015032400322](https://openairdocs.org/sdr/UHLA2015032400322), Mar 24, 2015: FRAME. CRACKED. DURING INSPECITON, A CRACK WAS FOUND ON THE LT FLANGE AT FRAME 67. THE AREA WAS REPAIRED IAW ETD2015-145-028481, REV A. - [SDR UHLA2015032400321](https://openairdocs.org/sdr/UHLA2015032400321), Mar 24, 2015: FRAME. CRACKED. DURING INSPECTION, THE LT REAR FUSELAGE, END FRAME 66, AT THE LOWER BEAM, WAS FOUND TO BE CRACKED. THE BEAM WAS REPAIRED IAW ETD2015-145-028481, REV A. - [SDR UHLA2015032300314](https://openairdocs.org/sdr/UHLA2015032300314), Mar 23, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RT REAR FUSELAGE SILL BETWEEN FRAME 71 AND FRAME 73. THE SILL WAS REPLACED IAW SRM 51-40-03. - [SDR UHLA2015032300313](https://openairdocs.org/sdr/UHLA2015032300313), Mar 23, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE RT REAR FUSELAGE SILL WAS FOUND TO BE CORRODED BETWEEN FRAME 65 AND FRAME 68. THE SILL WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015032300312](https://openairdocs.org/sdr/UHLA2015032300312), Mar 23, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE CENTER FUSELAGE III LT FLOOR STRUCTURE SILL NR 6 WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015032300311](https://openairdocs.org/sdr/UHLA2015032300311), Mar 23, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE CENTER FUSELAGE IV LT FLOOR STRUCTURE SILL NR 7 WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED AND INSTALLED WITH SOLID RIVETS IAW SRM 5 - [SDR UHLA2015032100318](https://openairdocs.org/sdr/UHLA2015032100318), Mar 21, 2015: MOUNT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE FORWARD RT GALLEY FITTING INBD AND OTBD. THE INBD AND OTBD RT GALLEY FLOOR FITTINGS WERE REPLACED IAW AMM 20-10-01 - [SDR UHLA2015032100317](https://openairdocs.org/sdr/UHLA2015032100317), Mar 21, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, THE EMERGENCY EQUIPMENT STOWAGE SEAT TRACK FITTING WAS FOUND TO BE CORRODED. THE FITTING WAS REPLACED IAW AMM 25-26-03. - [SDR UHLA2015032100310](https://openairdocs.org/sdr/UHLA2015032100310), Mar 21, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE IV RT FLOOR STRUCTURE SILL NR 6. THE SILL WAS REPLACED AND INSTALLED WITH SOLID RIVETS IAW SRM 51- - [SDR UHLA2015032100309](https://openairdocs.org/sdr/UHLA2015032100309), Mar 21, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE III RT FLOOR STRUCTURE SILL NR 5. THE SILL WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015032100308](https://openairdocs.org/sdr/UHLA2015032100308), Mar 21, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE III RT FLOOR STRUCTURE SILL NR 4. THE SILL WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015032100307](https://openairdocs.org/sdr/UHLA2015032100307), Mar 21, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE III RT FLOOR STRUCTURE SILL NR 3. THE SILL WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015032100306](https://openairdocs.org/sdr/UHLA2015032100306), Mar 21, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE II RT FLOOR STRUCTURE SILL NR 2. THE SILL WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015032100305](https://openairdocs.org/sdr/UHLA2015032100305), Mar 21, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE II RT FLOOR STRUCTURE SILL NR 1. THE SILL WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015032100304](https://openairdocs.org/sdr/UHLA2015032100304), Mar 21, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE III RT FLOOR STRUCTURE GUSSET NR 5. THE GUSSET WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015032100303](https://openairdocs.org/sdr/UHLA2015032100303), Mar 21, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RT FLOOR STRUCTURE GUSSET NR 2. THE GUSSET WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015032100302](https://openairdocs.org/sdr/UHLA2015032100302), Mar 21, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE II LT FLOOR STRUCTURE GUSSET NR 3. THE GUSSET WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015032100301](https://openairdocs.org/sdr/UHLA2015032100301), Mar 21, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE CENTER FUSELAGE 2 LT FLOOR STRUCTURE NR 2 WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015032100300](https://openairdocs.org/sdr/UHLA2015032100300), Mar 21, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, THE RT OTBD SEAT TRACK NR 4 WAS FOUND TO BE CORRODED FROM FRAME 47 TO FRAME 52. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06. - [SDR UHLA2015032100299](https://openairdocs.org/sdr/UHLA2015032100299), Mar 21, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, THE RT OTBD SEAT TRACK NR 3 WAS FOUND TO BE CORRODED FROM FRAME 35 TO FRAME 47. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06. - [SDR UHLA2015032100298](https://openairdocs.org/sdr/UHLA2015032100298), Mar 21, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, THE RT INBD SEAT TRACK NR 4 WAS FOUND TO BE CORRODED FROM FRAME 47 TO FRAME 52. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06. - [SDR UHLA2015032100297](https://openairdocs.org/sdr/UHLA2015032100297), Mar 21, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, THE RT INBD SEAT TRACK NR 3 WAS FOUND TO BE CORRODED FROM FRAME 35 TO FRAME 47. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06. - [SDR UHLA2015032100296](https://openairdocs.org/sdr/UHLA2015032100296), Mar 21, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, THE RT INBD SEAT TRACK NR 2 WAS FOUND TO BE CORRODED FROM FRAME 30 TO FRAME 35. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06. - [SDR UHLA2015032100295](https://openairdocs.org/sdr/UHLA2015032100295), Mar 21, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, THE RT INBD SEAT TRACK NR 1 WAS FOUND TO BE CORRODED FROM FRAME 24 TO FRAME 30. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06. - [SDR UHLA2015032100294](https://openairdocs.org/sdr/UHLA2015032100294), Mar 21, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, THE LT OTBD SEAT TRACK NR 5 WAS FOUND TO BE CORRODED FROM FRAME 47 TO FRAME 52. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06. - [SDR UHLA2015032100293](https://openairdocs.org/sdr/UHLA2015032100293), Mar 21, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, THE LT INBD SEAT TRACK NR 4 WAS FOUND TO BE CORRODED FROM FRAME 35 TO FRAME 47. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06. - [SDR UHLA2015032100292](https://openairdocs.org/sdr/UHLA2015032100292), Mar 21, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, THE LT INBD SEAT TRACK NR 3 WAS FOUND TO BE CORRODED FROM FRAME 30 TO FRAME 35. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06. - [SDR UHLA2015032100291](https://openairdocs.org/sdr/UHLA2015032100291), Mar 21, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, THE LT INBD SEAT TRACK NR 2 WAS FOUND TO BE CORRODED FROM FRAME 24 TO FRAME 30. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06. - [SDR UHLA2015032100290](https://openairdocs.org/sdr/UHLA2015032100290), Mar 21, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, THE LT INBD SEAT TRACK NR 1 WAS FOUND TO BE CORRODED FROM FRAME 18 TO FRAME 24. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06. - [SDR UHLA2015032000320](https://openairdocs.org/sdr/UHLA2015032000320), Mar 20, 2015: STRUCTURE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE BAGGAGE DOOR LOWER L-SHAPE AT FRAME 65 - 68. THE L-SHAPE WAS REPAIRED IAW ETD2015-145-032521. - [SDR UHLA2015032000319](https://openairdocs.org/sdr/UHLA2015032000319), Mar 20, 2015: BEAM. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE BAGGAGE DOOR LOWER BEAM. THE BEAM WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015032000289](https://openairdocs.org/sdr/UHLA2015032000289), Mar 20, 2015: STRUCTURE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE I FLOOR STRUCTURE RIGHT HAND MIDDLE BEAM AT FRAME 23. THE BEAM WAS REPAIRED IAW ETD2015-145-028592 - [SDR UHLA2015032000288](https://openairdocs.org/sdr/UHLA2015032000288), Mar 20, 2015: CHANNEL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRANCE DOOR FLOOR STRUCTURE FORWARD AND AFT OF THE U-SHAPE. THE FORWARD AND AFT U-SHAPE WERE REPLACED IAW S - [SDR UHLA2015032000287](https://openairdocs.org/sdr/UHLA2015032000287), Mar 20, 2015: DOUBLER. CORRODED. DURING INSPECTION, THE CENTER FUSELAGE I FLOOR STRUCTURE RIGHT HAND BEAM DOUBLER AT FRAME 22 WAS FOUND TO BE CORRODED. THE DOUBLER WAS REPLACED IAW SRM 51-40-02 - [SDR UHLA2015032000286](https://openairdocs.org/sdr/UHLA2015032000286), Mar 20, 2015: CHANNEL. CORRODED. DURING INSPECTION, THE CENTER FUSELAGE I, SERVICE DOOR BOTTOM CHANNEL WAS FOUND TO BE CORRODED. THE CHANNEL WAS REPAIRED IAW SRM 53-21-02. - [SDR UHLA2015032000285](https://openairdocs.org/sdr/UHLA2015032000285), Mar 20, 2015: FITTING. CORRODED. DURING INSPECTION, THE TOILET WASTE VALVE WAS FOUND TO BE CORRODED AROUND THE FITTING. THE FITTING WAS REPLACED IAW AMM 38-32-04 AND SRM 51-40-02. - [SDR UHLA2015031900324](https://openairdocs.org/sdr/UHLA2015031900324), Mar 19, 2015: FRAME. CRACKED. DURING INSPECTION, THE LT AND RT HAND FRAME 10 WERE FOUND TO BE CRACKED. THE LT AND RT FRAME 10 WERE REPLACED IAW SRM 51-40-02. - [SDR UHLA2015031900323](https://openairdocs.org/sdr/UHLA2015031900323), Mar 19, 2015: SKIN. LOOSE. DURING INSPECTION, LOOSE RIVETS WERE FOUND ON THE LT AND RT FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 3L-8L AND 3R-8R. THE SKIN WAS REPAIRED IAW ETD 2015-1450 - [SDR CHQA20140808239](https://openairdocs.org/sdr/CHQA20140808239), Aug 8, 2014: LIGHT. DISCONNECTED. DURING INSPECTION THE EMER FLOOR PROXIMITY STRIP WAS FOUND TO BE INOPERATIVE AT ROW 6. THE EMER LIGHT FLOOR STRIP WAS DEFERRED. THE DEFERRAL WAS CLEARED IN 8/8/ - [SDR CHQA20140125022](https://openairdocs.org/sdr/CHQA20140125022), Jan 25, 2014: BATTERY. DISCHARGED. CREW REPORTED THAT DURING PREFLIGHT INSPECTION, THE EMERGENCY LIGHTS AT ROW 8 WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATION - [SDR CHQA20130614207](https://openairdocs.org/sdr/CHQA20130614207), Jun 14, 2013: LIGHT. INOPERATIVE. DURING INSPECTION, THE AFT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX PERFORMED AN ADJUSTMENT OF THE LIGHT AFTER WHICH ALL OPS CHECKS WERE SUCCESSF - [SDR CHQA20130614206](https://openairdocs.org/sdr/CHQA20130614206), Jun 14, 2013: LIGHT. INOPERATIVE. DURING INSPECTION, THE LEFT EMERGENCY EXIT SIDEWALL LIGHT WAS FOUND TO BE INOPERATIVE. MX PERFORMED AN ADJUSTMENT OF THE LIGHT. OPS CHECKED SUCCESSFUL. - [SDR CHQA20130327096](https://openairdocs.org/sdr/CHQA20130327096), Mar 27, 2013: PDU. FAILED. CREW REPORTED THAT THEY RECEIVED A FLAP FAIL MESSAGE ON THE FINAL APPROACH WITH FLAP CHANNEL 2 ON MEL. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO KJFK. THE - [SDR CHQA201100378](https://openairdocs.org/sdr/CHQA201100378), Sep 21, 2011: INVERTER. INOPERATIVE. DURING INSPECTION, THE FORWARD SIDE OF THE EXIT LOCATOR, AT THE EXIT ROW, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE AC TO DC INVERTER. OPERATIONAL C - [SDR CHQA201100141](https://openairdocs.org/sdr/CHQA201100141), Apr 19, 2011: COMPUTER. INOPERATIVE. CREW REPORTED GPWS FAIL, TERRAIN INOP, AND RADIO ALTIMETER 1 FAIL MESSAGES AND DIVERTED TO CMH DUE TO WEATHER WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTE All 77: https://openairdocs.org/deregistered/N265SK-2018-09-08/reports.md ## FAA accident and incident reports (2) 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 20020131001039I](https://openairdocs.org/incident/20020131001039I), Jan 31, 2002: Emb EMB145 (N265SK), Boston, MA. (-23) On climb out, aircraft N265SK, Emb-145-145, s/n 145226, went into an uncontrollable vertical climb. Aircraft pitched up to 6300 ft. with run-away trim.… - [Incident 20000713035089I](https://openairdocs.org/incident/20000713035089I), Jul 13, 2000: Emb EMB145 (N265SK), Pittsburgh, PA. (-23)On July 13, 2000, at 1035E, chqa flight 4870, an Emb-145, registered as N265SK, S/N145-226, diverted to "pit" after the "in flight" shutdown of the #1… --- 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.